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AIRPORT PLANNING MANUAL
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AIRPORT PLANNING MANUAL
1 2 3 4 AIRPORT PLANNING MANUAL
AIRPORT PLANNING MANUAL LIST OF EFFECTIVE PAGES
Chapter Page Date Chapter Page Date 32 * Dec 05/2014 Effective Pages 1 * Dec 05/2014 33 * Dec 05/2014 2 * Dec 05/2014 34 * Dec 05/2014 35 * Dec 05/2014 Contents 1 * Dec 05/2014 36 * Dec 05/2014 2 * Dec 05/2014 37 * Dec 05/2014 3 * Dec 05/2014 38 * Dec 05/2014 4 * Dec 05/2014 39 * Dec 05/2014 5 * Dec 05/2014 40 * Dec 05/2014 6 * Dec 05/2014 41 * Dec 05/2014 42 * Dec 05/2014 Chapter 1 1 * Dec 05/2014 43 * Dec 05/2014 2 May 28/2001 44 * Dec 05/2014
Chapter 2 1 * Dec 05/2014 Chapter 3 1 May 28/2001 2 * Dec 05/2014 2 May 28/2001 3 * Dec 05/2014 3 May 28/2001 4 * Dec 05/2014 4 May 28/2001 5 * Dec 05/2014 5 May 28/2001 6 * Dec 05/2014 6 May 28/2001 7 * Dec 05/2014 7 May 28/2001 8 * Dec 05/2014 8 May 28/2001 9 * Dec 05/2014 9 May 28/2001 10 * Dec 05/2014 10 May 28/2001 11 * Dec 05/2014 11 May 28/2001 12 * Dec 05/2014 12 May 28/2001 13 * Dec 05/2014 13 May 28/2001 14 * Dec 05/2014 14 May 28/2001 15 * Dec 05/2014 15 May 28/2001 16 * Dec 05/2014 16 May 28/2001 17 * Dec 05/2014 18 * Dec 05/2014 Chapter 4 1 May 28/2001 19 * Dec 05/2014 2 May 28/2001 20 * Dec 05/2014 3 May 28/2001 21 * Dec 05/2014 4 May 28/2001 22 * Dec 05/2014 5 May 28/2001 23 * Dec 05/2014 6 May 28/2001 24 * Dec 05/2014 7 May 28/2001 25 * Dec 05/2014 8 May 28/2001 26 * Dec 05/2014 9 * Dec 05/2014 27 * Dec 05/2014 10 May 28/2001 28 * Dec 05/2014 29 * Dec 05/2014 Chapter 5 1 * Dec 05/2014 30 * Dec 05/2014 2 * Dec 05/2014 31 * Dec 05/2014 3 * Dec 05/2014
The asterisk (*) indicates pages revised, added or deleted by current revision.
Series: 400
EFFECTIVE Page 1 PAGES Dec 05/2014 AIRPORT PLANNING MANUAL Chapter Page Date Chapter Page Date 4 * Dec 05/2014 4 * Dec 05/2014 5 * Dec 05/2014 6 * Dec 05/2014 7 * Dec 05/2014 8 * Dec 05/2014 9 * Dec 05/2014 10 * Dec 05/2014 11 * Dec 05/2014 12 * Dec 05/2014 13 * Dec 05/2014 14 * Dec 05/2014 15 * Dec 05/2014 16 * Dec 05/2014
Chapter 6 1 * Dec 05/2014 2 * Dec 05/2014 3 * Dec 05/2014 4 * Dec 05/2014 5 * Dec 05/2014 6 May 28/2001 7 * Dec 05/2014 8 May 28/2001 9 May 28/2001 10 * Dec 05/2014 11 * Dec 05/2014 12 * Dec 05/2014
Chapter 7 1 May 28/2001 2 May 28/2001 3 May 28/2001 4 May 28/2001 5 May 28/2001 6 May 28/2001 7 May 28/2001 8 May 28/2001 9 May 28/2001 10 May 28/2001 11 May 28/2001 12 May 28/2001 13 May 28/2001 14 May 28/2001
Chapter 8 1 May 28/2001
Chapter 9 1 May 28/2001 2 * Dec 05/2014 3 * Dec 05/2014
The asterisk (*) indicates pages revised, added or deleted by current revision.
Series: 400
EFFECTIVE Page 2 PAGES Dec 05/2014 AIRPORT PLANNING MANUAL TABLE OF CONTENTS Title Page CHAPTER 1 PREFACE Scope 1
Series: 400
Page 1 CONTENTS Dec 05/2014 AIRPORT PLANNING MANUAL Title Page CHAPTER 2 AIRCRAFT DESCRIPTION General Information 1 General Airplane Characteristics 3 Aircraft Dimensions 5 Ground Clearances − General Arrangement 6 Maximum Ground Clearances−Standard MLG Tires 7 Minimum Ground Clearances−Standard MLG Tires 8 Maximum Ground Clearances−Optional MLG Tires 9 Minimum Ground Clearances−Optional MLG Tires 10 Series 400 (Model 402) Standard Interior Configuration 11 Series 400 (Model 402) Optional Interior Configuration 14 Passenger − Compartment Cross Section 19 Floor loading diagram 21 FWD Baggage − Compartment Dimensions (Standard 23 Interior Configuration) AFT Baggage Compartment Dimensions (Standard 24 Interior Configuration) AFT Baggage Compartment Dimensions (Optional Interior 25 Configuration) Nets and Tiedowns (Standard Interior Configuration) 26 Nets and Tiedowns (Optional Interior Configuration) 27 Door Clearances 28 Forward Passenger − Door Clearances 29 Aft Passenger − Door Clearances 30 Aft Service − Door Clearances 32 Forward Baggage Compartment / Forward Type I 34 Emergency Exit − Door Clearances Aft Baggage−Compartment − Door Clearances 36 Exterior Handles 38 Minimum Clearance Between Nacelles and Fuselage 40 Aft Baggage Compartment Vertical Dimensions (Typical 41 Configuration) Ground Clearances − Empennage and Sill of Aft Baggage 42 Door
Series: 400
Page 2 CONTENTS Dec 05/2014 AIRPORT PLANNING MANUAL Title Page CHAPTER 3 AIRCRAFT PERFORMANCE General Information 1 Payload/Range at Maximum Cruise Rating and Long 3 Range Cruise Maximum Permissible Take−Off Weight (Wat Limit) − 4 Flaps 5 Degrees Maximum Permissible Take−Off Weight (Wat Limit) − 5 Flaps 10 Degrees Maximum Permissible Take−Off Weight (Wat Limit) − 6 Flaps 15 Degrees Take−Off Runway Length Requirements − Flaps 5 7 Degrees Take−Off Runway Length Requirements − Flaps 10 8 Degrees Take−Off Runway Length Requirements − Flaps 15 9 Degrees Max. Landing Weight − Landing Flaps 10 and Approach 10 Flaps 5 Degrees Max. Landing Weight − Landing Flaps 15 and Approach 11 Flaps 10 Degrees Max. Landing Weight − Landing Flaps 35 and Approach 12 Flaps 15 Degrees Unfactored Landing Distance − Flaps 10 Degrees 13 Unfactored Landing Distance − Flaps 15 Degrees 14 Unfactored Landing Distance − Flaps 35 Degrees 15 Landing − Runway Length Required 16
Series: 400
Page 3 CONTENTS Dec 05/2014 AIRPORT PLANNING MANUAL Title Page CHAPTER 4 GROUND MANEUVERING General Information 1 Turning Radii (No Slip Angle) 2 Turning Radii Data (No Slip Angle) 3 Turning Radius at Minimum Power 4 Greater Than 90 Degree Turn − Runway to Taxiway with 5 Tracks 90 Degree Turn − Runway to Taxiway with Nose Gear 6 and Cockpit Tracks 90 Degree Turn − Taxiway to Taxiway with Nose Gear 7 and Cockpit Tracks Runway Holding Bay (Apron) 8 Aircraft Tie Down Provisions 9
CHAPTER 5 TERMINAL SERVICING General Information 1 Aircraft Servicing Arrangement (Typical − No APU) 2 Rapid Turnaround Using FWD and AFT Doors 5 Rapid Turnaround Using FWD Door Only 6 Ground Servicing Point Locations 7 Ground Service Connections Data 11 Electrical Requirements For Engine Starting 14 Ground Towing Requirements 15 Ground Air Conditioning Requirements − Pre−Conditioned 16 Airplane
Series: 400
Page 4 CONTENTS Dec 05/2014 AIRPORT PLANNING MANUAL Title Page CHAPTER 6 OPERATING CONDITIONS AND NOISE DATA General Information 1 Engine Exhaust Temp. Contours at Ground Idle − Top 2 View Engine Exhaust Temp. Contours at Ground Idle − Side 3 View Engine Exhaust Temp. Contours at Flight Idle − Top View 4 Engine Exhaust Temp. Contours at Flight Idle − Side View 5 Engine Exhaust Temp. Contours at Max. T.O. Power − 6 Top View Engine Exhaust Temp. Contours at Max. T.O. Power − 7 Side View Takeoff and Landing Noise Footprint − 3 Degree 8 Approach Takeoff and Landing Noise Footprint − 4 Degrees 9 Approach Ramp Noise Test Results for Optional APU 10 Propeller Slipstream Velocity Contours at Max Takeoff 11 Power Propeller Slipstream Velocity Contours on Ground 12
Series: 400
Page 5 CONTENTS Dec 05/2014 AIRPORT PLANNING MANUAL Title Page CHAPTER 7 PAVEMENT DATA General Information 1 Landing Gear Footprint 2 Maximum Pavement Loads 3 Landing Gear Loading on Pavement 4 Flexible Pavement Requirements − CBR (32x8.8−16 5 Tires) Flexible Pavement Requirements − CBR (34x10.75−16 6 Tires) Flexible Pavement Requirements − LCN Conversion 7 (32x8.8−16 Tires) Flexible Pavement Requirements − LCN Conversion 8 (34x10.75−16 Tires) Rigid Pavement Requirements − LCN Conversion 9 (32x8.8−16 Tires) Rigid Pavement Requirements − LCN Conversion 10 (34x10.75−16 Tires) Aircraft Classification Number − Flexible Pavement 11 (32x8.8−16 Tires) Aircraft Classification Number − Flexible Pavement 12 (34x10.75−16 Tires) Aircraft Classification Number − Rigid Pavement (32x8.8− 13 16 Tires) Aircraft Classification Number − Rigid pavement 14 (34x10.75−16 Tires)
CHAPTER 8 DERIVATIVE AIRCRAFT General Information 1
CHAPTER 9 SCALED DRAWINGS OF DASH−8 SERIES 400 General Information 1 Scaled Dash 8, Series 400 (Model 402) Drawing − 1 in. = 2 32 ft (1:384) Scaled (Model 402) Drawing − 1in. = 50 ft (1:600), 1in. = 3 100 ft (1:1200) Scaled Dash 8, Series 400 (Model 402) Drawing − 1:500 4 and 1:1000 (Metric)
Series: 400
Page 6 CONTENTS Dec 05/2014 CHAPTER 1
PREFACE AIRPORT PLANNING MANUAL
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Scope
1. Purpose A. This manual provides, in a standardized format, airport planning data for the Dash−8, Series 400 (Model 402). Because operational procedures are different for each airline and operator, the airport planner must coordinate specific data with the user airline before the design of facilities. B. The data contained in Chapter 3 (Aircraft Performance) is for reference only. Refer to the applicable Aircraft Flight Manual (AFM) for Model 402 operating−data. 2. Introduction A. The content of this document conforms to NAS 3601, Revision 6 (15 Jul/94). NAS 3601 is the result of agreements between representatives of the organizations that follow:
– Aerospace industries – Airport operators – Air Transport Association of America – International Air Transport Association. B. This manual provides Model 402 data for airport planners and operators, airlines, architectural and engineering consultant organizations (as well as other interested industry agencies). The content of this manual will change as options and aircraft changes occur. The data contained in this manual represents the typical Dash−8 Series 400 (Model 402) aircraft. C. For more information, contact: Director, Technical Publications Regional Aircraft Division Bombardier Aerospace Mail Stop N42−25 123 Garratt Blvd., Downsview Ontario, Canada M3K 1Y5. 3. A Brief Description of the Dash−8 Series 400 (Model 402) Aircraft A. The Dash−8 Series 400 (Model 402) is a pressurized, commercial transport airplane that is designed to accommodate 70 to 86 passengers. This airplane establishes new standards in speed, comfort and efficiency. A new feature of the Dash−8 series is the Noise and Vibration Suppression (NVS) system, which dramatically reduces cabin noise in flight.
Series: 400
Page 1 CHAPTER 1 Dec 05/2014 AIRPORT PLANNING MANUAL B. The aircraft is powered by two Pratt and Whitney PW150A turboprop engines. Large diameter, slow−turning, six−bladed Dowty R408 propellers provide high thrust efficiency and low noise levels. C. The Dash−8 Series 400 is capable of economic operations over a broad range of applications. These are:
– Scheduled airline operations – Resource and regional development work – Corporate and military transport roles. D. The aircraft is capable of operation in ambient temperatures of between −65 °F (−54 °C) and 122 °F and (50 °C), unless otherwise specified. Transfer from one climate to another can be done without penalties or extensive modifications or adjustment. E. Significant features of interest to the airport planner include the items that follow:
– The engines are located high and on the wing – The horizontal stabilizer is located on top of the fin – The aircraft has a self−contained airstair entry−door at the forward end of the cabin – Connections for single−point and overwing gravity refueling are provided – All servicing can be accomplished with standard ground equipment – High exhaust outlets produce modest pressure and temperature profiles.
Series: 400
Page 2 CHAPTER 1 May 28/2001 CHAPTER 2
AIRCRAFT DESCRIPTION AIRPORT PLANNING MANUAL
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General Information
1. General The Model 402 has a maximum take−off weight of up to 64,500 lb (29,257 kg). Other maximum weight parameters such as taxi weight (also known as ramp weight), landing weight and zero fuel weight are set accordingly. 2. Contents of Chapter This chapter contains the items that follow: A. General airplane characteristics and dimensions are shown in Figure 2−1 and Figure 2−2. B. Ground clearances are shown in Figure 2−3, Figure 2−4, Figure 2−5, Figure 2−6 and Figure 2−7. C. Interior configurations are shown in Figure 2−8, Figure 2−9, Figure 2−10. D. A cross−section of the passenger compartment is shown in Figure 2−11. E. A floor loading diagram is shown in Figure 2−12. F. Dimensions of the forward and aft baggage compartments are shown in Figure 2−13, Figure 2−14, and Figure 2−15. G. Nets and tiedowns of the aft baggage compartment are shown in Figure 2−16 and Figure 2−17. H. Clearances for the passenger, the service, the baggage and the forward type I emergency exit doors are shown in Figure 2−18, Figure 2−19, Figure 2−20, Figure 2−21, and Figure 2−22. I. External handles of the various doors are shown in Figure 2−23. J. Horizontal clearances between the fuselage and nacelles are shown in Figure 2−24. K. Vertical dimensions of a typical aft baggage compartment is shown in Figure 2−25. L. Ground clearances of empennage and sill of aft baggage door is shown in Figure 2−26. 3. Definitions The definitions that follow are used throughout this manual (refer to Figure 2−1): A. Maximum Design Taxi Weight (MTW) This is the maximum weight at which an aircraft can move safely on the ground. It includes the fuel for those displacements and the takeoff run. B. Maximum Design Landing Weight (MLW) This is the maximum approved weight at which an aircraft can land.
Series: 400
Page 1 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL C. Maximum Design Take−off Weight (MTOW) This is the maximum approved weight at which an aircraft can start a take−off run. D. Operational Weight Empty (OWE) This is the weight of structure, power plant, furnishings, systems, unusable fuel and other items of equipment that are a necessary part of an aircraft configuration. The OWE also includes certain standard items, personnel, equipment and supplies required for full operations, but does not include usable fuel or payload. E. Maximum Design Zero Fuel Weight (MZFW) This is the maximum weight of an aircraft before the usable fuel is loaded on the aircraft. F. Maximum Payload This is the weight you get when you subtract the OWE from the MZFW. G. Maximum Seating Capacity This is the maximum number of passengers specifically certified or anticipated for certification. H. Maximum Cargo Volume This is the maximum space available for cargo. I. Usable Fuel This is the fuel available for the aircraft engines.
