N209WQ
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
63 reports on file, 2009-08-27 – 2015-11-07.
Part: SKIN — GOUGED (BS 258-281) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND A GOUGE IN THE ACFT SKIN ON THE RT SIDE BETWEEN FRAME X258.5 TO X281.00, ALONG STRINGER 16S. MAINTENANCE PERFORMED MAJOR REPAIR TO THE ACFT SKIN ON THE RT SIDE BETWEEN FRAME X258.5 TO X281.00, ALONG STRINGER 16S ON SKIN PANEL, PN: 85360131 IAW RD 8/4-53-7153. MAINTENANCE FABRICATED DOUBLER AND FILLER FROM 2024-T3, .063 MATERIAL. REF PO 4591 FOR MATERIAL USED.
Part: SKIN — DENTED (ZONE 200) · airframe 13,580 hrs · 13,348 cycles
DURING MAINTENANCE, TWO DENTS ON LT FUSALAGE SKIN.
Part: SKIN — DENTED (BS 111) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND DENT ON FORWARD FUSELAGE SKIN APPROXIMATELY 4.5 FORWARD OF FS X-111.000 AND 2.250 UP FROM STIFFENER 12P. DAMAGE WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED ON PN 85313721 IAW RD 8/4-53-7129 AND SRM 51-42-05-02-01. REF VP-034491-2015, OP508.
Part: SKIN — DENTED (BS 281-301) · airframe 13,580 hrs · 13,348 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK DURING COMPLIANCE OF REPETITIVE INSPECTION FOR RD 8/4-53-2987 FOUND MORE DAMAGE TO AREA BETWEEN BS X281.00 - X301.00 AND STRINGERS 9P-13P. MAINTENANCE REMOVED DAMAGED AREA OF SKIN PANEL, PN 85360131 AND INSTALLED A DOUBLER REPAIR IAW RD 8/4-53-7124. FOR DETAIL OF WORK PERFORMED SEE VP-034500-2015, WO VP034500-N, OP-019.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND SUSPECT CORROSION UNDER THRESHOLD OF FWD EMERGENCY EXIT. MAINTENANCE R & R BEAM, PN 85329514-101 IAW SRM 51-42-05-02-01, REF OP 429.
Part: SKIN — GOUGED (ZONE 100) · airframe 13,580 hrs · 13,348 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND SMALL GOUGE ON LOWER CENTER FUSELAGE NEAR BS X1.00 BETWEEN STR 33 TO 32P. MAINTENANCE BLENDED PANEL 85327051 IAW RD 8/4-53-7136. REF WORK PACKET CO VP-034491-2015, WO VP-034491-N, OP-426.
Part: SEAT TRACK — CORRODED (BS 701-728) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND LT INBD SEAT TRACK AT BS 701- 728.10, LBL-12.5, HAS MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R SEAT TRACK IAW SRM 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (BS 701-728) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND RT OTBD SEAT TRACK AT BS 701- 728.10, RBL 27 HAS MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R SEAT TRACK IAW SRM 51-40-07-02-01.
Part: SEAT TRACK — CORRODED (BS 701-728) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK AT BS 701-728.10, RBL- 1.5, MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R SEAT TRACK IAW SRM 51-42-05-02-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND LT INBD SEAT TRACK BS X-39 - BS 94.80 HAS MULTIPLE AREAS OF POSSIBLE CORROSION. R & R SEAT TRACK IAW SRM 51-42-05. REF VISIT PACKAGE, VP-034491-2015, OP356.
Part: SEAT TRACK — CORRODED (BS 94-236) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK FOUND LT INBD SEAT TRACK BS 94.8- 236 HAS MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R SEAT TRACK IAW SRM 51-40-15-02-01.
Part: SEAT TRACK — CORRODED (BS 564-664) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND LT INBD SEAT TRACK BS 564.5 - 664.5 HAS MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R THE SEAT TRACK IAW SRM 51-42-05-02-01 AND 51-41-00-00-01.
