N233JQ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
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.
45 reports on file, 2020-02-27 – 2026-07-12.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 43,692 hrs · 28,451 cycles
BLEED 2 OVERPRESSURE RIGHT AFTER TAKE OFF. MAX OBSERVED PSI 110. FOLLOWED QRH PROCEDURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED EMB FIM TASK 36-11-00-810-812-A AND 36-14-00-810-818-A. NO DEFECTS NOTED. PERFORMED ENGINE PNEUMATIC BLEED SYSTEM OPS CHECK, OPS CHECK GOOD.
Earlier reports · 2020–2025 · 44 reports
2025
Part: RIB — CRACKED (ZONE 500) · airframe 41,464 hrs · 26,783 cycles
LEFT WING RIB 4A UPPER AND LOWER FASTENER HOLES FOUND TO HAVE CRACKS PRESENT INSIDE OF HOLES AT 12 O'CLOCK POSITIONS. REPAIRED LT WING RIB 4A UPPER AND LOWER FASTENER HOLES REF. ETD2025-170-925529
Part: BEAM — MISLOCATED (ZONE 200) · airframe 41,464 hrs · 26,783 cycles
AFT SERVICE DOOR LOWER BEAM HAD 2 HOLES MIS-DRILLED, INSTALLED HAT BUSHINGS.
Part: SKIN — CRACKED (ZONE 500) · airframe 41,464 hrs · 26,783 cycles
LEFT WING LOWER SKIN IS CRACKED AT RIB 4A AND SPAR 2. REPAIRED LH WING LOWER SKIN AT RIB 4A AND SPAR 2 ETD2025-170-924781 REV.: B
Part: BATTERY — NO TEST (ZONE 200) · airframe 41,015 hrs · 26,426 cycles
L2 DOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. R&R EMERGENCY BATTERY 3.
Part: ENGINE — STALLED (ZONE 400) · airframe 40,783 hrs · 26,262 cycles
COMPRESSOR STALL IN AIR. NUMBER 2 ENGINE, TWO SETS OF LOUD BANGS FOLLOWED BY HIGH ITT INDICATION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E2.
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,752 hrs · 23,243 cycles
LIGHTING STRIKE DAMAGE AT FRA 24 TO FRA 25 BELOW STR 25L. FABRICATED AND INSTALLED REPAIR IAW EMB 170/175 SRM 53-21-01 REPAIR 13. ALSO REF VP-018676-2023 N/R 14 C1 THRU C3 FOR WORK PERFORMED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 36,752 hrs · 23,243 cycles
LIGHTING STRIKE DAMAGE AT FRA 21 ABOVE STR 26L.FABRICATED AND INSTALLED REPAIR IAW ETD2023-170-011274 REV B. ALSO REF VP-018676-2023 N/R 11 C1-C3 FOR WORK PERFORMED.
2022
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 81 BETWEEN STRINGERS 27R AND 28R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 76 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 84 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 83 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 82 BETWEEN STRINGERS 27R AND 26R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 82 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 75 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 74 BETWEEN STRINGERS 29R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
CORROSION ON STRINGER AT RIVET ON STRINGER 19R AFT OF FRAME 88. REPAIRED STRINGER 19R PER ETD2022-170-028727.
Part: SHEAR ANGLE — CORRODED (ZONE 100) · airframe 35,668 hrs · 22,344 cycles
SHEAR CLIP IS CORRODED AT FRAME 74 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.
2021
Part: LIGHT — DIRTY (ZONE 100) · airframe 33,965 hrs · 21,180 cycles
PHOTOLUMINESCENT FLOOR LIGHTING WORN AND WILL NOT ILLUMINATE. CLEANED ALL AIRCRAFT PHOTOLUMINESCENT INDICATOR LIGHT STRIPS ON FLOOR.
Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 32,738 hrs · 20,299 cycles
L1 DOOR SLIDE IS PARTIALLY DEPLOYED. R&R L1 SLIDE ASSEMBLY.
2020
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,489 hrs · 19,274 cycles
EMERGENCY BATTERY LIGHT FAULT ON EICAS DURING ELPU FUNCTIONAL TEST. R & R ELPU 2, REF AMM 33-50-01.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 31,489 hrs · 19,273 cycles
"SUSPECTED CRACK ON RIB 11 RH HORIZONTAL STABILIZER. COMPLIED WITH EO 170EO-55-10-0004_1. LEFT AND RIGHT HSTAB RIB 10A, 11A & 12A REPLACEMENTS."