Series: 400
Page 2 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL
BASIC GROSS INTERMEDIATE HIGH GROSS DESCRIPTION WEIGHT GROSS WEIGHT WEIGHT 61,900 lb 64,130 lb 64,700 lb MAXIMUM DESIGN TAXI WEIGHT (28,077 kg) (29,089 kg) (29,347 kg) 61,700 lb 63,930 lb 64,500 lb MAXIMUM DESIGN TAKE−OFF WEIGHT (27,987 kg) (28,998 kg) (29,257 kg) 60,500 lb 61,750 lb 61,750 lb MAXIMUM DESIGN LANDING WEIGHT (27,442 kg) (28,009 kg) (28,009 kg) 55,500 lb 57,000 lb 57,000 lb MAXIMUM DESIGN ZERO FUEL WEIGHT (25,174 kg) (25,855 kg) (25,855 kg)
POWERPLANT
DESCRIPTION WEIGHT (PER SIDE) ENGINE (PWC 150 A, DRESSED, 1925 lb INCLUDING EXHAUST NOZZLE) (873.1 kg) EXHAUST ONLY (JET PIPE) 169.5 lb (76.9 kg) PROPELLERS (DOWTY R408, SIX−BLADE, 555.4 lb INCLUDES BETA TUBE UNIT AND SPINNER) (251.9 kg)
APU DESCRIPTION WEIGHT (PER SIDE) 139.0 lb APU WET (63.0 kg) 40.4 lb STARTER/GENERATOR (18.3 kg)
TANK CAPACITY − USABLE FUEL
STANDARD TANKS US GALS LBS LITRES KG
LEFT 862 5862 3263 2659
RIGHT 862 5862 3263 2659
TOTAL 1724 11724 6526 5318
NOTE BASED ON : 6.8 lb /U.S. GALLON (0.775 kg/l) br838a01.dg, sw/cm, jun19/2013 GENERAL AIRPLANE CHARACTERISTICS (Sheet 1 of 2)
Figure 2 − 1 Series: 400
Page 3 CHAPTER 2 Dec 05/2014 Series: 400 ( +7in.Pallet=61in.)H. 1. Powerplantshippingcratedimensionsare46in.W x108in.L54 NOTES 2. Assemblywheelweighs248.48lbperside(124.24 lbeach). 3. Brakecarbonweighs138.4lbperside(69.2each set). ENGINE (DRY,WITHDRAINSYSTEMINSTALLED) DC STARTERGENERATOR BRUSH BLOCKBRACKET PCU P2.7 HBOVDUCT ENGINE HYDRAULICDRIVEPUMP INTAKE ADAPTERANDV−BANDCLAMP P2.2 HBOVDUCT FUEL ITEMS ENGINE MOUNTSSYSTEM AC GENERATOR EXHAUST NOZZLEASSEMBLY OVERSPEED GOVERNOR AUX PUMPUNIT EEA IPAECAATRSIS(Sheet 2of2) GENERAL AIRPLANECHARACTERISTICS POWER PLANTWEIGHTBREAKDOWNDETAILS DESCRIPTION AIRPORT PLANNINGMANUAL Figure 2−1 CHAPTER 2 DRESSED POWERPLANT WEIGHT PERSIDE(lb) WEIGHT: 1808.6lb 1573.0 16.9 12.0 11.0 76.6 39.3 1.7 6.2 47.0 8.9 8.1 2.1 2.1 3.7 Dec 05/2014 ae4 Page
br838a02.dg, kh, aug05/2013 AIRPORT PLANNING MANUAL 93ft 3in. (28.42m) 30ft 5in. (9.27m) 13ft 6in. (4.11m)
DIHEDRAL 2.5 o
43.31in. (1.10m) 28ft 10in. (8.80m) 36.00 in. (91.44 cm)
36ft 10in. NOTE (11.22m) Refer to Ground Clearance Illustrations.
8ft 2in. (2.48m) 12ft 4in. (3.76m)
45ft 9in. (13.99m)
GROUND REFERENCE LINE 101ft 10in. (31.04m) 107ft 9in.
(32.83m) br245a01.dg, gv, 05/04/01 AIRCRAFT DIMENSIONS
Figure 2 − 2 Series: 400
Page 5 CHAPTER 2 Dec 05/2014 A Series: 400 B E N C P D GROUND CLEARANCES −GENERALARRANGEMENT F M AIRPORT PLANNINGMANUAL H Figure 2−3 CHAPTER 2 Q R G Dec 05/2014 L K ae6 Page J
brc76a01.dg, gg/gv, 05/04/01 Series: 400 5 2. MainWheelTiresare32x8.8−16,inflatedto227 psi(1565kPa)loaded. 1. NoseWheelTires22x6.5−10,inflatedto89psi (614kPa)loaded. 3. Tirepressuresshownareforcalculationpurposes only.RefertoAMMCh.12forservicepressures. NOTES Forward typeIemergency exit doorisinstalledonlyonaircraftwithextracapacity configuration. Type II/IIIemergencyexitdoorisde−activatedforthe extracapacityconfiguration. ITEM ITEM N M N M A A H H G G E B E B C C D R F D R F Q Q K K P P J J L L FORWARD RHTYPEIEXITDOOR FORWARD RHTYPEIEXITDOOR SILL OFFWDBAGGAGEDOOR/ SILL OFFWDBAGGAGEDOOR/ FLIGHT DECK FLIGHT DECK CABIN FLOOR PROP HEIGHTCLEARANCE CABIN FLOOR PROP HEIGHTCLEARANCE HORIZONTAL STABILIZER PROP GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE HORIZONTAL STABILIZER PROP GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE TOP OFFUSELAGE SILL OFSERVICEDOOR/TYPEIEXIT TOP OFFUSELAGE SILL OFAFTPAXDOORTYPEIEXIT SILL OFAIRSTAIRDOOR SILL OFTYPEII/IIIEXIT SILL OFSERVICEDOOR/TYPEIEXIT SILL OFAFTBAGGAGEDOOR SILL OFAIRSTAIRDOOR SILL OFAFTPAXDOORTYPEIEXIT SILL OFTYPEII/IIIEXIT SILL OFAFTBAGGAGEDOOR NACELLE LOWERSURFACE NACELLE LOWERSURFACE VERTICAL STABILIZER VERTICAL STABILIZER MAXIMUM GROUNDCLEARANCES−STANDARD MLGTIRES WING TIP WING TIP HEIGHT HEIGHT AIRPORT PLANNINGMANUAL Figure 2−4 5 5 WEIGHT : WEIGHT : C.G. : C.G. : WT ONNLG: WT ONNLG: 25.67 26.92 25.95 27.23 FEET FEET 17.19 17.14 13.11 13.11 11.47 11.29 MAXIMUM GROUNDCLEARANCE MAXIMUM GROUNDCLEARANCE 4.67 5.16 5.20 4.55 5.08 4.64 4.39 5.32 5.20 4.45 7.14 5.01 4.51 5.58 7.10 5.36 4.73 4.59 2.86 3.05 3.65 3.71 CHAPTER 2 35,387 lb(16,085kg) 35,387 lb(16,085kg) STA. X410.980 STA. X387.160 2190 lb(995kg) 3743 lb(1701kg) METERS METERS 3.99 4.00 1.53 1.57 5.24 5.22 1.55 1.58 0.93 0.87 1.44 1.39 1.37 1.42 1.13 1.36 1.58 1.34 1.40 1.62 7.83 2.18 2.16 1.70 1.63 1.41 3.49 1.11 8.30 3.44 7.91 8.21 Dec 05/2014 ae7 Page
cg3531a01.dg, cs, aug06/2014 Series: 400 1. NoseWheelTires22x6.5−10,inflatedto89psi (614kPa)loaded. 5 3. Tirepressuresshownareforcalculationpurposes only.RefertoAMMCh.12forservicepressures. 2. MainWheelTiresare32x8.8−16,inflatedto227 psi(1565kPa)loaded. Forward typeIemergency exit doorisinstalledonlyonaircraftwithextracapacity configuration. NOTES Type II/IIIemergencyexitdoorisde−activatedforthe extracapacityconfiguration. ITEM ITEM N M A H G E B C D R F Q N M K A P J H L G E B C D R F Q K P J L FLIGHT DECK FORWARD RHTYPEIEXITDOOR CABIN FLOOR PROP HEIGHTCLEARANCE HORIZONTAL STABILIZER PROP GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE SILL OFFWDBAGGAGEDOOR/ MINIMUM GROUNDCLEARANCES−STANDARD MLGTIRES TOP OFFUSELAGE SILL OFSERVICEDOOR/TYPEIEXIT SILL OFAFTPAXDOORTYPEIEXIT SILL OFAIRSTAIRDOOR SILL OFAFTBAGGAGEDOOR SILL OFTYPEII/IIIEXIT NACELLE LOWERSURFACE FLIGHT DECK FORWARD RHTYPEIEXITDOOR VERTICAL STABILIZER CABIN FLOOR PROP HEIGHTCLEARANCE SILL OFFWDBAGGAGEDOOR/ HORIZONTAL STABILIZER PROP GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE WING TIP TOP OFFUSELAGE SILL OFSERVICEDOOR/TYPEIEXIT SILL OFAFTPAXDOORTYPEIEXIT SILL OFAIRSTAIRDOOR SILL OFTYPEII/IIIEXIT SILL OFAFTBAGGAGEDOOR NACELLE LOWERSURFACE VERTICAL STABILIZER WING TIP HEIGHT HEIGHT AIRPORT PLANNINGMANUAL Figure 2−5 5 5 WEIGHT : C.G. : WEIGHT : WT ONNLG: C.G. : WT ONNLG: 25.79 27.09 FEET 12.82 16.82 24.94 26.69 FEET 12.86 10.94 MINIMUM GROUNDCLEARANCE 16.91 11.18 MINIMUM GROUNDCLEARANCE 4.14 4.95 5.09 4.97 4.02 4.07 6.79 3.34 4.24 4.97 2.48 4.37 4.75 4.94 4.25 4.82 4.33 5.27 6.86 4.43 2.75 3.42 CHAPTER 2 64,700 lb(29,347kg) STA. X398.280 6100 lb(2772kg) 64,700 lb(29,347kg) STA. X410.980 3920 lb(1782kg) METERS METERS 5.13 1.52 3.91 1.51 0.76 3.92 1.26 1.24 1.02 1.29 1.45 1.55 1.22 7.86 2.07 5.15 1.47 1.52 8.26 0.84 3.33 1.04 1.29 1.33 1.32 1.35 7.60 2.09 8.14 1.51 1.61 3.41 Dec 05/2014 ae8 Page
cg3532a01.dg, cs, aug06/2014 Series: 400 5 2. MainWheelTiresare34x10.75−16,inflatedto141 psi(972kPa)loaded. 1. NoseWheelTires22x6.5−10,inflatedto89psi (614kPa)loaded. 3. Tirepressuresshownareforcalculationpurposes only.RefertoAMMCh.12forservicepressures. NOTES Forward typeIemergency exit doorisinstalledonlyonaircraftwithextracapacity configuration. Type II/IIIemergencyexitdoorisde−activatedforthe extracapacityconfiguration. ITEM ITEM N N M M A A H H G G E E B B C C D D R R F F Q Q K K P P J J L L FORWARD RHTYPEIEXITDOOR SILL OFFWDBAGGAGEDOOR/ FLIGHT DECK FLIGHT DECK CABIN FLOOR CABIN FLOOR PROP HEIGHTCLEARANCE PROP HEIGHTCLEARANCE FORWARD RHTYPEIEXITDOOR PROP GROUNDCLEARANCE HORIZONTAL STABILIZER PROP GROUNDCLEARANCE HORIZONTAL STABILIZER FUSELAGE GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE TOP OFFUSELAGE TOP OFFUSELAGE SILL OFSERVICEDOOR/TYPEIEXIT SILL OFFWDBAGGAGEDOOR/ SILL OFSERVICEDOOR/TYPEIEXIT SILL OFAIRSTAIRDOOR SILL OFAIRSTAIRDOOR SILL OFAFTPAXDOORTYPEIEXIT SILL OFAFTPAXDOORTYPEIEXIT SILL OFAFTBAGGAGEDOOR SILL OFTYPEII/IIIEXIT SILL OFAFTBAGGAGEDOOR SILL OFTYPEII/IIIEXIT NACELLE LOWERSURFACE NACELLE LOWERSURFACE VERTICAL STABILIZER VERTICAL STABILIZER WING TIP WING TIP MAXIMUM GROUNDCLEARANCES−OPTIONAL MLGTIRES HEIGHT HEIGHT AIRPORT PLANNINGMANUAL Figure 2−6 5 5 WEIGHT : WEIGHT : C.G. : C.G. : WT ONNLG: WT ONNLG: 26.19 27.49 27.18 25.92 FEET FEET 17.28 13.22 13.22 17.22 11.49 MAXIMUM GROUNDCLEARANCE MAXIMUM GROUNDCLEARANCE 11.31 4.70 5.20 4.53 5.35 5.37 5.49 5.37 4.58 5.25 4.47 4.65 5.36 7.18 7.23 3.74 3.79 4.77 5.58 2.87 4.63 3.07 4.41 CHAPTER 2 35,387 lb(16,085kg) 35,387 lb(16,085kg) STA. X387.160 STA. X410.960 2190 lb(995kg) 3743 lb(1701kg) METERS METERS 4.03 4.03 1.58 1.63 5.27 5.25 1.64 1.60 0.94 0.87 1.36 1.14 1.15 1.38 1.64 1.43 1.39 1.34 1.42 1.67 1.45 7.90 7.98 2.20 2.19 1.70 1.63 8.28 8.38 3.50 1.41 3.45 Dec 05/2014 ae9 Page
cg3533a01.dg, cs, aug06/2014 Series: 400 5 2. MainWheelTiresare34x10.75−16,inflatedto141 psi(972kPa)loaded. 1. NoseWheelTires22x6.5−10,inflatedto89psi (614kPa)loaded. 3. Tirepressuresshownareforcalculationpurposes only.RefertoAMMCh.12forservicepressures. NOTES Forward typeIemergency exit doorisinstalledonlyonaircraftwithextracapacity configuration. Type II/IIIemergencyexitdoorisde−activatedforthe extracapacityconfiguration. ITEM ITEM N M N M A A H H G G E B E B C C D R F D R F Q Q K K P P J J L L FORWARD RHTYPEIEXITDOOR SILL OFFWDBAGGAGEDOOR/ FORWARD RHTYPEIEXITDOOR SILL OFFWDBAGGAGEDOOR/ FLIGHT DECK FLIGHT DECK CABIN FLOOR CABIN FLOOR PROP HEIGHTCLEARANCE PROP HEIGHTCLEARANCE HORIZONTAL STABILIZER PROP GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE HORIZONTAL STABILIZER PROP GROUNDCLEARANCE FUSELAGE GROUNDCLEARANCE TOP OFFUSELAGE SILL OFSERVICEDOOR/TYPEIEXIT TOP OFFUSELAGE SILL OFAIRSTAIRDOOR SILL OFSERVICEDOOR/TYPEIEXIT SILL OFAFTPAXDOORTYPEIEXIT SILL OFTYPEII/IIIEXIT SILL OFAFTBAGGAGEDOOR SILL OFAIRSTAIRDOOR SILL OFAFTPAXDOORTYPEIEXIT SILL OFTYPEII/IIIEXIT SILL OFAFTBAGGAGEDOOR NACELLE LOWERSURFACE NACELLE LOWERSURFACE VERTICAL STABILIZER VERTICAL STABILIZER WING TIP WING TIP MINIMUM GROUNDCLEARANCES−OPTIONAL MLGTIRES HEIGHT HEIGHT AIRPORT PLANNINGMANUAL Figure 2−7 5 5 WEIGHT : WEIGHT : C.G. : C.G. : WT ONNLG: WT ONNLG: 25.64 26.90 25.99 FEET FEET 16.97 12.92 16.89 12.92 27.31 11.20 10.93 MINIMUM GROUNDCLEARANCE MINIMUM GROUNDCLEARANCE 4.39 4.16 5.10 5.08 4.96 4.27 4.34 5.23 4.04 4.08 4.91 6.97 4.46 5.27 3.49 6.86 2.85 4.27 4.97 2.49 5.11 3.41 CHAPTER 2 64,700 lb(29,347kg) 64,700 lb(29,347kg) STA. X410.980 STA. X398.280 6100 lb(2772kg) 3920 lb(1782kg) METERS METERS 3.94 3.94 1.50 1.55 5.17 5.15 1.56 0.87 0.76 1.06 1.34 1.04 1.27 1.24 1.36 1.30 1.32 1.55 1.59 1.30 1.23 7.82 7.92 1.51 2.09 2.13 1.52 8.20 8.33 3.33 1.61 3.41 Dec 05/2014 ae10 Page
cg3534a01.dg, cs, aug06/2014 Series: 400
SERIES 400 (TYPE SPECIFICATION MODEL 402) INTERIOR CONFIGURATION 74 SEATS AT 31 INCH (78.74 cm) PITCH EIS40SADR NEIRCNIUAIN (Sheet1of2) SERIES 400STANDARD INTERIORCONFIGURATIONS BAGGAGE DOOR TYPE II/III EXIT 24.00 in. W x 54.00 in. H 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) (51.31 cm x 1.42 m) SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H 5 ft 9 in. (60.96 cm x 1.37 m) (1.75 m) 11.00 ft. (3.35 m)
3 1 6 AIRPORT PLANNINGMANUAL Figure 2−8
4 5 5 2 CHAPTER 2 AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT BAGGAGE DOOR 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H 51.00 in. W x (76.20 cm x 1.65 m) (60.96 cm x 1.65 m) 59.00 in. H (1.30 m x 1.50 m) PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m)
LEGEND 1. Forward baggage compartment 91.00 ft 3 (2.58 m 3 ). NOTE 2. Rear baggage compartment Standard configuration shown. 411.00 ft 33 (11.64 m ). Dec 05/2014 Layout may vary with optional 3. Lavatory. ae11 Page configurations. 4. Wardrobe. 5. Flight attendant. 6. Galley. br195a01.dg, gg/gw, aug5/2008 Series: 400
SERIES 400 (TYPE SPECIFICATION MODEL 401) INTERIOR CONFIGURATION 70 SEATS AT 33 INCH (83.82 cm) PITCH
EIS40SADR NEIRCNIUAIN (Sheet2of2) SERIES 400STANDARD INTERIORCONFIGURATIONS BAGGAGE DOOR TYPE II/III EXIT 24.00 in. W x 54.00 in. H 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) (51.31 cm x 1.42 m) SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H 5 ft 9 in. (60.96 cm x 1.37 m) (1.75 m) 11.00 ft. (3.35 m) 3 1 6 AIRPORT PLANNINGMANUAL Figure 2−8
4 5 5 2 CHAPTER 2 AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT BAGGAGE DOOR 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H 51.00 in. W x (76.20 cm x 1.65 m) (60.96 cm x 1.65 m) 59.00 in. H PASSENGER CABIN LENGTH (1.30 m x 1.50 m) 61 ft 8 in. (18.80 m)
LEGEND 1. Forward baggage compartment 91.00 ft 3 (2.58 m 3 ). NOTE 2. Rear baggage compartment Standard configuration shown. 33
Dec 05/2014 411.00 ft (11.64 m ). Layout may vary with optional 3. Lavatory. ae12 Page configurations. 4. Wardrobe. 5. Flight attendant. 6. Galley. br195a02.dg, gg/gw, aug5/2008 Series: 400
SERIES 400 (MODEL 402) STANDARD INTERIOR CONFIGURATION 74 SEATS AT 31 INCH PITCH (78.74 cm) SERIES 400(MODEL402) STANDARDINTERIORCONFIGURATION BAGGAGE DOOR TYPE II/III EXIT 24.00 in. W x 54.00 in. H 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) (51.31 cm x 1.42 m) SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H 5 ft. 11 in. (60.96 cm x 1.37 m) (1.81 m) 11.00 ft. (3.35 m)
3 1 6 AIRPORT PLANNINGMANUAL Figure 2−9
4 5 5 2 CHAPTER 2 AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT BAGGAGE DOOR 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H 51.00 in W x (76.20 cm x 1.65 m) (60.96 cm x 1.65 m) 59.00 in. H PASSENGER CABIN LENGTH (1.30 m x 1.50 m) STA. X−39.00 61 ft 8 in. (18.80 m) STA. X701.00
LEGEND 1. Forward baggage compartment 91.00 ft 3 (2.58 m 3 ). NOTE 2. Rear baggage compartment Standard configuration shown. 411.00 ft 33 (11.64 m ). Dec 05/2014 Layout may vary with optional 3. Lavatory. ae13 Page configurations. 4. Wardrobe. 5. Flight attendant. 6. Galley. br307a01.dg, pt/kmw, aug08/2008 Series: 400
SERIES 400 (MODEL 402) INTERIOR CONFIGURATION 78 SEATS AT 30 INCH (76.2 cm) PITCH BAGGAGE DOOR SERIES 400OPTIONAL INTERIORCONFIGURATIONS 24.00 in. W x 54.00 in. H SERVICE DOOR/TYPE I EXIT 5 ft 9 in. TYPE II/III EXIT (60.96 cm x 1.37 m) 24.00 in. W x 54.00 in. H 11.00 ft. (1.75 m) 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) (3.35 m) (51.31 cm x 1.42 m) 3 1 6 AIRPORT PLANNINGMANUAL
Figure 2−10 4 5 5 2 PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m) FORWARD PASSENGER PAX DOOR/TYPE I EXIT AIRSTAIR DOOR 24.00 in. W x 65.00 in. H
CHAPTER 2 STA STA 30.00 in. W x 65.00 in. H (60.96 cm x 1.65 m) X−39.00 (76.20 cm x 1.65 m) X701.00 BAGGAGE DOOR 51.00 in. W x 59.00 in. H (1.30 m x 1.50 m) (Sheet 1of5)
LEGEND 1. Forward baggage compartment 3 3 91.00 ft (2.58 m ). NOTE 2. Rear baggage compartment Layout may vary with optional configurations. 365.00 ft 33(10.33 m ). Dec 05/2014 3. Lavatory. ae14 Page 4. Wardrobe. 5. Flight attendant. 6. Galley. cg3535a01.dg, cs, aug06/2014
Series: 400
SERIES 400 (MODEL 402) INTERIOR CONFIGURATION 72 SEATS AT 32 INCH (81.28 cm) PITCH SERIES 400OPTIONAL INTERIORCONFIGURATIONS
BAGGAGE DOOR 24.00 in. W x 54.00 in. H SERVICE DOOR/TYPE I EXIT (60.96 cm x 1.37 m) TYPE II/III EXIT 24.00 in. W x 54.00 in. H 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) 37.80 in. 11.00 ft 96.01 cm (51.31cm x 1.42 m) (3.35 m) 6 3 1 6 6 AIRPORT PLANNINGMANUAL Figure 2−10
4 5 5 7 2 PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m) FORWARD PASSENGER
CHAPTER 2 PAX DOOR/TYPE I EXIT AIRSTAIR DOOR 24.00 in. W x 65.00 in. H STA STA 30.00 in. W x 65.00 in. H X−39.00 (60.96 cm x 1.65 m) X701.00 (76.20 cm x 1.65 m)
(Sheet 2of5) LEGEND BAGGAGE DOOR 51.00 in. W x 59.00 in. H 1. Forward Baggage Compartment (1.30 m x 1.50 m) 51.00 ft 3(1.44 m3 ). 2. Rear baggage compartment NOTE 365.00 ft 3(10.33 m3 ). Layout may vary with optional configurations. 3. Lavatory. 4. Wardrobe. Dec 05/2014 5. Flight attendant Seat. ae15 Page 6. Galley. 7. Cart storage.
