N8905F
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PINNACLE AIR INC | Operator | on 2007-04-12 | Operator named in NTSB report |
Accident & incident history
Operated by PINNACLE AIR INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
74 reports on file, 2005-06-20 – 2017-12-20.
Part: HOSE — DAMAGED (PORT O2 MASK) · airframe 27,460 hrs · 24,977 cycles
PORTABLE OXYGEN BOTTLE 4LMP MASK HOSE DAMAGED. REMOVED AND REPLACED THE MASK ASSEMBLY.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 27,390 hrs · 24,896 cycles
CREW O2 LOW, WAS REFILLED THIS MORNING AND IS BELIEVED TO BE LEAKING. FOUND CAPT'S AND FO'S MASKS TO BE LEAKING. R&R CAPT'S AND FO'S CREW OXYGEN MASKS IAW AMM 35-11-12. NO LEAKS NOTED. OK FOR SVC.
Part: CONTROL UNIT — FAULTED (FLAPS) · airframe 27,342 hrs · 24,844 cycles
FLAP FAILED ON TAKEOFF CAUTION. DIVERTED. RT WINDOW HEAT CAUTION. PERFORMED TROOBLESHOOTING IAW FIM REV 53. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD. RT WINDOW HEAT OPS CHECKED GOOD IAW AMM 30-41-01.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 27,209 hrs · 24,687 cycles
OXYGEN LOW PRESSURE CAUTION MESSAGE, 1410 PSI. LEAK CHECKED THE CREW OXYGEN SYSTEM AND FOUND THE LEFT PILOT OXYGEN MASK LEAKING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD. OXYGEN PSI HOLDING AFTER 4 HOURS.
Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 27,002 hrs · 24,460 cycles
EMERGENCY LIGHT INOPERATIVE. CYCLED F/A EMERGENCY LIGHT SWITCH, AND THE COCKPIT PANEL SWITCH. ALL CHECKED GOOD IAW AMM 33-50-00.
Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 27,002 hrs · 24,460 cycles
THE EXIT LIGHT BY THE SIDE DOOR AT ROW 8 LEFT INOPERATIVE. CYCLED F/A EMERGENCY LIGHT SWITCH AND COCKPIT PANEL SWITCH. ALL CHECKED GOOD IAW AMM 33-50-00.
Part: ELT — NO TEST (CABIN) · airframe 25,824 hrs · 23,234 cycles
ELT FAILED OPERATIONAL CHECK. R & R THE ELT IAW AMM 25-62-01 OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (ROWS 1-5 CD) · airframe 25,819 hrs · 23,227 cycles
ROW 1-5 CD EMERGENCY LIGHTS INOPERATIVE. R & R THE CABLE ASSY AND LAMP IAW AMM 33-51-01. OPS CHECKED GOOD.
Earlier reports · 2005–2016 · 66 reports
2016
Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 25,767 hrs · 23,173 cycles
FO O2 MASK RELEASE O2 WHILE LEFT 02 DOOR IS OPEN. REMOVED AND REPLACED FO O2 MASK IAW AMM 35-11-12. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.
Part: BPSU — INOPERATIVE · airframe 25,721 hrs · 23,125 cycles
FLAPS FAIL CAUTION MESSAGE. FLAPS IN 0 POSITION. R & R LEFT BPSU IAW AMM 27-51-10 OPS CHECK GOOD.
Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 25,693 hrs · 23,096 cycles
WHILE REMOVING CAPTAINS BROKEN FLASHLIGHT SEAL FOUND THAT BLINKING RED LIGHT WAS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT AND HOLDER ASSEMBLY AND PERFORMED OP'S CHECK
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,167 hrs · 22,568 cycles
EMERGENCY FLOOR TRACK LIGHTING NOT WORKING ROW 2 TO ROW 5. RESET ACFT POWER, PERFORMED OPS CHECK OF EMERGENCY LIGHTS NO DEFECT NOTED IAW AMM 33-51-00
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,073 hrs · 22,471 cycles
EMERGENCY LIGHTS NOT COMING ON WITH SWITCH IN THE ON POSITION FROM FLT DECK OVERHEAD PANEL OR FLT ATTENDANT'S PANEL. DURING FFOD CHECK. LET BATTERIES FULLY CHARGE ON EXTERNAL POWER. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,036 hrs · 22,435 cycles
6 ROWS OF EMERGENCY FLOOR LEVEL LIGHTING STRIP IS SLOW TO ILLUMINATE WHEN COLD WORKS FINE AFTER STRIP IS WARMED UP. PERFORMED OPS CHECKED OF EMERGENCY FLOOR LEVEL LIGHTING, OPS CHECKED GOOD IAW AMM 33-51-01. ACFT OK FOR SERVICE.
Part: SMOKE WARNING — FALSE ACTIVATION · airframe 25,018 hrs · 22,416 cycles
SMOKE ALARM SOUNDED FOR NO REASON AND NOW FAILS TO TEST PROPERLY. UNABLE TO DUPLICATE. OPS CHECKED GOOD IAW MM 26-16-01.
Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 24,873 hrs · 22,267 cycles
OBSERVERS MASK FAILS TEST. REPLACED OXYGEN MASK STORAGE BOX IAW 35-11-12. OPS & LEAK CHECKED GOOD.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 24,828 hrs · 22,221 cycles
EMERGENCY EXIT FLOOR TRACK LIGHTING ROWS 2-5 INOPERATIVE. RECONNECT, RESEATED EMERGENCY EXIT FLOOR LIGHT CONNECTORS, ALL LIGHTS OPS CHECK GOOD IAW AMM 33-51-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,487 hrs · 21,867 cycles
PASSENGER CALL LIGHT IN EMER EXIT SIGN ON CEILING IS NOT WORKING, WHEN CALL BUTTON PUSHED. R & R LIGHT BULB ON PAX OVERHEAD CALL SIGN IAW AMM 33-51-14. OK FOR SERVICE.
2015
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,936 hrs · 21,322 cycles
RIGHT SIDE SEAT RAIL FROM FS 444.02 TO FS 495.98, HAS SEVERAL AREAS OF CORROSION. R & R NEW SEAT RAIL FROM RFS 444.02 TO 495.98, PN 601R38312-115S, IAW AMM 53-01-11-400-802.
Part: STOP FITTING — BROKEN (WING) · airframe 23,936 hrs · 21,322 cycles
PANEL 594JB HAS BUTE DOOR STOP TAB BROKEN OFF THE END OF THE PANEL. REMOVED THE BROKEN DOOR STOP AT PANEL 594JB IAW SRM 51-42-06. RECEIVED NEW DOOR STOP, PN 600-10196-15. INSTALLED TO PANEL 594JB IAW SRM 51-42-06. WORK SUMMARY STATEMENT REQUIRED. R & R DAMAGED DOOR STOP, PN 600-10196-15 IAW SRM 51-42-06.
Part: FAIRING — CHAFED (TE FLAP) · airframe 23,936 hrs · 21,322 cycles
LEFT STUB FAIRING CHAFED ON AFT END APPROX 1" WIDE BY 1" HIGH BY .008 DEEP. R & R WITH NEW SERVICEABLE OUTER LT FLAP STUB FAIRING SKIN, PN 601R31199-89, UPPER SEAL PN 601R31199-81, LOWER SEAL PN 601R31199-99, BRACKET PN 610R31199-5, HINGE HALF PN 601R31199-21, HINGE HALF 601R31199-23 & HINGE PIN 601R31199-25 I.
