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Circular Advisory PDF

459 Pages·2005·3.34 MB·English
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Advisory U.S. Department of Transportation C i r c u l a r Federal Aviation Administration AC 25-7A DATE: 3/31/98 FLIGHT TEST GUIDE FOR CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES Subject: FLIGHT TEST GUIDE FOR Date: 6/3/99 AC No: 25-7A CERTIFICATION OF TRANSPORT Initiated By: ANM-110 Change: 1 CATEGORY AIRPLANES 1. PURPOSE. This change provides updated guidance material to ensure consistent application of certain airworthiness requirements adopted by recent amendments to 14 CFR part 25. Changed material is indicated in the margins by asterisks and at the top of each changed page with the change number and date. New material on pages 80-1 through 80-28 is indicated by the change number and date only. Some text, although not changed, has been rearranged to accommodate new material. 2. PRINCIPAL CHANGES. a. New guidance regarding an acceptable means of compliance with the wet runway and worn brake requirements adopted by Amendment 25-92, “Improved Standards for Determining Rejected Takeoff and Landing Performance.” b. Additional guidance regarding criteria for locating the gate when the airplane has multiple go-around configurations, for compliance with the gate design requirements adopted by Amendment 25-98, “Revision of Gate Requirements for High-Lift Device Controls.” PAGE CONTROL CHART Remove Pages Dated Insert Pages Dated iii thru x 3/31/98 iii thru x 6/3/99 71 thru 105 3/31/98 71 thru 106 6/3/99 129 thru 148 3/31/98 129 thru 149 6/3/99 283 thru 300 3/31/98 283 thru 301 6/3/99 /s/ John J. Hickey Acting Manager, Transport Airplane Directorate Aircraft Certification Service Subject: FLIGHT TEST GUIDE FOR Date: 3/31/98 AC No: 25-7A CERTIFICATION OF TRANSPORT Initiated By: ANM-110 Change: CATEGORY AIRPLANES 1. PURPOSE. This revised advisory circular (AC) provides updated guidance for the flight test evaluation of transport category airplanes. These guidelines provide an acceptable means of demonstrating compliance with the pertinent regulations of 14 CFR part 25. The methods and procedures described herein have evolved through many years of flight testing of transport category airplanes and, as such, represent current certification practice. Like all AC material, these guidelines are not mandatory and do not constitute regulations. They are derived from previous FAA experience in finding compliance with the airworthiness requirements and represent methods and procedures found to be acceptable by that experience. Although mandatory terms such as “shall” and “must” are used in this AC, because the AC method of compliance is not in itself mandatory, these terms apply only to applicants who seek to demonstrate compliance by use of the specific methods described in this AC. 2. CANCELLATION. AC 25-7, “Flight Test Guide for Certification of Transport Category Airplanes,” dated April 9, 1986. 3. BACKGROUND. Since AC 25-7 was released on April 9, 1986, it has been the primary source of guidance for flight test methods and procedures to show compliance with the regulations contained in subpart B of part 25, which are related to airplane performance and handling characteristics. For certification flight testing to show compliance with other part 25 regulations, Order 8110.8, “Engineering Flight Test Guide for Transport Category Airplanes,” provided guidance for internal FAA use in determining acceptable means of compliance. Order 8110.8, as revised on September 26, 1974, has been subject to five change updates to reflect significant policy changes; the last change being the removal of the subpart B-related material concurrent with the original release of AC 25-7. Order 8110.8 reflected the policy in place when Amendment 25-29 to part 25 was adopted, and the original release of AC 25-7 reflected an Amendment 25-59 time frame. Part 25 has been amended significantly since the two referenced documents were last revised and, likewise, guidance and policy have changed in many areas as experience has been gained. During this time period, many advances in technology have also taken place that require new or modified test techniques. This revision updates the original AC to incorporate the latest policy and guidance material applicable to all sections of part 25. The material related to regulations outside of subpart B supersedes that contained in Order 8110.8, which has been cancelled accordingly upon issuance of this AC. AC 25-7A 3/31/98 4. APPLICABILITY. These methods and procedures are promulgated, in the interest of standardization, for use during all transport category airplane flight test certification activities. This material is not to be construed as having any legal status and must be treated accordingly. The procedures set forth herein are one acceptable means of compliance with applicable sections of part 25. Any alternate means proposed by the applicant should be given due consideration. Applicants are encouraged to use their technical ingenuity and resourcefulness in order to develop more efficient and less costly methods of achieving the objectives of Part 25. Since these methods and procedures are only one acceptable means of compliance, individuals should be guided by the intent of the methods provided in this AC. As deviations from the methods and procedures described in this AC may occur, FAA certification personnel will coordinate what they consider to be major deviations with the Transport Standards Staff (ANM-110) of the Transport Airplane Directorate. If in their judgment, however, a deviation is considered to be minor, coordination with ANM-110 may not be necessary. 