N856GT
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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.
121 reports on file, 2014-07-18 – 2025-12-05.
Part: WARNING MESSAGE — ILLUMINATED (APU) · airframe 58,049 hrs · 9,569 cycles
EICAS APU INDICATION IN FLIGHT. APU DUCT LEAK STATUS MSG. QRH COMPLIED WITH (APU FIRE HANDLE PULLED)(<P>OPERATED APU FOR ABOUT 3 HOURS WITH BLEED ON, NO LEAKAGE OBSERVED AND DETECTED REF AMM 49-11-00-862-001.
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 17R SUSPECT CRACKED(<P>EMP - STA 2598 AFT FACE STRINGER 17R CRACKED AREA REPAIRED I.A.W RI-53-81-17720 REV.A DATE: 28 JUL 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 2180 AFT AND FWD, S-12L STRINGER FOUND CRACKED.(<P>M/D - STA 2180 AFT AND FWD, S-12L STRINGER CRACKED AREA REPAIRED IAW SRM 53-60-03-2R-3 ALTERNATIVE 4 FIG 205 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 7R SUSPECT CRACKED.(<P>EMP - STA 2598 FWD FACE STRINGER 7R CRACKED AREA REPAIRED I.A.W RI-53-81-17714 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 958 S9R STRINGERS AREA FOUND CRACK AS PER EO 4853A131 1&2(<P>M/D STA 958 S9R STRINGERS AREA CRACKED REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 978 S8R STRINGER AREA FOUND CRACK AS PER EO 4853A131 1&2(<P>M/D STA 970 TO 980+10 S8R STRINGER AREA FOUND CRACK AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 12R SUSPECT CRACKED. STA 2598 AFT FACE STRINGER 12R CRACKED AREA REPAIRED I.A.W RI 53-81-17726 REV.A DATE: 28 JUL 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 798 S9L STRINGER AREA FOUND CRACK AS PER EO 4853A 131 1 & 2.(<P>M/D STA 798 S9L STRINGER AREA CRACKS WERE REPAIRED IAW B747-8F SRM 53-20-03 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 927 S7R STRINGERS AREA FOUND CRACK AS PER EO 4853A13 1 & 2.(<P>M/D STA 927 S7R STRINGERS CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-20-03 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
2 EA CRACK WERE FOUND ON STRINGER O/B SIDE AT FWD OF BS 2360 STR 2L AREA.(<P>2 EA CRACKS ON STRINGER O/B SIDE AT FWD OF BS 2360 STR 2L AREA WERE REPAIRED IAW RI-53-61-17703 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 905 S8R STRINGER FOUND CRACK.<BR>(<P>M/D - STA 905 S8R STRINGER CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 25L SUSPECT CRACKED.(<P>EMP - STA 2598 AFT FACE STRINGER 25L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-1 REPAIR 1 TR 53-151. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
CRACKS WERE FOUND ON STRINGER I/B AND O/B SIDE AT FWD OF BS 2360 STR 2R AREA.(<P>CRACKS ON STRINGER I/B AND O/B SIDE AT FWD OF BS 2360 STR 2R AREA WERE REPAIRED IAW RI-53-61-17706 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: RIB — CRACKED (ZONE 500 AILERON) · airframe 56,498 hrs · 9,332 cycles
LHW T/E I/B AILERON R/H HINGE ATTACH R/H RIB UPPER FLANGE FOUND CRACKED.(<P>HW T/E I/B AILERON R/H HINGE ATTACH R/H RIB UPPER FLANGE REPAIRED I.A.W RI-57-20-17699 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 2180 AFT AND FWD, S-11R STRINGER FOUND CRACKED.(<P>M/D - STA 2180 AFT AND FWD, S-11R STRINGER CRACKED AREA REPAIRED IAW SRM 53-60-03-2R-3 AL 4 FIG 205 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 8L SUSPECT CRACKED. - STA 2598 FWD FACE STRINGER 8L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 6L SUSPECT CRACKED.(<P>EMP - STA 2598 AFT FACE STRINGER 6L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
