INS = Inertial Navigation System ICAO = International Civil Aviation Organization ILS = Instrument Landing System ISA = International Standard Atmosphere JAR = Joint Aviation Requirements (of Europe) Log = logarithmic value to base 10 m = meter MLW = Maximum Landing Weight MSL = Mean Sea Level altitude, feet MTOGW = Maximum Take-off Gross Weight N1 = Low Pressure Rotor Speed (Power Setting Parameter), rpm or % NAC = No Acoustical Change NCS = Noise Certification Specialist NIST = National Institute of Standards and Technology NPD = Noise-Power-Distance RFM = Rotorcraft Flight Manual RH = Relative Humidity, % rms = root-mean-square rpm = revolutions per minute SAE = Society of Automotive Engineers SBV = Surge Bleed Valve (engine internal operating valves) STC = Supplemental Type Certificate TIA = Type Inspection Authorization TC = Type Certificate TM = Technical Manual (“ICAO Environmental Technical Manual on the use of Procedures in the Noise Certification of Aircraft”) TSPI = Time Space Positional Information VNTSC = Volpe National Transportation System Center (DOT) VREF = Reference Landing Speed
6. - 7. RESERVED.
TABLE OF CONTENTS
1. PURPOSE1
2. CANCELLATION6
3. REFERENCES6
4. DEFINITIONS7
5. ABBREVIATION AND ACRONYMS9
6. - 7. RESERVED10
I. CERTIFICATION PROCEDURES FOR PRODUCT AND PARTS 14 CFR PART 2119
8. PART 21 - GENERAL19
9.-11. [RESERVED]19
II. NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION 14 CFR
PART 3620
12. PART 36 – SUBPART A-GENERAL20
13. Section 36.1 Applicability and definitions20
14. Section 36.1(a)20
15. Section 36.1(b)21
16. Section 36.1(c)22
17. Section 36.1(d)24
18. Section 36.1(e)25
19. Section 36.1(f)26
20. Section 36.1(g)26
21. Section 36.1(h)27
22. Section 36.2 Requirements as of date of application28
23. Section 36.3 Compatibility with airworthiness requirements29
24. Section 36.5 Limitation of part29
25. Section 36.6 Incorporations by reference30
26. Section 36.6(a)30
27. Section 36.6(b)30
28. Section 36.6(c)31
29. Section 36.6(d)31
30. Section 36.6(e)32
31. Section 36.7 Acoustical Change: Transport category large airplanes and jet airplanes37
32. Section 36.7(a)37
33. Section 36.7(b)37
34. Section 36.7(c)38
35. Section 36.7(d)39
36. Section 36.7(e)39
37. Section 36.9 Acoustical change: Propeller-driven small airplanes and propeller-driven commuter
category airplanes [To be completed later]40
38. Section 36.9(a) [To be completed later]40
39. Section 36.9(b) [To be completed later]40
40. Section 36.11 Acoustical Change: Helicopters40
41. Section 36.11(a)40
42. Section 36.11(b)41
43. Section 36.11(c)42
44. – 50. RESERVED42
III. SUBPART B— TRANSPORT CATEGORY LARGE AIRPLANES AND JET AIRPLANES43
51. Section 36.101 Noise measurement and evaluation43
52. Section 36.103 Noise limits44
53. Section 36.103(a)45
54. Section 36.103(b)45
IV. SUBPART C—RESERVED46
V. SUBPART D—NOISE LIMITS FOR SUPERSONIC TRANSPORT CATEGORY AIRPLANES47
55. Section 36.301 Noise limits: Concorde47
56. Section 36.301(a)47
57. Section 36.301(b)47
VI. SUBPART E--[RESERVED]48
VII. SUBPART F--PROPELLER-DRIVEN SMALL AIRPLANES AND PROPELLER-DRIVEN,
COMMUTER CATEGORY AIRPLANES49
58. Section 36.501 Noise Limits49
59. Section 36.501(a)49
60. Section 36.501(b)49
61. Section 36.501(c)49
VIII. SUBPART G--[RESERVED]50
62. -65 [RESERVED]50
IX. SUBPART H--HELICOPTERS51
66. Section 36.801 Noise measurement [To be completed later]51
67. Section 36.803 Noise evaluation and calculation [To be completed later]51
68. Section 36.805 Noise limits [To be completed later]51
69. Section 36.805(a) [To be completed later]51
70. Section 36.801(b) [To be completed later]51
71. Section 36.805(c)51