5. RELATED PUBLICATIONS. Certification personnel should be familiar with FAA Order 8110.4A, “Type Certification Process,” and FAA Order 8100.5, “Aircraft Certification Directorate Procedures.” In this AC, reference is made to other FAA advisory circulars that provide guidance on various aspects of type certification and supplemental type certification. /s/ Ronald T. Wojnar Manager, Transport Airplane Directorate Aircraft Certification Service ii 6/3/99 AC 25-7A Chg. 1 CONTENTS Paragraph Page No. CHAPTER 1. GENERAL 1. FAR 25.1 Applicability [RESERVED] 1 2. FAR 25.2 Special Retroactive Requirements [RESERVED] 1 CHAPTER 2. FLIGHT Section 1. GENERAL 3. FAR 25.21 Proof of Compliance.................................................................31 Figure 3-1 Weight Tolerance Limits..........................................................33 Figure 3-2 Equivalent Weight Extrapolation..............................................34 Figure 3-3 Test Parameters That Normally Can Be Corrected...................35 Figure 3-4 Wind Profile Variation..............................................................36 4. FAR 25.23 Load Distribution Limits [RESERVED]..................................42 5. FAR 25.25 Weight Limits [RESERVED]...................................................42 FAR 25.27 Center of Gravity Limits [RESERVED]...................................42 6. FAR 25.29 Empty Weight and Corresponding Center of Gravity [RESERVED]..........................................................42 7. FAR 25.31 Removable Ballast [RESERVED]............................................42 8. FAR 25.33 Propeller Speed and Pitch Limits..............................................43 Section 2. PERFORMANCE 9. FAR 25.101 General......................................................................................71 FAR 25.103 Stalling Speed (see paragraph 29) 10. FAR 25.105 Takeoff......................................................................................71 FAR 25.107 Takeoff Speeds..........................................................................71 11. FAR 25.109 Accelerate-Stop Distance..........................................................80 Figure 11-1 Accelerate-Stop Time Delays...............................................80-7 Figure 11-2 Accelerate-Stop Speed Vs. Distance.....................................80-9 Figure 11-3 Anti-Skid System Response Characteristics (On-Off System).................................................................80-13 Figure 11-4 Anti-Skid System Response Characteristics (Quasi-Modulating System)................................................80-15 Figure 11-5 Anti-Skid System Response Characteristics (Fully Modulating System).................................................80-17 Figure 11-6 Instantaneous Brake Force and Peak Brake Force..............80-21 Figure 11-7 Anti-Skid Efficiency-Wheel Slip Relationship...................80-23 Figure 11-8 Substantiation of the Optimal Slip Value...........................80-24 iii AC 25-7A 6/3/99 Chg. 1 12. FAR 25.111 Takeoff Path..............................................................................81 13. FAR 25.113 Takeoff Distance and Takeoff Run...........................................88 Figure 13-1 Takeoff Distance on a Dry Runway..........................................89 Figure 13-2 Takeoff Distance (All Engines Operating)...............................89 Figure 13-3 Takeoff Distance on a Wet Runway.........................................90 Figure 13-4 Takeoff Run (Critical Engine Fails at V )...............................91 EF Figure 13-5 Takeoff Run (All Engines Operating).......................................91 Figure 13-6 Clearway Profiles......................................................................92 14. FAR 25.115 Takeoff Flight Path...................................................................92 Figure 14-1 Takeoff Segments & Nomenclature..........................................93 Figure 14-2 Net Takeoff Flight Path.............................................................94 15. FAR 25.117 Climb: General..94 16. FAR 25.119 Landing Climb: All-Engines Operating....................................95 17. FAR 25.121 Climb: One-Engine-Inoperative................................................96 18. FAR 25.123 En route Flight Paths.................................................................97 19. FAR 25.125 Landing.....................................................................................98 Figure 19-1 Landing Time Delays..............................................................103 Section 3. CONTROLLABILITY AND MANEUVERABILITY 20. FAR 25.143 General....................................................................................121 Figure 20-1 Sample Pitch Tracking Task...................................................129 Figure 20-2 A-PC Rating Criteria & Comparison to MIL Standard..........130 Figure 20-3 Example of Minimum Permitted HQ Rating for A-PC Tendencies..............................................................................131 21. FAR 25.145 Longitudinal Control...............................................................135 22. FAR 25.147 Directional and Lateral Control..............................................140 