Part: MOUNT BRACKET — CRACKED (TE FLAP) · airframe 23,936 hrs · 21,322 cycles
RIGHT FLAP STUB FAIRING, FWD MOUNT BRACKET IS CRACKED. LOCATED, DRILLED & INSTALLED NEW FWD MOUNT BRACKET, PN 601R31199-6 IAW SRM 51-40-11 & 51-42-06 ON RT FLAP STUB FAIRING.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,936 hrs · 21,322 cycles
LEFT SIDE SEAT RAIL FROM FS 364 TO FS 409.00+16, HAS SEVERAL AREAS OF CORROSION. R & R LT PAX SEAT RAIL, PN 601R38312-31, FROM FS 364 TO 409.00+18.02 IAW AMM 53-61-11-000 400-802.
Part: POWER CABLE — DEFECTIVE (CABIN) · airframe 23,936 hrs · 21,322 cycles
FIRST LIGHT ON CABIN FLOOR TRACK IS NOT WORKING. REPLACED UNSERVICEABLE CABLE ASSEMBLY AT FWD CONNECTION WITH NEW CABLE ASSEMBLY IAW ESPM 20-17-10. OPERATIONS CHECKED GOOD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,936 hrs · 21,322 cycles
RIGHT SIDE SEAT RAIL FORM FS 364 TO FS 409.00+16, HAS SEVERAL AREAS OF CORROSION. REMOVED RT SIDE SEAT RAIL, PN 601R38312-031S, FROM RFS 364 TO 409+16 IAW AMM 53-01-11. RECEIVED RT SIDE SEAT RAIL 601R38312-31, INSTALLED TO RFS 364 - 409+16 IAW AMM 53-01-11-420-001.
Part: POST — DAMAGED (FUSELAGE) · airframe 23,936 hrs · 21,322 cycles
FS 409 & 128, RBL 18, INBD & OTBD VERTICAL POSTS HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69, APPROX 0.250" LONG BY GREATER THAN 50% FSH. BOTH INDICATIONS FAILED NDT INSPECTION. REMOVED OVERBOARD EXHAUST VLV IAW QMM 21-24-34-000-401. INSTALLED SAME SERVICEABLE OVERBOARD EXHAUST VLV IAW AMM 21-24-34-400-801. INSTALLED SAME SERVICEABLE INSULATION AT FS 409+128, RBL 18 IAW AMM 25-81-01-400-801. LOCATED & DRILLED NEW SERVICEABLE FS 409+128 INBD & OTBD VERTICAL POST AT RBL 18 IAW SRM 51-409-11. INSTALLED NEW SERVICEABLE FS 40+128, RBL 18 VERTICAL POST IAW REO 601R-53-41-889 & SRM 51-42-06. FABRICATED NEW FS 409+128, RBL 18 INBD STIFFENER IAW EO 601R2208, SNIEO S18, DATD 11/0/15. PERFORMED OPERATIONS TEST OF THE OVERBOARD EXHAUST VLV IAW AMM 21-2-43-710-801. NO DEFECTS NOTED.
Part: RAM AIR TURB — DEPLOYED · airframe 23,397 hrs · 20,757 cycles
RAM AIR TURBINE DEPLOYED JUST AFTER WEIGHT OFF WHEELS. RETURNED & LANDING WITHOUT INCIDENT. PERFORMED ADG DEPLOYMENT, INFLIGHT, INSP IAW AMM 05-51-19 & SB ERPS10AG-24-3 REV 3 INSPECTION GOOD. NO DEFECTS FOUND. COMPONENT WAS REPLACED AT MOTR REQUEST, ADG CONTROL PANEL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,868 hrs · 20,192 cycles
EMERGENCY LIGHT ABOVE RIGHT WING INOPERATIVE, FIRST LIGHT. R & R EMER LIGHT BULB IAW AMM 33-51-21. OPERATIONS CHECKED GOOD.
2014
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,365 hrs · 19,683 cycles
ONE INFANT LIFE VEST & OBSERVERS LIFE VEST BAGS TORN. R & R ONE INFANT LIFE VEST & ONE OBSERVERS LIFE VEST IAW AMM 25-61-03 & PA 25-096A.
