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Max takeoff weight
6500 lbs
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Max Shaft Horsepower
1100
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red OIL PX annunciator with PCL at idle
<15 psi
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amber OIL PX annunciator with PCL at idle
15-40 psi
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amber & red OIL PX annunciator with PCL at idle
15-40 psi(5 sec+)
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red OIL PX annunciator with PCL above idle
<40 psi
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amber OIL PX annunciator with PCL above idle
40-90psi(10 sec+)
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turbine output shaft speed
30,000 RPM
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prop operating speed
2000 RPM
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prop diameter (4 blade, const-speed, variable pitch, non-reversing, feathering)
97 in.
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– torque available from sea level to approx. 12K to 16K ft
100%
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torque @ prop shaft when 100% torque
2900 ft/lbs
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thrust @ sea level, zero airspeed when 100% torque
2750 lbs
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blade angle when prop in low pitch
15°
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voltage supplied by PMA to PMU (PMU converts it to DC)
32 VAC
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PMU switches to 28 VDC battery bus
40-50% Np
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PMU managed minimum above 10K
80% N1
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IOAT reads as 121°
96-121°C (IOAT)
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PMU goes offline
+121°C (IOAT)
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ignition and boost pump deactivated during auto start
50% N1
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fuel pressure switch limit, turns on BP
10 psi
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manual motor after aborted start/inverted flight limit
20 seconds
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– normal wing tank capacity
527 lbs
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– collector tank capacity
47 lbs
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usable fuel (through single point refueling system)
1100 lbs
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over wing refueled full fuel load (manually filled)
1200 lbs
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imbalance where FUEL BAL annunciator illuminated & auto balance turns off
30 lbs (for 2 minutes)
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auto fuel balance
20 lbs (30 sec+)
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middle fuel probe
445 (± 50) lbs
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inner fuel probe
308 (± 50) lbs
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collector tank pressurized by transfer jet pumps
1 to 1.5 psi
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pressure in supply line where FUEL PX annunciator illuminated
<10psi
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L or R FUEL LO annunciator illuminated
110 lbs
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starter/generator output
28 VDC (300 amp)
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main (lead-acid) battery output
24 VDC (42A/HR
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aux battery output (30 minutes of emergency power)
24 VDC (5 A/HR)
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minimum generator voltage to charge the battery
25VDC
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minimum battery voltage to connect external power
22 VDC
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normal hydraulic pressure
3000±120 psi
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hydraulic system total capacity (below 1Qt - HYDRO FL LO annunciator)
5 Qt
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hydraulic reservoir capacity
0.6 gal
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min hydraulic pressure to operate NW steering, gear&doors, flaps, speed brake
1800 psi
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– hydro pressure display goes from white to amber
<1800 psi
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– emergency accumulator pressure where EHYD PX LO annunciator illum.
<2400±150
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– fuel pressure supplied by engine driven low pressure fuel pump
40 psi
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– fuel pressure supplied by engine driven high pressure fuel pump
700 psi
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– max hydraulic volume allowed past the hydraulic fuse
45 cubic inches
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– hydraulic pressure relief valve opens
3250 to 3500 psi
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– EHYD PX LO annunciator illuminates
2400 (± 150) psi
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– hydro system fluid level where HYDR FL LO annunciator illuminates
1 qt
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– normal gear extension/retraction time
6 seconds
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gear warning horn sounds if A/S is below 120
87% N1
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flap deflection in TO
23°
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– flap deflection in LDG
50°
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speed brake deflection when deployed
70°
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TAD active with no weight on wheels
80 knots
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Below this Mach is blanked on A/S ind
0.40 Mach
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– on speed AOA
10 to 11 AOA
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Optimum approach speed decrease rate
1 knot/100 lbs
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– Optimum max range AOA altitude
25,000’ MSL
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Pre-stall stick shaker
5 - 10 kts (15.5 units)
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windscreen designed for bird strike of
4 lbs @ 270 KIAS
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– CFS handle lanyard length
10 ft
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Ejection seat limits
0’/0 KIAS to 35,000’/370 KIAS
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Automatic seat/pilot separation
14,000’ to 16,000’ MSL
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ISS BOTH rear seat ejection delay
0.37 seconds
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– emergency oxygen supply lasts
10 min
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Bleed air inflow prevented with A/C clutch engaged
<7500’ MSL
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automatically maintained until 18,069’ MSL (3.6 + 0.1 psid)
8000’ cockpit P/A
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– CKPT ALT annunciator illuminated
19,000’ cockpit P/A
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– CKPT PX annunciator illuminated
3.9 + 0.1 psid
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– DUCT TEMP annunciator illuminated
300° F
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– UHF/VHF memory
20 frequencies
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– RMU cursor automatically reverts to UHF field
20 seconds
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– NAV memory
10 frequencies
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ELT transmission limit (battery limited)
50 hours
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– EADI declutters
> +30°/-20° pitch or 65° roll
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– Full EADI presentation reappears after unusual attitude
< +25°/-15° pitch and 60° roll
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– NACWS display time limit after trigger is released
7 seconds
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– NACWS landing mode
1.5 NM range
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NACWS vertical separation alert (enroute mode)
± 2700’
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– NACWS vertical separation alert (landing mode)
± 500’
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NACWS rectangle with digits
Less than or equal to ±300’
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NACWS upward/downward pointing triangle with digits
Less than or equal to ± 400’ to 900’
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– NACWS upward/downward pointing triangle with no digits
Less than or equal to ± 1000’ to 2700’
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– GPS self test indications
34.5 NM, 315 DTK, 130° bearing
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– GPS user defined waypoints
250
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GPS stored flightplans
25
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max waypoints per flight plan
30
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flash prior to turn to next waypoint
20 seconds
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CDI full scale deflection, enroute mode
± 5 NM
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CDI full scale deflection, approach arm
± 1 NM
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CDI full scale deflection, approach active
± 0.3 NM
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FDR annunciator illuminates
80% full
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AUX BAT test light will not illuminate
<50% capacity
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OBOGS TEMP annunciator illuminates
200° F
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NORMAL O2 concentration, sea level to 15,000’ MSL
25% to 70%
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NORMAL O2 concentration, 15,000’ to 31,000’ MSL
45% to 95%
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O2 concentration, MAX selected
95%
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OBOGS warm-up time (after engine start)
3 minutes
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OBOGS FAIL annunciator extinguishes during BIT test
< or = 2 minutes
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– baggage compartment weight limit
80 lbs
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icing inhibitor mix
.5 pint/ 50 gal fuel
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external power requirements
28 to 28.5 VDC/1000 to 1500 Amps
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main gear tire pressure
225 ± 5 psi
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nose wheel tire pressure
120 ± 5 psi
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