cg3535a02.dg, cs, aug06/2014 Series: 400
SERIES 400 (MODEL 402) INTERIOR CONFIGURATION 66 SEATS AT 31 in. (78.74 cm) PITCH AND 8 SEATS AT 34 in. (86.36 cm) PITCH
SERIES 400OPTIONAL INTERIORCONFIGURATIONS BAGGAGE DOOR SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H 24.00 in. W x 54.00 in. H (60.96 cm x 1.37 m) TYPE II/III EXIT (60.96 cm x 1.37 m) 5 ft 9 in. 20.20 in. W x 56.00 in. H (1.75 m) (51.31cm x 1.42 m) 11.00 ft (3.35 m) 3 1 6 AIRPORT PLANNINGMANUAL
5 Figure 2−10 4 5 2 PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m) STA STA X−39.00 FORWARD PASSENGER PAX DOOR/TYPE I EXIT X701.00 AIRSTAIR DOOR 24.00 in. W x 65.00 in. H
CHAPTER 2 30.00 in. W x 65.00 in. H (60.96 cm x 1.65 m) BAGGAGE DOOR (76.20 cm x 1.65 m) 51.00 in. W x 59.00 in. H (1.30 m x 1.50 m)
(Sheet 3of5) LEGEND 1. Forward baggage compartment 3 91.00 ft (2.58 m3 ). 2. Rear baggage compartment 365.00 ft 33(10.33 m ). 3. Lavatory.
Dec 05/2014 NOTE 4. Wardrobe. Layout may vary with optional configuration. 5. Flight attendant. ae16 Page 6. Galley.
cg3535a03.dg, cs, aug06/2014 Series: 400
SERIES 400 (MODEL 402) THREE−ABREAST TRIPLE CLASS INTERIOR CONFIGURATION 7 SEATS AT 36 in. (91.44 cm) PITCH, 10 SEATS AT 34 in. (86.36 cm) PITCH AND 54 SEATS AT 30 in. (76.20 cm) PITCH SERIES 400OPTIONAL INTERIORCONFIGURATIONS BAGGAGE DOOR SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H TYPE II/III EXIT 24.00 in. W x 54.00 in. H (60.96 cm x 1.37 m) 5 ft 9 in. 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) (51.31cm x 1.42 m) 11.00 ft. (1.75 m) (3.35 m) 3 1 6 AIRPORT PLANNINGMANUAL
Figure 2−10 4 5 5 2 PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m)
STA FORWARD PASSENGER PAX DOOR/TYPE I EXIT STA X−39.00 AIRSTAIR DOOR 24.00 in. W x 65.00 in. H X701.00 30.00 in. W x 65.00 in. H (60.96 cm x 1.65 m) CHAPTER 2 (76.20 cm x 1.65 m) BAGGAGE DOOR 51.00 in. W x 59.00 in. H (1.30 m x 1.50 m) (Sheet 4of5)
LEGEND 1. Forward baggage compartment 91.00 ft 33(2.58 m ). NOTE 2. Rear baggage compartment 33 Layout may vary with optional configuration. 365.00 ft (10.33 m ).
Dec 05/2014 3. Lavatory. 4. Wardrobe. ae17 Page 5. Flight attendant. 6. Galley.
cg3535a04.dg, cs, aug06/2014 Series: 400
SERIES 400 (MODEL 402) EXTRA CAPACITY INTERIOR CONFIGURATION 86 SEATS AT 29 INCH (73.66 cm) PITCH SERIES 400OPTIONAL INTERIORCONFIGURATIONS FORWARD TYPE I EMERGENCY EXIT DOOR SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H TYPE II/III EMERGENCY 24.00 in. W x 54.00 in. H (60.96 cm x 1.37 m) EXIT DE−ACTIVATED (60.96 cm x 1.37 m) 11.00 ft (3.35 m) 2 5 AIRPORT PLANNINGMANUAL Figure 2−10
3 4 4 1 PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m) FORWARD PASSENGER
CHAPTER 2 PAX DOOR/TYPE I EXIT AIRSTAIR DOOR 24.00 in. W x 65.00 in. H STA STA 30.00 in. W x 65.00 in. H X−39.00 (60.96 cm x 1.65 m) X701.00 (76.20 cm x 1.65 m)
(Sheet 5of5) BAGGAGE DOOR 51.00 in. W x 59.00 in. H LEGEND (1.30 m x 1.50 m) 1. Rear baggage compartment 365.00 ft 3(10.33 m3 ). 2. Lavatory. 3. Wardrobe. Dec 05/2014 NOTE 4. Flight attendant Seat.
ae18 Page 5. Galley. Layout may vary with optional configurations.
cg3535a05.dg, cs, aug06/2014 (1.95 m) 77.0 in. Series: 400 GROUND REFERENCELINE GROUND REFERENCELINE (1.44 m) 1 56.5 in. aircraftconfigurationandloadingconditions. NOTE This dimensionisapproximateandwillvarywith (0.62 m) 24.3 in. (0.32 m) 12.4 in. PASSENGER PASSENGER COMPARTMENT (0.40 m) 15.8 in. (0.51 m) 20.0 in OPRMN RS ETO (Sheet1of 2) COMPARTMENT CROSS SECTION (CLASSIC) AIRPORT PLANNINGMANUAL 106.0 in. (2.69 m) (2.51 m) (0.66 m) (2.03 m) 99.0 in. 25.9 in. 80.0 in. Figure 2−11 108.8 in. 101.1 in. (2.76 m) (2.56 m) CHAPTER 2 (CAPACITY IS1.67ft(0.047m)/PAX.) OVERHEAD STOWAGEBINS (1.82 m) 71.8 in. AT DOORCENTERLINE 6.21 in.(15.8cm) AT AFTEDGEOFDOOR 5.74 in.(14.6cm) AT FWDEDGEOFDOOR 11.37 in.(28.9cm) 3 Dec 05/2014 3 ae19 Page 1 1
br721a01.dg, gv/gw, nov13/2014 AIRPORT PLANNING MANUAL
OVERHEAD STOWAGE BINS (CAPACITY IS 1.75 ft 33 (0.049 m )/PAX.)
106.0 in. (2.69 m)
24.1 in. (0.61 m)
20.4 in. 76.1 in. (0.52 m) (1.93 m) 97.9 in. 56.3 in. (2.49 m) (1.43 m) 16.0 in. (0.41 m) 24.5 in. (0.62 m) 71.8 in. (1.82 m)
11.1 in. (0.28 m)
81.9 in. (2.08 m) GROUND REFERENCE LINE
101.1 in. (2.56 m)
108.8 in. (2.76 m)
1 11.37 in. (28.9 cm) AT DOOR CENTER LINE PASSENGER COMPARTMENT
(NEXT GEN)
NOTE 1 This dimension is approximate and will vary with aircraft configuration and loading conditions. r721a02.dg, gw, nov13/2014 b PASSENGER COMPARTMENT CROSS SECTION (Sheet 2 of 2)
Figure 2 − 11 Series: 400
Page 20 CHAPTER 2 Dec 05/2014 Series: 400
70 TO 78 SEATS CONFIGURATION−SERIES 400
FORWARD AFT BAGGAGE BAGGAGE COMPARTMENT SEAT SERVICE COMPARTMENT LAVATORY DOOR FORWARD RAILS BAGGAGE DOOR LO ODN IGA (Sheet1of2) FLOOR LOADINGDIAGRAM AIRPORT PLANNINGMANUAL Figure 2−12
AFT GALLEYS (2) AFT BAGGAGE WARDROBE FORWARD PASSENGER DOOR CHAPTER 2 PASSENGER DOOR DOOR
LEGEND
Floor panels that can support a maximum floor loading of 37.5 lb/ft 2 (183 kg/m2 ).
2 2 Floor panels that can support a maximum floor loading of 75.0 lb/ft (366 kg/m ).
2 2 Dec 05/2014 Floor panels that can support a maximum floor loading of 125.0 lb/ ft (610 kg/m ). ae21 Page
br297a01.dg, pt/cs, jul29/2014 Series: 400
86 SEATS EXTRA CAPACITY INTERIOR CONFIGURATION−SERIES 400
AFT BAGGAGE FORWARD TYPE I EMERGENCY SERVICE COMPARTMENT EXIT DOOR WITH SEAT LAVATORY DOOR DITCHING DAM RAILS LO ODN IGA (Sheet2of2) FLOOR LOADINGDIAGRAM AIRPORT PLANNINGMANUAL Figure 2−12
AFT GALLEY AFT BAGGAGE WARDROBE FORWARD DOOR CHAPTER 2 PASSENGER PASSENGER DOOR DOOR
LEGEND
Floor panels that can support a maximum floor loading of 37.5 lb/ft 2 (183 kg/m2 ).
2 2 Floor panels that can support a maximum floor loading of 75.0 lb/ft (366 kg/m ).
2 2 Dec 05/2014 Floor panels that can support a maximum floor loading of 125.0 lb/ ft (610 kg/m ). ae22 Page
br297a02.dg, cs, jul29/2014 FWD BAGGAGE−COMPARTMENT DIMENSIONS(STANDARDINTERIOR CONFIGURATION) Series: 400 C L AIRPORT PLANNINGMANUAL 2. Forwardbaggagecompartmentandforward 1. Thedimensionsshownaremeasuredatfloorlevel. 3 Figure 2−13 NOTES door isremovedfortheextracapacityconfiguration. Type IemergencyexitdoorisinstalledinforwardRHside for theextracapacityconfiguration.
Y11.80 EMERGENCY EXITDOOR COMPARTMENT DOOR/ VIEW LOOKINGDOWN FORWARD BAGGAGE FORWARD TYPEI CHAPTER 2 ACCESS (70.6 cm) DOOR 27.8 in. 3 (1.75 m) 5 ft9in. FWD Dec 05/2014 X1.00 X70.0 ae23 Page
br757a01.dg, pt/cs, jul29/2014 Series: 400 AFT BAGGAGECOMPARTMENT DIMENSIONS(STANDARDINTERIOR CONFIGURATION) measured atfloorlevel. NOTE The dimensionsshownare 51.44 in. 80.05 in. (1.31 m) (2.03 m) AIRPORT PLANNINGMANUAL Figure 2−14 76.34 in. (1.94 m) 78.41 in. 50.15 in. 48.43 in. (1.99 m) (1.23 m) (1.27 m) CHAPTER 2 X783.10 X834.54 X703.05 Dec 05/2014 ae24 Page
br758a01.dg, sw, 08/04/98 Series: 400 AFT BAGGAGECOMPARTMENT DIMENSIONS(OPTIONALINTERIOR CONFIGURATION) measured atfloorlevel. NOTE The dimensionsshownare 61.40 in. 51.44 in. (1.56 m) (1.31 m) AIRPORT PLANNINGMANUAL Figure 2−15 76.34 in. (1.94 m) 78.41 in. 50.15 in. 48.43 in. (1.99 m) (1.23 m) (1.27 m)
CHAPTER 2 Y−12.35 X783.10 X834.54 X721.70 X703.05 Dec 05/2014 ae25 Page
br759a01.dg, sw, 08/04/98 Series: 400 TIE−DOWN RINGS(4) FORWARD−FLOOR 2000 lb(907kg) VIEW LOOKINGAFT(NETS ANDPOLESOMITTEDFORCLARITY) 180 o NETS ANDTIE−DOWNS (DETAILSPEC.CONFIGURATION) AIRPORT PLANNINGMANUAL Figure 2−16 CARGO NETS CENTER CHAPTER 2 POST SIDEWALL (ANDAFTBULKHEAD TIE−DOWN RINGS(12) POST AFT 2000 lb(907kg) 120 Dec 05/2014 o ae26 Page ) br876a01.dg, gg/pt, 12/01/01 AIRPORT PLANNING MANUAL CARGO CENTER AFT 180 o NETS POST POST
FORWARD−FLOOR TIE−DOWN RINGS (4) 2000 lb (907 kg)
FWD
120o
SIDEWALL (AND AFT BULKHEAD) TIE−DOWN RINGS (11) 2000 lb (907 kg)
VIEW LOOKING AFT (NETS AND POLES OMITTED FOR CLARITY) r883a01.dg, pt, 12/01/01 b NETS AND TIE−DOWNS (G3 GALLEY)
Figure 2 − 17 Series: 400
Page 27 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL
Door Clearances
1. General The door clearance sheets provide the door size and location of the passenger, service and baggage compartment doors. 2. The forward passenger (airstair) door opens outwards and downwards and is manually controlled from inside or outside the aircraft. 3. The aft passenger door/Type 1 exit opens inward and upwards, then moves outward and forward. 4. The aft service door/Type 1 exit opens inwards and upwards, then moves outwards and forward. 5. The forward baggage−compartment door opens inward and upward, then moves outwards and forward. 6. The aft baggage−compartment door opens outwards and upwards.