72. Section 36.805(d) [To be completed later]52
X. SUBPARTS I--N [RESERVED]53
73. –75 [RESERVED]53
XI. SUBPART E--RESERVED54
XII. SUBPART O--OPERATING LIMITATIONS AND INFORMATION55
76. Section 36.1501 Procedures, noise levels and other information55
77. Section 36.1501(a)55
78. Section 36.1501(b)61
79. Section 36.1581 Manuals, markings, and placards62
80. Section 36.1581(a)62
81. Section 36.1581(b)64
82. Section 36.1581(c)65
83. Section 36.1581(d)65
84. Section 36.1581(e)66
85. Section 36.1581(f)66
86. Section 36.1581(g)66
87. Section 36.1583 Noncomplying agricultural and fire fighting airplanes66
88. Section 36.1583(a)66
89. Section 36.1583(b)67
90. - 99 [RESERVED]68
XIII. APPENDIX A TO Part 36-AIRCRAFT NOISE MEASUREMENT AND EVALUATION UNDER §
36.101 69
100. Appendix A to Part 36-Aircraft Noise Measurement and Evaluation Under § 36.10169
101. Section A36.1 Introduction69
102. Section A36.1.169
103. Section A36.1.269
104. Section A36.1.369
105. Section A36.2. Noise certification test and measurement conditions69
106. Section A36.2.1 General69
107. Section A36.2.1.170
108. Section A36.2.2 Test environment70
109. Section A36.2.2.170
110. Section A36.2.2.271
111. Section A36.2.2.2(a)72
112. Section A36.2.2.2(b)72
113. Section A36.2.2.2(c)73
114. Section A36.2.2.2(d)74
115. Section A36.2.2.2(e)75
116. Section A36.2.2.2(f)76
117. Section A36.2.2.2(g)77
118. Section A36.2.2.377
119. Section A36.2.2.479
120. Section A36.2.3 Flight path measurement80
121. Section A36.2.3.180
122. Section A36.2.3.281
123. Section A36.2.3.383
124. Section A36.3 Measurement of Airplane Noise Received on the Ground83
125. Section A36.3.1 Definitions84
126. Section A36.3.1.184
127. Section A36.3.1.284
128. Section A36.3.1.384
129. Section A36.3.1.484
130. Section A36.3.1.584
131. Section A36.3.1.684
132. Section A36.3.1.785
133. Section A36.3.1.885
134. Section A36.3.1.985
135. Section A36.3.1.1085
136. Section A36.3.1.1185
137. Section A36.3.1.1285
138. Section A36.3.1.1385
139. Section A36.3.1.1485
140. Section A36.3.1.1585
141. Section A36.3.1.1686
142. Section A36.3.2 Reference environmental conditions86
143. Section A36.3.2.186
144. Section A36.3.3 General86
145. Section A36.3.3.187
146. Section A36.3.3.288
147. Section A36.3.4 Windscreen88
148. Section A36.3.4.188
149. Section A36.3.5 Microphone system88
150. Section A36.3.5.188
151. Section A36.3.5.288
152. Section A36.3.5.389
153. Section A36.3.5.489
154. Section A36.3.6 Recording and reproducing systems91
155. Section A36.3.6.191
156. Section A36.3.6.291
157. Section A36.3.6.391
158. Section A36.3.6.492
159. Section A36.3.6.592
160. Section A36.3.6.692
161. Section A36.3.6.792
162. Section A36.3.6.892
163. Section A36.3.6.992
164. Section A36.3.7 Analysis systems94
165. Section A36.3.7.194
166. Section A36.3.7.294
167. Section A36.3.7.394
168. Section A36.3.7.494
169. Section A36.3.7.595
170. Section A36.3.7.695
171. Section A36.3.7.795
172. Section A36.3.8 Calibration systems96
173. Section A36.3.8.196
174. Section A36.3.9 Calibration and checking of system96
175. Section A36.3.9.196
176. Section A36.3.9.296
177. Section A36.3.9.397
178. Section A36.3.9.497
179. Section A36.3.9.597
180. Section A36.3.9.697
181. Section A36.3.9.797
182. Section A36.3.9.897
183. Section A36.3.9.998
184. Section A36.3.9.1098
185. Section A36.3.10 Adjustments for ambient noise100
186. Section A36.3.10.1100
187. Section A36.3.10.2101
188. Section A36.4 Calculation of Effective Perceived Noise Level From Measured Data101
189. Section A36.4.1 General101
190. Section A36.4.1.1101
191. Section A36.4.1.2101
192. Section A36.4.1.3101