Part: DOOR SEAL — LACK OF LUBE (CABIN DOOR) · airframe 22,346 hrs · 19,659 cycles
LOUD PRESS SQUEAL COMING FROM MAIN CABIN DOOR IN FLIGHT. INSPECTED & LUBED SEAL & PERFORMED PRESS CHECK IAW AMM 21-32-00. OPERATIONS & PRESS CHECKED GOOD AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,936 hrs · 19,253 cycles
ROW 8 EMER ELECTROLUMINESCENT FLOOR LIGHT INOPERATIVE. R & R FLOOR LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
Part: INSULATION — OUT OF POSITION (EMERGENCY EXIT) · airframe 21,892 hrs · 19,207 cycles
RIGHT EMER DOOR HAS INSULATION AROUND PULL HANDLE THAT STOPS HANDLE FROM OPENING ALL THE WAY. REMOVED INSULATION FROM RT EMER EXIT DOOR PULL HANDLE THUS PERMITTING HANDLE TO OPEN ALL THE WAY IAW AMM 52-21-00.
Part: LENS — CRACKED (CABIN) · airframe 21,892 hrs · 19,207 cycles
GALLEY EMER EXIT & VENT PANEL HAS A CRACKED EMER LIGHT LENS & SHROUD. R & R GALLEY EMER LIGHT ASSEMBLY IAW 200 AMM 33-51-10. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.
Part: SHROUD — CRACKED (CABIN) · airframe 21,892 hrs · 19,207 cycles
EMERGENCY EXIT LIGHT LENS SHROUD IS CRACKED ON WARDROBE. R & R EMER LIGHT FLOOR LEVEL FLOOD LIGHT ASSEMBLY ON WARDROBE IAW AMM 33-51-19. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 21,892 hrs · 19,207 cycles
THE NR 1 EMER LIGHT BATTERY PACK IS INOPERATIVE. R & R NR 1 EMER LIGHT BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD IAW AMM 33-51-04-740-801.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 21,892 hrs · 19,207 cycles
THE NR 4 EMER LIGHT BATTERY PACK IS INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD IAW AMM 33-51-04-740-801.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
RIGHT WING LOWER ACCESS HOLES FOR PANELS 650EB & 650DB CORRODED. REPAIRED IAW REO 601R-57-21-030.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
CORROSION ON THE PANEL LANDING FOR PANELS 640AT, 640BT & 640CT ON THE RT UPPER WING SKIN AT WS 74.15, WS 96.34 & WS 114.27. REPAIRED IAW EA CRJ257-02626.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
CORROSION ON THE PANEL LANDING FOR PANELS 540AT, 540BT & 540CT ON THE LT UPPER WING SKIN AT WS 74.15, WS 96.34 & WS114.27.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
RIGHT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB CORRODED. REPAIRED IAW REO 601R-57-21-030.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
RIGHT WING LOWER PLANK ACCESS HOLES FOR PANELS 640EB & 640DB CORRODED. REPAIRED IAW REO 601R-57-21-030.
Part: WEB — CRACKED (FUSELAGE) · airframe 21,834 hrs · 19,147 cycles
FS 280 WEB CRACKED OTBD OF LBL 9 & RBL 9. REPAIRED IAW REO 601R-53-11-171 & 601R-53-11-136.
Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
FS 280 RBL 9 OTBD CLIP CRACKED & AFT FLOOR ANGLE CORRODED. REPAIRED IAW REO 601R-53-11-136.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,834 hrs · 19,147 cycles
LEFT WING PLANK ACCESS HOLES FOR PANEL 510AB & 540BB CORRODED. REPAIRED IAW REO 601R-57-21-030.
Part: BEAM — CHAFED (FUSELAGE) · airframe 21,834 hrs · 19,147 cycles
BL0 VERTICAL BEAM CHAFED FROM 10TH STAGE ISO VLV. REPAIRED IAW REO 601R-53-61-1523 & 601R-53-61-5286.
