Type Certificate Compliance Checklist

Project Number: Date:

Originator: Revision:

Make:
DRAFT
Description of Change: TC  ATC 
One-only STC  Multiple STC 
Model:

TCDS #:

Original Certification Basis:

Proposed Certification Basis:

*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

Appendix 1
Page ___ of ___

AC 23-25
A1-3
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:
DRAFT
Regulation Applicable Method of Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks
A1-4

Title 14 CFR part 23: (CAR 3)

Appendix 1
AC 23-25
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 DE AC 23-8B
2nd sent. of (a)(2) and 2nd and 3rd
sent. of (b)), 3.20-1, 3.20-2 (1st sent.)

Subpart B -- Flight

GENERAL

23.21 Proof of compliance. (3.61, AN, GT, FT AC 23-8B

3.71-1)
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
23.29 Empty weight and AN, GT AC 23-8B
corresponding center of gravity. (3.73
(1st sent.),
3.73-3(b))
23.31 Removable ballast. (3.72) DE, AN AC 23-8B

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.33 Propeller speed and pitch limits. AN, FT AC 23-8B

(3.418, 3.419, 3.420, 3.421)

PERFORMANCE

23.45 General. (3.81) AN, GT, FT AC 23-8B

23.49 Stalling period. (3.82, 3.81-1, AN, FT AC 23-8B
3.83)
23.51 Takeoff speeds. (3.84 (less (c)), AN, FT AC 23-8B
3.84-2, 3.84a, 3.780(a) (1st sent.))
23.53 Takeoff performance. AN, FT AC 23-8B
23.55 Accelerate-stop distance. GT, FT AC 23-8B
23.57 Takeoff path. FT AC 23-8B
23.59 Takeoff distance and takeoff FT AC 23-8B
run.
23.61 Takeoff flight path. FT AC 23-8B
23.63 Climb: General. FT AC 23-8B
23.65 Climb: All engines operating. FT AC 23-8B
(3.85(a),3.85-5(b) (less (1) and (2)),
3.85a(a), 3.419-1 (a) (2nd sent.))
23.66 Takeoff climb: One-engine FT AC 23-8B
inoperative.
23.67 Climb: One engine inoperative. FT AC 23-8B
(3.85(b), 3.85-3, 3.85a(b))
23.69 Enroute climb/descent. FT Appendix 1 AC 23-8B
23.71 Glide: Single-engine airplanes. FT AC 23-25 AC 23-8B

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.73 Reference landing approach FT AC 23-8B

speed.
23.75 Landing distance. (3.86(a), FT AC 23-8B
3.87, 3.780(a) (1st sent.))
23.77 Balked landing. (3.85 (less (a) FT AC 23-8B
and (b)),3.85a (less (a) and (b)))

FLIGHT CHARACTERISTICS

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

CONTROLLABILITY AND
MANEUVERABILITY

23.143 General. (3.106) FT AC 23-8B, AC 23.143-1

23.145 Longitudinal control. (3.109) FT AC 23-8B
23.147 Directional and lateral control. FT AC 23-8B
(3.110)
23.149 Minimum control speed. FT AC 23-8B
(3.111)
23.151 Acrobatic maneuvers. (3.107, FT AC 23-8B
3.108)
23.153 Control during landings. FT AC 23-8B
23.155 Elevator control force in FT AC 23-8B
maneuvers.
23.157 Rate of roll. FT AC 23-8B

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

TRIM

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

STABILITY

23.171 General. (3.113) FT AC 23-8B

23.173 Static longitudinal stability. FT AC 23-8B
(3.114, 3.115 (less (a)-(c)))
23.175 Demonstration of static FT AC 23-8B
longitudinal stability. (3.115 (a)-(c))
23.177 Static directional and lateral FT AC 23-8B
stability. (3.118)
23.181 Dynamic stability. (3.117) FT AC 23-8B

STALLS

23.201 Wings level stall. (3.120(a), FT AC 23-8B

3.120(b), 3.120 (less (a)-(f)), 3.120-1,
3.122 (2nd sent.))
23.203 Turning flight and accelerated FT AC 23-8B

Appendix 1
AC 23-25
turning stalls. (3.120(c), 3.120(d),
3.120(e) (1st through 26th words),
3.121, 3.122 (less 2nd sent.))
23.207 Stall warning. (3.120(f)) FT AC 23-8B

SPINNING
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.221 Spinning. (3.124(a) (less last FT AC 23-8B

sent.), 3.124(b), 3.124(c) (less (4)),
3.124(d))

