N859GT
Registered owner: ATLAS AIR INC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ATLAS AIR INC (UIEA) | Operator | on 2024-01-18 | Operator named in NTSB report |
Accident & incident history
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.
115 reports on file, 2016-02-22 – 2025-09-17.
Part: FLAP — DAMAGED · airframe 43,427 hrs · 6,945 cycles
NUMBER 18 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 1140 STRINGER 20R FWD SIDE CRACKED. STRINGER 20R REPAIRED IAW RI-53-41-17867 REV.A. NO FURTHER DEFECTS NOTED.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
MDC - STA 1550 RBL 11 SEAT TRACK SLOT HOLE ELONGATED(<P>MDC - STA 1550 RBL 11 SEAT TRACK SLOT HOLE ELONGATED REPAIRED I.A.W RI-53-60-17877 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 6R SUSPECTED CRACKED. STRINGER 6R REPAIRED IAW RI-53-80-17718 REV A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2180, STRINGER 12R CRACKED FWD AND AFT SIDE. STRINGER 12R REPAIRED IAW SRM 53-60-03-2R-3, TR53-154, ALTERNATIVE 4, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
ONE CRACK FOUND, STA 2360 FWD STRINGER 6L. STRINGER 6L REPAIRED IAW SRM 53-60-03-2R-8, TR53-157. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
FWD OF BS 2360, STRINGER 7R FOUND CRACKED. STRINGER 7R REPAIRED IAW SRM 53-60-03-2R-8, TR53-157. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2180, STRINGER 11R CRACKED FWD AND AFT SIDE. STRINGER 11R REPAIED IAW SRM 53-60-03-2R-3, ALTERNATIVE 4, TR53-154, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 5L SUSPECTED CRACKED. STRINGER 5L REPAIRED IAW RI-53-80-17848, REV.B. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
FWD OF BS 2360, STRINGER 6R CRACKED. STRINGER 6R REPAIRED IAW SRM 53-60-03-2R-8, TR53-157, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT STRINGER 20R SUSPECT CRACK. STA 2360 AFT STRINGER 20R SUSPECT CRACK AREA REPAIRED IAW SRM 53-80-03-2R-3 TR53-153. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 1960 STRINGER 12R CRACKED AFT SIDE. STRINGER 12R REPAIRED IAW SRM 53-60-03-2R-4 & ALTERNATIVE 4, TR53-155. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 AFT SIDE STRINGER 2L SUSPECTED CRACKED. STRINGER 2L REPAIRED IAW RI-53-81-17871 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD STRINGER 6L FOUND CRACKED. STRINGER 6L REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46 DATE: 20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
ONE CRACK FOUND ON STA 2360 FWD STRINGER 7L. STRINGER 7L REPAIRED IAW SRM 53-60-03-2R-8, TR53-157. NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 300) · airframe 43,427 hrs · 6,945 cycles
RIGHT HORIZONAL STAB. TIP FAIRING U CHANNEL FOUND CRACKED. REPLACED THE CHANNEL IAW RI-55-10-17841, REV A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
ONE CRACK FOUND ON BS 2360 FWD STRINGER 10L. STRINGER 10L REPAIRED IAW SRM 53-60-03-2R-8 TR53-157 REV.46 DATE: 20JUN 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 3L SUSPECT CRACKED. STRINGER REPAIRED IAW RI-53-81-17881 REV.A. NO FURTHER DEFECTS NOTED.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
MDC - SEAT TRACK BETWEEN STA 1786 AND 2106 LBL 11.33" FOUND 2EA LOCATION SLOT HOLE ELONGATED STA 1850, 1870 AREA(<P>MDC - SEAT TRACK BETWEEN STA 1786 AND 2106 LBL 11.33" FOUND 2EA LOCATION SLOT HOLE ELONGATED STA 1850 & 1870 AREA REPAIRED I.A.W RI-53-60-17850 REV.A. NO FURTHER DEFECTS NOTED</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2180, STRINGER 13L CRACKED FWD AND AFT SIDE. STRINGER 13L REPAIRED IAW RI-53-80-17842, REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
