N606UP
Registered owner: CC & 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.
83 reports on file, 2018-03-25 – 2026-08-23.
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 34,508 hrs · 5,021 cycles
DOOR SILL LIGHTS AND OVERDOOR EMERGENCY LIGHTS INOPERATIVE. EMERGENCY LIGHT BATTERY REPLACED AND TESTED IAW AMM 33-51-04 PB201 REV.51. FOUND SATIS.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 33,195 hrs · 4,829 cycles
EMERGENCY DECLARED, SIMULTANEOUS BLEED DUCT LCR LEAK. GOT CMC 36061/36062/36063, T/S PER FIM 36-11-00-810-818/819/820, THESE WERE INTERMITTENT FAULT, ALL FOUR ENGS RUNNING NORMAL, NO CAUTION AND STATUS MSGS, NO EXISTING FAULT, ACFT OK FOR SVC.
Part: TURBINE CASE — CRACKED (NR 1 ENGINE) · airframe 33,022 hrs · 4,808 cycles
OPENED NR 1 ENG TO ACCESS FAMV, FOUND ENGINE 1 HEAVILY SOILED WITH SOOT AND HYD FLUID. SIGNS OF OVERHEATING FOUND MELTED CLAMPS OF WIRE HARNESSES. HYD CONNECTION BOX THROWS HEAT BUBBLES. CONTINUED T/S IAW FIM: G75-23-00-810-805. FOUND CRACK IN TOP FUEL MANIFOLD. IDG FEEDER CABLE OUTER ISOLATION BURNED OFF IN FAMV AREA AND CLAMPS BURNED OFF. FOUND HEAT BUBBLES AND SOOT ON INBOARD FWD ENGINE STRUT STRUCTURE, FWD OF THE FAMV DUE TO OVERHEAT CONDITION. HYD SUPPLY HOSE AT RACEWAY SERVICE DISONNECT PANEL AREA LEAKING & HEAT BUBBLES ON SPRAY BLANKET. FOUND ELECTRICAL CONNECTOR ON FAMV DAMAGED. OPENED SEPERATE FAULTS FOR FINDINGS. CONFIRMED ALL TOOLS AND PARTS REMOVED FROM AIRCRAFT.
Earlier reports · 2018–2025 · 80 reports
2025
Part: NONE — NONE (NONE) · airframe 30,484 hrs · 4,438 cycles
SDR FOR EO-85445-JIC1 STEP 137
Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 30,484 hrs · 4,438 cycles
SDR FOR EO-85445-JIC2 STEP 137
Part: SKIN — WORN (ZONE 300 ELEV) · airframe 30,498 hrs · 4,440 cycles
MAJOR REPAIR, DURING PERFORMANCE OF EO-85445-JIC 1, FOUND FASTENER HOLES (CODE G) WORN NEAR FRONT SPAR AREA AT ELEVATOR STA 244.3. I.A.W AMM 51-24-11-477-083 REV 48, REPAINT REWORK AREA.
Part: SPAR — DAMAGED (ZONE 300 ELEV) · airframe 30,484 hrs · 4,438 cycles
DURING PERFORM EO-85445-JIC 1 , FOUND FASTENER HOLES (CODE G) WORN NEAR FRONT SPAR AREA AT ELEV STA 244.3. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6" AROUND HEATED AREA I.A.W. B767 NTM PART1 51-01-01 REV: 141. RESULT: NO DEFECT FOUND.
Part: SNUBBER — OUT OF LIMITS (ZONE 800) · airframe 30,484 hrs · 4,438 cycles
FOUND MAIN ENTRY DOOR ROTARY SNUBBER PIN EXTENSION IS OUT OF LIMIT (REPLACE) OK TO WORK
Part: SNUBBER — OUT OF LIMITS (ZONE 800) · airframe 30,498 hrs · 4,440 cycles
FOUND MAIN ENTRY DOOR ROTARY SNUBBER PIN EXTENSION IS OUT OF LIMITS. IAW AMM TASK 52-11-10-000-801 REV.48 AND AMM TASK 52-11-10-400-801 REV.48 REPLACED L1 MAIN ENTRY DOOR ROTARY SNUBBER.