Part: SEAT TRACK — CORRODED (BS 604-664) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK BS 604.5 - 664.5 HAS MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R RT INBD SEAT TRACK IAW SRM 51-42-05-02-01.
Part: A/C PACK — CORRODED (BS 665-700) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK FOUND SUSPECT POSSIBLE CORROSION AT BOTTOM OF AFT ENTRY DOOR CUT OUT UNDER THRESHOLD. MAINTENANCE R & R EDGE ANGLE, PN 85339512-101 AT BOTTOM OF AFT ENTRY DOOR CUT OUT UNDER THRESHOLD, IAW SRM 51-42-45-02-01, REF OP 358.
Part: SEAT TRACK — CORRODED (BS 534-604) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK BS 564.50 - BS 604.50 HAS MULTIPLE AREAS OF POSSIBLE CORROSION. MAINTENANCE R & R SEAT RAIL AT BS 564.50 - BS 604.50, PN 85338210-113 IAW SRM 51-40-15-02-01.
Part: SEAT TRACK — CORRODED (BS 229-571) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND RT OTBD SEAT TRACK BS 229.50-571.50 HAS MULTIPLE ARES OF POSSIBLE CORROSION. MAINTENANCE R & R THE SEAT TRACK. ACFT
Part: SKIN — DAMAGED (ZONE 800) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND DOOR SEAL FASTENER PULLED THROUGH SKIN OF AFT SERVICE DOOR LOCATED LOWER AFT AREA. REPAIRED DOOR OUTER SKIN, PN 85247101 IAW RD 8/4-52-1369, REF OP315 ACFT REMAINS IN RFD FOR COMPLETION.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND SUSPECT FRETTING DAMAGE ON FORWARD EDGE OF LANDING FOR PANEL 262FT. EMERGENCY MAINTENANCE BLENDED PANEL 262 FT IAW RD8/4-53-451, PN 85713404, REF VP-034491-N OP191.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND SUSPECT FRETTING DAMAGE ON FORWARD EDGE OF LANDING PN 85713508 FOR PANEL 262HT. MAINTENANCE REMOVED CORROSION FROM L/E OF LANDING FOR PANEL 262HT IAW RD 8/4 53-451. REF MAINTENANCE PACKAGE, VP-034491-2015, OP195.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND SUSPECT FRETTING DAMAGE ON FORWARD EDGE OF LANDING PANEL 261FT. EMERGENCY MAINTENANCE REMOVED CORROSION ON FORWARD EDGE OF LANDING PANEL 261FT, PN 85713508, REF RD 8/4-53-451. FOR WORK PERFORMED REF VP-034491-2015, OP201.
Part: PANEL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE BOTTOM OF THE FORWARD BAGGAGE DOOR CUTOUT TO CHANNEL, PN: 85329604-001 AND EDGE PANEL, PN: 85329603-103. MAINTENANCE R & R THE CHANNEL, PN: 85329604-001 AND EDGE PANEL, PN: 85329603-103 AT THE BOTTOM OF THE FORWARD BAGGAGE DOOR CUTOUT IAW SRM 51-40-07, 51-42-90, 51-42-75, 51-23-00, 51-42-45 & 51-42-05.
Part: CHANNEL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, MAINTENANCE REPORTED CORROSION AT THE BOTTOM OF THE FORWARD BAGGAGE DOOR CUTOUT TO CHANNEL, PN: 85329604-001 AND EDGE PANEL, PN: 85329603-103. MAINTENANCE R & R THE CHANNEL, PN: 85329604-001 AND EDGE PANEL, PN: 85329603-103 AT THE BOTTOM OF THE FORWARD BAGGAGE DOOR CUTOUT IAW SRM 51-40-07, 51-42-90, 51-42-75, 51-23-00, 51-42-45 & 51-42-05.
