N575FE
Registered owner: FEDERAL EXPRESS CORP, TN (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.
416 reports on file, 2005-06-29 – 2023-03-27.
Part: PRESSURE SWITCH — UNKNOWN (ZONE 200) · airframe 93,856 hrs · 21,701 cycles
L1 DOOR SLIDE PRESS TO TEST LIGHT IS INOP. AIRCRAFT REPOSITIONED TO LONG TERM STORAGE.
Earlier reports · 2005–2022 · 415 reports
2022
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08 AND FOUND LOWER FACE EXCEED LIMIT BASE THE DIFFERENCE BETWEEN DRAWING AND CMM MAXIMUM REWORK LIMIT FOR BARREL NUT HOLE.REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA #1- 5750-T0366641 PART 1 STEP 2 AND STEP 2.E.TITLE: WINGS-FLIGHT SURFACES - EO 1-5750- 7- 5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750- T0366641 PART 1 FOR DETAILS.
Part: SUPPORT — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2R REPAIR 5 FIGURE 201. REPAIR ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM57-50-02-2R FIGURE 201 AND EA#1-5750-T0366907 P1 STEP 1A. TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR.REPAIR ECCENTRIC BUSHING INSTALLED AS PER AMM27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N01073 ATTACHED EA#1-5750-T0366907 PART 1 FOR WORK DETAILS.
Part: SUPPORT — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2R REPAIR 5 FIGURE 201. REPAIR ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM57-50-02-2R FIGURE 201 AND EA#1-5750-T0366907 P1 STEP 1A. TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR.REPAIR ECCENTRIC BUSHING INSTALLED AS PER AMM27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N01073 ATTACHED EA#1-5750- T0366907 PART 1 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM57-44-08. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA#1-5750-T0306870 C PART 2 STEP 1. TITLE: WINGS- FLIGHT SURFACES-RH WING-OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM : N00221 ATTACHED EA#1-5750- T0306870 C PART 1 STEP 1.
Part: SUPPORT — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2R REPAIR 5 FIGURE 201. REPAIR ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM 57-50-02-2R FIGURE 201 AND EA#1-5750-T0366907 P1 STEP 1A. TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REPAIR BUSHING INSTALLED AS PER AMM 27-50-32-4.
Part: SUPPORT — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM57-50- 02-2R REPAIR 5 FIGURE 201. REPAIR ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER MD-11 SRM57-50-02-2R FIGURE 201 AND EA#1-5750-T0366907 P1 STEP 1A. TITLE: WINGS - FLIGHT SURFACES - LH WING - OUTBD FLAP VANE ASSY- TRACK SUPPORT FITTING SLOT HOLES CORROSION REPAIR.REPAIR ECCENTRIC BUSHING INSTALLED AS PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N01073 ATTACHED EA#1-5750-T0366907 PART 1 FOR WORK DETAILS.
Part: SUPPORT — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-04. AND EA .#1- 5750-T0366833 P1 STEP 2A AND STEP 2. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7-5002-LH WING -OUTBD FLAP -OUTBD HINGE (FLAP SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
Part: SUPPORT — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-04. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-52-04 AND EA#1- 5750-T0366395 P1 STEP 1. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES-RH OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
Part: SKIN — NONE (500) · airframe 91,177 hrs · 21,044 cycles
LEFT HAND WING NUMBER 2 SLAT LOWER AFT EDGE ADJACENT TO NUMBER 3 SLAT TRACK COVER FOUND CHAFFED , BETWEEN STATION XIS 247.028 AND STATION XIS 253.212 . LEFT HAND WING NUMBER 2 SLAT LOWER AFT EDGE ADJACENT TO NUMBER 3 SLAT TRACK COVER CHAFFED MARK BETWEEN STATION XIS 247.028 AND STATION XIS 253.212 REPAIR CARRIED OUT AS PER EA # 1-5750-T0366811. P1 . TITLE : WINGS - FLIGHT SURFACES - LEFT HAND WING NUMBER 2 SLAT ASSEMBLY - CHAFE DAMAGE FOUND ON OUTER SKIN , INNER SURFACE BETWEEN STATION XIS 247.028 AND STATION XIS 253.212 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SKIN — DAMAGED (800) · airframe 91,177 hrs · 21,044 cycles
CABIN - LEFT 1 ENTRY DOOR FORWARD UPPER CORNER EXTERIOR SKIN FOUND EDGE DAMAGED. . CABIN - LEFT 1 ENTRY DOOR FORWARD UPPER CONER EXTERIOR SKIN DAMAGED EDGE , REPAIR CARRIED OUT AS PER FEDEX EA # 1-5210-T0366880 P1 . TITLE : DOORS - PASSENGER / CREW - L1 PASSENGER ENTRY DOOR - REPAIR ON OUTER SKIN AT UPPER FORWARD CORNER - RSC TRACKING . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#1-5750-T0366641 PART1 STEP 2 AND STEP 2C. TITLE: WINGS- FLIGHT SURFACES - EO 1-5750- 7-5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750-T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08 . OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM 57-44-08 AND EA#1-5750-T0306870 C PART 2 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING -OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#1-5750-T0366641 PART1 STEP 2 AND STEP 2D. TITLE: WINGS-FLIGHT SURFACES - EO 1-5750- 7-5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750-T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#1- 5750-T0366641 PART1 STEP 2 AND STEP 2.A. TITLE: WINGS-FLIGHT SURFACES - EO 1-5750- 7- 5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750- T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11CMM57-44-08. REPAIR CARRIED OUT AS PER EA.#1-5750-T0366641 PART1 STEP 2 AND STEP 2.E.FIGURE 2. TITLE: WINGS-FLIGHT SURFACES - EO 1-5750- 7-5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750-T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA#1- 5750-T0306870 C PART 2 STEP 1. TITLE: WINGS- FLIGHT SURFACES-RH WING-OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM # N00221 ATTACHED EA#1-5750-T0306870 C PART 1 STEP 1.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE(#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#1-5750-T0366641 PART1 STEP 2 AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES - EO 1-5750- 7-5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750-T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-08. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-08 AND EA#1-5750-T0306870 C PART 2 STEP 1. TITLE: WINGS- FLIGHT SURFACES-RH WING- OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM # N00221 ATTACHED EA#1-5750-T0306870 C PART 1 STEP 1.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#1-5750-T0366641 PART1 STEP 2 AND STEP 2B. TITLE: WINGS-FLIGHT SURFACES - EO 1-5750- 7-5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750-T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA .#1-5750-T0366641 PART1 STEP 2 AND STEP 2D. TITLE: WINGS-FLIGHT SURFACES-EO 1-5750-7- 5002-LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA#1-5750-T0306870 C PART 2 STEP 1. TITLE: WINGS- FLIGHT SURFACES-RH WING-OUTBD FLAP INBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM # N00221 ATTACHED EA#1-5750-T0306870 C PART 2 STEP 1.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. REPAIR SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-08 AND EA.#1-5750-T0366641 PART1 STEP 2 AND STEP 2C. TITLE: WINGS- FLIGHT SURFACES - EO 1-5750- 7-5002 - LH WING OUTBD FLAP INBD FWD HINGE (WING SIDE)- CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100. REFER TO SNRM #N00143 ATTACHED EA#1-5750-T0366641 PART 1 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE(#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306917 B P3 STEP 1E AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306917 B P3 STEP 1D AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750-T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE(#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING-OUTBD FLAP OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT INBOARD LUG HOLE BORE(#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306918 B PART 3 STEP STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750- T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. REPAIR EVALUATED AND FOUND ACCEPTED AS PER EA#1-5750-T0306918 B PART 3 STEP 1 FIGURE 4. TITLE: WINGS- FLIGHT SURFACES- RH WING-OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306917 B P3 STEP 1A AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750- T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306917 B P3 STEP 1E AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750-T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD LUG HOLE BORE(#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306918 B P3 STEP STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306917 B P3 STEP 1B AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO 1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750- T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306917 B P3 STEP 1F AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO1- 5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750- T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE(#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE(#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44- 09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44- 09 AND EA#1-5750-T0306917 B P3 STEP 1D AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO 1- 5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750- T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD HOLE BORE(#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306917 B P3 STEP 1C AND STEP 1. TITLE: WINGS- FLIGHT SURFACES- EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1- 5750-T0306917 B PART 3 FOR WORK DETAILS
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT INBOARD HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57- 44-09 AND EA#1-5750-T0306917 B P3 STEP 1C AND STEP 1. TITLE: WINGS- FLIGHT SURFACES- EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1- 5750-T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING- OUTBD FLAP OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00161 ATTACHED EA#1-5750-T0306918 B PART 3 FOR DETAILS.
Part: BRACKET — CORRODED (ZONE 600) · airframe 91,177 hrs · 21,044 cycles
RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE(#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306918 B PART 3 STEP 1. TITLE: WINGS- FLIGHT SURFACES- RH WING-OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306917 B P3 STEP 1A AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750-T0306917 B PART 3 FOR WORK DETAILS.