Part: RIB — CRACKED (ZONE 500) · airframe 30,498 hrs · 4,440 cycles
MAJOR REPAIR, CRACKED RIB, INBD SIDE OF LT WING INBD AILERON UPPER FLANGE, WBL 445. PERFORM EO-94842-REQ1 REV.1 AND EI NO.F2025A57M-1675 REV.1. 2. JOB COMPLETED.
Part: RIB — CRACKED (ZONE 500 AILERON) · airframe 30,484 hrs · 4,438 cycles
CRACKED RIB, INBD SIDE OF LT WING INBD AILERON UPPER FLANGE, WBL 445. EI NO.F2025A57M-1675 SEQUENCE A STEP 20.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACK, FWD AND AFT SIDE OF BS 1960, S11L. PERFORMED EO-94878-REQ1, REV 2, & EI F2025A53M-1842 REV 0, & EGAT WORK SHEET 50607.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S12R. PERFORMED EO-94840-REQ 1, REV 1, EI F2025A53M-1806, REV 0, AND EGAT WORK SHEET 50609.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S12L. PERFORM EO-94883-REQ 1, REV 1, EI F2025A53M-1805, REV 0, AND EGAT WORK SHEET 50605.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S10R. PERFORMED EO-94877-REQ 1, REV 1, EI F2025A53M-1804, REV 0, & EGAT WORK SHEET 50622.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
STRINGER CRACK, FWD SIDE OF STA 1140 S-18R (LEVEL2) (REPAIR). ACCOMPLISHED REPAIR I.A.W EO-94923-REQ1 REV.1 AND EGAT EI NO.F2025A53M-1822 REV.1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF BS 2360, S9L. PERFORMED EO-94716-REQ 1, REV 1, EI F2025A53M-1777, REV 0, AND EGAT WORK SHEET 50611.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACK, FWD SIDE OF BS 1960, S14L. ACCOMPLISHED REPAIR IAW UPS EO-94934-REQ 1, REV 1 AND EI F2025A53M-1722, REV 2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,518 hrs · 4,442 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF BS 2360, S10L. ACCOMPLISHED REPAIR IAW SRM 53-60-03-2R-8, REV 46, TR:53-149, EGAT WORK SHEET 50610, EO-94717-REQ 1, REV 1, AND EGAT EI F2025A53M-1778 REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S10L. PERFORMED EO-94838-REQ 1, REV 1, EI.F2025A53M-1746, REV 0, & EGAT WORK SHEET 50606.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF BS 1960, S24R. PERFORM EO-94933-REQ1, REV 1, AND EI.F2025A53M-1824, REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S11R. PERFORMED EO-94879-REQ 1, REV 1, EI F2025A53M-1843, REV 0, AND EGAT WORK SHEET 50623.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACK, FWD SIDE OF BS 2360, S7R. REPAIRED DAMAGE AREA IAW SRM 53-60-03-2R-8 REV.46/TR:53-149, EGAT WORK SHEET 50612, EO EO-94715-REQ 1, REV 1, AND EGAT EI F2025A53M-1792 REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S19R. REPAIRED DAMAGE AREA IAW EO-94836-REQ 1, REV 2, EGAT EI F2025A53M-1807, REV 0, AND EGAT WORK SHEET 50608.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 1960, S15R. PERFORMED EO-94897-REQ 1, REV 1, AND EI F2025A53M-1796, REV 1.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S36L. ACCOMPLISHED REPAIR IAW EO-94924-REQ 1, REV 1, AND EI F2025A53M-1797, REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 2387, S5L. ACCOMPLISHED REPAIR IAW UPS-94960-REQ1 REV 1, AND EGAT EI F2025A53M-1849 REV 3.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S23L. ACCOMPLISHED REPAIR IAW EO-9495-REQ 1, REV 1, AND EGAT EI F2025A53M-1727 REV.2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF STA 2180 S14R. PERFORMED EO-94947-REQ1 REV.1 AND EI F2025A53M-1832 REV.1 2. JOB COMPLETED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S14L. ACCOMPLISHED REPAIR IAW EO-94946-REQ1 REV 1 AND EGAT EI F2025A53M-1841, REV 1.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960 S45L. PERFORMED EO-94958-REQ1 REV 1 & EI F2025A53M-1853 REV 1 2.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 1960, S35L. PERFORMED EO-94941-REQ 1, REV 1, AND EI F2025A53M-1724, REV 2.
