12.05.2010

A320 CH27


27

1.       THERE ARE 2 FLAP AND 5 SLAT
2.       A321 HAS DOUBLE SLOTTED FLAP
3.       SPD BRAKE IS 2,3,4 AND ROLL SPOILER IS 2,3,4,5
4.       SIDE STICK P/B HAS 2 FUNC: A/P DISCON AND PRIORITY GIVE
5.       SIDE STICK PRIORITY LIT ON TO IND LAST PRIORITY GENERATED IN ELAC & SEC
6.       STICK FAIL THEN MASTER CAUTION + CRC
7.       IF NO PRIORITY SELECTED CAPT & F/O LITS FLASH AND AURAL “DUAL INPUT” EVERY 5SEC
8.       BOTH STICK MOVE:
a.       SAME SIDE : ADDED
b.      DIFF SIDE: SUBTRACTED
9.       AFTER TOUCH DOWN THS GOES TO NEUTRAL
10.   RUD TRIM SW OPERATES ELEC TRIM ACTUATOR TO NEW NEUTRAL POS
11.   GND SPOILERS SHOWN IN WHEEL PAGE
12.   FLAP SLAT SHOWN IN ENG WARN DISPLAY
13.   EFCS COMPUTERS:
            a.       2 ELAC (ELEV & AIL COMP) FOR PITCH / ROLL
            b.      3 SEC (SPOILER & ELEV COMP) FOR PITCH/ROLL
            c.       2 FCDC (FLT CONT DATA CONCEMTRATOR) FOR TEST & IND
            d.      2 FMGC (FLT MANAGE & GUIDANCE COMPUTER) FOR A/P CMD
            e.      2 SFCC (SLAT/FLAP CONT COMPUTER)
14.   ALL COMP ARE IN AFT AV BAY BUT SEC3 IS IN FWD
15.   NORMALLY ELAC2 ACTIVE IN PITCH,ELAC1 IN ROLL ,SEC’S  FOR SPOILERS
16.   ALL SURFACE ARE ELEC CONT & HYD ACTUATE
17.   RUDD & THS ALSO HAS A MECH CONT
18.   RUD TRIM & TRAVEL LIMIT AND THS SERVO ARE ELEC OPERATED
19.   RUD TRIM AUTO CONT BY FMGC AND MANUALLY VIA FAC
20.   NORMALLY ONE ELEV CONT BY ELAC & ONE BY SEC
21.   AIL,ELEV AND YAW DAMPER HAVE 2 SERVO : ONE IS ACTIVE
22.   THS HAS ONE SERVO CONTROL WITH 3 ELEC MOTOR 2 HYD MOTOR CONT BY SEC OR ELAC
23.   3 THS ELEC MOTOR:
                       a.       #1 CONT BY ELAC2
                       b.      #2 BY ELAC1 & SEC1
                       c.       #3 BY SEC2
24.   FLAP/SLAT HAS PCU
25.   EFCS COMPUTERS HAVE 3 LAW:
                                       a.       NORMAL : FULL PROTECTION
                                       b.      ALTERNATE: IF NORMAL FAIL SOME PROTECTION REDUCED
                                       c.       DIRECT : NO PROTECTION
26.   DIRECT LAW ACTIVATED ON GND
27.   WING TIP BRAKE HYD ACTIVE CAN RESET ON GND
28.   PPU (POS PICKOFF UNIT) SENDS FLAP/SLAT POS TO SFCC & ECAM
29.   2 FLAP SENSOR BETWEEN IN & OUT FLAP SEND FLAP FAIL TO LGCIU
30.   SLAT CAN’T RETRACT IN HI AOA ( α LOCK)
31.   SPOILERS ARE AUTO RET IF FAIL
32.   YAW MOVE IS 25° BUT IN A319 IS 30°
33.   ELAC SEND YAW DAMP & TURN COORD TO FAC
34.   FAC DO YAW DAMP IF NO ELAC OR A/P NOT ENGAGE
35.   EMER GEN RUN THEN FAC1 ALTERNATE LAW ACTIVE
36.   RUD MOVE IS 3.5° MAX IF A/S > 380KTS LIMITED BY FAC
37.   IF BOTH FAC FAIL FULL DEFLECTION AVAIL IN SLAT EXT   AND RUD TRIM LIM IS IN LOW SPD
38.   ROLL ORDER HAS PRIORITY OVER SPD BRK
39.   SPD BRK RET IF α FLOOR ACTIVE
40.   SPOILERS HAS NO BACKUP IF SEC FAIL
41.   IPPU AND FPPU ARE IN DIFF GEAR BOX AND APPU ON WTB
42.   IPPU SEND SIG TO ECAM AND FPPU/APPU TO SFCC
43.   ENG FAIL COMPENSATION ACTIVE IN T/O , G/A, RUNWAY 







































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