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION AT BOTTOM OF SERVICE DOOR. MAINTENANCE REPAIRED BY COMPLYING WITH SRM 51-42-05-02-01,51-42-45-02-01. ACFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.
Part: SKIN — CHAFED (FUSELAGE) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, FOUND RUBBING/CHAFE DAMAGE TO ACFT SKIN UNDER AFT CORNER OF AFT BAGGAGE DOOR CUTOUT. MAINTENANCE BLENDED IAW RD 8/4-53-7121.
Part: SKIN — DENTED (ZONE 100) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND DENT RT FUSELAGE AFT OF ICE SHIELD. MAINTENANCE REPAIRED IAW RD 8/4-53-7099. ACFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: CABLE — BROKEN (PAX DOOR) · airframe 13,537 hrs · 13,301 cycles
CREW REPORTED THAT WHEN THE F/A OPENED THE MAIN CABIN DOOR, THE DOOR ASSIST CABLE SNAPPED. MAINTENANCE INSPECTED, R & R THE LOWER CABLE ASSEMBLY IAW AMM AND OPS CHECKED GOOD.
Part: SKIN — DENTED (ZONE 100) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, RE-EVALUATED DENT ON LOWER FUSELAGE SKIN FROM FS -34.100 TO FS -18.250 BETWEEN STR 33 AND STR 32L. REF MAINTENANCE WC, JOB 8420915, OP 20. MAINTENANCE BLENDED SKIN DAMAGED AREA FS -34.100 TO FS -18.250 BETWEEN STR 33 AND STR 32L, PN 85313720 IAW RD 8/4-53-7093.
Part: BULKHEAD WEB — CHAFED (BS 124-128) · airframe 13,580 hrs · 13,348 cycles
DURING HEAVY CHECK, MAINTENANCE FOUND BULKHEAD INSIDE PANEL 113AL TO HAVE CHAFE DAMAGE CAUSED BY BATTERY. MAINTENANCE REMOVED DAMAGE AND INSTALLED A DOUBLER REPAIR IAW RD 8/4-53-7067.
Part: SKIN — DENTED (ZONE 200) · airframe 13,580 hrs · 13,348 cycles
DENTS FOUND ON FUSALAGE SKIN.
Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 13,418 hrs · 13,168 cycles
CREW REPORTED THAT THE EMERGENCY LIGHTS WERE STAYING ON WITH THE POWER OFF. MAINTENANCE R & R THE K1 & K2 RELAYS IAW AMM AND OPS CHECKED GOOD.
Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 13,414 hrs · 13,163 cycles
CABIN EMERGENCY LIGHT WOULD NOT SHUT OFF AFTER TURNING ACFT POWER OFF. MAINTENANCE REMOVED, INSPECTED AND INSTALLED K1 & K2 RELAYS ON CIRCUIT BREAKER PANEL ASSY IAW AMM AND OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 13,411 hrs · 13,160 cycles
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT BATTERIES WERE INOPERATIVE. MAINTENANCE R & R FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,388 hrs · 13,136 cycles
MAINTENANCE REPORTED THAT THE RT FORWARD EMERGENCY EXIT DOOR EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LAMPS IAW AMM AND OPS CHECKED GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,291 hrs · 13,038 cycles
MAINTENANCE REPORTED THAT THE CENTER AISLE AFT EMERGENCY EXIT SIGN WAS ONLY ILLUMINATED FOR 4 SECONDS. MAINTENANCE R & R THE AFT FORWARD EMERGENCY LIGHT POWER SUPPLY IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: SEAL — FAILED (L2 DOOR) · airframe 13,237 hrs · 12,980 cycles
