First Flight Checks Flashcards
Aircraft status check: (FMAN)
- Flaps
- Maintenance
- APU Area (CRJ200)
- Nose Door (CRJ200
Logbook/Forms/Manuals verify checked?
What are you looking for
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
FIRE DETECTION/FIREX MONITOR Test
700) (900
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
FIRE DETECTION/FIREX MONITOR Test
(200)
What do you check before you do the test
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
FIRE DETECTION/FIREX MONITOR Test
(200)
Warn Position What Lights come on?
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
FIRE DETECTION/FIREX MONITOR Test
(200)
At WARN position What EICAS messages?
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
FIRE DETECTION/FIREX MONITOR Test
(200)
TEST Position What Lights come on?
• Both master cautions, single chime
FIRE DETECTION/FIREX MONITOR Test
(200)
At TEST position What EICAS messages?
And the following Amber Caution messages: • L FIRE FAIL • R FIRE FAIL • APU FIRE FAIL • L JET OVHT FAIL • R JET OVHT FAIL
ENGINE BOTTLE 1 & 2 switches (200)
Verify the following Green Advisory messages: • L ENG SQUIB 1 • R ENG SQUIB 1 • L ENG SQUIB 2 • R ENG SQUIB 2
CARGO BOTTLE switch TEST 1
- Both master warnings, triple chime
- NORMAL & STANDBY CARGO SMOKE PUSH switchlights illuminated
- NORMAL BOTTLE ARMED PUSH TO DISCH switchlight illuminated
- “SMOKE” aural
CARGO BOTTLE switch TEST 1
EICAS messages
• SMOKE CARGO
And the following Green Advisory message:
• CARGO SQUIB 1
CARGO BOTTLE switch TEST 2
- Both master warnings, triple chime
- NORMAL & STANDBY CARGO SMOKE PUSH
- STANDBY BOTTLE ARMED PUSH TO DISCH
- “SMOKE” aural
CARGO BOTTLE switch TEST 2
EICAS messages
The following Red Warning message:
• SMOKE CARGO
And the following Green Advisory message:
• CARGO SQUIB 2
DUCT MON Bleed Air Test
TEST position what are you checking?
Checks for continuity of all loops
Bleed Air Test
LOOP A, LOOP B position
Tests the 10th stage loops for shorts
DUCT MON Bleed Air Test
TEST position what lights come on ?
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
DUCT MON Bleed Air Test
TEST what EICAS messages ?
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
Ice Detector Test.
DET TEST switchlight …….. hold in
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
What does FAIL light on the LCV switch indicate
LCV not in commanded position
MLG Overheat Test
MLG BAY switch …………..Hold at OVHT
• Both master warnings, triple chime • “GEAR BAY OVERHEAT” aural And the following Red Warning message: • MLG BAY OVHT release and message goes away
MLG Overheat Test
OVHT TEST switch ………………. Hold at WARN FAIL
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
TCAS Test.
Radio Tuning Unit (RTU)
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
Public Address System Test
ACP transmit knob …….. Select PA
Interphone control unit ……… Push PA switchlight
• Green PA Switchlight remains ON
• Transmit a test message
STAB and MACH TRIM
— 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
YAW DAMPER
— 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
Stall Protection System Test
Before test
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
Stall Protection System Test
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
EGPWS Test
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