ONE CRACK WAS FOUND ON STA 2360 FWD STRINGER 2L. STRINGER 2L REPAIRED IAW SRM 53-60-03-2R-8, TR53-157. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 5R SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 5L SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152. NO FURTHER DEFECTS NOTED
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 1960, STRINGER 10L CRACKED. STRINGER 10.L REPAIRED IAW SRM 53-60-03-2R-4, TR53-155, ALTERNATIVE 2. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 24R SUSPECTED CRACKED. STRINGER 24R REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
MDC - SEAT TRACK BETWEEN STA 1265 AND 1480 LBL 11.33" FOUND 7EA LOCATION SLOT HOLE ELONGATED AT STA 1250, 1270, 1290, 1350, 1390, 1430 & 1470 AREA(<P>MDC - SEAT TRACK BETWEEN STA 1265 AND 1480 LBL 11.33" FOUND 7EA LOCATION SLOT HOLE ELONGATED AT STA 1250, 1270, 1290, 1350, 1390, 1430 & 1470 AREA REPAIRED I.A.W RI-53-40-17897 REV.A. NO FURTHER DEFECTS NOTED</P>)
Part: FLAP — DAMAGED · airframe 43,427 hrs · 6,945 cycles
NUMBER 6 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 8R CRACKED. STRINGER 8R REPAIRED IAW SRM 53-80-03-2R-3, TR53-153, REV 46. NO FURTHER DEFECTS NOTED.
Part: SKIN — CHAFED (NR 4 FLAP) · airframe 43,427 hrs · 6,945 cycles
NUMBER 4 V/C FLAP BULLNOSE EDGE CHAFED. PERFORMED REPAIR AT CHAFED AREA IAW SRM 51-70-04, REPAIR 7. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2180, STRINGER 12L CRACKED FWD AND AFT SIDE. STRINGER 12L REPAIRED IAW SRM 53-60-03-2R-3, ALTERNATIVE 4, TR53-154 REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
M/D STA 1960 STRINGER 11R FWD AND AFT FOUND CRACKED. STRINGER 11R REPAIRED IAW SRM 53-60-03-2R-4, TR53-155, ALTERNATIVE 4. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 1960, STRINGER 9R CRACKED FWD SIDE. STRINGER 9R REPAIRED IAW SRM 53-60-03-2R-4, TR53-155, ALTERNATIVE 4, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 8R SUSPECTED CRACKED. STRINGER 8R REPAIRED IAW SRM 53-80-03-2R-2, TR53-152. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE S20L SUSPECT CRACKED(<P>STA 2360 AFT SIDE S20L SUSPECT CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-80-03-2R-3 TR53-153 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: GRILL — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
COCKPIT - CAPT SIDE CONSOLE LWR AIR GRILL CRACKED. AIR GRILL REPAIRED IAW AMM 25-00-00, AND RI-25-00-17869, REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD STRINGER 25R FOUND CRACKED. STRINGER 25R REPAIRED IAW RI-53-81-17708 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2180, STRINGER 9R FWD SIDE CRACKED. STRINGER 9R REPAIRED IAW SRM 53-60-03-2R-3, TR53-154, ALTERNATIVE 2, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 3R SUSPECTED CRACKED. STRINGER 3R REPAIRED IAW RI-53-81-17719 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 7R SUSPECTED CRACKED. STRINGER 7R REPAIRED IAW SRM 53-80-03-2R-3, TR53-153 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT STRINGER 22R SUSPECTED CRACKED. STRINGER 22R REPAIRED IAW SRM 53-80-03-2R-3, TR53-153, REV 46. NO FURTHER DEFECTS NOTED.
Part: RIB — CRACKED (ZONE 600) · airframe 43,427 hrs · 6,945 cycles
RIGHT WING NR 20 VC FLAP PANEL UPPER RIB MOST INBD FOUND CRACKED. RT WING NR 20 VC FLAP PANEL RIB REPAIRED IAW RI-57-44-17855 REV A. NO FURTHER DEFECTS NOTED.
