TSA lim. Engine, APU Flashcards

1
Q

Engine Model

A

AE3007A1 (LR)

AE3007A1E (XR)

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2
Q

Engine: MIN Oil Temp. (LR)

A

21 C

For start is -40C for oil lubrication specified by MIL-L-23699D

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3
Q

Engine: Min Oil Pressure Below 88% N2

A

34 psi

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4
Q

Engine: Max Oil Pressure Below 88% N2

A

110 psi

(2) May be exceeded during start if oil temp is below 21 C. Engine must remain idle until oil press is less than 110 psi
(7) In Amber range 111-115 for Max of 5 min, 116 -155 for Max of 2 min, Total max time above 110 psi is 5 Min.

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5
Q

Engine: Max Oil Pressure At or Above 88%N2

A

110 psi

(7) In Amber range 111-115 for Max of 5 min, 116 -155 for Max of 2 min, Total max time above 110 psi is 5 Min.

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6
Q

APU: Max Operational Alt

A

37,000 ft

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7
Q

APU: Max temp. for Start ( T-62T-40C11)

A

884° C

(1) May be exceeded up to 925 C Above 25,000ft during 10 sec

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8
Q

APU: Max temp. for start (T-62T-40C14 )

A

884° C

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9
Q

APU: Max continuous temp.

A

680° C

(6) The APU EGT may be exceeded up to 717 C for 5 min Max.

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10
Q

APU: Max Altitude for Start

A

30,000 ft

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11
Q

APU Starter Limits

- cooling period between each starting attemp:

A

Between 3 consec attemps - 1 min OFF

Between 2 series of 3 con. Attemps -30min OFF

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12
Q

Vibration in amber range…?

A

Below 2.5 IPS is time limited to 5 min during takeoff or go-around phases or 10 sec during the remained of the flight phases

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13
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

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14
Q

Engine Cool-Down

A

The engine must run for at least 1 minute at idle or taxi thrust before shut-down

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15
Q

N1 maximum

A

100%

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16
Q

Engine Max ITT Temp for Start (all models)

A

800° C

17
Q

Max ITT Temp for Take-Off (LR)

A

948° (Take-off thrust is time limited to 5min)

18
Q

Max ITT Continuous temp (LR, XR)

A

901° C (LR)

935° C (XR)

19
Q

Max ITT Temp All modes (XR)

A

992° C. Temps between 971° C and 992° C are time limited to 90 sec. 970° C Is time limited to 5min.

20
Q

Minimum Oil pressure at or above 88%N2 (LR)

A

50 psi. While this is an abnormal condition, Operations between 50 and 34 psi is permitted during take-off and go-around phases

21
Q

Minimum Oil pressure at or above 88%N2 (XR)

A

48 psi. While this is an abnormal condition, Operations between 48 and 34 psi is permitted during take-off and go-around phases

22
Q

APU max amps above FL300

A

300 amps

23
Q

Engine min oil Temp (XR)

A

21 C
• For start is -40°C for oil lubrication specified by MIL-L-23699D
• and -54°C for lubrication oil specified by MIL-L-7808K

24
Q

Engine Starter Limits

A

On Ground:
Starting or Dry motoring: up to 5min on, 5 min off
1st - 4th Cycles…… 1 min ON, 1 min OFF
Following Cycles….. 1 min ON, 5 min OFF

In Flight:
Max Continuous Operating time…. 5 min ON

25
Q

Minimum battery temp for APU start is?

A

-20°C

26
Q

Engine Max Oil Temp (all models)

A

126°C