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52 Cards in this Set

  • Front
  • Back

Normal flight

65-110 KIAS

TALS automatic abort

Airspeed > 78 KIAS or < 52 KIAS for 2 seconds

Alert Displayed (display turns yellow)

55 KIAS

Maneuvering speed

70 KIAS

Max reported airspeed (descent)

90 KIAS

Operating temp range

-20c degrees to 50c degrees

Rain limit

.2 inches per hour for 15 mins

Relative humidity

95% non condensing

Snow and ice

Operations prohibited

Minimum safe FTS deploy

500 ft AGL

Minimum altitude

ELOS

Service ceiling

16,000 ft MSL

Max takeoff altitude

10,500 DA

Bus voltage, engine running

29+/- 1VDC

Allowable fluctuation, engine running on ground

+/-3 initial, +/- 1 prior to launch

Battery fail

<19V or <20 min battery life remaining


21 VDC=can’t land


19 VDC=erratic


18 VDC=FTSX

Climb law

62 KIAS fixed

Descent law

70-90 KIAS (AO selectable)

Max flight tome

9 hrs

Max operational rpm

8,000 RPMs for 2 minutes

Max continuous RPM

7800 RPM

Max continuous cruise RPM

7500 RPM

Minimum in flight RPM

3800 RPM

Warm-up RPM and RAT (of RAIN equipped)

4500 RPM (80c degrees)

Warm up RPM and RAT (if FAFS equipped)

4500 RPM (64c degrees)

Min static full throttle rpm ax static full throttle rom

6300 rpm

Max static full throttle rom

7200 rpm

Static idle rpm (payload and IFF on)

3720 rpm +/- 120

Duration at max rpm on ground

10 seconds

RAT operating range

64-175 degrees C

Rat operating range (if FAFS equipped)

50-175 degrees C

CHT operating range

80-260 degrees C

Max continuous CHT

170 degrees C

Max continuous CHT

250 degrees C

Max RAT at takeoff

160 degrees C

Caution range RAT

170-175 degrees C for 2 mins during initial climb

Caution range CHT

250-260 degrees C for 2 minutes during initial climb

Type fuel

100 low lead AV gas (OAT) oil mix if temp is -5 degrees C

Min landing fuel

10L

Roll in knobs

+/- 20 AOB

Commanded roll tolerance

+/- 6 AOB

Roll in auto land

+/- 25 AOB

Pitch angle

20 degrees, -15 degrees sustained pitch down >10 degrees during descent prohibited

Max gross weight (takeoff)

Refer to LAU pre charge pressure chart

Aircraft maximum weight

467 lbs at 10,500 DA

Surface Headwind/Crosswind component (max)

20 kts steady, 25 kts gusting

Takeoff tailwind component (max)

Refer to launcher pre charge pressure chart

Landing tailwind component > 8000 ft DA

0 kt at surface

Landing tailwind component (max)

5kts at surface prior to dp

Prohibited maneuver 1

Intentional maneuvers involving abrupt changes in aircraft attitude and abnormal acceleration not necessary for normal flight

Prohibited maneuver 2

Flight into forecast moderate to severe, or any known level of icing is prohibited

Prohibited maneuver 3

Flight into known or forecast severe or extreme turbulence is prohibited