N27515
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES, INC. (CALA) | Operator | on 2024-10-24 | Operator named in NTSB report |
Accident & incident history
Operated by United Airlines (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.
18 reports on file, 2022-02-17 – 2026-08-01.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 17,688 hrs · 5,840 cycles
FWD HORSESHOE PANEL BATTERY PACK M02816 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M02816 IAW AMM 33-51-06-960-802. OPS CHKD GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 17,688 hrs · 5,840 cycles
RIGHT FWD OVERWING BATTERY PACK M01695 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M01695 IAW AMM 33-51-06-960-802. OPS CHKD GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 17,688 hrs · 5,840 cycles
LEFT FWD OVERWING BATTERY PACK M01694 INOPERATIVE. REMOVED AND REPALCED THE BATTERY PACK M1694 IAW AMM 33-51-06-960-802. OPS CHKD GOOD.
Part: SKIN — GOUGED (ZONE 100) · airframe 17,688 hrs · 5,840 cycles
LEFT RAM AIR INLET DUCT CLAMP IS GOUGING THE STRUCTURE. ACCOMPLISHED SKIN BLEND REPAIR PER REO-G25998 REV IR AND EC/RA 5715-01121.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,688 hrs · 5,840 cycles
MAIN CABIN BS 951 FLOOR SUPPORT CORRODED. MAIN CABIN BS 951 FLOOR SUPPORT REMOVED AND REPLACED. NO ISSUES NOTED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,688 hrs · 5,840 cycles
MAIN CABIN AFT WET AREA FLOOR SUPPORT AT BS 951, RBL 40 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND BAC DWG 147A5650 REV -.
Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,688 hrs · 5,840 cycles
MAIN CABIN AFT WET AREA LAV SUPPORT AT BS 947 - 967, RBL51 CORRODED. REMOVED & REPLACED LAV SUPPORT IAW SRM 51-40-02 & DWG 147A5660-22.
Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,688 hrs · 5,840 cycles
MAIN CABIN, BS 947, LBL 24, LAV SUPPORT CORRODED. THE LAV SUPPORT WAS REMOVED AND REPLACED. REMOVED CORROSION AND EVALUATED AREA WITH ORIGINAL 0.200" REF DWG 147A5650; MATERIAL LOSS .030" AND REMAINING .170" FOUND TO BE OUT OF LIMITS IIAW SRM 53-70-51-1A-1 REMOVED LAV SUPPORT AT LBL24 BETWEEN BS 947 - 967. LOCATED DRILLED AND REPLACED IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 & DWG 147A5650, REV.A.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,688 hrs · 5,840 cycles
LEFT SIDE T CAP AT LBL24 UNDER LAV D AREA AT STA 947 HAVE CORROSION. ALL WORK ACCOMPLISHED AT AAR GSO NON-ROUTINE 9284231. PREFORMED FLAP REPAIR AT BS 947 FROM LBL24 TO RBL58 IAW SRM 53-70-51-2R-5. REMOVED. PERFORMED T-CAP REPAIR AT STA 947 FROM LBL 24 TO RBL 58 IAW SRM 53-70-51-2R-5. REPAIR ACCOMLISHED REFERENCE SRM 53-70-51-2R-5 ADD EMP:AAR QC 444; V900858
Part: PRESSURE DECK — DENTED (ZONE 200) · airframe 17,688 hrs · 5,840 cycles
COCKPIT FLOOR STRUCTURE SKIN BETWEEN BS 250 - 270, LBL 12 - RBL 10 DENTED. REPAIRED AREA IAW SRM 53-10-51-2R-2.
Earlier reports · 2022–2025 · 8 reports
2025
Part: SLIDE — EXPOSED (ZONE 800) · airframe 14,915 hrs · 4,900 cycles
L1 DOOR SLIDE IS EXPOSED AND DOOR IS DIFFICULT TO ARM REPLACED SLIDE DOOR 1L. REF. AMM 25-66-01-000-801, 25-66-01-400-802, 25-66-01-400-803. ACCOMP RII INSPECTION OF DOOR 1L SLIDE INSTALLATION REF. AMM 25-66-01-000-801.
Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 14,689 hrs · 4,822 cycles
NEED INSPECTION OF FWD RIGHT ESCAPE SLIDE DUE TO CATERING ATTEMPTING OPENING DOOR WHILE ARMED. PERFORMED ESCAPE SLIDE PACK VISUAL CHECK IAW AMM 25-66-01-200-802 & ESCAPE SLIDE PACK IONFLATION CYLINDER. BOTH OPS CHECK GOOD AT THIS TIME. NO PRESSURE LOSS ON CYLINDER.
Part: PIN — OUT OF POSITION (ZONE 800) · airframe 14,662 hrs · 4,814 cycles
EMERGENCY ESCAPE SLIDE FOR DOOR R1 HAS A SHORN OFF DRIFT PIN ON THE QUICK RELEASE MECHANISM. DAMAGE IS ON AN ESCAPE SLIDE. UPDATED FOR AN SDR. SAFETY PIN HAS BEEN INSTALLED ON THE R1 SLIDE AS REQUIRED. REPLACED SHORN PIN. LATCH BLOCK ASSEMBLY OPERATES NORMALLY. OK TO CONTINUE.
Part: WIRE — UNSECURE (ZONE 800) · airframe 14,548 hrs · 4,778 cycles
DOOR 2L LOOSE WIRE HANGING BELOW GIRT BAR LEFT SIDE. STOWED BENCH TEST CONNECTOR BACK BEHIND THE SLIDE. OK TO CONTINUE.