Part: BRACKET — CORRODED (ZONE 500) · airframe 91,177 hrs · 21,044 cycles
LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING -WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-09 AND EA#1-5750-T0306917 B P3 STEP 1B AND STEP 1. TITLE: WINGS- FLIGHT SURFACES-EO1-5750-7-5002- LH WING- OUTBD FLAP-OUTBD HINGE (WING SIDE)-CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.REFER TO SNRM #N00098 ATTACHED EA#1-5750-T0306917 B PART 3 FOR WORK DETAILS.
Part: TRACK — DAMAGED (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - LEFT HAND STATION 5-110 X = 8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN - LEFT HAND STATION 5-110 X = 8.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 5-83 TO EXISTING SPLICE STATION 5-123 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FORMER — CRACKED (600) · airframe 91,177 hrs · 21,044 cycles
RIGHT HAND WING OUTBOARD LEADING EDGE COMPOARTMENT AT APPROXIMATELY STATION XOS 559 01 EACH FORMER FOUND CRACK . RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 559 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG . FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 1162 REVISION 'S' . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (500) · airframe 91,177 hrs · 21,044 cycles
LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 754 TO 759 BEADED DOUBLER FOUND CRACK . LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT STATION XOS 754 TO 759 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: DOUBLER — CRACKED (600) · airframe 91,177 hrs · 21,044 cycles
RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 758 TO 763 BEADED DOUBLER FOUND CRACK . RIGHT HAND WING OUTBOARD LEADING EDGE CPMPARTMENT AT APPROXIMATELY STATION XOS 758 TO 763 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER 57-40-02-2R REPAIR 15 FIGURE 203 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: TRACK — DAMAGED (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - RIGHT HAND STATION 1545 X = -8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN RIGHT STATION 1545 X = -8.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1571 TO EXISTING SPLICE STATION 1531 X = -8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: TRACK — DAMAGED (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - LEFT HAND STATION 1545 X = 8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN LEFT HAND STATION 1545 X = 8.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1571 TO EXISTING SPLICE STATION 1531 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: TRACK — DAMAGED (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - RIGHT HAND STATION 5-10 X = -8.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN RIGHT HAND STATION 5-10 X = -8.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 5-43 TO EXISTING SPLICE STATION 5-0 X = -8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: FRAME — NONE (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - LEFT HAND STATION 535 LONGERON 24 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING AS MARKED. CABIN LEFT HAND STATION 535 LONGERON 24 LEFT FRAME REPAIR CARRIED OUT AS PER SRM 53-20-07-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (BS 790) · corrosion level 2 · airframe 91,177 hrs · 21,044 cycles
CABIN - LEFT HAND STATION 790 X = 8.5 SEAT TRACK FOUND CORROSION . CABIN LEFT HAND STATION 790 X = 8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 745 TO STATION 799 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: TRACK — DAMAGED (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - RIGHT HAND STATION 5-5 X = - 27.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN RIGHT HAND STATION 5-5 X = -27.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 5-43 TO EXISTING SPLICE STATION 5-0 X = -27.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: TRACK — DAMAGED (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - RIGHT HAND SEAT TRACK STATION 5-10 X = -47.5 SEAT TRACK CROWN FOUND DAMAGED . CABIN RIGHT HAND STATION 5-10 X = -47.5 DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES . STATION 5 - 0 TO STATION 5-43 X = -47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: FRAME — NONE (200) · airframe 91,177 hrs · 21,044 cycles
CABIN - LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR OUTER ANGLE FOUND CHAFFING AS MARK. CABIN LEFT HAND STATION 535 LONGERON 19 LEFT FRAME REPAIR CARRIED OUT AS PER SRM 53-20-07-2R REPAIR 1 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
2020
Part: ENGINE — FAILED (NR 3) · airframe 88,374 hrs · 20,169 cycles
PASSING THROUGH APPROX 1000 FEET DURING INITIAL CLIMB OUT AIRCRAFT BEGAN TO LURCH ACCOMPANIED BY A LOUD BANGING NOISE. THIS A/C WAS PREVIOUSLY WRITTEN UP AFTER A REJECTED T/O DUE TO THE NR 3 ENGINE COMPRESSOR STALLING. THE CREW INITIATED A SHUTDOWN OF THE NR 3 ENGINE WITH THIS IN MIND. THERE WERE NO INSTRUMENT INDICATIONS OF ENGINE DAMAGE EXCEPT THE NR 1 ENGINE EVM THAT WAS MEL'ED. THE CONTROL TOWER REPORTED "SPARKS" COMING FROM THE NR 1 ENGINE. PER SERVICE ENGINEERING WITH METAL FOUND IN TAILPIPE NR 1 ENGINE HAS BEEN APPROVED FOR REMOVAL. W/C: 71T0901-GE,7110000-00-96, 79T0901, 7110000-10-99, 29T0301, 7110000-00-94. COMPLETED ENGINE 1 INSTALL & OPERATIONS CHECKS.
Part: GUIDE — DAMAGED (MLG) · airframe 88,281 hrs · 20,145 cycles
ON DEPARTURE AT GEAR RETRACTION, RIGHT MAIN INDICATED UNSAFE RAN QRH, CYCLED GEAR WITH NO CHANGE. LANDED WITH ALL INDICATING SAFE, NO FUTURE PROBLEMS. WITH GEAR RETRACTED FOUND BRAKE HARNESS CATCHING ON SENSOR ARM. INDICATION SHOWING RED WITH HANDLE UP AND HYD POWER APPLIED. FOUND BROKEN CLAMP ON GEAR STRUT, REPLACED CLAMP. RETRACTED GEAR, INDICATION WAS NORMAL.
Part: LANDING GEAR — MALFUNCTIONED · airframe 88,275 hrs · 20,142 cycles
PDIS 575 32-30 9359 14NOV20 MEM OPEN. UPON GEAR RETRACTION RIGHT MAIN GEAR PRIMARY AND SECONDARY INDICATED RED UNSAFE CONDITIONS. GEAR WAS CYCLED AND QRH WAS REFERENCED. AIR TURN BACK WAS ACCOMPLISHED. DURING OPS TEST FOUND R MLG INDICATION UNSAFE HARD FAULT, ALSO FOUND GAP BETWEEN LATCH ROLLER AND HOOK AT R/H MLG BELOW LIMITS, ADDED SHIMS TO ADJUST GAP LIMITS REF MD-11 AMM 32-34-05-5, OPS CHECK GOOD.
Part: LANDING GEAR — MALFUNCTIONED (RIGHT) · airframe 88,275 hrs · 20,142 cycles
PDIS 575 32-30 9359 14NOV20 MEM OPEN. UPON GEAR RETRACTION RIGHT MAIN GEAR PRIMARY AND SECONDARY INDICATED RED UNSAFE CONDITIONS. GEAR WAS CYCLED AND QRH WAS REFERENCED. AIR TURN BACK WAS ACCOMPLISHED. DURING OPS TEST FOUND R MLG INDICATION UNSAFE HARD FAULT, ALSO FOUND GAP BETWEEN LATCH ROLLER AND HOOK AT R/H MLG BELOW LIMITS, ADDED SHIMS TO ADJUST GAP LIMITS REF MD-11 AMM 32-34-05-5, OPS CHECK GOOD.
Part: WIRE HARNESS — DEFECTIVE (FIRE WARNING) · airframe 86,981 hrs · 19,806 cycles
DURING CLIMB OUT AT APPROXIMATELY 16,000 FT, NR 1 FIRE LIGHT AND ALERT ILLUMINATED, WENT OUT AFTER 30-40 SECONDS, SEEMS TO HAVE GONE OUT AFTER THROTTLES CAME BACK DURING LEVEL OFF. REMOVED AND REPLACED HARNESS FROM TB2 TO DH5 LUG A IAW AMM 26-11-03-4-1. DUE TO REPLACEMENT OF THE HARNESS FROM TB2 TO DH5 REQUIRING COMPLETE REMOVAL OF THE DH5 RESPONDER.
Part: TIRE — FAILED (NR 10) · airframe 86,627 hrs · 19,726 cycles
DURING LANDING ROOLOUT, TIRE FAILURE ALERT. #10 TIRE SHOWS 0 PSI. #10 BLOWN ON LANDING. NO OTHER DAMAGE NOTED. REMOVED AND REPLACED #10 TIRE AND #9 TIRE IAW AMM 32-41-01-4. OK FOR SERVICE.