Part: FLAP — DAMAGED · airframe 43,427 hrs · 6,945 cycles
NUMBER 9 V/C FLAP DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 2L SUSPECTED CRACKED. STRINGER 2L REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46, DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED
Part: FLAP — DAMAGED · airframe 43,427 hrs · 6,945 cycles
NUMBER 8 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE S24L SUSPECT CRACKED. STRINGER REPAIRED IAW RI-53-80-17740 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 AFT SIDE STRINGER 2R SUSPECTED CRACKED. STRINGER 2R REPAIRED IAW RI-53-81-17870 REV.A. NO FURTHER DEFECTS NOTED.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
MDC - SEAT TRACK BETWEEN STA 1000 AND 1265 LBL 11.33" FOUND 5EA LOCATION SLOT HOLE ELONGATED AT STA 1070, 1090, 1110, 1130 & 1150 AREA(<P>MDC - SEAT TRACK BETWEEN STA 1000 AND 1265 LBL 11.33" FOUND 5EA LOCATION SLOT HOLE ELONGATED AT STA 1070, 1090, 1110, 1130 & 1150 AREA REPAIRED I.A.W RI-53-40-17849 REV.A. NO FURTHER DEFECTS NOTED</P>)
Part: SEAT TRACK — OUT OF LIMITS (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
M/D STA 1510 AND STA 1550 LBL 11. SEAT TRACK INDEX FOUND OUT OF LIMIT. M/D BS 1510 AND 1550 LBL 11. SEAT TRACK INDEX FOUND OUT OF LIMIT AREA REPAIRED IAW SRM 53-00-52-2R-9 REPAIR 9 REV.46 DATE 20 JUN 2025 & RI-53-60-17886 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 AFT SIDE STRINGER 4L SUSPECTED CRACKED. STRINGER 4L REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 8L FOUND CRACKED. STRINGER 8L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153, REV.46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 21L SUSPECTED CRACKED. STRINGER 21L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
Part: STRUT — BROKEN (ZONE 600) · airframe 43,427 hrs · 6,945 cycles
RHE ILES 440 APPROX L/E CAVITY DIAGONAL STRUT & UPPER ATTACH FITTING FOUND BROKEN. RHE ILES 440 APPROX L/E CAVITY DIAGONAL STRUT & UPPER ATTACH FITTING REPAIRED IAW SRM 57-41-09-2R-2 REPAIR 2, FIG 203 REV 46. . NO FURTHER DEFECTS NOTED.
Part: CHANNEL — CRACKED (ZONE 300) · airframe 43,427 hrs · 6,945 cycles
LEFT HORIZONAL STAB TIP FAIRING U CHANNEL FOUND CRACKED. REPLACED THE CHANNEL IAW RI-55-10-17840, REV A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2180, STRINGER 10L AND SPLICE AFT SIDE, CRACKED. STRINGER 10L AND SPLICE AFT SIDE REPAIRED IAW SRM 53-60-03-2R-3, TR53-154, ALTERNATIVE 3. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
FWD OF BS 2360 STRINGER 2R CRACKED. STRINGER 2R REPAIRED IAW SRM 53-60-03-2R-8, TR53-157, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 22L SUSPECT CRACKED. STRINGER 22L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153, REV 46. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 1L SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 1960 STRINGER 10R CRACKED FWD AND AFT SIDE. STRINGER 10R REPAIRED IAW SRM 53-60-03-2R-4, ALTERNATIVE 4, TR53-155. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 6L SUSPECTED CRACKED. STRINGER 6L REPAIRED IAW RI-53-80-17717 REV.A. NO FURTHER DEFECTS NOTED.
Part: FLAP — DAMAGED · airframe 43,427 hrs · 6,945 cycles
NUMBER 21 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
Part: SEAT TRACK — OUT OF LIMITS (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
M/D - STA 1480+50 LBL11. SEAT TRACK INDEX HOLE FOUND OUT OF LIMIT. M/D - STA 1480+50 LBL11. SEAT TRACK INDEX HOLE FOUND OUT OF LIMIT. AREA REPAIRED I.A.W B747-8F SRM 53-00-52-2R-9 REPAIR 9 REV.46 DATE 20 JUN 2025 & RI-53-60-17886 REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 5R SUSPECTED CRACKED. STRINGER 5R REPAIRED IAW RI-53-80-17741, REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 24L SUSPECTED CRACKED. STRINGER 24L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 7L SUSPECTED CRACKED. STRINGER 7L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 7L SUSPECTED CRACKED. STRINGER 7L REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46, DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD STRINGER 8L FOUND CRACKED. STRINGER 8L REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46 DATE: 20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: FLAP — DELAMINATED (NR 14 KRUEGER) · airframe 43,427 hrs · 6,945 cycles
NUMBER 14 K-FLAP FOUND DELAMINATED. PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-04, REPAIR 1. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD SIDE STRINGER 6R SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2360 AFT SIDE STRINGER 4R SUSPECTED CRACKED. STRINGER 4R REPAIRED IAW RI-53-80-17734, REV.A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 43,427 hrs · 6,945 cycles
STA 2598 FWD STRINGER 7R FOUND CRACKED. STRINGER 7R REPAIRED IAW SRM 53-80-03-2R-2 TR53-152 REV.46 DATE 20 JUN 2025 & RI-53-80-17882 REV. A. NO FURTHER DEFECTS NOTED.