Part: LIGHT — UNSECURE (ZONE 200) · airframe 13,791 hrs · 4,529 cycles
EMERGENCY EXIT ROW 21A DOOR PANEL FALLING OUT. REPLACED CAP ON ARM REST. OK TO CONTINUE.
Part: LIGHT — BROKEN (ZONE 200) · airframe 13,172 hrs · 4,331 cycles
EMERGENCY EXIT LIGHT IS BROKEN AND HANGING IN THE AISLE AT 9C. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORMED INTERIM REPAIR PER PART 1 OF ECRA 2520-07881. OPENED DIP TO ACCOMPLISH REPETITIVE INSPECTION PER PART 2 EACH FLIGHT AND ACCOMPLISH PERMANENT REPAIRPER PART 3 WITHIN 3 FLIGHT CYCLES REF ECRA 2520-07881 - PERFORMED INTERIM REPAIR PER PART 1 OF ECRA 2520-07881. OPENED DIP TO ACCOMPLISH REPETITIVE INSPECTION PER PART 2 EACH FLIGHT AND ACCOMPLISH PERMANENT REPAIRPER PART 3 WITHIN 3 FLIGHT CYCLES REF ECRA 2520-07881 CARRIED DIRECTLY BY TOMC TOMC-APPROVAL FROM SC1ELBYC COMMENT TA M&E: 42-9925-8-0270 S/N: 7515 LIMIT: NHA: 42-2000-9-0001 NHA S/N: 7515 INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS REVIEW. CONTROL #: N/A SOURCE DOCUMENT: ECRA 2520-07881 QC CONTROL #: SOURCE DOCUMENT: ECRA 2520-07 REPETITIVE LABOR HOURS: 0001 GROUND TIME: 0001 TERMINATING LABOR HOURS: 0002 GROUND TIME: 0004 QC REVIEW RESECURED AISLE EMERGENCY LIGHT ASSEMBLY IAW IFM 25-22-64-4641. DIP CLEARED. OPS CHECK OF SEAT AISLE LIGHT GOOD. TOMCQC REV PERFORMED
2024
Part: SKIN — DENTED (ZONE 100) · airframe 12,223 hrs · 4,030 cycles
DENT ACROSS STRUCTURE LOCATED AT BS 727F & JUST ABOVE S20R EXTERNAL SKIN PERFORM STEPS E 1-4 AFTER BAG BIN ACCESS NO DAMAGE FOUND TO UNDERLYING STRUCTURE REMVED FASTNERS NEED TO COMPLY WITH REPAIR 4 STEP E (1) (2) (3) EWIS COMPLIED WITH AT STA.727F SEE REF. AMM 20-60-07-910-801. REMOVED SHEAR TIE TO EVALUATE, REF LOG 9674178 FOR SHEAR TIE OF SRM 53-00-01-2R-36. REMOVAL , PERFORMED SKIN CUTOUT TO REMOVE DAMAGE REF SRM 53-00-01-2R-36 , COMPLIED WITH STEPS PARA 4 A-D. REQUEST INSP TO PERFORMED HFEC OF SKIN CUTOUT AND FASTENER HOLES AS REQD PER SRM VERIFIED MATERIALS REQUIRED TO FABRICATE -1 DOUBLER .040 2024-T3 VERIFIED COMPLETION OF SRM 53-00-01-2R-36 PARAGRAPH 4 STEPS H 53-00-01-2R-36 REPAIR 4 STEP E (1), (2) & (3). NO CRACKS NOTED. PO#: 1562637, -2 TRIPLER .063 2024-T3 PO#: 3621067, AND -3 THROUGH N (FABRICATION OF REPAIR PARTS ETC.) AND STEP P (INSTALL OK TO CONTINUE. FILLER .071 2024-T3 PO#: 3210561. OF COUNTERSUNK WASHERS TO SKIN). OK TO PRIME. PERFORMED INSURANCE CUT TO DAMAGE CUTOUT AND DVI OF UNDERLYING MATERIAL VERIFICATION REQUIRED TO FABRICATE -1 DOUBLER .040 ALSO VERIFIED INSURANCE CUT TO DAMAGE CUTOUT AND DVI OF COMPLIED WITH STEPS H THROUGH N (FABRICATION OF REPAIR PARTS COMPLIED WITH STEPS H THROUGH N (FABRICATION OF REPAIR PARTS AND ADJACENT STRUCTURE WITH NO OTHER DEFECTS NOTED REF SRM 2024-T3 PO#: 1562637, -2 TRIPLER .063 2024-T3 PO#: 3621067, AND UNDERLYING AND ADJACENT STRUCTURE REF SRM 53-00-01-2R-36 AND GMM ETC.) AND STEP P.
2022
Part: SHROUD — LOOSE (SEAT8 TO 38) · airframe 3,089 hrs · 1,093 cycles
COACH SEATS AISLE END BAY EPL SHROUDS ARE LOOSE 8,9,10,11,12,15,21,23,24,25,26,32,35,36,37,38C. BLANK TRIM SHROUD 9,11,15,22,23,24,26,39D. SECURED ALL ABOVE LISTED EPL AND BLANK TRIM SHROUDS IAW CMM 25-21-65. REF FIG. #16. ALL EPL OPS. CHK. NORMAL.