Part: TIRE — FAILED (NR 10) · airframe 86,627 hrs · 19,726 cycles
DURING LANDING ROOLOUT, TIRE FAILURE ALERT. #10 TIRE SHOWS 0 PSI. #10 BLOWN ON LANDING. NO OTHER DAMAGE NOTED. REMOVED AND REPLACED #10 TIRE AND #9 TIRE IAW AMM 32-41-01-4. OK FOR SERVICE.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-07 AND EA # 1-5750-T0338380 A PART 3 STEP 1 AND STEP 3. TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FORWARD HINGE BRACKET ASSEMBLY- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 07 AND EA # 1-5750-T0338380 A PART 3 STEP 1 AND STEP 3. TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FORWARD HINGE BRACKET ASSEMBLY- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 07 AND EA # 1-5750-T0338379 A PART 3 STEP 1 AND STEP 3. TITLE: WINGS- FLIGHT SURFACES- LH WING INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) REPAIR PSE 57.55.01.1 ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57- 44-07 AND EA # 1-5750-T0338379 A PART 3 STEP 1 AND STEP 3. TITLE: WINGS- FLIGHT SURFACES- LH WING INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) REPAIR PSE 57.55.01.1 ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: LONGERON SPLICE — CORRODED (BS 1710) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
CENTER CARGO COMPARTMENT STATION 1710 LONGERON 52 SPLICE FITTING FOUND CORRODED. CORROSION ON SPLICE FITTING AT CENTER CARGO COMPARTMENT STATION 1701 LONGERON 52, REMOVED AND REPLACED WITH NEW SPLICE FITTING AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: RIB — CRACKED (SLAT FAIRING) · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING #1 SLAT CRUISE PERFORMANCE FAIRING RIB CRACKED AT XIS 150.7474. RIGHT HAND WING #1 SLAT CRUISE PERFORMANCE FAIRING RIB AT XIS 150.7474 REPAIR CARRIED OUT AS PER EA: 1-5750-T0352236 P1. TITEL: WINGS ÿ½ FLIGHT SURFACE ÿ½ RH WING - #1 SLAT ASSY ÿ½ SLAT - TO FUSLAGE FILLER ASSY ÿ½ XIS 150.7474 CANTED RIB FOUND CRACKED AT EXISTING B/P RETAINER LOCATION. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: LONGERON — CORRODED (BS 1968) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
WASTE TANK COMPARTMENT STATION 1968 LONGERON 43 RIGHT FOUND CORRODED. CORROSION AT WASTE TANK COMPARTMENT STATION 1968 LONGERON 43 RIGHT EVALUATED FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE. REPAIR CARRIED OUT AS PER EA # 1-5310-T0352290 P1. TITLE: FUSELAGE ÿ½ MAINFRAME ÿ½ CORROSION REPAIR ON AFT FUSELAGE LONGERON 43R, BETWEEN STA 1931 AND STA 1942.REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: LONGERON — CORRODED (BS 1701) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
CENTER CARGO COMPARTMENT BILGE AREA STATION 1701 LONGERON 52 FOUND CORROSION. CORROSION AT LONGERON 52, STATION 1701 CENTER CARGO COMPARTMENT BILGE AREA REMOVED AND FOUND OUT OF LIMIT AS PER SRM 53-00-00-2R FIGURE 202. SEGMENT REPLACEMENT FABRICATED LONGERON 52 FROM STATION 1691 TO STATION 1710 AS PER DOUGLAS DRAWING AFA7762 REVISION G. REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING LEADING EDGE CAVITY AT XOS 626 ÿ½ XOS 629 BEADED DOUBLER CRACKED. LEFT HAND WING LEADING EDGE CAVITY AT XOS 626 ÿ½ XOS 629 BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING LEADING EDGE CAVITY AT XOS 629 ÿ½ XOS 633 BEADED DOUBLER CRACKED. LEFT HAND WING LEADING EDGE CAVITY AT XOS 629 ÿ½ XOS 633 BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP VANE OUTBOARD HINGE FITTING CAVITY WALL CORROSION. RIGHT HAND WING INBOARD FLAP VANE OUTBOARD HINGE FITTING CAVITY WALL CORROSION REMOVED AS PER SRM 51-21-01-0G AND MEASURE REWORKED AREA. ORIGINAL THICKNESS 0.145ÿ½, MATERIAL REMOVED 0.060ÿ½ AS PER EA: 1-5750-T0352291 P1. TITLE: WING ÿ½ FLIGHT SURFACE ÿ½ CORROSION BLENDOUT ON SIDEWALL OF RHW INBD FLAP VANE, #2 AND #3 VANE SPRT INNER BRACKETS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: VANE — CRACKED (RT WING TE FLAP) · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING INBOARD FLAP VANE OUTBOARD LEADING EDGE CRACKED AT STATION XIFH 279.360 . LEFT HAND WING INBOARD FLAP VANE , CRACKED OUTBOARD LEADING EDGE AT STATION XIFH 279.360 REPAIRED AS PER E.A. # : 1-5750-T0338537 A P2 . TITLE : WINGS - FLIGHT SURFACES - LH INBOARD FLAP VANE SKIN REPAIRS - RSC TRACKING . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100
Part: BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP VANE CENTER HINGE FITTING CAVITY WALL CORROSION. RIGHT HAND WING INBOARD FLAP VANE CENTER HINGE FITTING CAVITY WALL CORROSION REMOVED AS PER SRM 51-21-01-0G AND MEASURE REWORKED AREA, ORIGINAL THICKNESS 0.100ÿ½, MATERIAL REMOVED 0.048ÿ½ AS PER EA: 1-5750-T0352291 P1 TITLE: WING ÿ½ FLIGHT SURFACES ÿ½ CORROSION BLENDOUT ON SIDEWALL OF RHW INBD FLAP VANE, #2 AND #3 VANE SPRT INNER BRACKETS. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE # 3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 07 AND EA # 1-5750-T0338380 A PART 3 STEP 1 AND STEP 3. TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD FORWARD HINGE BRACKET ASSEMBLY- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND PIVOT HOLE SURFACE REMAINING THICKNESS IS CORRECT AS PER EA # 1-5750-T0338379 A PART 3 FIGURE 1. TITLE: WINGS- FLIGHT SURFACES- LH WING INBOARD FLAP OUTBOARD FWD HINGE (WING SIDE) REPAIR PSE 57.55.01.1 ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: ANGLE — CHAFED (BS 535) · airframe 86,102 hrs · 19,608 cycles
CABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING OUTER REPAIR ANGLE CHAFFED AT LEFT HAND STATION 535 , LONGERON 24 LEFT . CABIN - MAIN DECK CARGO COMPARTMENT AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT , CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE . EXISTING OUTER CHAFFED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — DAMAGED (BS 745) · airframe 86,102 hrs · 19,608 cycles
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 745 , X = 75.25 . CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK LEFT HAND STATION 745 X = 75.25 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 725 TO EXISTING SPLICE STA 765 X = 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: ANGLE — CHAFED (BS 535) · airframe 86,102 hrs · 19,608 cycles
CABIN - MAIN DECK CARGO COMPARTMENT EXISTING OUTER REPAIR ANGLE CHAFFED AT LEFT HAND STATION 535 , LONGERON 19 LEFT . CABIN - MAIN DECK CARGO COMPARTMENT AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT CHAFFED MARK AT EXISTING OUTER REPAIR ANGLE FOUND TO EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 205 ALLOWABLE DAMAGE . EXISTING OUTER CHAFFED REPAIR ANGLE REMOVED AS PER SRM 51-33-01-0G AND REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: SEAT TRACK — CORRODED (BS 1240) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT STATION 1240 , X = - 75.25 . CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE AT STATION 1240 , X = - 75.25 CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STATION 1269 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND EA # 1-5750-87612 F PART 5 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57508373)
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND EA # 1-5750-87612 F PART 5 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- RH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION- PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57508373)
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52- 03 AND E.A. # : 1-5750-162394 B PART 2 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57508036)
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 86,102 hrs · 19,608 cycles
LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # : 1-5750-162394 B PART 2 STEP 2A AND STEP 2B. TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD HINGE (FLAP SIDE) BRACKET CORROSION-PSE 57.55.01.2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (WRI: 57508036)
2019
Part: BUSHING — NOT REPORTED (LT MLG DOOR) · airframe 85,566 hrs · 19,454 cycles
WHEN GEAR WAS RETRACTED INITIALLY SHOWED LEFT MAIN GEAR UNSAFE ON BOTH GEAR LIGHT AND CONFIG PAGE. AFTER QRH PROCEDURES, WE THEN HAD LEFT AND RIGHT MAIN GEAR UNSAFE. DURING CRUISE .70 MACH FL340 ONLY RIGHT MAIN GEAR REMAINED UNSAFE. REPALACED LOWER TRAPEZOID FITTING BUSHING ON LH DOOR REF MD 11 MM 32-14-20-4 DID NOT BREAK INTO RIG OR MAKE ANY ADJUSTMENTS TO THE DOOOR SWUNG GEAR TIMES HAD NO FAULTS OPS CHECK GOOD .
Part: SKIN — CORRODED (FUSELAGE) · airframe 85,051 hrs · 19,306 cycles
SURFACE CORROSION FOUND AROUND FORWARD JACK PAD ATTACH POINT. REMOVED MINOR SURFACE CORROSION AND ALODINED AROUND FWD JACK PAD IAW SRM 51-21-01 & 51-21-02.
Part: SKIN — CORRODED (BS 598) · airframe 85,051 hrs · 19,306 cycles
SURFACE CORROSION FOUND AROUND FORWARD JACK PAD ATTACH POINT.