Part: HINGE FITTING — GOUGED (TE FLAP) · airframe 21,834 hrs · 19,147 cycles
RIGHT INBD FLAP INBD HINGE ARM GOUGED ON LOWER FWD & AFT OTBD SIDE. REPAIRED IAW REO 601R-57-54-259.
Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 21,834 hrs · 19,147 cycles
FS 621 TOP LT CORNER NEAR J6CD CONNECTOR HAS FOUR SCRATCHES IN BULKHEAD. REPAIRED IAW REO 601R-53-61-2155.
Part: COVER — LOOSE (CABIN) · airframe 21,500 hrs · 18,822 cycles
EMERGENCY LIGHTING STRIP ON 1CD LOOSE. SECURED EMERGENCY FLOOR PATH LIGHTING COVER IAW AMM 33-51-01. ALL CHECKED GOOD.
Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 21,393 hrs · 18,712 cycles
AFT CEILING EXIT SIGN FWD & AFT EMERGENCY LIGHT CAP COVERS MISSING. R & R AFT EXIT SIGN WHITE LIGHT CAPS IAW AMM 33-20-00. OPS CHECKED GOOD.
Part: COVER — BROKEN (CABIN) · airframe 21,333 hrs · 18,658 cycles
EMERGENCY FLOOR STRIP LIGHTING ROW 1C - D PLASTIC COVER ABOUT 2 FEET LONG BROKEN & THE EMERGENCY FLOOR STRIP EXPOSED. REPLACED EMERGENCY FLOOR TRACK LIGHT COVER FROM ROWS 1C - D THRU 5C - D. ALL CHECKED GOOD IAW REF CRJ 200 AMM CH 33-51-00.
2013
Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 20,423 hrs · 17,768 cycles
FLAPS HALFSPEED STATUS ILLUMINATED AFTER LANDING WHILE BRINGING FLAPS UP. RESET FALP HALFSPEED STARTING UNDER DIRECTION OF MOC TC IAW FIM FAULT MSG RESET PROCEDURES CYCLED FLAPS MESSAGE NO LONGER REAMINS.
Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 20,423 hrs · 17,768 cycles
FLAPS HALFSPEED STATUS MESSAGE AFTER LANDING. CYCLED CIRCUIT BREAKERS IAW FIM MESSAGE CLEARED. OK FOR SERVICE.
Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 20,404 hrs · 17,748 cycles
FLAPS HALFSPEED STATUS MESSAGE POSTED AFTER LANDING DURING FLAP RETRACTION. PERFORMED FIM RESET PROCEDURE FOR "FLAPS HALFSPEED" MESSAGE DISSAPATED. ACFT OK FOR SERVICE, IAW MX CONTROL.
Part: CONTAINER — TORN (LIFE VEST) · airframe 20,386 hrs · 17,729 cycles
F/O LIFE VEST BAG TORN. R & R F/O LIFEVEST IAW AMM 25-61-03.
Part: HEATER — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 20,020 hrs · 17,371 cycles
AT LIFTOFF, TAT PROBE HEAT, RT AOA HEAT, RT STATIC HEAT , RT PITOT HEAT CAUTION ALL CAME ON. RAN QRH TO NO AVAIL, R & R HEATER AIR DATA SENSOR HEATER COMTROL IAW 30-31-15. OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,825 hrs · 17,175 cycles
EMERGENCY EXIT LIGHTS INOPERABLE - OUTSIDE AFT, 2 OVERWING. REMOVED & REPLACED ALL BATTERY PACKS PER CRJ200 AMM 33-51-04.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,510 hrs · 16,871 cycles
FLIGHT ATTENDANT FLASHLIGHT IS INOPERABLE. REMOVED AND REPLACED FLASHLIGHT BATTERY.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,499 hrs · 16,862 cycles
CRACK FOUND IN CAP ANGLE AT RBL 18 AND LBL 18 ON FS 559 SEMI-PRESSURE BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-41-260, 601R-53-41-609 AND PA 53-025.
