Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks 8/24/05 AC 23-24 AC 23-24 Appendix 1Appendix 1 A1-7 A1-7
23.237 Operation on water. FT AC 23-8B
23.239 Spray characteristics. (3.147) FT AC 23-8B
MISCELLANEOUS FLIGHT
REQUIREMENTS
23.251 Vibration and buffeting.
(3.159) FT AC 23-8B, PS-ACE100-2001-004, PS-ACE100-2002-008
23.253 High speed characteristics. FT AC 23-8B
Subpart C -- Structure
GENERAL
23.301 Loads. (3.171,3.171-1) AN, GT, FT AC 23-19
23.302 Canard or tandem wing configurations.
AN, GT, FT AC 23-19
23.303 Factor of safety. (3.172) AN, GT AC 23-19
23.305 Strength and deformation.
(3.173) AN, GT AC 23-19, PS-ACE100-2001-006, PS-ACE100-2004-10030
23.307 Proof of structure. (3.174) AN, GT AC 23-19, PS-ACE100-2001-006, PS-ACE100-2004-10030
Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable
Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks
A1-8 AC 23-24 8/24/05 Appendix 1
FLIGHT LOADS
23.321 General. (3.181, 3.182) AN, GT, FT AC 23-19
23.331 Symmetrical flight conditions.
(3.183, 3.189) AN AC 23-19
23.333 Flight envelope. (3.185,
3.187, Figure 3-1) AN, GT AC 23-19
23.335 Design airspeeds. (3.184) AN AC 23-19
23.337 Limit maneuvering load factors. (3.186) AN AC 23-19
23.341 Gust loads factors. (3.188,
3.188-1) AN AC 23-19
23.343 Design fuel loads. AN, GT AC 23-19
23.345 High lift devices. (3.190 and note, 3.190-1)
AN, GT AC 23-19
23.347 Unsymmetrical flight conditions. (3.191 (less (a) and (b))) AN AC 23-19
23.349 Rolling conditions. (3.191(a) and note) AN, GT AC 23-19
23.351 Yawing conditions. (3.191(b)) AN, GT AC 23-19
23.361 Engine torque. (3.195) AN, GT AC 23-19
23.363 Side load on engine mount.
(3.196) AN, GT AC 23-19 Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks 8/24/05 AC 23-24 AC 23-24 Appendix 1Appendix 1 A1-9 A1-9
23.365 Pressurized cabin loads.
(3.197) AN, GT AC 23-19
23.367 Unsymmetrical loads due to engine failure.
AN, GT AC 23-19
23.369 Rear lift truss. (3.194 and note) AN AC 23-19
23.371 Gyroscopic and aerodynamic loads.
AN AC 23-19
23.373 Speed control devices. AN, GT AC 23-19
CONTROL SURFACE AND
SYSTEM LOADS
23.391 Control surface loads. (3.211) AN, GT AC 23-19
23.393 Loads parallel to hinge line. AN AC 23-19
23.395 Control system loads. (3.231,
3.231-1 (1st and 4th sent.), 3.231-2) AN, GT AC 23-19
23.397 Limit control forces and torques. (3.212, 3.212-1, Figure 3-11) AN, GT AC 23-19
23.399 Dual control system. (3.232) AN, GT AC 23-19
23.405 Secondary control system.
(3.234) AN AC 23-19
23.407 Trim tab effects. (3.213) AN AC 23-19
23.409 Tabs. (3.224) AN AC 23-19 Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks AC 23-24 8/24/05 Appendix 1
A1-10 A1-10
23.415 Ground gust conditions.
(3.233, 3.233-1) AN AC 23-19
HORIZONTAL STABILIZING
AND BALANCING SURFACES
23.421 Balancing loads. (3.215 and note) AN AC 23-19
23.423 Maneuvering loads. (3.216 and notes, 3.216-4 (a) and (b)) AN AC 23-19
23.425 Gust loads. (3.217 and notes) AN AC 23-19
23.427 Unsymmetrical loads. (3.218) AN AC 23-19
VERTICAL SURFACES
23.441 Maneuvering loads. (3.219 and notes) AN AC 23-19
23.443 Gust loads. (3.220) AN AC 23-19
23.445 Outboard fins or winglets.
(3.221) AN, GT AC 23-19
Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks 8/24/05 AC 23-24 AC 23-24 Appendix 1Appendix 1 A1-11 A1-11
