Aircraft Rescue Firefighting Guide

UPS Flight Operations October 2018

A MESSAGE FROM THE UPS AIRLINES CHIEF PILOT

Global Operations Center 825 Lotus Avenue Louisville, KY 40213

To: All Airport Rescue & Fire Fighting Department Chiefs From: UPS Airlines, Flight Operations Date: October 2018

UPS has provided your department with this updated guide depicting UPS cargo aircraft. This document provides basic aircraft layouts and important information relevant to Aircraft Rescue & Fire Fighting (ARFF) responders. These include locations of significant components, freight containers, and crew/occupant seating. Also included are tactical considerations for the incident commander.

This guide may be used for ARFF training and maintained as a reference guide for future emergency response to UPS aircraft. The “Considerations for ARFF Responding to a UPS Aircraft” were developed with input from highly experienced members of the ARFF Working Group. This guide was created in cooperation with UPS Airlines Flight Operations and the Independent Pilots Association with contributions by the SDF Department of Public Safety.

It is Intended for REFERENCE ONLY and may be updated by UPS Airlines as the UPS fleet evolves to different models.

Safe Regards,

Captain Chris Williams Chief Pilot UPS Airlines 3

Global Operations Center INTRODUCTION 825 Lotus Avenue Louisville, KY 40213

UPS Aircraft Rescue Contents Firefighting Guide BOEING The UPS policy book defines the company’s values, mission, and strategy. A common 757-200F theme amongst these items is safety. The safety of our employees, customers, and the Pg. 7 general public is of utmost importance. UPS believes that there is no room for unsafe work practices in any aspect of our operations. This document was designed with Aircraft Rescue and Fire Fighting (ARFF) needs in mind. It provides important safety AIRBUS information to improve the ability of ARFF departments to respond to UPS Aircraft N120UP A300-600F during an emergency. The information included in this document is for reference use Pg. 20 only, and was developed with input from experienced members of the ARFF Working Group. BOEING Questions and comments regarding this reference guide can be directed to: 767-300F Pg. 33 Jeff Lassell UPS Airlines ARFF Training Coordinator 802 Grade Lane Louisville, 40213 BOEING MD-11F Contact phone: 502-338-4402 Pg. 46 Email: [email protected]

BOEING N570UP 747-400F Pg. 60

BOEING 747-8F Pg. 73 5

BOEING 757-200F UPS Aircraft Rescue Firefighting Guide

Max. Payload: 86,900 LBS

Main Deck: 15 containers

Max. Fuel 75,000 LBS Load: 11,240 GAL (42,548 LIT)

Range: 1,840-1,950 NM

Cruising Speed: 465 KTS/535 MPH

Engines: Rolls Royce RB211 Pratt & Whitney 2040

For Emergency Responders; Direct Contact Numbers to UPS Flight Operations

UPS System Operations: 502.359.5350

UPS Flight Control: 502.359.5100

UPS HAZMAT 502.380.1800 Support Center: 800.554.9964 BOEING INTAKES AND EXHAUST 757-200F

9 ft – NO Entry (2.7M) 1650 ft 50 ft (15M) (503M) RADIUS

TAKE OFF THRUST

CAUTION INLET DANGER AREA EXHAUST DANGER AREA Typical Intake & Exhaust Hazards

IDLE THRUST

180 ft 25 ft (8M) 5 ft (55M) RADIUS (1.5M)

TAKE OFF THRUST VISUALIZED Ft M 100 30 60 20 10 20 0 Feet 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000

Meters 0 25 50 75 100 125 150 175 200 225 250 275 300 325 350 375 400 425 450 475 500 525 550 575 600 625 6508 675 700 725 750 775 800 825 850 875 900 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING EMERGENCY RESCUE ACCESS 757-200 PACKAGE FREIGHTER EMERGENCY757-200F RESCUE ACCESS-2

2” WIDE BAND OF CONTRASTING COLOR INDICATING ALL DOORS, HAO PT ECHES N AND WINDOWS EXTERNALLY OPERABLE.

APU ACCESS P P U U 2 CUT-IN AREAS S L (NOT MARKED ON ALL AIRPLANES) H L

EMERGENCY EXIT PULL HANDLE UNFOLD CRANK ROTATE AS SHOWN

WINDOW DETAIL LOWER DECK CARGO DOOR ON RIGHT SIDE - OPERATING INSTRUCTIONS ON DOOR

LOWER DECK CARGO DOOR ON RIGHT SIDE - OPERATING INSTRUCTIONS ON DOOR

PILOT’S WINDOW ON RIGHT SIDE ONLY

SIDE CARGO DOOR

AVERAGE DISTANCE FLOOR LEVEL TO GROUND 1 ENTRY DOOR WHEELS RETRACTED: 6 FT 6 IN WHEELS EXTENDED: 13 FT

For Reference Only, some configurations may vary. 9

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 757.1.3 BOEING EMERGENCY RESCUE ACCESS 757-200F

MAXIMUM SEATING CAPACITY FOR FLIGHT: SIX (6) PEOPLE

Lavatory Entry Door

Small Cargo Access Door

For Reference Only, some configurations may vary. 10 BOEING EMERGENCY RESCUE ACCESS 757-200F

EMERGENCY ESCAPE ROPES THRU OPEN WINDOWS OR DOOR

56"

CREW ENTRY DOOR DOOR OPENS INWARD HINGES ON RIGHT

EMERGENCY ESCAPE INERTIAL REEL DEVICES THRU OPEN DOOR 22"

For Reference Only, some configurations may vary. 11 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION

757-200 PACKAGE FREIGHTER FLIGHT DECK CONTROL SWITCHBOEING LOCATIONS FLIGHT DECK CONTROL SWITCH LOCATIONS 757-200F

APU CONTROL SWITCH - OFF

BATTERY SWITCH - PUSH NOTE: ON SYMBOL IS REMOVED

THRUST LEVERS - RETARD

APU FIRE SWITCHES - PULL (IF NOT ILLUMINATED, PUSH AND HOLD THE BUTTON UNDER THE SWITCH TO RELEASE)

ENGINE FIRE SWITCHES - PULL (IF NOT ILLUMINATED, PUSH AND HOLD THE BUTTON UNDER THE SWITCH DEPR TO RELEASE) CARGO

MAIN

FWD AFT

CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES. FUEL CONTROL SWITCHES - CUTOFF For Reference Only, some configurations may vary. 12

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 757.1.5 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING BATTERY LOCATIONS 757-200 PACKAGE FREIGHTER BATTERY757-200F LOCATIONS

AFT CARGO DOOR

Emergency Locator Transmitter (ELT) (as installed)

FWD CARGO DOOR

MAIN BATTERY

NOSE GEAR COMPARTMENT APU BATTERY

ACCESS DOOR For Reference Only, some configurations may vary. 13

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 757.1.4 February 15, 2017 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING FLAMMABLE MATERIAL LOCATIONS 757-200F 757-200 PACKAGE FREIGHTER FLAMMABLE MATERIAL LOCATIONS

CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across sections of aircraft that have been exposed to fatigue or fire as the result of an accident. Crews need to verify the integrity of the surface area before moving their weight and equipment across it. Signs could include but are not limited to deformity of structure, visual signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike pole, axe or any instrument used to sound surfaces for integrity. APU

HYDRAULIC RESERVOIR AND SURGE TANK ACCUMULATOR IN RIGHT WHEEL WELL

CENTER FUEL TANK

RIGHT MAIN APU FUEL LINE FUEL TANK 2170 GAL - 8214 L

DRY BAY HYDRAULIC RESERVOIR IN LEFT WING FILLET

6900 GAL - LEFT MAIN FUEL TANKS 26119 L HYDRAULIC RESERVOIR IN APU EMERGENCY LEFT WHEEL WELLS CONTROL PANEL SURGE TANK LOCATED ON THE NOSE GEAR 2170 GAL - 8214 L

HOT BRAKES Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own. Water mist: Can be deployed from turret or handline. CREW OXYGEN BOTTLE IN Fans: Placing fans may place firefighters very close to the hazard zone. RIGHT SIDE, FORWARD WHEEL FIRE CARGO COMPARTMENT AFT Apply large amounts of water initially with turrets. Transition to handline application to continue and OF DOOR maintain a cooling effect. Wheels are equipped with fusible plugs designed to melt and deflate the tire when the ENGINE OIL TANK - temperature is excessive. FLIGHT DECK PORTABLE LEFT OR RIGHT SIDE OXYGEN BOTTLE ON PORTABLE OXYGEN BOTTLES IN OF EACH ENGINE BULKHEAD BEHIND LAVATORY WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when CAPTAIN For Referenceapproaching Only, hot brakessome or configurations fighting a wheel fire,may as vary. rims and tires14 may pose a fragmentation hazard.

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 757.1.1 BOEING AIRCRAFT DIMENSIONS 757-200F

44 ft 6 in (13.6 m) 44 ft 6 in (13.6 m)

13 ft (3.9 m) 13 ft (3.9 m)

155 ft 3 in (47.0 m) 155 ft 3 in (47.0 m)

124 ft 10 in (47.3 m) 124 ft 10 in (47.3 m)

35 ft (10.7 m) 35 ft (10.7 m) 15 BOEING CONTAINER LOCATIONS 757-200F

Main Deck - 15 Positions

Main Cargo Door

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

The first location for“ACCESSIBLE, CARGO AIRCRAFT ONLY” shipments (if carried). NOTOC ENVELOPE WARNING: ANY POSITION MAY CONTAIN HAZMAT! Definitions: • “CARGO AIRCRAFT ONLY” (CAO) shipments are hazmat that would not be authorized aboard a passenger-carrying aircraft. CAO shipments requiring in- flight accessibility by the crew (“ACCESSIBLE”) will be loaded in the red hashed position. Additional CAO positions on the main deck may added by creating a walkway between subsequent positions. • “PASSENGER QUANTITY SHIPMENTS” are hazmat shipments that would be authorized aboard a passenger-carrying aircraft. They may be loaded anywhere in UPS aircraft.