Part: ATTACH BRACKET — CRACKED (ZONE 700) · airframe 85,051 hrs · 19,306 cycles
DURING B-56 WO#75149 FOUND NLG LOCK/UNLOCK ACTUATOR CYCLINDER ATTACH BRACKET DAMAGED...PARTS ORDERED ..MSN#1980722 REMOVED AND REPLACED NLG LOCK/UNLOCK ACTUATER BRACKET REF EA 1-5340-T0348829 NOSE GEAR RETRACT BRACKET ASSY-REPAIR OF HOLE MISMATCH OF REPLACEMENT UNIT PT1,2 AND 3, DWG ACA0007-1,MD11 SRM 51-30-00. NLG STEERING RESPONSE TIME HAS BEEN COMPLIED WITH REF MD11 AMM 32-50-00-5.
Part: BRACKET — CRACKED (NLG WW) · airframe 85,051 hrs · 19,306 cycles
FOUND NLG LOCK/UNLOCK ACTUATOR CYCLINDER ATTACH BRACKET DAMAGED.
Part: BOLT — SEIZED (RT MLG DOOR) · airframe 84,536 hrs · 19,148 cycles
DID NOT RECEIVE AN UP & LOCKED INDICATION ON THE RIGHT MAIN GEAR AFTER T/O ON BOTH PRIMARY & SECONDARY DISPLAY. RAN THE CHECKLIST,CYCLED THE GEAR,GOOD DOWN AND LOCKED,NEGATIVE RIGHT MAIN UP AND LOCKED. FELT A SLIGHT VIBRATION AT 16K,230KTS WITH GEAR HANDLE UP. LANDING UNEVENTFUL. REMOVED RH MLG DOOR LINK. FOUND BOLT SIEZED INTO FLOAT BUSHING. AFTER REMOVAL CLEANED ENTIRE AREA. HAT BUSHINGS FOUND SERVICEABLE. REPLACED THE BOLT AND FLOAT BUSHING AND REINSTALLED RH MLG DOOR LINK. SPRING PRESSURE NOW PULLS DOOR UPLOCK LINK FIRMLY BACK EVERY TIME. IAW AMM 32-34-05-4. ALSO IAW TSI 32-60/7388, CHANGED RT GEAR DOOR UPLOCK SENSOR D1-80. IAW 32-61-15-4. PERFORMED GAP CHECKS OF LINK AND BRACKET ASSEMBLY IAW AMM 32-34-05-5. ALL GAP CHECKED GOOD.
Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 84,466 hrs · 19,133 cycles
PDIS 575 32-30 7353 11MAY19 MEM OPEN U LOGPAGES:2867635 RT MAIN GEAR TOOK UNUSUALLY LONG TIME TO RETRACT AFTER TAKEOFF, THEN CAME UP SO HARD IT SHOOK THE ENTIRE PLANE AND KNOCKED OFF AUTOPILOT. SHGN 11MAY19 07:54 MEM U OPENED RT GEAR DOOR REF AMM 32-34-00-2 AND PERFORMED GVI OF WHEELWELL AREA. NO OBVIOUS DEFECTS NOTED IN WHEEL WELL OR OPERATION OF DOOR. NEXT STEP OF FIM/FRM 32-30-15 IS TO TEST RETRACT TIME. COMPLETED INSTALL OF RT MAIN LANDING GEAR RETRACT ACTUATOR STARTING AND INCLUDING INCLUDING STEP 3.G.(4)D. REF AMM 32-33-20-4. PERFORMED GEAR SWING TIME CHECK IAW AMM 32-31-00-5. ALL GEAR RETRACTED IN 12 SECONDS (13 SECOND LIMIT). THE NOSE GEAR EXTENDED IN 19 SECONDS (17-22 SECOND LIMIT), CENTER GEAR EXTENDED IN 16 SECONDS (14-18 SECOND LIMIT) AND THE MAIN GEAR WERE BOTH EXTENDED IN 22 SECONDS (19-23 SECOND LIMIT). NO UNUSUAL SHAKING DETECTED. OPS CHECK GOOD. OK FOR SERVICE.
Part: SPAR — CORRODED (LT WING) · airframe 83,908 hrs · 18,989 cycles
WHILE REMOVING LOCK FASTENERS FROM UPPER WING PANEL, FOUND CORROSION ON LH WING REAR SPAR UNDER #5 SPOILER, BEHIND BRACKET (ARH 0357-3) COMPLIED WITH E.A. #1-5700-T0345190. REINSTALLED BRACKET PN ARB005-345 IAW SRM 51-33-01.
2018
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 82,546 hrs · 18,595 cycles
AFTER TAKEOFF AND DURING SLAT RETRACTION, HAD A SLAT DISAGREE WITH A ROLL TO THE RIGHT. COMPLETED FUNCTIONAL TEST OF THE RIGHT OUTBOARD SLAT RANGE OF MOVEMENT CHECKED IAW AMM 27-80-00-710-802, ALL CHECKED GOOD, OK FOR SERVICE.
Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 82,287 hrs · 18,503 cycles
EMERGENCY LIGHT WILL NOT TEST. RECYCLED THE EMERGENCY LIGHT TEST SWITCH AS PER SMP AND DID EMERGENCY LIGHT TEST AS PER AMM 33-50-00-5 SEVERAL TIMES. EMERGENCY LIGHT TEST PASSED. NIL FAULT NOTED. A/C OK FOR SERVICE.
Part: SEAT TRACK — CORRODED (BS 770) · corrosion level 2 · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK AT BS 770, RBL 75.25 FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1, AND EA 1- 5320-T0338510, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (BS 635) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK AT BS 635, LBL 27.5 FOUND CRACKED. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
DURING HFEC INSPECTION AT LT WING SLAT TRACK NR 10 CUTOUT XOS 657 FOUND ONE CRACK WITH APPROXIMATE LENGTH 0.15 INCH. THE SLAT TRACK CUTOUT WAS REPAIRED IAW SRM 57-40-02-2R, FIG 201, REPAIR 7. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: FORMER — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
LEFT WING LEADING EDGE COMPARTMENT LOWER SURFACE FORMER AT XOS 1025 FOUND CRACKED. THE FORMER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G. FABRICATED FORMER IAW DRAWING ARB2920, REVISION BB. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — CRACKED (RT WING) · airframe 81,514 hrs · 18,322 cycles
RIGHT WING, NR 15 SLAT TRACK CUTOUT, LOWER INBD CORNER SKIN, AT XOS 994 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 201, REPAIR 7. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — GOUGED (BS 1281) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK, BS 1281, LBL 47.5, FOUND THE CROWN WAS GOUGED. OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK, BS 5-11, LBL 47.5, FOUND THE CROWN GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 81,514 hrs · 18,322 cycles
RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 669, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — GOUGED (BS 1281) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK BS 1281, RBL 47.5, FOUND THE CROWN GOUGED. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — CRACKED (LT WING LE) · airframe 81,514 hrs · 18,322 cycles
LEFT WING, DROOPED LEADING EDGE, UPPER SURFACE FOUND CRACKED AT XDLE 325. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 5. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 581, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (BS 1374) · airframe 81,514 hrs · 18,322 cycles
CENTER LANDING GEAR WHEEL WELL, RT SIDE BULKHEAD, FWD CROSS DOUBLER FOUND CRACKED AT BS 1374, Z 75 TO Z 87. A DOUBLER WAS FABRICATED IAW DWG AEA0526, REV NC. REMOVED AND REPLACED IAW SRM 51-33-01-OG. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — GOUGED (BS 1281) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK, BS 1281, RBL 8.5, FOUND THE CROWN GOUGED. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 81,514 hrs · 18,322 cycles
RIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK, BS 5-11, RBL 47.5, FOUND THE CROWN GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 765, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 646, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 81,514 hrs · 18,322 cycles
MAIN DECK SEAT TRACK, BS 5-11, LBL 8.5, FOUND THE CROWN GOUGED. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 81,514 hrs · 18,322 cycles
LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 731, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
2017
Part: PITOT HEAD — CLOGGED (CAPTAIN'S) · airframe 81,166 hrs · 18,210 cycles
DURING CRUISE, RECEIVED AN AMBER NO COMPARE ON THE CAPTAIN`S PFD AND AMBER X ON EAD. NO SENSOR ALERTS AND ALTITUDES WITHIN 100 FT. NO OTHER MISCOMPARE ANNUNCIATIONS. RECEIVED AN IAS DISAGREE ON APPROACH. F/O AIRSPEED AGREED WIITH STANDBY INDICATOR. NUMERIOUS AUTOPILOT DISCONNECTS. NOTED CLOGGED CAPTAIN'S PITOT TUBE DRAIN HOLES. CLEANED IAW MM 34-11-01-2. PERFORMED CAPTAIN'S PITOT SYS LEAK CHECK IAW MM 34-11-00-2. NO LEAKS NOTED. REMOVED AND REPLACED THE CAPTAIN'S NR 1 CADC IAW MM 34-16-01-4. AFS RTS AND AUTOLAND RTS TESTS TO BOTH FCC'S NORMAL. IAW MM 22-00-00-5. RVSM AND LLM IN COMPLIANCE. OK FOR SERVICE.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 80,956 hrs · 18,156 cycles
EMER LT BAT 1 LO ALERT DISPLAYED DURING EMERGENCY LIGHTS TEST. CHARGED THE BATTIES, PERFORMED AN EMERGENCY LIGHT TEST IAW MM 33-51-01-5, OPS NORMAL, NO FAULTS FOUND.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 79,831 hrs · 17,833 cycles
PDIS 575 32-30 4634 21JUN17 IND OPEN U ON TAKE OFF OUT OF JFK, WE HAD 4 UNSAFE GEAR INDICATIONS ON THE PRIMARY AND SECONDARY INDICATORS AFTER RAISING THE GEAR HANDLE. AS PER THE QRH, WE LOWERED THE GEAR HANDLE AND HAD 4 DOWN AND LOCKED. RAISED THE GEAR HANDLE AGAIN, OBTAINED 4 UP AND LOCKED INDICATIONS ON BOTH THE PRIMARY AND SECONDARY INDICATORS. FACT 21JUN17 17:48 IND JACKED A/C IAW AMM 7-11-00-2. ACCOMPLISHED SEVERAL GEAR EXTENSIONS AND RETRACTIONS WITH NO FAULTS OR INDICATION FAULTS. LANDING GEAR CHECKS NORMAL IAW AMM 32-31-00-5. REMOVED AND REPLACED PSEU (PRECAUTIONARY) IAW AMM 31-71-01-2. ACCOMPLISHED FUNCTIONAL CHECK OF PSEU IAW AMM 31-71-01-7. PSEU CHECKS NORMAL, NO FAULTS NOTED. ACCOMPLISHED SEVERAL GEAR SWINGS IAW 32-31-00-5. ALL GEAR EXT AND RET CHECKS NORMAL. REMOVED A/C FROM JACKS TO NORMAL CONFIG IAW AMM 07-11-00-2. (SDR INFO: PSEU. MFG'R=ELDEC. PN= 8-598-03, S/N 128).