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE AT WASTE BOX ON STRINGER 28R AT FRAME 88. REMOVED DAMAGE STRINGER BY CUTTING, DRILLED AND INSTALLED SPLICE REPAIR PARTS ON STRINGER 28R BETWEEN FRAMES 86-90 REF EDT2020-170-008593. RESTORED SURFACE PROTECTION PER SRM 51- 23-05, 51-23-06. A/C REMAINS IN CHECK.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - RH SIDE OF CROSSBEAM AT FRAME 14. REMOVED CORROSION BY BLENDING ON RH SIDE OF CROSSBEAM AT FRAME 14 PREVIOUS REPAIR PER SRM 51-10-03, FOUND OUT OF LIMITS PER SRM 53-10-10/AD02. INSTALLED NEW RH FR 14 REPAIR AS REQUIRED REF SRM 53-00-10 FIG 203 TABLE 204
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND RH FLOOR BEAM CORRODED AS MARKED @ FRAME 87. PERFORMED CUT-OUT OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER ON RH AFT FLOOR BEAM @ FR87 REF EMB SRM 53-23-10 R01P. APPLIED SURFACE PROTECTION PER SRM 51-23-05, 51-23-06. A/C REMAINS IN CHECK.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND LH FLOOR SILL CORRODED AS MARKED @ FRAME 90. REMOVED CORRODED LH FLOOR SILL @ FR90 REF EMB SRM 51-40-08 INSTALLED NEW LH SILL @FR90 REF EMB SRM 51-40-08
Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND RH FLOOR PANEL SUPPORT CORRODED FRAME 86 CROSSBEAM. REMOVED AND REPLACED RH FLOOR PANEL SUPPORT AT FRAME 86 REF EMB SRM 51-40-08, RESTORED SURFACE PROTECTION PER SRM 51-23-06. A/C REMAINS IN CHECK.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - RH SIDE OF CROSSBEAM AT FRAME 15. REMOVED CROSSBEAM SUPPORT AT FRAME 15 (RH SIDE). REF EMB SRM 51-40-08 INSTALLED NEW FLOOR SUPPORT AT CROSSBEAM FRAME 15 (RH SIDE). REF EMB SRM 51-40-08
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION RH FLOOR SILL AS MARKED FRAME 84. REMOVED AND REPLACED RH FLOOR SILL FRAME 84 REF EMB SRM 51-40-08
Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND RH FLOOR PANEL SUPPORT CORRODED AS MARKED FRAME 87 @ RH SHEAR PANEL. REMOVED RH FLOOR PANEL SUPPORT. FRAME 87 @ RH SHEAR PANEL. LOCATED, DRILLED, AND APPLIED ALODINE TO NEW RH FLOOR PANEL SUPPORT. FRAME 87 @ RH SHEAR PANEL PER REF EMB-175 SRM 51-40-02, 51-40-08, 51-23-04 INSTALLED NEW RH SHEAR PANEL PER REF EMB-175 SRM 51-40-08.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND SPLICE CORRODED AS MARKED @ CENTER OF FRAME 90. REMOVED CORROSION BY BLENDING AT CENTER SPLICE. FRAME 90. MATERIAL REMOVED: H-.010" NOMINAL .050" OUT OF LIMITS. REF EMB SRM 51-75-16 SRM 51-10-03 TOOLING TC1-66878-2 08-07-20 TC2-7449 09-17-20 TC2-7633 11-06-20 INSTALLED NEW AFT WET AREA CENTER FLOOR SPLICE PLATE AT FR90 REF EMB SRM 51-40-08.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND GUSSET CORRODED AS MARKED FRAME 84 @ RH INBD. SEAT TRACK. REMOVED AND REPLACED FLOOR GUSSET AT RH INBD SIDE OF FRAME 84 PER SRM 51-40-08. RESTORED SURFACE PROTECTION AND REMOVED EWIS PROTECTION PER SRM 51-23-06 PO# 258790, SWPM 20-67-00
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - RH SIDE OF CROSSBEAM AT FRAME 16. REMOVED CROSSBEAM SUPPORT AT FRAME 16 (RH SIDE). REF EMB SRM 51-40-08 INSTALLED NEW FLOOR SUPPORT AT CROSSBEAM FRAME 16 (RH SIDE). REF EMB SRM 51-40-08
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - LH SEAT TRACK BETWEEN FRAMES 12 AND 16. REMOVED CORROSION BY BLENDING ON LH SEAT TRACK BETWEEN FRAMES 12-16 PER SRM 51-10-03, FOUND OUT OF LIMITS PER SRM 53-10-10/AD01. FABRICATED NEW DOUBLER AND FILLER. REF EMB SRM 53-10-10/REPAIR 01 APPLIED ALODINE PRIMER AND TOP COAT PER SRM 51-23-04 PO# 243626 SRM 51-23-05 PO# 252323 SRM 51-23-06 PO# 258790 INSTALLED FABRICATED DOUBLER AND FILLERS (2) BETWEEN FRAMES 16-17. LH SEAT TRACK. REF EMB SRM 53-10-10/REPAIR 01