23. FAR 25.149 Minimum Control Speed........................................................143 Section 4. TRIM 24. FAR 25.161 Trim [RESERVED]................................................................157 Section 5. STABILITY 25. FAR 25.171 General [RESERVED]............................................................171 26. FAR 25.173 Static Longitudinal Stability...................................................171 FAR 25.175 Demonstration of Static Longitudinal Stability......................171 Figure 26-1 Longitudinal Static Stability...................................................173 27. FAR 25.177 Static Directional and Lateral Stability...................................173 28. FAR 25.181 Dynamic Stability....................................................................175 iv 6/3/99 AC 25-7A Chg. 1 Section 6. STALLS 29. Stall Testing............................................................................189 FAR 25.201 Stall Demonstration................................................................189 FAR 25.203 Stall Characteristics................................................................194 FAR 25.207 Stall Warning..........................................................................197 Figure 29-1 Stall Test Time History...........................................................199 Figure 29-2 Stall C vs. Entry Rate.........................................................200 LCG Figure 29-3 Stall C vs. Weight and Flap Setting......................................200 L Figure 29-4 Stall Speeds vs. Weight and Flap Setting...............................201 Figure 29-5 Thrust Effect on Stall C .........................................................201 L Section 7. GROUND AND WATER HANDLING CHARACTERISTICS 30. General....................................................................................211 FAR 25.231 Longitudinal Stability and Control.........................................211 FAR 25.233 Directional Stability and Control............................................211 FAR 25.235 Taxiing Condition [RESERVED]...........................................212 FAR 25.237 Wind Velocities......................................................................212 FAR 25.239 Spray Characteristics, Control, and Stability on Water..........213 Section 8. MISCELLANEOUS FLIGHT REQUIREMENTS 31. FAR 25.251 Vibration and Buffeting..........................................................221 Figure 31-1 Maneuvering Characteristics...................................................224 (Speeds up to the Lesser of V or M or Buffet Onset) FC FC Figure 31-2 Maneuvering Characteristics...................................................225 (Speeds between Figure 31-1 and V or M ) DF DF 32. FAR 25.253 High Speed Characteristics.....................................................225 33. FAR 25.255 Out-of-Trim Characteristics....................................................229 Figure 33-1 Mistrimmed Maneuvering Characteristics..............................231 CHAPTER 3. STRUCTURE [RESERVED] CHAPTER 4. DESIGN AND CONSTRUCTION Section 1. GENERAL [RESERVED] Section 2. CONTROL SURFACES [RESERVED] v AC 25-7A 6/3/99 Chg. 1 Section 3. CONTROL SYSTEMS 34. FAR 25.671 General....................................................................................261 [35-45] [RESERVED].........................................................................261 46. FAR 25.701 Flap and Slat Interconnections................................................261 47. FAR 25.703 Takeoff Warning System [RESERVED]................................262 Section 4. LANDING GEAR [48-51] [RESERVED].........................................................................283 52. FAR 25.729 Retracting Mechanisms...........................................................283 53. FAR 25.731 Wheels ....................................................................................284 54. FAR 25.733 Tires [RESERVED]................................................................286 55. FAR 25.735 Brakes.....................................................................................286 56. FAR 25.737 Skis [RESERVED].................................................................301 Section 5. FLOATS AND HULLS [57-59] [RESERVED].........................................................................311 Section 6. PERSONNEL AND CARGO ACCOMMODATIONS [60-61] [RESERVED].........................................................................323 62. FAR 25.773 Pilot Compartment View........................................................323 [63-72] [RESERVED].........................................................................323 Section 7. EMERGENCY PROVISIONS 73. FAR 25.801 Ditching [RESERVED]..........................................................333 74. FAR 25.803 Emergency Evacuation............................................................333 [75-83] [RESERVED].........................................................................333 Section 8. VENTILATION AND HEATING 84. FAR 25.831 Ventilation...............................................................................343 85. FAR 25.832 Cabin Ozone Concentration [RESERVED]...........................343 86. FAR 25.833 Combustion Heating Systems [RESERVED].........................343 Section 9. PRESSURIZATION 87. FAR 25.841 Pressurized Cabins..................................................................353 88. FAR 25.843 Tests for Pressurized