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612 Part 29—Airworthiness Stand- Ards: Transport

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612 Part 29—Airworthiness Stand- Ards: Transport Pt. 27, App. C 14 CFR Ch. I (1–1–03 Edition) (iii) The equipment, systems, and installa- 29.81—Landing distance (Ground level sites): tions must be designed so that one display of Category A. the information essential to the safety of 29.85—Balked landing: Category A. flight which is provided by the instruments 29.87(a)—Height-velocity envelope. will remain available to a pilot, without ad- 29.547(a) and (b)—Main and tail rotor struc- ditional crewmember action, after any single ture. failure or combination of failures that is not 29.861(a)—Fire protection of structure, con- shown to be extremely improbable; and trols, and other parts. (iv) For single-pilot configurations, instru- 29.901(c)—Powerplant: Installation. ments which require a static source must be 29.903(b) (c) and (e)—Engines. provided with a means of selecting an alter- 29.908(a)—Cooling fans. nate source and that source must be cali- 29.917(b) and (c)(1)—Rotor drive system: De- brated. sign. IX. Rotorcraft Flight Manual. A Rotorcraft 29.927(c)(1)—Additional tests. Flight Manual or Rotorcraft Flight Manual 29.953(a)—Fuel system independence. IFR Supplement must be provided and must 29.1027(a)—Transmission and gearboxes: Gen- contain— eral. (a) Limitations. The approved IFR flight en- 29.1045(a)(1), (b), (c), (d), and (f)—Climb cool- velope, the IFR flightcrew composition, the ing test procedures. revised kinds of operation, and the steepest 29.1047(a)—Takeoff cooling test procedures. IFR precision approach gradient for which 29.1181(a)—Designated fire zones: Regions in- the helicopter is approved; cluded. (b) Procedures. Required information for 29.1187(e)—Drainage and ventilation of fire proper operation of IFR systems and the rec- zones. ommended procedures in the event of sta- 29.1189(c)—Shutoff means. bility augmentation or electrical system 29.1191(a)(1)—Firewalls. failures; and 29.1193(e)—Cowling and engine compartment (c) Performance. If V differs from V , covering. YI Y 29.1195(a) and (d)—Fire extinguishing sys- climb performance at VYI and with maximum continuous power throughout the ranges of tems (one shot). weight, altitude, and temperature for which 29.1197—Fire extinguishing agents. 29.1199—Extinguishing agent containers. approval is requested. 29.1201—Fire extinguishing system materials. [Amdt. 27–19, 48 FR 4389, Jan. 31, 1983] 29.1305(a) (6) and (b)—Powerplant instru- ments. APPENDIX C TO PART 27—CRITERIA FOR 29.1309(b)(2) (i) and (d)—Equipment, systems, CATEGORY A and installations. 29.1323(c)(1)—Airspeed indicating system. C27.1 General. 29.1331(b)—Instruments using a power supply. A small multiengine rotorcraft may not be 29.1351(d)(2)—Electrical systems and equip- type certificated for Category A operation ment: General (operation without normal unless it meets the design installation and electrical power). performance requirements contained in this 29.1587(a)—Performance information. appendix in addition to the requirements of NOTE: In complying with the paragraphs this part. listed in paragraph C27.2 above, relevant ma- C27.2 Applicable part 29 sections. The fol- terial in the AC ‘‘Certification of Transport lowing sections of part 29 of this chapter Category Rotorcraft’’ should be used. must be met in addition to the requirements [Doc. No. 28008, 61 FR 21907, May 10, 1996] of this part: 29.45(a) and (b)(2)—General. 29.49(a)—Performance at minimum operating PART 29—AIRWORTHINESS STAND- speed. ARDS: TRANSPORT CATEGORY 29.51—Takeoff data: General. ROTORCRAFT 29.53—Takeoff: Category A. 29.55—Takeoff decision point: Category A. Subpart A—General 29.59—Takeoff Path: Category A. 29.60—Elevated heliport takeoff path: Cat- Sec. egory A. 29.1 Applicability. 29.61—Takeoff distance: Category A. 29.2 Special retroactive requirements. 29.62—Rejected takeoff: Category A. 29.64—Climb: General. Subpart B—Flight 29.65(a)—Climb: AEO. 29.67(a)—Climb: OEI. GENERAL 29.75—Landing: General. 29.21 Proof of compliance. 29.77—Landing decision point: Category A. 29.25 Weight limits. 29.79—Landing: Category A. 29.27 Center of gravity limits. 612 VerDate Dec<13>2002 08:22 Jan 27, 2003 Jkt 200041 PO 00000 Frm 00612 Fmt 8010 Sfmt 8010 Y:\SGML\200041T.XXX 200041T Federal Aviation Administration, DOT Pt. 29 29.29 Empty weight and corresponding cen- 29.337 Limit maneuvering load factor. ter of gravity. 29.339 Resultant limit maneuvering loads. 29.31 Removable ballast. 29.341 Gust loads. 29.33 Main rotor speed and pitch limits. 29.351 Yawing conditions. 29.361 Engine torque. PERFORMANCE 29.45 General. CONTROL SURFACE AND SYSTEM LOADS 29.49 Performance at minimum operating 29.391 General. speed. 29.395 Control system. 29.51 Takeoff data: general. 29.397 Limit pilot forces and torques. 29.53 Takeoff: Category A. 29.399 Dual control system. 