193. Section A36.4.2 Perceived noise level102
194. Section A36.4.2.1102
195. Section A36.4.3 Correction for spectral irregularities103
196. Section A36.4.3.1103
197. Section A36.4.3.2108
198. Section A36.4.4 Maximum tone-corrected perceived noise level109
199. Section A36.4.4.1109
200. Section A36.4.4.2110
201. Section A36.4.5 Duration correction110
202. Section A36.4.5.1110
203. Section A36.4.5.2111
204. Section A36.4.5.3111
205. Section A36.4.5.4111
206. Section A36.4.5.5112
207. Section A36.4.6 Effective perceived noise level112
208. Section A36.4.6112
209. Section A36.4.7 Mathematical formulation of noy tables113
210. Section A36.4.7.1113
211. Section A36.4.7.2113
212. Section A36.4.7.3 Calculate noy values using the following equations:113
213. Section A36.4.7.4113
214. Section A36.5. Reporting of Data to the FAA117
215. Section A36.5.1 General117
216. Section A36.5.1.1117
217. Section A36.5.1.2117
218. Section A36.5.1.3117
219. Section A36.5.2 Data reporting117
220. Section A36.5.2.1118
221. Section A36.5.2.2118
222. Section A36.5.2.3118
223. Section A36.5.2.4118
224. Section A36.5.2.5118
225. Section A36.5.3 Reporting of noise certification reference conditions119
226. Section A36.5.3.1119
227. Section A36.5.4 Validity of results119
228. Section A36.5.4.1120
229. Section A36.5.4.2120
230. Section A36.5.4.3120
231. Section A36.6 Nomenclature: Symbols and Units123
232. Section A36.7 Sound Attenuation in Air127
233. Section A36.7.1127
234. Section A36.7.2127
235. Section A36.7.3129
236. Section A36.8. [Reserved]130
237. Section A36.9. Adjustment of Airplane Flight Test Results130
238. Section A36.9.1130
239. Section A36.9.1.1131
240. Section A36.9.1.2133
241. Section A36.9.2 Flight profiles134
242. Section A36.9.2.1 Takeoff Profile134
243. Section A36.9.2.2 Approach Profile141
244. Section A36.9.3 Simplified method of adjustment145
245. Section A36.9.3.1 General145
246. Section A36.9.3.2 Adjustments to PNL and PNLT146
247. Section A36.9.3.2.1148
248. Section A36.9.3.2.1.1 PNLT Correction150
249. Section A36.9.3.2.1.2150
250. Section A36.9.3.2.2150
251. Section A36.9.3.3 Adjustments to duration correction151
252. Section A36.9.3.3.1151
253. Section A36.9.3.3.2151
254. Section A36.9.3.4 Source noise adjustments152
255. Section A36.9.3.4.1152
256. Section A36.9.3.4.2152
257. Section A36.9.3.5 Symmetry Adjustments152
258. Section A36.9.3.5.1152
259. Section A36.9.4 Integrated method of adjustment153
260. Section A36.9.4.1 General153
261. Section A36.9.4.2 PNLT computations154
262. Section A36.9.4.2.1157
263. Section A36.9.4.2.2158
264. Section A36.9.4.2.3158
265. Section A36.9.4.3 Duration correction158
266. Section A36.9.4.3.1158
267. Section A36.9.4.4 Source noise adjustment158
268. Section A36.9.4.4.1158
269. Section A36.9.5 Flight Path Identification Positions159
270. Section A36.9.6 Flight Path Distances159
271. - 289--RESERVED160
XIV. APPENDIX B TO part 36--NOISE LEVELS FOR TRANSPORT CATEGORY AND JET
AIRPLANES UNDER § 36.103161
290. Appendix B to Part 36-Noise Levels for Transport Category and Jet Airplanes Under § 36.103 161
291. Section B36.1 Noise Measurement and Evaluation161
292. Section B36.2 Noise Evaluation Metric161
293. Section B36.3 Reference Noise Measurement Points162
294. Section B36.4 Test noise measurement points162
295. Section B36.5 Maximum Noise Levels163
296. Section B36.6 Trade-Offs165
297. Section B36.7 Noise Certification Reference Procedures and Conditions166
298. Section B36.7(a) General conditions:166
299. Section B36.7(b) Takeoff reference procedure:167
300. Section B36.7(b)(1)167
301. Section B36.7(b)(2)168
302. Section B36.7(b)(3)168
