曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
§ 25.562(b)(2) Pre-amendment 25-64 Allowance for compliance to pre-amdt 25-
64 only applies to crew seat floor warpage
test requirements
§ 25.365(g) Amendment 25-54 Allowance for compliance to amdt 25-54
applies only to design of the cockpit wall
§§ 25.831(g), 25.831(a),
25.841(a)
§§ 25.831(g) and 25.831(a) at amendment
25-41
§ 25.841(a) at amendment 25-38.
b. 14 CFR Part 36, effective December 1, 1969, as amended by amendments 36-1 through 36-23.
c. 14 CFR Part 34, effective September 10, 1990, including all amendments effective on the TC date.
d. Special conditions in accordance with 14 CFR 21.16.
(i) Basic A340 Special Conditions also applicable to the A340-500 and A340-600:
Note 1: Refer to TCDS section III certification basis for the A340-200 and A340-300
Note 2: Special conditions issued for the A340 in accordance with Section 21.16 of the FAR and
published in the Federal Register Special Vol. 58, No. 71, dated April 15, 1993
(1) Electronic Flight Control System (EFCS) failures and Mode Annunciation
(2) Command Signal Integrity
(3)(a) Protection From Lightning and Unwanted Effects of High Intensity Radiated Fields (HIRF)
(5) Design Dive Speed
(6) Design Maneuver Requirements
(7) Limit Pilot Forces
(11)(a) Flight Characteristics Characteristic - Compliance Determination By handling Qualities rating
System for EFCS Failure Cases
(11)(c) Flight Characteristic – Lateral Directional Stability
(12)(a) Flight Envelope Protection – General Limiting Requirements
(12)(c) Flight Envelope Protection – Normal Load Factor g Limiting
(12)(d) Flight Envelope Protection – High Speed Limiting (12) Flight Envelope Protection
(12)(e) Pitch and Roll Limiting
(13) Side Stick Controllers
A43NM, Revision 4 Page 15 of 18 March 19, 2007
(ii) Special Conditions applicable to the A340-500 and A340-600:
Docket No. NM211; Special Conditions No. 25-200-SC, “Airbus, Model A340-500 and A340-600
Airplanes; Ground Loads and Conditions for Center Landing Gear with four Wheels and Braking
Capability,” Federal Register Vol. 67 No. 98, May 21, 2002.
Docket No. NM213; Special Conditions No. 25-201-SC, “Airbus, Model A340-500 and A340-600
Airplanes; Interaction of Systems and Structure…”, Federal Register Vol. 67 No. 126, July 1, 2002.
Docket No. NM213; Special Conditions No. 25-201-SC, “Airbus, Model A340-500 and A340-600
Airplanes; “…Electronic Flight Control System: Longitudinal Stability and Low Energy Awareness…”
Federal Register Vol. 67 No. 126, July 1, 2002.
Docket No. NM213; Special Conditions No. 25-201-SC, “Airbus, Model A340-500 and A340-600
Airplanes; “…Use of High Incidence Protection and Alpha Floor Systems”, Federal Register Vol. 67
No. 126, July 1, 2002.
Docket No. NM212; Special Conditions No. 25-02-04-SC, “Airbus, Model A340-500 and A340-600
Airplanes; Sudden Engine Stoppage,” Federal Register Vol. 67 No. 81, April 26, 2002.
e. Equivalent safety findings have been made in accordance with FAR 21.21(b)(1) for the following FAR paragraphs:
§ 25.621(c) Casting factors. The ESF is only applicable to the Inner Flap – Flap Rib Fitting of the A340-
500 and –600. For all other castings on the aircraft, as defined by the certification basis, the requirements
of § 25.621(c) amendment 25-0 apply
§§ 25.473, 25.723: Landing Gear Drop Tests
§§ 25.341(a)(5),(b),(c), 25.345(c)(2), 25.371, 25.373(a), 25.1517: Continuous Turbulence Loads
§ 25.331(c)(2): Checked Maneuver Loads
§ 25.107(e)(1)(iv): Reduced Margins between VMU and VLOF for Geometry Limited Airplanes
§§ FAR 25 (All FAR 25 sections, except structural, dealing with stall speeds and related factors): Use of
1-g Stall Speeds Instead of Minimum Speed in the Stall as a Basis for Determining Compliance
§ 25.831(a): Airplane Operation with Air Conditioning Packs Off During Takeoff
§§ 25.933(a)(1), 25.1585(a)(9): Flight Critical Thrust Reverser
§ 25.963(d) first sentence: Fuel Tank Loads. The ESF is to the first sentence of § 25.963(d); “Fuel tanks
within the fuselage contour must be able to resist rupture and to retain fuel, under the inertia forces
prescribed for emergency landing conditions in § 25.561.”
§ 25.1203(d): Rolls-Royce Trent 500 Turbine Overheat Detection
§§ 25.1305, 251501(b): Auxiliary Power Unit (APU) Instrumentation and Monitoring Requirements
§ 25.1305(c)(6), Warning Means for Engine Fuel Filter Contamination
f. Optional Design Regulations
(a) §25.801: Ditching Provisions
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
航空资料2(132)
