F-5 Emergencies

Question 1

In-flight Alignment

Answer 1

1) NAV/DISPLAY PWR-OFF
2) NAV/DISPLAY PWR-ON
3) Maintain straight and level flight until attitude flag disappears
4) Menu page - Select
5) Mode page - Select
6) IFA - Select
* Reliable heading and attitude could be available in as little as 30 seconds with an “ATT/HDG Available” message on CDU. A “NAV READY Degraded” status may take 4 minutes.

Question 2

Smoke, Fumes, or Odor in Cockpit

Answer 2

1) Oxygen - 100%
2) Check for fire
3) Descend to 25K’ or below
4) Green Ring - pull
5) Cockpit Pressure - RAM DUMP
6) Cockpit Pressure - DEFOG ONLY (When smoke clears)
7) If smoke is severe - Jettison canopy below 300 KIAS if practical

Question 3

During a single engine takeoff, aft stick should be applied ___ KIAS prior to single engine takeoff speed. However, if available runway permits, increase airspeed as much as possible before attempting takeoff.

Answer 3

5 KIAS

Question 4

During a single engine takeoff, do not raise landing gear until at least ___ KIAS above single engine takeoff speed but no later than ___ KIAS. Raising the gear too soon may result in ______.

Answer 4

10 KIAS
210 KIAS
…settling on the runway.

Question 5

Nosewheel Shimmy on takeoff:

If noswheel shimmy dampener fails, oscillations in nosewheel deflection are induced. These appear as a snaking motion and can result in catastrophic nosewheel failure at speeds as __. If this situation exists, abort. If possible, dehike nose gear and use back stick to reduce forces on nose gear.

Answer 5

30 KIAS

Question 6

Min single engine safe flying speed with gear and flaps up is ___ KIAS (N) and ____ KIAS (F). Add __ KIAS for each degree C above standar ambient temps. Single engine maximum thrust provides a min rate of climb of ___ FPM.

Answer 6

190 KIAS (N)
200 KIAS (F)
1 KT
300 FPM

Question 7

Electrical Failure

Answer 7

1. Battery and generator switches - OFF
   - At altitudes above 25,000’, engines may flame out
2. All electrical equipment - OFF.
3. Battery and generator switches - On as required.
4. Land as soon as practicable.

Question 8

SMOKE, FUMES, OR ODOR IN THE COCKPIT

Answer 8

1. Oxygen - 100%
2. Check for fire
3. Descend to 25,000 or below.
4. Oxygen emergency lever - Emergency.
5. Cockpit pressurization - RAM DUMP.
6. Cockpit pressurization switch - DEFOG ONLY after smoke clears.
7. If smoke is severe - Jettison canopy below 300KIAS.

Question 9

Oil pressure exceeds limits or a sudden change in pressure of 10 psi or more occurs:

Answer 9

1. Throttle - Reduce to maintain pressure within limits
2. Throttle - Off if 5 psi min pressure cannot be maintained at idle RPM or if engine seizure appears imminent.
   * If the remaining engine requires shutdown, the engine previously shutdown for oil pressure may be restarted.

Question 10

Failure of engine RPM indication and loss of oil pressure on the same engine may be an indication of a _____________. Consideration should be given to shutdown of the affected engine.

Answer 10

Sheared oil pump shaft

Question 11

COMPRESSOR STALL

Answer 11

1. Throttle - Retard until engine recovers
2. Increase airspeed and advance throttle slowly.
   If engine does not recover:
3. Throttle - OFF.
   *Rapidly retarding the throttle to IDLE and immediately pushing the engine start button may permit the engine to recover and prevent complete flameout.

Question 12

Overspeed or Overtemp

If engine RPM exceeds ___% or EGT exceeds ___ C during stabilized engine operation:

Answer 12

103% / 675 Deg C

1. Throttle - Retard until indication is within limits.

Question 13

LOSS OF CABIN PRESSURE / HYPOXIC SYMPTOMS

Answer 13

• 1. Oxygen diluter lever - 100%
     
     2. Emergency Oxygen Lever - EMERGENCY as required
     3. Descend below 10K’

Question 14

LOSS OF CANOPY

Answer 14

1. Slow aircraft to below 300 KIAS

* wind blast may cause circuit breakers behind seat to pop

Question 15

ELECTRICAL FAILURE

Answer 15

1. Throttles - Retard if above 25K’
2. Altitude - 25K’ or below
3. Electrical loads - Reduce
4. Battery switch - BATT (check)
5. Generator switch(es) - RESET, then on. Hold momentarily at RESET before placing on.
6. Crossfeed - As required
7. Circuit Breakers - Check
8. Land ASAP.

Question 16

A generator failure with a corresponding fuel pressure light

may indicate __________________________.

Answer 16

…failure of the remaining generator to pick up total load.

Question 17

AIRFRAME GEARBOX FAILURE
Indicated by simultaneous illumination of the _____ and _____ caution lights for the same engine.

If gearbox fails and vibration exists:

Answer 17

generator and hydraulic caution lights

1. Throttle (affected engine) - OFF

Question 18

Gearbox failure to shift is indicated when either generator caution light comes on when accelerating through ____ - ____%. If gearbox fails to shift:

Answer 18

68% - 72%

1. Throttle - Reduce RPM to range that sustains generator ops
2. Generator switch - RESET then ON
3. Throttle - Maintain in range where generator operates, then use normally for landing.

Question 19

Fake

Answer 19

Fake

Question 20

Electrical Fire

Answer 20

1. Battery and Generator Switches - Off
2. All electrical equipment - Off
3. Batt and Gen switches - On and L/R GEN as required
   Note:
   Turn on BATT and GEN switches and equipment essential for flight and landing
4. Land as soon as practicable

Question 21

Blank

Answer 21

Blank