303. Section B36.7(b)(4)169
304. Section B36.7(b)(5)169
305. Section B36.7(b)(6)170
306. Section B36.7(b)(7)170
307. Section B36.7(c) Approach reference procedure:171
308. Section B36.7(c)(1)171
309. Section B36.7(c)(2)171
310. Section B36.7(c)(3)171
311. Section B36.7(c)(4)172
312. Section B36.7(c)(5)173
313. Section B36.8 Noise Certification Test Procedures173
314. Section B36.8(a)173
315. Section B36.8(b)174
316. Section B36.8(c)174
317. Section B36.8(d)174
318. Section B36.8(e)175
319. Section B36.8(f)175
320. Section B36.8(g)175
321. - 349. [RESERVED]176
XV. 14 CFR PART 36 APPENDIX F. FLYOVER NOISE REQUIREMENTS FOR PROPELLER -
DRIVEN SMALL AIRPLANE AND PROPELLER-DRIVEN, COMMUTER CATEGORY
AIRPLANE CERTIFICATION TESTS PRIOR TO DECEMBER 22, 1988177
350. PART A - GENERAL177
351. Section F36.1 Scope [To be completed later.]177
352. PART B - NOISE MEASUREMENT177
353. Section F36.101 General Test Conditions [To be completed later.]177
354. Section F36.103 Acoustical Measurement System [To be completed later.]177
355. Section F36.105 Sensing, Recording, and Reproducing Equipment177
356. Section F36.107 Noise Measurement Procedures [To be completed later.]177
357. Section F36.109 Data Recording, Reporting, and Approval [To be completed later177
358. Section F36.111 Flight Procedures [To be completed later.]177
359. PART C - DATA CORRECTION177
360. Section F36.201 Correction of Data [To be completed later.]177
361. Section F36.203 Validity of Results [To be completed later.]177
362. PART D - NOISE LIMITS177
363. Section F36.301 Aircraft Noise Limits [To be completed later.]177
364. - 374. [RESERVED]177
XVI. 14 CFR PART 36 APPENDIX G. TAKE-OFF NOISE REQUIREMENTS FOR PROPELLER-
DRIVEN, SMALL AIRPLANE AND PROPELLER-DRIVEN, COMMUTER CATEGORY
AIRPLANE CERTIFICATION TESTS ON OR AFTER DECEMBER 22, 1988178
375. PART A - GENERAL178
376. Section G36.1 Scope178
377. PART B - NOISE MEASUREMENT178
378. Section G36.101 General test conditions178
379. Section G36.101(b)179
380. Section G36.101(c)181
381. Section G36.101(d)182
382. Section G36.103 Acoustical measurement system182
383. Section G36.103(b) & (c)182
384. Section G36.103(d)183
385. Section G36.105(a)184
386. Section G36.105(b)&(c)184
387. Section G36.105(d)185
388. Section G36.105(e)186
389. Section G36.105(f)187
390. Section G36.105(g)187
391. Section G36.107 Noise measurement188
392. Section G36.107(b)190
393. Section G36.107(c)191
394. Section G36.109 Data Recording, Reporting and Approval192
395. Section G36.109(b)193
396. Section G36.109(c) & (d)193
397. Section G36.109(e)194
398. Section G36.109(f)194
399. Section G36.109(g)194
400. Section G36.111 Flight procedures195
401. Section G36.111(b)196
402. Section G36.111(c)196
403. Section G36.111(c)(1)197
404. Section G36.111(c)(2)198
405. PART C - DATA CORRECTION199
406. [RESERVED]199
407. Section G36.201 Correction of Data199
408. Section G36.201(b)200
409. Section G36.201(c)201
410. Section G36.201(d)201
411. Section G36.201(d)(1)202
412. Section G36.201(d)(2)203
413. Section G36.201(d)(3)204
414. Section G36.201(d)(4)206
415. Section G36.203 Validity of Results208
416. PART D - NOISE LIMITS209
417. Section G36.301 Aircraft Noise Limits209
418. −429. [RESERVED]210
XVII. 14 CFR PART 36 APPENDIX H- NOISE REQUIREMENTS FOR HELICOPTERS UNDER SUB-
PART H [To be completed later]211
XVIII. 14 CFR PART 36 APPENDIX J- ALTERNATIVE NOISE CERTIFICATION PROCEDURE FOR
HELICOPTERS UNDER SUBPART H HAVING A MAXIMUM CERTIFICATED TAKE-OFF
WEIGHT OF NOT MORE THAN 6,000 POUNDS [To be completed later]211
APPENDICES