Series: 400
Page 28 CHAPTER 2 Dec 05/2014 Series: 400 (94.0 cm) (63.5 cm) 37.0 in. 1 25.0 in. 2 NOTE Refer toGroundClearanceillustrations. Dimensions areapproximateandwillvarywith aircraft configurationandloading conditions. VIEW LOOKINGINBOARD (68.6 cm) (61.0 cm) (50.8 cm) (76.2 cm) 27.0 in. 24.0 in. 20.0 in. 30.0 in. FORWARD PASSENGER −DOORCLEARANCES (1.58 m) 62.0 in. 16 ft3in. (4.95 m) AIRPORT PLANNINGMANUAL (50.8 cm) Figure 2−18 20.0 in. 44.0 in.(1.12m) (55.9 cm) 22.0 in. 1 VIEW LOOKINGAFT FS16.700 SECTION B−B CHAPTER 2 9 ft1in.(2.77m) 8 ft6in.(2.60m) GROUND REFERENCELINE 6.21 in.(15.8cm) AT AFTEDGEOFDOOR 5.74 in.(14.6cm) AT FWDEDGEOFDOOR AT DOORCENTERLIN 11.37 in.(28.9cm) Dec 05/2014 ae29 Page 2 2 E br540a01.dg, gg/sw, 04/10/99 AIRPORT PLANNING MANUAL
FS 683.450 71 ft. 9 in. TO NOSE (21.88 m) OF A/C (REF) 3 ft. 7 in. AFT (1.08 m) PASSENGER DOOR (OPEN POSITION) 14.81 in. (37.62 cm)
27.90 in. (70.87 cm)
5 ft. 4 in. (1.64 m) CLEAR OPENING 5 ft. 9 in. 5 ft. 8 in. 40.0 in. (1.75 m) (1.72 m) (1.02 m)
FLOOR LEVEL
AFT BAGGAGE DOOR (REF) 0.66 in. 0.85 in. (16.76 mm) 1 (21.59 mm)
GROUND REFERENCE LINE
VIEW LOOKING INBOARD ON L/H SIDE
NOTE 1 Refer to Ground Clearance illustrations. r845a01.dg, gg/sw, 04/10/99 b AFT PASSENGER − DOOR CLEARANCES (Sheet 1 of 2)
Figure 2 − 19 Series: 400
Page 30 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL CENTER LINE
AFT PASSENGER DOOR 27.90 in. (OPEN POSITION) (70.87 cm) FWD
L/H
AFT BAGGAGE DOOR 16.41 in. (REF) (41.68 cm) 24.55 in. (62.36 cm) CLEAR OPENING VIEW LOOKING DOWN ON L/H SIDE
CL 5 ft. 2 in. (1.57 m) 3 ft. 9 in. (1.14 m) UP
L/H R/H
AFT PASSENGER DOOR (OPEN POSITION)
7.73 in. (19.63 cm) 4 ft. 5 in. (1.34 m)
VIEW LOOKING FORWARD br845a02.dg, gw, 08/04/98 AFT PASSENGER − DOOR CLEARANCES (Sheet 2 of 2)
Figure 2 − 19 Series: 400
Page 31 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL
FS 683.450 71 ft. 9 in. (21.88 m) TO NOSE OF A/C (REF) AFT SERVICE DOOR 3 ft. 7 in. (OPEN POSITION) (1.08 m)
27.90 in. 14.81 in. (70.87 cm) (37.62 cm)
4 ft. 5 in. (1.36 m) CLEAR OPENING 40.0 in. 4 ft. 10 in. 4 ft. 9 in. (1.48 m) (1.45 m) (1.02 m)
FLOOR LEVEL
0.85 in. 0.66 in. UP (21.59 mm) (16.76 mm) 1 FWD
GROUND REFERENCE LINE VIEW LOOKING INBOARD ON R/H SIDE
NOTE 1 Refer to Ground Clearance illustrations. r466a01.dg, gg/sw, 04/10/99 b AFT SERVICE − DOOR CLEARANCES (Sheet 1 of 2)
Figure 2 − 20 Series: 400
Page 32 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL CENTER LINE 28.90 in. (73.41 cm)
AFT SERVICE DOOR (OPEN POSITION) L/H
FWD
16.41 in. 24.55 in. (41.68 cm) (62.36 cm) CLEAR OPENING
VIEW LOOKING DOWN ON R/H SIDE
CL
5 ft. 2 in. UP (1.58 m)
4 ft. 6 in. L/H R/H (1.37 m)
AFT SERVICE DOOR (OPEN POSITION)
FLOOR LEVEL 1.21 in. 4 ft. 5 in. (30.73 mm) (1.34 m)
VIEW LOOKING FORWARD r466a02.dg, gw, 08/04/98 b AFT SERVICE − DOOR CLEARANCES (Sheet 2 of 2)
Figure 2 − 20 Series: 400
Page 33 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL
FS18.250 16ft. 4in. TO NOSE (4.98m) OF A/C (REF)
FORWARD BAGGAGE DOOR/ FORWARD TYPE 1 EMERGENCY EXIT 3 ft. 6 in. (OPEN POSITION) (1.09 m)
14.81 in. 27.90 in. (37.62 cm) (70.87 cm)
4 ft. 5 in. (1.36 m) 4 ft. 10 in. 40.0 in. (1.48 m) 4 ft. 9 in. (1.02 m) (1.45 m)
FLOOR LEVEL
1 0.85 in. 0.66 in. (21.6 mm) (16.8 mm) GROUND REFERENCE LINE VIEW LOOKING INBOARD ON R/H SIDE
NOTES Refer to Ground Clearance illustrations.
2. Forward baggage compartment and forward baggage door is removed for the extra capacity configuration.
3. Forward type I emergency exit door is installed in lieu of forward baggage compartment door for the extra capacity configuration. g3536a01.dg, cs/kmw, nov21/2014 c FORWARD BAGGAGE COMPARTMENT/FORWARD TYPE 1 EMERGENCY EXIT − DOOR CLEARANCES (Sheet 1 of 2) Figure 2 − 21 Series: 400
Page 34 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL CENTERLINE FORWARD BAGGAGE DOOR/ FORWARD TYPE 1 EMERGENCY EXIT (OPEN POSITION)
27.90 in. (70.87 cm)
L/H
16.41 in. FWD (41.68 cm) 24.55 in. (62.35 cm) CLEAR OPENING VIEW LOOKING DOWN ON R/H SIDE
5 ft. 2 in. (1.58 m)
4 ft. 6 in. (1.37 m)
UP
L/H R/H
FORWARD BAGGAGE DOOR/ FORWARD TYPE 1 EMERGENCY EXIT (OPEN POSITION) FLOOR LEVEL 1.21 in. (30.73 mm) 4 ft. 5 in. (1.34 m) CL NOTES VIEW LOOKING FORWARD 2. Forward baggage compartment and forward baggage door is removed for the extra capacity configuration. 3. Forward type I emergency exit door is installed in lieu of forward baggage compartment door for the extra capacity configuration. g3536a02.dg, cs/kmw, nov21/2014 c FORWARD BAGGAGE COMPARTMENT/FORWARD TYPE 1 EMERGENCY EXIT − DOOR CLEARANCES (Sheet 2 of 2) Figure 2 − 21 Series: 400
Page 35 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL
CL 8 ft. 9 in. (2.66 m)
5 ft. 3 in. (1.59 m) AT FS 728.102
OPEN POSITION
5 ft. 5 in. (1.66 m)
4 ft. 12 in. (1.52 m)
FLOOR LEVEL
UP
L/H R/H 3 ft. 6 in. (1.06 m) AT VIEW LOOKING FORWARD FS 728.102 br412a01.dg, pt, 13/05/98 AFT BAGGAGE−COMPARTMENT − DOOR CLEARANCES (Sheet 1 of 2)
Figure 2 − 22 Series: 400
Page 36 CHAPTER 2 Dec 05/2014 AIRPORT PLANNING MANUAL AFT BAGGAGE DOOR FS 728.102 (OPEN POSITION) FS 783.102
4 ft. 11 in. CUTOUT (1.50 m)
HANDLE HEIGHT (WHEN CLOSED)
FLOOR LEVEL
12.0 in. (30.5 cm)
4 ft. 3 in. 1 (1.30 m) 2.36 in. CLEAR OPENING UP (6.0 cm)
FWD GROUND REFERENCE LINE
VIEW LOOKING INBOARD ON L/H SIDE
NOTE 1 Refer to Ground Clearance illustrations. r412a02.dg, gg/kmw, aug08/2008 b AFT BAGGAGE−COMPARTMENT − DOOR CLEARANCES (Sheet 2 of 2)
Figure 2 − 22 Series: 400
Page 37 CHAPTER 2 Dec 05/2014 Series: 400 WHILE LOWERING HANDLE INOPEN SUPPORT DOOR OUT ANDDOWN PULL HANDLE KEEP CLEAR POSITION WARNING OF DOOR TO OPEN EXTERIOR OFFWDPASSENGERDOOR PUSH PULL HANDLE AND TURN TO OPEN RELEASE PUSH TO EXTERIOR HANDLES AIRPORT PLANNINGMANUAL EXTERIOR OFAFTBAGGAGE DOOR Figure 2−23 LOWERING PULL HANDLE ASSIST DOOR AND TURN TO OPEN (Sheet 1of2) EXTERIOR OFAFTPASSENGERDOOR CHAPTER 2 BEFORE CLOSING BAGGAGE DOOR PULL HANDLE STOW STRUT AND TURN TO OPEN HANDLE INOPE PULL HANDLE AND TURN (TYPICAL) POSITION TO OPEN Dec 05/2014 ae38 Page
cg3538a01.dg, cs, aug06/2014 N Series: 400 PULL HANDLE 2 AND TURN TO OPEN Forward typeIemergency exit doorisinstalledonlyonaircraftwithextracapacity configuration. Type II/IIIemergencyexitdoorisde−activatedforthe extracapacityconfiguration. NOTES 2 EXTERIOR FORWARDBAGGAGE TYPE IEMERGENCYEXITDOOR DOOR/ EXTERIORFORWARD PULL HANDLE AND TURN TO OPEN D EXTERIOR HANDLES EXTERIOR OFAFTSERVICEDOOR AIRPORT PLANNINGMANUAL PULL HANDLE F AND TURN TURN HANDLEDOWN AND PUSHHATCHIN TO OPEN Figure 2−23 F RELEASE PUSH TO EXTERIOR OFTYPEII/IIIEMERGENCYEXIT (Sheet 2of2) CHAPTER 2 PULL HANDLE AND TURN E TO OPEN E D HANDLE INOPEN (78.7 cm) 31.0 in. POSITION Dec 05/2014 ae39 Page
cg3538a02.dg, cs, aug06/2014 Series: 400 NOTES 1. Rightsideofaircraftisshown,leftidentical. both sidesofthenacelles. Aft MLGdoorsprotrudeapprox.6in.(15.2cm)from Drain mastonleftsideofeachnacelle(viewedfrom aircraft isshown,leftsideidentical. and thefuselageis96in.(2.44m).Rightsideof behind theaircraft)protrudesapprox.4in.(10.2cm). The minimumclearancebetweenthenacelle(aftMLG doors) MINIMUM CLEARANCE BETWEENNACELLESANDFUSELAGE AIRPORT PLANNINGMANUAL Figure 2−24 CHAPTER 2 Dec 05/2014 ae40 Page
braa8a01.dg, ab, 26/08/01 Series: 400 AFT BAGGAGECOMPARTMENT VERTICALDIMENSIONS(TYPICAL CONFIGURATION) (1.90 m) 74.9 in. AIRPORT PLANNINGMANUAL Figure 2−25 (1.61 m) 63.5 in. CHAPTER 2 11.5 in. (29.2 cm) Dec 05/2014 ae41 Page
braa7a01.dg, ab, 26/03/01 1. KandKKvaluesarethroughC/Lofhorizontalstabilizer. Series: 400 NOTES 2. Dimensionsareapproximateandwillvarywith ITEM GSILLOFAFTBAGGAGEDOOR(ONJACKS) GG KK AA aircraft configurationandloadingconditions. JVERTICALSTABILIZER(ONJACKS) JJ OIOTLSAIIE OFJCS 5−2 7.62 −7.92 25−26 HORIZONTALSTABILIZER(OFFJACKS) K ILO F AGG OR(F AK)50 1.54 5.06 SILL OF AFTBAGGAGEDOOR(OFFJACKS) G AL(F AK)11.8 TAIL(OFFJACKS) A J (1.55 m) 5.07 ft TAIL (ONJACKS) HORIZONTAL STABILIZER(ONJACKS) VERTICAL STABILIZER(OFFJACKS) ON JACKS HEIGHT GG G AIRCRAFT DIMENSIONS OFF JACKS AIRPORT PLANNINGMANUAL (5.55 m) 18.2 ft Figure 2−26 (Sheet 1of3) 13 −13.9 5.7 26.7 −27.2 728.30 27.2 26.7 CHAPTER 2 ET(t METERS(m) FEET (ft) 12 ft4in. (3.76 m)
AA ON JACKS ON A JACKS OFF
KK ON JACKS ON
8.13 1.74 8.13 −8.30 3.96 −4.24 3.60
K JACKS OFF Dec 05/2014 JACKS ON JJ
ae42 Page J JACKS OFF
cg2886a01.dg, nn/kmw, sep19/2013 Series: 400 Dimensions areapproximateand loading conditions. NOTE will varywithA/Cconfigurationand AIRCRAFT EMPENNAGE−PLATFORMWORKING HEIGHTS GROUND LEVEL AIRCRAFT DIMENSIONS ITEM B 32 4.04 13.25 BBB BB AA 11 3.40 11.17 B A AIRPORT PLANNINGMANUAL ET(t METERS(m) FEET (ft) 06 3.25 10.67 24 3.79 12.42 Figure 2−26 .33.00 9.83 1 LEVEL 2 LEVEL (Sheet 2of3) CHAPTER 2
(3.76 m) 12.33 ft. A STATIC
AA ON JACKS ON (1.52 m) (2.79 m) 9.17 ft.
5 ft. B LEVEL A/C
BB STATIC (4.32 m) 14.17 ft.
