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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