For Reference Only, some configurations may vary. 16 CONSIDERATIONS FOR ARFF BOEING WHEN RESPONDING TO UPS AIRCRAFT 757-200F

RESOURCES: • Seek local UPS management personnel as soon as possible for on scene assistance to incident command. Call UPS Flight Control (502-359-5100) if contact info is not available. • Contact UPS Aircraft Maintenance control for technical assistance/gaining access (502-359-0001). A mechanic can also be requested for on scene assistance • Hazmat information is located in the cockpit (NOTOC envelope). See crew, or request a copy from UPS Flight Control (502-359-5100) PIERCING LOCATIONS • These considerations do not preclude the use of best judgment by the incident commander SAFETY: • Landing gear: consider underneath the aircraft as a collapse zone until Ten O’Clock Two O’Clock determined to be safe. Position Position ◦◦ Gear pins are located in the cockpit. Consult mechanic/aircraft maintenance for guidance ◦◦ If unable to install gear pins, landing gear may be unstable • Engines running: use extreme caution around operating engines ◦◦ Inlet and exhaust hazards ◦◦ Foreign object debris ingestion can cause catastrophic engine failure • Hot brakes: do not approach from side, front, or rear ◦◦ Approach wheels at a 45 degree angle ◦◦ Beware of tire bursting and thermal fuse plug discharge due to heat • Prevent rolling: ensure parking brake set, or install chocks on nose gear • Tail tipping: weight of water/foam injected into fuselage can cause tail tipping. ◦◦ Monitor nose strut extension and tire bulge changes for indicator of tipping TACTICAL CONSIDERATIONS (AFTER RESCUE OF CREW): • Use thermal imaging camera to locate fire within fuselage ◦◦ Note: research shows that thermal imaging may not show fire within a unit load device (ULD) container though the fuselage, until the fire breaches the container • Starve fire of oxygen (close doors/windows/hatches) Additional Aircraft Information • Pierce fuselage • AIRBUS: https://www.airbus.com/aircraft/support- ◦◦ Use the longest available piercing device to reach into a ULD container services/airport-operations-and-technical-data/ ◦◦ Piercing depths vary from 12 to 58 inches depending on aircraft, container aircraft-rescue-firefighting-charts.html design, and location on aircraft. Average depth is about 26 inches • Apply appropriate extinguishing agent • BOEING: http://www.boeing.com/commercial/ • When discharging halotron into cargo area, avoid ventilating as much as possible airports/rescue_fire.page

17 BOEING NOTES 757-200F

18

AIRBUS A300-600F UPS Aircraft Rescue Firefighting Guide

Max. Payload: 121,730 LBS

Main Deck: 22 Containers Lower Deck: 7 Containers

Max. Fuel 120,000 LBS Load: 18,000 GAL (68,100 L)

Range: 2,000 NM

Cruising Speed: 453 KTS/521 MPH

Engines: Pratt & Whitney 4158

For Emergency Responders; Direct Contact Numbers to UPS Flight Operations

UPS System Operations: 502.359.5350

UPS Flight Control: 502.359.5100

UPS HAZMAT 502.380.1800 Support Center: 800.554.9964 AIRBUS INTAKES AND EXHAUST A300-600F

9 ft – NO Entry (2.7M) 1650 ft (503M) 50 ft (15M) RADIUS

TAKE OFF 40 DEG ARC THRUST

CAUTION INLET DANGER AREA EXHAUST DANGER AREA Typical Intake & Exhaust Hazards

30 DEG ARC IDLE THRUST

25 ft (8M) 5 ft 180 ft RADIUS (1.5M) (55M)

TAKE OFF THRUST VISUALIZED Ft M 100 30 60 20 10 20 N120UP 0 Feet 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000

Meters 0 25 50 75 100 125 150 175 200 225 250 275 300 325 350 375 400 425 450 475 500 525 550 575 600 62521 650 675 700 725 750 775 800 825 850 875 900 AIRBUS EMERGENCY RESCUE ACCESS A300-600F

EVACUATION

EMERGENCY ESCAPE ROPES THRU OPENING WINDOWS

ESCAPE SLIDE

For Reference Only, some configurations may vary. 22 AIRBUS EMERGENCY RESCUE ACCESS A300-600F

MAXIMUM SEATING CAPACITY FOR FLIGHT: SEVEN (7) PEOPLE

Lavatory

Entry Door Cargo Access Door

For Reference Only, some configurations may vary. 23

A300F4-600 All Models AIRCRAFT RESCUE AND FIRE FIGHTING CHART

AIRBUS EMERGENCY RESCUE ACCESS

A300-600F

A300F4-600 All Models AIRCRAFT RESCUE AND FIRE FIGHTING CHART

Crew Doors and Emergency Exits - Opening

Page 6

Jun 01/07

For Reference Only, some configurations may vary. 24

Sliding Window - Opening

Page 8

Jun 01/07 AIRBUS FLIGHT DECK CONTROL SWITCH LOCATIONS A300-600F

For Reference Only, some configurations may vary. 25

A300F4-600 All Models AIRCRAFT RESCUE AND AIRBUS BATTERY LOCATIONS FIRE FIGHTING CHART A300-600F

For Reference Only, some configurations may vary. 26

C_RF_180000_1_A3F4600_01_00 Batteries and Control Panel - Location

Page 9

Jun 01/07

A300F4-600 All Models AIRCRAFT RESCUE AND FIRE FIGHTING CHART

A300F4-600 All Models AIRCRAFT RESCUE AND AIRBUS FLAMMABLE MATERIAL LOCATIONSFIRE FIGHTING CHART A300-600F

C_RF_020000_1_A3F4600_01_01 For Reference Only, some configurations may vary. 27 Highly Flammable Materials and Hazardous Components - Location

C_RF_020000_1_A3F4600_01_01 Page 1

Highly Flammable Materials and Hazardous Components - Location Jun 01/07

Page 1

Jun 01/07 AIRBUS AIRCRAFT DIMENSIONS A300-600F

54 ft 3 in (16.5 m) N120UP 54 ft 3 in (16.5 m) 24.5 ft N120UP (7.4 m) 15 ft 24.5 ft (4.6 m)* (7.4 m) 15 ft (4.6 m)

177 ft 5 in (54 m) 177 ft 5 in (54 m)

* WHEELS RETRACTED HEIGHT IS 8.5FT (2.6M)

147 ft 1 in (44.8 m) 147 ft 1 in (44.8 m)

31.5 ft (9.6 m) 31.5 ft (9.6 m) 28 AIRBUS CONTAINER LOCATIONS Main Deck - 22 Positions A300-600F Lower Deck - 7 Positions Main Deck - 22 Positions Lower Deck - 7 Positions

N120UP

N120UP 1 2 3 4 5 6 7 8 9 10 11 12 13

P1 P2 P3 P4 P5 P6 P7

2R 3R 4R 5R 6R 7R 8R 9R 10R 1 11 12 13 2L 3L 4L 5L 6L 7L 8L 9L 10L

Main Cargo Door

The first locationMain forCargo“ACCESSIBLE, Door CARGO AIRCRAFT ONLY” shipments (if carried). NOTOC ENVELOPE WARNING: ANY POSITION MAY CONTAIN HAZMAT! Definitions: • “CARGO AIRCRAFT ONLY” (CAO) shipments are hazmat that would not be authorized aboard a passenger-carrying aircraft. CAO shipments requiring in- flight accessibility by the crew (“ACCESSIBLE”) will be loaded in the red hashed position. Additional CAO positions on the main deck may added by creating a walkway between subsequent positions. • “PASSENGER QUANTITY SHIPMENTS” are hazmat shipments that would be authorized aboard a passenger-carrying aircraft. They may be loaded anywhere in UPS aircraft.

For Reference Only, some configurations may vary. 29 CONSIDERATIONS FOR ARFF AIRBUS WHEN RESPONDING TO UPS AIRCRAFT A300-600F

RESOURCES: • Seek local UPS management personnel as soon as possible for on scene assistance to incident command. Call UPS Flight Control (502-359-5100) if contact info is not available. • Contact UPS Aircraft Maintenance control for technical assistance/gaining access (502-359-0001). A mechanic can also be requested for on scene assistance • Hazmat information is located in the cockpit (NOTOC envelope). See crew, or request a copy from UPS Flight Control (502-359-5100) PIERCING LOCATIONS • These considerations do not preclude the use of best judgment by the incident commander SAFETY: • Landing gear: consider underneath the aircraft as a collapse zone until Ten O’Clock Two O’Clock determined to be safe. Position Position ◦◦ Gear pins are located in the cockpit. Consult mechanic/aircraft maintenance for guidance ◦◦ If unable to install gear pins, landing gear may be unstable • Engines running: use extreme caution around operating engines ◦◦ Inlet and exhaust hazards ◦◦ Foreign object debris ingestion can cause catastrophic engine failure • Hot brakes: do not approach from side, front, or rear ◦◦ Approach wheels at a 45 degree angle ◦◦ Beware of tire bursting and thermal fuse plug discharge due to heat • Prevent rolling: ensure parking brake set, or install chocks on nose gear • Tail tipping: weight of water/foam injected into fuselage can cause tail tipping. ◦◦ Monitor nose strut extension and tire bulge changes for indicator of tipping TACTICAL CONSIDERATIONS (AFTER RESCUE OF CREW): • Use thermal imaging camera to locate fire within fuselage ◦◦ Note: research shows that thermal imaging may not show fire within a unit load device (ULD) container though the fuselage, until the fire breaches the container • Starve fire of oxygen (close doors/windows/hatches) Additional Aircraft Information • Pierce fuselage • AIRBUS: https://www.airbus.com/aircraft/support- ◦◦ Use the longest available piercing device to reach into a ULD container services/airport-operations-and-technical-data/ ◦◦ Piercing depths vary from 12 to 58 inches depending on aircraft, container aircraft-rescue-firefighting-charts.html design, and location on aircraft. Average depth is about 26 inches • Apply appropriate extinguishing agent • BOEING: http://www.boeing.com/commercial/ • When discharging halotron into cargo area, avoid ventilating as much as possible airports/rescue_fire.page