BBB ON JACKS ON Dec 05/2014 (8.36 m 27.42 ft ae43 Page ) cg2886a02.dg, kh, nov12/2013 . AIRPORT PLANNING MANUAL
E
A D B C
L K J H G F
ITEM FEET (ft) METERS (m) A 25.67 7.82 B 12.83 3.91 C 3.22 0.98 D 3.61 1.10 E 13.5 4.11 F 27.33 8.33 G 5.07 1.55 H 5.07 1.55 J 4.08 1.24 K 3.82 1.16 L 10.75 3.28
EMERGENCY EXIT LOCATIONS AND ELEVATIONS cg2886a03dg, cs, sep08/2014 AIRCRAFT DIMENSIONS (Sheet 3 of 3)
Figure 2 − 26 Series: 400
Page 44 CHAPTER 2 Dec 05/2014 CHAPTER 3
AIRCRAFT PERFORMANCE AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. General This chapter contains the performance data of the Dash−8 Series 400 (Model 402) aircraft as required for airport planning purposes. This data reflects the performance levels of the Dash−8 Series 400, Performance Data (July 1999). 2. The various definitions used in this Chapter are as follows: A. Maximum Structural Weights As found in the July 1999 Performance Data, the maximum structural take−off weight is 63,750 lbs (28,916 kg), and the maximum landing weight is 61,250 lbs (27,782 kg). B. WAT Limits The maximum permissible take−off weight (refer to Figure 3−2, Figure 3−3 and Figure 3−4) and landing weight (refer to Figure 3−8, Figure 3−9 and Figure 3−10) are based on the climb requirements of FAR 25 (one engine inoperative). C. Take−off Runway Length The take−off runway length shown in Figure 3−5, Figure 3−6 and Figure 3−7 is the longest of:
– − The accelerate−stop distance – − The take−off distance to 35 feet altitude with one engine inoperative at V1 – − 1.15 times the all engine−operating take−off distance to 35 feet altitude. D. Landing Runway Length The landing runway length required in Figure 3−14 is the unfactored landing distance (refer to Figure 3−11, Figure 3−12 and Figure 3−13) multiplied by an operational factor of 1.67 (or 1/0.6) or 1.43 (or 1/0.7). The unfactored landing distance is based on an approach speed of 1.3 Vs and a screen height of 50 feet. E. Retardation Devices The retardation devices that follow are used: (1) Accelerate−Stop (a) Maximum main−wheel anti−skid braking. (b) One propeller in the DISC position, the other one is feathered. (c) Roll spoilers are extended. (2) Landing
Series: 400
Page 1 CHAPTER 3 May 28/2001 AIRPORT PLANNING MANUAL (a) Maximum main−wheel anti−skid braking. (b) One propeller in the DISC position, the other one is feathered. (c) Roll spoilers are extended. F. Standard Day Temperatures The table that follows shows the standard day temperatures that are used in this Chapter. STANDARD DAY TEMPERATURES ELEVATION STANDARD DAY TEMPERATURE FEET METERS °F °C 0 0 59 15 2000 610 51.9 11.1 4000 1220 44.7 7.1 6000 1830 37.6 3.1 8000 2440 30.5 −0.8 10,000 3050 23.3 −4.8
Series: 400
Page 2 CHAPTER 3 May 28/2001 Series: 400 PAYLOAD/RANGE ATMAXIMUM CRUISERATINGANDLONGRANGE CRUISE AIRPORT PLANNINGMANUAL Figure 3−1 CHAPTER 3 May 28/2001 ae3 Page
brb11a01.dc, sw, 25/01/00 Series: 400 MAXIMUM PERMISSIBLE TAKE−OFFWEIGHT(WATLIMIT)−FLAPS 5DEGREES AIRPORT PLANNINGMANUAL Figure 3−2 CHAPTER 3 May 28/2001 ae4 Page
brb12a01.dc, pm, 25/01/00 Series: 400 MAXIMUM PERMISSIBLE TAKE−OFFWEIGHT(WATLIMIT)−FLAPS 10DEGREES AIRPORT PLANNINGMANUAL Figure 3− CHAPTER 3 May 28/2001 ae5 Page
brb13a01.dc, sw, 26/01/00 Series: 400 MAXIMUM PERMISSIBLE TAKE−OFFWEIGHT(WATLIMIT)−FLAPS 15DEGREES AIRPORT PLANNINGMANUAL Figure 3−4 CHAPTER 3 May 28/2001 ae6 Page
brb14a01.dc, sw, 26/01/00 Series: 400 TAKE−OFF RUNWAYLENGTH REQUIREMENTS−FLAPS5DEGREES AIRPORT PLANNINGMANUAL Figure 3−5 CHAPTER 3 May 28/2001 ae7 Page
RUNWAY
brb15a01.dc, sw, 26/01/00 Series: 400 TAKE−OFF RUNWAYLENGTH REQUIREMENTS−FLAPS10DEGREES AIRPORT PLANNINGMANUAL Figure 3−6 CHAPTER 3 May 28/2001 ae8 Page
RUNWAY
brb16a01.dc, sw, 26/01/00 Series: 400 TAKE−OFF RUNWAYLENGTH REQUIREMENTS−FLAPS15DEGREES AIRPORT PLANNINGMANUAL Figure 3−7 CHAPTER 3 May 28/2001 ae9 Page
RUNWAY
brb17a01.dc, sw, 26/01/00 Series: 400 MAX. LANDINGWEIGHT −LANDINGFLAPS10ANDAPPROACH 5DEGREES AIRPORT PLANNINGMANUAL Figure 3−8 CHAPTER 3 May 28/2001 ae10 Page
brb18a01.dc, sw, 26/01/00 Series: 400 MAX. LANDINGWEIGHT −LANDINGFLAPS15ANDAPPROACH 10DEGREES AIRPORT PLANNINGMANUAL Figure 3−9 CHAPTER 3 May 28/2001 ae11 Page
brb19a01.dc, sw, 27/01/00 Series: 400 MAX. LANDINGWEIGHT −LANDINGFLAPS35ANDAPPROACH 15DEGREES AIRPORT PLANNINGMANUAL Figure 3−10 CHAPTER 3 May 28/2001 ae12 Page
brb20a01.dc, sw, 26/01/00 Series: 400 UNFACTORED LANDING DISTANCE−FLAPS10DEGREES AIRPORT PLANNINGMANUAL Figure 3−11 CHAPTER 3 May 28/2001 ae13 Page
brb21a01.dc, sw, 26/01/00 Series: 400 UNFACTORED LANDING DISTANCE−FLAPS15DEGREES AIRPORT PLANNINGMANUAL Figure 3−12 CHAPTER 3 May 28/2001 ae14 Page
brb22a01.dc, sw, 26/01/00 Series: 400 UNFACTORED LANDING DISTANCE−FLAPS35DEGREES AIRPORT PLANNINGMANUAL Figure 3−13 CHAPTER 3 May 28/2001 ae15 Page
brb23a01.dc, sw, 26/01/00 AIRPORT PLANNING MANUAL
LANDING − RUNWAY LENGTH REQUIRED
Figure 3 − 14 Series: 400
Page 16 CHAPTER 3 May 28/2001 CHAPTER 4
GROUND MANEUVERING AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. This Chapter supplies data on the items that follow:
– Aircraft turning capability (refer to Figure 4−1, Figure 4−2 and Figure 4−3) – Visibility from cockpit (Note, this information is not available at this time) – Maneuvering characteristics (refer to Figure 4−4, Figure 4−5, Figure 4−6 and Figure 4−7) – Mooring data (refer to Figure 4−8). 2. This data has been determined from the theoretical limits imposed by the geometry of the aircraft and includes normal allowance for tire slippage (as indicated). The purpose of this Chapter is to show the turning capability of the aircraft in favorable operating conditions (without the use of reverse thrust or differential braking). Use this data only as a guideline. 3. It is possible that each airline will use more conservative turning procedures to avoid excessive tire wear and possible maintenance problems. The operating techniques of each airline will be different and may be modified because of these physical factors within the maneuvering area:
– Adverse grades – Limited area – High risk of jet engine exhaust or propeller slipstream damage. 4. Because of these reasons the airport planner must coordinate the ground maneuvering data with the user airline for airport layout plan.
Series: 400
Page 1 CHAPTER 4 May 28/2001 AIRPORT PLANNING MANUAL
TURNING CENTER FOR NOSE−GEAR TURNING ANGLE. (TYPICAL)
NOSE−GEAR AXLE PROJECTION−LINE. (TYPICAL)
o 20
o 25
o 30
7 o 35
6 o 40
o 45
o 50 o STEERING 55 o 60 o 65 o o 70 o o o 75 90 85 80
TOWING R−1 (Inner).
R−2 (Outer Gear). R−3 (Nose Gear).
R−4 (Wing Tip).
R−5 (Nose). 6 R−6 (Tail).
7 Dimension "C" Typical. Refer to table for distance of individual points from aircraft center line. ra85a01.dg, pt, 05/08/98 b TURNING RADII (NO SLIP ANGLE)
Figure 4 − 1 Series: 400
Page 2 CHAPTER 4 May 28/2001 Series: 400
R−1 R−2 R−3 R−4 INNER OUTER NOSE WING R−5 R−6 DIMENSION STEERING GEAR GEAR GEAR TIP NOSE TAIL "C" ANGLE (DEGREES) in. m in. m in. m in. m in. m in. m in. m ft ft ft ft ft ft ft
5 6083.87 154.50 6459.50 164.10 6306.70 160.20 6831.25 173.50 6301.95 160.07 6483.96 164.70 6721.27 170.70 507.00 538.33 525.58 569.25 525.17 540.80 560.00 2923.90 74.27 3299.53 74.27 3171.20 80.50 3671.29 93.25 3172.68 80.60 3353.99 85.20 3111.30 79.03 TURNING RADIIDATA (NO SLIPANGLE) 10 243.67 275.00 264.25 305.25 264.42 279.50 259.25 15 1859.64 47.23 2235.26 56.80 2131.73 54.14 2607.04 66.20 2139.17 54.30 2318.22 58.90 2047.03 52.00 155.00 186.25 177.67 217.25 217.25 193.17 170.58 1319.17 33.50 1694.80 43.05 1616.16 41.05 2066.59 52.50 1629.56 41.40 1804.96 45.85 1506.57 38.20 20 AIRPORT PLANNINGMANUAL 109.92 141.25 134.67 172.25 135.83 150.42 125.58 25 988.09 25.10 1363.71 34.60 1310.45 33.29 1735.52 44.10 1329.46 33.80 1500.02 38.10 1175.48 29.80 82.33 113.67 109.17 144.67 110.75 125.00 97.92 30 761.53 19.30 1137.16 28.90 1109.77 28.19 1428.22 36.28 1134.09 28.80 1298.74 33.00 949.93 24.10
Figure 4−2 63.50 94.75 92.08 119.00 94.08 108.25 79.08 STEERING 35 594.53 15.10 970.15 24.60 969.26 24.62 1341.98 34.10 998.55 25.40 1156.38 29.40 781.93 20.00 49.58 80.83 80.75 111.83 83.25 96.33 65.17 40 464.56 11.80 840.19 21.30 866.51 22.00 1212.02 30.79 900.42 22.90 1050.63 26.70 651.96 16.56 38.75 70.00 72.25 101.00 75.00 87.58 54.33 45 359.08 9.12 734.71 18.70 789.14 20.04 1106.55 28.10 827.25 21.00 969.13 24.60 546.48 13.90 29.92 61.25 65.75 92.25 68.92 80.75 45.50 50 270.52 6.87 646.14 16.40 729.72 18.50 1018.00 25.90 771.61 19.60 904.55 23.00 457.91 11.60 22.58 53.83 60.83 84.83 64.33 75.42 38.17 CHAPTER 4 55 194.02 4.93 569.64 14.50 683.57 17.36 941.51 23.90 728.82 18.50 852.24 21.60 381.41 9.69 16.17 47.50 57.00 78.50 60.75 71.00 31.75 60 126.30 3.21 501.93 12.75 647.62 16.45 873.81 22.19 695.78 17.67 809.15 20.60 313.70 7.97 10.50 41.83 54.00 72.83 58.00 67.42 26.17 65 65.06 1.65 440.68 11.19 619.70 15.70 812.57 20.60 670.40 17.03 773.23 19.60 252.45 6.41 5.42 36.75 51.67 67.75 55.83 64.42 21.00 70 8.57 0.22 384.19 9.75 598.61 15.20 756.09 19.20 651.23 16.50 743.03 18.90 195.96 5.00 0.75 32.00 49.92 63.00 54.25 61.92 16.33 75 −44.48 −1.13 331.15 8.41 583.11 14.80 703.06 17.90 637.28 16.20 717.58 18.20 142.92 3.63 −3.67 27.58 48.58 58.58 53.08 59.83 11.92 80 −95.13 −2.41 280.49 4.50 572.60 14.50 652.42 16.60 627.87 15.90 696.18 17.70 92.26 2.34 −7.92 23.00 47.75 54.33 52.33 58.00 7.67 TOWING 85 −144.29 −3.67 231.34 5.88 566.64 14.40 603.28 15.30 622.54 15.80 678.39 17.20 43.11 1.09 −12.00 19.25 47.25 50.25 51.92 56.50 3.58 90 −192.14 −4.90 182.88 4.65 565.00 14.35 554.84 14.10 621.07 15.78 663.97 16.90 −5.35 −0.14 −16.00 15.25 47.08 46.25 51.75 55.33 −0.42 May 28/2001 NOTE ae3 Page The actual operating data will be greater than the values shown because tire slippage is not considered. The airport planner must consult with the user airline for specific operating procedures. brb39a01.dg, pt, 06/08/98 AIRPORT PLANNING MANUAL
MINIMUM TURNING CENTER ON MAIN−AXLE GEAR PROJECTION
STA. X 443.050
R−4 R−6
R−1
o o 70 R−2 APPROX. 2 84 ft. 5 in. (25.7m) DUE TO TIRE R−5 MINIMUM PAVEMENT o SLIP WIDTH FOR 180 TURN R−3 (WITHOUT BACKING UP)
ITEM RADIUS R−1 INNER GEAR 4 ft. 9 in. (1.52 m) R−2 OUTER GEAR 33 ft. 10 in. (10.32 m) R−3 NOSE GEAR 50 ft. 7 in. (15.41 m) R−4 WING TIP 64 ft. 9 in. (19.74 m) R−5 NOSE 54 ft. 10 in. (16.73 m) NOTES R−6 ELEVATOR TIP 62 ft. 9 in. (19.13 m) 1. Dimensions noted are for dry, hard, level surfaces at these tire pressures : 227 psi (loaded), 32 x 8.8−16 standard main−wheel tires, and 89 psi (loaded) for 22 x 6.50−10 standard nose−wheel tires. o 2. Nose gear steering limit is approximately 70 left and right. 3. Slip angle of 2 o is approximate only and may vary with aircraft configuration, loading and tire wear. 4. Dimensions given for maneuvering clearance and turning radii are minimum recommended limits. 5. Tire pressures shown are for calculation purposes only.
Refer to AMM Ch. 12 for service pressures. brc72a01.dg, sw, 17/01/00 TURNING RADIUS AT MINIMUM POWER
Figure 4 − 3 Series: 400
Page 4 CHAPTER 4 May 28/2001 AIRPORT PLANNING MANUAL SCALE 0 25 50 75 100 ft
0 10 20 30 m
NOTE The airport planner must consult with C C L L the user airline for specific operating procedures.
NOSE GEAR o STEERING ANGLE: 17.3
8.33 ft (2.54 m)
132.42 ft 100 ft (40.36 m) (30.48 m) 75 ft RADIUS RADIUS (22.86 m) TAXIWAY WIDTH
PILOT’S 23.08 ft NOSE GEAR CENTER LINE STRAIGHT (7.04 m) FORWARD TRACK VISION TRACK MAIN GEAR CENTER LINE TRACKS (PORT & STARBOARD) 150 ft (45.72 m) brb44a01, gv, 06/08/98 GREATER THAN 90 DEGREE TURN − RUNWAY TO TAXIWAY WITH TRACKS
Figure 4 − 4 Series: 400
Page 5 CHAPTER 4 May 28/2001 AIRPORT PLANNING MANUAL SCALE 0 25 50 75 100 ft
150 ft 0 10 20 30 m (45.72 m) NOTE The airport planner must consult with the user airline for specific operating procedures. CL
75 ft 6.17 ft (22.86 m) (1.88 m) TAXIWAY WIDTH
NOSE GEAR o STEERING ANGLE: 15
CL
23.08 ft (7.04 m)
100 ft (30.48 m) RADIUS
PILOT’S STRAIGHT NOSE GEAR CENTER LINE FORWARD TRACK VISION TRACK MAIN GEAR CENTER LINE TRACKS (PORT & STARBOARD) brb43a01, gv, 06/08/98 90 DEGREE TURN − RUNWAY TO TAXIWAY WITH NOSE GEAR AND COCKPIT TRACKS
Figure 4 − 5 Series: 400
Page 6 CHAPTER 4 May 28/2001 AIRPORT PLANNING MANUAL SCALE 0 25 50 75 100 ft
0 10 20 30 m
NOTE CL 75 ft The airport planner must consult with (22.86 m) the user airline for specific operating TAXIWAY WIDTH procedures.
75 ft 8.25 ft (22.86 m) (2.51 m) TAXIWAY WIDTH
NOSE GEAR o STEERING ANGLE: 20
CL
23.08 ft (7.04 m)
100 ft (30.48 m) RADIUS
PILOT’S NOSE GEAR CENTER LINE STRAIGHT TRACK FORWARD VISION MAIN GEAR CENTER LINE TRACKS TRACK (PORT & STARBOARD) brb42a01, gv, 06/08/98 90 DEGREE TURN − TAXIWAY TO TAXIWAY WITH NOSE GEAR AND COCKPIT TRACKS
Figure 4 − 6 Series: 400
Page 7 CHAPTER 4 May 28/2001 AIRPORT PLANNING MANUAL
SCALE 0 25 50 75 100ft 0 10 20 30 m
HOLDING APRON 20 ft (6.10 m) MIN.
100 ft (30.48 m) RADIUS
38 ft (11.58 m) MINIMUM CLEARANCE OF MOVING AIRCRAFT
MAIN GEAR CENTER LINE TRACKS (PORT & STARBOARD) CL
23 ft (7.01 m) MIN. 20 ft (6.10 m) MIN.
75 ft 150 ft (22.86 m) (45.72 m) TAXIWAY WIDTH RUNWAY WIDTH CL brc47a01.dg, pt, 30/03/01 RUNWAY HOLDING BAY (APRON)
Figure 4 − 7 Series: 400
Page 8 CHAPTER 4 May 28/2001 Series: 400 INBOARD 1. Protectivespool. LEGEND 2. Rope. 3. Attachmentsrings. R.H. GEAR 3 C L 2 ICATTEDW RVSOS(Sheet 1of2) AIRCRAFT TIEDOWN PROVISIONS APPROX. 80in. AIRPORT PLANNINGMANUAL (2 m) Figure 4−8 2 2 APPROX. 80in. CHAPTER 4 1 (2 m) APPROX. 40in. 1. LeftMLGsimilar. NOTES 2. Protectgearwithfoamrubber (1 m) or cleancottoncloths,etc.
AFT 3 Dec 05 /2014 ae9 Page
br997a01.dg, sw/gw, aug9/2007 AIRPORT PLANNING MANUAL
TOW SPOOLS
BUNGEE CORD
APPROX. 3 ft (1 m)
APPROX. 3 ft (1 m) br997a02.dg, sw, 15/07/98 AIRCRAFT TIE DOWN PROVISIONS (Sheet 2 of 2)
Figure 4 − 8 Series: 400
Page 10 CHAPTER 4 May 28/2001 CHAPTER 5
TERMINAL SERVICING AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. This chapter supplies ground service information for the Dash−8 Series 400. A. A typical servicing arrangement (no APU) is shown in Figure 5−1. B. Terminal operations are shown in Figure 5−2 and Figure 5−3. C. Locations of ground servicing points are shown in Figure 5−4. D. Data about the ground service connections is shown in Figure 5−5. E. The ground−power electrical requirements for engine starting are shown in Figure 5−6. F. Ground towing requirements are shown in Figure 5−7. G. Ground air conditioning requirements for pre conditioned airplane are shown in Figure 5−8.
