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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Make: Model: 

Description of Change: One-only STC  Multiple STC 

TCDS #: Original Certification Basis: Proposed Certification Basis: 

A1-1 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-2 

Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Method of Compliance* Plan, Drawing, Report Number Plan, Drawing, Report Number Person or Entity Finding Compliance Person or Entity Finding Compliance Applicable G

Applicable G

Title 14 CFR part 23: (CAR 3) Subpart A -- General Section 23.1 Applicability. (3.0) DE AC 23-8B 23.2 Special retroactive requirements. AN, GT 23.3 Airplane categories. (3.20 (less 2nd sent. of (a)(2) and 2nd and 3rd sent. of (b)), 3.20-1, 3.20-2 (1st sent.) DE AC 23-8B Subpart B -- Flight GENERAL 23.21 Proof of compliance. (3.61, 3.71-1) AN, GT, FT AC 23-8B 23.23 Load distribution limits. (3.71) DE, AN, FT AC 23-8B 23.25 Weight limits. (3.74, 3.75) AN, FT AC 23-8B 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-3

23.29 Empty weight and corresponding center of gravity. (3.73(1st sent.), 3.73-3(b))

AN, GT AC 23-8B

23.31 Removable ballast. (3.72) DE, AN AC 23-8B 23.33 Propeller speed and pitch limits. (3.418, 3.419, 3.420, 3.421)

AN, FT AC 23-8B 

PERFORMANCE 

23.45 General. (3.81) AN, GT, FT AC 23-8B 23.49 Stalling period. (3.82, 3.81-1, 3.83)

AN, FT AC 23-8B 

23.51 Takeoff speeds. (3.84 (less (c)),3.84-2, 3.84a, 3.780(a) (1st sent.))

AN, FT AC 23-8B 

23.53 Takeoff performance. AN, FT AC 23-8B23.55 Accelerate-stop distance. GT, FT AC 23-8B 23.57 Takeoff path. FT AC 23-8B23.59 Takeoff distance and takeoffrun. 

FT AC 23-8B

23.61 Takeoff flight path. FT AC 23-8B23.63 Climb: General. FT AC 23-8B23.65 Climb: All engines operating.(3.85(a),3.85-5(b) (less (1) and (2)), 3.85a(a), 3.419-1 (a) (2nd sent.))

FT AC 23-8B

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-4 

23.66 Takeoff climb: One-engine inoperative. 

FT AC 23-8B

23.67 Climb: One engine inoperative.(3.85(b), 3.85-3, 3.85a(b))

FT AC 23-8B

23.69 Enroute climb/descent. FT AC 23-8B23.71 Glide: Single-engine airplanes. FT AC 23-8B23.73 Reference landing approachspeed. 

FT AC 23-8B

23.75 Landing distance. (3.86(a), 3.87, 3.780(a) (1st sent.))

FT AC 23-8B

23.77 Balked landing. (3.85 (less (a)and (b)),3.85a (less (a) and (b))) 

FT AC 23-8B

FLIGHT CHARACTERISTICS 

23.141 General. (3.105) FT AC 23-8B

CONTROLLABILITY AND 

MANEUVERABILITY

23.143 General. (3.106) FT AC 23-8B, A23.145 Longitudinal control. (3.109) FT AC 23-8B23.147 Directional and lateral control. (3.110)

FT AC 23-8B

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-5

23.149 Minimum control speed. (3.111)

FT AC 23-8B

23.151 Acrobatic maneuvers. (3.107, 3.108)

FT AC 23-8B

23.153 Control during landings. FT AC 23-8B23.155 Elevator control force in maneuvers. 

FT AC 23-8B

23.157 Rate of roll. FT AC 23-8B

TRIM 

23.161 Trim. (3.112) FT AC 23-8B

STABILITY 

23.171 General. (3.113) FT AC 23-8B23.173 Static longitudinal stability. (3.114, 3.115 (less (a)-(c))) 

FT AC 23-8B

23.175 Demonstration of staticlongitudinal stability. (3.115 (a)-(c)) 

FT AC 23-8B

23.177 Static directional and lateral stability. (3.118)

FT AC 23-8B

23.181 Dynamic stability. (3.117) FT AC 23-8B

Page ___ of ___ 
Supplemental Type Certificate Compliance Checklist

Project Number: Date:

Originator: Revision:

pliance: 

FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of PExmpt = Petition for Exemption, N/A = Not Applicable 

Page ___ of ___ 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-6 

STALLS 

23.201 Wings level stall. (3.120(a),3.120(b), 3.120 (less (a)-(f)), 3.120-1,3.122 (2nd sent.))

FT AC 23-8B

23.203 Turning flight and accelerated turning stalls. (3.120(c), 3.120(d),3.120(e) (1st through 26th words), 3.121, 3.122 (less 2nd sent.))

FT AC 23-8B

23.207 Stall warning. (3.120(f)) FT AC 23-8B

SPINNING 

23.221 Spinning. (3.124(a) (less last sent.), 3.124(b), 3.124(c) (less (4)), 3.124(d))

FT AC 23-8B

GROUND AND WATER 

HANDLING CHARACTERISTICS

*Methods of Com23.231 Longitudinal stability and control. (3.144)

FT AC 23-8B

23.233 Directional stability and control. (3.145)

FT AC 23-8B

23.235 Operation on unpavedsurfaces. (3.146)

FT AC 23-8B
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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-7

23.237 Operation on water. FT AC 23-8B23.239 Spray characteristics. (3.147) FT AC 23-8B

MISCELLANEOUS FLIGHT 

REQUIREMENTS

23.251 Vibration and buffeting. (3.159)

FT AC 23-8B, PS

PS-ACE100-

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 23-1923.302 Canard or tandem wingconfigurations. 

AN, GT, FT AC 23-19

23.303 Factor of safety. (3.172) AN, GT AC 23-1923.305 Strength and deformation. (3.173)

AN, GT AC 23-19, PS

PS-ACE100-

23.307 Proof of structure. (3.174) AN, GT AC 23-19, PS

PS-ACE100-

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 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 G

A1-8 

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-9

23.365 Pressurized cabin loads. (3.197)

AN, GT AC 23-19

23.367 Unsymmetrical loads due toengine 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 23-1923.393 Loads parallel to hinge line. AN AC 23-1923.395 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 23-1923.405 Secondary control system. (3.234)

AN AC 23-19

23.407 Trim tab effects. (3.213) AN AC 23-1923.409 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

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. (3.216and notes, 3.216-4 (a) and (b))

AN AC 23-19

23.425 Gust loads. (3.217 and notes) AN AC 23-1923.427 Unsymmetrical loads. (3.218) AN AC 23-19

VERTICAL SURFACES 

23.441 Maneuvering loads. (3.219and notes)

AN AC 23-19

23.443 Gust loads. (3.220) AN AC 23-1923.445 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

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 23-1923.473 Ground load conditions andassumptions. (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 23-1923.493 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

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 23-1923.509 Towing loads. AN AC 23-1923.511 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 ofgravity positions. 

AN, GT AC 23-19

23.525 Application of loads. AN AC 23-1923.527 Hull and main float load factors. 

AN AC 23-19

23.529 Hull and main float landingconditions. 

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-13

23.533 Hull and main float bottompressures. 

AN AC 23-19

23.535 Auxiliary float loads. AN AC 23-1923.537 Seawing loads. AN, GT AC 23-19

EMERGENCY LANDING 

CONDITIONS 

23.561 General. AN, GT AC 23-1923.562 Emergency landing dynamic conditions. 

AN, GT AC 23-19, AC 

FATIGUE EVALUATION

23.571 Metallic pressurized cabinstructures. (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 fatigueevaluation of structure. 