2012
Part: PANEL — BENT (HORIZONTAL STAB) · airframe 18,353 hrs · 15,758 cycles
DURING APPROACH, WITH AUTOPILOT OFF. THERE WERE THREE VERY DISTINCT TIMES THE ELEVATOR FELT VERY ABNORMALLY HIGH RESISTANCE. THERE WAS NO ASSOCIATED CAUTION OR WARNING MESSAGES. ACCOMPLISHED FIM 27-32-00,27-30-00. ALL CHECKED NORMAL UNTIL BLOCK 4. FOUND RIGHT UPPER VISOR PANEL, AFT EDGE BENT, AND RUBBING ON ELEVATOR. REMOVED AND REPLACED RIGHT UPPER STAB VISOR PANEL IAW AMM 55-32-05. VISOR PANELS CHECK OK. ALSO PERFORMED OPERATIONAL CHECK OF PITCH FEEL CONTROL IAW AMM 27-31-21. OPS CHECKS NORMAL. NO OTHER DEFECTS NOTED. ELEVATOR CONTROL SYSTEM OPS CHECKS GOOD ON GROUND AT THIS TIME.
Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 18,201 hrs · 15,605 cycles
FLAPS FAILED ON TAKEOFF AT 8. PERFORMED TROUBLESHOOTING PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I). CHECKED WIRE FOR BPSU (RT). NO SHORTS FOUND REMOVED AND REPLACED RT BPSU. OPS CHECKED GOOD IAW AMM 27-51-10 CODES RT BPSU, FECU, WIRING RT BPSU 51A 12 2B 5 2A 12 1B.
Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 18,179 hrs · 15,582 cycles
CAPTAIN'S LIFE VEST BAG DAMAGED. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.
Part: LIGHT — MISSING (CABIN) · airframe 17,837 hrs · 15,236 cycles
ORANGE STRIP IS MISSING FROM FLOOR EMERGENCY EXIT LIGHTING STRIP AT SEAT 8C. INSTALLED LIGHT STRIP AND OPS CHECK GOOD IAW AMM 33-51-01.
Part: MOUNT BRACKET — BENT (COCKPIT) · airframe 17,751 hrs · 15,154 cycles
LEFT RUDDER PEDAL CA SIDE ONLY HAS A BINDING FEEL AFTER ABOUT 1/2 TRAVEL. FOUND LT OTBD DUST PANEL RUBBING AGAINST PEDAL. STAIGHTENED NUT PLATE MOUNTING BRACKETS IAW SRM 51-45-00. PERFORMED OPS CHECK OF RUDDER IAW AMM 27-21-00. OPS CHECK GOOD. OK FOR SERVICE.
Part: KNOB — OUT OF ADJUST (RUDDER TRIM) · airframe 17,623 hrs · 15,040 cycles
RUDDER TRIM KNOB STICKS MOVING TRIM FULL DEFLECTION. ADJ KNOB PER CRJ AMM, OP CHECK GOOD 27-20-00.
Part: ELEVATOR — DAMAGED (LEFT) · airframe 17,606 hrs · 15,023 cycles
LEFT ELEVATOR HAS LIGHTNING STRIKE DAMAGE TO TRAILING EDGE. REPAIRED IAW SRM 55-20-00 FIGURE 204.
Part: FLAP — OUT OF RIG (WING) · airframe 17,588 hrs · 15,009 cycles
STIFF FLIGHT CONTROLS AIRPLANE ROLLS LEFT WHEN CONFIGURING FOR FLAPS. STIFF AILERONS ONCE FLAPS WERE SELECTED AIRPLANE ROLLED LEFT AND WORSENED WITH GREATER FLAP DEGREE SETTINGS. RIGGED RT AND LT FLAP CONTROL SURFACE SYS IAW AMM 27-54-00-830-801. OPERATIONAL TEST GOOD. ALL SYSTEMS ARE IN TOLERANCE AND FUNCTIONING AS REQUIRED. REFER TO NON-ROUTINE TALLEY CARDS N23584, AND N23585 FOR FURTHER DETAILS.