Series: 400
Page 1 CHAPTER 5 Dec 05/2014 Series: 400 9 1. Fueltruck. LEGEND 2. Cabinandbuffetservicevehicle. 5. Portablestairway. 4. Tractorwithbaggagecarts. 3. Groundair−conditioningunit For option824CH00114,824SO90105. NOTES Zone aroundfuelvents−keepclearduringrefuelling. (not required,ifoptionalAPUisinstalled). 7 ICATSRIIGARNEET(YIA OAU (Sheet1of3) AIRCRAFT SERVICING ARRANGEMENT(TYPICAL−NOAPU) 8 AIRCRAFT SERVICINGARRANGEMENT (STANDARDCONFIGURATION) 6 9 4 AIRPORT PLANNINGMANUAL Figure 5−1 7. Towingtractor(ifrequired). 8. Toiletservicevehicle. 6. DCelectrical−powerunit. 9. ACelectrical−powerunit. (if required,formaintenanceactivities). CHAPTER 5 5 2 m ft 0 0 1 5 2 SCALE 4 015 10 4 3 Dec 05/2014 20 6 25 ae2 Page 8
br334a01.dg, gv/cs, sep09/2014 Series: 400 9 1. Fueltruck. LEGEND 2. Cabinandbuffetservicevehicle. 5. Portablestairway. 4. Tractorwithbaggagecarts. 3. Groundair−conditioningunit For option824CH00114,824SO90105. NOTES Zone aroundfuelvents−keepclearduringrefuelling. (not required,ifoptionalAPUisinstalled). 7 AIRCRAFT SERVICINGARRANGEMENT (EXTRACAPACITYCONFIGURATION) ICATSRIIGARNEET(YIA OAU (Sheet2of3) AIRCRAFT SERVICING ARRANGEMENT(TYPICAL−NOAPU) 8 6 9 AIRPORT PLANNINGMANUAL Figure 5−1 7. Towingtractor(ifrequired). 8. Toiletservicevehicle. 6. DCelectrical−powerunit. 9. ACelectrical−powerunit. (if required,formaintenanceactivities). CHAPTER 5 5 2 m ft 0 0 1 5 2 SCALE 4 015 10 4 3 Dec 05/2014 20 6 25 ae3 Page 8
br334a02.dg, nn/cs, sep09/2014 Series: 400 HYDRAULIC SYSTEM PRESSURE REFUELLING GROUND AIRCONDITIONING DISPENSER SERVICING/REPLENISHING HYDRAULIC HYDRAULIC POWERUNIT (PRESSURE) HYDRAULIC POWERUNIT GROUND CREWINTERPHONE DC ELECTRICALPOWER TOILET SERVICING AC ELECTRICALPOWER (RETURN) ICATSRIIGARNEET(YIA OAU (Sheet3of3) AIRCRAFT SERVICING ARRANGEMENT(TYPICAL−NOAPU) DESCRIPTION SYSTEM AIRPORT PLANNINGMANUAL SIZE 10 8 4 MS 2651−133ROYLYN’Y’DRAINCOUPLING (OPTIONAL INSTALLATION) MS 24484−2 (NATO 4−WAYJACKPLUG) MATING GROUNDCONNECTORPF051B 72340012−001 (SWITCHCRAFTC−55B); SWITCH −AIRCRAFTCONNECTOR 300 OHMIMPEDANCETHROATMICROPHONEWITH MS 25488(MATINGGROUNDCONNECTOR) MS 3506−1(AIRCRAFTCONNECTOR); MS 335628.00in.(20.32cm);RECEPTACLE PLUS STANDARD1.00in.(2.54cm)FILLPORT CANNON CE9310−10(AIRCRAFTCONNECTOR) CE9183 (MATINGGROUNDCONNECTOR) Figure 5−1 ADAPTER E91HAE81618H AE99111H E94EAE80660E AE99140E E94JAE80660J AE99140J INTERFACE DETAILS EQUIPMENT PROTECTIVE PLUG CHAPTER 5 ADAPTER DPE DUSTCAP ADAPTER E94EAE81724E AE99149E E93JAE81724J AE99139J AE9110H INTERFACE DETAILS AIRCRAFT AE81617H Dec 05/2014 ae4 Page
br334a03.dg, cs, sep09/2014 AIRPORT PLANNING MANUAL
ACTIVITY TIME (MINUTES)
0 2 4 6 8 10 12 14 16 18
Park on ramp Passengers deplane (fwd door) (aft door) Refuel Unload baggage (aft compt.) (fwd compt.) Service toilet Housekeeping Load baggage (aft compt.) (fwd compt.) Passengers enplane (fwd door) (aft door) Clear ramp
DEFINITION DESCRIPTION Park on ramp Aircraft stops, propellers stop turning, insert chocks. Connect external power and cooling equipment or start APU.
Passenger deplane Open forward passenger (airstair) door. Open aft passenger door and position stairs. Passenger use both doors to deplane with carry−on luggage.
Refuel Add fuel for 4 X 200 sm stages. Unload baggage Remove 1.5 pieces per passenger.
Service toilet Use standard external servicing−equipment. Housekeeping Tidy cabin, starting from rear. Service galley. Load baggage Load and stack 1.5 pieces per passenger. Passenger enplane Passenger stow carry−on baggage and are seated. Doors are closed. Clear ramp Disconnect ground, external power and cooling equipment. Start engines and remove chocks.
NOTE Forward baggage compartment and forward baggage door are removed for the extra capacity configuration. g3502a01.dg, cs, sep09/2014 c RAPID TURNAROUND USING FORWARD AND AFT DOORS
Figure 5 − 2 Series: 400
Page 5 CHAPTER 5 Dec 05/2014 AIRPORT PLANNING MANUAL
ACTIVITY TIME (MINUTES)
0246 8 10 12 14 16 18 20 22 24 Park on ramp Passengers deplane (fwd door) Refuel Unload baggage (aft compt.) (fwd compt.) Service toilet Housekeeping Load baggage (aft compt.) (fwd compt.) Passengers enplane (fwd door) Clear ramp
DEFINITION DESCRIPTION Park on ramp Aircraft stops, propellers stop turning, insert chocks. Connect external power and cooling equipment or start APU.
Passenger deplane Open forward passenger (airstair) door. Passenger use forward door to deplane with carry−on luggage.
Refuel Add fuel for 4 X 200 sm stages. Unload baggage Remove 1.5 pieces per passenger.
Service toilet Use standard external servicing−equipment. Housekeeping Tidy cabin, starting from rear. Service galley. Load baggage Load and stack 1.5 pieces per passenger. Passenger enplane Passenger stow carry−on baggage and are seated. Doors are closed. Clear ramp Disconnect ground, external power and cooling equipment. Start engines and remove chocks.
NOTE Forward baggage compartment and forward baggage door are removed for the extra capacity configuration. cg3545a01.dg, cs, sep09/2014 RAPID TURNAROUND USING FORWARD DOOR ONLY
Figure 5 − 3 Series: 400
Page 6 CHAPTER 5 Dec 05/2014 Series: 400 31 12 7 29 6 24 0 GROUND SERVICINGPOINT LOCATIONS(STANDARDCONFIGURATION) 25 32 27 5 SCALE (FT) GROUND SERVICINGPOINT LOCATIONS 33 015 10 8 3 1 1 4 20 25 AIRPORT PLANNINGMANUAL 19 16 19 18 26 17 18 17 Figure 5−4 30 28 26 13 28 15 21 15 20 23 7 CHAPTER 5 14 34 (Sheet 1of4) 9 5 2 11 22 7 10 Dec 05/2014 ae7 Page
cg3539a01.dg, cs, aug06/2014 Series: 400 GROUND SERVICINGPOINT LOCATIONS(STANDARDCONFIGURATION) 19. Engineoilfillerpanel. 18. Magnastick(fuelquantity−underwing−bothsides). 17. Gravityfuelfiller(overwing−bothsides). 16. Aircraftgroundpoint(onundercarriage−bothsides). 15. Groundpoint(overwing−bothsides). 14. Pressurerefuelingpanelandgroundpoint. 13. ElectricalACpowerreceptacle(optionalinstallationonrightnosefuselage). 12. ElectricalDCpowerreceptacle. 11. Optionalconditionedairconnection. 10. Optionalauxiliarypowerunit(APU). LEGEND 29. Noselandinggearjackingpoint. 28. Wingjackingpoint(underwing−bothsides). 27. Nosejackingpoint. 26. Mainlandinggearshockstrutchargingpoint(undernacelle−bothsides). 25. Noselandinggearshockstrutchargingpoint. 24. Emergencylandinggearhydraulicreservoirandhandpump. 23. Brakeaccumulatorandhydraulichandpump. 22. No.3Hydraulicsystem. 21. No.2Hydraulicsystem. 20. No.1Hydraulicsystem. 34. Optionalgalleywaterservice. 33. Wardrobe. 32. Avionicsbay. 31. Crewoxygensupply. 30. Mainlandinggearjackingpoint(bothsides). 1. Forwardpassengerdoor. 7. Interphoneconnectors(3). 8. Lavatoryservice/optionalwashwaterservice. 9. Galleyservicedoor/typeIemergencyexit. 6. Flightcompartmentemergencyexit. 2. Aftbaggagedoor. 5. Aftpassengerdoor. 4. TypeII/IIIemergencyexit. 3. Forwardbaggagedoor. GROUND SERVICINGPOINT LOCATIONS AIRPORT PLANNINGMANUAL Figure 5−4 CHAPTER 5 (Sheet 2of4) Dec 05/2014 ae8 Page
cg3539a02.dg, cs, aug06/2014 Series: 400 30 11 6 GROUND SERVICINGPOINT LOCATIONS(EXTRACAPACITYCONFIGURATION) 28 5 23 0 24 31 26 5 SCALE (FT) GROUND SERVICINGPOINT LOCATIONS 32 7 015 10 1 3 1 20 25 AIRPORT PLANNINGMANUAL 18 15 18 17 25 16 17 16 Figure 5−4 29 27 25 12 27 14 20 14 19 22 6 CHAPTER 5 13 33 (Sheet 3of4) 8 4 2 10 21 6 9 Dec 05/2014 ae9 Page
cg3539a01.dg, cs, sep09/2014 Series: 400 GROUND SERVICINGPOINT LOCATIONS(EXTRACAPACITYCONFIGURATION) 19. No.1Hydraulicsystem. 18. Engineoilfillerpanel. 17. Magnastick(fuelquantity−underwing−bothsides). 16. Gravityfuelfiller(overwing−bothsides). 15. Aircraftgroundpoint(onundercarriage−bothsides). 14. Groundpoint(overwing−bothsides). 13. Pressurerefuelingpanelandgroundpoint. 12. ElectricalACpowerreceptacle(optionalinstallationonrightnosefuselage). 11. ElectricalDCpowerreceptacle. 10. Optionalconditionedairconnection. LEGEND 29. Mainlandinggearjackingpoint(bothsides). 28. Noselandinggearjackingpoint. 27. Wingjackingpoint(underwing−bothsides). 26. Nosejackingpoint. 25. Mainlandinggearshockstrutchargingpoint(undernacelle−bothsides). 24. Noselandinggearshockstrutchargingpoint. 23. Emergencylandinggearhydraulicreservoirandhandpump. 22. Brakeaccumulatorandhydraulichandpump. 21. No.3Hydraulicsystem. 20. No.2Hydraulicsystem. 33. Optionalgalleywaterservice. 32. Wardrobe. 31. Avionicsbay. 30. Crewoxygensupply. 1. Forwardpassengerdoor. 9. Optionalauxiliarypowerunit(APU). 7. Lavatoryservice/optionalwashwaterservice.. 8. Galleyservicedoor/typeIemergencyexit. 6. Interphoneconnectors(3). 2. Aftbaggagedoor. 5. Flightcompartmentemergencyexit. 4. Aftpassengerdoor. 3. ForwardtypeIemergencyexitdoor. GROUND SERVICINGPOINT LOCATIONS AIRPORT PLANNINGMANUAL Figure 5−4 CHAPTER 5 (Sheet 4of4) Dec 05/2014 ae10 Page
cg3539a04.dg, cs, sep09/2014 AIRPORT PLANNING MANUAL SYSTEM DISTANCE DISTANCE FROM HEIGHT AFT OF NOSE AIRCRAFT FROM CENTER LINE GROUND LEFT SIDE RIGHT SIDE FT MFTM FT M FT M Hydraulic System (Phosphate− Ester Based Hydraulic−Fluid) 3 Service Points −Access door on inboard L/H 52 ft 15.9 m 12 ft 3.94 m 8 ft 2.64 m nacelle for No. 1 Hyd. System 2 in. 11 in. 8 in. (reservoir capacity is 8 U.S. quarts, (7.57 L) −Access door on inboard R/H 52 ft 15.9 m 15 ft 4.85 m 8 ft 2.64 m nacelle for No. 2 Hyd. System 2 in. 11 in. 8 in. (reservoir capacity is 12 U.S. quarts, (11.35 L) −No. 3 Hyd. System reservoir 90 ft 27.6 m 1 ft 50.1 cm 7 ft 2.34 m (located in aft fuselage, 8 in. 8 in. 8 in. 2 U.S. quarts, 1.89 L)
Electrical System 2 Service Connections −28 volt DC External Power 4 ft 1.51 m 2 ft 75.2 cm 3 ft 1.16 m Receptacle (capacity is 550 A 11 in. 6 in. 10 in. continuous, 2000 A peak) Nacelle Location 51 ft 15.8 m 12 ft 3.94 m 8 ft 2.52 m −115/200 volt A/C External 11 in. 11 in. 3 in. Power Receptacle (capacity is 20 KVA MIN.,3−PH.,400Hz)
Nose Fuselage Location 4 ft 1.51 m 2 ft 75.2 cm 3 ft 1.16 m −115/200 volt A/C External 11 in. 6 in. 10 in. Power Receptacle (capacity is 20 KVA MIN.,3−PH.,400Hz) Oxygen System
1 Service Connection
−Charging valve for one 39.8 ft 3 4 ft 1.37 m 1 ft 48.3 cm 4 ft 1.22 m (1100 L) Capacity Crew 6 in. 7 in. 0 in. Supply (in nose compartment) Three 11.0 ft 3 (311L) portable passenger cylinders One 11.0 ft 3 (311L) first−aid portable cylinder (optional)
NOTES These measurements are approximate. For option 824CH00114 and 824SO90105.
These measurements are approximate and will vary with aircraft configuration and loading conditions. br887a01.dg, sw/cm, nov13/2013 GROUND SERVICE CONNECTIONS DATA (Sheet 1 of 3)
Figure 5 − 5 Series: 400
Page 11 CHAPTER 5 Dec 05/2014 AIRPORT PLANNING MANUAL
SYSTEM DISTANCE DISTANCE FROM HEIGHT AFT OF NOSE AIRCRAFT FROM CENTER LINE GROUND LEFT SIDE RIGHT SIDE FT M FT M FT M FT M Fuel System
3 Service Points −One Single−Point 58 ft 17.8 m 14 ft 4.40 m 7 ft 2.22 m Refuel/Defuel Adapter 7 in. 5 in. 3 in. (on Refuel/Defuel Panel) −Two over−wing Gravity 49 ft 14.9 m 33 ft 10.1 m 33 ft 10.1 m 12 ft 3.94 m Filling−Points 1 in. 1 in. 1 in. 11 in. (one on each wing) −2 pairs of Fuel Vents 49 ft 14.9 m 34 ft 10.6 m 34 ft 10.6 m 12 ft 3.75 m (one pair under each wing) 0 in. 8 in. 8 in. 4 in.
Landing Gear System
3 Servicing Points (Nitrogen) −One Shock−Strut Valve on each 51 ft 15.8 m 14 ft 4.40 m 14 ft 4.40 m 4 ft 1.44 m Main Gear 9 in. 5 in. 5 in. 9 in. −One Shock−Strut Valve on 6 ft 1.88 m 2 ft 87.5 cm Nose Gear 2 in. 10 in. −Charging Valve for Parking 52 ft 15.9 m 3 ft 1.08 m 10 ft 3.33 m Brake Accumulator (behind 4 in. 11 in. 11 in. access panel on R/H fuselage at wing root). 1 Servicing Point (Phosphate−Ester Based Hydraulic−Fluid). −Filling Point for reservoir 4 ft 1.37 m 2 ft 71.1 cm 3 ft 1.10 m of Alternate Landing−Gear 6 in. 4 in. 7 in. Extension−System (in nose compartment) (1 U.S. quarts, 0.95 L)
These measurements are approximate.
These measurements are approximate and will vary with aircraft configuration and loading conditions. br887a02.dg, sw, 09/06/98 GROUND SERVICE CONNECTIONS DATA (Sheet 2 of 3)
Figure 5 − 5 Series: 400
Page 12 CHAPTER 5 Dec 05/2014 AIRPORT PLANNING MANUAL
SYSTEM DISTANCE DISTANCE FROM HEIGHT AFT OF NOSE AIRCRAFT FROM CENTER LINE GROUND LEFT SIDE RIGHT SIDE FT M FT M FT M FT M Air Conditioning System
1 Air−Conditioning ground connection (optional)
−One 8 inch (20.3 cm) 86 ft 26.3 m 1 ft 54.2 cm 6 ft 1.96 m receptacle (on R/H side of 4 in. 9 in. 5 in. aft fuselage)
Toilet
1 Service Point
−1 Service connection on 14 ft 4.29 m 2 ft 82.5 cm 3 ft 93.2 cm Lavatory Service Panel 1 in. 9 in. 1 in. (capacity of toilet flush reservoir is 3.3 U.S. gallons (13 L))
Oil
2 Servicing Points
−Oil Filter behind access door 40 ft 12.5 m 15 ft 4.85 m 12 ft 3.94 m 9 ft 2.91 m on L/H side of each nacelle 11 in. 11 in. 11 in. 7 in. (tank capacity is 5.9 U.S. gallons (22.3 L)
These measurements are approximate.
