Non Normals Flashcards
1
Q
Rejected Take Off
A
2
Q
ENGINE FIRE ON THE GROUND
A
3
Q
ON GROUND EMERGENCY
(Not engine fire)
A
4
Q
FAILURE MANAGEMENT
A
- FLY THE AIRCRAFT
* altitude, thrust, speed, gear up etc. * if possible, restore auto flight
- IDENTIFY AND CONFIRM THE FAILURE
* cross confirmation by both pilots is mandatory.
- SHORT TERM PLAN
* flight path (special proc. 45 deg HDG change, etc) * inform ATC (PAN PAN, MAYDAY)
- TAKE ACTION
* Memory Items (if required) then * MFDU Items > STS > QRH > AOM * If no MFDU items > QRH > STS > AOM * Circuit Breakers * Normal Checlists - LONG TERM PLAN
* AOM - additional information * AOM SUP - flight techniques * MEL - further dispatch * FORDEC
REMEMBER: F. I. S. T. L.
5
Q
Fokker 100 MEMORY ITEMS
A
- BOTH ENGINES FLAME OUT
- EMERGENCY DESCENT
- ON GROUND EMERGENCY / EVACUATION
- JET PIPE FIRE
- ENGINE START FAULT
- ENGINE START - NO LIGHT UP
- ENGINE START - HOT START
- ENGINE START - N2 STAGNATION (HUNG START)
6
Q
Both Engines Flame Out
A
7
Q
Emergency Descent
A
8
Q
On Ground Emergency / Evacuation
A
9
Q
JETPIPE FIRE
A
10
Q
ENGINE START FAULT
A
11
Q
ENGINE START - HOT START
A
12
Q
ENGINE FAILURE AFTER V1 (NAV + AFCAS)
A
13
Q
ENGINE FAILURE AFTER V1 - NAV PROF
A
14
Q
ENGINE FAILURE / FIRE AFTER V1 - DIAGRAM
A
15
Q
Approach to Stall Recovery
A
Remember:
S - “Stall” C - Click Click (disconnect AP and AT) U - UNLOAD R - ROLL T - THRUST S - Stabilize SCURTS
16
Q
Fuel Pump Fault
A
17
Q
Pack Fault
A
18
Q
PFD Failure
A
19
Q
IDG Temperature Alert
A
20
Q
Pitot Heat 1 Fault
A
21
Q
Bleed Fault
A
22
Q
NO LIGHT UP
A
23
Q
INTERRUPTED START
A
24
Q
N2 STAGNATION
(HUNG START)
A
25
WIND-SHEAR RECOVERY TAKE OFF
Indications
* IAS +/- 15 kt
* V/S +/- 500 rpm
* pitch +/- 5 deg
Precautions
* TOGA thrust
* Longest Runway
* Flap 8
* Consider increased Vr
* CONT ignition
* No FD/ AP below 1500’ if Wind-shear detection INOP
26
Wind shear Recovery Approach
Indications
* IAS +/- 15 kt
* vertical speed + / - 500 ft
* pitch +/- 5 deg
* glide slope +/- 1 dot
* unusual thrust lever position for a significant period of time.
Precautions
* Fly a stabilized approach
• Minimize thrust reductions
• Use the most suitable runway • Use ILS or VASIS for glide slope monitoring
• Consider flap 25 for landing.
• Consider increased approach speed
• Monitor AP and ATS
• Use AUTO ignition - or for aircraft not so equipped, select CONT ignition
27
Landing Gear Selector Blocked
F - Fly the Aircraft (FMA, AP, don’t retract LG)
I - Identify and Confirm
S - Short term plan (maintain HDG - climb to 400 ft - check
T - IF GND/ FLT CTL FAULT displayed then - Take action (QRH GND/FLT CONTROL FAULT - STS - AOM - CBs, Normal x-lists)
L - Long Term Plan (WTFN - return, divert or continue)
28
Emergency DC Bus Fault
Failure Management
F - FO take over, manual flight
I - Identify and confirm Emergency DC Bus Fault
S - Short term (lowest safe, stop climb ATC)
T - Take Action (MFDU, STS, QRH, AOM, CBs, Normal Cx Lists
L - Long term plan (return, landing PERF calc, CM, ATC, OCC)
29
Emergency DC Bus Fault
Bus Equipment List
30
Rapid Depressurization and Emergency Descent
31
TCAS
32
Electrical Smoke
33
Smoke Removal Procedure
34
Unreliable Airspeed
35
Upset Recovery - Nose High
36
Upset Recovery - Nose Low
37
Alpha Mode Activation
38
GPWS WARNING
TOGA - CLICK CLICK - FIREWALL - 20 DEGREES
39
TAWS CAUTION
40
Inadvertent Thrust Reverser Deployment
41
Thrust Reverser Unlocked Procedure
42
Jammed Stabilizer
43
Jammed Stabilizer Procedure
