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F100 PROCEDURES > Non Normals > Flashcards

Non Normals Flashcards

1
Q

Rejected Take Off

A
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2
Q

ENGINE FIRE ON THE GROUND

A
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3
Q

ON GROUND EMERGENCY
(Not engine fire)

A
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4
Q

FAILURE MANAGEMENT

A
  1. FLY THE AIRCRAFT
    * altitude, thrust, speed, gear up etc.
* if possible, restore auto flight
  2. IDENTIFY AND CONFIRM THE FAILURE
    * cross confirmation by both pilots is mandatory.
  3. SHORT TERM PLAN
    * flight path (special proc. 45 deg HDG change, etc)
* inform ATC (PAN PAN, MAYDAY)
  4. TAKE ACTION
    * Memory Items (if required) 
    then
* MFDU Items > STS > QRH > AOM
* If no MFDU items > QRH > STS > AOM
* Circuit Breakers
* Normal Checlists
  5. LONG TERM PLAN
    * AOM - additional information
* AOM SUP - flight techniques
* MEL - further dispatch
* FORDEC

REMEMBER: F. I. S. T. L.

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5
Q

Fokker 100 MEMORY ITEMS

A
  1. BOTH ENGINES FLAME OUT
  2. EMERGENCY DESCENT
  3. ON GROUND EMERGENCY / EVACUATION
  4. JET PIPE FIRE
  5. ENGINE START FAULT
  6. ENGINE START - NO LIGHT UP
  7. ENGINE START - HOT START
  8. ENGINE START - N2 STAGNATION (HUNG START)
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6
Q

Both Engines Flame Out

A
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7
Q

Emergency Descent

A
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8
Q

On Ground Emergency / Evacuation

A
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9
Q

JETPIPE FIRE

A
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10
Q

ENGINE START FAULT

A
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11
Q

ENGINE START - HOT START

A
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12
Q

ENGINE FAILURE AFTER V1 (NAV + AFCAS)

A
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13
Q

ENGINE FAILURE AFTER V1 - NAV PROF

A
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14
Q

ENGINE FAILURE / FIRE AFTER V1 - DIAGRAM

A
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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
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16
Q

Fuel Pump Fault

A
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17
Q

Pack Fault

A
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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
Q

WIND-SHEAR RECOVERY TAKE OFF

A

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
Q

Wind shear Recovery Approach

A

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
Q

Landing Gear Selector Blocked

A

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
Q

Emergency DC Bus Fault

A

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
Q

Emergency DC Bus Fault
Bus Equipment List

A
30
Q

Rapid Depressurization and Emergency Descent

A
31
Q

TCAS

A
32
Q

Electrical Smoke

A
33
Q

Smoke Removal Procedure

A
34
Q

Unreliable Airspeed

A
35
Q

Upset Recovery - Nose High

A
36
Q

Upset Recovery - Nose Low

A
37
Q

Alpha Mode Activation

A
38
Q

GPWS WARNING

A

TOGA - CLICK CLICK - FIREWALL - 20 DEGREES

39
Q

TAWS CAUTION

A
40
Q

Inadvertent Thrust Reverser Deployment

A
41
Q

Thrust Reverser Unlocked Procedure

A
42
Q

Jammed Stabilizer

A
43
Q

Jammed Stabilizer Procedure

A

F100 PROCEDURES (9 decks)

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