N303DQ
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.
23 reports on file, 2010-03-31 – 2020-09-23.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,010 hrs · 15,875 cycles
DURING INSPECTION FOUND LEFT SIDE OVER WING EMERGENCY AND AFT GALLEY EMERGENCY SIGNS INOPERATIVE. R& R BATTERIES, PER B737 AMM 33-51. OPS CK NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,627 hrs · 15,592 cycles
DURING INSPECTION, FOUND MULTIPLE EMERGENCY LIGHTS IN FWD GALLEY INOPERATIVE. R/R BATTERY PACK @ LOC M1675. OPS CHK GOOD.
Part: COMPRESSOR BLADE — DAMAGED (NR 2 ENGINE) · airframe 35,598 hrs · 15,576 cycles
A/C 3603 - IFSD/ATB - RETURNED TO ATL AND DECLARED AN EMERGENCY DUE TO NUMBER 2 ENGINE FAILURE. FLIGHT CREW PERFORMED QRH AND SHUT DOWN THE ENGINE. CORRECTIVE ACTION: INSPECTION FOUND DAMAGE TO 8TH STAGE HPC BLADES. REPLACED #2 ENGINE REFER TO LOG PAGE 1558574.
Part: ENGINE — FAILED (RIGHT) · airframe 34,896 hrs · 15,212 cycles
SHIP 3603 - ATO -DURING TAKEOFF ROLL THE RIGHT ENGINE STALLED AND FLAMES WERE REPORTED FROM TAILPIPE. CREW ABORTED TAKEOFF AND SHUTDOWN THE RIGHT ENGINE. CORRECTIVE ACTION: BOROSCOPE INSPECTION REVEALED HPC DAMAGE. MAINTENANCE REPLACED THE RIGHT ENGINE, AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 2010–2019 · 19 reports
2019
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,421 hrs · 14,988 cycles
(LOG 6585871) DURING INSPECTION FOUND FLOOR AISLE EMERGENCY LIGHTRS @ ROWS 18-23 INOPERATIVE. R&R BATTERY PACK AT LOC M1670. CKS GOOD. A/C OK FOR SVC. REF. B737 AMM 33-51.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,108 hrs · 14,374 cycles
DURING INSPECTION FOUND R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE ABOVE DOOR. R/R POWER SUPPLY BATTERY PACK M1672 IAW B37 AMM 33-51. OPS NML.
2018
Part: LIGHT — LOOSE (SEAT 28D) · airframe 29,556 hrs · 12,414 cycles
SEAT 28D MOUNTED EMERGENCY LIGHT LOOSE. SECURED THE LIGHT. OPS NORMAL.
2017
Part: LIGHT — DETACHED (SEAT 27D) · airframe 29,044 hrs · 12,145 cycles
DURING INSPECTION, FOUND THE EMERGENCY LIGHT UNDER SEAT 27D WAS DETACHED. MAINTENANCE ATTACHED THE EMERGENCY LIGHT AND OPS CHECKED GOOD.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 28,633 hrs · 11,919 cycles
DURING INSPECTION, FOUND EMERGENCY EXIT COVER DIFFUSER LENS DETACHED. MAINTENANCE REINSTALLED THE LENS.
Part: GUIDE ARM — DEFECTIVE (L1 DOOR) · airframe 28,624 hrs · 11,910 cycles
DURING OPERATIONS, DOOR 1L DIFFICULT TO OPEN. MAINTENANCE REPLACED FORWARD ENTRY DOOR GUIDE ARM PER AMM 52-11. DOOR OPS CHECKS GOOD.
Part: STRINGER — CRACKED (BS 500D) · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND CRACKED ON STRINGER 19R, BS 500D IN FORWARD CARGO COMPARTMENT. MAINTENANCE REPAIRED THE STRINGER IAW SRM 53-30-03, REPAIR 1.
