問題一覧
1
CABIN ALT WRN OR RAPID DESP NNC MEMORY ITEMS QTY **SEE EXPLANATION**
5
2
SEVERE TURBULENCE PROCEDURE:
1. Yaw Damper ON 2. Autothrottle DISENGAGE 3. Autopilot CWS 4. Eng Start Switches FLT 5. Thrust SET
3
STBY SYS feeds following systems:
1- THRUST REVERSERS 2- RUDDER 3- LEADING EDGE FLAPS & SLAT (extend only) 4- STBY YAW DAMPER
4
Aborted Engine Start due to “Wet Start” is considered when:
EGT is not increasing after 15 seconds engine start lever is moved to idle
5
FOR RVSM, Max difference between Capt/FO Altimeters and STBY Altimeter
60ft at SL, 80ft at 5000ft, 120ft at 10000ft
6
ENGINE OVERHEAT NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
3
7
APU FIRE NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
2
8
FLAP 1 SPEED:
VREF40 + 50
9
Max Hydraulic Pressure:
3500psi
10
Aborted Engine Start due to “Hang Start” is considered when:
N1 and N2 does not increase or increase slowly after EGT increases
11
Engine Anti Ice ON WHEN:
Icing conditions on Ground and both Engines on, Icing conditions on Climb/Cruise and SAT temp above -40C, Icing Conditions on Descent
12
INTERCEPTAR GLIDE DESDE ARRIBA
1- ASEGURARSE TENER VOR/LOC CAPTURED 2- ALT SELECTOR 1000ft AGL 3- SET V/S (Entre 1000 y 1500 FtxM dwn) 4- MONITOREAR VELOCIDAD PARA EVITAR FLAP LOAD RELIEF 5- CON GS CAPTURE, SELECTAR MISSED APP ALT Y SEGUIR PROC. NORMALES SI A LOS 1000AGL NO ESTAS GS CAPTURE Y FULL CONFIGURADO, GO AROUND
13
FLAP 5&10 SPEED:
VREF40 + 30
14
Aborted Engine Start due to “HOT START” is caused by:
EGT Quicly nears or exceed the limits
15
For RVSM, Max difference between any altimeter and field elevation
75ft
16
Max demostratted Crosswind
33kts
17
Max Engine vibration allowed:
4.0
18
Pressurization logic, Differential Pressure:
7.45psi at or below 28000ft, 7.80psi between 28000ft and 37000ft, 8.35 Above 37000ft
19
DRIFTDOWN PROCEDURE:
1. RUDDER TRIM 2. AUTOTHROTTLE OFF (SET MAX CONT N1) 3. ALT HOLD 4. SELECT DRIFTDOWN SPEED 5. SELECT DRIFTDOWN FL WHEN APPROACHING DRIFTDOWN SPEED: 6. LVL CHG 7. ATC COMMS 8. NNC
20
LANDING CONFIG NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
1
21
LOSS OF THRUST IN BOTH ENG NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
4
22
Max Tailwind TO/LDGs
10kts
23
Max Fuel Temp?
49C
24
Fuel tanks Capacity:
3915kg Tank 1/2 , 13066kg Main Tank
25
Difference between MAX Rate and MAX Angle on Climb:
MAX Rate speed is adjusted to get the maximum altitude on the shortest period of time. MAX Angle speed is adjusted to get the maximum altitude on the shortest horizontal distance.
26
For RVSM , Max difference between Capt and FO Altimeters
40ft at SL, 45ft at 5000, 50ft at 10000
27
En caso de contingencia RVSM:
1. COMUNICAR ATC 2. VIRAR 90° IZQ O DER 3. VOLAR LATERAL A LA RUTA 4. DESCENDER O ASCENDER 500FT POR ENCIMA/DEBAJO DEL NIVEL
28
When is reduced takeoff not allowed?
Contam Rwy, Windshear prob, Antiskid INOP, EEC INOP, At Capt discretion.
29
For RVSM, In Flight Max difference between Capt and FO Altimeters
200ft
30
Turbulent IAS:
280/.76 Climb,FMC TURB N1 on Cruise, 280/.76 Desc above 15000ft, 250 below 15000ft
31
EMERGENCY DESCENT NNC MEMORY ITEMS POF **SEE EXPLANATION **
11 PF, 5 PM
32
RUNAWAY STABILIZER NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
7
33
Max operating Altitude
41000ft
34
ENGINE FIRE ON ENG SEVERE DAMAGE OR SEP NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
5
35
FLAP 15 SPEED:
VREF40 + 20
36
ENG LIMIT OR SURGE OR STALL NNC MEMORY ITE,S QTY: **SEE EXPLANATION**
2
37
FLAP 25 SPEED:
VREF40 + 10
38
SYS B feeds following systems:
1- AILERONS 2- RUDDER 3- ELEVATOR & ELEVATOR FEEL 4- FLIGHT SPOILERS (3,5,8,10) 5- LEADING EDGE FLAPS & SLATS 6- NORMAL BRAKES 7- AUTOBRAKE 8- THRUST REVERSER 2 9- AUTOPILOT “B” 10- ALTN NOSE WHEEL STEERING 11- AUTOSLATS 12- YAW DAMPER 13- TRAILING EDGE FLAPS 14- LDG GR TRANSF UNIT – LDG GR
39
Minimum Oxygen Pressure required:
800psi for 2/3 Pilots, 1100psi for 4 Pilots
40
Max TO and LDG Altitude
8400ft
41
Minimum Hydraulic quantity:
76%
42
AIRSPEED UNRELIABLE NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
4
43
Por Politica de linea es obligatorio el uso de FLAP 40 cuando:
Tailwind,Cont Rwy,Antiskid INOP,Manual speed Brk,Reduced Brake performance ,CAT II/III Op.
44
ABORTED ENGINE START NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
1
45
APU LIMITATIONS:
10000ft Electrical Load + 1 Pack Bleed, 17000ft 1 Pack Bleed, 41000ft Electrical load
46
Max Rwy Slope
+-2%
47
Flap UP SPEED:
VREF40 + 70
48
SYS A feeds following systems:s
1- AILERONS 2- RUDDER 3- ELEVATOR & ELEVATOR FEEL 4- FLIGHT SPOILERS (2,4,9,11) 5- GROUND SPOILERS (1,6,7,12) 6- ALTERNATE BRAKES 7- THRUST REVERSER 1 8- AUTOPILOT “A” 9- NOSE WHEEL STEERING 10- LANDING GEAR 11- POWER TRANSFER UNIT (PTU)
49
Normal Electrical Parameters:
115V(+-5), 26V (+-4), 400HZ (+-10)
50
Use of Speedbrake:
Min altitude 1000ft, Not Recommended with Flaps extended but can be used with flaps config less than 15. In flight must not be retracted beyond FLIGHT DETENT
51
What is the max differential pressure? Relief Valve operates
9.1psi
52
What is considered Icing Conditions:
TAT Below 10C and Visible Moisture (or 1600mts/1SM Visibility)
53
TAKEOFF CONFIG NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
1
54
What is the max altitude flaps can be extended?
20000ft