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 87 STRINGER 28R. REMOVED DAMAGED SHEAR CLIP, IN AFT CARGO, AT FRAME 87 STRINGER 28R. LOCATED, DRILLED AND INSTALLED NEW SHEAR CLIP, IN AFT CARGO, AT FRAME 87 STRINGER 28R. SURFACE PROTECTION APPLIED. REF EMB SRM 51-23-00. A/C REMAINS IN CHECK.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SKIN AT WASTE BOX FRAME 88-89 STRINGER 28R. REMOVED AND REPLACE AFT FUSELAGE INTERNAL SKIN DOUBLER AT WASTE BOX BETWEEN FRAME 88-89 STRINGER 28R PER SRM 51-40-08, RESTORED SURFACE PROTECTION TO INTERNAL AND EXTERNAL FASTENERS PER SRM 51-23-04, 51-23-05, 51-23-06. A/C REMAINS IN CHECK.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION - LH SILL AT FRAMES 13, 14, 15 AND 16. REMOVED DAMAGED LH SILL AT FRAMES 13-16. LOCATED, DRILLED, AND INSTALLED NEW LH SILL, AT FRAMES 13-16. SURFACE PROTECTION APPLIED. REF. SRM 51-40-08, 51-23-00. A/C REMAINS IN CHECK.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 85 STRINGER 28R. REMOVED AND REPLACED AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 85 STRINGER 28R PER SRM 51-40-08, RESTORED SURFACE PROTECTIOM TO FASTENERS PER SRM 51-23-05, 51-23-06. A/C REMAINS IN CHECK.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - RH SILL AT FRAMES 12, 13 AND 14. REMOVED RH SILL AT FRAMES 12, 13 AND 14.PER REF SRM 51-40-02 51-40-08 INSTALLED NEW RH SILL AT FRAMES 12, 13 AND 14.PER REF SRM 51-40-02 51-40-08 APPLIED TOP COAT SRM 51-23-06 PO#258790
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL AFT INTERCOSTAL AT WATER DRAIN FRAME 86-87 STRINGER 28R. REMVED AND REPLACED AFT INTERCOSTAL AT WATER DRAIN FRAME 86-87 STRINGER 28R PER SRM 51-40-08, RESTORED SURFASCE PROTECTION TO FASTENERS PER SRM 51-23-06. A/C REMAINS IN CHECK.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 88 STRINGER 28R. REMOVED THE AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 88 STRINGER 28R T EVALUATE THE CORROSION. THE SHEAR CLIP IS 100% CORRODED. THIS IS OUT OF LIMITS.LOCATED, DRILLED AND INSTALLED NEW SHEAR CLIP AT FRAME 88 STRINGER 28R. REF SRM 51-40-08. SURFACE PROTECTION APPLIED. REF EMB SRM 51-23-00. A/C REMAINS IN CHECK.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - LH SILL AT FRAME 19. REMOVED, LOCATED, DRILLED, AND ALODINE LH SILL AT FRAME 19. REF SRM 51-40-02, 51-40-08, 51-23-04 INSTALLED AND APPLIED SURFACE PROTECTION TO LH SILL AT FRAME 19 . REF SRM 51-23-06, 51-40-08
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION, AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 84 STRINGER 28R. REMOVED AND REPLACED AFT FUSELAGE INTERNAL SHEAR CLIP AT FRAME 84 STRINGER 28R PER SRM 51-40-08. APPLIED SURFACE PROTECTIOIN TO RIVETS PER SRM 51-23-05, 51-23-06. A/C REMAINS IN CHECK.
Part: STAND OFF — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
WHILE IN HEAVY CHECK FOUND CORROSION - LH STAND OFF AT FRAME 17. REMOVED, REPLACED, AND APPLIED SURFACE PROTECTION ON LH STAND OFF AT FRAME 17. REF SRM 51-40-08, 51-23-04, 51-23-05, 51-23-06
Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,489 hrs · 19,273 cycles
DURING HEAVY CHECK MAINTENANCE FOUND SURFACE CORROSION ON SKIN AT LAV SERVICE PANEL AS MARKED. REMOVED AND REPLACED WASTE DOOR SERVICE PANEL PER SRM AMM 53-03-62-440-801-A TW# TC2-7398 DUE 6-10-20. RESTORED SURFACE PROTECTION TO SERVICE DOOR SKIN PANEL PER SRM 51-23-04, 51-23-05, 51-23-06. A/C REMAINS IN CHECK.