STA 2360 AFT FACE S4R CRACKED(<P>STA 2360 AFT FACE S4R CRACKED AREA REPAIRED IAW RI-53-81-17727 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2360 AFT FACE S3R FOUND CRACK.(<P>EMP - STA 2360 AFT FACE S3R CRACK AREA REPAIRED I.A.W RI-53-81-17730 REV.A DATE: 28 JUL 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
MAIN DECK STA 862 STRINGER 7R FOUND CRACK.(<P>MAIN DECK STA 862 STRINGER 7R CRACK AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 2180 FWD AND AFT, S-10R STRINGER FOUND CRACKED.(<P>M/D - STA 2180 FWD AND AFT, S-10R STRINGER CRACKED AREA REPAIRED IAW SRM 53-60-03-2R-3 ALTERNATIVE 4 FIG 205 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: FLAP — DAMAGED · airframe 56,498 hrs · 9,332 cycles
#8 V/C FLAP LSA DAMAGED.(<P>PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
Part: INLET — DAMAGED (ZONE 400) · airframe 56,498 hrs · 9,332 cycles
POWERPLANT - B747-8/GENX-2B #1 ENGINE INLET COWL LIP SKIN DENT/DAMAGE - REPAIRED POWERPLANT - B747-8/GENX-2B NR 1 ENGINE INLET COWL LIP SKIN DENT/DAMAGE - REPAIRED I.A.W B747-8F SRM 54-10-01-2R-7 REPAIR 7 REV.46 DATE:20JUN 2025 AND RI-54-10-17773 REV A. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 818 S7R STRINGER AREA FOUND CRACK AS PER EO 4853A131 1 & 2.(<P>M/D STA 818 S7R STRINGER CRACKED AREA REPAIRED IAW B747-8F SRM 53-20-03 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: LADDER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D TO U/D LADDER BETWEEN #6 AND #7 STEP AFT SUPPORT FOUND CRACKED(<P>M/D TO U/D LADDER BETWEEN #6 AND #7 STEP AFT SUPPORT CRACKED AREA REPAIRED I.A.W RI-25-13-17698 REV.A DTAE: 7 JUL 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
MAIN DECK STA 975 S7R FOUND CRACK.(<P>MAIN DECK STA 970 TO 980+10 S7R CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
2 EA CRACKS WERE FOUND ON STRINGER I/B SIDE AT FWD OF BS2360 STR 1R AREA.(<P>CRACKS ON STRINGER I/B SIDE AT FWD OF BS2360 STR 1R AREA REPAIRED IAW RI-53-61-17705 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 2180 AFT AND FWD, S-12R STRINGER FOUND CRACKED.(<P>M/D - STA 2180 AFT AND FWD, S-12R STRINGER CRACKED AREA REPAIRED IAW SRM 53-60-03-2R-3 ALTERNATIVE 4 FIG 205 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 2360 FWD, S-23R STRINGER FOUND CRACKED(<P>M/D - STA 2360 FWD, S-23R STRINGER CRACKED AREA REPAIRED I.A.W RI-53-61-17746 REV.A DATE:29 JUL 2025. NO FURTHER DEFECTS NOTED</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - #2360 PRESSURE BULKHEAD AFT FACE STR #4L SUSPECT CRACK. PRESSURE BULKHEAD AFT FACE STR #4L CRACK REPAIRED IAW RI-53-81-17724 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 1R SUSPECT CRACKED.(<P>EMP - STA 2598 FWD FACE STRINGER 1R CRACKED AREA REPAIRED IAW RI-53-81-17713 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
STA 2360 AFT FACE S6L CRACKED(<P>STA 2360 AFT FACE S6L CRACK AREA REPAIRED I.A.W RI-53-81-17721 REV.A DATE: 10 JUL 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 919 S8L STRINGER AREA FOUND CRACK AS PER EO 4853A131 1 & 2.(<P>M/D STA 919 S8L STRINGER AREA CRACKED AREA REPAIRED IAW B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 7L SUSPECT CRACKED.(<P>EMP - STA 2598 FWD FACE STRINGER 7L CRACKED AREA REPAIRED IAW RI-53-81-17707 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - #2360 PRESSURE BULKHEAD AFT FACE STR #16R SUSPECT CRACK.(<P>EMP - #2360 PRESSURE BULKHEAD AFT FACE STR #16R CRACK AREA REPAIRED IAW RI-53-81-17754 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 880-890 S8L STRINGER AREA FOUND CRACK AS PER EO 4853A131 1 & 2.(<P>M/D STA 880-890 S8L STRINGER CRACKED AREA REPAIRED AS PER EO 4853A131 1 & 2 B747-8F SRM 53-20-03 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