GROUND AND WATER

HANDLING CHARACTERISTICS

23.231 Longitudinal stability and FT AC 23-8B

control. (3.144)
23.233 Directional stability and FT AC 23-8B
control. (3.145)
23.235 Operation on unpaved FT AC 23-8B
surfaces. (3.146)
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. FT AC 23-8B, PS-ACE100-2001-004,

(3.159) PS-ACE100-2002-008
23.253 High speed characteristics. FT AC 23-8B

Subpart C -- Structure

GENERAL
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.301 Loads. (3.171,3.171-1) AN, GT, FT AC 23-19

23.302 Canard or tandem wing AN, GT, FT AC 23-19
configurations.
23.303 Factor of safety. (3.172) AN, GT AC 23-19
23.305 Strength and deformation. AN, GT AC 23-19, PS-ACE100-2001-006,
(3.173) PS-ACE100-2004-10030
23.307 Proof of structure. (3.174) AN, GT AC 23-19, PS-ACE100-2001-006,
PS-ACE100-2004-10030

FLIGHT LOADS

23.321 General. (3.181, 3.182) AN, GT, FT AC 23-19

23.331 Symmetrical flight conditions. AN AC 23-19
(3.183, 3.189)
23.333 Flight envelope. (3.185, AN, GT AC 23-19
3.187, Figure 3-1)
23.335 Design airspeeds. (3.184) AN AC 23-19
23.337 Limit maneuvering load AN AC 23-19

Appendix 1
AC 23-25
factors. (3.186)
23.341 Gust loads factors. (3.188, AN AC 23-19
3.188-1)
23.343 Design fuel loads. AN, GT AC 23-19
23.345 High lift devices. (3.190 and AN, GT AC 23-19
note, 3.190-1)

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.347 Unsymmetrical flight AN AC 23-19

conditions. (3.191 (less (a) and (b)))
23.349 Rolling conditions. (3.191(a) AN, GT AC 23-19
and note)
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. AN, GT AC 23-19
(3.196)
23.365 Pressurized cabin loads. AN, GT AC 23-19
(3.197)
23.367 Unsymmetrical loads due to AN, GT AC 23-19
engine failure.
23.369 Rear lift truss. (3.194 and AN AC 23-19
note)
23.371 Gyroscopic and aerodynamic AN AC 23-19
loads.
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, AN, GT AC 23-19
3.231-1 (1st and 4th sent.), 3.231-2)

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.397 Limit control forces and AN, GT AC 23-19

torques. (3.212, 3.212-1, Figure 3-11)
23.399 Dual control system. (3.232) AN, GT AC 23-19
23.405 Secondary control system. AN AC 23-19
(3.234)
23.407 Trim tab effects. (3.213) AN AC 23-19
23.409 Tabs. (3.224) AN AC 23-19
23.415 Ground gust conditions. AN AC 23-19
(3.233, 3.233-1)

HORIZONTAL STABILIZING
AND BALANCING SURFACES

23.421 Balancing loads. (3.215 and AN AC 23-19

note)
23.423 Maneuvering loads. (3.216 AN AC 23-19
and notes, 3.216-4 (a) and (b))
23.425 Gust loads. (3.217 and notes) AN AC 23-19

Appendix 1
AC 23-25
23.427 Unsymmetrical loads. (3.218) AN AC 23-19

VERTICAL SURFACES

23.441 Maneuvering loads. (3.219 AN AC 23-19

and notes)
23.443 Gust loads. (3.220) AN AC 23-19
23.445 Outboard fins or winglets. AN, GT AC 23-19
(3.221)
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

AILERONS AND SPECIAL

DEVICES

23.455 Ailerons. (3.222(a), (b), and AN AC 23-19

(e))
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 AN, GT AC 23-19
assumptions. (3.85-4 (last sent.),
3.242, 3.243)
23.477 Landing gear arrangement. AN AC 23-19
(3.244)
23.479 Level landing conditions. AN, GT AC 23-19
(3.245, 3.245-1(b))
23.481 Tail down landing conditions. AN, GT AC 23-19
(3.246)
23.483 One-wheel landing conditions. AN, GT AC 23-19
(3.247)
23.485 Side load conditions. (3.249) AN, GT AC 23-19
23.493 Braked roll conditions. AN, GT AC 23-19
(3.248)
23.497 Supplementary conditions for AN AC 23-19
tail wheels. (3.250, 3.251, 3.252)
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.499 Supplementary conditions for AN AC 23-19

nose wheels. (3.253, 3.254, 3.255,
3.256)
23.505 Supplementary conditions for AN AC 23-19
skiplanes. (3.257)
23.507 Jacking loads. AN AC 23-19
23.509 Towing loads. AN AC 23-19
23.511 Ground load; unsymmetrical AN AC 23-19
loads on multiple-wheel units.

