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Trans States Airlines 7/17 > TSA EMB 145 Memory Limitations > Flashcards

TSA EMB 145 Memory Limitations Flashcards

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1
Q

Maximum Altitude

A

37,000 Ft.

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2
Q

Maximum Operating Temperature

A

ISA + 35*C

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3
Q

TAT limit in cruise above 25,000 Ft.

A

-45*C

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4
Q

Landing Gear: Vlor

A

200 KIAS

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5
Q

Landing Gear: Vloe (Extension)

A

250 KIAS

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6
Q

Landing Gear: Vloe (Extended)

A

250 KIAS

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7
Q

Maximum Operating: Vmo/Mmo

A

0 to 8,000 ft. — 250 KIAS
10,000 ft to 26,000 ft — 320 KIAS
26,000 ft to 37,000 ft — 0.78 Mach

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8
Q

Maneuvering Va

A

200 KIAS

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9
Q

Flap Extended Vfe

A

Flaps 9 — 250 KIAS
Flaps 22 — 200 KIAS
Flaps 45 — 145 KIAS

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10
Q

Maximum Tailwind for T/O and Landing

A

10 Kts.

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11
Q

Direct Vision Window

A

Max to Remove: 140 KIAS (AFM)

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12
Q

Windshield Wiper

A

Max for Operation: 170 KIAS (AFM)

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13
Q

Turbulent Air Penetration (AFM)

A

At or below 10,000’ — 200 KIAS

Above 10,000’ — 250 KIAS/0.63 M lower value

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14
Q

Maximum Aft Cargo Weight

A

2,646 lbs.

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15
Q

Maximum Altitude to Extend Flaps

A

20,000 ft.

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16
Q

Maximum Airspeed after Take Off/During Climb without Re-trimming

A

160 KIAS

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17
Q

Maximum Recommended Crosswind

Dry Runway

A

30 kts including gusts

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18
Q

Maximum Recommended Crosswind

Wet Runway

A

30 kts including gusts

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19
Q

Maximum Recommended Crosswind

Compacted Snow

A

25 kts including gusts

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20
Q

Maximum Recommended Crosswind

Standing Water or Slush

A

20 kts including gusts

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21
Q

Maximum Recommended Crosswind

Ice (no melting)

A

10 kts including gusts

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22
Q

Maximum Temp for Anti-Icing Operation

A

10*C

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23
Q

Minimum Temp for Manual Anti-Icing Operation

A

-40*C

24
Q

Icing Conditions Holding Configuration

A

Landing Gear — UP
Flaps — UP
Min. Airspeed — 200 KIAS

25
Q

Icing Conditions Single Engine or Single Bleed

A

Max. Altitude 15,000 ft.

26
Q

Fuel: Maximum Imbalance

A

800 lbs.

27
Q

Maximum Usable Quantity each Tank

A

Main Tanks: 5,717 lbs. (844.9 US gal.)

28
Q

APU Altitude for start (c11 and c14)

A

Maximum 30,000 ft

29
Q

APU Operational Altitude (c11 and c14)

A

Maximum 37,000 ft

30
Q

APU Starter Limits

A

Cooling period between each starting attempt:
Between three consecutive attempts — 1 minute off
Between 2 series of 3 consecutive attempts — 30 minutes off

31
Q

Bleed/Pack Condition

Maximum operating altitude when one bleed or one pack is closed…

A

25,000 ft (AFM)

32
Q

Bleed/Pack Condition
When operating with APU bleed supplying Pack 1 (Eng. 1 bleed -=- closed) and engine 2 supplying Pack 2 (crossbleed closed).
Maximum Operating Altitude

A

37,000 ft (non-AFM)

33
Q

Engine Starter Limits

On Ground:

A

Starting or Dry Motoring…. up to 5 minutes on, 5 minutes off
First to Fourth cycles…. 1 minute on, 1 minute off
Following cycles…. 1 minute on, 5 minutes off

34
Q

Engine Starter Limits

In Flight:

A

Maximum Continuous Operation Time… 5 minutes

35
Q

Continuous OIL Pressure

A

Below 88% N2 …. Min 34 psi Max 110 psi (2)(6)
At or above 88% N2 …. Min 50 psi (7) Max 110 psi (6)

Note(2): May be exceeded during starts if oil temp. is below 21*C. The engine must remain at IDLE until the pressure is less than 110 psi.

Note(6): Operation in oil pressure amber range between 111 and 115 psi is permitted in all operational modes and time limited to 5 minutes, or between 116 and 155 psi in all operational modes time limited to 2 minutes. Total time above 110 psi may not exceed 5 minutes.

Note(7): While this is an abnormal condition, operation between 50 and 34 psi is permitted during takeoff and go around phases.

36
Q

Take off Thrust in the Takeoff Modes is time limited to…

A

5 minutes

37
Q

Continuous Oil Pressure… Note 7

A

While this is an abnormal condition, operation between 50 and 34 psi is permitted during takeoff and go around phases.

38
Q

Engine Warm-Up

A

Prior to take-off, the engines must be allowed to run at low thrust to stabilize the engine temperatures before take-off thrust is adjusted. After start, the engines must run at idle or taxi thrust during at least 4 minutes for cold engines (shut down for more than 90 minutes) or 2 minutes for warm engines. to increase N2 above 83% the engine oil temperature must be at 40*C minimum. In lieu of this limit, it is acceptable to run the engine for at least 8 minutes.

39
Q

Engine Cool-Down

A

The engines must run for at least 1 minute at idle or take thrust before shut-down.

40
Q

Autopilot - CAT I

Minimum Altitude Coupled to ILS

A

200 ft.

41
Q

Autopilot - CAT I

Single-engine Go-around

A

Prohibited

42
Q

Autopilot - CAT II

Minimum Altitude Coupled to ILS

A

50 ft.

43
Q

Autopilot - CAT II

Minimum Decision Height

A

100 ft.

44
Q

Autopilot:

Minimum Engagement Height After Takeoff or Go-Around

A

500 ft.

45
Q

Integrated Standby Instrument System (ISIS)

Minimum duration of ISIS when operating on batteries only:

A

40 minutes

Note: The maximum duration of battery power can be extended to 45 minutes if the Pitot 3 Sensor Heating Button is turned off when not operating in icing conditions.
Note: Airplane must not be moved during power-up initialization. Do not cage attitude in turning flight.

46
Q

CAT II Restrictions

A 
Minimum RVR - 1200'
Max Tailwind - 10 kts.
Max Crosswind - 10 kts.
Max Headwind (non-AFM) - 25 kts.
Single Engine CAT II - Prohibited
47
Q

N1 Maximum

A

100.0%

48
Q

N2 Maximum

A

102.4%

49
Q

ITT Maximums

A

Start — 800C
Takeoff Modes — 948C (5 minute limit)
Continuous — 901*C

50
Q

ENG OIL Temperature

A

Minimum — 21C (3)
Maximum — 126C
Note (3) Minimum oil temperature for starting is -40*C for lubrication oil specified by MIL-L-23699D.

51
Q

Fuel Temperature

A

Minimum — -54*C

Maximum — 52*C

52
Q

Crew Oxygen Requirements

A

1100 psi for 2 Crewmembers

1500 psi for 2 Crewmembers + ACM in Jump Seat

53
Q

Maximum Ramp Weight

A

48,722 lbs.

54
Q

Maximum Take-Off Weight

A

48,501 lbs.

55
Q

Maximum Landing Weight

A

42,549 lbs.

56
Q

Maximum Zero Fuel Weight

A

39,462 lbs.

Trans States Airlines 7/17 (2 decks)

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