2011
Part: CONTROL UNIT — DEFECTIVE (SPOILER SYS) · airframe 17,291 hrs · 14,731 cycles
GROUND SPOILERS DEPLOY ADVISORY POSTED ON TAKEOFF AT THROTTLE UP. REMOVED NR 1 SECU; REMOVED NR 2 SECU. REMOVED AND REPLACED ASCU & OP CHECK GOOD IAW AMM 32-44-16. PARTS EFFECTIVITY VERIFIED. INSTALLED SERVICEABLE SECU IN NR 1 POSITION IAW AMM 27-61-04. OP'S CHECKED GOOD AT THIS TIME. VERIFIED PART EFFECTIVITY. INSTALLED SERVICEABLE SECU IN NR 2 POSITION IAW AMM 27-61-05-04 OP'S CHECKED GOOD AT THIS TIME VERIFIED PART EFFECTIVITY. SPOILER SYS INTERFACE WITH ASCU, THROTTLE CONTROL & RA SYS CHECKS GOOD IAW AMM 27-60-00. NO DEFECTS FOUND ON TAXI CHECK.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,142 hrs · 14,595 cycles
F/AS FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY IAW AMM 25-60-00, OPC GOOD OK FOR SERVICE. VERIFIED PARTS EFFECTIVITY.
Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 17,112 hrs · 14,563 cycles
STAB CH 2 INOP STATUS MSG WILL NOT EXTINGUISH. REMOVED AND REPLACED HSTA IAW AMM 27-42-01. SEE AML 763415 DISCREPANCY NR 1 FOR OPS CHECK OF STAB TRIM SYSTEM. VERIFIED PARTS EFFECTIVITY.
2010
Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 15,463 hrs · 13,037 cycles
HYD PUMP 3A LEAKING. DEFERRED IAW MEL 29-12-01.
Part: RAMP — CORRODED (GALLEY CART) · corrosion level 2 · airframe 14,971 hrs · 12,534 cycles
SERVICE DOOR GALLEY CART RAMP CORROSION FOUND. REMOVED AND REPLACED SERVICE DOOR GALLEY CART RAMP.
Part: IDG — LOW (NR 1 ENGINE) · airframe 13,683 hrs · 11,291 cycles
IDG 1 CAUTION ON BEGINNING OF TAKEOFF ROLL AFTER CLEARED RUNWAY, IDG CAUTION WENT AWAY AND WAS REPLACED WITH GEN 1 OFF CAUTION (LOW SPEED ABORT). SERVICED NR 1 IDG AND PERFORMED OPS CHECK OF NR 1 IDG BY RUNNING NR 1 ENGINE IAW CRJ AMM 12-13-24. OPS CHECK GOOD. ACFT OK FOR SERVICE.
2009
Part: COALESCER BAG — CONTAMINATED (AC BAY) · airframe 12,815 hrs · 10,456 cycles
XNA/MEM WHILE DESCENDING THROUGH 100000FT CREW NOTICED A CHEMICAL SMELL IN THE COCKPIT CAUSING DISCOMFORT. BOTH PILOTS DONNED OXYGEN MASKS, DECLARED AN EMERGENCY, QRH FOLLOWED WITH UNEVENTFUL LANDING IN MEM. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT AND RIGHT COALESCER BAGS CONTAMINATED / DIRTY. BAGS REPLACED PER BOMBARDIER AMM 21-51-13, OPERATIONAL CHECKS PERFORMED WITH NO SYSTEM DEFECTS FOUND.
2005
Part: CONTROL SYSTEM — FAILED (TE FLAPS)
(REF NR: 05-076) FLAP FAIL ON APPROACH WHEN GOING FROM 20 TO 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K)