Engine Startup W,C,N

Question 1

BEFORE STARTING ENGINES

Answer 1

BEFORE STARTING ENGINES

Question 2

Before Starting Engines.
2W 1C

Answer 2

W. Remove Tiedowns
W. Able to reach and actuate all controls from seat
C. Dont grab foam from seat

Question 3

1-5 (DP)

Circuit breakers and switches- SET
1N

Answer 3

If IMC

N. Hold STBY INST switch for 5 sec in test pos. BATT GOOD appear for 5 sec

Question 4

1-6

BATT NO.1 and NO.2 switches- ON
1N

Answer 4

N. Beeping between ICS checks

Question 5

COCKPIT EQUIPMENT CHECKS

Answer 5

COCKPIT EQUIPMENT CHECKS

Question 6

2-2

APU CONT switch- ON
3N

Answer 6

N. If APU fails analyze bite before BATT NO1 or another APU start
N. No APU, No APU ACCUM LOW, No APU CONT ON pull manual override for another start
N. First 4 seconds APU FIRE T-HANDLE and MASTER FIRE light up=No real fire

Question 7

2-3

GENERATORS APU switch- ON
2W

Answer 7

W. Stabilator clear
W. TACAN clear

Question 8

2-5

EDECU- Check signal validation code 25%
3N

Answer 8

N. Verify 25% engine EDECU code on MFD Q Indicator
N. Can Verify EDECU on FMS Status Page
N. DEC display signal validation fault codes for 4 sec on, 2 sec off , 30 sec after engine shutdown

Question 9

2-9

MASTER WARNING PANEL- Check #1 ENG OUT, #2 ENG OUT, LOW ROTOR R.P.M segment lights are illuminated
1N

Answer 9

N. If lights doesn’t come on, pull out 1/4 in and push in to reset

Question 10

2-13

Press FCC FAILURE RESET SWITCHES.
1N

Answer 10

N. EGI must be in ORIENT

Question 11

2-14 (DP)

Load navigation database
3N

Answer 11

N. Need a derivative Nav-DB PMCA card
N. Load NAV DB from BC FMS
N. Clear asterisks date line on first reset by forcing BUS SWAP

Question 12

2-18 (DP)

Flight controls-0 Check first flight of the day
2W 2N

Answer 12

W. Ensure Gear Doesn’t interfere with controls
W. PRI SERVO 1 or 2 FAIL SERVO BYPASS VAULE JAMMED. DONT FLY!
N. Don’t push pedals past system stop with SAS/BOOST off during checks
N. 1.5 inch of play in controls

Question 13

2-21 (DP)

Stabilator- Check
1W

Answer 13

W. Any part of STABILATOR check fails, DONT FLY!

Question 14

2-23 (DP)

FMS initialization- Check as required
4N

Answer 14

N. FMS defaults to last known position, updates when GPS available
N. INIT will engage once GPS acquires satellites
N. Performance calculator works once Config of aircraft is verified
N. Drag and Performance variables must match aircraft config to have accurate performance

Question 15

2-25 (DP)

Set up MFD/FD/FMS for mission
1N

Answer 15

N. only 2 Unit task organizations (UTOs) per PCMCIA card

Question 16

STARTING ENGINES

Answer 16

STARTING ENGINES

Question 17

1

Starting engines
1C

Answer 17

C. Blades within 20 Degrees of center IF Rotor brake Start

Question 18

1-3

GUST LOCK ENGAGED caution- Verify off
1N

Answer 18

N. Verify GUST LOCK ENGAGED on EICAS

Question 19

1-4

STAB UNLOCKED caution- Verify off
1W 1N

Answer 19

W. If STAB UNLOCKED it could hit tail rotor
N. Verify STAB UNLOCKED NOT on EICAS

Question 20

1-9

Engine(s)- Start
1W 4C 7N

Answer 20

W. Rotor Brake slippage = release or shut down
C. Don’t turn ENGINE IGNITION ON if its OFF, ABORT
C. Don’t move ENG PWR CONT lever to OFF Pressing Starter
C. Cyclic neutral, collective no more than 1 inch, pedals centered (50%)
C. Minimize cyclic inputs
N. No NP or Q indications until rotor brake released
N. MAIN XMSN PRESS caution and no pressure indications until rotor break released
N. Hydraulic cautions on until rotor brake released
N. FUEL PRESS LOW caution may appear and disappear
N. Don’t use FUEL BOOST PUMP CONTROL to get rid of fuel press cautions
N. If ENG STARTER ON disappears and ENG POWER CONT lever is OFF, hold starter until 52-65% NG
N. 1 sec delay between started disengaging and engine starter

Question 21

1-15 (DP)

Hydraulic leak test system- Check
2N

Answer 21

N. Press and release test switch
N. Backup still on, switch to OFF the AUTO

Question 22

1-16 (DP)

Tail rotor servo transfer- Check
1N

Answer 22

N. Failed BACK UP PUMP ON or T/R SERVO 2 ON advisories means LDI system failure

Question 23

ENGINE RUNUP

Answer 23

ENGINE RUNUP

Question 24

1-1

ENG POWER CONT lever(s)- FLY
1W 1N

Answer 24

W. Move ENG POWER CONT lever slowly when tailwheel lockpin not engaged (can kill someone)
N. 45% SE or 57% DE NR prior to moving ENG POWER CONT levers (rotor brake ON)