Flight Safety Rev2/2011 Flashcards
(47 cards)
1
Q
Engine Failure During Takeoff
(Below V1-Takeoff Aborted)
A
- Brakes. Apply
- Thrust. IDLE
- Thrust Revers. Deploy
- Rev Lights. Verify
- Revrse. Thrust. As Req.
- Speed Brakes. Extend
2
Q
Engine Failure During Takeoff
(Above V1-Takeoff Continue)
A
- Nose Up Pitch @ (VR).
13-15 degrees - Landing Gear UP
(When Positive Rate) - Airspeed. V2
3
Q
Engine Fire - Bell Sounds
LFT or RT Engine Fire Push
Illuminates!
A
- Thrust (affectd Eng).
IDLE
*If Engine Fire Push Still Illuminated * Then - Thrust Lvr Affected ENg
CUTOFF - Illuminated Fire SW
PUSH - Either Fire Bottle Switch
PUSH
4
Q
Engine Fire Detector Failure
Left or Right Fire Det Fail Light illuminated
A
If the Fire Det Fail annunc. Illuminates following an engine fire push SW illumination, the fire should be considered to still be burning.
- Engine Fire Proced.
Complete Chck List - Remaining Fire Bottle SW
PUSH - Land
Nearest Suitable Airport
5
Q
IF Engine FIRE Det Fail
Annunciation illuminates without an ENG FIRE Push SW illumination or Anyother indication of an engine fire:
A
Repair Fault prior to the next flight.
6
Q
Engine Failure in Landing Configuration
A
- Thrust (operating eng)
As Required - Airspeed
VREF
7
Q
Dual Engine Flameout
A
Immediate Relight
1. N2 Verify ABV 52%
Caution: Engine Damage may result if an immediate relight is attempted BELOW 52% N2
- Ignitions ON
IF N2 is Not ABV 52% or neither engine delights then: - Battery. EMER
8
Q
Inadvertent Thrust REV
Deployment During T/O
(Below V1 - Takeoff Abort)
L TR ARM. R TR ARM
UNLOCK. UNLOCK
DEPLOY. DEPLOY
OR
A
- Brakes. Apply
- Thrust. IDLE
- T/R’s. Both Deploy
- Rev Lights. Verify
- Rev. Thrust. As Required
- Speed Brakes. Extend
9
Q
Inadvertent T/R Deployment
During Takeoff
(Above V1- Takeoff Cont.)
Unlock. Unlock
Deploy. OR. Deploy
L TR PUSH. R TR PUSH
EMER STOW. EMER STOW
OR
A
- Emer Stow Affected Eng
PUSH - Nose Up Pitch Attitude @ VR Rotation
13-15. Degrees - Landing Gear
When positive Rate:
UP - Airspeed
V2 Min
IF T/R Will Not Stow and lock - T/R. Affected Engjne
CUTOFF
10
Q
Inadvertent T/R Deployment
IN a FLIGHT
Unlock. Unlock
Deploy. OR. Deploy
L TR PUSH. R TR PUSH
EMER STOW. EMER STOW
OR
A
- Emer Stow Push Switch
Affected ENG
PUSH - Altitude
Below 30k Feet - Airspeed
Until TR stows and locks
Below 135 KIAS
11
Q
Inadvertent Overspeed
A
- Thrust IDLE
- Speed Brakes. Extend
- IF acft is in nose down attitude initiate a wings level pull-up without exceeding structural limits. (3.2G)
12
Q
Loss of Airspeed Indication
A
- Autopilot. Disconnect
- Airspeed. Slow to Maintain 0.2 AOA.
- Thrust. As Req.
- Speed Brakes. As Req.
Slow to 0.25 AOA w Speed. Takes Extended.
