Powerplant

Question 1

Min oil temp for start

Answer 1

-40˚C

Question 2

Max oil inlet temp

Answer 2

Continuous - 105˚C

15 min - 120˚C

Question 3

Min oil temp to move power levers

Answer 3

-30˚C

Question 4

Min oil pressure at idle

Answer 4

16 PSI

Question 5

Min engine fuel temp

Answer 5

-40˚C

Question 6

Max engine fuel temp

Answer 6

Continuous - 90˚C

15 min - 120˚C

Question 7

Min oil press for takeoff

Answer 7

30 PSI (@ TO Pwr)

Question 8

Minimum oil press to complete flight

Answer 8

97.5% HP (Max Cont) - 25 PSI
92% HP - 22 PSI
84% HP - 19 PSI
76% HP - 16 PSI

Question 9

Acceptable Takeoff Power EPR Range

Answer 9

TO EPR ≤ .01 of rated EPR

TO EPR ≤ .05 of rated EPR

Question 10

Airstart Ignition Duty Cycle

Answer 10

W/ASC 304 - NONE
W/O ASC 304 - 5 min on / 30 min off
30 sec on / 30 sec off - No Limitation

Question 11

Max ground start TGT

Answer 11

700˚C Momentary (2 sec)

Question 12

Max airstart TGT

Answer 12

780˚C Momentary (2 sec)

Question 13

Max Takeoff / Go-Around Power
LP
HP
TGT
Time

Answer 13

LP: 95.5%
HP: 99.7%
TGT: 716-800˚C

5 min / 10 min single engine

Question 14

Max Continuous Power
LP
HP
TGT

Answer 14

• LP: 95.5%
• HP: 97.5%
• TGT: 715˚C

Question 15

Minimum Approach Idle

Answer 15

LP: —-
HP: 67%
TGT: —-

Question 16

Minimum Ground Idle

Answer 16

LP: —-
HP: 46.6%
TGT: —-

Question 17

Max Reverse

Answer 17

LP: —-
HP: 88%
TGT: 695˚C

No time limit
1 min every 30 min if no ASC 166

Question 18

Max Overspeed

Answer 18

LP: 98.3%
HP: 102.6%
TGT: —-

20 sec

Question 19

Max crosswind for engine start

Answer 19

30 Kt

Question 20

Max TGT to initiate engine start

Answer 20

150˚C

Question 21

Max tailwind for engine start

Answer 21

24 Kt

Question 22

“OIL PRESS LOW” CAS message illuminates when?

Answer 22

Oil press < 16 PSI

Question 23

Engine Starter Duty Cycle

Answer 23

30 sec ON / 30 sec OFF
30 sec ON / 30 sec OFF
30 sec ON / 15 min OFF

Question 24

Thrust Rating

Answer 24

13,850 #

Question 25

Max altitude for guaranteed start

Answer 25

25,000 MSL

Question 26

Airstart Envelope

Answer 26

≤ 25,000 MSL | 200 - 324 KCAS

Question 27

Minimum altitude for autothrottles

Answer 27

Can be used for TO Landing: 50' AGL

Question 28

Automatic Idle Speeds (4)

Answer 28

Ground Idle: 46.6% HP Flight Idle: 48% HP Above 15,000': 49.5-78% HP (up to FL450) Approach: 67%

Question 29

Powerplant Make and Model Number

Answer 29

Rolls Royce Tay Mk 611-8

Question 30

What automatic shutdown protection feature is provided by the TAY 611-8?

Answer 30

LP shaft failure protection will shut the engine down and will lock the HP fuel cock in the OPEN position.

Question 31

What is the guaranteed minimum thrust rating on the TAY 611-8 engine?

Answer 31

13,850# @ 30º C

Question 32

What is indicated by illumination of the “ENG IDLE” light on the ground?

Answer 32

Engine idle is at approach idle (67% HP RPM)

Question 33

The amber EICAS indication identified as “SVO” should extinguish by what HP % RPM?

Answer 33

44.5% HP

Question 34

What does the green EICAS indication “IGN” indicate?

Answer 34

The ignition relay is energized

Question 35

What is the maximum altitude and the airspeed envelope for a guaranteed engine air start?

Answer 35

- 25,000 feet | - 200 - 324 KIAS

Question 36

During an auto throttle takeoff, when does the auto throttle system go to EPR HOLD mode?

Answer 36

At 60 knots indicated airspeed, regardless of EPR setting

Question 37

When does the red “OIL PRESS LOW” CAS message illuminate?

Answer 37

When the oil pressure < than 16 psi

Question 38

What are the autothrottle engagement requirements? (4)

Answer 38

- Isolation Valve Closed - Autothrottles Armed - TO / GA Mode Selected - EPR ≥ 1.17

Question 39

What conditions (9) would cause the autothrottles to disengage?

Answer 39

``` Autothrottle Arm Switch Selection of Opposite AT Computer Authrottle Disengage Switches Autothrottle Engage Switches (second push) Manual Override Isolation Valve Open Alternate Flap Selection LP Split > 20% Either HP < 41% ```

Question 40

If an engine fails after V1 during takeoff, when are the flaps retracted?

Answer 40

At V2 + 10 and 1500 feet AGL minimum

Question 41

On takeoff, with autothrottles engaged and FLCH selected, when is the power set to climb power?

Answer 41

At 400 feet AGL minimum altitude

Question 42

What is the limitation concerning the use of the engine starter?

Answer 42

- Continued use of the starter is limited to 3 crank cycles, with a maximum of 30 sec per cycle - Delay 3 minutes between start attempts - After 3 cycles, delay use of starter for at least 15 minutes

Question 43

What is the proper procedure if the green “IGN” mnemonic does not illuminate on the EICAS during an engine start?

Answer 43

The start may be salvaged by selecting AIR START IGN to ON prior to opening the HP fuel cock

Question 44

When performing an engine start during high tail wind conditions, what is an indication that the LP rotation is positive?

Answer 44

HP rotation stabilized

Question 45

During an engine start, when should engine ignition (light-off) occur?

Answer 45

Within 10 seconds after selecting the HP fuel cock to OPEN

Question 46

What is the correct procedure to follow if the start valve has not closed by the time that engine idle speed (46.6%) is reached during an engine start?

Answer 46

Accomplish the start valve failure checklist in the QRH

Question 47

If during an engine start, the EVM system momentarily displays values above the alert level (0.60), what action is required?

Answer 47

No action is required, this normally occurs on the first start of the day

Question 48

When does the “HOLD” mode of autothrottle operation occur?

Answer 48

- On takeoff, at approximately 60 knots until another vertical mode is selected after attaining 400 feet AGL. - Above 400 ft the servos are repowered and the power levers move to a thrust rating appropriate to the vertical mode selected on the guidance panel

Question 49

When is the “START” position of the HP fuel cocks used?

Answer 49

This position is never used for flight crew operations

Question 50

What is the time limitation on the air start ignition system?

Answer 50

- 30 sec on, 30 sec off OR 5 min on, 30 min off | - There is no time limitation with ASC 304 installed

Question 51

When should you check the oil level?

Answer 51

Within 30 minutes of engine shutdown at termination of the last flight of the day or at intervals not exceeding eleven (11.0) hours cumulative flight time.