Part: CONTROL VALVE — FAILED (BRAKE SYSTEM) · airframe 79,820 hrs · 17,828 cycles
AIRCRAFT WAS ROLLING OUT FROM A PRACTICE AUTOLAND KMEM RWY 18C WIND 1907. THE TOUCHDOWN WAS SLIGHTLY LEFT OF CENTERLINE WITH A 1.4G TOUCHDOWN. THE AUTOPILOT WAS DISENGAGED AND WHILE MAKING A SMALL CORRECTION TO CENTERLINE RECIEVED A TIRE FAIL ALERT. TAXIED OFF RWY 18C AND NOTICED TIRES 2 ,5, 6 AND 9 HAD FAILED. REMOVED AND REPLACED RIGHT INTERGRATED BRAKE CONTROL VALVE IN RIGHT WHEELWELL, PREFORMED LEAK AND OPS CHECK IAW MM 32-44-00-5, BLED MAIN GEAR BREAKS IAW MM 32-43-20. ALL OPS AND LEAK CHECKS GOOD.
Part: BRAKE — DAMAGED (MLG) · airframe 79,381 hrs · 17,684 cycles
AFTER LANDING RECEIVED A BRAKE DIF TEMP LEVEL ONE MSG. TIRE FIVE AND SIX READING 197 AND 413 RESPECTIVELY. ALL OTHERS AROUND 200. LIFTED REAR OF LT U/C TRUCK IAW3 MM 07-12-00-2. UNABLE TO TURN NR 5 WHEEL BY HAND AND BRAKE FULLY WORN. NR 6 BRAKE TURNED FREELY BUT INBOARD STATOR SHOWS SIGNS OF CARBON DETERIORATION. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2609472-4B POS: 5 SRL: B3370 CPN: 3200378 SRL: B2962 NR 5 BRAKE UNIT REPLACED IAW MM 32-43-20-4. IDENTIFIED PARTS BRAKE MPN: 2609472-4B CPN: 3200378 QTY: 1 NR 5 BRAKE UNIT REPLACED IAW MM 32-43-20-4.
Part: VALVE — CRACKED (HYD SYSTEM) · airframe 78,882 hrs · 17,511 cycles
DURING CRUISE, OBSERVED A LEVEL 1 ALERT FOR HYD 2 OFF. NR 2 HYD 2.7. AFTER TAXI IN, OBSERVED LEVEL 2 ALERT FOR HYD 2 QTY LOW AND NR 2 HYD QTY 1.6. REMOVED AND REPLACED THE RT OTBD FLAP LOCK VALVE IAW MM 27-52-11-4. OPS AND LEAK CHECKED GOOD.
2016
Part: ANGLE — CRACKED (TE FLAP) · airframe 78,273 hrs · 17,321 cycles
LT INBOARD FLAP, OUTBOARD CLOSEOUT ANGLE HAS 5 INCH CRACK IN RADIUS. REFERENCE EA 1-2750-T0329158. COMPLIED WITH PART 1 OF EA 1-2750-T0329158. THIS IS A MAJOR REPAIR.
Part: SWITCH — FAILED (L1 DOOR) · airframe 77,762 hrs · 17,170 cycles
CREW ENTRY DOOR 1L EMERGENCY SLIDE CONTINUITY CIRCUIT DOES NOT TEST GOOD. R & R 1L ENTRY DOOR REMOTE PRESSURE INDICATOR ASSY SWITCH IAW AMM 25-61-04-4-0. OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (R1 DOOR) · airframe 77,252 hrs · 17,033 cycles
UPON CLOSING & ARMING R1 DOOR, NO LIGHT ON SLIDE PRESS TO TEST BUTTON, MEL 25-61-02. R1 EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-02, VERIFY & RECORD IN THE AML. EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY. CHECKED R1 SLIDE PRESS. ACFT OK TO CONTINUE. REPLACED BATTERIES IN R1 REMOTE PRESSURE INDICATOR. ALL OPS CHECKS NORMAL IAW AMM: 25-61-04-4.
Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 77,052 hrs · 16,964 cycles
DURING VECTORS FOR FINAL APPROACH, GOT SEL ELEV FEEL MAN & FLAP LIM OVRD. LEVEL 2 ALERTS. ADDITION TO LOSS OF BOTH FLT DIRECTORS, AUTO PILOT, ATS BOTH RED, SELECT FADEC ALTN, AIRSPEED 1 LOSS & ERRATIC. FOLLOWED QRH CHECKLIST PROCEDURES FOR AIRSPEED UNRELIABLE & OTHER FLT CTRL LVL 2 ISSUES & LANDED. EXTREME WX/T STORMS & RAIN IN TERMINAL AREA. NO KNOWN ICING ENCOUNTERED. FLT CONDITIONS AT TIME OF LOSS, IMC, RAIN TEMP 7 DEG, C WIND VARIABLE, ALTITUDE FL 200, SPEED 290 IN DESCENT PHASE OF FLT. CADC SWAP & FLT DIR NR 1 OFF CORRECTED CAPTAINS SIDE AS & FD. FOUND WATER IN CAPT'S PITOT LINE, PURGED CAPTS PITOT LINE & TESTED IAW MM 34-11-00-2. SYS NOW CHECKS GOOD.
Part: SKIN — CRACKED (FUSELAGE) · airframe 76,695 hrs · 16,858 cycles
FUSELAGE, REFERENCE SNRM N00892, FOUND ONE EACH FASTENER HOLE CRACKED, AT STATION 1661, LONGERON 52 AREA. CARRIED OUT REPAIR IAW EA 1-5330-T0324043 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: STRUCTURE — CORRODED (BS 1671) · airframe 76,695 hrs · 16,858 cycles
LOWER CTR CARGO, LONGERON 52 AT BS 1671, FOUND CORROSION AFTER REMOVAL OF ANTI-COLLISION LIGHT DOME NUT RETAINER PLATE. REPAIRED IAW EA 1-5310-T0323995 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 200) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK UNDER FLOOR, CTR WING TANK UPPER SURFACE, AT BS 1226, X -72 FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5730-T0323866 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING FIXED LE COMPARTMENT, INTERNAL BEADED DOUBLER FOUND CRACKED, AT XORS 532. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: TRUNNION — CRACKED (NLG) · airframe 76,695 hrs · 16,858 cycles
DURING HFEC INSPECTION ON LT NLG WW TRUNNION WEB FITTING, REPAIRED AREA AT Y=595, FOUND CRACK LENGTH APPROX 0.13 INCH. CRACKED AREA REPAIRED IAW SRM 53-10-14-2R FIG 202 REPAIR 2. INITIAL INSPECTION TO BE CARRIED OUT AT 1,500 FLIGHT CYCLES & REPETITIVE INSPECTION AT 1,500 FLIGHT CYCLES IAW SRM 53-10-14-2R TABLE 201 REQUIREMENTS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — DENTED (RT AILERON) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING INBD AILERON LOWER SKIN FOUND WITH DENT, AT APPROX XIA 312. REPAIRED IAW EA 1-5750-T0323972 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 200) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK UNDER FLOOR, CTR WING TANK UPPER SURFACE AT BS 1226, X -66, FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5730-T0323866 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SKIN — DENTED (RT AILERON) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING INBD AILERON LOWER SKIN FOUND WITH DENT AT APPROX XIA 368 - XIA 337.5 & XIA 312, WRI 27109851. REPAIRED IAW EA 1-5750-T0323972 PT 1.