APPENDIX 1 – ICAO Committee on Aviation Environmental Protection - Environmental Technical Manual On The Use Of Procedures In The Noise Certification Of Aircraft, Steering Group Approved Revision 7 APPENDIX 2 – VNTSC Certification Validation Package APPENDIX 3 – Guidelines for Correction of Aircraft Noise Levels for the Effects of Background Noise APPENDIX 4 – Equivalent Procedures and Demonstrating "No Acoustical Change” for Propeller-Driven Small Airplanes and Commuter Category Airplanes
FIGURES
FIGURE 1 Document Format FIGURE 2 Noise Time History with Thrust (Power) Reduction FIGURE 3 Normal Full Thrust (Power) Take-Off FIGURE 4 Flight Path Intercept Take-off FIGURE 5 Take-off Flight Path FIGURE 6 Approach With Full Landing FIGURE 7 Flight Path Intercept Approach FIGURE 8 Approach Flight Path Deviations FIGURE 9-12 RESERVED FIGURE 13 Configuration for 1/2 in. Inverted Microphone Over Plate FIGURE 14 Graphic Representation of Adjusted Measurement Location FIGURE 15 Typical Test and Reference Flight Paths FIGURE 16 Obstruction Free Noise Measurement Cone (Flyover Case Illustrated) FIGURE 17 Temperature/Relative Humidity Test Window
(Note: The figures identified in the above list were developed for AC 36-4C. Figures contained within part 36 itself have not been included in this list.)
TABLES
TABLE 1 Example - Atmospheric Measurements TABLE 2 Example - Atmospheric Measurements TABLE 3 Example – Atmospheric Sound Attenuation Coefficients TABLE 4 Example – Effective Layer Depth TABLE 5 Rate of Atmospheric Absorption (α) at 500 Hz Frequency TABLE 6 Student’s t Distribution For 90 Percent Confidence Interval
(Note: The tables identified in the above list were developed for AC 36-4C. Tables contained within part 36 itself have not been included in this list.)
8. PART 21 - GENERAL
As part of the overall aircraft certification requirements identified in part 21, applicants must comply with the noise certification requirements of part 36. An applicant for a type certificate must show that the aircraft meets the applicable requirements of part 36 (part 21, section 21.17). In addition, an applicant is entitled to a type certificate for an aircraft if the applicant submits the type design, test reports, and computations necessary to show that the product to be certificated meets the applicable airworthiness and aircraft noise requirements (part 21, sections
21.21 & 21.25). Similar requirements are imposed for aircraft manufactured in a foreign country for import into the United States (part 21, section 21.29). Refer to the part 21 regulations for specific regulatory language.
a. Explanation
None
b. Supplemental Information
(1) Airworthiness Certification: All aircraft requiring noise certification by the FAA are required to meet the applicable airworthiness requirements of part 21, which identifies the specific airworthiness standards for each aircraft type and product, such as:
i. Part 23 for normal, utility, acrobatic, and commuter category airplanes,
ii. Part 25 for transport category airplanes,
iii. Part 27 for normal category rotorcraft,
iv. Part 29 for transport category rotorcraft,
v. Part 33 for aircraft engines,
vi. Part 35 for propellers,
vii. Primary category aircraft, and
viii. JAR-VLA aircraft.
(2) Changes in Type Design. Part 21 section 21.93(b) requires compliance with the appropriate part 36 “acoustical change” requirements for a voluntary type design change of an aircraft that may increase the noise levels of that aircraft, regardless of whether the change in type design is classified as a minor or major change in part 21, section 21.93(a). See paragraph 16 of this AC for further discussion of acoustical change.