Part: STRING — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S15L. ACCOMPLISHED REPAIR IAW EO-94948-REQ 1, REV 1, AND EGAT EI.F2025A53M-1800, REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S6R, ACCOMPLISHED REPAIR IAW SRM 53-60-03-2R-3, REV.46, TR:53-154, EGAT WORK SHEET 50601, EO-94839-REQ 1, REV 1, AND EI F2025A53M-1801 REV.0 2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 2377, S6L. PERFORM EO-94929-REQ 1, REV 1, AND EI F2025A53M-1730, REV 2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S13L. ACCOMPLISHED REPAIR IAW UPS EO-94945-REQ1 REV.1 AND EGAT EI F2025A53M-1834 REV 1.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF BS 1960, S39L. PERFORMED EO-94942-REQ1 REV 1 & EI F2025A53M-1838 REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 2180, S17L. PERFORM EO-94720-REQ1 REV.1, AND EI F2025A53M-1803, REV.0, AND EGAT WORK SHEET 50598 2.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,518 hrs · 4,442 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF STA 2180 S-18L. PERFORM EO-94718-REQ1 REV.1 AND EI F2025A53M-1858 REV.0 AND EGAT WORK SHEET 50599.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 2360 S-7R. REPAIR DAMAGE AREA I.A.W SRM 53-80-03-2R-3 REV.46/TR:53-153 AND EGAT WORK SHEET 50594 AND EO-94714-REQ1 REV.1 AND EGAT EI F2025A53M-1833, REV.0. 2. JOB COMPLETED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S22L. PERFORMED EO-94932-REQ 1, REV 1, AND EI F2025A53M-1726 REV 2.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-37L. ACCOMPLISHED REPAIR IAW UPS EO-94934-REQ1 REV.1 AND EGAT EI F2025A53M-1831 REV 1 2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,518 hrs · 4,442 cycles
MAJOR REPAIR, STRINGER CRACK, AFT SIDE OF STA 2360 S-6R. PERFORM EO-94888-REQ1 REV.1 AND EI NO.F2025A53M-1751 REV.1. 2. JOB COMPLETED.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S12L. ACCOMPLISHED REPAIR IAW SRM 53-60-03-2R-3, REV 46, TR:53-154, AND EGAT WORK SHEET 50597, AND EO-94962-REQ 1, REV 1, AND EGAT EI F2025A53M-1802 REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 2180, S20R. ACCOMPLISHED REPAIR IAW UPS EO-94961-REQ1 REV 1, AND EGAT EI F2025A53M-1863, REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACK, AFT SIDE OF BS 2360 S-5R. ACCOMPLISHED REPAIR IAW UPS EO-94959-REQ 1, REV 1, AND EGAT EI F2025A53M-1846, REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 1960, S39L. PERFORMED EO-94942-REQ 1, REV 1, EI F2025A53M-1838, REV 1 AND EGAT WORK SHEET 50596.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,518 hrs · 4,442 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF STA 1960 S-38L. PERFORM EO-94837-REQ1 REV.1 AND EI F2025A53M-1799 REV.0 AND EGAT WORK SHEET 50592. 2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 2180, S21L. PERFORMED EO-94949-REQ 1, REV 1, AND EI F2025A53M-1809, REV 1.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180 S10L. PERFORM EO-94925-REQ1 REV.1 AND EI NO.F2025A53M-1857 REV.2.
Part: BATTERY — MALFUNCTIONED (ZONE 200) · airframe 30,518 hrs · 4,442 cycles
REMOVE EMERGENCY LIGHT BATTERY 3 EA FOR PREVENT BATTERY DISCHARGER. IAW AMM 33-51-04-900-803 REV.48, REPLACED EMERGENCY LIGHT BATTERY M5170. IAW AMM 33-51-04-900-803 REV.48 PERFORMED EMERGENCY LIGHT BATTERY INSTALLATION TEST, RESULT WAS SATISFACTORY.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 1740, S42L. PERFORM EO-94931-REQ1 REV.1 AND EI NO.F2025A53M-1810 REV.1 2. JOB COMPLETED.