Part: SLAT TRACK — CRACKED (LE SLAT) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING FIXED LE SLAT TRACK NR 12, OTBD LOWER AFT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SLAT TRACK — CRACKED (LT WING LE SLAT) · airframe 76,695 hrs · 16,858 cycles
LEFT WING FIXED LE SLAT TRACK NR 14, OTBD AFT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIG 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: RIB — CRACKED (RT WING) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING LE COMPARTMENT, SKIN SUPPORT RIB FOUND CRACKED, AT XOS 667.6. R & R WITH NEW FABRICATED RIB IAW SRM 51-31-01-0G. NEW RIB FABRICATED IAW DWG ARB2930 REV F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK FLOOR SEAT TRACK, STATION 755, X= -8 .5, FOUND CRACKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 745 - 799, X = -8.5 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK FLOOR SEAT TRACK STATION 775, , X= 75.25, FOUND CROWN DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STATION 765 - 804, X =75.25 IAW SRM 53-00-52-2R FIG 201 REPAIR 1. NEW REPAIR SEAT TRACK SEGMENT REWORKED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 76,695 hrs · 16,858 cycles
LEFT WING FIXED LE COMPARTMENT INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 532. REPAIRED IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: STRINGER — CRACKED (RT WING) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING LE COMPARTMENT, SKIN SUPPORT STRINGER FOUND CRACKED AT STATION XOS 666. CARRIED OUT REPAIR IAW SRM 57-40-03-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: RIB — CRACKED (LT WING) · airframe 76,695 hrs · 16,858 cycles
LEFT WING FIXED LE COMPARTMENT, RIB FOUND CRACKED, AT XORS 490. R & R WITH NEW FABRICATED RIB IAW SRM 51-31-01-0G. NEW RIB FABRICATED IAW DWG ARB2931 REV H. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: SEAT TRACK — CRACKED (BS 635) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK SEAT TRACK AT BS 635, X=-8.5, FOUND CRACKED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (RT WING) · airframe 76,695 hrs · 16,858 cycles
RIGHT WING LE COMPARTMENT, RIB INTERNAL DOUBLER FOUND CRACK, AT STATION XORS 562. R & R WI RIB DOUBLER IAW SRM 51-31-01-0G. NEW RIB DOUBLER FABRICATED IAW DWG RB3954 REV K. CLASSIFIED AS MAJOR IAW GMM 6-2-100..
Part: SEAT TRACK — CRACKED (BS 635) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK FLOOR SEAT TRACK AT BS 635, X= 8.5, FOUND CRACKED. REPAIRED IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: DOUBLER — CRACKED (LT WING) · airframe 76,695 hrs · 16,858 cycles
LEFT WING FIXED LE COMPARTMENT, RIB INTERNAL DOUBLER FOUND CRACK, AT XORS 801. R & R WITH NEW RIB DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: STRUCTURE — CRACKED (ZONE 200) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK WHILE CARRYING OUT GVI L3 DOOR JAMBS PSE INSPECTION AREA. FOUND L3 DOOR FWD JAMB LOWER BOX AT BS 1250.75 - 1256.75, LONGERON 26 - 27L CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: STRUCTURE — CRACKED (BS 1250-1256) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK WHILE CARRYING OUT GVI R3 DOOR JAMBS PSE INSPECTION AREA. FOUND R3 DOOR FWD JAMB LOWER BOX AT BS 1250.75 - 1256.75, LONGERON 26 - 27R CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 76,695 hrs · 16,858 cycles
MAIN DECK WHILE CARRYING OUT GVI R3 DOOR JAMBS PSE INSPECTION AREA. FOUND R3 DOOR AFT FRAME LOWER BOX AT BS 1305.25 - 1315.42, LONGERON 26 - 27R CRACKED. REPAIRED IAW EA 1-5310-T0323974 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
2015
Part: DOOR — MISSING (RT MLG) · airframe 757 hrs · 16,571 cycles
ON WALK AROUND, FOUND RT MLG STRUT DOOR MISSING. REFERENCE SDR 15-2842. THIS SDR SUBMITTED FOR PART IDENTIFICATION.
Part: DOOR — MISSING (RT MLG) · airframe 755 hrs · 16,535 cycles
ON WALK AROUND FOUND RT MLG DOOR, OUTER DOOR MISSING. WHILE INSPECTING OUTSIDE PORTION OF DOOR FOR ANY ADDITIONAL MISSING HARDWARE, DAMAGE OR NOTEWORTHY AREAS. IT WAS DETERMINED THAT THERE HAD BEEN TWO AREAS OF TIRE RUBBING, CONTACT CORRESPONDING TO THE INBD SIDEWALLS OF RT MAIN TIRES NR 3 & 7. REMOVED ATTACHED BRACKETS FOR MISSING DOOR PANEL & REPLACED MLG OUTER DOOR. CHECKED MLG OUTER DOOR FOR FAIR, ALL CHECKED NORMAL. DURING GEAR SWING FOUND RT MAIN GEAR DOOR BY PASSING. REPLACED ACTUATOR, OPERATIONS & LEAKS CHECKS GOOD. R & R THE LG SELECTOR VLV. LEAK & OPERATIONS CHECKED GOOD.
Part: DOOR — MISSING (RT MLG) · airframe 757 hrs · 16,571 cycles
ON WALK AROUND, FOUND RT MLG STRUT DOOR MISSING. REFERENCE SDR 15-2842. THIS SDR SUBMITTED FOR PART IDENTIFICATION.
Part: SNAP RING — OUT OF POSITION (LT HORIZ STAB) · airframe 755 hrs · 16,527 cycles
RETAINER SNAP RING FOR BEARING ON SMALL DRIVE CHAIN SPROCKET FOR LT HORIZONTAL STAB MOTOR COMPLETELY POPPED OUT. REPLACED SMALL DRIVE CHAIN SPROCKET FOR LT HORIZONTAL STAB MOTOR & JACK SCREW WITH NEW ASSEMBLY. PERFORMED TENSION CHECK & SECURED HARDWARE IAW AMM 27-44-02-4.
Part: SOLENOID — MALFUNCTIONED (L1 DOOR) · airframe 742 hrs · 16,120 cycles
AFTER SHUTDOWN & L1 & RI DOORS DISARMED. COULD NOT ELEC OPEN THE L1 DOOR. THE R1 DOOR OPERATED NORMALLY. FOUND L1 DOOR LOCK RELEASE SOLENOID WORKED INTERMITTENTLY. R & R LOCK RELEASE SOLENOID, PN BAN7020-505 & L1 DOOR FUNCTION WAS NORMAL IAW AMM 52-10-06-4 5. ACFT OK FOR SVC.
2014
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RT WING OTBD FLAP, INBD FWD HINGE SIDE LOAD FITTING FACE CORRODED. REWORKED AND REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306870B PART. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING FACE CORRODED. REWORKED AND REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: PIVOT ASSY — WORN (LT WING TE FLAP) · airframe 71,766 hrs · 15,364 cycles
LT WING INBD FLAP AFT FLAP SIDE OTBD HINGE PIVOT FOUND EXCEED LIMITS AFTER WORN BUSHING REMOVED. REPAIRED IAW CMM 57-52-03 REVISION 78 AND EA 1-5750- 87606C PART 4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: PIVOT ASSY — WORN (RT WING TE FLAP) · airframe 71,766 hrs · 15,364 cycles
RT WING INBD FLAP AFT, FLAP SIDE OTBD HINGE PIVOT FOUND EXCEED LIMITS AFTER WORN BUSHING REMOVED. REPAIRED IAW CMM 57-52-03 REVISION 78 AND EA 1-5750-87612B PART 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: FRAME — DENTED (BS 449) · airframe 71,766 hrs · 15,364 cycles
DAMAGED FRAME AT BS 449 BETWEEN LONGERON 36 & 38 RT. REPAIR IAW SRM 53-00-07 REPAIR 4 FIGURE 201 REVISION 55 AND EA 1-5330-T0304462D PART 3 STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: FRAME — CRACKED (BS 469) · airframe 71,766 hrs · 15,364 cycles
FOUND DAMAGED FRAME AT BS 469 BETWEEN LONGERON 36 RT & 38 RT. REPAIRED IAW SRM 53-10-07 REPAIR 1 FIGURE 201. SRM 53-00-07 REPAIR 4 FIGURE 201 REVISION 55 AND EA 1-5330-T0304462D PART 3 STEP 3. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: SKIN — DENTED (ZONE 100) · airframe 71,766 hrs · 15,364 cycles
RIGHT LOWER FUSELAGE SKIN DAMAGED. REPAIRED IAW SRM 53-00-01 REPAIR 1.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: SUPPORT BEAM — CRACKED (BS 1747) · airframe 71,766 hrs · 15,364 cycles
CENTER CARGO DOOR ACTUATOR SUPPORT BEAM FOUND CRACKED AT BS 1747. REPAIRED IAW EA 1-5310-T0306921 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: PIVOT ASSY — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP, AFT OTBD HINGE PIVOT CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-04 REVISION 78. REPAIRED IAW CMM 57-52-04 REVISION 78 AND EA 1-5750-T0306919 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: PIVOT ASSY — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP, AFT INBD HINGE PIVOT CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-04 REVISION 78. REPAIRED IAW CMM 57-52-04 REVISION 78 AND EA 1-5750-T0306920 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP, OTBD FWD HINGE SIDE LOAD FITTING CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: ACCESS PANEL — CRACKED (LT WING) · airframe 71,766 hrs · 15,364 cycles
ACCESS PANEL FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION BETWEEN XORS = 683.4 & XORS = 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: LUG — CORRODED (ZONE 500) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP OTBD FWD HINGE FWD MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE FWD MOUNT CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: LUG — CORRODED (ZONE 500) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP OTBD FWD HINGE FWD MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57- 44-09 REVISION 78. . REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306917A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE FWD MOUNT CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP OTBD FWD HINGE INBD CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR INBD LUG FACE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: LUG — CORRODED (ZONE 500) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP, OTBD FWD HINGE ACTUATOR OTBD LUG CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306917 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: LUG — CORRODED (LT WING ACTUATOR) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP OTBD FWD HINGE ACTUATOR INBD LUG CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306917 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.
Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
CENTER ACCESSORY BAY LONGERON 43R, STATIONS 6 - 90 FOUND CORRODED. REPAIR IAW SRM 53-00-05 REPAIR 1 FIGURE 202 TYPE 1 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP OTBD FWD HINGE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP OTBD FWD HINGE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. REPAIRED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306918A PART. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: LUG — CORRODED (ZONE 500) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE LOWER MOUNT CORRODED. REWORKED AND FOUND OUT OF LIMITS CMM 57-44-08 REVISION 78. . REPAIR BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP INBD FWD HINGE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306870B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR LUG CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
RIGHT WING OTBD FLAP INBD FWD HINGE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306870B PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 71,766 hrs · 15,364 cycles
LEFT WING OTBD FLAP INBD FWD HINGE ACTUATOR LUG CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08 REVISION 78. REPAIRED IAW CMM 57-44-08 REVISION 78 AND EA 1-5750-T0306869A PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 120.
Part: TIRE — LEAKING (NLG) · airframe 71,523 hrs · 15,298 cycles
TIRE PRESS LOW ALERT WITH 80 PSI ON LT NOSE TIRE. R & R BOTH NOSE TIRES IAW AMM 32-42-01-04. ACFT OK FOR SERVICE.
2013
Part: AUTOPILOT SYS — MALFUNCTIONED (NR 1) · airframe 71,081 hrs · 15,173 cycles
NR 1 AUTOPILOT ALTITUDE WANDERS FROM SELECTED ALTITUDE TO UP TO 800 FEET LOW. NR 1 AUTOPILOT DISENGAGED TWICE IN FLIGHT. ACFT TRIMMED NORMALLY. PERFORMED SUCCESSFUL AFS TESTS BOTH FCCS IAW MM 22-00-00-5 AND FOLLOWING RVSM FLOW CHART IAW AMM 34-10-00-2. PERFORMED PROCEDURE TO RETURN TO RVSM OPERATIONS FOR ALL RVSM COMPONENTS LISTED IN TABLE 1 OF SAME MM REFERENCE. ALL COMPONENTS CHECKED GOOD AND PER CHART ACFT WILL REQUIRE RVSM WAVINESS INSPECTION ITEM 34-10-9271 CREATED. AFTER REPAIR OF AVIONICS EQUIPMENT RACK, PERFORMED ONE FINAL OPS CHECK OF FCC'S. ALL SYSTEM OP CHECKED NORMAL AND NO DEFECTS NOTED. IAW AMM 22-00-00-5.
Part: FMC — INOPERATIVE (NR 1) · airframe 70,546 hrs · 15,005 cycles
AFTER TAKE OFF, CAPTAIN LOST FD ROLL BAR, FOLLOWED BY A/T DISCONNECT. BOTH INITIALLY RECOVERED, THEN AT APPROX 12,000' THE A/P AND ATS DISCONNECTED FOLLOWED BY "SEL LDG ALT MANUALLY" ALERT. THEN A FEW MOMENTS LATER, BOTH FMS UNITS WENT TO "TIMEOUT RESELECT", SAT PHONE WAS INTERMITTENT, FMS WOULD TAKE NO INPUT A/S ON PFD'S WAS SOMEWHAT ERRATIC. A FEW ITEMS (FD MAINLY) WERE RECOVERED BEFORE LANDING. R & R FMC 1 PER MM 34-63-01-4, UPDATED FMC 1 WITH LATEST VERSION F11-1310-001 IAW MM 34-63-06-3, FMC 1 RTS PER MM 34-63-01-5.
Part: BATTERY PACK — FAILED (POWER SUPPLY) · airframe 70,251 hrs · 14,916 cycles
PRE-DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS BATTERY LOW DURING TEST. R & R EMERGENCY EXIT LIGHTS POWER SUPPLY BATTERY. OPS CHECKED OK IAW AMM 33-51-01-4 & AMM 33-51-01-5.
Part: LINE — DAMAGED (HYD SYSTEM) · airframe 69,175 hrs · 14,592 cycles
AFTER T/O WITH GEAR HANDLE UP. RED LIGHT WAS ON FOR LT GEAR IN BOTH INDICATORS. CYCLED DID NOT HELP. AFTER BLOCK IN NR 1 MLG HYD LINES AND BRACKETS ON BACK SIDE OF STRUT WAS TORN OFF AND BROKEN. ALONG WITH NR 6 BRAKE TEMP SENSOR LINE. WIRE BUNDLE WAS TORN OUT FROM UNDER AFT TRUCK.
2012
Part: ENGINE — FAILED (NR 1) · airframe 67,974 hrs · 14,223 cycles
PASSING 1500 AGL ON DEPARTURE CLIMB OUT, ENGINE NR 1 COMPRESSOR STALL. N1 RPM FLUCTUATIONS +- 15 PERCENT WITH AUDIBLE POPS AND BANGS. RAN CHECKLIST FOR ENG 1 COMPRESSOR STALL. DUMPED FUEL TO MAX GROSS LAND WEIGHT. SECURED DUMP AND RETURNED TO DEPARTURE. REMOVED NR 1 ENGINE.
Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 67,262 hrs · 14,034 cycles
LT WING NR 7 SLAT UPPER SURFACE OTBD AFT CORNER MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-00-00, FIG 201, REPAIR GENERAL REV 49. EA 1-5750-160960. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — MISREPAIRED (RT WING) · airframe 67,262 hrs · 14,034 cycles
RT WING INBD AILERON L/E MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-00-00, FIG 205. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — MISREPAIRED (LWS 453) · airframe 67,262 hrs · 14,034 cycles
LT WING T/E SKIN INBD ISLAND UPPER SURFACE FWD INBD AND OTBD CORNERS MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-50-01, FIG 202. REPAIR 6, REV 49 EO E1-5100-7-5001B-PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
Part: DOUBLER — CRACKED (BULKHEAD) · airframe 67,262 hrs · 14,034 cycles
CENTER LANDING GEAR, RT KEELBEAM FORWARD BULKHEAD LOWER HOLE CUT-OUT DOUBLER CRACKED. R & R IAW SRM 51-33-01, REV 49 FABRICATED DOUBLER IAW DWG AEA0526 REV NL REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: DOUBLER — CRACKED (BULKHEAD) · airframe 67,262 hrs · 14,034 cycles
LEFT KEELBEAM FORWARD BULKHEAD LOWER HOLE CUT-OUT DOUBLER CRACKED. R & R WITH FABRICATED DOUBLER IAW SRM 51-33-01, REV 49. NEW DOUBLER FABRICATED BY MACHINING IAW DWG AEA0526 REV NC. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: LONGERON — CRACKED (ZONE 200) · airframe 67,262 hrs · 14,034 cycles
CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 5-0, LONGERON -11L. REPAIRED IAW EA 1-5310-160957. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — CRACKED (LT WING) · airframe 67,262 hrs · 14,034 cycles
LT WING - L/E LOWER SURFACE NR 15 SLAT TRACK CUTOUT INBD AND OTBD CORNERS FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 49, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: LONGERON — CRACKED (ZONE 200) · airframe 67,262 hrs · 14,034 cycles
CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 5-0, LONGERON 1L. REPAIRED IAW SRM 53-00-05, FIG 201, REV 49, LONGERON MACHINED IAW DWG AEA7476, REV A REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — CRACKED (ZONE 100) · airframe 67,262 hrs · 14,034 cycles
STA 6-100 LONGERON 48LT EXTERIOR SKIN PANEL FOUND CRACKED. REPAIRED IAW SRM 53-00-01, FIG 201 REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: LONGERON SPLICE — CRACKED (BS 1541) · airframe 67,262 hrs · 14,034 cycles
CENTER CARGO COMPARTMENT BILGE AREA AT STA.1541 LONGERON SPLICE 51R CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01, REV 49 LONGERON SPLICE MACHINED IAW DWG A5A7114, REV E, REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — MISREPAIRED (BS 313) · airframe 67,262 hrs · 14,034 cycles
SKIN BS 313, LONGERON 52 MISREPAIRED. REPAIRED CARRIED OUT IAW SRM 53-00-01, FIG 201. REPAIR 1, REV 49 EO E1-5100-7- 5001B-PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — CRACKED (ZONE 600) · airframe 67,262 hrs · 14,034 cycles
FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT THE RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 690 AND 700. REPAIRED IAW EA 1-5710-160951 PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.