Earlier reports · 2016–2024 · 45 reports
2024
Part: FIRE WARNING — ILLUMINATED (NR 2 ENGINE) · airframe 36,468 hrs · 5,942 cycles
ENGINE 2 FIRE DURING CLIMB. REF LP 1741535 M16: R/R ENGINE 2 IAW ATLAS W.C. B-72-099-00-01. REF LP 1741537 M22: R/R ENG 2 BOTTLE B IAW AMM 26-21-03-400-801. REF LP 1741538 M23: R/R ENG 2 OUTBOARD T/R IAW AMM 78-31-01-400-801-G00.
2023
Part: PSEU — UNKNOWN (UNKNOWN) · airframe 36,330 hrs · 5,915 cycles
EXPANDED DISPLAY INDICATED RH BODY GEAR WAS NOT RETRACTED(<P>R/R PSEU & GROUND TEST PASSED PER AMM 32-09-03. FURTHER T/S REQUIRED.</P> / <P>LP 1727176 M10: R/R RH BLG TILT ACTUATOR IAW AMM 32-13-15-404-010, OPS CHECK NORMAL. PERFORMED GEAR SWING IAW AMM 32-31-00-860-801, TEST GOOD.</P>)
Part: PDU — UNKNOWN (UNKNOWN) · airframe 36,077 hrs · 5,875 cycles
"FLAPS DRIVE" EICAS OUTER SLATS LEFT AND RIGHT.(<P>REMOVED AND REPLACED R4 L/E PDU ASSY AND SERVICED OIL. OPS CHECK GOOD PER AMM 27-81-03, IPC 27-81-03-07.</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 820 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHED WITH TC 8545120</P>)
Part: MOTOR — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
INBD T/E FLAP ELEC PWR C/B POPPED OUT(<P>1) IAW AMM 27-51-17-000-801 REV 42 REMOVED INBD FLAP ELEC MOTOR. 2) IAW AMM 27-51-17-400-801 REV 42 INSTALL AND TEST INBD FLAP ELEC MOTOR. 3) CONDITION CHECK NORMAL</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 34,683 hrs · 5,668 cycles
CORROSION - FITTING AT STA 2360 RBL 35(<P>1) IAW AMM 53-44-00-200-801 REV 42 REMOVED M/D CGO FITTING AT STA 2360 RBL 35. 2) ACCOMPLISHED EI T2023A53M-2131 SEQUENCE A REV 0. 3) IAW AMM 53-44-00-200-801 REV 42 INSTALL M/D CGO FITTING AT STA 2360 RBL 35. 4) CONDITION CHECK NORMAL</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - FOUND MAIN DECK STRINGER CRACK STA 760 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHED WITH T/C 8545120</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 880 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C AND EI T2023A53M-2151 REV 0. 2) ACCOMPLISHED EI T2023A53M-2151 REV 1. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - FOUND MAIN DECK STRINGER CRACK STA 840 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHED WITH T/C 8545120</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 860 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHED WITH T/C 8545120</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 880 TO STA 900 S10R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-6 REV 40 AND DWG 142U3725 SH 19 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
