問題一覧
1
Max Rwy Slope
+-2%
2
Max Tailwind TO/LDGs
10kts
3
Max demostratted Crosswind
33kts
4
Max operating Altitude
41000ft
5
Max TO and LDG Altitude
8400ft
6
For RVSM , Max difference between Capt and FO Altimeters
40ft at SL, 45ft at 5000, 50ft at 10000
7
For RVSM, Max difference between any altimeter and field elevation
75ft
8
For RVSM, In Flight Max difference between Capt and FO Altimeters
200ft
9
FOR RVSM, Max difference between Capt/FO Altimeters and STBY Altimeter
60ft at SL, 80ft at 5000ft, 120ft at 10000ft
10
When is reduced takeoff not allowed?
Contam Rwy, Windshear prob, Antiskid INOP, EEC INOP, At Capt discretion.
11
APU LIMITATIONS:
10000ft Electrical Load + 1 Pack Bleed, 17000ft 1 Pack Bleed, 41000ft Electrical load
12
Aborted Engine Start due to “Wet Start” is considered when:
EGT is not increasing after 15 seconds engine start lever is moved to idle
13
Aborted Engine Start due to “Hang Start” is considered when:
N1 and N2 does not increase or increase slowly after EGT increases
14
Aborted Engine Start due to “HOT START” is caused by:
EGT Quicly nears or exceed the limits
15
What is the max differential pressure? Relief Valve operates
9.1psi
16
Max Engine vibration allowed:
4.0
17
Flap UP SPEED:
VREF40 + 70
18
FLAP 1 SPEED:
VREF40 + 50
19
FLAP 5&10 SPEED:
VREF40 + 30
20
FLAP 15 SPEED:
VREF40 + 20
21
FLAP 25 SPEED:
VREF40 + 10
22
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.
23
What is the max altitude flaps can be extended?
20000ft
24
Max Fuel Temp?
49C
25
Max Hydraulic Pressure:
3500psi
26
Minimum Hydraulic quantity:
76%
27
Turbulent IAS:
280/.76 Climb,FMC TURB N1 on Cruise, 280/.76 Desc above 15000ft, 250 below 15000ft
28
Minimum Oxygen Pressure required:
800psi for 2/3 Pilots, 1100psi for 4 Pilots
29
Normal Electrical Parameters:
115V(+-5), 26V (+-4), 400HZ (+-10)
30
What is considered Icing Conditions:
TAT Below 10C and Visible Moisture (or 1600mts/1SM Visibility)
31
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
32
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
33
Fuel tanks Capacity:
3915kg Tank 1/2 , 13066kg Main Tank
34
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
35
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)
36
STBY SYS feeds following systems:
1- THRUST REVERSERS 2- RUDDER 3- LEADING EDGE FLAPS & SLAT (extend only) 4- STBY YAW DAMPER
37
Pressurization logic, Differential Pressure:
7.45psi at or below 28000ft, 7.80psi between 28000ft and 37000ft, 8.35 Above 37000ft
38
SEVERE TURBULENCE PROCEDURE:
1. Yaw Damper ON 2. Autothrottle DISENGAGE 3. Autopilot CWS 4. Eng Start Switches FLT 5. Thrust SET
39
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.
40
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
41
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
42
ABORTED ENGINE START NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
1
43
AIRSPEED UNRELIABLE NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
4
44
APU FIRE NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
2
45
CABIN ALT WRN OR RAPID DESP NNC MEMORY ITEMS QTY **SEE EXPLANATION**
5
46
EMERGENCY DESCENT NNC MEMORY ITEMS POF **SEE EXPLANATION **
11 PF, 5 PM
47
ENGINE FIRE ON ENG SEVERE DAMAGE OR SEP NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
5
48
ENG LIMIT OR SURGE OR STALL NNC MEMORY ITE,S QTY: **SEE EXPLANATION**
2
49
ENGINE OVERHEAT NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
3
50
LANDING CONFIG NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
1
51
TAKEOFF CONFIG NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
1
52
LOSS OF THRUST IN BOTH ENG NNC MEMORY ITEMS QTY: **SEE EXPLANATION **
4
53
RUNAWAY STABILIZER NNC MEMORY ITEMS QTY: **SEE EXPLANATION**
7
54
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