9.-11. [RESERVED]
I. CERTIFICATION PROCEDURES FOR PRODUCT AND PARTS 14 CFR PART 21
12. PART 36 – SUBPART A-GENERAL
a. Explanation
This Subpart specifies the Applicability of part 36, Definitions of Terms Unique to part 36, part 36 Requirements as of the Date of Type Certificate Application, Airworthiness Compatibility requirements, Limitations, Information on References, and Acoustical Change Requirements.
b. Supplemental Information
None
c. Procedures
None
13. Section 36.1 Applicability and definitions
14. Section 36.1(a)
This part prescribes noise standards for the issue of the following certificates:
(1) Type certificates, and changes to those certificates, and standard airworthiness certificates, for subsonic transport category large airplanes and for subsonic jet airplanes regardless of category.
(2) Type certificates and changes to those certificates, standard airworthiness certificates, and restricted category airworthiness certificates, for propeller-driven, small airplanes, and for propellerdriven, commuter category airplanes except those airplanes that are designed for "agricultural aircraft operations" (as defined in § 137.3 of this chapter, as effective on January 1, 1966) or for dispersing fire fighting materials to which § 36.1583 of this part does not apply.
(3) A type certificate and changes to that certificate, and standard airworthiness certificates, for Concorde airplanes.
(4) Type certificates, and changes to those certificates, for helicopters except those helicopters that are designated exclusively for "agricultural aircraft operations" (as defined in § 137.3 of this chapter, as effective on January 1, 1966), for dispensing fire fighting materials, or for carrying external loads (as defined in § 133.1(b) of this chapter, as effective on December 20, 1976).
a. Explanation
This section specifies aircraft types and categories to which part 36 requirements are applicable as a condition for issuance of type certificates (TC), changes to type certificates, supplemental type certificates (STC), amended type certificates and airworthiness certificates.
b. Supplemental Information
(1) Applicable Requirements: Unless otherwise specified, the date to be used for determining the applicability of the appropriate part 36 standards for an aircraft type design is the date on which application for a type certificate was made. An application for type certification is effective for the time periods specified in section
21.17(c) of part 21.
(2) Noise Related Type Certification Requirements: See paragraph 6-3(h) of reference 7 of this AC.
II. NOISE STANDARDS: AIRCRAFT TYPE AND AIRWORTHINESS CERTIFICATION 14 CFR PART 36
(3) Supplemental Type Certificates: See paragraph 6-3(j) of reference 7 of this AC.
(4) Definitions of Terms: Paragraph 4 of this Advisory Circular provides definitions for the following terms related to the aircraft types and categories within Items (1) – (4) of section 36.1(a).
Aircraft Large Aircraft Airplane Small Aircraft Helicopter Propeller Airplane Categories (See Note A) Jet Airplane
- Acrobatic Turboprop Airplane (See Note C)
- Commuter
- Normal
- Primary
- Restricted (See Note B)
- Transport
- Utility Helicopter Categories
- Normal
- Transport
Notes:
(A) Airplane Categories and Aircraft Classes: Part 1 recognizes a distinction between Airplane Categories (e.g., acrobatic, commuter, normal, primary, restricted, transport and utility) and Aircraft Classes (e.g., Conventional Takeoff and Landing (CTOL), Vertical Takeoff and Landing (VTOL), Short Takeoff and Landing (STOL), Reduced Takeoff and Landing (RTOL), and Supersonic Transports (SST)). The noise certification requirements contained in part 36 are specified for several Airplane and Helicopter Categories but not for STOL, RTOL, SST (except for Concorde), or VTOL Aircraft Classes.
(B) Restricted Category Propeller-Driven Large Airplanes: Propeller-driven large airplanes that have been type certificated in the restricted category (See part 21, section 21.25) are not required to demonstrate compliance with the requirements of part 36. In the absence of part 36 applicability, an Environmental Assessment is required (See FAA Order 8110.B (reference 7 of this AC) paragraph 6-3(d) for additional information).
(C) Turboprop Airplanes: Turboprop-powered airplanes are included under the part 36 requirements applicable to propeller-driven airplanes (i.e. subsonic transport category large airplanes; propellerdriven small airplanes, including acrobatic, normal, restricted, and transport categories; or propeller-driven commuter category airplanes).
c. Procedures
None
15. Section 36.1(b)
Each person who applies under part 21 of this chapter for a type of airworthiness certificate specified in this part must show compliance with the applicable requirements of this part, in addition to the applicable airworthiness requirements of this chapter.
a. Explanation
This section specifies that an applicant must comply with appropriate airworthiness requirements and part 36 requirements as a part of the total aircraft certification process.