F/A REPORTED THAT THE SEAL ON THE L2 DOOR IN THE UPPER RT CORNER POPPED AND COULD SEE DAYLIGHT. CAPTAIN REPORTED THAT THE CABIN WAS NOT HOLDING PRESSURE AND ELECTED TO RETURN TO DEPARTURE. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE HEATED CHECK VALVE AND MAIN CABIN DOOR SEAL IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: SEAL — LEAKING (L1 DOOR) · airframe 13,154 hrs · 12,898 cycles
CREW REPORTED A NOISE AT THE L1 DOOR AND LOSS OF PRESSURE. CREW DID NOT DECLARE AN EMERGENCY, RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT WAS FLOWN VIA MAINTENANCE FERRY WHERE MAINTENANCE REPLACED THE AFT BAGGAGE DOOR PRESSURE SEAL AND THE DESICCANT FILTER AND INSPECTED THE DOOR SEAL RESERVIOR DRAIN VALVE IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,929 hrs · 12,675 cycles
CREW REPORTED THAT THE F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
Earlier reports · 2009–2014 · 26 reports
2014
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 12,230 hrs · 11,934 cycles
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,186 hrs · 11,897 cycles
MAINTENANCE REPORTED THE EMERGENCY LIGHT STRIP IN FRONT OF THE LAVATORY ARE NOT WORKING. MAINTENANCE R & R THE LIGHT IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: BOLT — SHEARED (PAX DOOR) · airframe 10,804 hrs · 10,516 cycles
CREW REPORTED THAT THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED AND FOUND THE RAIL PIN BOLT HAD SHEARED. ACFT WAS FLOWN VIA MAINTENANCE FERRY TO IAD WHERE MAINTENANCE R & R BOLT IAW AMM. ACFT IS GOOD FOR SERVICE.
2013
Part: SEAL — CONTAMINATED (L1 DOOR) · airframe 10,334 hrs · 10,005 cycles
CREW REPORTED A LOUD SQUEALING NOISE AND LIGHT SHINNING THRU L1 DOOR. PRESSURIZATION WAS NORMAL AND NOISE WENT AWAY ON REACHING ALTITUDE. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR SEAL AND FOUND WATER IN THE SEAL. DRAINED TANK AND CHECKED FILTERS IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,312 hrs · 9,986 cycles
CREW REPORTED THAT THE FORWARD F/A EMERGENCY LIGHT SWITCH WAS NOT WORKING. R & R THE EMERGENCY LIGHT SWITCH IAW AMM AND OPS CHECKED GOOD. AIRCRAFT IS GOOD FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 10,246 hrs · 9,920 cycles
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS NOT WORKING. MAINTENANCE INSTALLED NEW BATTERIES IAW AMM AND OPS CHECKED GOOD.
Part: SKIN — DENTED (ZONE 200) · airframe 9,375 hrs · 9,014 cycles
DURING HEAVY CHECK, FOUND DENT OUTSIDE FUSELAGE RT SIDE AT BS 509.5, STRINGER 22. MX BLENDED GOUGE FOUND TO OUT OF LIMITS AND PERFORMED REPAIR IAW RD 8/4-53-5474 ISSUE 1. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,375 hrs · 9,014 cycles
DURING HEAVY CHECK, FOUND RT SIDE WALL Y40.950 SEAT TRACK SECTION X94.800 TO X209.000 HAS BLENDED UNPROTECTED AREAS WITH CORROSION PRESENT ALONG THE ENTIRE LENGH. MX R & R SEAT TRACK IAW SRM 51-42-05 & 51-40-15.