AILERONS AND SPECIAL
DEVICES
23.455 Ailerons. (3.222(a), (b), and
(e)) AN AC 23-19
23.459 Special devices. (3.225) AN, GT AC 23-19
GROUND LOADS
23.471 General. (3.241) AN, GT AC 23-19
23.473 Ground load conditions and assumptions. (3.85-4 (last sent.),
3.242, 3.243) AN, GT AC 23-19
23.477 Landing gear arrangement.
(3.244) AN AC 23-19
23.479 Level landing conditions.
(3.245, 3.245-1(b)) AN, GT AC 23-19
23.481 Tail down landing conditions.
(3.246) AN, GT AC 23-19
23.483 One-wheel landing conditions.
(3.247) AN, GT AC 23-19
23.485 Side load conditions. (3.249) AN, GT AC 23-19
23.493 Braked roll conditions.
(3.248) AN, GT AC 23-19 Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks AC 23-24 8/24/05 Appendix 1
A1-12 A1-12
23.497 Supplementary conditions for tail wheels. (3.250, 3.251, 3.252) AN AC 23-19
23.499 Supplementary conditions for nose wheels. (3.253, 3.254, 3.255,
3.256) AN AC 23-19
23.505 Supplementary conditions for skiplanes. (3.257) AN AC 23-19
23.507 Jacking loads. AN AC 23-19
23.509 Towing loads. AN AC 23-19
23.511 Ground load; unsymmetrical loads on multiple-wheel units.
AN AC 23-19
WATER LOADS
23.521 Water load conditions. (3.265,
3.265-1(a), 3.265-2) AN, GT AC 23-19
23.523 Design weights and center of gravity positions.
AN, GT AC 23-19
23.525 Application of loads. AN AC 23-19
23.527 Hull and main float load factors.
AN AC 23-19
23.529 Hull and main float landing conditions.
AN AC 23-19
23.531 Hull and main float takeoff condition.
AN AC 23-19 Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks 8/24/05 AC 23-24 AC 23-24 Appendix 1Appendix 1 A1-13 A1-13
23.533 Hull and main float bottom pressures.
AN AC 23-19
23.535 Auxiliary float loads. AN AC 23-19
23.537 Seawing loads. AN, GT AC 23-19
EMERGENCY LANDING
CONDITIONS
23.561 General. AN, GT AC 23-19
23.562 Emergency landing dynamic conditions.
AN, GT AC 23-19, AC 23.562-1
FATIGUE EVALUATION
23.571 Metallic pressurized cabin structures. (3.270) AN, GT AC 23-19
23.572 Metallic wing, empennage, and associated structures.
AN, GT AC 23-19
23.573 Damage tolerance and fatigue evaluation of structure.
AN, GT AC 23-19, PS-ACE100-2001-006
23.574 Metallic damage tolerance and fatigue evaluation of commuter category airplanes.
AN, GT AC 23-19
23.575 Inspections and other procedures.
DE Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks AC 23-24 8/24/05 Appendix 1
A1-14 A1-14
Subpart D -- Design and Construction
23.601 General. (3.291) DE, AN, GT AC 23-19, PS-ACE100-2002-006, PS-ACE100-2001-006, PS-ACE100-2004-10039
23.603 Materials and workmanship.
(3.292) DE, AN, GT AC 23-19, PS-ACE100-2002-006, PS-ACE100-2001-006, PS-ACE100-2004-10039
23.605 Fabrication methods. (3.293) DE AC 23-19, PS-ACE100-2002-006, PS-ACE100-2001-006, PS-ACE100-2004-100399
23.607 Fasteners. (3.294 (last sent.)) DE AC 23-19, AC 23.607-1
23.609 Protection of structure.
(3.295) DE AC 23-19. PS-ACE100-2001-006, PS-ACE100-2004-10030
23.611 Accessibility provisions.
(3.296) DE AC 23-19
23.613 Material strength properties and design values. (3.301 and note) DE, AN, GT AC 23-19, PS-ACE100-2002-006, PS-ACE100-2001-006, PS-ACE100-2004-10030
23.619 Special factors. (3.302, 3.303) AN, GT AC 23-19
23.621 Casting factors. (3.304) AN, GT AC 23-19
23.623 Bearing factors. (3.305) AN AC 23-19
23.625 Fitting factors. (3.306) AN AC 23-19 Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks 8/24/05 AC 23-24 AC 23-24 Appendix 1Appendix 1 A1-15 A1-15
