曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

procedures and limits.
Permission is given to distribute or copy these notes under the following conditions:
 Nothing may be charged for the notes
 No changes may be made without express consent of the author
 Authors copyright must be included
Trust in the LORD with all thine heart; and lean not unto thine
own understanding. In all thy ways acknowledge him, and he
shall direct thy paths. Proverbs 3:5,6
US Airways Airbus A319, A320, A321 Notes
5
Limits
(memory items in bold italics, U stands for US Airways imposed limit)
Weight Limits (PH 1.2.3)
(in lbs.) A319 A320-231 A320-214&232 A321
Max Ramp: 167,329 167,329 170,635 205,909
Max Takeoff: 166,447 166,447 169,754 205,027
Max Landing: 137,787 142,198 142,198 171,517
Max Zero Fuel: 128,969 134,480 134,480 162,699
Seats new/old: 124 /120 150 150/142 183 / 169
Operational Limits (PH 1.3.1, 1.10.2)
Max 90° crosswind for Takeoff and Landing: 29 kts., gust 35 (U)
Max headwind for Autoland 30 kts.
Max 90° crosswind (including gusts) for Autoland: 20 kts.
Max 90° crosswind (including gusts) for CAT II/III: 15 kts. (U)
Max tailwind component for takeoff (ex. A320 IAE): 15 kts.
Max tailwind for takeoff, A320 IAE engines: 10 kts.
Max tailwind for Autoland 10 kts.
Max tailwind component for landing: 10 kts.
Max operating altitude: 39,000 ft. (U)
Max landing gear extension altitude: 25,000 ft.
Max operating altitude w/ slats and/or flaps extended: 20,000 ft.
Speed Limits (PH 1.4.1)
Max operating speed (VMO): 350 KIAS
Max operating speed (MMO): .82 M
Max gear extended (VLE): 280 KIAS / .67M
Max gear extension (VLO): 250 KIAS
Max gear retraction (VLO): 220 KIAS
Max windshield wiper operations speed (VWW): 230 kts.
Max window open speed (who is going to open it?): 200 kts.
Max tire speed: 195 kts.
Max taxi speed: 30 kts. (U)
Max taxi speed for 90° turn: 10 kts. (U)
Turbulence Penetration –
(PH 3.1.3)
at or above 20,000 ft.: below 20,000 ft.:
A319/320 275 KIAS / .76M 250 KIAS
A321 300 KIAS / .76M 270 KIAS
US Airways Airbus A319, A320, A321 Notes
6
Max Flaps / Slats (VFE) (PH 1.4.2):
Model Position: 1 1+F 2 3 FULL
A319/320 VFE 230 KIAS 215 KIAS 200 KIAS 185 KIAS 177 KIAS
A321 VFE 235 KIAS 225 KIAS 215 KIAS 195 KIAS 190 KIAS
Ice & Rain Protection (PH 1.5.2)
Engine anti-ice must be on during all ground and flight operations when icing
conditions exist (and prior to descent into icing conditions) except during climb
and cruise when the temperature is: Below -40° C SAT
Icing conditions exist on ground: OAT 10° C (50° F) or below
Icing conditions exist in flight: TAT 10° C (50° F) or below
Fuel (PH 1.6.1)
(6.676 lbs. per gal.) A319/A320 A321
Wing tanks: 27,500 lbs 27,500 lbs.
Center tank: 14,500 lbs. 14,500 lbs.
Additional Center tanks: N/A 10,500 lbs.
Total useable fuel: 42,000 lbs. 52,500 lbs.
Autopilot / Autoland (PH 1.10.1) Autopilot Engaged Minimum Height in ft.:
Min altitude after takeoff (if SRS is indicated) 100 ft. AGL
(Note: internal logic prevents autopilot engagement for 5 seconds after lifoff.)
Enroute (A319, A320): 500 ft. AGL
Enroute (A321): 900 ft. AGL
CAT I ILS 160 ft. AGL
Non-precision approach DA, DDA or MDA
After Manual Go-Around in SRS 100 ft. AGL
RVSM Altimeter tolerances (PH 1.16, 2e.8.1)
Ground Check: PFD 1 and 2 within plus/minus 75 ft. of known airport altitude
Max difference between PFD 1 and 2 within 20 ft.
In Flight: Max difference between Capt’s. and F/O’s PFD is 200 ft.
Max brake temp for takeoff (PH 1.8.2) 300° C
Min engine oil for dispatch (PH 1.12.14) 13 qts. (U)
US Airways Airbus A319, A320, A321 Notes
7
Systems
Note: pb stands for pushbutton (NOT peanut butter!) and there are lots of ‘em!
(see PH 5.16.1) Systems info. is now found in the new Training Manual, TM)
Ice & Rain Protection ( TM 7-30.x)
Wing Anti-ice (TM 7-30.1.2) - Wing anti-ice heats the three outer wing slat panels
on each wing.
Wing A-I is available for single-engine (if Engine Fire pb not pushed) by using
pack off and crossbleed open as per PH 21 After ENG 1(2) SHUT DOWN.
Wing A-I valves close automatically:
 On touchdown
 Leak detected
 Electrical power lost
Wing A-I is not permitted on ground or above TAT 10° C (PH 2.6.2)
APU bleed is NOT permitted for Wing anti-ice. (PH 1.13.3)
Note: Wing A-I test opens valves for 30 sec. on ground.
In normal use select Wing Anti-Ice (PH 3a.2):
 On after thrust reduction on take-off
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：航空資料4(150)