MAIN DECK STA 785 S7R FOUND CRACK.(<P>MAIN DECK STA 785 S7R CRACKED AREA REPAIRED I.AW B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 937 S8R STRINGERS AREA FOUND CRACK AS PER EO 4853A131 1&2(<P>M/D STA 937 S8R STRINGERS AREA CRACK REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 4L SUSPECT CRACKED.- STA 2598 AFT FACE STRINGER 4L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
1 EA CRACK WAS FOUND ON STRINGER UPPER SIDE AT FWD OF BS 2360 STR 6R AREA(<P>1 EA CRACK ON STRINGER UPPER SIDE AT FWD OF BS 2360 STR 6R AREA REPAIRED I.A.W B747-8F SRM 53-60-03-2R-8 REPAIR & TRE53-149 REV 46 20JUN2025. NO FURTHER DEFECTS NOTED</P>)
Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 56,498 hrs · 9,332 cycles
AIRCRAFT DAMAGE LOG 8337 - DENT RH WE 724.5 L/E CAMBER FLAP #17 WITHIN LIMITS PER SRM 57-41-01A-01 DETAIL VIII. W: 24. D" Y: 0.120" W/Y 33(<P>AIRCRAFT DAMAGE LOG 8337 - DENT RH WE 724.5 L/E NOSE SKIN REPAIRED I.A.W RI-57-40-17783 REV.A DATE: 22 JUL 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 850-862 S10L STRINGER AREA FOUND SEVERAL CRACKS AS PER EO 4853A131 1 & 2.(<P>M/D STA 850-862 S10L STRINGER CRACKED AREAS REPAIRED IAW B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: SKIN — CRACKED (ZONE 300 RUDDER) · airframe 56,498 hrs · 9,332 cycles
FOUND CRACK ON RUDDER.(<P>PERFORMED REPAIR AT CRACK AREA AS PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - #2360 PRESSURE BULKHEAD AFT FACE STR #16L SUSPECT CRACK. PRESSURE BULKHEAD AFT FACE STR #16L CRACK AREA REPAIRED IAW RI-53-81-17763 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 3L SUSPECT CRACKED.(<P>EMP - STA 2598 AFT FACE STRINGER 3L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 100) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 42R SUSPECT CRACKED.(<P>EMP - STA 2598 AFT FACE STRINGER 42R CRACKED AREA REPAIRED IAW RI-53-81-17716 REV 46. NO FURTHER DEFECTS NOTED.</P>)
Part: FAIRING — CRACKED (ZONE 100) · airframe 56,498 hrs · 9,332 cycles
LONGERON BOX FAIRING FOUND CRACK.(<P>PERFORMED REPAIR AT CRACKED AREA AS PER RI-53-40-17743 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: FLAP — DAMAGED · airframe 56,498 hrs · 9,332 cycles
#7 V/C FLAP LSA DAMAGED.(<P>PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
CRACKS WERE FOUND ON STRINGER O/B SIDE AT FWD OF BS 2360 STR 1L AREA(<P>CRACKS ON STRINGER O/B SIDE AT FWD OF BS 2360 STR 1L REPAIRED I.A.W RI-53-61-17704 REV.A . NO FURTHER DEFECTS.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 2180 FWD AND AFT, S-10L STRINGER FOUND CRACKED.(<P>M/D - STA 2180 FWD AND AFT, S-10L STRINGER CRACKED AREA REPAIRED IAW SRM 53-60-03-2R-3 ALTERNATIVE 4 FIG 205 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 879 AND STA 882 S7L STRINGER AREA FOUND CRACK AS PER EO 4853A131 1 & 2.(<P>M/D STA 879 AND STA 882 S7L STRINGER AREA CRACK REPAIRED IAW 747-8F SRM 53-20-03 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: LADDER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D TO U/D LADDER 8 & 10 STEP PANEL FOUND CRACKED. M/D TO U/D LADDER NR 8 & 10 STEP PANEL CRACKED AREA REPAIRED I.A.W RI-25-13-17698 REV.A DATE: 7JUL 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