1) CRACK - STRINGER OF FUSELAGE STA 820 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C AND EI T2023A53M-2151 REV 0. 2) ACCOMPLISHED EI T2023A53M-2151 REV 1 AND EI ATTACHED TO W/OO 8538401 (066). 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 980 - 1120 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 880 S9L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-6 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
Part: POWER SUPPLY — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
FOUND EMERGENCY LIGHT INOP (EQUIPMENT NUMBER L6690, L1533, L5735, L1853 & L1854) TOTAL 5(<P>IAW AMM 33-51-10-962-001, 33-51-09-960-901, 33-51-04-000-803 & 33-51-04-400-803 REV 41 R/R SLIDE LIGHT AND INERTIA REEL LIGHT LAMPS, M5170 POWER SUPPLY AND PERFORMED EMERGENCY LIGHT TEST, THE RESULT WAS GOOD</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - FOUND MAIN DECK STRINGER CRACK STA 780 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 34,683 hrs · 5,668 cycles
CORROSION - SEAT TRACK STA 1980 LBL 98.58(<P>1) REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 40. 2) PERFORM EI T2023A53M-2031 REV 0 SEQ A AND DWG 146U5234 SH 40 REV - & 146U5406 SH 42 REV -. 3) ACCOMPLISHED EI T2023A53M-2031 REV 1. 4) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,683 hrs · 5,668 cycles
CRACK - STRINGER OF FUSELAGE STA 980 + 160 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)
2022
Part: ACTUATOR — DAMAGED · airframe 29,884 hrs
CREW REPORTED CMC STATUS MESSAGE 32723 - L BODY GEAR TILT LVRLK PRIMARY PROX SWITCH TARGET FAIL, AND WERE UNABLE TO RETRACT THE GEAR.(<P>FOUND LEFT BODY GEAR TRUCK POSITIONING ACTUATOR BROKEN ROD. REMOVED & REPLACED ACTUATOR. BLEED & LEAK CHECK GOOD IAW AMM 32-13-15-004-001.</P>)
2021
Part: STRINGER — CRACKED (LT WING) · airframe 25,947 hrs · 4,290 cycles
LHW #7 V/C UPPER STRINGER AT LEFI BRACKET AREA FOUND CRACK(<P>THE SUBJECT STRINGER TIME LIMITED REPAIR CARRIED OUT AS PER RI-57-44-14755 REV A</P>)
Part: SKIN — PUNCTURED (RT MLG DOOR) · airframe 25,947 hrs · 4,290 cycles
RH BLG W/W O/B DOOR INTERIOR SURFACE FWD AREA FOUND PUNCTURE.(<P>THE SUBJECT DOOR INTERIOR SKIN REPAIR CARRIED OUT AS PER RI-52-80-14763 REV A</P>)
Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 25,947 hrs · 4,290 cycles
M/D - SEAT TRACK STA 2090 LBL 11 FOUND CORROSION.(<P>THE SUBJECT SEAT TRACK REPAIR CARRIED OUT AS PER RI-53-00-14762 REV A</P>)
Part: RIB — CRACKED (RT AILERON) · airframe 25,947 hrs · 4,290 cycles
RHW T/E RIB, AT I/B AILERON I/B SIDE AREA, AFT ANGLE FOUND SUSPECT 3" CRACK.(<P>THE SUBJECT RIB REPAIR CARRIED OUT AS PER RI-57-50-14759 REV A</P>)
Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 25,947 hrs · 4,290 cycles
LHW L/E ACCESS PANEL 521AB L/E AREA VAPOR BARRIER FOUND CRACK.(<P>THE SUBJECT VAPOR BARRIER REPAIR CARRIED OUT AS PER SRM 57-41-01-2R-6 REV 34, 20 JUN 2021.</P>)
Part: RIB — CRACKED (LT AILERON) · airframe 25,947 hrs · 4,290 cycles
LHW T/E RIB, AT I/B AILERON I/B SIDE AREA, AFT ANGLE FOUND SUSPECT 3" CRACK. THE SUBJECT RIB REPAIR CARRIED OUT AS PER RI-57-50-14760 REV A</P>)