23.627 Fatigue strength. (3.307) AN AC 23-19
23.629 Flutter. (3.311, 3.11-1, 3.311- 2(a)) AN, GT, FT AC 23-19, AC 23.629-1B, PS-ACE100-2002-008
WINGS
23.641 Proof of strength. (3.317) AN, GT AC 23-19
CONTROL SURFACES
23.651 Proof of strength. (3.327) AN AC 23-19
23.655 Installation. (3.328) DE, AN AC 23-19
23.657 Hinges. (3.329) AN AC 23-19
23.659 Mass balance. (3.330) AN AC 23-19
CONTROL SYSTEMS
23.671 General. (3.335) DE, AN, GT, FT AC 23-8B, AC 23-17B, PS-ACE100-2001-004
23.672 Stability augmentation and automatic and power-operated systems.
DE, AN, GT, FT AC 23-8B, AC 23-17B, PS-ACE100-2001-004
23.673 Primary flight controls.
(3.336) DE AC 23-17B
23.675 Stops. DE, AN, FT AC 23-17B Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks AC 23-24 8/24/05 Appendix 1
A1-16 A1-16
23.677 Trim systems. (3.337) DE, AN, FT AC 23-8B, AC 23-17B, PS-ACE100-2001-004
23.679 Control system locks. DE, GT AC 23-8B, AC 23-17B, PS-ACE100-2001-004
23.681 Limit load static tests. AN or GT AC 23-17B
23.683 Operation tests. GT, FT AC 23-17B
23.685 Control system details. DE AC 23-17B
23.687 Spring devices. AN, GT, FT AC 23-17B
23.689 Cable systems. DE AC 23-17B
23.691 Artificial stall barrier system. AN, FT AC 23-8B, AC 23-17B
23.693 Joints. AN AC 23-17B
23.697 Wing flap controls. DE, FT AC 23-8B, AC 23-17B
23.699 Wing flap position indicator. GT, FT AC 23-8B, AC 23-17B
23.701 Flap interconnection. DE, AN, FT AC 23-8B, AC 23-17B
23.703 Takeoff warning system. DE, FT AC 23-17B
LANDING GEAR
23.721 General. AN or FT AC 23-17B
23.723 Shock absorption tests. AN or GT AC 23-17B
23.725 Limit drop tests. GT AC 23-17B
23.726 Ground load dynamic tests. AN or GT AC 23-17B
23.727 Reserve energy absorption drop test.
GT AC 23-17B Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks 8/24/05 AC 23-24 AC 23-24 Appendix 1Appendix 1 A1-17 A1-17
23.729 Landing gear extension and retraction system.
DE, AN, FT AC 23-8B, AC 23-17B
23.731 Wheels. DE, AN AC 23-17B
23.733 Tires. DE, AN AC 23-17B
23.735 Brakes. AN, GT, FT AC 23-8B, AC 23-17B
23.737 Skis. AN AC 23-17B
23.745 Nose/tail wheel steering. FT AC 23-17B
FLOATS AND HULLS
23.751 Main float buoyancy. DE, AN AC 23-17B
23.753 Main float design. AN, GT AC 23-17B
23.755 Hulls. DE, AN AC 23-17B
23.757 Auxiliary floats. AN AC 23-17B
PERSONNEL AND CARGO
ACCOMMODATIONS
23.771 Pilot compartment. DE, FT AC 23-8B, AC 23-17B, AC 23-1311-1A, PS-ACE100-2001-004
23.773 Pilot compartment view. GT, FT AC 23-8B, AC 23-17B, AC 23-1311-1A, PS-ACE100-2001-004
23.775 Windshields and windows. DE, GT AC 23-8B, AC 23-17B Page ___ of ___
Supplemental Type Certificate Compliance Checklist Project Number: Date:
Originator: Revision:
*Methods of Compliance:
FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of Safety Finding, PExmpt = Petition for Exemption, N/A = Not Applicable Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Plan, Drawing, Report Number Person or Entity Finding Compliance Applicable Guidance, References, & Remarks AC 23-24 8/24/05 Appendix 1
A1-18 A1-18
23.777 Cockpit controls. DE, FT AC 23-8B, AC 23-17B, AC 23-1311-1A, PS-ACE100-2001-004
23.779 Motion and effect of cockpit controls. (Figure 3-14) DE, FT AC 23-17B
23.781 Cockpit control knob shape.
(Figure 3-13) DE AC 23-17B
23.783 Doors. (3.389) DE, AN, GT AC 23-17B
23.785 Seats, berths, litters, safety belts, and shoulder harnesses. (3.390,
3.390-2) DE, AN, GT AC 23-8B, AC 23-17B, PS-ACE100-2001-004
23.787 Baggage and cargo compartments. (3.392) DE, AN, GT AC 23-17B
23.791 Passenger information signs. DE, GT AC 23-17B
23.803 Emergency evacuation. GT AC 23-8B, AC 23-17B
23.805 Flightcrew emergency exits. DE, AN AC 23-17B
23.807 Emergency exits. DE, GT AC 23-8B, AC 23-17B
23.811 Emergency exit marking. DE, AN AC 23-17B
23.812 Emergency lighting. DE, AN, GT AC 23-17B
23.813 Emergency exit access. DE, AN AC 23-17B
23.815 Width of aisle. DE AC 23-17B
23.831 Ventilation. (3.393) AN, GT, FT AC 23-8B, AC 23-17B
Page ___ of ___