13
Q
Electrical Fire or Smoke
A
- Oxygen masks
Don - Smoke Goggles
Don - Mic Selectors
Oxy Mask - SPKR Switches (PIC & SIC)
ON or Don Headset - Interphone SW Pilot
ON - Smoke Removl Procedures
OF Needed - Faulted Circuits
Isolate - Battery
EMER - Master Gen SWITCHES
EMER
14
Q
Environmental system smoke or odor
A
- Oxygen masks
Don - Smoke Goggles
Don - Mic Selectors
Oxy Mask
. SPKR Switches (PIC & SIC)
ON or Don Headset - INTPH SW Pilot
ON - Cabin Pressure Source
Isolate SEL L ENG or R ENG
15
Q
Smoke Removal
A
Oxygen masks
Don
2. Smoke Goggles
Don
3. Mic Selectors
Oxy Mask
4. SPKR Switches (PIC & SIC)
ON or Don Headset
5. INTPH SW Pilot
ON
6. Checklist
16
Q
Cabin Decompression
A
- Oxygen masks
Don - Smoke Goggles
Don - Mic Selectors
Oxy Mask - SPKR Switches (PIC & SIC)
ON or Don Headset - INTPH SW Pilot
ON - Decompression chck list
17
Q
Emergency Descent
A
- Thrust
Idle - Speed Brakes
Extend - Autopilot
OFF - Initiate Moderate Bank
45 degree Bank - Descend to 10,000 ft or Min Safe Alt.
18
Q
Overpressurization
A
- Cabin Pressure Source
OFF - Oxygen masks
Don - Mic Selectors
Oxy Mask - SPKR Switches (PIC & SIC)
ON or Don Headset - INTPH SW Pilot
ON
19
Q
Loss BOTH Generators
L GEN OFF. And. R GEN OFF
A
- Gen FLD and START/GEN CB’s - Aft Main Panel
CHECK - Generator Reset L & R
Reset/Norm
20
Q
Pitch Trim Runaway or Failure!
Roll Trim Runaway or
Failure!
Rudder Trim Runaway or
Failure!
A
- Trim Interrupt/AP Disengage Switch
PUSH & HOLD
21
Q
Power Brake Failure
A
- Emergency Brake Handle.
Break Safety Wire and remove guard clip. - Emergency Brakes
Apply Gradually
22
Q
Autopilot Trim Fail
AP PITCH TRIM FAIL AP ROLL TRIM FAIL
A
- Trim Indicators
Check for proper position for flight condition. - Trim interrupt/AP Disengage Switch
PUSH
23
Q
Autopilot Overspeed Recovery
A
- Thrust
IDLE
24
Q
Flight Director Malfunctions
A
- Trim interrupt/AP Disengage Switch
PUSH
25
Maximum Operating Airspeed
VMO S.L to 8,000 Ft.
264
VMO 8,000 to 11,000 Ft.
264 to 320 linear Variatn
VMO 11,000 to 26,000 Ft.
320
Limiting Mach Mmo ABV
26,000 ft
0.78
26
Flap Extension and Operation
VFE/VFO. Flaps 10 and 20
VFO Flaps 30 degrees
VFE Flaps 30 degrees
1. VFE/VFO Flaps 10 & 20
200
2. VFO Flaps 30
170
3. VFE Flaps. 30
165
27
Landing Gear & Lights
Landing Gear Normal VLO
Landing Gear Ext VLE
Landing Gear Emer VLO
Landing Lights VLL
Landing Gear Normal VLO
200
Landing Gear Ext VLE
200
Landing Gear Emer VLO
150
landing Lights. VLL
200
28
SpeedBrakes Ext & Ops
VSB
VSB
NO LIMIT
29
Minimum Controllable Airspeed
Airborne & Ground
Airborne Vmca Flaps 0
Airborne Vmca Flaps 10&20
Ground. Vmcg. Flaps 0,10,20
Airborne Vmca Flaps 0
96
Airborne Vmca Flaps 10&20
89
Ground. Vmcg. Flaps 0,10,20
88
30
Windshield Wipers
Vww
Vww
200
(If Installed)
31
Tire Limiting Speed
V tire
V tire
165
True speed on the ground
32
Engine Speeds
Takeoff N1 Fan
Takeoff N2 Turbine
Idle N2 Turbine, Engine EFC ON
Idle N2 Turbine, Engine EFC OFF (in non icing condition)
Engine Speeds
Takeoff N1 Fan
104%
Takeoff N2 Turbine
96%
Idle N2 Turbine, Engine EFC ON
52%
Idle N2 Turbine, Engine EFC OFF (in non icing condition)
46%
33
Engine Temperatures
Takeoff ITT
Starting ITT
ITT for maximum continuous thrust
Takeoff ITT
700 C
Starting ITT