Part: SKIN — SCRATCHED (NR 3 ENG NSE CWL) · airframe 25,947 hrs · 4,290 cycles
NO.3 ENG NOSE COWL LIP SKIN 5:30 O'CLOCK AREA FOUND SCRATCH MARK.(<P>THE NOSE COWL SUBJECT AREA BLEND OUT REPAIR CARRIED OUT AS PER SRM 54-10-01-1A-1 REV 34 DATE 20 JUL 2021.</P>)
Part: STRIP — DAMAGED (FLAP) · airframe 25,947 hrs · 4,290 cycles
NO.17 V/C FLAP TOP EDGE METAL STRIP O/B AREA FOUND DAMAGE.(<P>NO.17 V/C FLAP TOP EDGE METAL STRIP REPLACED AS PER CMM 57-55-42 ASSEMBLY PAR 2C 5A (6).</P>)
Part: STRIP — DAMAGED (FLAP) · airframe 25,947 hrs · 4,290 cycles
NO.10 V/C FLAP TOP EDGE METAL STRIP O/B AREA FOUND DAMAGE(<P>NO.10 V/C FLAP TOP EDGE METAL STRIP REPLACED AS PER CMM 57-55-42 ASSEMBLY PAR 2C 5A ( 6 ).</P>)
Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 25,947 hrs · 4,290 cycles
M/D - SEAT TRACK STA 2110 LBL 11 FOUND CORROSION.(<P>THE SUBJECT SEAT TRACK REPAIR CARRIED OUT AS PER RI-53-00-14764 REV A</P>)
Part: CONTROLLER — FAULTED (NR 1)
BLEED 1 ADVISORY AND BLEED # 3 ADVISORY MSG. REMOVED AND REPLACED #1 IASC AND #3 IASC IAW B747-8 AMM 36-10-01/401</SPAN></P>)
Part: ECU — MALFUNCTIONED (ENGINE) · airframe 24,434 hrs · 4,057 cycles
UPON ENG SPOOL FOR T/O ACFT VEERED TO RIGHT. EXECUTED LOW SPEED (10 KNOTS APPROX) REJECTED T/O(<P ><SPAN>INSPECTED NOSE STEERING / SYSTEM IAW AMM 32-51-00, INSPECT A/C BRAKES IAW AMM 32-41-00, REPLACED BODY / GEAR STEERING ECU IAW AMM 32-53-03</SPAN></P>)
2019
Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 18,089 hrs · 2,996 cycles
AFTER AIRCRAFT BLOCKED IN, MAINTENANCE FOUND ON WALK AROUND INSPECTION, #3 ENGINE LEFT REVERSER HALF HOT GAS DAMAGE TO INTERIOR OF T/R SLEEVE AT THE 11 O'CLOCK POSITION.(<P>REMOVED AND REPLACED ENG 3, I/B T/R REF AMM 78-31-01. OPERATIONAL CHECK NORMAL. LEAK CHECK COMPLIED WITH, NO LEAKS NOTED. SEE LP 1114439 ITEM M19 FOR INSTALLED T/R, S/N: MCB01013, P/N CONVERSION FROM 608C0100-657 TO P/N 608C0100-661 PER EO 1978A265.</P>)
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,103 hrs · 2,826 cycles
M/D LBL 98 SEAT TRACK STA 1820-1840, FOUND CORRODED AS MARKED. (<P>M/D LBL 98 SEAT TRACK AT STA 1820-1840 CORRODED AREA REMOVED AND RE-PROTECTED PER SRM 51-10-02 AND SRM 51-20-01. BLENDED AREA DEPTH 0.025", WIDTH 0.7", LENGTH 3" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,103 hrs · 2,826 cycles
M/D LBL 98 SEAT TRACK STA 1720-1740 FOUND CORRODED AS MARKED. (<P>M/D LBL 98 SEAT TRACK AT STA 1720-1740 CORRODED AREA BLENDED OUT AREA DEPTH 0.015", WIDTH 0.7", LENGTH 10" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)
Part: DIVIDER — DAMAGED (CARGO BAY) · airframe 17,103 hrs · 2,826 cycles
FWD CARGO COMPARTMENT AFT B/H DIVIDER 123L SURROUNDING EDGE SEVERAL LOCATIONS FOUND TORN AND BUTTONS DAMAGED. (<P>FWD CARGO COMPARTMENT AFT B/H DIVIDER 123L CURTAIN PATCH STITCHES REPAIRED AS PER RI NO: RI-25-52-13647 REV A 16JUL2019.</P>)