2 EA CRACKS WERE FOUND ON STRINGER UPPER SIDE AT FWD OF BS 2360 STR 7R AREA.(<P>2 EA CRACKS ON STRINGER UPPER SIDE AT FWD OF BS 2360 STR 7R AREA REPAIRED IAW B747-8F SRM 53-60-03-2R-8 REPAIR 8 TR53-149. NO FURTHER DEFECTS NOTED.</P>)
Part: RIB — CRACKED (ZONE 600 AILERON) · airframe 56,498 hrs · 9,332 cycles
RHW R/H O/B AILERON ATTACH HINGE L/H AFT SPAR RIB (691JB) FLANGE FOUND CRACKED AS MARKED.(<P>RHW R/H O/B AILERON ATTACH HINGE L/H AFT SPAR RIB (691JB) FLANGE FOUND CRACKED AREA REPAIRED IAW RI-57-51-17702 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: CHANNEL — CRACKED (ZONE 300) · airframe 56,498 hrs · 9,332 cycles
HORIZONTAL STAB. T/E AFT SUPPORT WEDGE U CHANNEL FOUND CRACK.(<P>REPLACED U CHANNEL AS PER RI-55-10-17723 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 5L SUSPECT CRACKED. - STA 2598 AFT FACE STRINGER 5L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 770 S7R STRINGERS AREA FOUND CRACK AS PER EO 4853A131 1 & 2.(<P>M/D STA 770 S7R STRINGERS AREA FOUND CRACK AREA REPAIRED IAW B747-8F SRM 53-20-03 REPAIR 1 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 957 S7R STRINGERS AREA FOUND CRACK AS PER EO 4853A131 1&2(<P>M/D STA 957 S7R STRINGERS CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
STA 2360 AFT FACE S6R CRACKED.(<P>STA 2360 AFT FACE S6R CRACKED AREA REPAIRED IAW RI-53-81-17725 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
MAIN DECK R/H STRINGER 7R STA 842 FOUND CRACK.(<P>MAIN DECK R/H STRINGER 7R STA 842 CRACKED AREA REPAIRED I.AW B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED</P>)
Part: FLAP — DAMAGED · airframe 56,498 hrs · 9,332 cycles
#19 V/C FLAP LSA DAMAGED.(<P>PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 51L SUSPECT CRACKED. - STA 2598 FWD FACE STRINGER 51L CRACKED AREA REPAIRED I.A.W RI-53-81-17739 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: RIB — CRACKED (ZONE 600 AILERON) · airframe 56,498 hrs · 9,332 cycles
RHW T/E I/B AILERON L/H O/B ATTACH HINGE RIB UPPER T/E FLANGE FOUND CRACKED AS MARKED.(<P>RHW T/E I/B AILERON L/H O/B ATTACH HINGE RIB UPPER T/E FLANGE CRACKED AREA REPAIRED IAW RI-57-20-17701 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 879 S7R STRINGERS AREA FOUND CRACK AS PER EO 4853A131 1 & 2.(<P>M/D STA 879 S7R STRINGERS CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE:20 JUN 2025. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 26R SUSPECT CRACKED.(<P>EMP - STA 2598 AFT FACE STRINGER 26R CRACKED AREA REPAIRED IAW RI-53-81-17744 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: RIB — CRACKED (ZONE 600 AILERON) · airframe 56,498 hrs · 9,332 cycles
RHW T/E I/B AILERON L/H I/B ATTACH HINGE RIB UPPER T/E FLANGE FOUND CRACKED AS MARKED.(<P>RHW T/E I/B AILERON L/H I/B ATTACH HINGE RIB UPPER T/E FLANGE REPAIRED IAW RI-57-20-17700 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: FLAP — DAMAGED · airframe 56,498 hrs · 9,332 cycles