WATER LOADS

23.521 Water load conditions. (3.265, AN, GT AC 23-19

Appendix 1
AC 23-25
3.265-1(a), 3.265-2)
23.523 Design weights and center of AN, GT AC 23-19
gravity positions.
23.525 Application of loads. AN AC 23-19
23.527 Hull and main float load AN AC 23-19
factors.
23.529 Hull and main float landing AN AC 23-19
conditions.
23.531 Hull and main float takeoff AN AC 23-19
condition.
23.533 Hull and main float bottom AN AC 23-19
pressures.
23.535 Auxiliary float loads. AN AC 23-19
23.537 Seawing loads. AN, GT AC 23-19
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

EMERGENCY LANDING
CONDITIONS

23.561 General. AN, GT AC 23-19

23.562 Emergency landing dynamic AN, GT AC 23-19, AC 23.562-1
conditions.

FATIGUE EVALUATION

23.571 Metallic pressurized cabin AN, GT AC 23-19

structures. (3.270)
23.572 Metallic wing, empennage, AN, GT AC 23-19
and associated structures.
23.573 Damage tolerance and fatigue AN, GT AC 23-19, PS-ACE100-2001-006
evaluation of structure.
23.574 Metallic damage tolerance and AN, GT AC 23-19
fatigue evaluation of commuter
category airplanes.
23.575 Inspections and other DE
procedures.

Subpart D -- Design and

Construction

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

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

23.601 General. (3.291) DE, AN, GT AC 23-19, PS-ACE100-2002-006,

PS-ACE100-2001-006,
PS-ACE100-2004-10030
23.603 Materials and workmanship. DE, AN, GT AC 23-19, PS-ACE100-2002-006,
(3.292) PS-ACE100-2001-006,
PS-ACE100-2004-10030
23.605 Fabrication methods. (3.293) DE AC 23-19, PS-ACE100-2002-006,
PS-ACE100-2001-006,
PS-ACE100-2004-10030
23.607 Fasteners. (3.294 (last sent.)) DE AC 23-19, AC 23.607-1
23.609 Protection of structure. DE AC 23-19, PS-ACE100-2001-006,
(3.295) PS-ACE100-2004-10030
23.611 Accessibility provisions. DE AC 23-19
(3.296)
23.613 Material strength properties DE, AN, GT AC 23-19, PS-ACE100-2002-006,
and design values. (3.301 and note) PS-ACE100-2001-006,
PS-ACE100-2004-10030
23.619 Special factors. (3.302, 3.303) AN, GT AC 23-19, PS-ACE100-2001-006

Appendix 1
AC 23-25
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
23.627 Fatigue strength. (3.307) AN AC 23-19
23.629 Flutter. (3.311, 3.11-1, 3.311- AN, GT, FT AC 23-19, AC 23.629-1B,
2(a)) PS-ACE100-2002-008

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

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, AC 23-8B, AC 23-17B,

FT PS-ACE100-2001-004
23.672 Stability augmentation and DE, AN, GT, AC 23-8B, AC 23-17B,
automatic and power-operated systems. FT PS-ACE100-2001-004
23.673 Primary flight controls. DE AC 23-17B
(3.336)
23.675 Stops. DE, AN, FT AC 23-17B
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
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

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

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 GT AC 23-17B

23.723 Shock absorption tests. AN or GT AC 23-17B
23.725 Limit drop tests. GT AC 23-17B

Appendix 1
AC 23-25
23.726 Ground load dynamic tests. AN or GT AC 23-17B
23.727 Reserve energy absorption GT AC 23-17B
drop test.
23.729 Landing gear extension and DE, AN, FT AC 23-8B, AC 23-17B
retraction system.
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

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

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, AN, FT AC 23-8B, AC 23-17B
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 DE, FT AC 23-17B
controls. (Figure 3-14)
23.781 Cockpit control knob shape. DE AC 23-17B
(Figure 3-13)
23.783 Doors. (3.389) DE, AN, GT AC 23-17B

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.785 Seats, berths, litters, safety DE, AN, GT AC 23-8B, AC 23-17B,

belts, and shoulder harnesses. (3.390, PS-ACE100-2001-004
3.390-2)
23.787 Baggage and cargo DE, AN, GT AC 23-17B
compartments. (3.392)
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