Part: ACCESS PANEL — CHAFED (NR 3 PYLON) · airframe 17,103 hrs · 2,826 cycles
#3 PYLON TORQUE BOX ACC PANEL 472GL, FOUND CHAFE MARK AS MARKED. (<P>DAMAGE REMOVED AND NDT INSPECTION CARRIED OUT WITH NO CRACK FOUND RESULT. REPAIR INSTRUCTION PER RI 54-50-13651 REV A.</P>)
Part: PANEL — CRACKED (RT WING) · airframe 17,103 hrs · 2,826 cycles
RT WING T/E I/B TOP FIXED PANEL AT #8 SPOILER, O/B FWD CUTOUT FOUND CRACKED. (<P>RT WING T/E I/B UPPER FIXED PANEL AT #8 SPOILER O/B FWD, COMPOSITE HOT BOND REPAIRED AS PER RI NO: RI-57-51-13650 REV A AND REF PROCESS CARD: UVH502709-01.</P>)
Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 16,786 hrs · 2,771 cycles
AT FL 320, AFTER 1 HR 25 MIN OF FLIGHT, WE HEARD A LOUD BANG. #2 ENGINE ROLLED BACK AND SHUT DOWN. AUTO START TRIED SEVERAL TIMES TO RE-LIGHT BUT IT DID NOT START. N1 21%, N2 22%, OIL PRES 9. HIGHEST EGT DURING RESTART WAS 825. DESCENDED TO FL 300 AND ACCOMPLISHED QRH. SINCE ENGINE WASN'T SEIZED, ATTEMPTED ANOTHER START. DID NOT START, ENGINE WAS CUTOFF. REMOVED AND REPLACED #2 ENGINE ASSY PER ATLAS AIR TASK CARD B-72-099-00-01. ACCOMPLISHED MCS PACKAGE 52306 AS ASSIGNED.
2018
Part: CONTROL UNIT — MALFUNCTIONED · airframe 14,705 hrs · 2,429 cycles
NUMEROUS ELECTRICAL MALFUNCTIONS REQUIRING AIR TURN BACK.(<P>REMOVED AND REPLACED #1 BCU IAW AMM 24-*23-01. OPS CHECK NORMAL IAW AMM 24-23-01</P>)
Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 10,354 hrs · 1,723 cycles
OUTFLOW VALVE FAILED TO OPEN IN AUTO AND MANUAL.
2017
Part: CHANNEL — CRACKED (LT WING) · airframe 8,489 hrs · 1,420 cycles
LEFT WING WS 500 CHANNEL CRACKED. REPAIRED IAW R5-57-22-12058, REV A.
Part: CHANNEL — CRACKED (RT WING) · airframe 8,489 hrs · 1,420 cycles
RIGHT WING WS 500 CHANNEL CRACKED. REPAIRED IAW R5-57-22-12059, REV A.
Part: SKIN — DENTED (BS 2341) · airframe 8,489 hrs · 1,420 cycles
DENT FOUND ON THE FWD SKIN AT BS 2341 BETWEEN STRINGERS 19R -20R. REPAIRED IAW R1-53-61-12063, REV B.
2016
Part: ESCAPE ROPE — UNSECURE (COCKPIT) · airframe 2,614 hrs · 446 cycles
COCKPIT DESCENT DEVICE H CABLE PULL FROM ASSEMBLY, PN 379103D-23 & SN 25189. R & R COCKPIT DESCENT DEVICE H IAW AMM 25-61-01-000 & AMM 25-61-01-400.
Part: TIRE — BLOWN (LT BLG) · airframe 1,355 hrs · 236 cycles
LEFT BODY, GEAR WARNING INDICATION AFTER TAKEOFF. ACFT ON GND. AFTER LANDING FOUND NR 8 TIRE BLOWN. BLOWN TIRE INSPECTION ACCOMPLISHED. DUE TO TIRE BLOWN, DAMAGE FOUND TO LT BODY GEAR HARNESS, WING TO BODY FAIRINGS DAMAGED. FRAME ASSY AT LT WING TO BODY FAIRINGS DAMAGED. INTERCOSTAL AT LT WING TO BODY FAIRINGS DAMAGED. CLOSURE PANEL AT STA 1480 DAMAGED. WING GEAR ALT DOOR EXT RELEASE CABLE PULLEY BROKEN. ALL REPAIRS ACCOMPLISHED. GEAR SWING ACCOMPLISHED PER AMM 32-33-00.