#20 V/C FLAP LSA DAMAGED. PERFORMED REPAIR AT LSA DAMAGE AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D STA 986 S7R STRINGERS AREA FOUND CRACK AS PER EO 4853A131 1 & 2(<P>M/D STA 980+10 TO 980+30 S7R STRINGERS CRACKED AREA REPAIRED I.A.W B747-8F SRM 53-20-03-2R-1 REPAIR 1 REV.46 DATE 20 JUN 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 5R SUSPECT CRACKED.- STA 2598 FWD FACE STRINGER 5R CRACKED AREA REPAIRED IAW RI-53-81-17715 REV.A. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 25R SUSPECT CRACKED. - STA 2598 AFT FACE STRINGER 25R CRACKED AREA REPAIRED IAW RI-53-81-17753 REV.A. NO FUTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 7L SUSPECT CRACKED.(<P>EMP - STA 2598 AFT FACE STRINGER 7L CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: RETAINER — CRACKED (ZONE) · airframe 56,498 hrs · 9,332 cycles
LH WLG FWD O/B CUTOUT SEAL RETAINER FOUND CRACK(<P>LH WLG FWD O/B CUTOUT SEAL RETAINER CRACK AREA REPAIRED I.A.W RI-53-51-17751 REV A DATE:29 JUL 2025. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
1 EA CRACK WAS FOUND ON STRINGER UPPER SIDE AT FWD OF BS 2360 STR 7L.(<P>1 EA CRACK WAS FOUND ON STRINGER UPPER SIDE AT FWD OF BS 2360 STR 7L AREA REPAIRED IAW B747-8F SRM 53-60-03-2R-8 REPAIR8 TR53-149. NO FUTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 FWD FACE STRINGER 1L SUSPECT CRACKED.(<P>EMP - STA 2598 FWD FACE STRINGER 1L CRACKED AREA REPAIRED IAW B747-8F SRM 53-80-03-2R-2 REPAIR 2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
EMP - STA 2598 AFT FACE STRINGER 4R SUSPECT CRACKED. BS 2598 AFT FACE STRINGER 4R CRACKED AREA REPAIRED IAW SRM 53-80-03-2R-2 TR 53-152. NO FURTHER DEFECTS NOTED.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 56,498 hrs · 9,332 cycles
M/D - STA 1960 AFT, S-8R STRINGER FOUND CRACKED.(<P>M/D - STA 1960 AFT, S-8R STRINGER CRACKED AREA REPAIRED IAW SRM 53-60-03-2R-4 ALTERNATIVE 3 FIG 204 REV.46. NO FURTHER DEFECTS NOTED.</P>)
Part: WARNING MESSAGE — ACTIVATED (CABIN PRESSURE) · airframe 56,367 hrs · 9,310 cycles
CABIN ALTITUDE WARNING MSG AT 39,100". C/W IAI AND CHECKLIST(<P>CMC REVIEWED, NIL RELATED FAULT MSG. REF IFIM 31-98-00-810-801 CORRECTIVE ACTION C/W CPCS CENTER A & B CMC TEST OK. REF AMM 21-31-03</P>)
Earlier reports · 2014–2023 · 44 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
DURING EO 4852A061 - NOSE CGO DOOR SEAL INSTALLATION (65B13077-221#C) TIME LIMITED REPAIR. THE OUTER SKIN PLATE P/N: 65B13077-6 FOUND 1EA FASTENER HOLE COUNTERSINK ENLARGED(<P>NOSE CGO DOOR SEAL RETAINER AND SKIN PLATE DAMAGE AREA REPAIRED IAW RI-52-71-16340 REV A. NO FURTHER DEFECTS NOTED.</P>)
Part: CHANNEL — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
LH HORIZONTAL STAB TIP FAIRING T/E WEDGE FOUND CRACK(<P>NEW "U" CHANNEL REPLACED AS PER RI-55-10-16341 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
#19 V/C FLAPÃÂ LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA DAMAGED AREA AS PER CMM 57-55-42- REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
EMP - LH HORIZONTAL STAB TIP FAIRING L/E FAIRING UPPER SURFACE FASTENER HOLE FOUND ELONGATED(<DIV ID="1520" CLASS="LEVEL_1"> / <DIV CLASS="VALUE"> / <P>EMP - LH HORIZONTAL STAB TIP FAIRING L/E FAIRING P/N 65B03521-55 FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-55-10-16345 REV A. NO FURTHER DEFECTS NOTED.</P> / </DIV> / </DIV>)
Part: POWER SUPPLY — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
EMERGENCY LT BATTERY PACKS CAPACITY CHECK FOUND POWER SUPPLY M5168 AND M5169 FAIL.(<P>POWER SUPPLY M5168 AND M5169 REPLACED AND OPERATION CHECKED NORMAL IAW AMM 33-51-04. PN: 56813 (M5168) & 57412 (M5169)</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
