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Saab 2000 > Limitations > Flashcards

Limitations Flashcards

1
Q

Pressure Alt Limits

A

-1000 to 8000

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2
Q

Max Operating Alt (with & without RVSM)

A

31,000 with 28,000 without

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3
Q

Max Runway Slope

A

-2% to +2%

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4
Q

Takeoff from wet/contaminated runways

A

Check AFM 5-10/5-11

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5
Q

%MAC to prevent tail tipping

A

Forward of 50% MAC or use tail stand

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6
Q

Max Crosswind Component (With and without MOD.)

A

With: 40 KTS (AFM 5-2)
Without: 26 KTS

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7
Q

Flap Speeds (Company/Saab)

A

7: 180/190
15: 175/185
20: 170/180
35: 155/165

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8
Q

Va/Vra

A

205

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9
Q

Max Wiper Speed

A

190

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10
Q

Load Factor Limits (Flaps Retracted/Extended)

A

Retracted: +2.5 to -1.0 G
Extended: +2.0 to 0.0 G

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11
Q

Zero Fuel Weight (MZFW)

A

44,090 LBS

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12
Q

Max Taxi Weight (MTW)

A

51,140 LBS

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13
Q

Max Takeoff Weight (MTOW)

A

50,700 LBS

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14
Q

Max Landing Weight (MLW)

A

48,500 LBS

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15
Q

VMO/MMO

A

270 KIAS/.062 MACH

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16
Q

Max Landing Gear Speeds

VLOR

A

VLOR: 175

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17
Q

Max Landing Gear Speeds

VLOE

A

VLOE: 220

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18
Q

Max Landing Gear Speeds

VLOEE (Max/Min)

A

VLOEE:220 (150 MIN.)

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19
Q

Max Landing Gear Speeds

VLE

A

VLE: 220

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20
Q

Max Tailwind Component (PA -1000 to 6000 ft) (>6000)

A

-1000 to 6000 ft: 15kt
>6000 ft: 10kt

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21
Q

APR Operation must be…

A

Off for landing

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22
Q

APU Altitude Limit

A

25,000 ft unless emergency
(above 20,000 feet repeated starts may be required)

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23
Q

APU Normal Temp Limits

A

Normal: Steady State: 720c, Starting: 1030c

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24
Q

APU Emergency Temp Limits

A

Emergency: Steady State: 845c, Starting: 1180c

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25
Q

APU in Flight Start Attempts

A

Consecutive in flight attempts limited to 3 in succession, with 30 sec between attempts.

After 3 attempts must allow 5 min rest before next set of 3.

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26
Q

Hydraulic Ground Operation Temp/Time Limit without MOD 5448

A

Without Mod 5448 30 min at ambient temps warmer than +36c

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27
Q

Hydraulic System Capacities (3)

A
  1. Left System: 19L
  2. Right System: 24.5 L
  3. Center System: 2.3 L
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28
Q

Fuel Quantity Limits with mod 5129

A

9385 LBS=1402 GAL

29
Q

Fuel Quantity Limits Without mod 5129

A

9370 LBS=1400 GAL

30
Q

Max Allowable Fuel Imbalance

A

300 LBS

31
Q

Jet A Temp Operating Limits
(Straight Jet)

A

Jet A: -37 to 43c up to 31,000

32
Q

Jet A1, JP5, JP8 Fuel Temp Limits

A

-43 to 43c up to 31000

33
Q

CIS Fuel Minimum Temp

A

CIS Fuels min temp -40

34
Q

CIS Fuel Additive Limits

Anti-Icing Liquid “I”

A

Anti-Icing Liquid “I”: 0.10 to 0.15% by volume.