30 AIRBUS NOTES A300-600F

31

BOEING 767-300F UPS Aircraft Rescue Firefighting Guide

Max. Payload: 132,200 LBS

Main Deck: 24 Containers Lower Deck: 7 Containers

Max. Fuel 160,200 LBS Load: 23,900 GAL (89,700 L)

Range: 3,000 NM

Cruising Speed: 465 KTS/535 MPH

Engines: General Electric CF6-80C2

For Emergency Responders; Direct Contact Numbers to UPS Flight Operations

UPS System Operations: 502.359.5350

UPS Flight Control: 502.359.5100

UPS HAZMAT 502.380.1800 Support Center: 800.554.9964 BOEING INTAKES AND EXHAUST 767-300F

9 ft – NO Entry (2.7M) 1650 ft 50 ft (15M) (503M) RADIUS

TAKE OFF THRUST

CAUTION INLET DANGER AREA EXHAUST DANGER AREA Typical Intake & Exhaust Hazards

IDLE THRUST

25 ft (8M) 5 ft 180 ft RADIUS (1.5M) (55M) TAKE OFF THRUST VISUALIZED Ft M 100 30 60 20 10 20 0 Feet 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000

Meters 0 25 50 75 100 125 150 175 200 225 250 275 300 325 350 375 400 425 450 475 500 525 550 575 600 34625 650 675 700 725 750 775 800 825 850 875 900 BOEING EMERGENCY RESCUE ACCESS 767-300F

AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION

Freer EERGEN RESE AESS

WIDE AND OF ONTRASTING OLOR INDIATING ALL DOORS, HATHES AND WINDOWS ETERNALL OPERALE

AP AESS TIN AREAS

WINDOW DETAIL

TIN AREAS PILOT’S WINDOW ON RIGHT SIDE ARGO DOOR ON RIGHT AIN ARGO DOOR SIDE OPERATING INSTRTIONS ON DOOR

TIN AREAS

ARGO DOOR ON RIGHT SIDE OPERATING INSTRTIONS ON DOOR

ENTR DOOR LEFT SIDE ONL

AERAGE DISTANE FLOOR LEEL TO GROND EERGEN ESAPE WHEELS RETRA FT IN ROPES THR OPEN EERGEN ESAPE WHEELS ETENDED FT WINDOWS OR DOOR INERTIAL REEL DEIES THR OPEN DOOR

For Reference Only, some configurations may vary. 35

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. Ferry , BOEING EMERGENCY RESCUE ACCESS 767-300F

MAXIMUM SEATING CAPACITY FOR FLIGHT: SIX (6) PEOPLE Cargo Access Door (Access To PRM If Installed)

Galley Entry Door Supernumerary Area

Rigid Cargo Barrier

Smoke Seal Between PRM & Supernumerary Area

Two (2) O Bottles 767 Pilot Rest Module: 2 (Outside Each Bunk) A Pilot Rest Module (PRM) is occasionally installed on UPS 767 aircraft. It provides 2 bunks and 2 additional chairs for relief pilots or Sleeping Bunks jumpseaters in a rest area Two (2) Stacked separated from the flight deck. When used, the PRM will be installed, instead of cargo, in container position 1 on the main cargo deck. Entry is via the main cargo deck access door. The PRM is not authorized for use during takeoff or landing, so ARFF responders should not expect it to be occupied Lavatory during an emergency. However, depending on the Fire Extinguisher nature of the emergency, (Outside Each Bunk) ARFF responders should not overlook this compartment when searching for crewmembers.

For Reference Only, some configurations may vary. 36 AIRPLANE BOEINGRESCUE AND FIRE FIGHTING INFORMATION EMERGENCY RESCUE ACCESS 767-300F SERIES EERGEN RESE AESS

ENTRSERIE DOOR OERWING ESAPE HATHES TPE EERGEN EIT DOOR ETERNAL HANDLE

FWD

TO OPEN DOOR TO OPEN HATH TO OPEN DOOR PSH IN DISAR LEER RED LIFT LOWER PORTION OF HANDLE AWA PSH ON PSH PANEL TO GAIN AESS TO HANDLE SRFAE LALED PSH FRO THE SIDE OF THE AIRPLANE PLL HANDLE FORWARD AND OTWARD PLL AND LIFT OPERATING PSH INWARD AND P ON THE HANDLE DOOR OPENS OTWARD AND DOWN HANDLE TO NLATH DOOR PSH HATH INWARD OE DOOR PWARD WARNING STAND TO THE SIDE OF DOOR WHEN PLLING DOOR OPENS INWARD HANDLE ESAPE SLIDE DOES NOT DISAR AND WILL P INTO OERHEAD DEPLO IEDIATEL WHEN A TPE DOOR IS OPENED FRO THE OTSIDE

For Reference Only, some configurations may vary. 37 TIN AREAS NOTES FOR ENTRSERIE DOORS AND OERWING HATHES, ESAPE SLIDE DISARS NOTE TIN AREAS REIRE ETAL TTING PORTALE POWER EIPENT ATOATIALL WHEN DOOR OR HATH IS OPENED FRO THE OTSIDE EASE OF TPE OF STRTRE AND POSSILE INR TO PERSONNEL WITHIN, IT IS ON PASSENGER AIRPLANES, OPIT WINDOWS ANNOT E OPENED FRO REOENDED THAT AOR EFFORT TO GAIN AESS E DIRETED TO HATHES AND THE OTSIDE DOORS RGEN OF SITATION WILL DITATE THE NEESSIT FOR A TIN ON FREIGHTERS, THE RIGHT SIDE OPIT WINDOW AN E OPENED FRO THE OTSIDE

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. Ferry , AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION

BOEING 767 -2CFLIGHT Freighter DECK CONTROL SWITCHFLIGHT LOCATIONS DECK CONTROL SWITCH767-300F LOCATIONS

BAT STBY POWER APU AUTO ON START ON OFF BAT APU CONTROL OFF SWITCH - OFF OFF O F F

BATTERY SWITCH - PUSH NOTE: ON SYMBOL IS REMOVED

THRUST LEVERS - RETARD

APU FIRE SWITCHES - PULL (IF NOT ILLUMINATED, PUSH AND HOLD THE BUTTON UNDER THE SWITCH TO RELEASE)

ENGINE FIRE SWITCHES - PULL (IF L ENG ENG BTL ENG BTL R ENG CARGO FIRE NOT ILLUMINATED, PUSH AND HOLD OVHT 1 DISCH 2 DISCH OVHT APU BTL DISCH THE BUTTON UNDER THE SWITCH DEPR TO RELEASE) CARGO L FUEL CONTROL R R RUN L I E G ARMED F H T MAIN CUT OFF T

CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES. FUEL CONTROL SWITCHES - CUTOFF

For Reference Only, some configurations may vary. 38

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 767.1.5 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING BATTERY LOCATIONS 767 SERIES BATTERY767-300F LOCATIONS

AFT CARGO DOOR

Emergency Locator Transmitter (ELT) (as installed)

FWD CARGO DOOR

MAIN BATTERY

AFT CARGO DOOR

APU BATTERY EQUIPMENT ACCESS DOOR

NOSE GEAR DOOR

For Reference Only, some configurations may vary. 39

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 767.0.4 February 15, 2017 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING FLAMMABLE MATERIAL LOCATIONS

767 (tab)767 767-300F SEIRES SEIRES ELAALF LAIRETA SNOITAOL

ATION Rece cre ern fll PPE o ncle SA’ e con en on cro econ of rcrf e een eoe o fe or fre e rel of n ccen re nee o erfy e nery of e rfce re efore on er e n een cro Sn col ncle re no le o efory of rcre, l n of fle neen or neen rfce Srfce nery cn e cece e ole, e or ny nren e o on rfce for nery

SRGE TAN HDRALI ALATOR IN AP RIGHT WHEEL WELL

HDRALI RESEROIR IN RIGHT WHEEL WELL

FEL TAN AP FEL LINE GAL DR A L

OPTIONAL PORTALE OGEN OTTLES THROGHOT AIN

FEL TAN , LS OPTIONAL PORTALE OGEN OTTLES ON , L SRGE TAN FORWARD SIDE OF LHEAD

GAL L

AP EERGEN ONTROL PANEL FEL TAN LOATED ON THE NOSE GEAR REW OGEN OTTLE IN RIGHT SIDE, E E OPARTENT

ENGINE OIL TAN FORWARD RIGHT OR REAR LEFT SIDE OF EAH ENGINE Weel re ee fle l ene o el n efle e re en e eerForre Referenceecee Only, some configurations may vary. 40 WARNING Aroc lnn er rc fro forr or f eree nle en rocn o re or fn eel fre, r n re y oe frenon r

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. Ferry , BOEING AIRCRAFT DIMENSIONS 767-300F

52 ft (15.852 ft m) (15.8 m)

14 ft (4.314 ftm) (4.3 m)

180 ft 3 in (54.9 m) 180 ft 3 in (54.9 m)

167 ft 2 in 167(50.9 ft 2m) in (50.9 m)

Note: Some Aircraft DoNote: Not Have WingletsSome Aircraft Do Not Have Winglets

30 ft 6 in 30(9.3 ft m)6 in (9.3 m) 41 BOEING CONTAINER LOCATIONS Main Deck - 24 Positions 767-300F Lower Deck - 7 Positions Main Deck - 24 Positions Lower Deck - 7 Positions

1 2 3 4 5 6 7 8 9 10 11 12 13

P1 P2 P3 P4 P5 P6 P7

2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 1 13 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L

Main Cargo Door

The first location for“ACCESSIBLE, CARGO AIRCRAFT ONLY” shipments (if carried). NOTOC ENVELOPE Main Cargo Door WARNING: ANY POSITION MAY CONTAIN HAZMAT! Definitions: • “CARGO AIRCRAFT ONLY” (CAO) shipments are hazmat that would not be authorized aboard a passenger-carrying aircraft. CAO shipments requiring in- flight accessibility by the crew (“ACCESSIBLE”) will be loaded in the red hashed position. Additional CAO positions on the main deck may added by creating a walkway between subsequent positions. • “PASSENGER QUANTITY SHIPMENTS” are hazmat shipments that would be authorized aboard a passenger-carrying aircraft. They may be loaded anywhere in UPS aircraft.