AN, GT AC 23-19, PS

23.574 Metallic damage tolerance andfatigue evaluation of commuter category airplanes. 

AN, GT AC 23-19

23.575 Inspections and otherprocedures. 

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-14 

Subpart D -- Design and 

Construction 

23.601 General. (3.291) DE, AN, GT AC 23-19, PS

PS-ACE100-PS-ACE100-

23.603 Materials and workmanship. (3.292)

DE, AN, GT AC 23-19, PS

PS-ACE100-PS-ACE100-

23.605 Fabrication methods. (3.293) DE AC 23-19, PS

PS-ACE100-PS-ACE100-

23.607 Fasteners. (3.294 (last sent.)) DE AC 23-19, AC 23.609 Protection of structure. (3.295)

DE AC 23-19. PS

PS-ACE100-

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

PS-ACE100-PS-ACE100-

23.619 Special factors. (3.302, 3.303) AN, GT AC 23-1923.621 Casting factors. (3.304) AN, GT AC 23-1923.623 Bearing factors. (3.305) AN AC 23-1923.625 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-15

23.627 Fatigue strength. (3.307) AN AC 23-1923.629 Flutter. (3.311, 3.11-1, 3.311-2(a))

AN, GT, FT AC 23-19, AC 

PS-ACE100-

WINGS 

23.641 Proof of strength. (3.317) AN, GT AC 23-19

CONTROL SURFACES 

23.651 Proof of strength. (3.327) AN AC 23-1923.655 Installation. (3.328) DE, AN AC 23-1923.657 Hinges. (3.329) AN AC 23-1923.659 Mass balance. (3.330) AN AC 23-19

CONTROL SYSTEMS 

23.671 General. (3.335) DE, AN, GT,

FT 

AC 23-8B, A

PS-ACE100-

23.672 Stability augmentation and automatic and power-operated systems. 

DE, AN, GT,

FT 

AC 23-8B, A

PS-ACE100-

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-16 

23.677 Trim systems. (3.337) DE, AN, FT AC 23-8B, A

PS-ACE100-

23.679 Control system locks. DE, GT AC 23-8B, A

PS-ACE100-

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, A23.693 Joints. AN AC 23-17B 23.697 Wing flap controls. DE, FT AC 23-8B, A23.699 Wing flap position indicator. GT, FT AC 23-8B, A23.701 Flap interconnection. DE, AN, FT AC 23-8B, A23.703 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-17

23.729 Landing gear extension and retraction system. 

DE, AN, FT AC 23-8B, A

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, A23.737 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 23-17B23.753 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, A

AC 23-1311-PS-ACE100-

23.773 Pilot compartment view. GT, FT AC 23-8B, A

AC 23-1311-PS-ACE100-

23.775 Windshields and windows. DE, GT AC 23-8B, A

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-18 

23.777 Cockpit controls. DE, FT AC 23-8B, A

AC 23-1311-PS-ACE100-

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, A

PS-ACE100-

23.787 Baggage and cargocompartments. (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, A23.805 Flightcrew emergency exits. DE, AN AC 23-17B 23.807 Emergency exits. DE, GT AC 23-8B, A23.811 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, A

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

PRESSURIZATION 

23.841 Pressurized cabins. (3.395) DE, AN, GT AC 23-8B, A23.843 Pressurization tests. (3.396) GT, FT AC 23-8B, A

FIRE PROTECTION

23.851 Fire extinguishers. DE AC 23-17B 23.853 Passenger and crewcompartment interiors. 

AN, GT AC 23-2, AC 

PS-ACE100-PS-ACE100-

23.855 Cargo and baggage compartment fire protection. 

DE, GT AC 23-2, AC 

23.859 Combustion heater fire protection.

DE, AN, GT AC 23-17B 

23.863 Flammable fluid fireprotection.

DE and AN or

GT 

AC 23-17B

23.865 Fire protection of flightcontrols, engine mounts, and other flight structure.

DE, AN, GT AC 23-17B 

A1-19 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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

A1-20 

ELECTRICAL BONDING AND 

LIGHTNING PROTECTION

23.867 Electrical bonding andprotection against lightning and static electricity. 

DE, GT AC 23-17B, P

MISCELLANEOUS 

23.871 Leveling means. (3.401) DE AC 23-17B

Subpart E -- Powerplant 

GENERAL 

23.901 Installation. (3.411) DE, AN, GT,

FT 

AC 23-8B, A

AC 23-1311-

23.903 Engines. (3.415) DE, AN, GT,

FT 

AC 23-8B, A

23.904 Automatic power reserve system. 

AN, GT, FT AC 23-16A

23.905 Propellers. (3.416) DE, AN, GT,

FT 

AC 23-8B, A

23.907 Propeller vibration. (3.417) AN, GT, FT AC 23-16A23.909 Turbocharger systems. AN, GT, FT AC 23-8B, A

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 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 G