Part: SEAT TRACK — CORRODED (BS 209-571) · corrosion level 2 · airframe 9,375 hrs · 9,014 cycles
DURING HEAVY CHECK, FOUND RT SIDEWALL Y40.950 SEAT TRACK BS 209 TO 571.5 HAS BLENDED, UNTREATED AREAS WITH CORROSION PRESENT ALONG ENTIRE LENGTH. MX R & R SEAT TRACK IAW SRM 51-40-15/51-42-05.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,375 hrs · 9,014 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND LVL 2 CORROSION ON SEAT RAIL BETWEEN X698.00 AND X722.102 AT Y+9250. MX R & R SEAT RAIL PN 85338210-119 IAW SRM 51-40-07. ACFT REMAINS FOR HEAVY CHECK COMPLETION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,375 hrs · 9,014 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK FOUND LVL 2 CORROSION ON SEAT TRACK UNDER G3 GALLEY AREAAT X698.00 AND X722.102. MX R & R SEAT RAIL, PN 85338210-111 IAW SRM 51-42-05. ACFT REMAINS FOR HEAVY CHECK COMPLETION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,375 hrs · 9,014 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND LVL 2 CORROSION ON SEAT RAIL BETWEEN X648.00 AND X722.102. MX R & R SEAT RAIL, PN 85337843-105 IAW SRM 51-42-05. ACFT REMAINS FOR HEAVY CHECK COMPLETION.
Part: SKIN — DENTED (ZONE 200) · airframe 9,375 hrs · 9,014 cycles
DURING HEAVY CHECK, FOUND ONE DENT ON LT FUSELAGE SKIN FS 866.303 TO 882.703 BETWEEN S20-21L. FOUND OUT OF LIMITS IAW SRM 53-50-31 AND RD 8/4-53-666 ISSUE 1. PERFORMED REPAIR IAW EO Q400-53-00273.
2012
Part: FADEC — DEFECTIVE (ENGINE) · airframe 8,292 hrs · 7,989 cycles
A/C RETURNED TO FIELD DUE TO A POWER PLANT MESSAGE. MX REMOVED AND REPLACED THE FADEC.
2011
Part: RIB — CRACKED (RT WING) · airframe 7,943 hrs · 7,622 cycles
UPPER AND LOWER END OF I/B AND O/B CLOSING RIBS ON RT WING I/B LEADING EDGE 611AR ARE CRACKED. REF TD 400-57-11-17 AND MM 409 400232 FOR REPAIR DETAILS.
Part: CONNECTOR — LOOSE (CARGO DOOR) · airframe 6,297 hrs · 6,083 cycles
DURING EN ROUTE CLIMB AT APPROXIMATELY FL200, THE CREW RECEIVED MASTER WARNING INDICATION FOR FUSELAGE DOORS/FWD CARGO. CREW LEVELED THE AIRCRAFT AND RAN QRH. VERIFIED PRESSURIZATION WAS HOLDING AND ANNOUNCED INTENTIONS TO ATC TO DIVERT TO DAL. FUSELAGE DOORS/FWD CARGO INDICATION EXTINGUISHED AFTER APPROXIMATELY 4 MINUTES AND DID NOT ILLUMINATE AGAIN DURING FLIGHT. FLIGHT LANDED IN DAL WITHOUT FURTHER INCIDENT. FOUND PROX SWITCH ON FWD CARGO DOOR FRAME PLUG TO BE LOOSE. RE-TIGHTENED CONNECTOR. ALSO LUBED ALL TRACK GUIDES, ROLLERS. OPS CHECKED GOOD.
Part: HANDLE — NOT SEATED (CARGO DOOR) · airframe 6,283 hrs · 6,071 cycles
AT CRUISING ALTITUDE 22000FT, 150 MILES EAST OF MFE, FWD CARGO DOOR WARNING LIGHT ILLUMINATED. CREW RAN THE CHECKLIST AND LANDED AT NEAREST SUITABLE AIRPORT (VCT). FOUND DOOR HANDLE NOT SEATED PROPERLY RESEATED HANDLE IAW AMM 52-10-00, OPS CHECKED GOOD.
Part: WARNING SYSTEM — MALFUNCTIONED (TE FLAP) · airframe 6,297 hrs · 6,083 cycles
THE FLAP POWER LIGHT ILLUMINATED IN FLIGHT AT 10 DEGREES. CREW FOLLOWED THE CHECK LIST AND DECLARED EMERGENCY. LANDED WITHOUT FURTHER COMPLICATIONS. PERFORMED FUNCTIONAL TEST OF FLAP CONTROL SYS IAW Q400 AMM 27-51-00-720-801. OPS CHECK GOOD. NO FLAP PROBLEMS NOTED DURING FUNCTIONAL TEST.
Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 5,874 hrs · 5,706 cycles
FORWARD BAG DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. DIVERTED TO ALB AS A PRECAUTION. LANDED WITHOUT FURTHER COMPLICATIONS. MAINTENANCE CHECKED THE DOOR AND FOUND THE HANDLE IS NOT FLUSH.
2010
Part: WARNING SYSTEM — FALSE ACTIVATION (CABIN PRESSURE) · airframe 5,456 hrs · 5,316 cycles
DURING CRUISE THE CABIN PRESSURE LIGHT ILLUMINATED AND CREW DECLARED EMERGENCY IN ORDER TO BE ABLE TO DESCEND TO 10,000 FT AND PROCEED WITH CHECKLIST. WHILE GOING THROUGH CHECKLIST DISCOVERED THE ISSUE AND CORRECTED. CANCELED EMERGENCY AND CLIMBED BACK TO CRUISING ALTITUDE. CREW DID VERIFY BEFORE DEPARTURE THAT DOORS WERE SECURE.
Part: WARNING SYSTEM — ACTIVATED (CARGO DOOR) · airframe 5,393 hrs · 5,260 cycles
FWD BAGGAGE LIGHT ILLUM IN FLT, DIVERTED TO BUF. ON CALL MX, RE-SECURED IAW 52-32-00-710-801, OPS CHECK GOOD.
Part: ARM — DEFECTIVE (SPOILER) · airframe 5,082 hrs · 4,990 cycles
SPOILER 1 PUSH OFF LIGHT ILLUMINATED, RETURNED TO GATE. REMOVED AND REPLACED ARMS ON THE NR 1 SPOILER MICRO SWITCH.
Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 4,940 hrs · 4,853 cycles
DURING CLIMB, AT APROX 14,000 FT CREW NOTICED GEN LIGHT ILLUMINATE. CREW COMPLIED WITH CHECKLIST AND AFTER CONFERRING WITH DISPATCHER, RETURNED TO EWR. CREW DID NOT DECLARE EMERGENCY BUT EWR TOWER DISPATCHED EMERGENCY EQUIPMENT. THE FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LT DC GEN.
Part: RECEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 35,788 hrs · 36,548 cycles
WEATHER RADAR STOPPED WORKING DURING CRUISE. DIVERTED TO ALTERNATE DUE TO THUNDERSTORMS EN ROUTE AND DESTINATION. REMOVED AND REPLACED RADAR RECEIVER.
Part: O-RING — DAMAGED (FUEL SYSTEM) · airframe 4,727 hrs · 4,650 cycles
DURING TAXI, F/A REPORTED TO CAPTAIN THAT THERE WAS AN ODOR IN THE CABIN. CAPTAIN SMELLED FAINT TRACE OF ODOR AND RETURNED TO GATE. FOUND FUEL LEAKING FROM NR 2 ENG TRANSFER TUBE ON FUEL OIL HEAT EXCHANGER. REMOVED AND REPLACED O-RINGS ON THE FUEL OIL HEAT EXCHANGER TRANSFER TUBES IAW Q400 AMM 73-11-01, OPS CHECKED GOOD.
2009
Part: SELECTOR VALVE — FAULTY (LANDING GEAR) · airframe 2,809 hrs · 2,806 cycles
CREW REPORTED GEAR WOULD NOT EXTEND. CREW RAN CHECK LIST AND MANUALLY EXTENDED GEAR, LANDED NO ISSUES. DIVERTED FROM FLIGHT PATH. CREW DID NOT DECLARE EMERGENCY. CREW REPORTED NO NOSE STEERING AND NO BRAKES. TUGGED FROM RUNWAY. REMOVED AND REPLACED SELECTOR VALVE P/N 48300-3.