N612UP
Registered owner: C C & E I LLC, KY (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.
61 reports on file, 2019-02-03 – 2026-08-10.
Part: SUPPORT BRACKET — BROKEN (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
FOUND LT TAIL CONE SUPPORT BRACKET BROKEN BS 2460, LBL 36.
Part: ACCESS PANEL — ERODED (ZONE 300) · airframe 30,661 hrs · 4,488 cycles
VERTICAL STABILIZER TIP ACCESS PANEL 327 SKIN EROSION (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 6" AROUND HEATED AREA ,PER 747 NDT MANUAL PART 1 51-01-01 REV:183 <BR>RESULT:NO DEFECT WAS FOUND
Part: RIB — CRACKED (ZONE 500) · airframe 30,661 hrs · 4,488 cycles
CRACKED RIB, AFT SIDE OF LT WING INBD AILERON INBD WEB UPPER CHORD, WBL 445.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, FWD SIDE OF STA 740 S-45L.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, FWD SIDE OF STA 2360 AT S-2L (LEVEL2) (REPAIR) FABRICATED REPAIR STRINGER IAW. EGAT WORK SHEET NO.60604 STEP 10. (SRM 53-60-03-2R-8 REV.49)
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF BS 740 S-31L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
MAJOR REPAIR - STRINGER CRACK, FWD SIDE OF STA 740 S-46L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, FWD SIDE OF BS 1960, S38L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF BS 1960, S39L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, FWD SIDE OF BS 1960 S-39L.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF BS 2180 S-15R. INSPECTION COMPLETED FOR PERFORMED EGAT EI NO.F2026A53M-1616 SEQUENCE B STEP 22. RESPECTIVELY PART MARK THE REPAIR PARTS RII COMPLETED FOR PERFORMED EGAT EI NO.F2026A53M-1616 SEQUENCE B STEP 23. VALIDATE SPECIALIZED PROCESS OUTLINED IN REPAIR INSTRUCTIONS WERE ACCOMPLISHED. 24. OK TO INSTALL.
Part: SEAL — BROKEN (ZONE 500 FLAP) · airframe 30,661 hrs · 4,488 cycles
BROKEN MOLDING SEAL , LT WING NR 4 V.C FLAP OUTBD SIDE MOLDING SEAL IAW SRM 57-43-02-2R-4, REV 49, REFER TO SOPM 20-50-12 REV 160. PERFORM REPAIR AS BELOW STEP :1. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70 F FOR 20 HOURS.2. CONDITION CHECK IS SATISFACTORY.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, FWD SIDE OF BS 1960 S15R. CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, FWD SIDE OF BS 1960, S14R. CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF BS 1960 S-17L. COMPLETED FOR PERFORMED EGAT EI F2026A53M-1619 SEQUENCE B STEP FINAL INSPECTION. VALIDATE THE LIST OF REPAIR MATERIALS WITH PO TRACEABILITY IS DOCUMENTED ON THE FAULT THAT IS ASSOCIATED. INCLUDING FASTENERS, RAW MATERIAL, AND COMPONENTS/PARTS. FINAL INSPECTION ON REPAIR AREA TO ENSURE COMPLIANCE WITH REPAIR REQUIREMENTS.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF STA 1960 S-21R.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER 21L CRACKED, AFT SIDE OF BS 2180. ACCOMPLISHED REPAIR I.A.W EO-98289-REQ0020 REV.1 AND EGAT EI NO.F2026A53M-1699 REV.0 AND EGAT WORK SHEET NO.60603 AND SRM 53-60-03-2R-12 REV.49.
Part: SKIN — DEBONDED (ZONE 500) · airframe 30,661 hrs · 4,488 cycles
DISBOND - SKIN , LOWER FACE OF L/H WING NO. 4 FLAP TRACK AFT FAIRING (REPAIR) PERFORMED NDT/UT FOR REWORKED AREA AND PLUS 6" AROUND HEATED AREA, I.A.W 747 NDT MANUAL PART 1 51-01-01 REV.183, RESULT: NO DEFECT FOUND.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF BS 2180, S15L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF BS 1960, S38L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF BS 1960, S42L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF BS 1960, S40L.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF BS 1960, S41L.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, AFT SIDE OF STA 2360 AT S-7R (LEVEL 2) (REPAIR) RII COMPLETED FOR PERFORMED SRM 53-80-03-2R-3 REV.49 AND EGAT WORK SHEET NO.60585 STEP E.FUTURE MAINTENANCE REQUIREMENTS: 1. RECORDED EGAT EI NO. F2026A53M-1708.