PRESSURIZATION

23.841 Pressurized cabins. (3.395) DE, AN, GT AC 23-8B, AC 23-17B

23.843 Pressurization tests. (3.396) GT, FT AC 23-8B, AC 23-17B

Appendix 1
AC 23-25
FIRE PROTECTION

23.851 Fire extinguishers. DE AC 23-17B

23.853 Passenger and crew AN, GT AC 23-2, AC 23-17B,
compartment interiors. PS-ACE100-2004-10023,
PS-ACE100-2004-10030

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.855 Cargo and baggage DE, GT AC 23-2, AC 23-17B

compartment fire protection.
23.859 Combustion heater fire DE, AN, GT AC 23-17B
protection.
23.863 Flammable fluid fire DE and AN or AC 23-17B
protection. GT
23.865 Fire protection of flight DE, AN, GT AC 23-17B
controls, engine mounts, and other
flight structure.

ELECTRICAL BONDING AND

LIGHTNING PROTECTION

23.867 Electrical bonding and DE, GT AC 23-17B, PS-ACE100-2004-10030

protection against lightning and static
electricity.

MISCELLANEOUS

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

Subpart E -- Powerplant

GENERAL

23.901 Installation. (3.411) DE, AN, GT, AC 23-8B, AC 23-16A, AC 20-136,

FT AC 23-1311-1A
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFTPlan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.903 Engines. (3.415) DE, AN, GT, AC 23-8B, AC 23-16A, AC 20-136

FT
23.904 Automatic power reserve AN, GT, FT AC 23-16A
system.
23.905 Propellers. (3.416) DE, AN, GT, AC 23-8B, AC 23-16A
FT
23.907 Propeller vibration. (3.417) AN, GT, FT AC 23-16A
23.909 Turbocharger systems. AN, GT, FT AC 23-8B, AC 23-16A
23.925 Propeller clearance. (3.422, AN, GT AC 23-8B, AC 23-16A
3.422-2)
23.929 Engine installation ice AN, GT, FT AC 23-8B, AC 23-16A
protection.
23.933 Reversing systems. AN, GT, FT AC 23-8B, AC 23-16A
23.934 Turbojet and turbofan engine AN, GT, FT AC 23-16A
thrust reverser systems tests.
23.937 Turbopropeller-drag limiting AN AC 23-16A
systems.
23.939 Powerplant operating AN, GT, FT AC 23-8B, AC 23-16A

Appendix 1
AC 23-25
characteristics.
23.943 Negative acceleration. FT AC 23-8B, AC 23-16A

FUEL SYSTEM

23.951 General. (3.429, 3.430) AN, GT, FT AC 23-16A

23.953 Fuel system independence. AN, GT, FT AC 23-16A
(3.431)

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.954 Fuel system lightning DE, AN AC 23-16A, AC 20-53A, AC 20-136

protection.
23.955 Fuel flow. (3.433, 3.434, DE, AN, GT AC 23-16A
3.435, 3.436)
23.957 Flow between interconnected DE, AN, GT AC 23-16A
tanks. (3.439)
23.959 Unusable fuel supply. AN, GT, FT AC 23-8B, AC 23-16A
(3.437(a) (less last sent.), 3.437 (less
(a)))
23.961 Fuel system hot weather DE, AN, GT, AC 23-8B, AC 23-16A
operation. (3.438) FT
23.963 Fuel tanks: General. (3.440 DE, AN, GT AC 23-16A
(less last two sent.))
23.965 Fuel tank tests. (3.441) AN, GT AC 23-16A
23.967 Fuel tank installation. (3.442, DE, AN AC 23-16A
3.442-1)
23.969 Fuel tank expansion space. DE, AN AC 23-16A
(3.443)
23.971 Fuel tank sump. (3.444) DE, AN AC 23-16A
23.973 Fuel tank filler connection. DE, AN AC 23-16A
(3.445)
23.975 Fuel tank vents and carburetor DE, AN, GT, AC 23-16A
vapor vents. (3.446, 3.447A) FT
23.977 Fuel tank outlet. (3.448) DE, AN AC 23-16A
23.979 Pressure fueling systems. DE AC 23-16A

FUEL SYSTEM COMPONENTS

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.991 Fuel pumps. (3.449, 3.449-1) DE, AN, GT, AC 23-16A

FT
23.993 Fuel system lines and fittings. DE, AN, GT AC 23-16A
(3.550)
23.994 Fuel system components. DE, AN AC 23-16A
23.995 Fuel valves and controls. DE, AN, FT AC 23-16A
(3.551, 3.633)
23.997 Fuel strainer or filter. (3.552) DE, AN, GT AC 23-16A
23.999 Fuel system drains. (3.553) DE, AN, GT AC 23-16A
23.1001 Fuel jettisoning system. DE, AN, GT, AC 23-8B, AC 23-16A
FT