35
Q

CIS Fuel Additive Limits

“Lubricity DNK”

A

Lubricity DNK: Concentration 0.002% to 0.004% by weight

36
Q

CIS Fuel Additive Limits

Antioxidant Ionol (Antidol-1, Topanol-0)

A

Concetration shall be 0.003 to 0.004 by weight

37
Q

Anti-ice additives MIL-27686E or MIL 85470B

A

Concentration 0.06 to 0.15% max by volume

38
Q

Do Not Operate Two Packs with…

A

Bleed air from one engine

39
Q

AMB air must not be selected on when

A

A) ECS packs are on
B) ECS packs are off and the cabin pressure differential exceeds 0.5 psi

40
Q

Pressurization Safety Valve Opens at

A

7.5 PSI

41
Q

CAB DIFF PRESS HI warning comes on at

A

7.3 PSI

42
Q

CAB ALT HI

A

Cabin altitude >9600

43
Q

Min Main Battery Temp for Takeoff

A

-20C

44
Q

Generator Reset Attempts

A

2 per generator

45
Q

Autopilot Minimum Altitudes

A

Takeoff…200 AGL
Cruise…500 AGL
Couples Approach CAT 1…100 AGL
Non-Coupled Approach…130 AGL

46
Q

Only Authorized Climb Mode in ICE

A

IAS

47
Q

GA Mode in Takeoff

A

is not authorized

48
Q

Backcourse Mode

A

Is not authorized

49
Q

The aircraft must be trimmed

A

in roll before the autopilot is engaged

50
Q

Before final approach, after initial flap extension

A

disengage the autopilot trim the aircraft in roll and reengage the autopilot

51
Q

Radar Limitations

A

180 feet of other aircraft being fueled or personnel within 90 feet of beam area

52
Q

Do not exercise the pedals and/or control column heavily on the ground with…

A

the left engine off and L HYD STBY pump running at speeds below 40 KIAS

53
Q

Water/Waste System

A

Toilet prefilled with 8L (2 GAL of water and 60G (2.0 oz) of chemical (blue juice).

54
Q

RVSM Equipment Requirements

A

-Two ADC’s
-Autopilot
-Altitude Alerting System
-One transponder
-Pitot tube heating
-Static pressure shutoff valves must be opened
-Autopilot hold must be used
-Cannot be using STBY altimeter
-TCAS II software version 7.0 or later

55
Q

Engine Ground Running at High Power

A

Do not run engines at PLA >60 degrees in any mode, with static if the wind speed is >10kts unless the aircraft is pointed into the wind +/- 45 degrees.

56
Q

Backing Limitations

A

-Steering wheel must be depressed the entire time

-Nose wheel steering in reverse 45 degrees

57
Q

Max braking with anti skid inoperative

A

40 kts

58
Q

Antiskid Limitations

A

-must be on for takeoff and landing unless corrections have been made for it being inoperative

59
Q

Max tire speed

A

182 kts

60
Q

Aquaplaning speed

A

103

61
Q

Max structural temp

A

+80C

62
Q

Max operating temp with and without mod

A

ISA+35/ISA+25

63
Q

Steep Approach Operaton

A

-Requires MOD 5668
-Deliberate OEI approaches not allowed
-Autopilot use below 200 AGL is not authorized
-Max crosswind coupled is 22 kts
-CATII not authorized
-Max tailwind 5 kts

64
Q

Fuel Quantity Indicators

A

Fuel remaining in the tanks when fuel quantity indicators indicate zero in flight cannot be safely used in all flight conditions

Max error in quantity indication is +/-75% of full scale and +/-2% of indication

65
Q

Ice Detector

A

Cannot be used as a cue for switching on ENG/PROP.

66
Q

De-Ice Boot Temp Limit

A

-40C

67
Q

Icing Conditions

A

Exist when OAT on the ground for takeoff or SAT in flight is +5 degrees C or below and visible moisture of any kind exist. (Clouds, fog with vis of 1 mile or less, rain, snow, sleet, ice crystals).

Icing conditions also exist when the OAT on the ground and for takeoff is +5C or below when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on nacelles, props, or engine sensor probes.

68
Q

Cargo Fire Protection

A

-Basic: 40 Min (FRE)
-MOD 5320: 60 Min
-MOD 5320 & 5575: 90 Min

Saab 2000 (7 decks)

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