Part: NOT REPORTED — NOT REPORTED · airframe 30,661 hrs · 4,488 cycles
FAULT - ADD SDR FOR EO-85445-JIC1. (EVALUATE) C/W EO-85445-JIC1
Part: NOT REPORTED — NOT REPORTED · airframe 30,661 hrs · 4,488 cycles
FAULT - ADD SDR FOR EO-85445-JIC2. (EVALUATE) C/W EO-85445-JIC2. (EVALUATE)
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER 5L CRACKED, FWD SIDE OF BS 2598. ACCOMPLISHED REPAIR I.A.W. EO-98289-REQ0029 REV.1 AND EGAT EI NO. F2026A53M-1649 REV.0 AND EGAT WORK SHEET NO.60581 AND SRM 53-80-03-2R-2 REV.49.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER 5L CRACKED, AFT SIDE OF BS 2598. ACCOMPLISHED REPAIR I.A.W EO-98289-REQ0028 REV.1 AND EGAT EI F2026A53M-1648 REV.0 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET 60579.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF STA 2360 AT S-7L.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF STA 2360 AT S-6L.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, FWD SIDE OF STA 2598 S-8R. ACCOMPLISHED REPAIR I.A.W EO-98289-REQ0033 REV.1 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET 60578 AND GAT EI F2026A53M-1653 REV.0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, FWD SIDE OF STA 2598 S-5R. ACCOMPLISHED REPAIR I.A.W EO-98289-REQ0030 REV.1 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET NO.60582 AND EGAT EI NO. F2026A53M-1650 REV.0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, FWD SIDE OF BS 2598 S-6R. ACCOMPLISHED REPAIR I.A.W EO-98289-REQ0031 REV.1 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET NO.60583 AND EGAT EI NO. F2026A53M-1651 REV.0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACKED, FWD SIDE OF BS 2598 S-7R. ACCOMPLISHED REPAIR I.A.W EO-98289-REQ0032 REV.1 AND SRM 53-80-03-2R-2 REV.49 AND EGAT WORK SHEET NO.60580 AND EGAT EI NO. F2026A53M-1652 REV.0.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, FWD SIDE OF STA 740 S-19L (LEVEL 1) (REPAIR), RII COMPLETED FOR PERFORMED SRM 53-20-03-2R-5 REV.49 AND EGAT WORK SHEET NO.60592 STEP 19.COMPLETED SHOT PEEN FOR REPAIR CLIP , PERFORMED SPWPS-SP-003 REV.00, VALIDATE THE LIST OF REPAIR MATERIALS WITH PO TRACEABILITY IS DOCUMENTED ON THE FAULT THAT IS ASSOCIATED. INCLUDING FASTENERS, RAW MATERIAL, AND COMPONENTS/PARTS. 44. VERIFY REPAIR IS ACCOMPLISHED PER REQUIREMENTS.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, FWD AND AFT SIDE OF STA 740 S-18L RII COMPLETED FOR PERFORMED SRM 53-20-03-2R-5 REV.49 AND EGAT WORK SHEET NO.60593 STEP 19.COMPLETED SHOT PEEN FOR REPAIR CLIP. PERFORMED SPWPS-SP-003 REV.00, VALIDATE THE LIST OF REPAIR MATERIALS WITH PO TRACEABILITY IS DOCUMENTED ON THE FAULT THAT IS ASSOCIATED. INCLUDING FASTENERS, RAW MATERIAL, AND COMPONENTS/PARTS. 44. VERIFY REPAIR IS ACCOMPLISHED PER REQUIREMENTS.