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Applicable G

23.925 Propeller clearance. (3.422, 3.422-2)

AN, GT AC 23-8B, A

23.929 Engine installation ice protection.

AN, GT, FT AC 23-8B, A

23.933 Reversing systems. AN, GT, FT AC 23-8B, A23.934 Turbojet and turbofan engine thrust reverser systems tests. 

AN, GT, FT AC 23-16A

23.937 Turbopropeller-drag limiting systems. 

AN AC 23-16A

23.939 Powerplant operatingcharacteristics. 

AN, GT, FT AC 23-8B, A

23.943 Negative acceleration. FT AC 23-8B, A

FUEL SYSTEM

23.951 General. (3.429, 3.430) AN, GT, FT AC 23-16A23.953 Fuel system independence. (3.431)

AN, GT, FT AC 23-16A

23.954 Fuel system lightningprotection.

DE, AN AC 23-16A, A

23.955 Fuel flow. (3.433, 3.434,3.435, 3.436)

DE, AN, GT AC 23-16A

23.957 Flow between interconnectedtanks. (3.439) 

DE, AN, GT AC 23-16A

A1-21 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-22 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.959 Unusable fuel supply. (3.437(a) (less last sent.), 3.437 (less (a))) 

AN, GT, FT AC 23-8B, A

23.961 Fuel system hot weatheroperation. (3.438)

DE, AN, GT,

FT 

AC 23-8B, A

23.963 Fuel tanks: General. (3.440(less last two sent.))

DE, AN, GT AC 23-16A

23.965 Fuel tank tests. (3.441) AN, GT AC 23-16A23.967 Fuel tank installation. (3.442, 3.442-1)

DE, AN AC 23-16A

23.969 Fuel tank expansion space. (3.443)

DE, AN AC 23-16A

23.971 Fuel tank sump. (3.444) DE, AN AC 23-16A23.973 Fuel tank filler connection.(3.445)

DE, AN AC 23-16A

23.975 Fuel tank vents and carburetorvapor vents. (3.446, 3.447A) 

DE, AN, GT,

FT 

AC 23-16A

23.977 Fuel tank outlet. (3.448) DE, AN AC 23-16A23.979 Pressure fueling systems. DE, GT AC 23-16A 

FUEL SYSTEM COMPONENTS 

23.991 Fuel pumps. (3.449, 3.449-1) DE, AN, GT,

FT 

AC 23-16A

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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.993 Fuel system lines and fittings. (3.550)

DE, AN, GT AC 23-16A

23.994 Fuel system components. DE, AN AC 23-16A23.995 Fuel valves and controls. (3.551, 3.633)

DE, AN, FT AC 23-16A

23.997 Fuel strainer or filter. (3.552) DE, AN, GT AC 23-16A23.999 Fuel system drains. (3.553) DE, AN, GT AC 23-16A23.1001 Fuel jettisoning system. DE, AN, GT, 

FT 

AC 23-8B, A

OIL SYSTEM

23.1011 General. (3.561, 3.561-1(b)) DE, AN, GT,

FT 

AC 23-16A

23.1013 Oil tanks. (3.563, 3.565,3.566, 3.567, 3.568, 3.569)

DE, AN, GT AC 23-2, AC 

23.1015 Oil tank tests. (3.564) AN, GT AC 23-16A23.1017 Oil lines and fittings. (3.570, 3.575)

DE, GT AC 23-16A

23.1019 Oil strainer or filter. (3.573) AN, GT AC 23-16A23.1021 Oil system drains. (3.574) AN, GT AC 23-16A23.1023 Oil radiators. (3.572) GT AC 23-16A23.1027 Propeller feathering system. (3.577)

AN, GT, FT AC 23-8B, A

A1-23 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-24 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

COOLING 

23.1041 General. (3.581) AN, GT, FT AC 23-8B, A23.1043 Cooling tests. (3.582, 3.582-1, 3.583, 3.583-1 (1st sent.), 3.584, 3.585)