For Reference Only, some configurations may vary. 42 CONSIDERATIONS FOR ARFF BOEING WHEN RESPONDING TO UPS AIRCRAFT 767-300F

RESOURCES: • Seek local UPS management personnel as soon as possible for on scene assistance to incident command. Call UPS Flight Control (502-359-5100) if contact info is not available. • Contact UPS Aircraft Maintenance control for technical assistance/gaining access (502-359-0001). A mechanic can also be requested for on scene assistance • Hazmat information is located in the cockpit (NOTOC envelope). See crew, or request a copy from UPS Flight Control (502-359-5100) PIERCING LOCATIONS • These considerations do not preclude the use of best judgment by the incident commander SAFETY: • Landing gear: consider underneath the aircraft as a collapse zone until Ten O’Clock Two O’Clock determined to be safe. Position Position ◦◦ Gear pins are located in the cockpit. Consult mechanic/aircraft maintenance for guidance ◦◦ If unable to install gear pins, landing gear may be unstable • Engines running: use extreme caution around operating engines ◦◦ Inlet and exhaust hazards ◦◦ Foreign object debris ingestion can cause catastrophic engine failure • Hot brakes: do not approach from side, front, or rear ◦◦ Approach wheels at a 45 degree angle ◦◦ Beware of tire bursting and thermal fuse plug discharge due to heat • Prevent rolling: ensure parking brake set, or install chocks on nose gear • Tail tipping: weight of water/foam injected into fuselage can cause tail tipping. ◦◦ Monitor nose strut extension and tire bulge changes for indicator of tipping TACTICAL CONSIDERATIONS (AFTER RESCUE OF CREW): • Use thermal imaging camera to locate fire within fuselage ◦◦ Note: research shows that thermal imaging may not show fire within a unit load device (ULD) container though the fuselage, until the fire breaches the container • Starve fire of oxygen (close doors/windows/hatches) Additional Aircraft Information • Pierce fuselage • AIRBUS: https://www.airbus.com/aircraft/support- ◦◦ Use the longest available piercing device to reach into a ULD container services/airport-operations-and-technical-data/ ◦◦ Piercing depths vary from 12 to 58 inches depending on aircraft, container aircraft-rescue-firefighting-charts.html design, and location on aircraft. Average depth is about 26 inches • Apply appropriate extinguishing agent • BOEING: http://www.boeing.com/commercial/ • When discharging halotron into cargo area, avoid ventilating as much as possible airports/rescue_fire.page

43 BOEING NOTES 767-300F

44

BOEING MD-11F UPS Aircraft Rescue Firefighting Guide

Max. Payload: 207,895 LBS

Main Deck: 26 Containers Lower Deck: 13 Containers

Max. Fuel 257,200 LBS Load: 38,400 GAL (144,200 L)

Range: 3,950 NM

Cruising Speed: 487 KTS/560 MPH

Engines: Pratt & Whitney 4460/4462 or General Electric CF6-80C2

For Emergency Responders; Direct Contact Numbers to UPS Flight Operations

UPS System Operations: 502.359.5350

UPS Flight Control: 502.359.5100

UPS HAZMAT 502.380.1800 Support Center: 800.554.9964 BOEING INTAKES AND EXHAUST MD-11F

9 ft – NO Entry (2.7M) 1650 ft (503M) 50 ft (15M) RADIUS

TAKE OFF 40 DEG ARC THRUST

CAUTION INLET DANGER AREA EXHAUST DANGER AREA Typical Intake & Exhaust Hazards

30 DEG ARC IDLE THRUST

25 ft (8M) 5 ft RADIUS 180 ft (1.5M) (55M) TAKE OFF THRUST VISUALIZED Ft M 100 30 60 20 10 20 0 Feet 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000

Meters 0 25 50 75 100 125 150 175 200 225 250 275 300 325 350 375 400 425 450 475 500 525 550 575 600 47625 650 675 700 725 750 775 800 825 850 875 900 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING EMERGENCY RESCUE ACCESS MD-11F D SERIES EERGEN RESE AESS

AFT AESSOR OPARTENT DOOR OPERALE SERIE DOOR LEFT SIDE ONL

AP OPARTENT DOOR INOPERATIE PASSENGER AND FORWARD ARGO SERIE DOORS DOOR PRESSRE LHEAD

HORIONTAL STAILIER A SREWS AND OTORS AESS DOOR TIN AREAS

AFT ARGO DOOR

FORWARD SERIE PPER ARGO DOOR ON OI ONL ENTRANE DOOR ENTER ARGO DOOR

AIONIS OPARTENT DOORS

TIN AREAS

PPER ARGO DOOR ON PASSENGER ONERTILE FREIGHTER ENTRANE DOOR AIRPLANES ONL

AERAGE DISTANE WIDE AND OF ONTRASTING FLOOR LEEL TO GROND OLOR INDIATING ALL DOORS, HATHES AND WINDOWS LEARIEW WINDOW WHEELS RETRATED FT ETERNALL OPERALE TIN AREA WHEELS ETENDED FT

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.For Reference Only, some configurations may vary. 48 Ferry , D BOEING EMERGENCY RESCUE ACCESS MD-11F

MAXIMUM SEATING CAPACITY FOR FLIGHT: SEVEN (7) PEOPLE

MD-11 Bunks: Flight Deck Door UPS MD-11 aircraft have 2 bunks in a compartment that extends across the L1 entry door Lavatory when used. The bunks are not authorized for use during takeoff Curtain or landing, so ARFF responders should not expect them to be Entry Service extended or occupied during an Door Entrance Door emergency. However, depending on the nature of the emergency, ARFF responders should not overlook this compartment when searching for crewmembers. If the bunks are extended, entry should be made via the R1 entry door.

Small Cargo Access Door

For Reference Only, some configurations may vary. 49 BOEING EMERGENCY RESCUE ACCESS MD-11F

AIRPLANE RESCUE AND FIRE FIGHTING INFORMATAIRPLANEION RESCUE AND FIRE FIGHTING INFORMATION

D SERIES MD-11 SERIESEERGEN RESE AESSEMERGENCY RESCUE ACCESS-2 PASSENGER AND SERIE DOORS 2 CARGO ACCESS DOORS

PSH TTON TPE NON PSH TTON TPE

NOTE WHEN OED TO EERGEN POSITION AND HELD, ALLOWS DOOR NOTE WHENPLAED IN EERGEN POSITION, DOOR ONTROL HANDLE WILL ONTROL HANDLE TO E OED TO EERGEN POSITION FOR REAIN IN THAT POSITION EERGEN OPENING OF THE DOOR IF ELETRIAL POWER IS NOT AAILALE

4 CUT-IN AREAS CUT-IN AREAS

NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. D February 15, 2017 Ferry , MD-11.0.3

For Reference Only, some configurations may vary. 50 BOEING FLIGHT DECK AIRPCONTROLLANE RE SCUESWITCH AND FIRLOCATIONSE FIGHTING INFORMATION MD-11F D SERIES FLIGHT DE ONTROL SWITH LOATIONS Critical switch locations and their operation are shown with the expanded views of the control modules.

AP FIRE HANDLE

ENGFIRE HANDLE GARD

AGENT DISH ENGAP ENGFIRE HANDLE FIRE TEST AP FIRE

PLLTRN AP AP STARTSTOP SWITH START AP STOP GEN ON FEL FAIL OFF OFF DOOR ENGFIRE HANDLE

AFT OERHEAD PANEL

AFT OERHEAD PANEL AP SHTDOWN AND FIRE PROEDRE

PSH AP STARTSTOP SWITH TO OFF IF AP FIRE LIGHT IN HANDLE IS ILLINATED PLL AND ROTATE AP FIRE HANDLE IN EITHER ENG START DIRETION AFTER SEONDS , PLL AND ROTATE AP FIRE HANDLE IN THE OPPOSITE DIRETION ENGINE SHTDOWN AND FIRE PROEDRE FEL ON ON ON FEL SWITHES FRO ON TO OFF DOWN IF LIGHTS IN FEL SWITHES OR ENG FIRE HANDLES ARE ILLINATED LIFT ENGFIRE HANDLE GARDS OFF OFF OFF PLL HANDLES DOWN AND FORWARD WHILE HOLDING FORWARD PRESSRE ON HANDLE, TWIST HANDLE LOWISE AND HOLD ENGINE FEL SWITHES AFTER SEONDS, TWIST HANDLE ONTERLOWISE ONTROL STAND For Reference Only, some configurations may vary. 51