UPPER RUDDER L/H LWR AREA T/E FOUND DENT(<P>PERFORMED REPAIR AT DENT AREA AS PER SRM 51-70-04 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)
Part: LAMP — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
U/D STA 406 L5730 EMER AISLE LT FOUND INOP.(<P>EMER AISLE LT AND FUSE REPLACED & OPERATION CHECKED NORMAL IAW AMM 33-51-07.</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
VERTICAL STAB LH ANCHOR NUT RETAINER FOR TIP FAIRING DAMAGED.(<P>VERTICAL STABILIZER TIP RIB LH GANG CHANNEL P/N: G12447-2-3-2503-5 REPAIRED IAW RI-55-30-16346 REV A. NO FURTHER DEFECTS NOTED.</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
APU COMPARTMENT L/H STA 2664 WL 305 FRAME FOUND CRACKED.(<P>APU COMPARTMENT L/H STA 2664 WL 305 FRAME P/N: 65B02757-13 CRACK AREA REPAIRED IAW RI-53-82-16342 REV A. NO FURTHER DEFECTS NOTED.</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
EMP - LH HORIZONTAL STAB TIP FAIRING LOWER SUPPORT CHORD FOUND CRACKED.(<P>EMP - LH HORIZONTAL STAB TIP FAIRING AREA LOWER CHORD P/N: 65B03520-53 CRACK AREA REPAIRED IAW SRM 55-10-09-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
UPPER RUDDER R/H LWR AREA T/E FOUND DENT(<P>PERFORMED REPAIR AT DENT AREA AS PER SRM 51-70-04 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
#7 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA DAMAGED AREA AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
Part: LAMP — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
EMER SLIDE LT L1533 FOUND INOP.(<P>LAMPS REPLACED AND OPERATION CHECKED NORMAL IAW AMM 33-51-10. NO FURTHER DEFECTS NOTED</P>)
Part: FRAME — UNKNOWN (UNKNOWN) · airframe 48,144 hrs · 8,109 cycles
REFER TO EO 1957A593 PART 2, SB 747-57-2369, #8 FLAP TRACK FAIRING ACTUATOR FRAME FOUND EXISTING REPAIR MOD.(<P>EO 1957A593 PART 2, SB 747-57-2369, #8 FLAP TRACK FAIRING ACTUATOR FRAME EXISTING REPAIR MOD AREA ACCOMPLISHED IAW RI-57-50-16339 REV A. NO FURTHER DEFECTS NOTED</P>)
Part: WHEEL — UNKNOWN (UNKNOWN) · airframe 48,124 hrs · 8,104 cycles
TIRE PRESSURE CAUTION MSG FOLLOWED BY TIRE PRESSURE STS MSG.(<P>#12 MAIN TIRE PRESSURE LOW. R/R #11 AND #12 WHEELS PER AMM 32-45-01. OPS & LEAK CHECK GOOD</P>)
2022
Part: THRUST REVERSER — DAMAGED · airframe 45,758 hrs
NO 4 ENG VIBRATION ON 4.1 AFTER FL280 FOR ALL CLIMBS PERFORMED ENGINE VIBRATION INSPECTION IAW AMM 71-00-00. FOUND MISSING PANEL AND DAMAGE TO THRUST REVERSER. PERFORMED PARTS DEPARTED INSPECTION IAW AMM 05-51-59)
2021
Part: NONE — NONE · airframe 42,297 hrs · 7,187 cycles
MAIN CARGO DECK FLOOR WEB DAMAGED FS228(<P>REPAIRED PER EO 4853A136</P>)
2020
Part: INDICATOR — NO INDICATION (AIRSPEED) · airframe 37,047 hrs · 6,257 cycles
CREW REPORTED LOW SPEED, REJECTED T.O. NO LEFT AIRSPEED INDICATION AFTER BRAKES RELEASED, REF AMM 05-51-10. NO ACTION REQUIRED. BRAKES CHECK GOOD AND PLUGS ARE INTACT, NDN. PERFORMED GROUND TEST OF ADIRU L, TEST PASSED, REF AMM 34-25-00. PERFORMED GVI OF PITOT HEADS PER FIM 34-21-00-810, NO DEFECTS OR RESTRICTIONS.
2019
Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 31,964 hrs · 5,370 cycles
REPAIR - DISCREPANT CONDITION ON FUSELAGE SKIN NEAR STA 636, S-40R. &NBSP;(<P>ACCOMPLISHED THE JOB IAW EI NO. T2019A53M-3049 REV. 2. JOB COMPLETED AND CONDITION CHECK SATISFIED.&NBSP;</P>)
Part: MOTOR — FAILED (TE FLAP) · airframe 31,964 hrs · 5,370 cycles
