T6 Numbers
Terms
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- Empty weight
- 4900 lbs
- Max Takeoff Weight
- 6500 lbs
- Max Shaft HP
- 1100
- Oil Capacity
- 18 quarts
- OIL PX annunciator with PCL above idle
- 40 psi
- OIL PX annunciator with PCL at idle
- 15 psi
- turbine output shaft speed
- 30,000 rpm
- prop operating speed
- 2000 rpm
- ground mode at idle
- 60% N1
- flight mode at idle
- 67% N1
- PMU managed minimum above 10K
- 80% N1
- ignition and boost pump deactivated during auto start
- 50% N1
- fuel pressure switch limit, turns on BP
- 10 psi
- manual motor after aborted start/inverted flight limit
- 20 seconds
- normal wing tank capacity
- 530 lbs
- collector tank capacity
- 40 lbs
- SPR refueled full fuel load
- 1100 lbs
- over wing refueled full fuel load
- 1200 lbs
- (for 2 minutes) imbalance where FUEL BAL annunciator illuminated
- 30 lbs
- auto fuel balance
- 20 lbs
- middle fuel probe
- 445 (+ 50) lbs
- inner fuel probe
- 308 (+ 50) lbs
- collector tank pressurized by transfer jet pumps
- 1 to 1.5 psi
- L or R FUEL LO annunciator illuminated
- 110 lbs
- starter/generator output
- 28 VDC (300 amp)
- main battery output
- 24 VDC (40A HR)
- aux battery output
- 24 VDC (5 A HR)
- hydraulic pressure
- 3000 psi
- hydraulic system total capacity
- 1.25 gal
- hydraulic reservoir capacity
- 0.6 gal
- min hydraulic pressure to operate NW steering, gear, flaps, speed brake
- 1800 psi
- fuel pressure supplied by engine driven low pressure fuel pump
- 40 psi
- fuel pressure supplied by engine driven high pressure fuel pump
- 700 psi
- max hydraulic volume allowed past the hydraulic fuse
- 45 cu in
- hydraulic pressure relief valve opens
- 3250 to 3500 psi
- EHYD PX LO annunciator illuminates
- 2400 (+ 150) psi
- HYDR FL LO annunciator illuminates
- 1 qt
- normal gear extension/retraction time
- 60 seconds
- gear warning horn sounds if A/S is below 120
- 87% N1
- NWS range
- 24 degrees
- flap deflection in TO
- 23 degrees
- flap deflection in LDG
- 50 degrees
- speed brake deflection when deployed
- 70 degrees
- TAD active with no weight on wheels
- 80 knots
- Below this Mach is blanked on A/S ind
- 0.40 Mach
- stall
- 18 AOA
- on speed
- 10 to 11 AOA
- on speed AOA
- 1.3 VS
- max endurance
- 8.8 AOA
- max range
- 4.9 AOA
- Optimum approach speed decrease rate
- 1 knot/100 lbs
- Optimum max range AOA altitude
- 25,000’ MSL
- Pre-stall stick shaker
- 5 - 10 kts (15.5 units)
- Ejection seat limits
-
0’/0 KIAS
to
35,000’/370 KIAS - Automatic seat man separation
- 10,000’ to 18,000’ MSL
- ISS BOTH rear seat ejection delay
- 0.37 seconds
- Bleed air inflow prevented with A/C clutch engaged
- <7500’ MSL
- automatically maintained until 18,069’ MSL (3.6 + 0.1 psid)
- 8000’ cockpit P/A
- CKPT ALT annunciator illuminated
- 19,000’ cockpit P/A
- CKPT PX annunciator illuminated
- 3.9 + 0.1 psid
- DUCT TEMP annunciator illuminated
- 300 degrees F
- RMU cursor automatically reverts to UHF field
- 20 seconds
- UHF/VHF memory
- 20 frequencies
- NAV memory
- 10 frequencies
- ELT transmission limit (battery limited)
- 50 hours
- EADI declutters
-
> +30ï‚°/-20ï‚° pitch
or
65ï‚° roll - Full EADI presentation reappears after unusual attitude
-
< +25ï‚°/-15ï‚° pitch
and
60ï‚° roll - NACWS display time limit after trigger is released
- 7 seconds
- NACWS landing mode
- 1.5 NM range
- NACWS vertical separation alert (enroute mode)
- +/- 2700’
- NACWS vertical separation alert (landing mode)
- +/- 500'
- NACWS rectangle with digits
- </= +/- 300’
- NACWS upward/downward pointing triangle with digits
- >/= +/- 400’ to 900’
- NACWS upward/downward pointing triangle with no digits
- >/= +/- 1000’ to 2700’
- GPS self test indications
- 34.5 NM, 315 DTK, 130ï‚° bearing
- GPS user defined waypoints
- 250
- GPS stored flightplans
- 25
- max waypoints per flight plan
- 30
- flash prior to turn to next waypoint
- 20 seconds
- CDI full scale deflection, enroute mode
- +/- 5 NM
- CDI full scale deflection, approach arm
- +/- 1 NM
- CDI full scale deflection, approach active
- +/- 0.3 NM
- Approach arm
- 30 NM
- Approach active
- 2 NM
- FDR annunciator illuminates
- 80% full
- AUX BAT test light will not illuminate
- <50% capacity
- OBOGS TEMP annunciator illuminates
- 200 degrees F
- NORMAL O2 concentration, sea level to 15,000’ MSL
- 25% to 70%
- NORMAL O2 concentration, 15,000’ to 31,000’ MSL
- 45% to 95%
- O2 concentration, MAX selected
- 95%
- OBOGS warm-up time (after engine start)
- 3 minutes
- OBOGS FAIL annunciator extinguishes during BIT test
- </= 2 minutes
- baggage compartment weight limit
- 80 lbs
- icing inhibitor mix
- .5 pint/ 50 gal fuel
- external power requirements
- 28 to 28.5 VDC/1000 to 1500 Amps
- main gear tire pressure
- 225 + 5 psi
- nose wheel tire pressure
- 120 + 5 psi