Cabins...................................................355 vi 6/3/99 AC 25-7A Chg. 1 Section 10. FIRE PROTECTION [RESERVED] Section 11. MISCELLANEOUS [RESERVED] CHAPTER 5. POWERPLANT Section 1. GENERAL 89. FAR 25.901 Installation [RESERVED]......................................................387 90. FAR 25.903 Engines....................................................................................387 FAR 25.903(b) Engine Isolation......................................................................387 FAR 25.903(c) Control of Engine Rotation.....................................................387 FAR 25.903(d) Turbine Engine Installations...................................................388 FAR 25.903(e) Engine Restart Capability.......................................................389 91. FAR 25.904 Automatic Takeoff Thrust Control Systems (ATTCS)...........390 92. FAR 25.905 Propellers................................................................................392 93. FAR 25.907 Propeller Vibration [RESERVED].........................................392 94. FAR 25.925 Propeller Clearance [RESERVED].........................................392 95. FAR 25.929 Propeller Deicing....................................................................392 96. FAR 25.933 Reversing Systems..................................................................393 97. FAR 25.934 Turbojet Engine Thrust Reverser Sys. Tests [RESERVED]..396 98. FAR 25.937 Turbopropeller-Drag Limiting Systems..................................396 99. FAR 25.939 Turbine Engine Operating Characteristics..............................398 100. FAR 25.941 Inlet, Engine, and Exhaust Capability (RESERVED..............398 101. FAR 25.943 Negative Acceleration.............................................................399 102. FAR 25.945 Thrust or Power Augmentation System [RESERVED]..........399 Section 2. FUEL SYSTEM [103-108] [RESERVED].........................................................................419 109. FAR 25.959 Unusable Fuel Supply.............................................................419 110. FAR 25.961 Fuel System Hot Weather Operation......................................421 [111-116] [RESERVED].........................................................................423 117. FAR 25.975 Fuel Tank Vents and Carburetor Vapor Vents........................423 [118-120] [RESERVED].........................................................................424 Section 3. FUEL SYSTEM COMPONENTS [121-126] [RESERVED].........................................................................445 127. FAR 25.1001 Fuel Jettisoning System..........................................................445 Section 4. OIL SYSTEM [RESERVED] vii AC 25-7A 6/3/99 Chg. 1 Section 5. COOLING [128-130] [RESERVED].........................................................................481 Section 6. INDUCTION SYSTEM 131. FAR 25.1091 Air Induction...........................................................................497 132. FAR 25.1093 Induction System Icing Protection..........................................499 [133-136] [RESERVED].........................................................................501 Section 7. EXHAUST SYSTEM 137. FAR 25.1121 General....................................................................................511 [138-140] [RESERVED] Section 8. POWERPLANT CONTROLS AND ACCESSORIES [141-154] [RESERVED].........................................................................521 Section 9. POWERPLANT FIRE PROTECTION [155-158] [RESERVED].........................................................................537 159. FAR 25.1187 Drainage and Ventilation of Fire Zones..................................537 [160-164] [RESERVED].........................................................................537 165. FAR 25.1197 Fire Extinguishing Agents......................................................537 [166-169] [RESERVED].........................................................................538 CHAPTER 6. EQUIPMENT Section 1. GENERAL 170. FAR 25.1301 Function and Installation.........................................................559 171. FAR 25.1303 Flight and Navigation Instruments..........................................592 172. FAR 25.1305 Powerplant Instruments [RESERVED]..................................594 173. FAR 25.1307 Miscellaneous Equipment [RESERVED]..............................594 174. FAR 25.1309 Equipment, Systems, and Installations...................................594 Section 2. INSTRUMENTS: INSTALLATION 175. FAR 25.1321 Arrangement and Visibility [RESERVED]............................605 176. FAR 25.1322 Warning, Caution, and Advisory Lights [RESERVED].........605 177. FAR 25.1323 Airspeed Indicating System....................................................605 178. FAR 25.1325 Static Pressure Systems...........................................................608 179. FAR 25.1326 Pitot Heat Indicator Systems [RESERVED]..........................609 180. FAR 25.1327 Magnetic Direction Indicator [RESERVED]..........................609 viii

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ADQ. ADQ. CON. SAT = Satisfactory ADQ = Adequate CON = Controllable. NFE = Normal flight envelope LFE = Limit flight envelope n airflow angle of attack on the horizontal tail, ice shapes will lso be required on the wing surface, and should be representative of the ice accumulation that ou n rma y
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