AN, GT, FT AC 23-8B, A

23.1045 Cooling test procedures forturbine engine powered airplanes.(3.586)

AN, GT, FT AC 23-8B, A

23.1047 Cooling test procedures forreciprocating engine powered airplanes. (3.587)

AN, GT, FT AC 23-8B, A

LIQUID COOLING 

23.1061 Installation. (3.588. 3.589, 3.591, 3.592, 3.593, 3.594, 3.595)

DE, AN AC 23-16A

23.1063 Coolant tank tests. (3.590) AN, GT AC 23-16A

INDUCTION SYSTEM

23.1091 Air induction system. (3.605)

DE, AN, GT,

FT 

AC 23-2, AC 

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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.1093 Induction system icingprotection. (3.606) 

DE, SI, AN,

GT, FT 

AC 23-8B, A

23.1095 Carburetor deicing fluid flowrate. (3.607)

AN, GT AC 23-16A

23.1097 Carburetor deicing fluidsystem capacity. (3.608)

DE, AN AC 23-16A

23.1099 Carburetor deicing fluidsystem detail design. (3.609) 

DE, AN AC 23-16A

23.1101 Induction air preheaterdesign. (3.610)

DE, AN AC 23-16A

23.1103 Induction system ducts. (3.611)

DE, AN AC 23-16A

23.1105 Induction system screens. (3.612)

DE, AN AC 23-16A

23.1107 Induction system filters. DE, AN, GT AC 23-16A 23.1109 Turbocharger bleed air system. 

DE, AN, GT AC 23-16A

23.1111 Turbine engine bleed airsystem. 

DE, AN, GT,

FT 

AC 23-16A

EXHAUST SYSTEM

23.1121 General. (3.615) DE, AN, GT,

FT 

AC 23-16A

A1-25 Page ___ of ___ 
Supplemental Type Certificate Compliance Checklist

Project Number: Date:

Originator: Revision:

pliance: 

FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of PExmpt = Petition for Exemption, N/A = Not Applicable 

Page ___ of ___ 

A1-26 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.1123 Exhaust system. (3.616) DE, AN, GT,

FT 

AC 23-16A

23.1125 Exhaust heat exchangers.(3.617, 3.618)

DE, AN, GT,

FT 

AC 23-16A

POWERPLANT CONTROLS AND 

ACCESSORIES

*Methods of Com23.1141 Powerplant controls: General.(3.627)

DE, AN, GT,

FT 

AC 23-8B, A

23.1142 Auxiliary power unitcontrols. 

DE, AN, GT,

FT 

AC 23-16A

23.1143 Engine controls. (3.628) DE, AN, FT AC 23-16A23.1145 Ignition switches. (3.629) DE, AN AC 23-8B, A23.1147 Mixture controls. (3.630) DE, AN, FT AC 23-16A23.1149 Propeller speed and pitchcontrols. (3.631)

DE, AN, GT,

FT 

AC 23-16A

23.1153 Propeller feathering controls. (3.632)

DE, AN, GT,

FT 

AC 23-8B, A

23.1155 Turbine engine reverse thrustand propeller pitch settings below the flight regime. 

DE, AN, GT,

FT 

AC 23-16A

23.1157 Carburetor air temperaturecontrols. (3.634)

AN, GT AC 23-16A
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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.1163 Powerplant accessories. (3.635)

DE, AN AC 23-16A

23.1165 Engine ignition systems. (3.636)

AN, GT, FT AC 23-16A

POWERPLANT FIRE 

PROTECTION

23.1181 Designated fire zones; regions included. 

DE AC 23-16A

23.1182 Nacelle areas behindfirewalls. 

DE, AN, GT AC 23-16A

23.1183 Lines, fittings, andcomponents. (3.638)

DE, AN, GT AC 23-2, AC 

23.1189 Shutoff means. (3.637) DE, AN, GT AC 23-2, AC 23.1191 Firewalls. (3.623, 3.623-1, 3.624)

DE, AN, GT AC 23-2, AC 

23.1192 Engine accessory compartment diaphragm.

DE, AN, GT AC 23-2, AC 

23.1193 Cowling and nacelle. (3.625) DE, AN, GT AC 23-2, AC 23.1195 Fire extinguishing systems. DE, AN, GT, 

FT 

AC 23-16A

23.1197 Fire extinguishing agents. DE, AN, GT AC 23-16A

A1-27 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-28 

Regulation Title 14 CFR (1964 CAR 3) Applicable Amendment Method of Compliance* Method of Compliance* Plan, Drawing, Report Number Plan, Drawing, Report Number Person or Entity Finding Compliance Person or Entity Finding Compliance Applicable G