OIL SYSTEM

Appendix 1
AC 23-25
23.1011 General. (3.561, 3.561-1(b)) DE, AN, GT, AC 23-16A
FT
23.1013 Oil tanks. (3.563, 3.565, DE, AN, GT AC 23-16A
3.566, 3.567, 3.568, 3.569)
23.1015 Oil tank tests. (3.564) AN, GT AC 23-16A
23.1017 Oil lines and fittings. (3.570, DE, GT AC 23-16A
3.575)
23.1019 Oil strainer or filter. (3.573) AN, GT AC 23-16A
23.1021 Oil system drains. (3.574) AN, GT AC 23-16A
23.1023 Oil radiators. (3.572) GT AC 23-16A
23.1027 Propeller feathering system. AN, GT, FT AC 23-8B, AC 23-16A
(3.577)
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

COOLING

23.1041 General. (3.581) AN, GT, FT AC 23-8B, AC 23-16A

23.1043 Cooling tests. (3.582, 3.582- AN, GT, FT AC 23-8B, AC 23-16A
1, 3.583, 3.583-1 (1st sent.), 3.584,
3.585)
23.1045 Cooling test procedures for AN, GT, FT AC 23-8B, AC 23-16A
turbine engine powered airplanes.
(3.586)
23.1047 Cooling test procedures for AN, GT, FT AC 23-8B, AC 23-16A
reciprocating engine powered airplanes.
(3.587)

LIQUID COOLING

23.1061 Installation. (3.588. 3.589, DE, AN AC 23-16A

3.591, 3.592, 3.593, 3.594, 3.595)
23.1063 Coolant tank tests. (3.590) AN, GT AC 23-16A

INDUCTION SYSTEM

23.1091 Air induction system. DE, AN, GT, AC 23-8B, AC 23-16A

(3.605) FT
23.1093 Induction system icing DE, SI, AN, AC 23-8B, AC 23-16A
protection. (3.606) GT, FT

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1095 Carburetor deicing fluid flow AN, GT AC 23-16A

rate. (3.607)
23.1097 Carburetor deicing fluid DE, AN AC 23-16A
system capacity. (3.608)
23.1099 Carburetor deicing fluid DE, AN AC 23-16A
system detail design. (3.609)
23.1101 Induction air preheater DE, AN AC 23-16A
design. (3.610)
23.1103 Induction system ducts. DE, AN AC 23-16A
(3.611)
23.1105 Induction system screens. DE, AN AC 23-16A
(3.612)
23.1107 Induction system filters. DE, AN, GT AC 23-16A
23.1109 Turbocharger bleed air DE, AN, GT AC 23-16A

Appendix 1
AC 23-25
system.
23.1111 Turbine engine bleed air DE, AN, GT, AC 23-16A
system. FT

EXHAUST SYSTEM

23.1121 General. (3.615) DE, AN, GT, AC 23-16A

FT
23.1123 Exhaust system. (3.616) DE, AN, GT, AC 23-16A
FT
23.1125 Exhaust heat exchangers. DE, AN, GT, AC 23-16A
(3.617, 3.618) FT

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

POWERPLANT CONTROLS AND

ACCESSORIES

23.1141 Powerplant controls: General. DE, AN, GT, AC 23-8B, AC 23-16A

(3.627) FT
23.1142 Auxiliary power unit DE, AN, GT, AC 23-16A
controls. FT
23.1143 Engine controls. (3.628) DE, AN, FT AC 23-16A
23.1145 Ignition switches. (3.629) DE, AN AC 23-8B, AC 23-16A
23.1147 Mixture controls. (3.630) DE, AN, FT AC 23-16A
23.1149 Propeller speed and pitch DE, AN, GT, AC 23-16A
controls. (3.631) FT
23.1153 Propeller feathering controls. DE, AN, GT, AC 23-8B, AC 23-16A
(3.632) FT
23.1155 Turbine engine reverse thrust DE, AN, GT, AC 23-16A
and propeller pitch settings below the FT
flight regime.
23.1157 Carburetor air temperature AN, GT AC 23-16A
controls. (3.634)
23.1163 Powerplant accessories. DE, AN AC 23-16A
(3.635)
23.1165 Engine ignition systems. AN, GT, FT AC 23-16A
(3.636)

