Trans States Limitations And Memory Items Notes

Front 1

Unusuable Fuel increases to ___ lbs if any of the associated electric fuel pumps is inoperative

Back 1

365 lbs

Front 2

When performing pressure refueling, the usable fuel quantity in each tank may be reduced to ____ US Gal

Back 2

13.2 US Gal

Front 3

The values have been determined for an adopted fuel density of ______ lb/US GAl

Back 3

6.767

Front 4

APU T-62T-40C11

(1) Start temp may be exceeded up to ____degrees above _____ft. during ___ seconds

Back 4

925 degrees
25,000 ft
10 seconds

Front 5

APU T-62T-40C11

For airplanes post mod SB 145-49-0010 or equipped with equiv. mod. factory incorporated. Min Temp for APU start is ____ up to ______ft.

Back 5

-54 degrees up to 30,000 ft.

Front 6

(3) Minimum battery temperature for APU Start is

Back 6

-20 degrees C

Front 7

(4) Refer to ____________ for other APU related starting limits

Back 7

Fuel tank temperature limitaitons

Front 8

(5) The APU Model T-62T-40C14 will automatically shut down at _______ rotor speed

Back 8

104%

Front 9

(6) The APU EGT May be exceeded up to ____ degrees for __ minutes maximum

Back 9

717 degrees
5 minutes

Front 10

(1) Takeoff Thrust is time limited to __ Minutes

Back 10

5 minutes

Front 11

(2) Oil pressure PSI Below 88% N2 may be exceeded during starts if oil temp. is below ___. The engine must remain at IDLE until the pressure is less than ___ psi

Back 11

21 degrees
110 PSI

Front 12

(3) Minimum oil pressure for starting is __ degrees for lubrication oil specified by MIL-L_23699D

Back 12

-40 degrees

Front 13

(4) Vibration in the amber range below ___ IPS is time limited to __ minutes during the T/O or Go-around phases or __ seconds during the remainder of the flight phases

Back 13

2.5 IPS
5 minutes
10 seconds

Front 14

(5) Any engine ___ or ____ must be monitored and ____ by the crew

Back 14

exceedance or peak, logged

Front 15

(7) Operation in oil pressure amber range between ___ and ___ psi is permitted in all operational modes and time limited to _ mins, or between __ and __ psi in all operational modes time limited to _ mins. Total time above __ psi may not exceed _ min.

Back 15

111 and 115 psi
5 minutes
116 and 155 psi
2 minutes
110 psi
5 minutes

Front 16

(8) for airplanes Pre-Mod SB 145-73-0030 the N2 limit is _____

Back 16

102.5%

Front 17

(9) While this is an abnormal condition, operation between __ and __ psi is permitted during T/O and Go-around phases (for AE 3007A engines only)

Back 17

50 and 34 psi

Front 18

Engine Warm-Up
Prior to take-off, the engines must be allowed to run at ____ thrust to stabilize the engine temps before _____ thrust is adjusted

Back 18

low thrust,
take off thrust.

Front 19

Engine Warm-Up 1
After start, the engines must run at idle or taxi thrust during at least _ min. for cold engines (shut down for more than __ mins) or _ mins for warm engines

Back 19

4 minutes
90 minutes
2 minutes

Front 20

Engine Warm-up 2
To increase N2 above __% the engine oil temp must be at __C min. In lieu of this limit, it is acceptable to either run the engine for at least _ min or complete a static run up to __% N2, stabilize, and check to ensure oil pres. is equal or less than __ psi

Back 20

83%
40 degrees
8 minutes
88% N2
83 psi

Front 21

Maximum duration of ISIS when operating on batteries only is __ mins

Back 21

40 minutes

Front 22

ISIS Note: the max duration of the battery can be extended to __ min if the ____ is turned off when not operating in ________

Back 22

45 minutes
Pitot 3 sensor heating button
icing conditions

Front 23

ISIS note: Airplane must not be moved during _________. Do not _________ in turning flight.

Back 23

power-up initialization.
cage attitude during turning flight

Front 24

Electromechanical gust lock
Each time the E.G.L lever is set to _______ position elevator movement must be checked.

Back 24

unlocked position

Front 25

EGL check must be performed at least __ secs after positioning the gust lock lever to the ___ position by moving the control column to the ____ stop to the ____ stop and back to the ____ position

Back 25

10 seconds
unlocked
full up stop
full down stop
full up stop

Front 26

Cockpit Security Door
_ crewmembers must be in the cockpit during all flight phases. Must be closed at all times during flight except to permit access and egress according to GOM procdures ____ for ______ the door

Back 26

2, if one leaves must be replaced, positive ID must be obtained before opening door.
GOM 6-1.2.1 for opening, closing, and locking the door

Front 27

Anytime that cockpit door is opened in flight, a ________________ must be used to verify that the door is closed and locked

Back 27

challenge and response closing and locking verification procedure