Applicable G

23.1199 Extinguishing agent containers. DE, AN AC 23-16A 23.1201 Fire extinguishing systems materials. DE, AN, GT AC 23-16A 23.1203 Fire detector system. DE, AN, GT AC 23-16A Subpart F -- Equipment GENERAL 23.1301 Function and installation. (3.651 (less 1st sent.), 3.652, 3.652-1) DE, AN, GT, FT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1303 Flight and navigation instruments. (3.655(a)) DE, AN, GT, FT AC 23-8B, A

AC 23.1311-

23.1305 Powerplant instruments. (3.655(b)) DE, GT, FT AC 23-8B, A23.1307 Miscellaneous equipment. (3.655(d)(1), 3.655 (less (a), (b), and (d))) DE AC 23-8B, A23.1309 Equipment, systems, and installations. AN, GT, FT AC 23-8B, A

AC 23.1309-AC 20-136, P

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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

INSTRUMENTS: INSTALLATION 

23.1311 Electronic display instrumentsystems. 

DE, AN, GT,

FT 

AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1321 Arrangement and visibility. (3.661, 3.662)

DE, GT, FT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1322 Warning, caution, andadvisory lights.

DE, GT, FT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1323 Airspeed indicating system. (3.663)

DE, GT, FT AC 23-8B, A

AC 23.1311-

23.1325 Static pressure system. (3.665)

DE, GT, FT AC 23-8B, A

23.1326 Pitot heat indication systems. DE, GT, FT AC 23-8B, A

PS-ACE100-

23.1327 Magnetic direction indicator. (3.666)

GT, FT AC 23-8B, A

23.1329 Automatic pilot system. (3.667)

DE, GT, FT AC 23-8B, A

23.1331 Instruments using a power source. (3.668)

DE, AN, GT,

FT 

AC 23-8B, A

AC 23.1311-

23.1335 Flight director systems. (3.669)

DE, GT, FT AC 23-8B, A

AC 23.1311-

A1-29 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-30 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.1337 Powerplant instruments installation. (3.671, 3.672, 3.672-1,3.673, 3.674, 3.675)

DE, GT, FT AC 23-8B, A

AC 23.1311-

ELECTRICAL SYSTEMS AND 

EQUIPMENT

23.1351 General. (3.681, 3.682, 3.685, 3.686, 3.687)

(DE and AN)

or GT, FT

AC 23-8B, A

AC 23.1311-

23.1353 Storage battery design and installation. (3.683)

AN, GT, FT AC 23-8B, A

AC 23.1311-

23.1357 Circuit protective devices. (3.690, 3.691, 3.692)

DE, AN, FT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1359 Electrical system fire protection.

AN, GT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1361 Master switch arrangement. (3.688, 3.689)

DE, GT AC 23-8B, A

AC 23.1311-

23.1365 Electric cables and equipment. (3.693)

DE, AN, GT AC 23-8B, A

AC 23.1311-

23.1367 Switches. (3.694, 3.695) DE, GT AC 23-8B, A

AC 23.1311-PS-ACE100-

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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

LIGHTS 

23.1381 Instrument lights. (3.696, 3.696-1, 3.697)

DE, GT, FT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1383 Taxi and landing lights. (3.698, 3.699)

