Quantcast Appendix A - T-39 Aircraft Liminations - Cont'd - P-8570077

 

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STUDENT GUIDE T-39N/G NATOPS
MISCELLANEOUS
starter limits
4 - 30 second attempts, 2 mins between ea. in a 20 min
period
igniter limits
2 min on, 3 min off, 2 min on, 23 min off
1.5 EPR
required for engine anti-icing
3300 lbs
takeoff power thrust at sea level
0 - 2500 AGL
limits of radar altimeter
0 - 8000 MSL
no pressurization occurs
1500 AGL-
min altitude for autopilot engagement; T/R switch OFF
10,000 + 400 MSL
CABIN PRESS FAIL light on; FASTEN SEATBELT It
13,500 + 500 MSL
02 warning horn; automatic passenger 02 flow
FL 180
max for aux air conditioner
25,000 MSL
remain below if cabin unpressurized.
41,000 MSL
all occupants wear oxygen masks above
45,000 MSL
aircraft ceiling
260 - 600 PPH
start fuel flow, each engine
1063 gallons
useable fuel
200 lbs
max fuel imbalance for takeoff or landing
300 lbs
low fuel lights on
400 lbs
max fuel imbalance enroute
11,700
empty weight
13,300
zero fuel weight
17,500
max landing weight
20,000 lbs
max takeoff weight
20,400 lbs
max gross weight
10 seconds
max time allowed at zero or negative g
20 seconds
if no lightoff during start, windmill; if no oil pressure
during start, shutdown
0 2.0 g
gear and/or flaps extended
-1.0 - 4.0 g
sea level to 20,000 MSL, upper limit decreasing by 1/2g
each additional 5,000 feet
1.6 gallons
oil capacity
2 gallons
hydraulic reservoir capacity
Airstart envelope
below 29,000 MSL, > 160 KIAS
Max range
25,000 MSL and .55 PAN (with cabin press failed)
Clean glide
21NM per 10,000 AGL (dirty is approximately 1/2 of this)
Noise abatement T/O
set EPR = 1.6, 160 KIAS climb
30 minutes
emergency lights battery life
4 hours
standby attitude indicator power
45 minutes
battery life with dual generator failure
AIRCRAFT LIMITATIONS
A-3


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