POWERPLANT FIRE
PROTECTION

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFTPlan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1181 Designated fire zones; DE AC 23-16A

regions included.
23.1182 Nacelle areas behind DE, AN, GT AC 23-16A
firewalls.
23.1183 Lines, fittings, and DE, AN, GT AC 23-16A
components. (3.638)
23.1189 Shutoff means. (3.637) DE, AN, GT. AC 23-8B, AC 23-16A
FT
23.1191 Firewalls. (3.623, 3.623-1, DE, AN, GT AC 23-16A
3.624)
23.1192 Engine accessory DE, AN, GT AC 23-16A
compartment diaphragm.
23.1193 Cowling and nacelle. (3.625) DE, AN, GT AC 23-16A

Appendix 1
AC 23-25
23.1195 Fire extinguishing systems. DE, AN, GT, AC 23-16A
FT
23.1197 Fire extinguishing agents. DE, AN, GT AC 23-16A
23.1199 Extinguishing agent DE, AN AC 23-16A
containers.
23.1201 Fire extinguishing systems DE, AN, GT AC 23-16A
materials.
23.1203 Fire detector system. DE, AN, GT, AC 23-16A
FT

Subpart F -- Equipment

GENERAL

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFTPlan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1301 Function and installation. DE, AN, GT, AC 23-8B, AC 23-17B, AC 20-136,
(3.651 (less 1st sent.), 3.652, 3.652-1) FT AC 23-1311-1A,
PS-ACE100-2001-004
23.1303 Flight and navigation DE, AN, GT, AC 23-8B, AC 23-17B,
instruments. (3.655(a)) FT AC 23-1311-1A
23.1305 Powerplant instruments. DE, GT, FT AC 23-8B, AC 23-17B,
(3.655(b)) AC 23-1311-1A
23.1307 Miscellaneous equipment. DE AC 23-8B, AC 23-17B
(3.655(d)(1), 3.655 (less (a), (b), and
(d)))
23.1309 Equipment, systems, and AN, GT, FT AC 23-8B, AC 23-17B,
installations. AC 23.1309-1C, AC 23-1311-1A,
AC 20-136, PS-ACE100-2001-004

INSTRUMENTS: INSTALLATION

23.1311 Electronic display instrument DE, AN, GT, AC 23-8B, AC 23-17B,

Appendix 1
AC 23-25
systems. FT AC 23.1311-1A,
PS-ACE100-2001-004
23.1321 Arrangement and visibility. DE, GT, FT AC 23-8B, AC 23-17B,
(3.661, 3.662) AC 23-1311-1A,
PS-ACE100-2001-004
23.1322 Warning, caution, and DE, GT, FT AC 23-8B, AC 23-17B,
advisory lights. AC 23-1311-1A,
PS-ACE100-2001-004
23.1323 Airspeed indicating system. DE, GT, FT AC 23-8B, AC 23-17B,
(3.663) AC 23-1311-1A

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1325 Static pressure system. DE, GT, FT AC 23-8B, AC 23-17B

(3.665)
23.1326 Pitot heat indication systems. DE, GT, FT AC 23-8B, AC 23-17B,
AC 23-1311-1A,
PS-ACE100-2002-007
23.1327 Magnetic direction indicator. GT, FT AC 23-8B, AC 23-17B
(3.666)
23.1329 Automatic pilot system. DE, GT, FT AC 23-8B, AC 23-17B
(3.667)
23.1331 Instruments using a power DE, AN, GT, AC 23-8B, AC 23-17B,
source. (3.668) FT AC 23-1311-1A
23.1335 Flight director systems. DE, GT, FT AC 23-8B, AC 23-17B,
(3.669) AC 23-1311-1A
23.1337 Powerplant instruments DE, GT, FT AC 23-8B, AC 23-17B,
installation. (3.671, 3.672, 3.672-1, AC 23-1311-1A
3.673, 3.674, 3.675)

ELECTRICAL SYSTEMS AND

EQUIPMENT

23.1351 General. (3.681, 3.682, DE and AN or AC 23-8B, AC 23-17B,

3.685, 3.686, 3.687) GT, FT AC 23-1311-1A
23.1353 Storage battery design and DE, AN, GT, AC 23-8B, AC 23-17B,
installation. (3.683) FT AC 23-1311-1A
23.1357 Circuit protective devices. DE, AN, FT AC 23-8B, AC 23-17B,
(3.690, 3.691, 3.692) AC 23-1311-1A,
PS-ACE100-2001-004
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1359 Electrical system fire AN, GT AC 23-2, AC 23-17B,

protection. AC 23-1311-1A,
PS-ACE100-2004-10023
23.1361 Master switch arrangement. DE, GT AC 23-8B, AC 23-17B,
(3.688, 3.689) AC 23-1311-1A
23.1365 Electric cables and DE, AN, GT AC 23-2, AC 23-17B,
equipment. (3.693) AC 23-1311-1A
23.1367 Switches. (3.694, 3.695) DE, GT AC 23-8B, AC 23-17B,
AC 23-1311-1A,
PS-ACE100-2001-004