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD AND AFT SIDE OF BS 2180, S35R. PERFORM EO-94926-REQ1 REV.1 AND EI F2025A53M-1729, REV.2 2.
Part: BATTERY PACK — NOT REPORTED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
CUSTOMER REQUEST REMOVE EMERGENCY LIGHT BATTERY 3 EA FOR SHOP TO PERFORM BATTERY FUNCTION TEST. OK TO WORK
Part: STRINGER — CRACKED (ZONE 100) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, FWD SIDE OF BS 740, S47L. ACCOMPLISHED REPAIR IAW SRM 53-20-03-2R-5 REV.46 AND EGAT WORK SHEET 50593 AND EO-94940 REQ1 REV.1 EGAT WORK SHEET 50593 AND EGAT EI F2025A53M-1917 REV.0 2.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACK, BS 2598 FWD SIDE S-1R. REPAIR DAMAGE AREA IAW SRM 53-80-03-2R-2 REV.46, TR:53-152 AND EGAT WORK SHEET 50575 AND EO-94695-REQ1 REV.1 AND EGAT EI F2025A53M-1818, REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR. STRINGER CRACKED, STA 2598 AFT SIDE S-4L. REPAIR DAMAGE AREA I.A.W SRM 53-80-03-2R-2 REV.46/RE:53-152 AND EGAT WORK SHEET 50570 AND UPS EO-94697-REQ1 REV.1 AND EGAT EI F2025A53M-1811 REV.0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598, FWD SIDE S2L REPAIRED DAMAGE AREA IAW SRM 53-80-03-2R-2 REV.46, TR:53-152 AND EGAT WORK SHEET 50571 AND EO-94696-REQ 1, REV 1, AND EGAT EI F2025A53M-1817, REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598 FWD SIDE S8L. ACCOMPLISHED REPAIR IAW SRM 53-80-03-2R-2 REV.46, TR:53-152 AND EGAT WORK SHEET 50574 AND EO-94703-REQ1 REV.1 AND EGAT EI F2025A53M-1815 REV.0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598 FWD SIDE S5L ACCOMPLISHED REPAIR IAW EO-94699-REQ 1, REV 2, AND EGAT EI F2025A53M-1844, REV 0, AND SRM 53-80-03-2R-2 REV 46, TR53-152, AND EGAT WORK SHEET 50572.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598 AFT SIDE S5L. PERFORM EO-94700-REQ 1, REV.2, AND EI F2025A53M-1845, REV 0, AND EGAT WORK SHEET 50569.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598 FWD SIDE S4R. REPAIRED DAMAGE AREA IAW SRM 53-80-03-2R-2 REV.46, TR:53-152, EGAT WORK SHEET 50576, UPS EO-94698-REQ 1, REV 1, AND GAT EI F2025A53M-1819 REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598 FWD SIDE S7R. REPAIR DAMAGE AREA IAW SRM 53-80-03-2R-2 REV.46, TR:53-152, AND EGAT WORK SHEET 50578 AND EO-94702-REQ 1, REV 1 & EI .F2025A53M-1820, REV 0.
Part: STRINGER — CRACKED (ZONE 200) · airframe 30,484 hrs · 4,438 cycles
MAJOR REPAIR, STRINGER CRACKED, BS 2598 FWD SIDE S6L. ACCOMPLISHED REPAIR AREA IAW SRM 53-80-03-2R-2 REV.46, TR:53-152, EGAT WORK SHEET 50573, UPS EO-94701-REQ 1, REV 1 AND EGAT EI F2025A53M-1816, REV 0.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 30,203 hrs · 4,395 cycles
L1 EMERGENCY LIGHT INOP.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 30,203 hrs · 4,395 cycles
L1 EMERGENCY LIGHT INOP. REALAMP L1 ENTRYWAY EMERGENCY LIGHT PER AMM 33-51-07-960-801. OPS CHECK GOOD.
