曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

Number of Seats:
The maximum number of passengers approved for emergency evacuation is: 375 passengers with a 3 pair Type A and 1 pair Type 1 exit
configuration, and 379 passengers with a 4 pair Type A exit configuration.
A46NM Revision 10 9 March 19, 2007
Maximum Baggage:
Cargo Compartment Maximum Load
(kg / lb)
Forward 22,861 / 50,408
Aft 18,507 / 40,808
Rear 3,468 / 7,647
For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weight) see
Weight and Balance Manual Ref. 00G080A0006/C3S for A330-300 airplanes.
Fuel Capacity:
Two Tank Airplane
Usable Fuel Unusable fuel
Model A330-301/-321/-322/-341/-342 A330-323/-343 All Models
Tank
Liters
(kg)
Gallons
(lb)
liters
(kg)
gallons
(lb)
liters
(kg)
gallons
(lb)
Wing 91,764
(73,411)
24,244
(161,871)
91,300
(73,040)
24,122
(161,053)
348
(279)
92
(615)
Trim
Tank
6,121
(4,897)
1,617
(10,798)
6,230
(4,984)
1,646
(10,990)
6
(5)
1.6
(11)
Total 97,885
(78,308)
25,861
(172,669)
97,530
(78,024)
25,768
(172,043)
354
(284)
94
(626)
Maximum Operating Altitude:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Control Surface Movements: (Total one-way travel in each direction of each movable control surface on the aircraft.)
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Manufacturer’s Serial Numbers:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Import Requirements:
See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes.
Certification Basis (A330-300):
a. Part 25 of the FAR effective February 1, 1965, including the following:
• Amendments 25-1 through 25-63, amendments 25-65, 25-66, 25-77
b. Part 25 of the FAR amendment 25-64 with the following exceptions:
• Cockpit seats will not meet FAR 25.562 amendment 25-64 but will meet FAR 25.561
• Compliance with 25.785(a), (b), and (c) at amendment 25-64 for front row seats in front of a bulkhead will be
based on ensuring a 35 inch free head strike envelope.
c. Special conditions in accordance with § 21.16 of the FAR.
1. Special conditions published in the Federal Register on April 15, 1993, (ref. Docket No. NM-75, Special Conditions
No. 25-ANM-69):
(1) Operation without Normal Electrical Power
(2) Electronic Flight Control System (EFCS) failures and Mode Annunciation
(3) Command Signal Integrity
(4) Protection From Lightning and Unwanted Effects of High Intensity Radiated Fields (HIRF)
(5) Interaction of Systems and Structures
(6) Design Dive Speed
(7) Design Maneuver Requirements
(8) Limit Pilot Forces
(9) Tail plane Tank Emergency Landing Loads
A46NM Revision 10 10 March 19, 2007
(10) Limit Engine Torque
(11) Flight Characteristics
(12) Flight Envelope Protection
(13) Side Stick Controllers
(14) Computerized Airplane Flight Manual (AFM) Performance Information
2. Special condition for the optional installation of the Lower Deck Mobile Crew Rest Compartment:
(published in the Federal Register on January 6, 2005, Docket No. NM287, Special Condition No. 25-281-SC)
Lower Deck Mobile Crew Rest (LD-MCR) Compartment (optional installation)
d. Special Federal Aviation regulation FAR Part 34, effective September 10, 1990.
e. Part 36 of the FAR as amended by amendments 36-1 through 36-20.
f. The technical requirements are complemented by the following guidance material:
For precision approach and landing,
1. AC 120-29
2. AC 120-28C
and for the automatic flight control system
1. AC 20-57A for automatic landing
2. AC 25.1329-1A for cruise
g. Equivalent safety findings have been made in accordance with FAR 21.21(b)(1) for the following paragraphs of the FAR:
(1) 25.335(d) for design airspeeds
(2) 25.345 for high lift devices
(3) 25.349 for control surface loads
(4) 25.351(b) for unsymmetrical loads
(5) 25.371 for gyroscopic loads
(6) 25.373 for speed control devices
(7) 25.101(I); 25.105(c)(1); 25.109(a)(b)(c)(d)(e)(f); 25.113(a)(b)(c); 25.115(a); 25.735(f)(g)(h)(b) for rejected
takeoff and landing performance
(8) 25.933(a)(1)(ii), 25.1309(b)(1) for flight critical thrust reverser
(9) 25.1203(d) for turbine overheat detection (RR Trent 700 powered A330-341, -342, -343 only)
(10) 25.1305(c)(6) Warning means for engine fuel filter contamination (RR Trent 700 powered A330-341, -342 and
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：航空資料2(140)