LIGHTS

23.1381 Instrument lights. (3.696, DE, GT, FT AC 23-8B, AC 23-17B,

3.696-1, 3.697) AC 23-1311-1A,
PS-ACE100-2001-004
23.1383 Taxi and landing lights. DE, FT AC 23-8B, AC 23-17B
(3.698, 3.699)
23.1385 Position light system DE, AN, GT AC 23-17B, AC 20-74
installation. (3.700)
23.1387 Position light system dihedral DE, AN, GT AC 23-17B, AC 20-74

Appendix 1
AC 23-25
angles. (3.701)
23.1389 Position light distribution and DE, AN, GT AC 23-17B
intensities. (3.702, 3.702-1, 3.702-2)
23.1391 Minimum intensities in the DE, GT AC 23-17B
horizontal plane of position lights.
(Figure 3-15)

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1393 Minimum intensities in any DE, GT AC 23-17B

vertical plane of position lights.
(Figure 3-16)
23.1395 Maximum intensities in DE, GT AC 23-17B
overlapping beams of position lights.
(Figure 3-17)
23.1397 Color specifications. (3.703) GT AC 23-17B
23.1399 Riding light. (3.704) GT AC 23-17B
23.1401 Anticollision light system. DE, AN, GT, AC 23-17B, AC 20-74
(3.705, 3.705-1 (1st sent.), Figure 3-18) FT

SAFETY EQUIPMENT

23.1411 General. (3.711 (1st through DE, AN AC 23-8B, AC 23-17B

27th words))
23.1415 Ditching equipment. (3.716, DE, GT AC 23-8B, AC 23-17B
3.717, 3.718)
23.1416 Pneumatic de-icer boot DE, AN, GT, AC 23-8B, AC 23-17B, AC 23.1419-

Appendix 1
AC 23-25
system. FT 2C, AC 20-73, AC 23.143-1
23.1419 Ice protection. (3.712) DE, SI, AN, AC 23-8B, AC 23-17B, AC 23.1419-
GT, FT 2C, AC 20-73, AC 23.143-1
The analysis and tests to be conducted
must be specified. An exemption may
be required for stall speed in icing.

MISCELLANEOUS EQUIPMENT

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

23.1431 Electronic equipment. AN, GT, FT AC 23-8B, AC 23-17B,

(3.721) AC 23-1311-1A, AC 20-136,
PS-ACE100-2001-004
23.1435 Hydraulic systems. (3.726, AN, GT AC 23-8B, AC 23-17B
3.727, 3.728)
23.1437 Accessories for multiengine DE AC 23-17B
airplanes. (3.725)
23.1438 Pressurization and pneumatic AN or GT AC 23-17B
systems.
23.1441 Oxygen equipment and DE AC 23-8B, AC 23-17B
supply.
23.1443 Minimum mass flow of AN AC 23-17B
supplemental oxygen.
23.1445 Oxygen distribution system. DE AC 23-17B
23.1447 Equipment standards for DE, GT, FT AC 23-8B, AC 23-17B
oxygen dispensing units.
23.1449 Means for determining use of DE AC 23-8B, AC 23-17B
oxygen.
23.1450 Chemical oxygen generators. DE AC 23-17B
23.1451 Fire protection for oxygen DE AC 23-17B
equipment.
23.1453 Protection of oxygen DE, GT AC 23-17B

Appendix 1
AC 23-25
equipment from rupture.
23.1457 Cockpit voice recorders. DE, GT, FT AC 23-8B, AC 23-17B
23.1459 Flight recorders. DE, GT, FT AC 23-8B, AC 23-17B
23.1461 Equipment containing high AN, GT AC 23-17B
energy rotors.
*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