RITIAL SWITH LOATIONS AND THEIR OPERATION ARE SHOWN WITH THE EPANDED IEWS OF THE ONTROL ODLES

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. Ferry , D AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING BATTERY LOCATIONS MD-11F MD-11 SERIES BATTERY LOCATIONS

TYPICAL BATTERY SENSOR CENTER ACCESSORY ELECTRICAL CONNECTOR COMPARTMENT LOOKING AFT

MAIN BATTERY

BATTERY CHARGER TYPICAL OVERBOARD VENT IN 2 PLACES

For Reference Only, some configurations may vary. 52

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. MD-11.0.6 February 15, 2017 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION

MD-11 (tab) MD-11 SERIES FLAMMABLE MATERIAL LOCATIONSBOEING HOT BRAKES FLAMMABLE MATERIAL LOCATIONSCAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own. sections of aircraft that have been exposed to fatigue or fire as the result ofMD-11F an accident. Water mist: Can be deployed from turret or handline. Crews need to verify the integrity of the surface area before moving their weight and Fans: Placing fans may place firefighters very close to the hazard zone. equipment across it. Signs could include but are not limited to deformity of structure, visual WHEEL FIRE signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike Apply large amounts of water initially with turrets. Transition to handline application to continue and pole, axe or any instrument used to sound surfaces for integrity. maintain a cooling effect. Wheels are equipped with fusible plugs designed to melt and deflate the tire when the temperature is excessive. ENGINE 2 FUEL FIRE SHUTOFF VALVE WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when approaching hot brakes or fighting a wheel fire, as rims and tires may pose a ENGINE 2 HYDRAULIC FIRE SHUTOFF VALVE fragmentation hazard. ENGINE 2 / APU FIRE EXTINGUISHER AGENT CONTAINERS ENGINE 2 OIL PORTABLE OXYGEN TANK BOTTLES

UPPER CARGO FIRE OVERBOARD VENT EXTINGUISHER ON OUTLET COMBI ONLY FUEL HYDRAULIC FLUID FUEL VENT BOX TANKS HYDRAULIC RESERVOIR ACCUMULATORS TYPICAL PRESSURE REFUELING IN RIGHT WHEEL 1958 GALLONS ADAPTER WELL 7412 LITERS

APU EXHAUST DUCT ON ENGINE 3 FUEL FIRE SHUTOFF VALVE RIGHT SIDE ONLY ENGINE 3 HYDRAULIC FIRE SHUTOFF VALVE

6100 GAL - FIRE EXTINGUISHERS ENGINE 3 FIRE EXTINGUISHER 23091 L AGENT CONTAINERS HYDRAULIC ACCUMULATORS IN LEFT WHEEL WELL

AUXILIARY FUEL TANK HYDRAULIC RESERVOIRS IN WHEEL WELLS 9700 GAL - 36718 L ENGINE 2 FORWARD FUEL FIRE SHUTOFF VALVE

ENGINE 3 OIL TANK FUEL VENT BOX 14600 GAL - FUEL TANK 55267 L OVERBOARD VENT OUTLET

CREW FIXED OXYGEN 6100 GAL - 23091 L SYSTEM BOTTLES

APU FUEL FIRE SHUTOFF VALVE RAIN REPELLENT CONTAINERS ENGINE 1 FUEL FIRE SHUTOFF VALVE

ENGINE 1 HYDRAULIC FIRE SHUTOFF VALVE LOWER CARGO FIRE EXTINGUISHER CONTAINER ENGINE 1 FIRE EXTINGUISHER AGENT CONTAINERS

PORTABLE OXYGEN FIRE EXTINGUISHERS BOTTLES ENGINE 1 OIL TANK

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.For Reference Only, some configurations may vary. 53 February 15, 2017 MD-11.0.1 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION

MD-11 SERIES EXTERNAL APU FIREBOEING CONTROLS EXTERNAL APU FIRE CONTROLS MD-11F

3 FIRE AGENT 1

4 FIRE AGENT 2

APU AGENT AGENT 1 2 APU SHUTDOWN AND FIRE PROCEDURE: 2 APU FIRE LIGHT FIRE LOW LOW

1. TURN APU SWITCH TO “OFF” (UP). FIRE AGENT 1 FIRE AGENT 2 SERVICE 2. IF APU FIRE LIGHT IS ON... DISCHARGE DISCHARGE INTERPHONE APU OFF 3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP). AGENT ARM HORN OFF 4. AFTER 30 SECONDS, FIRE AGENT 2 SWITCH TO 1 APU SWITCH “DISCHARGE” (UP). NORMAL NORMAL NORMAL NORMAL

ON

OFF

SERVICE LIGHT

For Reference Only, some configurations may vary. 54

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. MD-11.0.8 February 15, 2017 BOEING AIRCRAFT DIMENSIONS MD-11F

57 ft 11 in (17.6 m) 57 ft 11 in (17.6 m) 29 ft 2 in (8.9 m) 29 ft 2 in (8.9 m) 17 ft 5 in (5.3 m) 17 ft 5 in (5.3 m) 80 ft 9 in (24.6 m) 80 ft 9 in (24.6 m) 200 ft 11 in (61.2 m) 200 ft 11 in (61.2 m)

169 ft 10 in (51.7 m) 169 ft 10 in (51.7 m)

9 ft 5 in (2.9 m) 9 ft 5 in (2.9 m)

35 ft (10.7 m) 35 ft (10.7 m) 55 BOEING CONTAINER LOCATIONS Main Deck - 26 Positions MD-11F Lower Deck - 13 Positions Main Deck - 26 Positions Lower Deck - 13 Positions

1 2 3 4 5 6 7 8 9 10 11 12 13 14

P1 P2 P3 P4 P5 P6 P7 P8 P9 P10 P11 P12 P13

1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13C 14C 1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L

Main Cargo Door

The first location for“ACCESSIBLE, CARGO AIRCRAFT ONLY” shipments (if carried). NOTOC ENVELOPE Main Cargo Door WARNING: ANY POSITION MAY CONTAIN HAZMAT! Definitions: • “CARGO AIRCRAFT ONLY” (CAO) shipments are hazmat that would not be authorized aboard a passenger-carrying aircraft. CAO shipments requiring in- flight accessibility by the crew (“ACCESSIBLE”) will be loaded in the red hashed position. Additional CAO positions on the main deck may added by creating a walkway between subsequent positions. • “PASSENGER QUANTITY SHIPMENTS” are hazmat shipments that would be authorized aboard a passenger-carrying aircraft. They may be loaded anywhere in UPS aircraft.

For Reference Only, some configurations may vary. 56 CONSIDERATIONS FOR ARFF BOEING WHEN RESPONDING TO UPS AIRCRAFT MD-11F

RESOURCES: • Seek local UPS management personnel as soon as possible for on scene assistance to incident command. Call UPS Flight Control (502-359-5100) if contact info is not available. • Contact UPS Aircraft Maintenance control for technical assistance/gaining access (502-359-0001). A mechanic can also be requested for on scene assistance • Hazmat information is located in the cockpit (NOTOC envelope). See crew, or request a copy from UPS Flight Control (502-359-5100) PIERCING LOCATIONS • These considerations do not preclude the use of best judgment by the incident commander SAFETY: • Landing gear: consider underneath the aircraft as a collapse zone until Ten O’Clock Two O’Clock determined to be safe. Position Position ◦◦ Gear pins are located in the cockpit. Consult mechanic/aircraft maintenance for guidance ◦◦ If unable to install gear pins, landing gear may be unstable • Engines running: use extreme caution around operating engines ◦◦ Inlet and exhaust hazards ◦◦ Foreign object debris ingestion can cause catastrophic engine failure • Hot brakes: do not approach from side, front, or rear ◦◦ Approach wheels at a 45 degree angle ◦◦ Beware of tire bursting and thermal fuse plug discharge due to heat • Prevent rolling: ensure parking brake set, or install chocks on nose gear • Tail tipping: weight of water/foam injected into fuselage can cause tail tipping. ◦◦ Monitor nose strut extension and tire bulge changes for indicator of tipping TACTICAL CONSIDERATIONS (AFTER RESCUE OF CREW): • Use thermal imaging camera to locate fire within fuselage ◦◦ Note: research shows that thermal imaging may not show fire within a unit load device (ULD) container though the fuselage, until the fire breaches the container • Starve fire of oxygen (close doors/windows/hatches) Additional Aircraft Information • Pierce fuselage • AIRBUS: https://www.airbus.com/aircraft/support- ◦◦ Use the longest available piercing device to reach into a ULD container services/airport-operations-and-technical-data/ ◦◦ Piercing depths vary from 12 to 58 inches depending on aircraft, container aircraft-rescue-firefighting-charts.html design, and location on aircraft. Average depth is about 26 inches • Apply appropriate extinguishing agent • BOEING: http://www.boeing.com/commercial/ • When discharging halotron into cargo area, avoid ventilating as much as possible airports/rescue_fire.page

57 BOEING NOTES MD-11F

58

BOEING 747-400F UPS Aircraft Rescue Firefighting Guide

Max. Payload: 273,300 LBS

Main Deck: 33 Containers Lower Deck: 9 Containers

Max. Fuel 406,200 LBS Load: 60,600 GAL (230,000 L)

Range: 4,445 NM

Cruising Speed: 487 KTS/560 MPH

Engines: General Electric CF6-80C2

For Emergency Responders; Direct Contact Numbers to UPS Flight Operations

UPS System Operations: 502.359.5350

UPS Flight Control: 502.359.5100

UPS HAZMAT 502.380.1800 Support Center: 800.554.9964 BOEING INTAKES AND EXHAUST 747-400F

