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CJ1 525 > Operating Limitations > Flashcards

Operating Limitations Flashcards

1
Q

Maximum design ramp weight

A

10,700 lbs

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2
Q

Maximum design takeoff weight

A

10,600 lb

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3
Q

Maximum design Landing weight

A

9,800 lbs

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4
Q

Maximum design zero fuel weight

A

8,400 lbs

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5
Q

Take off weight is limited by the most restrictive of the following

A

Maximum certified takeoff weight
Maximum take off weight permitted by climb
Take off field length

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6
Q

Landing weight is limited by the most restrictive of the following

A

Maximum certified Landing weight
Maximum Landing weight permitted by climb requirements
Landing distance

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7
Q

The Cessna cj1 525 is powered by what type of engines

A

Williams International fj44-1a turbo fan

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8
Q

Minimum oil pressure at startup

A

25 psi minimum

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9
Q

What is the maximum allowable cold day start oil pressure

A

100 PSI for 5 minutes with oil pressure returning to normal range

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10
Q

The engine should not be operated above _____ %N2 until oil temp is above ____ °C.

A

85%N2. 10°C

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11
Q

Maximum ITT temperature at idle

A

620° C @ 56.2 +/- 1.3 %N2

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12
Q

What is the maximum ITT temperature at takeoff power?

A

820° C @ 99.3%N2

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13
Q

What is the maximum continuous ITT temperature?

A

796° C @ 99.3%N2

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14
Q

What is the oil temperature range for starting?

A

-40 to 121° C

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15
Q

What is the oil temperature range for idle?

A

-40 to 121 ° C

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16
Q

What is the oil temperature range for takeoff?

A

10 to 121° C

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17
Q

What is the oil temperature range during maximum continuous power?

A

10 to 121° C

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18
Q

Take off power thrust limit

A

Take off thrust 5 minute limit for engine life to TBO. Performance data, including Vmca in section 4, is based on the use of takeoff thrust setting.

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19
Q

What is the minimum oil pressure at idle?

A

35 PSI minimum

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20
Q

What is normal oil pressure range during takeoff power?

A

45-90 PSI

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21
Q

Minimum oil pressure is ____ PSIG when operating above 80% N2 and ____ PSIG when operating below 80% N2.

A

45 above. 35 below.

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22
Q

Engine start maximum Tailwind component

A

10 knots

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23
Q

Engine start maximum crosswind component

A

12 knots

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24
Q

Engine start maximum time to light off

A

10 seconds

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25
Q

Minimum ambient temperature for battery start

A

-18° C

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26
Q

Maximum temperature for engine start

A

39° C or 102° F

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27
Q

Maximum airport elevation for battery start

A

10,000 ft

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28
Q

Maximum airport elevation for ground external power start

A

14,000 ft

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29
Q

Minimum battery voltage for battery start

A

24 volts DC

30
Q

Minimum / maximum external power current capacity for start

A

28 volts DC at 800 to 1100 amps

31
Q

Engine power reduction at high altitude

A

Left and right ignition must be selected to “ON” prior to reducing power less than 90% N2 at or above flight level 350. Ignition may be returned to “Norm” after engines have stabilized at reduced power setting.

32
Q

Starter cycle limitations

A

Three engine starts per 30 minutes with a 60 second rest period between Cycles

33
Q

Use of an external power source with voltage in excess of ____ VDC or current in excess of ____ amps may damage the starter.

A

Voltage in excess of 29 volts or current in excess of 1100 amps may damage the starter.

34
Q

Battery cycle limitations

A

Three engine starts per hour. Three generator assisted cross starts are equal to one battery start. If an external power unit is used for start, no battery cycle is counted.

35
Q

Ground operation generator current limitations

A

300 amps for less than 15 minutes. 250 amps for 15 minutes or more.

36
Q

Limit for ground operation of pitot/static heat

A

2 minutes

37
Q

The maximum permissible oil consumption during normal operation is

A

.023 gallons per hour during normal operation

38
Q

Maximum speed Mmo above 30,500 ft

A

0.710 Mach indicated

39
Q

Maximum speed Vmo between sea level and 30,500 ft

A

263 knots indicated airspeed

40
Q

Maximum flap extended speed for takeoff and approach position 15°

A

200 knots indicated airspeed

41
Q

Maximum flap extended speed full flaps landing position 35°

A

161 knots indicated airspeed

42
Q

Maximum flap extended speed ground flaps 60° ( prohibited in flight / failed to 60°).

A

140 knots indicated airspeed

43
Q

Maximum landing gear extended speed VLE

A

186 knots

44
Q

Maximum landing gear operating speed VLO

A

186 knots

45
Q

Maximum speed brake operation speed VSB

A

No Limit

46
Q

Maximum altitude limit for takeoff

A

14,000 ft

47
Q

Maximum Tailwind component for takeoff

A

10 knots

48
Q

Maximum ambient temperature for takeoff

A

39° C or 102° F

49
Q

Minimum ambient temperature for takeoff

A

-53° C

50
Q

What is the maximum intentional asymmetric fuel differential

A

200 lb

51
Q

What is the maximum demonstrated asymmetric fuel differential in an emergency

A

600 lb

52
Q

Maximum autopilot operation speed

A

263 knots or 0.710 Mach

53
Q

Speed brakes must be retracted prior to ___ ft on landing.

A

50 ft

54
Q

Maximum Tire ground speed

A

165 knots

55
Q

Maximum operating altitude

A

41,000 ft

56
Q

Maximum enroute generator load

A

300 amps up to 41,000 ft

57
Q

Load Factor range with flaps zero

A

-1.52 to +3.6 G’s at 10,600 lb

58
Q

Load factor with flaps take off and approach to land position between 15 and 35°

A

0.0 to +2.0 G’s at 10,600 lb

59
Q

Normal cabin pressurization limitations

A

0.0 to 8.6 PSI differential

60
Q

Autopilot minimum engage height

A

250 ft AGL

61
Q

Autopilot minimum use height during Cruise

A

1,000 ft AGL

62
Q

Autopilot minimum use height during non-precision approach

A

250 ft AGL

63
Q

Autopilot minimum use height during Precision approach

A

71 ft AGL

64
Q

Continuous use of the supplemental oxygen system above ____ feet cabin altitude with passengers or above _____ feet cabin altitude crew only is prohibited.

A

Above 25,000 ft with passengers or above 41,000 ft crew only, continuous use of supplemental oxygen system is prohibited.

65
Q

Icing conditions exist when indicated Ram air temperature in Flight is ____ or below and visible moisture in any form is present.

A

+ 10° C or below with visible moisture present - icing conditions exist

66
Q

Minimum engine N2 speed for effective anti-icing

A

70% N2

67
Q

Minimum temperature for operating tail de-icing boots

A

-35° C

68
Q

Minimum AirSpeed for sustained flight in icing conditions except for approach and Landing

A

160 kts

69
Q

For inoperative anti-skid

A

Multiply takeoff field length and Landing Distance by 1.4

70
Q

Vmca

A

92 knots

71
Q

Vmcg (on ground)

A

93 knots

72
Q

Maximum demonstrated crosswind landing

A

21 knots

CJ1 525 (5 decks)

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