29.55 Takeoff decision point (TDP): Cat- 29.411 Ground clearance: tail rotor guard. egory A. 29.427 Unsymmetrical loads. 29.59 Takeoff path: Category A. 29.60 Elevated heliport takeoff path: Cat- GROUND LOADS egory A. 29.61 Takeoff distance: Category A. 29.471 General. 29.62 Rejected takeoff: Category A. 29.473 Ground loading conditions and as- 29.63 Takeoff: Category B. sumptions. 29.64 Climb: General. 29.475 Tires and shock absorbers. 29.65 Climb: All engines operating. 29.477 Landing gear arrangement. 29.67 Climb: One engine inoperative (OEI). 29.479 Level landing conditions. 29.71 Helicopter angle of glide: Category B. 29.481 Tail-down landing conditions. 29.75 Landing: General. 29.483 One-wheel landing conditions. 29.77 Landing Decision Point (LDP): Cat- 29.485 Lateral drift landing conditions. egory A. 29.493 Braked roll conditions. 29.79 Landing: Category A. 29.497 Ground loading conditions: landing 29.81 Landing distance: Category A. gear with tail wheels. 29.83 Landing: Category B. 29.501 Ground loading conditions: landing 29.85 Balked landing: Category A. gear with skids. 29.87 Height-velocity envelope. 29.505 Ski landing conditions. 29.511 Ground load: unsymmetrical loads on FLIGHT CHARACTERISTICS multiple-wheel units. 29.141 General. 29.143 Controllability and maneuverability. WATER LOADS 29.151 Flight controls. 29.519 Hull type rotorcraft: Water-based and 29.161 Trim control. amphibian. 29.171 Stability: general. 29.521 Float landing conditions. 29.173 Static longitudinal stability. 29.175 Demonstration of static longitudinal MAIN COMPONENT REQUIREMENTS stability. 29.177 Static directional stability. 29.547 Main and tail rotor structure. 29.181 Dynamic stability: Category A rotor- 29.549 Fuselage and rotor pylon structures. craft. 29.551 Auxiliary lifting surfaces. GROUND AND WATER HANDLING EMERGENCY LANDING CONDITIONS CHARACTERISTICS 29.561 General. 29.231 General. 29.562 Emergency landing dynamic condi- 29.235 Taxiing condition. tions. 29.239 Spray characteristics. 29.563 Structural ditching provisions. 29.241 Ground resonance. FATIGUE EVALUATION MISCELLANEOUS FLIGHT REQUIREMENTS 29.571 Fatigue evaluation of structure. 29.251 Vibration. Subpart D—Design and Construction Subpart C—Strength Requirements GENERAL GENERAL 29.601 Design. 29.301 Loads. 29.602 Critical parts. 29.303 Factor of safety. 29.603 Materials. 29.305 Strength and deformation. 29.605 Fabrication methods. 29.307 Proof of structure. 29.607 Fasteners. 29.309 Design limitations. 29.609 Protection of structure. 29.610 Lightning and static electricity pro- FLIGHT LOADS tection. 29.321 General. 29.611 Inspection provisions. 613 VerDate Dec<13>2002 08:22 Jan 27, 2003 Jkt 200041 PO 00000 Frm 00613 Fmt 8010 Sfmt 8010 Y:\SGML\200041T.XXX 200041T Pt. 29 14 CFR Ch. I (1–1–03 Edition) 29.613 Material strength properties and de- 29.815 Main aisle width. sign values. 29.831 Ventilation. 29.619 Special factors. 29.833 Heaters. 29.621 Casting factors. 29.623 Bearing factors. FIRE PROTECTION 29.625 Fitting factors. 29.851 Fire extinguishers. 29.629 Flutter and divergence. 29.853 Compartment interiors. 29.631 Bird strike. 29.855 Cargo and baggage compartments. 29.859 Combustion heater fire protection. ROTORS 29.861 Fire protection of structure, controls, 29.653 Pressure venting and drainage of and other parts. rotor blades. 29.863 Flammable fluid fire protection. 29.659 Mass balance. 29.661 Rotor blade clearance. EXTERNAL LOADS 29.663 Ground resonance prevention means. 29.865 External loads. CONTROL SYSTEMS MISCELLANEOUS 29.671 General. 29.871 Leveling marks. 29.672 Stability augmentation, automatic, 29.873 Ballast provisions. and power-operated systems. 29.673 Primary flight controls. Subpart E—Powerplant 29.674 Interconnected controls. 29.675 Stops. GENERAL 29.679 Control system locks. 29.681 Limit load static tests. 29.901 Installation. 29.683 Operation tests. 29.903 Engines. 29.685 Control system details. 29.907 Engine vibration. 29.687 Spring devices. 29.908 Cooling fans. 29.691 Autorotation control mechanism. ROTOR DRIVE SYSTEM 29.695 Power boost and power-operated con- trol system. 29.917 Design. 29.921 Rotor brake. LANDING GEAR 29.923 Rotor drive system and control mech- 29.723 Shock absorption tests. anism tests. 29.725 Limit drop test. 29.927 Additional tests. 29.727 Reserve energy absorption drop test. 29.931 Shafting critical speed. 29.729 Retracting mechanism. 29.935 Shafting joints. 29.731 Wheels. 29.939 Turbine engine operating characteris- 29.733 Tires. tics. 29.735 Brakes. FUEL SYSTEM 29.737 Skis. 29.951 General. FLOATS AND HULLS 29.952 Fuel system crash resistance. 29.751 Main float buoyancy. 29.953 Fuel system independence. 29.753 Main float design. 29.954 Fuel system lightning protection. 29.755 Hull buoyancy. 29.955 Fuel flow. 29.757 Hull and auxiliary float strength. 29.957 Flow between interconnected tanks. 29.959 Unusable fuel supply. PERSONNEL AND CARGO ACCOMMODATIONS 29.961 Fuel system hot weather operation.
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