1650 ft (503M) 50 ft (15M) RADIUS

TAKE OFF THRUST

CAUTION INLET DANGER AREA EXHAUST DANGER AREA Typical Intake & Exhaust Hazards

IDLE THRUST

25 ft (8M) RADIUS 150 ft (45.7M) TAKE OFF THRUST VISUALIZED Ft M 100 30 60 20

10 N570UP 20 0 Feet 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000

Meters 0 25 50 75 100 125 150 175 200 225 250 275 300 325 350 375 400 425 450 475 500 525 550 575 600 61625 650 675 700 725 750 775 800 825 850 875 900 BOEING EMERGENCY RESCUE ACCESS AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION 747-400F FREIGHTER SERIES EERGEN RESE AESS

WIDE AND OF ONTRASTING OLOR INDIATING ALL DOORS, HATHES AND WINDOWS ETERNALL OPERALE

TIN AREAS OPEN NOT ARED ON ALL AIRPLANES

PUSH RED BUTTON ON HANDLE HANDLE WILL RELEASE ROTATE AS SHOWN PUSH TOP OF DOOR INWARD

EXIT AP AESS HATH

AIN DE TO PPER HATCH DETAIL DE LADDER SIDE ARGO DOOR ON OI

PPER DE REW DOOR RH SIDE ONL AP EERGEN ONTROL PANEL ∙ ESCAPE SLIDE LOATED ON RIGHT INOARD AIN ∙ DOOR OPENS INWARD; LANDING GEAR LHEAD AND AFT

REW OERHEAD ESAPE HATH ∙ OPENS INWARD EERGEN ESAPE INERTIAL REEL DEIES THR HATH A ONTROL AINLONGE FLOOR LEEL TO GROND WHEELS RETRATED FT IN WHEELS ETENDED FT IN PPER DE REW DOOR HANDLE WHEELS RETRATED FT IN WHEELS ETENDED FT ENTR DOOR L PASSENGER AIN FLOOR LEEL TO GROND ∙ OPENS OUTWARD WHEELS RETRATED FT IN WHEELS ETENDED FT AND FOWARD D D ENTR DOOR HANDLE E WHEELS RETRATED FT WHEELS ETENDED FT IN A E REW OERHEAD ESAPE HATH WHEELS RETRATED FT IN WHEELS ETENDED FT

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. For Reference Only, some configurations may vary. 62 Ferry , BOEING EMERGENCY RESCUE ACCESS 747-400F

747-400BCF (PAX Conversion) 747-400F Maximum seating capacity for flight: Maximum seating capacity for flight: Twelve (12) people Eight (8) people

Curtain Lavatory Service Entrance Door Crew Rest Lavatory

Ladder Ladder

Crew Rest Crew Rest

Emergency Emergency Exit Exit

For Reference Only, some configurations may vary. 63 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING EMERGENCY RESCUE ACCESS 747-400F 747-400 FREIGHTER SERIES EMERGENCY RESCUE ACCESS-1

1 ENTRY DOORS EXTERNAL HANDLE (2) 2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE HANDLE RELEASE TO OPEN DOOR: BUTTON 1. PUSH HANDLE RELEASE BUTTON AND PULL HANDLE FROM RECESS. 2. ROTATE 180° IN DIRECTION OF “OPEN” ARROW. 3. PULL DOOR OUTWARD

NOTE: OPENING A DOOR FROM THE OUTSIDE DISENGAGES THE EMERGENCY EVACUATION SYSTEM AND THE ESCAPE SLIDE WILL NOT DEPLOY. TO OPEN HATCH: 1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM RECESS APPROXIMATELY 3 INCHES). 2. ROTATE HANDLE 180° CLOCKWISE. 3. PUSH HATCH INWARD.

3 UPPER DECK EMERGENCY DOOR 4 CUT-IN AREAS

TO OPEN DOOR: NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER 1. PUSH OUTSIDE DISARM LEVER. EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO 2. LIFT DOOR HANDLE. GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN. NOTE: PUSHING IN THE DISARM LEVER DISARMS THE SLIDE AND DISENGAGES THE EMERGENCY POWER SYSTEM. NOTE: CONTROL ACCESS COVER FORWARD OF THE LH DOOR AND AFT OF THE RH DOOR.

3. OPEN CONTROL ACCESS COVER 4. MOVE GUARDED EMERGENCY DOOR SWITCH TO OPEN. EMER DOOR DOOR OPEN OPEN CAUTION: STAND TO THE SIDE OF THE DOOR AS THE DOOR WILL OPEN RAPIDLY AND CANNOT BE STOPPED. DOOR OFF CLOSE PULL PUSH

For Reference Only, some configurations may vary. 64

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 747.7.2 February 15, 2017 BOEING FLIGHT DECK CONTROLAIRPLANE RESCUE SWITCH AND FIRE LOCATIONS FIGHTING INFORMATION 747-400F 747-400 FREIGHTER SERIES FLIGHT DECK CONTROL SWITCH LOCATIONS

ENGINE FIRE T-HANDLES - PULL APU SELECTOR - (IF NOT ILLUMINATED, MAY REQUIRE ROTATE OFF PUSHING AND HOLDING THE BUTTON UNDER THE SWITCH TO RELEASE)

BATTERY SWITCH - PRESS DISCH DISCH DISCH DISCH AAB B AB BA NOTE: ON SYMBOL IS MAIN DECK EXTINGUISHERS AVAILABLE ON FREIGHTER VERSION REMOVED 1 234

L UTILITY R STANDBY POWER APU BTL A BTL B BTL A BTL B AUTO ON DISCH DISCH DISCH DISCH OFF BAT ON ON OFF START APU BTL CARGO FIRE OFF OFF DISCH MAIN DISCH ARMED BATTERY AFT DEPRESS EXT PWR 1 APU GEN 1 APU GEN 2 EXT PWR 2 DISCH ON APU FWD AFT DISCH A A A A ARMED ARMED V V OFF V V A ON A ON A ON A ON I I I I FWD AFT L L L L

AUTO AUTO AUTO AUTO BUS ISLN ISLN TIE ISLN ISLN APU SWITCH - PULL BUS BUS BUS BUS (IF NOT ILLUMINATED, MAY REQUIRE

ON ON ON ON GEN PUSHING AND HOLDING THE BUTTON OFF OFF CONT OFF OFF UNDER THE SWITCH TO RELEASE) 1 2 3 4

DRIVE DISC DRIVE DRIVE DRIVE DRIVE THRUST LEVERS - RETARD

FUEL CONTROL 1234 RUN RUN

CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES. CUTOFF CUTOFF

FUEL CONTROL SWITCHES - CUTOFF

For Reference Only, some configurations may vary. 65

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 747.7.5 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING BATTERY LOCATIONS 747-400 FREIGHTER SERIES BATTERY747-400F LOCATIONS

Emergency Locator Transmitter (ELT) (as installed)

APU BATTERY

MAIN BATTERY

ACCESS DOOR

INBD FWD NOSE GEAR COMPARTMENT

For Reference Only, some configurations may vary. 66

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 747.7.4 February 15, 2017 BOEING AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION FLAMMABLE MATERIAL LOCATIONS 747-400F 747-400 FREIGHTER SERIES FLAMMABLE MATERIAL LOCATIONS

SURGE TANKS

APU FUEL VENT AND OVERFLOW (BENEATH WING)

1635 GAL - HYDRAULIC 6189 L ACCUMULATORS FUEL TANK IN RIGHT BODY WHEEL WELL

5550 GAL - 21009 L FUEL TANK APU FUEL LINE

FUEL TANKS 14550 GAL - 55078 L SIDE CARGO DOOR

HYDRAULIC RESERVOIR 4 FUEL TANKS PLACES ON ENGINE SURGE TANK CREW OXYGEN STRUTS SYSTEM BOTTLE IN 17164 GAL - 64973 L FWD CARGO COMPARTMENT 14550 GAL - 55078 L 5550 GAL - 21009 L 1635 GAL - 6189 L

FUEL VENT AND OVERFLOW (BENEATH WING)

FLIGHT DECK PORTABLE ENGINE OIL TANK - HOT BRAKES OXYGEN BOTTLE FORWARD RIGHT SIDE OR Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own. REAR LEFT SIDE Water mist: Can be deployed from turret or handline. OF EACH ENGINE Fans: Placing fans may place firefighters very close to the hazard zone. WHEEL FIRE Apply large amounts of water initially with turrets. Transition to handline application to continue and CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across For Reference Only, some configurations may vary. 67 maintain a cooling effect. sections of aircraft that have been exposed to fatigue or fire as the result of an accident. Wheels are equipped with fusible plugs designed to melt and deflate the tire when the Crews need to verify the integrity of the surface area before moving their weight and temperature is excessive. equipment across it. Signs could include but are not limited to deformity of structure, visual signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when pole, axe or any instrument used to sound surfaces for integrity. approaching hot brakes or fighting a wheel fire, as rims and tires may pose a fragmentation hazard.

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 747.7.1 BOEING AIRCRAFT DIMENSIONS 747-400F

63 ft 8 in 63(19.4 ft 8m) in (19.4 m)

N570UP

N570UP

84 ft 0 in 84(25.6 ft 0m) in (25.6 m) 231 ft 10 in (70.6 m) 231 ft 10 in (70.6 m)

211 ft 5 in 211(64.4 ft m)5 in (64.4 m)

36 ft 1 in 36(11.0 ft 1m) in (11.0 m) 68 BOEING CONTAINER LOCATIONS 747-400F Main Deck - 30 Positions Lower Deck - 9 Positions Main Deck - 30 Positions Lower Deck - 9 Positions

N570UP

N570UP 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17

P1 P2 P3 P4 P5 P6 P7 P8 P9

3 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R 15R 16R 1 2 17 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L 15L 16L

Main Cargo Door

Main Cargo Door The first location for“ACCESSIBLE, CARGO AIRCRAFT ONLY” shipments (if carried). NOTOC ENVELOPE WARNING: ANY POSITION MAY CONTAIN HAZMAT! Definitions: • “CARGO AIRCRAFT ONLY” (CAO) shipments are hazmat that would not be authorized aboard a passenger-carrying aircraft. CAO shipments requiring in- flight accessibility by the crew (“ACCESSIBLE”) will be loaded in the red hashed position. Additional CAO positions on the main deck may added by creating a walkway between subsequent positions. • “PASSENGER QUANTITY SHIPMENTS” are hazmat shipments that would be authorized aboard a passenger-carrying aircraft. They may be loaded anywhere in UPS aircraft.

