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97 Cards in this Set
- Front
- Back
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
|
> +30/-20 pitch
or 65 roll |
|
Full EADI presentation reappears after unusual attitude
|
< +25/-15 pitch
and 60 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, 130 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
|