EP’s And Limits Flashcards
Max TOT starting
8.5 FLI
785 TOT
TOT starting transient
8.5-11 FLI
5 seconds
865 TOT
AEO takeoff Power range
8.5 - 10 FLI
5 minutes
%tq 71-88
AEO take off power Max
10 FLI
5 minutes
88% TQ
OEI MCP Max
11 FLI
91 % TQ
OEI 2.5 minute power
12 FLI
2.5 min
125 % TQ
AEO transient Max
10.5 FLI
12 seconds
97 % tq
OEI transient Max
14 FLI
12 seconds
140% TQ
Max gross mass for flight
7905 lbs
Airspeed limits
Vne OEI: 110 Kias
Vne Steady auto : 90 Kias
Min a/s auto: 60 Kias
Target a/s auto: 75 Kias
Slope limits
Slope left: 11°
Slope right: 6°
Slope nose up or down: 8°
Prohibited flight maneuvers
Aerobatic maneuvers
Full auto
Flight into icy cond.
Rotor rpm
95% steady light/ low beep tone
106% flash light gong
110% flash light high tone
Eng 1 or 2 fail
OEI flight cond. : Establish
Affected engine: identify
Sees: perform
Practicable
Fire 1 or 2
OEI flight condition; establish
Airspeed: reduce if IAS exceeding 100 Kias
Fire switch (affected engine): raise Guard, press
Bot 1/2 pb : Press; bot 1 activate - ext Ind come on
Clock - start after bot I legend and ext Ind go off
Affected engine - identify
Sees : perform
Land as soon as possible
If Fire still on:
Bot 1/2: Press ext Ind go on
Land immediately
XSMN oil Press
Power: reduce
Land as soon as Practicable
If both Ind. Below 1.0 bar
Land immediately
SEF HOGE
Collective lever - adjust to maintain rotor rpm
Airspeed - increase if possible
- forced landing
Landing attitude - establish
Collective - raise as necessary to stop descent or cushion landing
Affected engine - I’d
Sees - perform
- transition to OEI flight
Collective - adjust to Oe limits or below
Rotor speed -trim to max
Airspeed - gain 65 knots
- after reaching safe altitude
Collective - reduce to OEI MCP or below
Affected engine-id
Sees-perform
SEF - flight
OEI flight condition - establish
Rotor speed _. trim to max
Affected engine-id
Sees - perform
Single engine emergency shutdown (sees)
Twist grip (affected engine) - rotate slowly to idle (check indications)
Rotor speed - trim to max
Engine over speed (governor failure)
OE1 flight condition - establish
Var NAR - check Man
N2 trim sw - trim to 101% with matched TQ
- if step 3 not possible-
Affected engine - id
Twist grip - rotate to idle until N2 and NRO stabilize
Engine underspeed ( Gov failure )
OE1 flight cond.- establish
Bleed air consumers- off
Var NAR - check man
Affected engine- id
N2 trim sw - compensate n2/nro drop and match TQ
-If match tq not possible-
Twist grip (affected engine ) - release stop plate rotate towards flight until n2 match
Sees - perform
Double engine emergency shut down
Both twist grips - off
Both fuel pumps prime - off
Bat master sw- Off
-In flight -
Both twist grips - off
Both emer off sw- press
Autorotation
Collective - reduce to maintain NRO within limits
Airspeed - 75 knots
Double engine emergency shutdown - perform
-
-
-
Bat master sw - off
Tail rotor Drive/ fixed pitch
Collective - reduce to obtain minimum side slip
Airspeed - 70 knots or higher
Shallow approach nose left- perform
Airspeed - reduce close to ground until nose aligned with flight path
Landing - perform
- can’t land -
Airspeed - increase
Approach - abort climb to sufficient altitude to perform auto
Auto-perform