For Reference Only, some configurations may vary. 69 CONSIDERATIONS FOR ARFF BOEING WHEN RESPONDING TO UPS AIRCRAFT 747-400F

RESOURCES: • Seek local UPS management personnel as soon as possible for on scene PIERCING LOCATIONS assistance to incident command. Call UPS Flight Control (502-359-5100) if contact info is not available. • Contact UPS Aircraft Maintenance control for technical assistance/gaining access Ten O’Clock Two O’Clock (502-359-0001). A mechanic can also be requested for on scene assistance • Hazmat information is located in the cockpit (NOTOC envelope). See crew, or Position Position request a copy from UPS Flight Control (502-359-5100) • These considerations do not preclude the use of best judgment by the incident commander SAFETY: • Landing gear: consider underneath the aircraft as a collapse zone until determined to be safe. ◦◦ Gear pins are located in the cockpit. Consult mechanic/aircraft maintenance for guidance ◦◦ If unable to install gear pins, landing gear may be unstable • Engines running: use extreme caution around operating engines ◦◦ Inlet and exhaust hazards NOSE CHOP ◦◦ Foreign object debris ingestion can cause catastrophic engine failure (IF NO POWER) • Hot brakes: do not approach from side, front, or rear ◦◦ Approach wheels at a 45 degree angle ◦◦ Beware of tire bursting and thermal fuse plug discharge due to heat

• Prevent rolling: ensure parking brake set, or install chocks on nose gear N570UP • Tail tipping: weight of water/foam injected into fuselage can cause tail tipping. ◦◦ Monitor nose strut extension and tire bulge changes for indicator of tipping TACTICAL CONSIDERATIONS (AFTER RESCUE OF CREW): • Use thermal imaging camera to locate fire within fuselage ◦◦ Note: research shows that thermal imaging may not show fire within a unit load device (ULD) container though the fuselage, until the fire breaches the container • Starve fire of oxygen (close doors/windows/hatches) Additional Aircraft Information • Pierce fuselage • AIRBUS: https://www.airbus.com/aircraft/support- ◦◦ Use the longest available piercing device to reach into a ULD container services/airport-operations-and-technical-data/ ◦◦ Piercing depths vary from 12 to 58 inches depending on aircraft, container aircraft-rescue-firefighting-charts.html design, and location on aircraft. Average depth is about 26 inches • Apply appropriate extinguishing agent • BOEING: http://www.boeing.com/commercial/ • When discharging halotron into cargo area, avoid ventilating as much as possible airports/rescue_fire.page

70 BOEING NOTES 747-400F

71

BOEING 747-8F UPS Aircraft Rescue Firefighting Guide

Max. Payload: 307,600 LBS

Main Deck: 34 Containers Lower Deck: 12 Containers

Max. Fuel 379,400 LBS Load: 56,600 GAL (214,300 L)

Range: 4,200 NM

Cruising Speed: 487 KTS/560 MPH

Engines: GEnx-2B

For Emergency Responders; Direct Contact Numbers to UPS Flight Operations

UPS System Operations: 502.359.5350

UPS Flight Control: 502.359.5100

UPS HAZMAT 502.380.1800 Support Center: 800.554.9964 BOEING INTAKES AND EXHAUST 747-8F

2,588 ft (789M) 50 ft (15M) RADIUS

TAKE OFF THRUST

CAUTION INLET DANGER AREA EXHAUST DANGER AREA Typical Intake & Exhaust Hazards

IDLE THRUST 25 ft (8M) RADIUS 150 ft (45.7M) TAKE OFF THRUST VISUALIZED 200mph 150mph Ft M (322km/hr) (241km/hr) 100mph (161km/hr) 50mph (80km/hr) 35mph (56km/hr) 100 30 60 20 10 20 0 Feet 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 2900 3000

Meters 0 25 50 75 100 125 150 175 200 225 250 275 300 325 350 375 400 425 450 475 500 525 550 575 600 625 650 675 700 725 750 775 800 825 850 875 900 74 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING EMERGENCY RESCUE ACCESS 747-8F FREIGHTER SERIES EERGEN RESE AESS

WIDE AND OF ONTRASTING OLOR INDIATING ALL DOORS, HATHES AND WINDOWS ETERNALL OPERALE

AESS DOOR R Se

OPEN TIN AREAS PUSH RED BUTTON ON HANDLE NOT ARED ON ALL AIRPLANES HANDLE WILL RELEASE ROTATE AS SHOWN PUSH TOP OF DOOR INWARD

EXIT AP AESS HATH

HATCH DETAIL AIN DE TO PPER DE LADDER SIDE ARGO DOOR

PPER DE REW DOOR AP EERGEN ONTROL PANEL RH SIDE ONL LOATED ON RIGHT INOARD AIN LANDING GEAR LHEAD ∙ ESAPE SLIDE ∙ DOOR OPENS INWARD AND AFT

REW OERHEAD ESAPE HATH ∙ OPENS INWARD EERGEN ESAPE INERTIAL REEL A ONTROL AINLONGE FLOOR LEEL TO GROND DEIES THR WHEELS RETRATED FT IN WHEELS ETENDED FT IN HATH PPER DE REW DOOR HANDLE WHEELS RETRATED FT IN WHEELS ETENDED FT PASSENGER AIN FLOOR LEEL TO GROND ENTR DOOR L ∙ OPENS OTWARD WHEELS RETRATED FT IN WHEELS ETENDED FT AND FOWARD D D ENTR DOOR HANDLE WHEELS RETRATED FT WHEELS ETENDED FT IN E A E REW OERHEAD ESAPE HATH WHEELS RETRATED FT IN WHEELS ETENDED FT

some configurations may vary. 75 Copyright © Boeing. May be subject to export restrictions under EAR.For See Referencetitle page for details. Only, Ferry , BOEING EMERGENCY RESCUE ACCESS 747-8F

MAXIMUM SEATING CAPACITY FOR FLIGHT: TEN (10) PEOPLE

Emergency Escape Hatch

Lavatory Service Entrance Door

Galley Curtain

Ladder

Crew Rest Crew Rest

For Reference Only, some configurations may vary. 76 BOEING EMERGENCY RESCUE ACCESS 747-8F AIRPLANEAIRPLANE RESCUE RESCUE AND ANDFIRE FIREFIGHTING FIGHTING INFORMATION INFORMATION

747-8747-8 FREIGHTER FREIGHTER SERIES SERIES EMERGENCYEMERGENCY RESCUE RESCUE ACCESS-1 ACCESS-1

1 ENTRY1 ENTRY DOORS DOORS EXTERNAL EXTERNAL HANDLE HANDLE (2) (2) 2 CREW2 CREW OVERHEAD OVERHEAD ESCAPE ESCAPE HATCH HATCH EXTERNAL EXTERNAL HANDLE HANDLE HANDLEHANDLE RELEASE RELEASE TO OPENTO DOOR: OPEN DOOR: BUTTONBUTTON 1. PUSH1. HANDLE PUSH HANDLE RELEASE RELEASE BUTTON BUTTON AND AND PULL HANDLEPULL HANDLE FROM RECESS. FROM RECESS. 2. ROTATE2. ROTATE 180° IN 180°DIRECTION IN DIRECTION OF “OPEN” OF “OPEN” ARROW.ARROW. 3. PULL3. DOOR PULL OUTWARD DOOR OUTWARD

NOTE: OPENINGNOTE: OPENING A DOOR AFROM DOOR THE FROM OUTSIDE THE OUTSIDE DISENGAGESDISENGAGES THE EMERGENCY THE EMERGENCY EVACUATION EVACUATION SYSTEM SYSTEMAND THE AND ESCAPE THE ESCAPESLIDE WILL SLIDE NOT WILL NOT DEPLOY.DEPLOY. TO OPENTO HATCH: OPEN HATCH: 1. PUSH1. RELEASE PUSH RELEASE TRIGGER TRIGGER ON HANDLE ON HANDLE (HANDLE (HANDLE WILL SPRING WILL SPRING OUT FROM OUT FROM RECESSRECESS APPROXIMATELY APPROXIMATELY 3 INCHES). 3 INCHES). 2. ROTATE2. ROTATE HANDLE HANDLE 180° CLOCKWISE. 180° CLOCKWISE. 3. PUSH3. HATCH PUSH HATCHINWARD. INWARD.

3 CUT-IN3 CUT-IN AREAS AREAS

NOTE: CUT-INNOTE: AREAS CUT-IN REQUIRE AREAS REQUIRE METAL CUTTING METAL CUTTING PORTABLE PORTABLE POWER POWER EQUIPMENT.EQUIPMENT. BECAUSE BECAUSE OF TYPE OF OF TYPE STRUCTURE OF STRUCTURE AND POSSIBLE AND POSSIBLE INJURY INJURY TO PERSONNELTO PERSONNEL WITHIN, ITWITHIN, IS RECOMMENDED IT IS RECOMMENDED THAT MAJOR THAT EFFORTMAJOR EFFORTTO TO GAIN ACCESSGAIN ACCESS BE DIRECTED BE DIRECTED TO HATCHES TO HATCHES AND DOORS. AND DOORS. URGENCY URGENCY OF OF SITUATIONSITUATION WILL DICTATE WILL DICTATE THE NECESSITY THE NECESSITY FOR A CUT-IN. FOR A CUT-IN.