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF STA 2360 AT S-6R. RII COMPLETED FOR PERFORMED EGAT EI NO.F2026A53M-1644 SEQUENCE B STEP 23. VALIDATE SPECIALIZED PROCESS OUTLINED IN REPAIR INSTRUCTIONS WERE ACCOMPLISHED (EX: HEAT TREAT, SHOT/FLAP PEEN, NDT, PLATING, COMPOSITE CURE/BOND TIMES, ETC.) 24. OK TO INSTALL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF STA 2360 AT S-3L. COMPLETED FOR PERFORMED EGAT EI NO.F2026A53M-1664 SEQUENCE A STEP 25. VALIDATE THE LIST OF REPAIR MATERIALS WITH PO TRACEABILITY IS DOCUMENTED ON THE FAULT THAT IS ASSOCIATED. INCLUDING FASTENERS, RAW MATERIAL, AND COMPONENTS/PARTS. 26. VERIFY REPAIR IS ACCOMPLISHED PER REQUIREMENTS.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,661 hrs · 4,488 cycles
STRINGER CRACK, AFT SIDE OF STA 2360 AT S-3R. COMPLETED FOR PERFORM EGAT EI NO.2026A53M-1623 SEQUENCE B STEP 8. HEAT TREAT FROM 7075-O TO T62 CONDITION. 9. DYE PENETRANT INSPECT THE -6 AFT REPAIR STRINGER TO ENSURE A CRACK FREE CONDITION PER SOPM 20-20-02.RESULT:NO CRACK WAS FOUND. INSPECTION COMPLETED FOR PERFORMED EGAT EI NO.F2026A53M-1623 SEQUENCE B STEP 17. RESPECTIVELY PART MARK THE REPAIR PARTS RII COMPLETED FOR PERFORM EGAT EI NO.2026A53M-1623 SEQUENCE B STEP 18. VALIDATE SPECIALIZED PROCESS OUTLINED IN REPAIR INSTRUCTIONS WERE ACCOMPLISHED. 19. OK TO INSTALL.
Part: HANDLE — LACK OF LUBE (ZONE 800) · airframe 29,374 hrs · 4,310 cycles
L1 MAIN ENTRY DOOR EXTERIOR HANDLE DIFFICULT TO EXTEND & STOW. LUBRICATED EXTERIOR FOLDABLE HANDLE JOINT AS NEEDED. SUBSEQUENT OPS CHECK OF L1 ENTRY DOOR HANDLES SATISFACTORY IAW AMM 52-11-13. NO DAMAGE OR DEFECTS NOTED AT THIS TIME.
Part: BULB — INOPERATIVE (ZONE 200) · airframe 29,170 hrs · 4,281 cycles
RIGHT FUSELAGE EXTERIOR EMERGENCY LIGHT IN UPPER DECK AREA AT APPROX BS 580. FWD BULB INOPERATIVE FWD SLIDE LIGHT, LAMP REPLACED IAW AMM 33-51-10-962-001, REV 50. OPS TESTED GOOD.
Earlier reports · 2019–2025 · 20 reports
2025
Part: WARNING MESSAGE — ACTIVATED (CABIN PRESSURE) · airframe 27,082 hrs · 3,971 cycles
**ATB** AT FL320 WE RECEIVED THE CABIN ALT WARING. THE CABIN ALT WAS 10,800. WE RAN THE CHECKLIST AND DESCENDED TO 14000. PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE TEST, LEAKAGE RATE FOUND TO BE WITHIN LIMITS, REF AMM 05-51-08-702-001. AIRCRAFT OK FOR CONT. SERVICE.
Part: CONTROLLER — FALSE INDICATION (SMOKE DETECTION) · airframe 25,158 hrs · 3,688 cycles
AFT FIRE CARGO INDICATION AT 2000 FT ON TK-OFF 35L. SMELLED SMOKE WHILE RUNNING CHECKLIST. NO OBSERVATION FROM FIRE DEPT. AIR TURN BACK. REMOVED AND REPLACED LOWER CARGO SMOKE DETECTION CONTROLLER REF MM 26-16-06-400-801. TESTS NORMAL. OK TO CONTINUE. VISUALLY INSPECTED LOWER AFT PIT, NO DEFECTS NOTED, LOOKED AT ALL THE CARGO SYSTEM PDUÃâ¬â¢S AND ASSOCIATED WIRES, NO DEFECTS NOTED.
Part: FIRE WARNING — ACTIVATED (ZONE 100) · airframe 25,149 hrs · 3,687 cycles
**EMERGENCY DECLARED** **ATB** AFT FIRE CARGO INDICATION AT 2000 FT ON TK-OFF 35L. SMELLED SMOKE WHILE RUNNING CHECKLIST. NO OBSERVATION FROM FIRE DEPT. AIR TURN BACK. OPEN
Part: HOLDER — BROKEN (ZONE 800) · airframe 24,664 hrs · 3,618 cycles
*SDR FILED OPEN* L1 DOOR HAND HOLD FOR CLOSING IS BROKEN REPLACEMENT REQUIRED.