FOUND INBD FLAP ELEC MOTOR FAIL. (<P>PERFORMED WIRING CHECK, THE RESULT WAS SATISFACTORY IAW WDM 27-51-21 REV. 21. INSTALLED NEW INBD ELECTRICAL MOTOR IAW AMM 27-51-17-000-801 REV. 29 AND 27-51-17-400-801 REV. 29, STEP 3, A TO D (3). PERFORMED INSTALLATION TEST, TEST RESULT WAS NORMAL IAW AMM 27-51-17-400-801 REV. 29.&NBSP;</P>)
Part: AILERON — DELAMINATED (LT AILERON) · airframe 31,964 hrs · 5,370 cycles
FOUND LT WING OTBD AILERON DELAMINATION. &NBSP;(<P>CUT OUT THE DELAMINATION MATERIAL AND CLEANED. MEASURED THE DAMAGED AREA (L = 2", W = 0.7", D = 4 PLIES 0), (FROM AFT EDGE .69 FROM INBD EDGE, WBL 918), BOND PLIES (L = 8", W = 5"). USED WET LAYUP WITH RESIN, CURED AT 200 DEG F FOR 240 MINUTES AND MAINTAINED MINIMUM VACUUM PRESSURE AT 32 IN/HG IAW SRM 57-60-01-2R-2. REFER TO SRM 51-70-04-2R-0 REV. 27. MADE AN ENTRY OF REWORK MOMENT ON THE ALUMINUM FOIL MOMENT MARKER. IAW SRM 51-60-01-0G-0 REV. 27, CHECK CONDITION WAS SATISFACTORY.</P>)
Part: BRACKET — WORN (LT ELEVATOR) · airframe 31,964 hrs · 5,370 cycles
L INBD ELEVATOR IDLE CRANK BRACKET ASSY AND ATTACH BOLT WORN, AND BEARING MIGRATION AT CRANK ASSY. (<P>REMOVED AND REPLACED LT INBD ELEVATOR IDLE CRANK BRACKET ASSY IAW AMM 20-51-01-912-008 REV. 29. CONDITION CHECK SATISFACTORY.&NBSP;</P>)
2018
Part: DOOR — DAMAGED (LT BMLG) · airframe 29,881 hrs · 5,027 cycles
ON ARRIVAL FOUND LEFT HAND BODY GEAR DOOR DAMAGED AT TWO AREAS 3.5 X 3.5&NBSP; AND 3.5 X 4.5&NBSP;(<P>PERFORMED TEMP REPAIR REF EO 4852A050.&NBSP;</P>)
2017
Part: CHANNEL — DEFORMED (BS 600-640) · airframe 24,247 hrs · 4,108 cycles
FWD CARGO BAY, BS 600 - 640, RBL 90.8, CEILING SUPPORT CHANNEL DEFORMED. REPAIRED IAW RI-25-50-12007, REV A.
Part: FAIRING — DAMAGED (NR 4 PYLON) · airframe 24,247 hrs · 4,108 cycles
NR 4 PYLON OTBD AFT FAIRING FWD LOWER SPAR FOUND HEAT DAMAGE AT WEB AREA APPROX 12" X 1". REPAIRED IAW RI-54-00-12009, REV A.
Part: ATTACH BRACKET — CRACKED (LT OVERWING) · airframe 24,247 hrs · 4,108 cycles
LT OVERWING ACCESS PANEL 51GT INNER CAVITY NR 2 VAPOR BARRIER OTBD EDGE ATTACH SUPPORT BRACKET FOUND CRACKED. REPAIRED IAW RI-57-41-12002, REV A.
Part: SUPPORT CHANNEL — CRACKED (LT MLG) · airframe 24,247 hrs · 4,108 cycles
LT LANDING GEAR OTBD SUPPORT CHANNEL FOUND CRACKED. REPAIRED IAW RI-57-22-1195, REV A.
Part: BRACKET — DAMAGED (RT WING) · airframe 24,247 hrs · 4,108 cycles
RIGHT WING MLG WS 500 RETRACT ACTUATOR HYD SUPPLY HOSE ANGLE BRACKET ELONGATED. FABRICATED AND INSTALLED A NEW BRACKET IAW RI-32-32-12023, REV A.
Part: CHANNEL — DEFORMED (BS 630-640) · airframe 24,247 hrs · 4,108 cycles
FWD CARGO BAY, BS 630 - 640, RBL 78.3, CEILING SUPPORT CHANNEL DEFORMED. REPAIRED IAW RI-25-50-11999, REV A.
Part: SUPPORT — DEFORMED (AFT CARGO BAY) · airframe 24,247 hrs · 4,108 cycles
AFT CARGO BAY BS 1830 CEILING LINER SUPPORT WEB DEFORMED. THE CEILING LINER SUPPORT WEB WAS REPAIRED IAW RI-25-53-12010, REV A.
Part: SUPPORT CHANNEL — DEFORMED (BS 1840) · airframe 24,247 hrs · 4,105 cycles
AFT CARGO BAY CEILING LINER SUPPORT CHANNEL DEFORMED AT BS 1840, RBL 62. REPAIRED IAW RI-25-53-12017, REV A.
Part: SKIN — GOUGED (CARGO DOOR) · airframe 24,207 hrs · 4,108 cycles
M/D SIDE CARGO DOOR OUTER SKIN GOUGE DAMAGE(<P>M/D SIDE CARGO DOOR OUTER SKIN GOUGE DAMAGE AREA REPAINTED AS PER RJ-52-32-12000 REVA</P>)
Part: SUPPORT BRACKET — CRACKED (RT OVERWING) · airframe 24,247 hrs · 4,108 cycles
RT OVERWING ACCESS PANEL 611GT INNER CAVITY NR 3 PYLON VAPOR BARRIER OTBD EDGE ATTACH SUPPORT BRACKET FOUND CRACKED. REPAIRED IAW RI-57-41-12003, REV A.
