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569 

Federal Aviation Administration, DOT 

Pt. 29 

(4) From 100 MHz to 8 GHz, use radiated 

susceptibility tests at a minimum of 5 V/m. 

[Doc. No. FAA–2006–23657, 72 FR 44027, Aug. 6, 
2007] 

PART 29—AIRWORTHINESS STAND-

ARDS: TRANSPORT CATEGORY 
ROTORCRAFT 

Subpart A—General 

Sec. 
29.1

Applicability. 

29.2

Special retroactive requirements. 

Subpart B—Flight 

G

ENERAL

 

29.21

Proof of compliance. 

29.25

Weight limits. 

29.27

Center of gravity limits. 

29.29

Empty weight and corresponding cen-

ter of gravity. 

29.31

Removable ballast. 

29.33

Main rotor speed and pitch limits. 

P

ERFORMANCE

 

29.45

General. 

29.49

Performance at minimum operating 

speed. 

29.51

Takeoff data: general. 

29.53

Takeoff: Category A. 

29.55

Takeoff decision point (TDP): Cat-

egory A. 

29.59

Takeoff path: Category A. 

29.60

Elevated heliport takeoff path: Cat-

egory A. 

29.61

Takeoff distance: Category A. 

29.62

Rejected takeoff: Category A. 

29.63

Takeoff: Category B. 

29.64

Climb: General. 

29.65

Climb: All engines operating. 

29.67

Climb: One engine inoperative (OEI). 

29.71

Helicopter angle of glide: Category B. 

29.75

Landing: General. 

29.77

Landing Decision Point (LDP): Cat-

egory A. 

29.79

Landing: Category A. 

29.81

Landing distance: Category A. 

29.83

Landing: Category B. 

29.85

Balked landing: Category A. 

29.87

Height-velocity envelope. 

F

LIGHT

C

HARACTERISTICS

 

29.141

General. 

29.143

Controllability and maneuverability. 

29.151

Flight controls. 

29.161

Trim control. 

29.171

Stability: general. 

29.173

Static longitudinal stability. 

29.175

Demonstration of static longitudinal 

stability. 

29.177

Static directional stability. 

29.181

Dynamic stability: Category A rotor-

craft. 

G

ROUND AND

W

ATER

H

ANDLING

 

C

HARACTERISTICS

 

29.231

General. 

29.235

Taxiing condition. 

29.239

Spray characteristics. 

29.241

Ground resonance. 

M

ISCELLANEOUS

F

LIGHT

R

EQUIREMENTS

 

29.251

Vibration. 

Subpart C—Strength Requirements 

G

ENERAL

 

29.301

Loads. 

29.303

Factor of safety. 

29.305

Strength and deformation. 

29.307

Proof of structure. 

29.309

Design limitations. 

F

LIGHT

L

OADS

 

29.321

General. 

29.337

Limit maneuvering load factor. 

29.339

Resultant limit maneuvering loads. 

29.341

Gust loads. 

29.351

Yawing conditions. 

29.361

Engine torque. 

C

ONTROL

S

URFACE AND

S

YSTEM

L

OADS

 

29.391

General. 

29.395

Control system. 

29.397

Limit pilot forces and torques. 

29.399

Dual control system. 

29.411

Ground clearance: tail rotor guard. 

29.427

Unsymmetrical loads. 

G

ROUND

L

OADS

 

29.471

General. 

29.473

Ground loading conditions and as-

sumptions. 

29.475

Tires and shock absorbers. 

29.477

Landing gear arrangement. 

29.479

Level landing conditions. 

29.481

Tail-down landing conditions. 

29.483

One-wheel landing conditions. 

29.485

Lateral drift landing conditions. 

29.493

Braked roll conditions. 

29.497

Ground loading conditions: landing 

gear with tail wheels. 

29.501

Ground loading conditions: landing 

gear with skids. 

29.505

Ski landing conditions. 

29.511

Ground load: unsymmetrical loads on 

multiple-wheel units. 

W

ATER

L

OADS

 

29.519

Hull type rotorcraft: Water-based and 

amphibian. 

29.521

Float landing conditions. 

M

AIN

C

OMPONENT

R

EQUIREMENTS

 

29.547

Main and tail rotor structure. 

29.549

Fuselage and rotor pylon structures. 

29.551

Auxiliary lifting surfaces. 

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