Part: HANDLE — INOPERATIVE (ZONE 800) · airframe 24,921 hrs · 3,655 cycles
L1 DOOR HAND HOLD FOR CLOSING IS BROKEN. INSTALLED HANDLE MM 52-11-02
2024
Part: ACTUATOR — FAULTED (MLG) · airframe 22,866 hrs · 3,362 cycles
ATB. AFTER TAKE-OFF MLG DISAGREE EICAS. COMPLETED CHKLIST, INSTALLED LT WING LG DOWNLOCK ACTUATOR, CHKD OK IAW AMM 29-11-00-292-571 REV 45. REPLACED CASE DRAIN FILTER OF HYD SYS NR 4, AFTER BLED OF HYD IAW AMM 32-32-15-404-006 REV 45 STEP 3A TO STEP 3F(4). INSTALL LWLG DOWNLOCK ACT, CHKD NORMAL. IAW AMM 05-51-58-200-801 REV 45. PERFORMED ALTERNATE LG EXTEND PHASE 1 INSP IAW AMM 32-32-15-404-006 REV. 45. INSTALLED LWLG DOWNLOCK ACT, SERVICEABLE IAW AMM 32-11-33-400-801 REV. 45. INSTALLED LWLG SIDE STRUT SWIVEL. SERVICEABLE IAW AMM 32-32-04-404-006 REV. 45. INSTALLED LWLG DOWNLOCK, OPS SEQUENCE VALVE. SERVICEABLE IAW AMM 32-32-00-350-801 REV.45, PERFORM WLG SWING TEST 3 X. JOB COMPLETE & ACFT RTS.
Part: LANDING GEAR — WARNING MESSAGE (ZONE 700) · airframe 22,865 hrs · 3,361 cycles
ATB, AFT TAKE-OFF GEAR DISAGREE EICAS MESSAGE COMPLETED CHECKLIST OK TO INSTALL ACTUATOR AND I.A.W. AMM 32-32-15-404-006 REV. 45 STEP 3A TO STEP 3.F.(4) INSTALL L/H WING GEAR DOWNLOCK ACTUATOR CHECK OK. OPEN
Part: SUPPORT BRACKET — CRACKED (BLG WW) · airframe 22,865 hrs · 3,361 cycles
FAULT - CRACK - BRACKET, RH BLG W/W PRESSURE OPERATED SHUTOFF VALVE SUPPORT, STA 1394. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV43. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV43
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 19,096 hrs · 2,812 cycles
*SDR FILED OPEN* MAIN DECK ENTRYWAY EMERGENCY LIGHT INOP DEFERRAL OF MAIN DECK ENTRYWAY EMERGENCY LIGHT MEL 33-51-1-1A DMP - NONE
Part: LIGHT — INOPERATIVE (UNKNOWN) · airframe 19,312 hrs · 2,842 cycles
*SUPPLEMENTAL SDR* MAIN DECK ENTRYWAY EMERGENCY LIGHT INOP REPLACED MAIN DECK ENTRYWAY LAMP PER AMM TASK 33-51-07-960-801 AND OPS NML
2022
Part: DOOR — BROKEN · airframe 15,538 hrs · 2,276 cycles
FOUND DR INTERNEL MCHSM A ROD ASSY BRKN FORWORD ONE AND MAKE A HOLE ON OUTER SKIN. MN DECK CRGO DR HOOK OPEN & CLSD SEQ SWTCHS ADJ PER MM 52-32-00-820-801
2021
Part: FAN — OVERHEATED (E/E COOLING) · airframe 13,032 hrs · 1,871 cycles
DESCENDING THRU 7000 FT ENTIRE COCKPIT REC'D A BURNING ELEC SMELL. NO SMOKE. DISSAPATED BY LANDING. T/S PERF, FOUND AT PRES LEG FAULTS E/E CLNG SUP FAN STATUS WITH MSG 21409. IAW FIM 21-58-00-810-808 REV 2021/09/15. 03:01. E/E COOLING SUPPLY FAN HOT AND MAKES BAD NOISES. NO MAT AT CGN. NEW COOLING SUPPLY FAN AND ON CMC GROUND TEST PASS PER AMM 21-58-01/401.
