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 | 2024-01-18 – 2024-01-18 | Operator named in NTSB report |
| ATLAS AIR INC | Operator | 2024-01-18 – 2024-01-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
STA 2598 FWD SIDE STRINGER 5L SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152. NO FURTHER DEFECTS NOTED
STA 2360 AFT SIDE S24L SUSPECT CRACKED. STRINGER REPAIRED IAW RI-53-80-17740 REV.A. NO FURTHER DEFECTS NOTED.
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.
STA 2598 FWD SIDE STRINGER 5R SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152. NO FURTHER DEFECTS NOTED.
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.
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.
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
STA 2598 FWD SIDE STRINGER 3R SUSPECTED CRACKED. STRINGER 3R REPAIRED IAW RI-53-81-17719 REV.A. NO FURTHER DEFECTS NOTED.
STA 2598 AFT SIDE STRINGER 2R SUSPECTED CRACKED. STRINGER 2R REPAIRED IAW RI-53-81-17870 REV.A. NO FURTHER DEFECTS NOTED.
STA 2598 FWD STRINGER 25R FOUND CRACKED. STRINGER 25R REPAIRED IAW RI-53-81-17708 REV.A. NO FURTHER DEFECTS NOTED.
STA 1140 STRINGER 20R FWD SIDE CRACKED. STRINGER 20R REPAIRED IAW RI-53-41-17867 REV.A. NO FURTHER DEFECTS NOTED.
STA 2360 AFT SIDE STRINGER 6L SUSPECTED CRACKED. STRINGER 6L REPAIRED IAW RI-53-80-17717 REV.A. NO FURTHER DEFECTS NOTED.
STA 2598 AFT SIDE STRINGER 2L SUSPECTED CRACKED. STRINGER 2L REPAIRED IAW RI-53-81-17871 REV.A. NO FURTHER DEFECTS NOTED.
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.
STA 2598 FWD SIDE STRINGER 8R SUSPECTED CRACKED. STRINGER 8R REPAIRED IAW SRM 53-80-03-2R-2, TR53-152. NO FURTHER DEFECTS NOTED.
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.
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.
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>)
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>)
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>)
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>)
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.
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.
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.
LEFT HORIZONAL STAB TIP FAIRING U CHANNEL FOUND CRACKED. REPLACED THE CHANNEL IAW RI-55-10-17840, REV A. NO FURTHER DEFECTS NOTED.
RIGHT HORIZONAL STAB. TIP FAIRING U CHANNEL FOUND CRACKED. REPLACED THE CHANNEL IAW RI-55-10-17841, REV A. NO FURTHER DEFECTS NOTED.
NUMBER 14 K-FLAP FOUND DELAMINATED. PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-04, REPAIR 1. NO FURTHER DEFECTS NOTED.
NUMBER 4 V/C FLAP BULLNOSE EDGE CHAFED. PERFORMED REPAIR AT CHAFED AREA IAW SRM 51-70-04, REPAIR 7. NO FURTHER DEFECTS NOTED.
STA 2180, STRINGER 13L CRACKED FWD AND AFT SIDE. STRINGER 13L REPAIRED IAW RI-53-80-17842, REV.A. NO FURTHER DEFECTS NOTED.
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.
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.
STA 2360 AFT SIDE STRINGER 21L SUSPECTED CRACKED. STRINGER 21L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
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.
STA 2360 AFT SIDE STRINGER 5R SUSPECTED CRACKED. STRINGER 5R REPAIRED IAW RI-53-80-17741, REV.A. NO FURTHER DEFECTS NOTED.
STA 2360 AFT SIDE STRINGER 24L SUSPECTED CRACKED. STRINGER 24L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
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.
FWD OF BS 2360, STRINGER 7R FOUND CRACKED. STRINGER 7R REPAIRED IAW SRM 53-60-03-2R-8, TR53-157. NO FURTHER DEFECTS NOTED.
ONE CRACK FOUND, STA 2360 FWD STRINGER 6L. STRINGER 6L REPAIRED IAW SRM 53-60-03-2R-8, TR53-157. NO FURTHER DEFECTS NOTED.
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.
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.
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.
STA 2360 AFT SIDE STRINGER 24R SUSPECTED CRACKED. STRINGER 24R REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
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.
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.
STA 1960, STRINGER 10L CRACKED. STRINGER 10.L REPAIRED IAW SRM 53-60-03-2R-4, TR53-155, ALTERNATIVE 2. NO FURTHER DEFECTS NOTED.
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.
STA 2360 AFT SIDE STRINGER 5L SUSPECTED CRACKED. STRINGER 5L REPAIRED IAW RI-53-80-17848, REV.B. NO FURTHER DEFECTS NOTED.
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.
NUMBER 6 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
NUMBER 8 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
NUMBER 9 V/C FLAP DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
NUMBER 18 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
NUMBER 21 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGED AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED.
STA 2360 AFT SIDE STRINGER 6R SUSPECTED CRACKED. STRINGER 6R REPAIRED IAW RI-53-80-17718 REV A. NO FURTHER DEFECTS NOTED.
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.
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.
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.
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.
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.
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.
STA 2598 FWD SIDE STRINGER 1L SUSPECTED CRACKED. STRINGER REPAIRED IAW SRM 53-80-03-2R-2 TR53-152. NO FURTHER DEFECTS NOTED.
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.
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.
STA 2360 AFT SIDE STRINGER 4R SUSPECTED CRACKED. STRINGER 4R REPAIRED IAW RI-53-80-17734, REV.A. NO FURTHER DEFECTS NOTED.
STA 2360 AFT SIDE STRINGER 7L SUSPECTED CRACKED. STRINGER 7L REPAIRED IAW SRM 53-80-03-2R-3, TR53-153. NO FURTHER DEFECTS NOTED.
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.
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.
STA 2360 AFT SIDE STRINGER 3L SUSPECT CRACKED. STRINGER REPAIRED IAW RI-53-81-17881 REV.A. NO FURTHER DEFECTS NOTED.
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.
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.
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.
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>)
"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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
#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>)
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.
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>)
OUTFLOW VALVE FAILED TO OPEN IN AUTO AND MANUAL.
DENT FOUND ON THE FWD SKIN AT BS 2341 BETWEEN STRINGERS 19R -20R. REPAIRED IAW R1-53-61-12063, REV B.
RIGHT WING WS 500 CHANNEL CRACKED. REPAIRED IAW R5-57-22-12059, REV A.
LEFT WING WS 500 CHANNEL CRACKED. REPAIRED IAW R5-57-22-12058, REV A.
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.
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.