Part: HEAT SHIELD — TORN (A/C BAY) · airframe 24,247 hrs · 4,108 cycles
NR 2 PACK INBD HEAT SHIELD FOUND TORN. REPAIRED IAW RI-53-49-12019, REV A.
Part: CHANNEL — DEFORMED (BS 630-640) · airframe 24,247 hrs · 4,108 cycles
FWD CARGO BAY, BS 630 - 640, RBL 70.1, CEILING SUPPORT CHANNEL DEFORMED. REPAIRED IAW RI-25-50-11999, REV A.
Part: SUPPORT CHANNEL — DAMAGED (BS 1840) · airframe 24,247 hrs · 4,108 cycles
AFT CARGO BAY CEILING LINER SUPPORT CHANNEL AT BS 1840, RBL 72 DEFORMED AND CRACKED. REPAIRED IAW RI-25-53-12017, REV A.
2016
Part: FUEL SYS — MALFUNCTIONED · airframe 20,918 hrs · 3,572 cycles
COULD NOT GET FUEL OUT OF CENTER TANK. RT CENTER WING JETTISON & OVERRIDE PUMP OPS NORMAL IAW AMM 28-31-00.
2015
Part: SKIN — DAMAGED (BS 180-251) · airframe 15,623 hrs · 2,768 cycles
LIGHTNING STRIKE, FUSELAGE SKIN, NOSE, CARGO DOOR UPPER EXTERNAL SURFACE BS 190 S14L AND BS 251, S-12L AND BS 180, S14L. REPAIRED THE AREA IAW EI T2015A52B-1826 REV 2.
Part: SKIN — DAMAGED (BS 337-600) · airframe 15,623 hrs · 2,768 cycles
FOUND FIVE LIGHTNING STRIKES ON FASTENER HEADS AT SEC 41 AND 42 OUTER SKIN SURFACE. REPAIRED DAMAGED AREA IAW EI T2015A53B-1781, REV. 2.
Part: SKIN — DAMAGED (BS 368) · airframe 15,623 hrs · 2,768 cycles
LIGHTNING STRIKE ON FASTENER LT FUSELAGE LOWER EXTERNAL SURFACE AT BS 368, S32L. REPAIRED THE AREA IAW EI T2015A53B-1795, REV 2.
Part: SKIN — DAMAGED (BS 370) · airframe 15,623 hrs · 2,768 cycles
LIGHTNING STRIKE ON FASTENER, LT FUSELAGE LOWER EXTERNAL SURFACE AT BS 370 S35L. REPAIRED THE AREA IAW EI T2015A53B-1800, REV.
Part: DRIVE UNIT — FAILED (HYD SYSTEM) · airframe 14,136 hrs · 2,542 cycles
EICAS MESSAGES HYDRAULIC PRESSURE SYS 1 FOLLOWED ECL/QRH PROCEDURES, LANDED. REMOVED NR 1 ADU IAW MM 29-11-08, OPS NORMAL, INSPECTED NR 1 EDP IAW MM 29-11-05 BOTH PUMPS OPS & LEAK CHECKD GOOD. HYD SYSTEM, OPS CHECK NORMAL.
2014
Part: RIVET — DAMAGED (FUSELAGE) · airframe 11,215 hrs · 2,106 cycles
SDR UIEA2014071800338. LIGHTNING STRIKE AT 12 O'CLOCK POSITION. EO4853A013 DOCUMENTS & APPROVES THE CAT. A PERMANENT REPAIR TO THE PSE & FCBS STRUCTURE DAMAGED BY THIS EVENT. THIS EO DOCUMENTS & APPROVES THE RIVET REPAIRS ACCOMPLISHED WHETHER THEY ARE REPLACEMENT OR HOLE PLUG RIVETS, ACCOMPLISHED IAW PROCEDURES DEFINED IN SRM 53-00-01-2R-9.
Part: ANTENNA — DAMAGED (VHF COMM) · airframe 11,215 hrs · 2,106 cycles
LIGHTNING STRIKE AT 12 O'CLOCK POSITION. PRELIMINARY INSPECTION IAW AMM 05-51-13 201 FOUND MULTIPLE BURN MARKS AROUND RIVETS, DAMAGED VHF, GPS, ELT, ADF & HF ANTENNAS. REPLACEMENT OF DAMAGED PARTS & REPAIRS ARE CURRENTLY IN PROGRESS & REMAINDER OF CONDITIONAL INSPECTION WAS COMPLETED.