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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
APU in Flight Start Attempts
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.
26
Hydraulic Ground Operation Temp/Time Limit without MOD 5448
Without Mod 5448 30 min at ambient temps warmer than +36c
27
Hydraulic System Capacities (3)
1. Left System: 19L 2. Right System: 24.5 L 3. Center System: 2.3 L
28
Fuel Quantity Limits with mod 5129
9385 LBS=1402 GAL
29
Fuel Quantity Limits Without mod 5129
9370 LBS=1400 GAL
30
Max Allowable Fuel Imbalance
300 LBS
31
Jet A Temp Operating Limits (Straight Jet)
Jet A: -37 to 43c up to 31,000
32
Jet A1, JP5, JP8 Fuel Temp Limits
-43 to 43c up to 31000
33
CIS Fuel Minimum Temp
CIS Fuels min temp -40
34
CIS Fuel Additive Limits Anti-Icing Liquid "I"
Anti-Icing Liquid "I": 0.10 to 0.15% by volume.
35
CIS Fuel Additive Limits "Lubricity DNK"
Lubricity DNK: Concentration 0.002% to 0.004% by weight
36
CIS Fuel Additive Limits Antioxidant Ionol (Antidol-1, Topanol-0)
Concetration shall be 0.003 to 0.004 by weight
37
Anti-ice additives MIL-27686E or MIL 85470B
Concentration 0.06 to 0.15% max by volume
38
Do Not Operate Two Packs with...
Bleed air from one engine
39
AMB air must not be selected on when
A) ECS packs are on B) ECS packs are off and the cabin pressure differential exceeds 0.5 psi
40
Pressurization Safety Valve Opens at
7.5 PSI
41
CAB DIFF PRESS HI warning comes on at
7.3 PSI
42
CAB ALT HI
Cabin altitude >9600
43
Min Main Battery Temp for Takeoff
-20C
44
Generator Reset Attempts
2 per generator
45
Autopilot Minimum Altitudes
Takeoff...200 AGL Cruise...500 AGL Couples Approach CAT 1...100 AGL Non-Coupled Approach...130 AGL
46
Only Authorized Climb Mode in ICE
IAS
47
GA Mode in Takeoff
is not authorized
48
Backcourse Mode
Is not authorized
49
The aircraft must be trimmed
in roll before the autopilot is engaged
50
Before final approach, after initial flap extension
disengage the autopilot trim the aircraft in roll and reengage the autopilot
51
Radar Limitations
180 feet of other aircraft being fueled or personnel within 90 feet of beam area
52
Do not exercise the pedals and/or control column heavily on the ground with...
the left engine off and L HYD STBY pump running at speeds below 40 KIAS
53
Water/Waste System
Toilet prefilled with 8L (2 GAL of water and 60G (2.0 oz) of chemical (blue juice).
54
RVSM Equipment Requirements
-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
Engine Ground Running at High Power
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
Backing Limitations
-Steering wheel must be depressed the entire time -Nose wheel steering in reverse 45 degrees
57
Max braking with anti skid inoperative
40 kts
58
Antiskid Limitations
-must be on for takeoff and landing unless corrections have been made for it being inoperative
59
Max tire speed
182 kts
60
Aquaplaning speed
103
61
Max structural temp
+80C
62
Max operating temp with and without mod
ISA+35/ISA+25
63
Steep Approach Operaton
-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
Fuel Quantity Indicators
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
Ice Detector
Cannot be used as a cue for switching on ENG/PROP.
66
De-Ice Boot Temp Limit
-40C
67
Icing Conditions
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
Cargo Fire Protection
-Basic: 40 Min (FRE) -MOD 5320: 60 Min -MOD 5320 & 5575: 90 Min

Saab 2000 (7 decks)

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