Part: STRINGER — DAMAGED (ZONE 100) · airframe 29,664 hrs · 4,320 cycles
MAJOR REPAIR, STR34L DAMAGED AT STA 180.
Part: FRAME — DAMAGED (ZONE 100) · airframe 29,856 hrs · 4,347 cycles
FRAME DAMAGED @STA 180 STR34L REPAIR ACCOMPLISHED ON EO-93709-REQ1. THE SECOND STAGE DAMAGE TOLERANCE ANALYSIS (DTA) HAS BEEN COMPLETED. THE REPAIR IS TIME LIMITED PENDING THIRD STAGE DTA INSPECTION REQUIREMENTS. COMPLETE THIS STEP AND CERTIFY THE ASSOCIATED FAULT AS THE UPDATED REPAIR THRESHOLD IS TO BE TRACKED ON EO-93709-REQ2.
Part: STRINGER — DAMAGED (ZONE 100) · airframe 29,856 hrs · 4,347 cycles
**SUPPLEMENTAL SDR** STR34L DAMAGED @STA 180 ALL STEPS ACCOMPLISHED PER EO 93710 REQ1. THE SECOND STAGE DAMAGE TOLERANCE ANALYSIS (DTA) HAS BEEN COMPLETED. THE REPAIR IS TIME LIMITED PENDING THIRD STAGE DTA INSPECTION REQUIREMENTS. COMPLETE THIS STEP AND CERTIFY THE ASSOCIATED FAULT AS THE UPDATED REPAIR THRESHOLD IS TO BE TRACKED ON EO-93710-REQ2
Part: FRAME — DAMAGED (ZONE 100) · airframe 29,664 hrs · 4,320 cycles
MAJOR REPAIR. FRAME DAMAGED AT STA 180 STR34L.
Part: SKIN — DAMAGED (ZONE 100) · airframe 29,664 hrs · 4,320 cycles
MAJOR REPAIR. DAMAGE ON RH SIDE NOSE CARGO DOOR STA 200 BETWEEN STRINGER S20 AND S21 PERFORMED PROTECTIVE TREATMENT OF SKIN SURFACE IAW. SRM 51-20-01-0G-0 REV. 45 WITH PRIMER. DEFERRED DAMAGE IAW. SRM 53-00-01-1A-2 FIGURE 101 CHART AREA B FOR 50 FLIGHT CYCLES. DMI OPENED.
2023
Part: SKIN — DENTED (UNKNOWN) · airframe 23,097 hrs · 3,376 cycles
DURING WINDOW CLEANING HIGH LIFTER DAMAGED LH SIDE OF NOSE CARGO DOOR.***SM/LMX*** REVIEWED
2022
Part: PRESSURE SWITCH — INOPERATIVE (NR 3 ENG OIL PSI) · airframe 20,503 hrs · 2,996 cycles
**ATB**ENG 3 OIL SYS STATUS #3 OIL PRESSURE 26 PSI MSG NO 73300 T/S FIM 79-32-00810-817. EEC SHOP FAULT FINDING EEC 3A AND 3B FAULT CODE 423 T/S FIM 73-20-00-810-912. R/R'D NEW ENG 3 OIL PRESS SW AND ENG RUN AND LEAK CHK'D NORMAL PER AMM 79-32-01-401, 71-00-00-501 PART LOAN FROM ATLAS
2021
Part: NONE — NONE (FUSELAGE) · airframe 16,767 hrs · 2,401 cycles
INSPECTION TYPE:N/A"MD DET AFT 15" STATUS MESSAGE. LOSS OF SMOKE DETECTOR IS IN THE AFT ZONE OF THE MAIN DECK CARGO COMPARTMENT.SMOKE DETECTOR AFT 15 R/R IAW AMM 26-14-01-401 REL 37.00. P/N OFF-ON: 3301-21, S/N OFF: 3742490, S/N ON: 3889551. TEST SATIS. EFF REF IPC: 26-14-01-01A-110.