For Reference Only, some configurations may vary. 77

Copyright ©Copyright Boeing. ©May Boeing. be subject May tobe export subject restrictions to export restrictions under EAR. under See titleEAR. page See for title details. page for details. 747.9.2747.9.2 FebruaryFebruary 15, 2017 15, 2017 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BOEING FLIGHT DECK CONTROL SWITCH LOCATIONS 747-8F 747-8 FREIGHTER SERIES FLIGHT DECK CONTROL SWITCH LOCATIONS

ENGINE FIRE T-HANDLES - PULL APU SELECTOR - (IF NOT ILLUMINATED, MAY REQUIRE ROTATE OFF PUSHING AND HOLDING THE BUTTON UNDER THE SWITCH TO RELEASE)

BATTERY SWITCH - PRESS DISCH DISCH DISCH DISCH AAB B AB BA NOTE: ON SYMBOL IS MAIN DECK EXTINGUISHERS AVAILABLE ON FREIGHTER VERSION REMOVED 1 234

L UTILITY R STANDBY POWER APU BTL A BTL B BTL A BTL B AUTO ON DISCH DISCH DISCH DISCH OFF BAT ON ON OFF START APU BTL CARGO FIRE OFF OFF DISCH MAIN DISCH ARMED BATTERY AFT EXT PWR 1 APU GEN 1 APU GEN 2 EXT PWR 2 DISCH ON APU FWD AFT DISCH A A A A ARMED ARMED V V OFF V V A ON A ON A ON A ON I I I I FWD AFT L L L L

AUTO AUTO AUTO AUTO BUS ISLN ISLN TIE ISLN ISLN APU SWITCH - PULL BUS BUS BUS BUS (IF NOT ILLUMINATED, MAY REQUIRE

ON ON ON ON GEN PUSHING AND HOLDING THE BUTTON OFF OFF CONT OFF OFF UNDER THE SWITCH TO RELEASE) 1 2 3 4

DRIVE DISC DRIVE DRIVE DRIVE DRIVE

THRUST LEVERS - RETARD

FUEL CONTROL 1234RUN RUN

CUTOFF CUTOFF CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.

FUEL CONTROL SWITCHES - CUTOFF

For Reference Only, some configurations may vary. 78

Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. February 15, 2017 747.9.5 BOEING AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION BATTERY LOCATIONS 747-8F 747-8 FREIGHTER SERIES BATTERY LOCATIONS

Emergency Locator Transmitter (ELT) (as installed)

APU BATTERY

MAIN BATTERY

ACCESS DOOR

INBD FWD NOSE GEAR COMPARTMENT

For Reference Only, some configurations may vary. 79 Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 747.9.4 February 15, 2017 BOEING FLAMMABLE MATERIALAIRPLANE RESCUE LOCATIONS AND FIRE FIGHTING INFORMATION 747-8F 747-8 FREIGHTER SERIES FLAMMABLE MATERIAL LOCATIONS

SURGE TANKS APU FUEL VENT AND OVERFLOW (BENEATH WING)

1635 GAL - HYDRAULIC 6189 L ACCUMULATORS FUEL TANK IN RIGHT BODY WHEEL WELL

FUEL TANK APU FUEL LINE 5550 GAL - 21009 L

FUEL TANKS SIDE CARGO DOOR 12546 GAL - 47492 L HYDRAULIC RESERVOIR 4 PLACES ON ENGINE STRUTS FUEL TANKS CREW OXYGEN SURGE TANK SYSTEM BOTTLE IN 17164 GAL - FWD CARGO 64973 L COMPARTMENT 12546 GAL - 47492 L 4482 GAL - 16966 L 1322 GAL - 5004 L

FUEL VENT AND OVERFLOW (BENEATH WING) HOT BRAKES ENGINE OIL TANK - Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own. FORWARD RIGHT SIDE OR Water mist: Can be deployed from turret or handline. REAR LEFT SIDE Fans: Placing fans may place firefighters very close to the hazard zone. FLIGHT DECK PORTABLE OF EACH ENGINE OXYGEN BOTTLE WHEEL FIRE Apply large amounts of water initially with turrets. Transition to handline application to continue and CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across maintain a cooling effect. sections of aircraft that have been exposed to fatigue or fire as the result of an accident. Wheels are equipped with fusible plugs designed to melt and deflate the tire when the Crews need to verify the integrity of the surface area before moving their weight and temperature is excessive. equipment across it. Signs could include but are not limited to deformity of structure, visual signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when pole, axe or any instrument used to sound surfaces for integrity. approaching hot brakes or fighting a wheel fire, as rims and tires may pose a fragmentation hazard. Copyright © Boeing. May be subject to export restrictions under EAR. See title page forFor details. Reference Only, some configurations may vary. 80 February 15, 2017 747.9.1 BOEING COMPOSITE MATERIALSAIRPLANE RESCUE LOCATIONS AND FIRE FIGHTING INFORMATION 747-8F 747-8 FREIGHTER SERIES COMPOSITE MATERIALS LOCATIONS TIP FAIRING RUDDER

VERTICAL STABILIZER TRAILING EDGE PANELS VERTICAL STABILIZER FORWARD TORQUE BOX UPPER WING LEADING EDGE ELEVATORS AILERONS

ENGINE PYLONS STABILIZER TIP SPOILERS

INLET, FAN, AND REVERSER COWLS UPPER WING TRAILING EDGE

RADOME

WING TO BODY LOWER WING FAIRING TRAILING EDGE

LOWER WING LEADING EDGE

FLAP TRACK FAIRINGS

For Reference Only, some configurations may vary. 81 Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 747.9.6 February 15, 2017 BOEING AIRCRAFT DIMENSIONS 747-8F

64 ft 2 in (19.5 m)

64 ft 2 in (19.5 m)

250 ft 2 in (76.2 m)

250 ft 2 in (76.2 m)

224 ft 5 in (68.4 m)

224 ft 5 in (68.4 m)

82 BOEING CONTAINER LOCATIONS 747-8F Main Deck - 34 Positions Lower Deck - 12 Positions Main Deck - 34 Positions Lower Deck - 12 Positions

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19

P1 P2 P3 P4 P5 P6 P7 P8 P9 P10 P11 P12

3 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R 15R 16R 17R 18R 1 2 19 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L 15L 16L 17L 18L

Main Cargo Door

The first location for“ACCESSIBLE, CARGO AIRCRAFT ONLY” shipments (if carried). NOTOC ENVELOPE WARNING: ANY POSITION MAY CONTAIN HAZMAT! Definitions: • “CARGO AIRCRAFT ONLY” (CAO) shipments are hazmat that would not be authorized aboard a passenger-carrying aircraft. CAO shipments requiring in- flight accessibility by the crew (“ACCESSIBLE”) will be loaded in the red hashed position. Additional CAO positions on the main deck may added by creating a walkway between subsequent positions. • “PASSENGER QUANTITY SHIPMENTS” are hazmat shipments that would be authorized aboard a passenger-carrying aircraft. They may be loaded anywhere in UPS aircraft.

For Reference Only, some configurations may vary. 83 CONSIDERATIONS FOR ARFF BOEING WHEN RESPONDING TO UPS AIRCRAFT 747-8F

RESOURCES: PIERCING LOCATIONS • Seek local UPS management personnel as soon as possible for on scene assistance to incident command. Call UPS Flight Control (502-359-5100) if contact info is not available. • Contact UPS Aircraft Maintenance control for technical assistance/gaining access Ten O’Clock Two O’Clock (502-359-0001). A mechanic can also be requested for on scene assistance Position Position • Hazmat information is located in the cockpit (NOTOC envelope). See crew, or request a copy from UPS Flight Control (502-359-5100) • These considerations do not preclude the use of best judgment by the incident commander SAFETY: • Landing gear: consider underneath the aircraft as a collapse zone until determined to be safe. ◦◦ Gear pins are located in the cockpit. Consult mechanic/aircraft maintenance for guidance ◦◦ If unable to install gear pins, landing gear may be unstable • Engines running: use extreme caution around operating engines ◦◦ Inlet and exhaust hazards NOSE CHOP ◦◦ Foreign object debris ingestion can cause catastrophic engine failure (IF NO POWER) • Hot brakes: do not approach from side, front, or rear ◦◦ Approach wheels at a 45 degree angle ◦◦ Beware of tire bursting and thermal fuse plug discharge due to heat • Prevent rolling: ensure parking brake set, or install chocks on nose gear • Tail tipping: weight of water/foam injected into fuselage can cause tail tipping. ◦◦ Monitor nose strut extension and tire bulge changes for indicator of tipping TACTICAL CONSIDERATIONS (AFTER RESCUE OF CREW): • Use thermal imaging camera to locate fire within fuselage ◦◦ Note: research shows that thermal imaging may not show fire within a unit load device (ULD) container though the fuselage, until the fire breaches the container • Starve fire of oxygen (close doors/windows/hatches) Additional Aircraft Information • Pierce fuselage • AIRBUS: https://www.airbus.com/aircraft/support- ◦◦ Use the longest available piercing device to reach into a ULD container services/airport-operations-and-technical-data/ ◦◦ Piercing depths vary from 12 to 58 inches depending on aircraft, container aircraft-rescue-firefighting-charts.html design, and location on aircraft. Average depth is about 26 inches • Apply appropriate extinguishing agent • BOEING: http://www.boeing.com/commercial/ • When discharging halotron into cargo area, avoid ventilating as much as possible airports/rescue_fire.page

84 BOEING NOTES 747-8F

85 © 2018 of America, Inc. UPS, the UPS brandmark, the color brown and photos are trademarks of United Parcel Service of America, Inc. All rights reserved.

180713RP