DE, FT AC 23-8B, A

23.1385 Position light systeminstallation. (3.700)

DE, AN, GT AC 23-17B, A

23.1387 Position light system dihedralangles. (3.701)

DE, AN, GT AC 23-17B, A

23.1389 Position light distribution and intensities. (3.702, 3.702-1, 3.702-2)

DE, AN, GT AC 23-17B 

23.1391 Minimum intensities in the horizontal plane of position lights. (Figure 3-15)

DE, GT AC 23-17B 

23.1393 Minimum intensities in any vertical plane of position lights. (Figure 3-16)

DE, GT AC 23-17B 

23.1395 Maximum intensities inoverlapping beams of position lights. (Figure 3-17)

DE, GT AC 23-17B 

23.1397 Color specifications. (3.703) GT AC 23-17B23.1399 Riding light. (3.704) GT AC 23-17B23.1401 Anticollision light system. (3.705, 3.705-1 (1st sent.), Figure 3-18)

DE, AN, GT,

FT 

AC 23-17B, A

A1-31 Page ___ of ___ 
Supplemental Type Certificate Compliance Checklist

Project Number: Date:

Originator: Revision:

pliance: 

FT = Flight Test, GT = Ground Test, AN = Analysis, DE = Design, SI = Similarity, ELOS = Equivalent Level of PExmpt = Petition for Exemption, N/A = Not Applicable 

Page ___ of ___ 

*Methods of Com

A1-32 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

SAFETY EQUIPMENT 

23.1411 General. (3.711 (1st through27th words))

DE AC 23-8B, A

23.1415 Ditching equipment. (3.716,3.717, 3.718)

DE, GT AC 23-8B, A

23.1416 Pneumatic de-icer bootsystem. 

DE, GT AC 23-8B, A

AC 23.1419-AC 23.143-1

23.1419 Ice protection. (3.712) DE, SI, AN,

GT, FT, 

PExmpt

AC 23-8B, A

AC 23.1419-AC 23.143-1The analysis must be specibe required fo

MISCELLANEOUS EQUIPMENT 

23.1431 Electronic equipment.(3.721)

AN, GT, FT AC 23-8B, A

AC 23.1311-PS-ACE100-

23.1435 Hydraulic systems. (3.726, 3.727, 3.728)

AN, GT AC 23-8B, A

23.1437 Accessories for multiengine airplanes. (3.725)

DE AC 23-17B
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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.1438 Pressurization and pneumatic systems. 

AN or GT AC 23-17B 

23.1441 Oxygen equipment and supply. 

DE AC 23-8B, A

23.1443 Minimum mass flow ofsupplemental oxygen. 

AN AC 23-17B

23.1445 Oxygen distribution system. DE AC 23-17B 23.1447 Equipment standards for oxygen dispensing units. 

DE, GT, FT AC 23-8B, A

23.1449 Means for determining use ofoxygen.

DE AC 23-8B, A

23.1450 Chemical oxygen generators. DE AC 23-17B23.1451 Fire protection for oxygenequipment.

DE AC 23-17B

23.1453 Protection of oxygenequipment from rupture.

DE, GT AC 23-17B 

23.1457 Cockpit voice recorders. DE, GT, FT AC 23-8B, A23.1459 Flight recorders. DE, GT, FT AC 23-8B, A23.1461 Equipment containing highenergy rotors. 

AN, GT AC 23-17B

Subpart G -- Operating Limitations

and Information

23.1501 General. (3.735, 3.737) DE, FT AC 23-8B, A

A1-33 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-34 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

23.1505 Airspeed limitations. (3.738, 3.739, 3.740)

DE, FT AC 23-8B 

23.1507 Operating maneuvering speed. (3.741)

DE, FT AC 23-8B 

23.1511 Flap extended speed. (3.742) DE, FT AC 23-8B 23.1513 Minimum control speed. (3.743)

DE, FT AC 23-8B 

23.1519 Weight and center of gravity. (3.748)

DE, FT AC 23-8B 

23.1521 Powerplant limitations. (3.744)

DE, FT AC 23-8B 

23.1522 Auxiliary power unitlimitations. 

DE, FT

23.1523 Minimum flight crew. (3.749)

DE, FT AC 23-8B, A

PS-ACE100-

23.1524 Maximum passenger seating configuration. 

DE, FT AC 23-8B 

23.1525 Kinds of operation. (3.750) DE, FT AC 23-8B 23.1527 Maximum operating altitude. DE, FT AC 23-8B23.1529 Instructions for Continued Airworthiness. 