These measurements are approximate and will vary with aircraft configuration and loading conditions. br887a03.dg, sw, 09/06/98 GROUND SERVICE CONNECTIONS DATA (Sheet 3 of 3)
Figure 5 − 5 Series: 400
Page 13 CHAPTER 5 Dec 05/2014 Series: 400 NOMINAL STARTING VOLTAGE (VDC) NOTE: SETTHEGROUNDDCPOWERCARTLIMIT TO1500AMPSMINIMUM. 28 3 2 ELECTRICAL REQUIREMENTS FORENGINESTARTING 4 ENGINE STARTCURRENTREQUIRED CONDITIONS ATTYPICALENGINESTART 6 1 FROM GROUNDDCPOWER AIRPORT PLANNINGMANUAL CART (AMPS) 1200−1400 600−800 5 400 Figure 5−6 6. Startergenerator. 1. ExternalDCpowerreceptacle. 2. Batteryinstallation. 5. Ignitionbox. 4. Overheadconsolepanel. 3. DCcontactorbox(includesstart LEGEND control relays). 5 6 CHAPTER 5 CORRESPONDING DURATIONOF CRANKING (SECONDS) 2−3 60 5 Dec 05/2014 ae14 Page
br299a01.dg, pt/ak, apr04/2013 Series: 400
DRAWBAR PULL (x 1000 lb) 3 load is5,250lb(2,381kg). 1 0 2 or pushrequiredis3,000lb(1,360kg)andthetotaltraction wheel of 2%andwithawetconcretesurface,thecorespondingdrawbarpull 7 At anaircraftgrossweightof50,000lb(22,676kg),uphillslope 5 4 6 EXAMPLE : 0 1.5 .5 1.0 2.0 2.5 3.0
1000 KG. TOTAL TRACTIONWHEELLOAD(x1000lb) 2 1 4 1000 KG
2 DRY CONCRETE = 0.80
GROUND TOWINGREQUIREMENTS WET ASPHALT = 0.75 WET CONCRETE = 0.57 SNOW CHAINS = 0.45 u 6 u HARD SNOW = 0.20 AIRPORT PLANNINGMANUAL 3
ICE = 0.05 u u
u 8
u Figure 5−7 4 10 EXAMPLE 5 12 CHAPTER 5 0 1. UNUSUALBREAKWAYCONDITIONS NOT REFLECTED. ASSOCIATED CONDITIONS 2. ESTIMATEDFORTOWVEHICLE 3. COEFFICIENTOFFRICTION(u) WITH RUBBERTIRES. APPROXIMATE. MAX. DESIGNTAXIWEIGHT 64,700 lb.(29,347kg) RUNWAY SLOPE(PERCENTAGE) 1 2 AIRCRAFT GROSS
WEIGHT 30,000 lb (13,605 kg) 64,700 lb (29,347 kg) 40,000 lb (18,141 kg) 50,000 lb (22,676 kg) 60,000 lb (27,211 kg) 3 u Dec 05/2014 4 ae15 Page
brc73a01.dg, sw, 18/01/00 AIRPORT PLANNING MANUAL 30 1.08
1.0
25 0.9
0.8
20 0.7
0.6
15
0.5 PRESSURE PSI INCHES OF WATER
0.4 10
0.3 DUCT ICING LIMIT DUCT OVERHEAT CAUTION 0.2 5
0.1
0 −20 0 2.8 20 40 6071 80 100 INLET TEMPERATURE − C NOTE 0 20 3740 60 80 100 120 140 160 180 200 Acceptable limits INLET TEMPERATURE − F
within shaded area. brbs23a01.dg, kmw, jul30/2014 GROUND AIR CONDITIONING REQUIREMENTS − PRE CONDITIONED AIR
Figure 5 − 8 Series: 400
Page 16 CHAPTER 5 Dec 05/2014 CHAPTER 6
OPERATING CONDITIONS AND NOISE DATA AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. Aircraft operating conditions and noise are important to airport and community planners. While an airport is a major element in an community transportation system and is vital to its growth, it must be a good neighbor. This can only be accomplished with proper planning. Because aircraft noise extends beyond the boundaries of the airport, it is vital to consider the impact on surrounding communities. 2. The Dash−8, Series 400 aircraft is designed with advanced, quiet, turboprop technology. Its noise impact is minimal compared to most aircraft, larger and smaller, currently being operated in a typical airport. 3. To help the airport planner to estimate the impact of the Dash−8 Series 400 on airport operations, the following material is provided: A. Engine Exhaust Temperature Contours (1) Data on the exhaust temperature contours at ground idle, flight idle and take−off power settings are shown in Figure 6−1, Figure 6−2, Figure 6−3, Figure 6−4, Figure 6−5 and Figure 6−6. B. Airport and Community Noise Data for Powerplants (1) Data on the takeoff and landing noise footprints for the PW150A powerplants are shown in Figure 6−7 and Figure 6−8. (2) The Dash−8, Series 400 complies with the Stage 3 noise−level limits under the trade−off clause specified in FAR 36, Section C36.5b and also under AWM 516 and JAR 36 standards. A summary of the certified noise levels, measured and corrected to these standards, is shown in the table that follows: FAR 36 Stage 3 Dash−8 Series 400 Noise Limit Noise Level (EPNdB) (EPNdB) Margin (EPNdB) Take−off 89 78.3 +10.7 Lateral 94 84.2 +9.8 Approach 98 94.9 +3.1 C. Community Noise Data for Optional APU (1) The results of ramp noise tests for the optional APU are shown in Figure 6−9. NOTE: Exhaust temperature contours for the optional APU is not available at this time. D. Propeller/Engine Slipstream Velocity Contours (1) Data on the Propeller/Engine slipstream velocity contours as on ground (18% and 43% torque) and at maximum takeoff power settings are shown in Figure 6−10, and Figure 6−11
Series: 400
Page 1 CHAPTER 6 Dec 05/2014 Series: 400
TOP VIEW − GROUND IDLE ENGINE EXHAUSTTEMP. CONTOURSATGROUNDIDLE−TOPVIEW 80 ASSOCIATED CONDITIONS:
40 1. ALL TEMPERATURES IN o C. 60 50 2. SEA LEVEL, ZERO WIND, ISA DAY. 60 70 3. 660 RPM NP. 4. ZERO PROPELLER PRESSURE RISE
80 ASSUMED. AIRPORT PLANNINGMANUAL 100 150 20 40 Figure 6−1 0 CHAPTER 6 −20
EXHAUST NOZZLES (ft) AIRCRAFT SYMMETRY PLANE −40 −60 −80
Dec 05/2014 0 20 40 60 80 100 120 140 DISTANCE DOWNSTREAM FROM NOZZLES (ft) ae2 Page
brn10a01.dg, sw/kmw, oct02/2013 Series: 400
SIDE VIEW − GROUND IDLE ENGINE EXHAUSTTEMP. CONTOURSATGROUNDIDLE−SIDEVIEW 80 ASSOCIATED CONDITIONS:
1. ALL TEMPERATURES IN o C. 70 2. SEA LEVEL, ZERO WIND, ISA DAY. 3. 660 RPM NP. 4. ZERO PROPELLER PRESSURE RISE
60 ASSUMED. AIRPORT PLANNINGMANUAL 50 Figure 6−2
40 40 50
60 30 CHAPTER 6
EXHAUST NOZZLES (ft) 70 80 20 100 150 10 GROUND 0 0 20 40 60 80 100 120 140 Dec 05/2014 DISTANCE DOWNSTREAM FROM NOZZLES (ft) ae3 Page
brn09a01.dg, sw/gw, may5/2011 Series: 400
TOP VIEW − FLIGHT IDLE ENGINE EXHAUSTTEMP. CONTOURSATFLIGHTIDLE−TOPVIEW 80 ASSOCIATED CONDITIONS:
1. ALL TEMPERATURES IN o C. 60 40 2. SEA LEVEL, ZERO WIND, ISA DAY. 50 60 3. 660 RPM NP. 70 4. ZERO PROPELLER PRESSURE RISE 80
100 ASSUMED. AIRPORT PLANNINGMANUAL 150 20 40 Figure 6−3 0 CHAPTER 6 −20
EXHAUST NOZZLES (ft) AIRCRAFT SYMMETRY PLANE −40 −60 −80
Dec 05/2014 0 20 40 60 80 100 120 140 DISTANCE DOWNSTREAM FROM NOZZLES (ft) ae4 Page
brn08a01.dg, sw/kmw, oct02/2013 Series: 400
SIDE VIEW − FLIGHT IDLE ENGINE EXHAUSTTEMP. CONTOURSATFLIGHTIDLE−SIDEVIEW 80 ASSOCIATED CONDITIONS:
1. ALL TEMPERATURES IN o C. 70 2. SEA LEVEL, ZERO WIND, ISA DAY. 3. 660 RPM NP. 4. ZERO PROPELLER PRESSURE RISE
60 ASSUMED. AIRPORT PLANNINGMANUAL 50 Figure 6−4 40 40 50
60 30 CHAPTER 6
EXHAUST NOZZLES (ft) 70 80 20 100 150 10 GROUND 0 0 20 40 60 80 100 120 140 Dec 05/2014 DISTANCE DOWNSTREAM FROM NOZZLES (ft) ae5 Page
brn07a01.dg, sw/gw, may9/2011 Series: 400
ENGINE EXHAUSTTEMP. CONTOURSATMAX.T.O.POWER−TOP VIEW TOP VIEW − MAX. TAKE−OFF 80 ASSOCIATED CONDITIONS:
40 1. ALL TEMPERATURES IN o C. 60 50 2. SEA LEVEL, ZERO WIND, ISA DAY. 60 70 3. 100 % NP. 4. ZERO PROPELLER PRESSURE RISE 40
80 ASSUMED. AIRPORT PLANNINGMANUAL 100 150 20 Figure 6−5 0 CHAPTER 6 −20
EXHAUST NOZZLES (ft) AIRCRAFT SYMMETRY PLANE −40 −60 −80
May 28 /2001 0 20 40 60 80 100 120 140 DISTANCE DOWNSTREAM FROM NOZZLES (ft) ae6 Page
brn06a01.dg, sw, 29/09/99 Series: 400
ENGINE EXHAUSTTEMP. CONTOURSATMAX.T.O.POWER−SIDE VIEW SIDE VIEW − MAX. TAKE−OFF 80 ASSOCIATED CONDITIONS:
1. ALL TEMPERATURES IN o C. 70 2. SEA LEVEL, ZERO WIND, ISA DAY. 3. 100 % NP. 4. ZERO PROPELLER PRESSURE RISE 60
ASSUMED. AIRPORT PLANNINGMANUAL 50 Figure 6−
40 40 50
CHAPTER 6 60 30
EXHAUST NOZZLES (ft) 70 80 20 100 150 10 GROUND 0
Dec 05 /2014 0 20 40 60 80 100 120 140 DISTANCE DOWNSTREAM FROM NOZZLES (ft) ae7 Page
brn05a01.dg, sw, 21/09/99 Series: 400 TAKEOFF ANDLANDING NOISEFOOTPRINT−3DEGREEAPPROACH
3 DEGREES APPROACH 15.81 % TAKEOFF GRADIENT 9.2 %CLIMB GRADIENT AT 850 RPM AT 1020 RPM AT MAX. CLIMB POWER 1000 m 35 DEG. FLAPS CUTBACK ALTITUDE 2 1000 ft 0 0 7 654 3 210 1 2 3 4 5 6 7 HEIGHT ABOVE
DISTANCE FROM RUNWAY THRESHOLD − 1000 M RUNWAY − 1000 FT AIRPORT PLANNINGMANUAL
1000 m
Figure 6−7 70 2 0 0 75 2 1000 m 80 1000 − FT 85
AREA ENCLOSED DISTANCE TO SIDE CHAPTER 6 NOISE LEVEL (dBA) (SQ. MILES) (SQ. KM) 70 2.677 6.933 75 1.262 3.269 80 0.575 1.490 85 0.271 0.702
o ASSOCIATED CONDITIONS: 1. SEA LEVEL. ISA + 10 C., ZERO WIND. SCALE: 2. TAKEOFF WT. − 63,250 lb (28,750 kg). 1 in. = 6000 ft. 3. LANDING WT. − 61,250 lb (27,841 kg).
25 20 15 10 5 0 5 10 15 20 25 May 28/2001 DISTANCE FROM RUNWAY THRESHOLD − 1000 FT ae8 Page
brn11a01.dg, sw, 30/09/99 Series: 400 TAKEOFF ANDLANDING NOISEFOOTPRINT−4DEGREESAPPROACH
4 DEGREES APPROACH 15.81 % TAKEOFF GRADIENT 9.2 %CLIMB GRADIENT AT 1020 RPM AT 1020 RPM AT MAX. CLIMB POWER 1000 m 35 DEG. FLAPS CUTBACK ALTITUDE 2 1000 ft 0 0 7 654 3 210 1 2 3 4 5 6 7 HEIGHT ABOVE
DISTANCE FROM RUNWAY THRESHOLD − 1000 M RUNWAY − 1000 FT AIRPORT PLANNINGMANUAL
1000 m 70 Figure 6−8 2 0 0 75 2
1000 m 80 1000 − FT 85
AREA ENCLOSED DISTANCE TO SIDE CHAPTER 6 NOISE LEVEL (dBA) (SQ. MILES) (SQ. KM) 70 2.381 6.166 75 1.149 2.975 80 0.529 1.369 85 0.252 0.652
o ASSOCIATED CONDITIONS: 1. SEA LEVEL. ISA + 10 C., ZERO WIND. SCALE: 2. TAKEOFF WT. − 63,250 lb (28,750 kg). 1 in. = 6000 ft. 3. LANDING WT. − 61,250 lb (27,841 kg).
25 20 15 10 5 0 5 10 15 20 25 May 28 /2001 DISTANCE FROM RUNWAY THRESHOLD − 1000 FT ae9 Page
brn12a01.dg, sw, 01/10/99 Series: 400 15 17 13 14 18 16 19 20 21 Forward typeIemergency exit doorisinstalledonlyonaircraftwithextracapacity configuration. NOTE DOOR) DOOR) DOOR) BAGG. (FWD (AFT (AFT PAX PAX 211 12 223 22 30 2 1 RAMP NOISETESTRESULTS FOROPTIONALAPU SERVICE (GALLEY 3 29 DOOR) EMERGENCY (FWD BAGG. (REFUELING) DOOR/FWD EXIT DOOR) (20.0 m) 65.6 ft 4 TYPE I 10 AIRPORT PLANNINGMANUAL 24 Figure 6−9 7 8 9 6 28 27 26 5 25 OPERATING CONDITIONS Recirculation fan:on Pneumatic load:36.3kg/min ACM operatingmode:maximumcooling APU exhaustgastemperature:1,173C APU shaftspeed:100%or64,154RPM APU shaftload:65%or260Amps(100%=400Amps) APU normalratedspeed:64,154RPM Air conditioningpacksoperating:2 (20.0 m) 65.6 ft CHAPTER 6 POSITION dB(A) APU /ECSNOISEREADINGS 14 10 15 13 12 11 7 6 8 9 4 2 5 3 1 79 79 84 84 84 70 85 82 83 82 83 83 82 82 81 o 16 19 18 17 26 29 27 24 28 20 25 30 23 22 21 Dec 05/2014 ae10 Page 76 77 74 78 66 78 75 69 67 80 73 72 68 72 63
braa9a01.dg, ab/cs, jul30/2014 PROPELLER /ENGINE SLIPSTREAMVELOCITYCONTOURATMAXIMUM TAKEOFFPOWER Series: 400 DISTANCE FROM AIRCRAFT CENTERLINE (FT) −300 −200 −100 100 200 0 160 ft/sec 0 0 0 0 0 0 0 800 700 600 500 400 300 200 100 120 ft/sec 140 ft/sec 100 ft/sec PROPELLER/ENGINE SLIPSTREAMVELOCITYCONTOURS DISTANCE DOWNSTREAMPROPELLERPLANE(FT) 80 ft/sec AIRPORT PLANNINGMANUAL (MAXIMUM TAKEOFFPOWER) 60 ft/sec Figure 6−10 40 ft/sec CHAPTER 6 20 ft/sec Dec 05/2014 ae11 Page
cg2866a01.dg, ms, aug30/2013 Series: 400 PROPELLER /ENGINE SLIPSTREAMVELOCITYCONTOURASONGROUND DISTANCE FROM DISTANCE FROM AIRCRAFT CENTERLINE (FT)
−100 AIRCRAFT CENTERLINE (FT) PROPELLER/ENGINE SLIPSTREAMVELOCITYCONTOURS(~18%TORQUE) PROPELLER/ENGINE SLIPSTREAMVELOCITYCONTOURS(~43%TORQUE) −200 −100 100 100 0 0 DISTANCE DOWNSTREAMPROPELLERPLANE(FT) DISTANCE DOWNSTREAM PROPELLERPLANE(FT) 90 ft/sec 0 0 0 0 500 400 300 200 100 80 ft/sec 100 AIRPORT PLANNINGMANUAL 70 ft/sec (STATIONARY ONGROUND) (STATIONARY ONGROUND) 50 ft/sec 60 ft/sec Figure 6−11 40 ft/sec 50 ft/sec 200 40 ft/sec 30 ft/sec CHAPTER 6 30 ft/sec 25 ft/sec 300 20 ft/sec 20 ft/sec Dec 05/2014 ae12 Page
cg2865a01.dg, ms, aug30/2013 CHAPTER 7
PAVEMENT DATA AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. The pavement requirements for commercial aircraft are customarily derived from the static analysis loads imposed on the main landing−gear wheels and tires through the shock struts. A. Basic data on the landing−gear footprint configuration, maximum−design taxi loads, and tire sizes and pressures are shown in Figure 7−1. B. Maximum pavement loads for certain critical conditions at the tire−ground interfaces are shown in Figure 7−2. C. Landing−gear loading on pavement at various aircraft weights is shown in Figure 7−3. D. The California Bearing Ratio (CBR) for unlimited commercial use at all aircraft weights is shown in Figure 7−4 and Figure 7−5. E. The minimum Load Classification Number (LCN) for flexible and rigid pavement are shown in Figure 7−6, Figure 7−7, Figure 7−8 and Figure 7−9. F. The minimum Aircraft Classification Number (ACN) for flexible and rigid pavement are shown in Figure 7−10, Figure 7−11, Figure 7−12 and Figure 7−13. 2. Make sure that all runways or pavements to be used meet these minimum CBR, LCN and ACN requirements.
