First Flight Checks Flashcards

1
Q

Aircraft status check: (FMAN)

A
  1. Flaps
  2. Maintenance
  3. APU Area (CRJ200)
  4. Nose Door (CRJ200
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2
Q

Logbook/Forms/Manuals verify checked?

What are you looking for

A

Confirm all manuals are current using the DRS.
Verify the following items are onboard:
• Airworthiness certificate
• Aircraft registration
• FCC operating license
• Maintenance logbook and MEL stickers
• Normal checklists (2 normal, 1 required)*
• MEL/CDL
• QRH
• POH (1 must be onboard the aircraft)
• FOM (1 must be onboard the aircraft)
• Speed Books (2 normal, 1 required)*
• Weight and balance forms
• SeeGee calculator
• Jumpseat briefing card (a verbal briefing of ACM may be substituted)*
* Before departing a maintenance base, a full supply of aircraft forms and manuals must be obtained if available.
• Confirm 3 landing gear pins and 1 ADG pin are onboard

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3
Q

FIRE DETECTION/FIREX MONITOR Test

700) (900

A

LH/RH ENG FIRE PUSH
BOTTLE 1/BOTTLE 2 ARMED PUSH TO DISCH
APU FIRE PUSH and BOTTLE ARMED PUSH TO DISCH
FWD & AFT CARGO and BOTTLE ARMED PUSH TO DISCH
And the following Green Advisory message:
• FIRE SYS OK
• After 30 seconds, test is complete, and all fire detection indications are removed. Any malfunctions will be shown in the form of Caution or Status messages

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4
Q

FIRE DETECTION/FIREX MONITOR Test
(200)
What do you check before you do the test

A

Make sure no APU FIRE FAIL Amber Caution message
displayed on the Primary page. If APU FIRE FAIL Amber Caution message is displayed, do NOT
carry out the Fire Detection/Firex Monitor Test, do NOT start the APU, and advise Maintenance
Control

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5
Q

FIRE DETECTION/FIREX MONITOR Test
(200)
Warn Position What Lights come on?

A

Both master warnings, triple chime
• LH/RH ENG FIRE PUSH and BOTTLE 1/BOTTLE 2 ARMED PUSH TO DISCH
• APU FIRE PUSH and BOTTLE ARMED PUSH TO DISCH
• Fire bell & “JETPIPE OVERHEAT” aural
And the following Red Warning messages:
• L ENG FIRE
• R ENG FIRE
• APU FIRE
• L JETPIPE OVHT
• R JETPIPE OVHT
Ensure no FIRE FAIL Amber Caution messages appear

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6
Q

FIRE DETECTION/FIREX MONITOR Test
(200)
At WARN position What EICAS messages?

A
And the following Red Warning messages:
• L ENG FIRE
• R ENG FIRE
• APU FIRE
• L JETPIPE OVHT
• R JETPIPE OVHT
Ensure no FIRE FAIL Amber Caution messages appear
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7
Q

FIRE DETECTION/FIREX MONITOR Test
(200)
TEST Position What Lights come on?

A

• Both master cautions, single chime

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8
Q

FIRE DETECTION/FIREX MONITOR Test
(200)
At TEST position What EICAS messages?

A
And the following Amber Caution messages:
• L FIRE FAIL
• R FIRE FAIL
• APU FIRE FAIL
• L JET OVHT FAIL
• R JET OVHT FAIL
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9
Q

ENGINE BOTTLE 1 & 2 switches (200)

A
Verify the following Green Advisory messages:
• L ENG SQUIB 1
• R ENG SQUIB 1
• L ENG SQUIB 2
• R ENG SQUIB 2
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10
Q

CARGO BOTTLE switch TEST 1

A
  • Both master warnings, triple chime
  • NORMAL & STANDBY CARGO SMOKE PUSH switchlights illuminated
  • NORMAL BOTTLE ARMED PUSH TO DISCH switchlight illuminated
  • “SMOKE” aural
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11
Q

CARGO BOTTLE switch TEST 1

EICAS messages

A

• SMOKE CARGO
And the following Green Advisory message:
• CARGO SQUIB 1

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12
Q

CARGO BOTTLE switch TEST 2

A
  • Both master warnings, triple chime
  • NORMAL & STANDBY CARGO SMOKE PUSH
  • STANDBY BOTTLE ARMED PUSH TO DISCH
  • “SMOKE” aural
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13
Q

CARGO BOTTLE switch TEST 2

EICAS messages

A

The following Red Warning message:
• SMOKE CARGO
And the following Green Advisory message:
• CARGO SQUIB 2

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14
Q

DUCT MON Bleed Air Test

TEST position what are you checking?

A

Checks for continuity of all loops

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15
Q

Bleed Air Test

LOOP A, LOOP B position

A

Tests the 10th stage loops for shorts

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16
Q

DUCT MON Bleed Air Test

TEST position what lights come on ?