550c to 600c for 4 Sec Max
600c to 700c for 2 Sec Max
ITT for maximum continuous thrust
680c
34
Engine Oil
Oil Temp takeoff and max continuous thrust
Oil Pressure takeoff and max continuous thrust
Minimum oil temperature for Starting
Oil pressure at idle RPM
Oil Temp takeoff and max continuous thrust
10 to 121 c
Oil Pressure takeoff and max continuous thrust
60 to 83 PSI
Minimum oil temperature for Starting
-40 c
Oil pressure at idle RPM
40 PSI minimum
35
Thrust Reverser Limitations
Full Reverse Cutoff Speed
Time for Continuous Rev Thrust above reverse idle
Deployed Time during taxi operations
Thrust Reverser Limitations
Full Reverse Cutoff Speed
55 KIAS or above
Time for Continuous Rev Thrust above reverse idle
30. SECs Max
Deployed Time during taxi operations
5. Seconds
36
External Power Assisted Start
Limited to three (3) cycles as follows:
Secs ON. Mins OFF
1st Cyc:
2nd CYC:
3rd CYC:
Secs ON. Mins OFF
1st Cyc: 30. 5
2nd CYC: 30. 15
3rd CYC: 30. 60
37
Battery Start
Do not attempt battery start if battery voltage is below____volts.
22 Volts
38
Generator Assisted Start
Do not attempt to start the second engine until the generator load is below _____AMPS.
150. AMPS
39
Starter Generator Limits
Ground Operation
Max Generator Load
Starter Generator Limits
Ground Operation
Max Generator Load
280 AMPS Each Generator
40
Starter Generator Limits
In flight Operation
Both Generators Operating Up to 41,000 ft _____
Both Generator’s Operating Above 41,000 ft.______
In flight Operation
Both Generators Operating Up to 41,000 ft _280 AMPS
Both Generator’s Operating Above 41,000 ft _260 AMPS
41
Limitations
In Flight Operation:
One Gen Operating Up to 29,000 ft.
One Generator Operating Up to 29,000 ft Icing Cond
Transient below 20,000 ft. 30 secs Max
One Generator Operating From 29,000 ft. To 41,000 ft.
One Generator Operating Above 41,000
In Flight Operation:
One Gen Operating Up to 29,000 ft.
400
One Generator Operating Up to 29,000 ft Icing Cond
440
Transient below 20,000 ft. 30 secs Max
525
One Generator Operating From 29,000 ft. To 41,000 ft.
280
One Generator Operating Above 41,000
260
42
Structural Limitations
RK 1-343. 344 & After
Max Rmp.
Max T/O
Max Ldg
Max Zero
1-343. 344 & Aftr
Max Rmp. 16,300. 16,500
Max T/O. 16,100. 16,300
Max Ldg. 15,700
Max Zero. 13,000
43
Maneuvering Load Factors
Flaps 0
Flaps. 10,20 and 30
Flaps 0
-1.0 to +3.2 G
Flaps. 10,20 and 30
0 to. +2.0 G
44
Takeoff & Landing Ops
Airfield Op Press Altitude
Ambient Temperature
Max Tailwind for TO @ LDG
Max Fuel Unbalance T/O
Max Fuel Unbalance. LDG
Airfield Op Press Altitude
Up to 10,000 feet
Ambient Temperature
-40 c to ISA +35 c
Max Tailwind for TO @ LDG
10 knots
Max Fuel Unbalance T/O
100 lbs
Max Fuel Unbalance. LDG
300 ibs
45
Fuel Limits
Min Fuel Temp
Max Fuel Temp
Min Fuel Temp
-40 c
Max Fuel Temp
+50 c
46
Enroute Operations
Cert Ceiling
Ambient Air Temp
Max Fuel Unbalance
Yaw Damper
Ext of Gear, Flaps, Ldg Lights
Refrigerant AC
Cert Ceiling
45,000.
Ambient Air Temp
-65 c to ISS +35 c
Max Fuel Unbalance
300 lbs
Yaw Damper
Operable and on for flight in icing cons or flight above 28,000 ft.
Ext of Gear, Flaps, Ldg Lights
Prohibited above 20,000 ft
Refrigerant AC
Prohibited above 18,000 ft
47
EGPWS WARNING
