Instrument Failures and GPS/INS Failures
T-45C TS & ADV BIFP-09; IUT BIFP-05
7.
Join with wingman if possible
8.
Consider declaring in-flight emergency
VII. Airspeed indicator failure
Sg 7, fr 2
INSTRUMENT FAILURES
A. Use ADI and HUD airspeed indication
* GINA failure
* Standby attitude indicator
failure
*
MFD failure
* AOA indicator failure
B. Use AOA as cross-check of standby airspeed
*
HSI failure
* Radar altimeter failure
*
ADI failure
* VOR failure
indication (see flight condition, angle of attack
*
Turn and slip
* TACAN bearing/DME
indicator failure
failure
units matrix on page V-15-9 of the NATOPS
*
Pitot static
* ILS glideslope failure
malfunctions
manual)
*
Airspeed indicator * ILS localizer failure
failure
*
Barometric
* ILS marker beacon failure
altimeter failure
C. Procedures for dealing with airspeed indication
*
Vertical speed
* Flight with partial panel
indication failure
failure
Sg 7, fr 3
1.
Use standby airspeed indication if available
2.
Use AOA as cross-check of standby
airspeed indication
D. Procedures for dealing with a combined display
system and standby airspeed indicator failure
1.
Check PITOT HEAT—ON
AIRSPEED INDICATOR FAILURE
2.
Report failure to ATC
Sg 7, fr 4
3.
Fly AOA in place of airspeed
ANGLE OF
ANGLE OF
FLIGHT CONDITION
FLIGHT CONDITION
ATTACK - UNITS
ATTACK - UNITS
4.
Watch for other indications of pitot static
PENETRATION
TAKEOFF (LIFTOFF)
Speed brakes out, 80percent rpm,
1/2flaps................................................ 19.5
4,000 to 6,000 fpm rate of descent....... 11
Full flaps............................................... 20
system problems
LANDING
AFTER CLEAR OF OBSTACLES
13
Gear extension.....................................
Start flaps up........................................ 17
13
Flapextension......................................
13
GCA pattern(clean)..............................
MRT CLIMB
10
GCA pattern(landing configuration).....
10
0 to 10,000 feet.....................................
17
GCA pattern(final)................................
10
10,000to20,000 feet............................
17
Carrierpattern and approach ...............
10
20,000to30,000 feet............................
11
30,000to40,000 feet............................
STALLWARNING (rudder pedal shaker)
All configurations.................................. 21.5
MAXIMUM ENDURANCE
Any altitude........................................... 14
MAXIMUM RANGE................................. 12 to13
EQUIVALENT AOA
Page 9-16
(4-01) Original
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