Part: WARNING MESSAGE — ILLUMINATED (LANDING GEAR) · airframe 15,094 hrs · 2,131 cycles
INSPECTION TYPE:NA**ATB - NO EMERG DECLARED - NO EMERG EQPT USED - LANDED W/OUT INCIDENT** AFTER TAKE OFF GOT " GEAR TILT" EICAS, RETURNED BACK TO SYD.HYD QTY AND PRESS CHKD SATIS, REF PREVIOUS TLP BLEEDING OF LH BLG SYS 1 HYD BLEEDING C/O AND ASSOCIATED FUSE RESET CHK IAW AMM 32-13.24.401 SATIS. GEAR TILT MESSAGE ERASED.
2020
Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 12,062 hrs · 1,693 cycles
INSPECTION TYPE: N/A. EMERGENCY DECLARED, LANDED UNEVENTFUL, CREW REPORTED HOT BRAKES & WAS TOWED FROM THE RUNWAY TO THE RAMP. AFTER START RECEIVED FLAPS PRIMARY EICAS MSG. INBOARD TE FLAPS FAILED TO EXTEND NORMALLLY. T/S PER FIM 27-51-00-810-892, FOR MAINT MSG:27776. CLEANED & RESECURED ELEC CONN ON TE FLAP DRIVE ACTUATOR. FOUND CONNECTOR DM7880 ON INBOARD TE FLAP CONTROL MODULE POSITION TRANSMITTER LOOSE, CLEANED & RESECURED SAME. OPERATED FLAPS THROUGH 3 CYCLES PER AMM 27-51-00. ALL INDICATIONS NORMAL.
Part: DOOR SEAL — PULLED (L1 DOOR) · airframe 10,664 hrs · 1,493 cycles
INSPECTION TYPE:N/ADOOR SEAL OF L1 DOOR AS DAMAGED.DOOR SEAL PULLED FRAME. REALIGNED SEAL INTO CHANNEL IAW AMM 52-09-02. SEAL NOT DAMAGED. OK FOR SERVICE.
2019
Part: PANEL — CORRODED (NR 3 PYLON) · airframe 8,122 hrs · 1,133 cycles
INSPECTION TYPE: C1, CORROSION ON THE INBD LWR PANEL (P/N: 313U8740-1) OF PYLON #3.REPAIR I.A.W. SRID: 4-4594220677 AND EO B747-5450-74170-A.
Part: PANEL — CORRODED (NR 1 PLYON) · airframe 8,122 hrs · 1,133 cycles
INSPECTION TYPE: C1, CORROSION ON THE INBD LWR PANEL (P/N: 323U8704-2) OF PYLON #1.REPAIR I.A.W. SRID: 4-4594281148 AND UPS EO B747-5450-74169-A.
2018
Part: SMOKE DETECTOR — MALFUNCTIONED (MAIN DECK) · airframe 4,441 hrs · 611 cycles
MAIN DECK DETECTOR FWD 9 STATUS MESSAGE. R & R THE MAIN DECK FWD SMOKE DETECTOR ASSY IAW AMM 26-14-00/401. OPS TESTED GOOD.
Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 4,226 hrs · 578 cycles
RECEIVED A FLAPS DRIVE MESSAGE DURING FLAP RETRACTION. INBOARD TRAILING EDGE FLAPS STUCK AT 5. INBOARD TRAILING EDGE FLAP INDICATION SHOWED 5 ALL THE WAY THROUGH LANDING WITH FLAPS 25 SELECTED. OUTBOARDS INDICATED FUCTIONED OK. TROUBLESHOT AND FOUND THE RT INBD T/E FLAP DRIVE TRANSMITTER INOPERATIVE. R & R THE FLAP DRIVE TRANSMITTER IAW AMM 27-58-01-401 AND PERFORMED AN OPS TEST. FOUND GOOD. NO RELATED MESSAGES NOTED. ACFT OK FOR SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,346 hrs · 323 cycles
INERTIA REEL LIGHT IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-09, OPS CHECKED GOOD.
Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 1,602 hrs · 225 cycles
FLIGHT DECK OVERHEAD DOOR EICAS MESSAGE DURING ROLL OUT, AFTER LANDING. CHECKED THE DOOR AREA. FOUND THE CONDITION NORMAL IAW AMM 52-21-00.