A
Verify the following:
• Both master warnings, triple chime
• “BLEED AIR DUCT” aural
On the BLEED AIR and ANTI-ICE overhead panels, verify the following red switchlights:
• L 10TH STAGE DUCT FAIL
• R 10TH STAGE DUCT FAIL
• L 14TH STAGE DUCT FAIL
• R 14TH STAGE DUCT FAIL
• WING ANTI-ICE DUCT FAIL
17
Q

DUCT MON Bleed Air Test

TEST what EICAS messages ?

A
The following Red Warning messages:
• L 10TH STAGE DUCT
• R 10TH STAGE DUCT
• L 14TH STAGE DUCT
• R 14TH STAGE DUCT
• ANTI-ICE DUCT
And the following Green Advisory message:
• DUCT TEST OK
18
Q

Ice Detector Test.

DET TEST switchlight …….. hold in

A

Below a preset temperature, verify the following:
• Both master cautions, single chime
• ICE switchlight illuminated
And the following Amber Caution message:
• ICE
Above 18 deg, verify the following Green Advisory message only:
• ICE

19
Q

What does FAIL light on the LCV switch indicate

A

LCV not in commanded position

20
Q

MLG Overheat Test

MLG BAY switch …………..Hold at OVHT

A
• Both master warnings, triple chime
• “GEAR BAY OVERHEAT” aural
And the following Red Warning message:
• MLG BAY OVHT
release and message goes away
21
Q

MLG Overheat Test

OVHT TEST switch ………………. Hold at WARN FAIL

A
Verify the following:
• Both master cautions, single chime
And the following Amber Caution message:
• MLG OVHT FAIL
OVHT TEST switch .....Release
• Caution message is removed
22
Q

TCAS Test.

Radio Tuning Unit (RTU)

A

TCAS line key ……… Select
TEST line key ……… Select
Verify the following:
• On the VSI: TRAFFIC, TCAS test & red/green bands
• On the MFD: Four levels of targets (hollow cyan diamond, solid cyan diamond, solid yellow circle, and solid red square)
• “TCAS SYSTEM TEST OK” aural

23
Q

Public Address System Test

A

ACP transmit knob …….. Select PA
Interphone control unit ……… Push PA switchlight
• Green PA Switchlight remains ON
• Transmit a test message

24
Q

STAB and MACH TRIM

A

— STAB TRIM CH1 & CH2……………. Press
• After pressing one STAB TRIM button, the STAB TRIM Amber Caution message should be removed, and a STAB
CH 1 (or 2) INOP White Status message will appear until the other STAB TRIM button is pressed
— CAPTAIN’S STAB TRIM DISCONNECT………………………….. Press
Note the following Amber Caution message:
• STAB TRIM
Repeat procedure using First Officer stab trim disconnect.
— STAB TRIM CH1 & CH2………………………… Press
— MACH TRIM………………………………………….. Press
• Confirm that all messages are removed

25
Q

YAW DAMPER

A

— YD1 & YD2………………ENGAGE
• After engaging one YD, the YAW DAMPER Amber Caution message and amber YD indication on both PFDs
should be removed, and a YD 1 (or 2) INOP White Status message will appear until the other YD is engaged
• Confirm YD 1 INOP and YD 2 INOP White Status messages are not displayed

26
Q

Stall Protection System Test

Before test

A

FLAPS lever………… 0
STAB TRIM position……… 6 ±0.2 units
Hydraulic pressure ………. Checked
• Ensure that hydraulic system 3 pressure is normal
STALL PTCT, PUSHER switches…………………Select to ON

27
Q

Stall Protection System Test

A

STALL switch…………………. Select momentarily and check for the following events:
• CONT IGNITION ON White Status message
• Display Flight Control Synoptic page on ED2
• Captain’s and First Officer’s stick shaker is activated
• CONT, ON light on
• Stick pusher, STALL switches flash
• EICAS R/H elevator surface pointer indicates full travel or First Officer control column is against forward stop
• Stick pusher is de-activated and STALL switches out
• Captain’s and First Officer’s stick shaker stops
• CONT, ON light out
• CONT IGNITION White Status message out
Hydraulic Pump 3A…………………OFF

28
Q

EGPWS Test

A

GND PROX TERRAIN switchlight ……… Selected out and guarded
GPWS switchlight ………. Push and release (less than 3 secs)
Verify the following:
• GPWS and G/S lights illuminated
• “GLIDESLOPE,” “WHOOP, WHOOP, PULL UP,” “TERRAIN,” and “WINDSHEAR” aurals
• On the MFDs: TERRAIN TEST and TERRAIN DISPLAY FAIL messages and a display test pattern
• On the PFDs: Windshear warning
And the following White Status messages:
• GPWS FAIL
• WINDSHEAR FAIL
• TERRAIN FAIL