Part: SUPPORT — CRACKED (BS 737-787) · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND A CRACK ON THE SUPPORT ZEE STRINGER 25R, BS 767 - 787 IN AFT CARGO BAY. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-10-02, 51-40-02, AND DRAWING 146A0081.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION FOUND CORROSION ON FLOORBEAM LOCATED BS 986.5 LBL 45.5 AT AFT GALLEY AREA. MAINTENANCE REPAIRED FLOORBEAM AT BS986.5 FROM LBL 0 TO LBL 50 PAX CABIN AS PER SRM 53-70-51 REPAIR 4.
Part: SUPPORT — CORRODED (BS 727A-767) · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND CORROSION ON THE SUPPORT ZEE STRINGER 25R BETWEEN BS 727A - 767. REPLACED THE SUPPORT ZEE IAW SRM 51-10-02, 51-40-02, AND DWG 146A7500.
Part: WEB — CORRODED (BS 716-727) · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND CORROSION ON THE WEB AT BS 716.3 - 727. REPLACED THE WEB IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 144A5900.
Part: WEB — CORRODED (BS 695-706) · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND CORROSION ON THE WEB AT BS 695 - 706. REPLACED THE WEB IAW SRM 51-10-02, PARAGRAPH 9, AND DRAWING 144A5900.
Part: BULKHEAD WEB — CRACKED · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND CRACK ON THE BULKHEAD WEB, WL 208.1, LBL 13. REPLACED BULKHEAD WEB IAW SRM 57-10-02; 51-40-02 AND DWG 148A0922.
Part: SKIN — CRACKED · airframe 27,334 hrs · 11,162 cycles
DURING INSPECTION, FOUND A CRACK ON CUTOUT ON EXTERNAL GROUND ELECTRICAL POWER AFT EDGE ON LOWER FUSELAGE. REPAIRED IAW SRM 53-10-15, REPAIR 4.
Part: SIGN — BROKEN (CABIN) · airframe 27,096 hrs · 11,031 cycles
DURING INSPECTION FOUND RIGHT EXIT DOOR EMERGENCY EXIT SIGN BROKEN. MAINTENANCE R AND R RT EXIT SIGN. CKS GOOD PER AMM 33-51.
2013
Part: LIGHT — INOPERATIVE (SEAT 13D) · airframe 15,607 hrs · 5,498 cycles
DURING INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. MX REPLACED EMERGENCY LIGHT ASSY AT SEAT 13D IAW AMM33-51-41. OPS CHECK OK.
2012
Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 27,335 hrs · 11,164 cycles
DURING INSPECTION, FOUND AN 8 INCH CRACK IN THE VAPOR BARRIER FORWARD LOWER WALL OF RIGHT WHEEL WELL AT RBL 20. MAINTENANCE PERFORMED PERMANENT REPAIR.
Part: MECHANISM — OUT OF LIMITS (RT ELEVATOR TAB) · airframe 12,451 hrs · 4,181 cycles
08MAR12; WHILE WORKING PSV4, OPN 59086 FOUND THE RT ELEV CONTROL TAB MECHANISM, "GAP CHECK BETWEEN OUTER FACE OF THE AFT LUG AND THE SWAGE RING" BEYOND LIMITS. NR 58 WAS WRITTEN FOR MECHANISM REPLACEMENT, PART NBR 251A2430-18. FCF TO BE COMPLIED WITH DUE TO REPLACEMENT. REPLACEMENT PERFORMED PER ERA 501153-14AD_(MRR 121486)(DALA1214863603).
2010
Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 5,519 hrs · 1,787 cycles
DURING FLIGHT, F/A REPORTS DETECTED AN ELECTRICAL SMELL NEAR BACK OF THE CABIN BY ROW 27 ABC. MX SUSPECTED BALLAST AS CAUSE. TURNED CAB/UTIL SWITCH OFF AND SMELL SUBSIDED. NO SMOKE OBSERVED. TURNED ON GALLEY POWER, RAN OVENS, NO ABNORMAL SMELLS NOTED.