Series: 400
Page 1 CHAPTER 7 May 28/2001 Series: 400 PERCENTAGE WEIGHTONMAINGEAR Refer toAMMCh.12forservicepressure. NOTE Tire pressuresshownareforcalculationpurposesonly. NOSE−GEAR TIREPRESSURE MAIN−GEAR TIREPRESSURE MAXIMUM DESIGNTAXIWEIGHT NOSE−GEAR TIRESIZE MAIN−GEAR TIRESIZE 15.0 in. (38.1 cm) LANDING GEARFOOTPRINT AIRPORT PLANNINGMANUAL Figure 7−1 (13.94 m) 45 ft9in. (REFER TOLANDINGGEARLOADINGON OPT −135PSI(931kPa)UNLOADED STD −218PSI(1503kPa)UNLOADED (49.63 cm) OPTIONAL 19.54 in. (53.34 cm) STANDARD 21.0 in. PAVEMENT ILLUSTRATION) 34 x10.75−16OPTIONAL 32 x8.8−16STANDARD 85 PSI(586kPa)UNLOADED 89 PSI(614kPa)LOADED 227 PSI(1565kPa)LOADED 141 PSI(972kPa)LOADED CHAPTER 7 22 x6.50−10 (29,347 kg) 64,700 lb 28 ft10in. (8.8 m) May 28/2001 ae2 Page
brc74a01.dg, gg/sw, 18/01/00 MODEL Series: 400 402 1 2 3 Instantaneous brakingappliedduringasteady run. Maximum main−gearhorizontal−forceexcludesthealleviating effectofnose−gearrollingfriction. Upper C.G.limitisapproximately12.77ft(3.89m)above groundline. H =MaximumHorizontalGroundLoadfromBraking. V =MaximumVerticalNose−GearGroundLoadatMostForwardC.G.. All loadscalculatedusingaircraftMaximumDesignTaxiWeight. V =MaximumVerticalMain−GearGroundLoadatMost AftC.G.. NOTES: MG NG (29,347 kg) MAXIMUM 64,700 lb WEIGHT DESIGN TAXI V NG FORWARD (2929 kg) (AT MOST 6458 lb STATIC C.G.) V NG STATIC +BRAKING MAXIMUM PAVEMENT LOADS DECELERATION (3.05 m/sec) AT 10ft/sec AIRPORT PLANNINGMANUAL (5514 kg) 12,159 lb H 2 Figure 7−2 2 1 V MG OCCURRING AT STATIC AFTC.G. V MAXIMUM (13,682 kg) MG (PERSTRUT) 30,169 lb LOAD CHAPTER 7 DECELERATION BRAKING OF AT STEADY (3.05 m/sec) 10 ft/sec (4249 kg) 9369 lb 2 2 2 H (PERSTRUT) INSTANTANEOUS OF FRICTION0.8) (COEFFICIENT BRAKING (10,946 kg) 24,135 lb AT May 28/2001 ae3 Page 3
brc75a01.dg, pt/sw, 18/01/00 Series: 400
WEIGHT ON MAIN LANDING GEAR (X 1000 LB) 45 70 65 55 60 40 50 30 35 85.00 NOTE Unshaded arearepresentsoperationallimits. PERCENT OFWEIGHTONMAINGEAR LANDING GEARLOADING ONPAVEMENT 10 10 90.00 AIRPORT PLANNINGMANUAL PERCENT MAC 20 20 64,700 LB 53,000 LB 35,000 LB 45,000 LB 61,75O LB Figure 7−3 30 30 40 40 CHAPTER 7 95.00 100.00 May 28/2001 45 70 65 60 55 40 50 35 30 ae4 Page
AIRCRAFT GROSS WEIGHT (X 1000 LB) brr39a01.dg, sw, 24/01/00 AIRPORT PLANNING MANUAL
CALIFORNIA BEARING RATIO (CBR)
35 10 20 30
AIRCRAFT WEIGHT 64,700 LB 55,000 LB 45,000 LB 35,000 LB
ANNUAL DEPARTURES (20 YEAR PAVEMENT LIFE) 1,200 3,000 6,000 15,000 25,000
35 10 20 30
FLEXIBLE PAVEMENT THICKNESS (INCHES)
NOTES 1. Tires are 32 x 8.8−16 (21.0 in. centers), inflated to 227 psi (1565 kPa), loaded. 2. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 3. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). 4. U.S. Army Corps of Engineers design method (S−77−1) and FAA design method used. re57a01.dg, sw, 19/01/00 b FLEXIBLE PAVEMENT REQUIREMENTS − CBR (32X8.8−16 TIRES)
Figure 7 − 4 Series: 400
Page 5 CHAPTER 7 May 28/2001 AIRPORT PLANNING MANUAL
CALIFORNIA BEARING RATIO (CBR)
35 10 20 30
AIRCRAFT WEIGHT 64,700 LB 55,000 LB 45,000 LB 35,000 LB
ANNUAL DEPARTURES (20 YEAR PAVEMENT LIFE) 1,200 3,000 6,000 15,000 25,000
35 10 20 30
FLEXIBLE PAVEMENT THICKNESS (INCHES) NOTES 1. Tires are 34 x 10.75−16 (19.5 in. centers), inflated to 141 psi (972 kPa), loaded. 2. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 3. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). 4. U.S. Army Corps of Engineers design method (S−77−1) and FAA design method used. re58a01.dg, sw, 19/01/00 b FLEXIBLE PAVEMENT REQUIREMENTS − CBR (34X10.75−16 TIRES)
Figure 7 − 5 Series: 400
Page 6 CHAPTER 7 May 28/2001 Series: 400 FLEXIBLE PAVEMENT REQUIREMENTS −LCNCONVERSION(32X8.8−16 TIRES)
A 30 30 B
C 20 20 D
10 10
AIRCRAFT WEIGHT AIRPORT PLANNINGMANUAL
(X 1000 LB) A − 64,700 LB B − 55,000 LB ESWL (X 1000 LB) C − 45,000 LB 5 Figure 7−6 5 D − 35,000 LB
5 6 7 8 9 10 20 30 40 50 10 20 30 40 50 EQUIVALENT SINGLE − WHEEL LOAD (ESWL) EQUIVALENT SINGLE − WHEEL PAVEMENT THICKNESS (in.) LOAD CLASSIFICATION NUMBER
CHAPTER 7 (LCN)
NOTES 1. Tires are 32 x 8.8−16 (21.0 in. centers). 2. 227 psi (1565 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% at approx. 94% of weight on MLG). May 28/2001 ae7 Page
brc90a01.dg, sw, 19/01/00 Series: 400 FLEXIBLE PAVEMENT REQUIREMENTS −LCNCONVERSION(34X10.75−16 TIRES)
A 30 30 B C 20 20 D AIRPORT PLANNINGMANUAL
AIRCRAFT WEIGHT
(X 1000 LB) 10 10
A−64,700 LB ESWL (X 1000 LB) Figure 7− 8 B−55,000 LB 8 C−45,000 LB D−35,000 LB
5 10 20 30 40 50 10 20 30 40 EQUIVALENT SINGLE − WHEEL LOAD (ESWL) EQUIVALENT SINGLE − WHEEL
CHAPTER 7 PAVEMENT THICKNESS (in.) LOAD CLASSIFICATION NUMBER (LCN)
NOTES 1. Tires are 34 x 10.75−16 (19.5 in. centers). 2. 141 psi (972 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). May 28/2001 ae8 Page
brc91a01.dg, sw, 19/01/00 Series: 400 RIGID PAVEMENTREQUIREMENTS −LCNCONVERSION(32X8.8−16 TIRES)
30 30 A
20 B 20 C
D 10 10 AIRPORT PLANNINGMANUAL AIRCRAFT WEIGHT (X 1000 LB) A − 64,700 LB ESWL (X 1000 LB)
Figure 7−8 B − 55,000 LB C − 45,000 LB 5 D − 35,000 LB 5 10 50 100 10 20 30 40 EQUIVALENT SINGLE − WHEEL LOAD (ESWL) EQUIVALENT SINGLE − WHEEL
CHAPTER 7 RADIUS OF RELATIVE STIFFNESS (L) LOAD CLASSIFICATION NUMBER (LCN)
NOTES 1. Tires are 32 x 8.8−16 (21.0 in. centers). 2. 227 psi (1565 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). May 28/2001 ae9 Page
brc92a01.dg, sw, 20/01/00 Series: 400 RIGID PAVEMENTREQUIREMENTS −LCNCONVERSION(34X10.75−16 TIRES)
30 30 A B 20 20 C
D
10
(X 1000 LB) 10 AIRPORT PLANNINGMANUAL
AIRCRAFT WEIGHT ESWL (X 1000 LB) A − 63,450 LB B − 55,000 LB C − 45,000 LB Figure 7−9 D − 35,312 LB 10 50 100 10 20 30 40
EQUIVALENT SINGLE − WHEEL LOAD (ESWL) EQUIVALENT SINGLE − WHEEL RADIUS OF RELATIVE STIFFNESS (L) LOAD CLASSIFICATION NUMBER (LCN) CHAPTER 7
NOTES 1. Tires are 34 x 10.75−16 (19.5 in. centers). 2. 141 psi (972 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). May 28/2001 ae10 Page
brc93a01.dg, sw, 21/01/00 AIRPORT PLANNING MANUAL
20 D
C
B A 15
10
A − CBR 15 5
AIRCRAFT CLASSIFICATION NUMBER (ACN) B − CBR 10 C − CBR 6 D − CBR 3
0 30000 35000 40000 45000 50000 55000 60000 65000
AIRCRAFT GROSS WEIGHT (LBS)
NOTES 1. Tires are 32 x 8.8−16 (21.0 in. centers). 2. 227 psi (1565 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). rc94a01.dg, sw, 21/01/00 b AIRCRAFT CLASSIFICATION NUMBER − FLEXIBLE PAVEMENT (32X8.8−16 TIRES)
Figure 7 − 10 Series: 400
Page 11 CHAPTER 7 May 28/2001 AIRPORT PLANNING MANUAL
D 20
C
B
15 A
10
A − CBR 15
AIRCRAFT CLASSIFICATION NUMBER (ACN) 5 B − CBR 10 C − CBR 6 D − CBR 3
0 30000 35000 40000 45000 50000 55000 60000 65000
AIRCRAFT GROSS WEIGHT (LBS)
NOTES 1. Tires are 34 x 10.75−16 (19.5 in. centers). 2. 141 psi (972 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). rc95a01.dg, sw, 21/01/00 b AIRCRAFT CLASSIFICATION NUMBER − FLEXIBLE PAVEMENT (34X10.75−16 TIRES)
Figure 7 − 11 Series: 400
Page 12 CHAPTER 7 May 28/2001 AIRPORT PLANNING MANUAL
25
D C 20 B A SUBGRADE MODULUS − K A − 550 LBF/IN3 −HIGH B − 300 LBF/IN 3 −MEDIUM C − 150 LBF/IN 3 −LOW D − 75 LBF/IN 3 −ULTRA LOW 15
AIRCRAFT CLASSIFICATION NUMBER (ACN) 10
5 30000 35000 40000 45000 50000 55000 60000 65000
AIRCRAFT GROSS WEIGHT (LBS)
NOTES 1. Tires are 32 x 8.8−16 (21.0 in. centers). 2. 227 psi (1565 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). rc96a01.dg, pt/sw, 18/01/00 b AIRCRAFT CLASSIFICATION NUMBER − RIGID PAVEMENT (32X8.8−16 TIRES)
Figure 7 − 12 Series: 400
Page 13 CHAPTER 7 May 28/2001 AIRPORT PLANNING MANUAL
25
20 D SUBGRADE C MODULUS − K B 3 A − 550 LBF/IN −HIGH A B − 300 LBF/IN 3 −MEDIUM C − 150 LBF/IN 3 −LOW D − 75 LBF/IN 3 −ULTRA LOW 15
AIRCRAFT CLASSIFICATION NUMBER (ACN) 10
5 30000 35000 40000 45000 50000 55000 60000 65000
AIRCRAFT GROSS WEIGHT (LBS)
NOTES 1. Tires are 34 x 10.75−16 (19.5 in. centers). 2. 141 psi (972 kPa) inflation pressure (loaded). 3. Tire pressure is for calculation purposes only, refer to AMM Ch 12 for service pressures. 4. Max. Aft C.G. (36% MAC at approx. 94% of weight on MLG). brc97a01.dg, pt/sw, 18/01/00 AIRCRAFT CLASSIFICATION NUMBER − RIGID PAVEMENT (34X10.75−16 TIRES)
Figure 7 − 13 Series: 400
Page 14 CHAPTER 7 May 28/2001 CHAPTER 8
DERIVATIVE AIRCRAFT AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. There are no plans to develop any derivative aircraft at this time.
Series: 400
Page 1 CHAPTER 8 May 28/2001 AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK CHAPTER 9
SCALED DRAWINGS OF DASH-8 SERIES 400 AIRPORT PLANNING MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK AIRPORT PLANNING MANUAL
General Information
1. The scaled drawings that follow can be used to plan/verify runway, ramp and maintenance facility layouts. A. The 1 in. = 32 ft. (1:384) scaled drawing is shown in Figure 9−1. B. The 1 in. = 50 ft (1:600) and 1 in. = 100 ft (1:1200) scaled drawings are shown in Figure 9−2. C. The 1:500 and 1:1000 (Metric) scaled drawings are shown in Figure 9−3.
Series: 400
Page 1 CHAPTER 9 May 28/2001 Series: 400 2 Forward typeIemergencyexitdoorisinstalledonlyon aircraftwithextracapacityconfiguration. Type II/IIIemergencyexitdoor isde−activatedfortheextracapacityconfiguration. NOTES SCALED DASH8,SERIES 400(MODEL402)DRAWING−1IN.=32FT (1:384) V 70 o MLG E2 E1 L F B1 NLG MLG B2 LEGEND V X4 X3 X2 X1 A2 A1 B2 X3 E1 X1 Forward passengerairstairdoor. Fuel vent(onbothwings). Pressure refuelingpoint. Forward baggagecompartment/ Lavatory. Electrical connection(AC). Electrical connection(DC). Nose landinggear. Main landinggear. Galley servicedoor. Ground air−conditioningconnection(ifnoAPUisinstalled). Type II/IIIemergencyexit. forward typeIemergencyexitdoor Aft passengerdoor. Aft baggagecompartment. Air conditioning. Turning radiuspoints:70 AIRPORT PLANNINGMANUAL 1 IN=32FT(1:384) NLG A1 X4 B1 X2 L A2 Figure 9−1 F E2 MLG o , 60 2 o , 50 o CHAPTER 9 , 40 o , 30 o , 25 o TURNING RADIUSPOINTS , 20 o . 70 60 25 50 40 30 Dec 05/2014 o o o o o o 20 o ae2 Page
brb09a01.dg, gv/cs, jul30/2014 Series: 400 2 Forward typeIemergencyexitdoorisinstalledonlyon aircraftwithextracapacityconfiguration. Type II/IIIemergencyexitdoor isde−activatedfortheextracapacityconfiguration. NOTES SCALED (MODEL402) DRAWING −1IN.=50FT(1:600),100 FT (1:1200) V 70 MLG o B2 X3 1 IN=50FT(1:600) X1 L F E2 E1 B1 NLG MLG B2 LEGEND V X3 X2 X1 X4 A2 A1 E1 Pressure refuelingpoint. Forward passengerairstairdoor. Fuel vent(onbothwings). Lavatory. Electrical connection(AC). Electrical connection(DC). Forward baggagecompartment/ Nose landinggear. Main landinggear. Galley servicedoor. Ground air−conditioningconnection(ifnoAPUisinstalled). Type II/IIIemergencyexit. forward typeIemergencyexitdoor Turning radiuspoints:70 Aft passengerdoor. Aft baggagecompartment. Air conditioning. NLG A1 B1 X2 L MLG X4 A2 AIRPORT PLANNINGMANUAL E2 F Figure 9−2 TURNING RADIUSPOINTS o , 60 2 o , 50 o , 40 CHAPTER 9 o 20 70 60 25 50 40 30 , 30 o o o o o o o o , 25 1 IN=100FT(1:1200) o , 20 o . Dec 05/2014 ae3 Page
brb40a01.dg, gv/cs, jul30/2014 Series: 400 SCALED DASH8,SERIES 400(MODEL402)DRAWING−1:500AND 1:1000(METRIC) 2 V Forward typeIemergencyexitdoorisinstalledonlyon aircraftwithextracapacityconfiguration. Type II/IIIemergencyexitdoor isde−activatedfortheextracapacityconfiguration. 70 NOTES o MLG X3 B2 X1 E1 L F E2 E1 B1 NLG MLG B2 LEGEND V X4 X3 X2 X1 A2 A1 SCALE 1:500 Pressure refuelingpoint. Forward passengerairstairdoor. Fuel vent(onbothwings). Lavatory. Electrical connection(AC). Electrical connection(DC). Forward baggagecompartment/ Nose landinggear. Main landinggear. Galley servicedoor. Ground air−conditioningconnection(ifnoAPUisinstalled). Type II/IIIemergencyexit. forward typeIemergencyexitdoor Aft passengerdoor. Aft baggagecompartment. Air conditioning. Turning radiuspoints:70 NLG A1 X2 B1 L MLG AIRPORT PLANNINGMANUAL X4 A2 E2 F Figure 9−3 TURNING RADIUSPOINTS o , 60 2 o , 50 o CHAPTER 9 , 40 o , 30 o , 25 20 70 60 25 50 40 30 o o , 20 o o o o o o SCALE 1:1000 o . Dec 05/2014 ae4 Page
brb41a01.dg, gv/cs, jul30/2014