DE, AN, GT,

FT 

AC 23.1311-

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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 PExmpt = Petition for Exemption, N/A = Not Applicable 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

MARKINGS AND PLACARDS

23.1541 General. (3.755) DE, FT AC 23-8B, A

AC 20-88A

23.1543 Instrument markings: General. (3.756)

DE, FT AC 23-8B, A

AC 20-88A

23.1545 Airspeed indicator. (3.757) DE, FT AC 23-8B, A23.1547 Magnetic direction indicator. (3.758)

DE, FT AC 23-8B 

23.1549 Powerplant and auxiliary power unit instruments. (3.759)

DE, FT AC 23-8B, A

AC 20-88A

23.1551 Oil quantity indicator. (3.760)

DE, FT AC 23-8B, A

23.1553 Fuel quantity indicator. (3.761 (less 49th through 85th words))

DE, FT AC 23-8B, A

23.1555 Control markings. (3.762, 3.762-1, 3.763, 3.764, 3.765)

DE, FT AC 23-8B, A

PS-ACE100-

23.1557 Miscellaneous markings and placards. (3.766, 3.767, 3.768, 3.769)

DE, FT AC 23-8B 

23.1559 Operating limitations placard. (3.770, 3.772)

DE, FT AC 23-8B, A

23.1561 Safety equipment. DE, FT AC 23-8B23.1563 Airspeed placards. (3.771) DE, FT AC 23-8B 23.1567 Flight maneuver placard. DE, FT AC 23-8B

A1-35 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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-36 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

AIRPLANE FLIGHT MANUAL 

AND APPROVED MANUAL 

MATERIAL

23.1581 General. (3.777) DE, FT AC 23-8B, A23.1583 Operating limitations. (3.124(a) (last sentence), 3.124(c)(4),3.761 (49th through 85th words), 3.778)

DE, FT AC 23-8B, A

23.1585 Operating procedures. (3.779)

DE, FT AC 23-8B 

23.1587 Performance information.(3.84(c), 3.86(b), 3.120(e) (less 1stthrough 26th words), 3.123(b) (less (1)and (2)), 3.437(a) (last sent.), 3.440 (next to last sent.), 3.780, 3.780(b) (1stsent.))

DE, FT AC 23-8B 

23.1589 Loading information. (3.73-3 (less (a) and (b)),3.76)

DE, FT AC 23-8B 

Appendix A to Part 23 -- Simplified Design Load Criteria 

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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-37

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

Appendix B to Part 23 [Reserved](note following 3.211, Figures 3-3(a), 3-3(b), 3-4, 3-5(a), 3-5(b), 3-6, 3-7, 3-8, 3-9, 3-10)Appendix C to Part 23 -- Basic Landing Conditions (Figures 3-12(a), 3-12(b))Appendix D to Part 23 -- Wheel SpinUp and Spring-Back Loads (3.245-1(b)(equation and following))Appendix E to Part 23 [Reserved]Appendix F to Part 23 -- TestProcedure Appendix G to Part 23 -- Instructionsfor Continued Airworthiness Appendix H to Part 23 -- Installation ofAn Automatic Power Reserve (APR) SystemAppendix I to Part 23 -- Seaplane Loads 

EQUIVALENT LEVELS OF 

SAFETY (ELOS):

ELOS for 23.xxxELOS for 23.xxx

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 PExmpt = Petition for Exemption, N/A = Not Applicable 

A1-38 

Regulation 

Title 14 CFR (1964 CAR 3)

Applicable 

Amendment

Method of 

Compliance*

Method of 

Compliance*

Plan, Drawing, 

Report Number 

Plan, Drawing, 

Report Number 

Person or Entity 

Finding Compliance 

Person or Entity 

Finding Compliance 

Applicable GApplicable G

EXEMPTIONS:Exemption to 23.xxxExemption to 23.xxxSPECIAL CONDITIONS: Special Condition 1 Special Condition 2 Title 14 CFR part 34:

 Piston Engine N/A Turbine Engine (Reference 34.11) FAA only

Title 14 CFR part 36: [No Acoustical

Change] 

AN, FT FAA only AC 36-4C 

Title 14 CFR part 36: [Acoustical Change] 

AN, FT FAA only AC 36-4C 

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