Subpart G -- Operating Limitations

and Information

23.1501 General. (3.735, 3.737) DE, FT AC 23-8B, AC 23-1311-1A

23.1505 Airspeed limitations. (3.738, DE, FT AC 23-8B
3.739, 3.740)
23.1507 Operating maneuvering DE, FT AC 23-8B
speed. (3.741)
23.1511 Flap extended speed. (3.742) DE, FT AC 23-8B
23.1513 Minimum control speed. DE, FT AC 23-8B
(3.743)
23.1519 Weight and center of gravity. DE, FT AC 23-8B
(3.748)
23.1521 Powerplant limitations. DE, FT AC 23-8B
(3.744)
23.1522 Auxiliary power unit DE, FT
limitations.
23.1523 Minimum flight crew. DE, FT AC 23-8B, AC 23.1523,
(3.749) PS-ACE100-2001-004
23.1524 Maximum passenger seating DE, FT AC 23-8B
configuration.
23.1525 Kinds of operation. (3.750) DE, FT AC 23-8B
23.1527 Maximum operating altitude. DE, FT AC 23-8B
23.1529 Instructions for Continued DE, AN, GT, AC 23-1311-1A
Airworthiness. FT

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

MARKINGS AND PLACARDS

23.1541 General. (3.755) DE, FT AC 23-8B, AC 23-1311-1A,

AC 20-88A
23.1543 Instrument markings: DE, FT AC 23-8B, AC 23-1311-1A,
General. (3.756) AC 20-88A
23.1545 Airspeed indicator. (3.757) DE, FT AC 23-8B, AC 23-1311-1A
23.1547 Magnetic direction indicator. DE, FT AC 23-8B
(3.758)
23.1549 Powerplant and auxiliary DE, FT AC 23-8B, AC 23-1311-1A,
power unit instruments. (3.759) AC 20-88A
23.1551 Oil quantity indicator. DE, FT AC 23-8B, AC 23-1311-1A
(3.760)
23.1553 Fuel quantity indicator. DE, FT AC 23-8B, AC 23-1311-1A
(3.761 (less 49th through 85th words))
23.1555 Control markings. (3.762, DE, FT AC 23-8B, AC 23-1311-1A,
3.762-1, 3.763, 3.764, 3.765) PS-ACE100-2001-004
23.1557 Miscellaneous markings and DE, FT AC 23-8B

Appendix 1
AC 23-25
placards. (3.766, 3.767, 3.768, 3.769)
23.1559 Operating limitations placard. DE, FT AC 23-8B, AC 23-1311-1A
(3.770, 3.772)
23.1561 Safety equipment. DE, FT AC 23-8B
23.1563 Airspeed placards. (3.771) DE, FT AC 23-8B
23.1567 Flight maneuver placard. DE, FT AC 23-8B

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

AIRPLANE FLIGHT MANUAL

AND APPROVED MANUAL
MATERIAL

23.1581 General. (3.777) DE, FT AC 23-8B, AC 23-1311-1A

23.1583 Operating limitations. DE, FT AC 23-8B, AC 23-1311-1A
(3.124(a) (last sentence), 3.124(c)(4),
3.761 (49th through 85th words),
3.778)
23.1585 Operating procedures. DE, FT AC 23-8B
(3.779)
23.1587 Performance information. DE, FT AC 23-8B
(3.84(c), 3.86(b), 3.120(e) (less 1st
through 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) (1st
sent.))
23.1589 Loading information. (3.73-3 DE, FT AC 23-8B
(less (a) and (b)),
3.76)

Appendix A to Part 23 -- Simplified

Design Load Criteria
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)

*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
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 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

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

Appendix C to Part 23 -- Basic Landing

Conditions (Figures 3-12(a), 3-12(b))
Appendix D to Part 23 -- Wheel Spin-
Up and Spring-Back Loads (3.245-1(b)
(equation and following))
Appendix E to Part 23 [Reserved]
Appendix F to Part 23 -- Test
Procedure
Appendix G to Part 23 -- Instructions
for Continued Airworthiness
Appendix H to Part 23 -- Installation of
An Automatic Power Reserve (APR)
System
Appendix I to Part 23 -- Seaplane
Loads

EQUIVALENT LEVELS OF

Appendix 1
AC 23-25
SAFETY (ELOS):
ELOS for 23.xxx

ELOS for 23.xxx

EXEMPTIONS:
Exemption to 23.xxx

Exemption to 23.xxx

*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
Page ___ of ___
 Type Certificate Compliance Checklist
Project Number: Date:
Originator: Revision:

Regulation Applicable Method of

DRAFT
Plan, Drawing, Person or Entity Applicable Guidance, References, &
Title 14 CFR (1964 CAR 3) Amendment Compliance* Report Number Finding Compliance Remarks

SPECIAL 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 AN, FT FAA only AC 36-4C
Change]

Title 14 CFR part 36: [Acoustical AN, FT FAA only AC 36-4C

Change]

*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
Page ___ of ___