Part: UNKNOWN — ODOR (CABIN) · airframe 12,941 hrs · 1,854 cycles
SMELL OF BURNT RUBBER AFTER FLAP RET / EXTENSION.OBSERVED THAT THE FLAPS WOULD ONLY EXTEND IN ALT MODE WITH A CTR FLAP CNTRL MSG. R/R CTR FLAP CTRL MOD IAW AMM 27-51-10-401, AND INSPECTED FLT DK PEDESTAL AREA, E&E RACKS & C/O EQUIP COOLING SYS CHK'S IAW AMM 21-5-00 ALL SATIS, UNABLE TO REPRODUCE SMELL AFTER
Part: STATUS MESSAGE — FALSE ACTIVATION (OVERRIDE VALVE) · airframe 12,580 hrs · 1,788 cycles
INSPECTION TYPE:N/ASMOKE/OVRD VLV STS MSG APPEARED IN CRUISEACCOMPLISHED GROUND TEST PER FIM 21-58-00-810-805 NO FAULTS NOTED OK TO CONTINUE
Part: COOLING FAN — ODOR (COCKPIT) · airframe 10,648 hrs · 1,504 cycles
INSPECTION TYPE:N/ASTATUS MSG EE CLNG SUP FAN FAIL DURING CLIMB. NOTICABLE ELEC BURNING ODOR NOTICED IN COCKPITMSG E/E COOLING SUPPLY FAN FAIL OF CMC NOTED. ODOR CONFIRMED FROM MEC COMPARTMENT. FOUND C/C C03145 EQUIP COOLING SUPPLY FAN PWR POP OUT. OBSERVED STRANGE NOISE OF E/E COOLING SUPPLY FAN. ABNORMAL FUNCTION. E/E COOLING SUPPLY FAN REPLACED IAW AMM 21-58-01 P401 REV 34A.01. EQUIPMENT COOLING CMC GROUN
2020
Part: SWITCH — FAILED (DOOR) · airframe 9,216 hrs · 1,299 cycles
INSPECTION TYPE: N/A ALERT (INT) DOOR F/D OVERHEAD EICAS MESSAGE DISPLAYED TECH RECOMMENDS. R & R S2312 SW WAN 3189233. REMOVED AND REPLACED OVERHEAD HATCH DOOR WARNING SWITCH S2312, PER AMM 52-71-01. OPERATIONS CHECK GOOD.
Part: ESCAPE HATCH — WARNING MESSAGE (COCKPIT) · airframe 8,889 hrs · 1,258 cycles
INSPECTION TYPE: NA DOOR F/O OVERHEAD EICAS MESSAGE CAME ON ON LANDING ROLL RIG OPERATIONS CHECK OVERHEAD HATCH. OPERATIONS CHECKED NORMAL, PER AMM 582-21-00.
Part: PANEL — DISCOLORED (NR 3 PYLON) · airframe 8,294 hrs · 1,174 cycles
INSPECTION TYPE:C1, DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 313U8740-1) OF PYLON #3.REPAIR IAW SRID: 4-4850528193 AND EO B747-5450-77515-A.
Part: PANEL — DISCOLORED (NR 4 PYLON) · airframe 8,294 hrs · 1,174 cycles
INSPECTION TYPE:C1. DISCOLORATION AND CORROSION ON THE INBD LWR PANEL (P/N: 323U8740-1) OF PYLON #4.REPAIR IAW SRID: 4-4850555663 AND EO B747-5450-77514-A.
2019
Part: SWITCH — FAILED (OVERHEAD HATCH) · airframe 1,712 hrs · 248 cycles
DOOR F/D OVERHEAT MESSAGE OUT OF 1000 FEET. RAN CHECKLIST. A/C RELEASED FOR SERVICE PER MEL 52-71-1-1, M661115, CREW OVHD DOOR IND INOP. REPLACED SWITCH FOR CREW OVERHEAD HATCH -DOOR INDICATION IAW SWPM 20-30-12 REV 69.01. FUNCTIONAL TEST PERFORMED, FOUND SATIS. DMI M661115 CLOSED, DMP REVERSED, PLACARD REMOVED.