Part: SKIN — CRACKED (ZONE 500) · airframe 67,262 hrs · 14,034 cycles
FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND 700. REPAIRED IAW EA 1-5710-157200 PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,262 hrs · 14,034 cycles
IMPACT DAMAGE TO LOWER CARGO DOOR AT THE FORWARD EDGE, REPAIRED IAW EA 1-5230-160323. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: TEE FITTING — CRACKED (MLG WW) · airframe 67,262 hrs · 14,034 cycles
CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT TEE FITTING FOUND CRACKED. TEE FITTING REMOVED IAW SRM 51-31-01, REV 49. NEW TEE FITTING FABRICATED IAW DWG APB7158 REV C AND INSTALLED IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.
Part: PANEL — CRACKED (VERTICAL STAB) · airframe 67,262 hrs · 14,034 cycles
LOWER VERTICAL STAB RT REAR CENTER SPAR LOWER PANEL FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49 AND DWG AJC7582 REV H. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.
Part: SUPPORT — CRACKED (L3 DOOR) · airframe 67,262 hrs · 14,034 cycles
L3 DOOR NR 7 BEAM FORWARD STOP SUPPORT FOUND CRACKED. REMOVED IAW SRM 51-31-01, REV 49 AND REPLACED IAW SRM 51-33-01 AND 51-35-01, REV 49 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 49.
Part: WIRE — BROKEN (BATTERY CHARGER) · airframe 67,115 hrs · 13,992 cycles
EMERGENCY POWER TEST FAIL. TROUBLESHOT IAW FIM 24-30-03-00 FOUND PIN K AT P1-1957 BATTERY CHARGER R7-10 BROKEN. RETERMINATED PIN K IAW SWPM 20 & WDM 24-33-01. OPS NORMAL IAW AMM SECURE PLANE BATTERY CHARGER MAINT PRAC 24-30-00-2.
2010
Part: BATTERY PACK — OUT OF POSITION (TEST LIGHT) · airframe 62,521 hrs · 12,879 cycles
TEST LIGHT ON L1 DOOR DOES NOT ILLUMINATE DURING TEST. REPOSITIONED BATTERIES IAW AMM 25-61-04-4-0. OPS WAS NORMAL. ACFT OK FOR CONTINUED SERVICE.
Part: COMPUTER — MALFUNCTIONED (NR 2) · airframe 61,710 hrs · 12,707 cycles
LIGHTING STRIKE ON DEPT OUT OF VHHH. LOST CADC 2 ACCOMPANIED BY NUMEROUS ALERTS. DUMPED 140,000 LBS OF FUEL AND RETURNED TO AN UNEVENTFVL LANDING. PERFORMED LIGHTENING STRIKE INSPECTION CHECK PER MM 05-53-01-6, NO DEFECT NOTED. REMOVED AND REPLACED NR 2 CADC PER MM 34-16-01-4. PERFORMED ADJUSTMENT TEST OK PER MM 34-16-01-5. A/C OK FOR SERVICE.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,320 hrs · 12,623 cycles
MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA. 1341 X= 8.5 FOUND WITH CORROSION. REPAIR CARRIED OUT FROM STA. 1331 TO 1371 X= 8.5 AS PER SRM 53-00-52 FIG. 201 REPAIR I REV. 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.
Part: LONGERON SPLICE — CRACKED (BS 1511-1531) · airframe 61,320 hrs · 12,623 cycles
CABIN - 1 OFF LONGERON SPLICE AT STA 1511-1531 LONGERON 15R CRACK AT TOP CORNER AREA. REMOVED AND REPLACED AS PER SRM 51-31-01 REV. 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV.110
2009
Part: ENGINE — MAKING METAL (NR 2) · airframe 57,740 hrs · 11,817 cycles
FROM CAN AT FL331, RECEIVED LVL2 "ENG 2 OIL FILTER" ALERT RAN QRH PROCEDURE, NO HELP. SHUT DOWN ENG NR 2. ALERT REMAINED FOR DURATION OF ELT. PERFORMED NR 2 ENG INSPECTION FOUND MASTER CHIP DETECTOR HEAVILY COVER BY METALLIC SILVER FLAKES, REMOVED OIL FILTER ELEMENT AND FOUND HEAVY CONTAMINATED BY METALLIC SILVER,CONSULTED WITH MOCC AND NEEDED CHANGE NR 2 ENG PER FIM79-00-03 FIG.105. REMOVED NR 2 ENG AS PER W/C 71T0002-GE NR 2 ENG REMOVAL. INSTALLED NR 2 ENG PER W/C 71T0902-GE, PERFORMED ENG RUN TEST NORMAL PER JRH.
2008
Part: DOUBLER — CHAFED (ZONE 600) · airframe 56,868 hrs · 11,615 cycles
RIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT OUT REPAIR DOUBLER FOUND CHAFED. DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME II AND INSTALLED WITH A NEW REPAIR DOUBLER AS PER EA 1-5740-122639 PART 1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30-5. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CORRODED (CENTER WING) · 11,615 cycles
MAIN DECK, UNDER FLOOR CENTER WING UPPER PANEL UPPER SURFACE FOUND CORROSION AT STATION 1229, -X97, RIGHT. REPAIR CARRIED OUT AS PER EA 1-5710-122662. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 56,868 hrs · 11,615 cycles
AFT CARGO COMPARTMENT RIGHT TUNNEL, LONGERON SPLICE FITTING CRACKED AT STATION 1861 L-38. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II WITH NEW FABRICATED LONGERON SPLICE AS PER DRAWING AFA7105. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: TRUNNION — CORRODED (ZONE 100) · airframe 56,868 hrs · 11,615 cycles
CENTER LANDING GEAR WHEEL WELL FOUND LEFT TRUNNION AFT HOLE INTERIOR SURFACE CORRODED. CORROSION REPAIRED AS PER EA NR 1-5310-122650. REPAIR BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: BEAM — CRACKED (FUSELAGE) · airframe 56,868 hrs · 11,615 cycles
CABIN LEFT DOOR NR 3 FORWARD STOP, 5TH FROM TOP, FOUND CRACK APPROXIMATELY 2 INCHES. CABIN LEFT DOOR NR 3 FORWARD CRACKED STOP (BEAM) (5TH FROM TOP) REMOVED AS PER SRM 51-31-01 VOLUME II. NEW BEAM HOLES PICKED UP AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FRAME — CHAFED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
CABIN LEFT FRAME STATION 535 BETWEEN LONGERON 23 AND 24 FOUND WITH CHAFING MARKS. REPAIR CARRIED OUT AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 600) · airframe 56,868 hrs · 11,615 cycles
07 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. REAMED AND REPAIR CARRIED OUT AS PER EA NR 1-5710-122655. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: FRAME — CHAFED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
CABIN LEFT FRAME STATION 535 BETWEEN LONGERON 19 AND 20 FOUND WITH CHAFING MARKS. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: LONGERON — CRACKED (ZONE 700) · airframe 56,868 hrs · 11,615 cycles
DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM OUT, FOUND LONGERON CRACKED. CRACKED LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING REMOVED AS PER SRM 51-31-01 VOLUME II. NEW LONGERON HOLES PICKED UP AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CRACKED (ACCESS DOOR) · airframe 56,868 hrs · 11,615 cycles
08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. EACH CRACKED FASTENER HOLES REAMED AND REPAIR CARRIED OUT AS PER EA NR 1-5710-122654. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: SEAT TRACK — CORRODED (BS 1289-1321) · airframe 56,868 hrs · 11,615 cycles
CABIN RIGHT SEAT TRACK STATION 1289 TO 1321 FOUND WITH CORROSION AS MARKED AT X = -75.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FITTING — CRACKED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES NR B AND NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOR CRACKED BOLT HOLES NR B AND NR C, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7, FOR CRACKED BOLT HOLES NR A, NR B AND NR D, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FITTING — CRACKED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATION AT HOLE NR A. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 56,868 hrs · 11,615 cycles
EMPENNAGE, RIGHT AFT FUSELAGE EXTERNAL SKIN COMMON TO BODY FAIRING NR 347DF MATING SURFACE FOUND WITH CORROSION. CORRODED SKIN AT EMPENNAGE RIGHT AFT FUSELAGE EXTERNAL SKIN COMMON TO BODY FAIRING NR 347DF. REPAIRED AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION FOUND EXCEEDED LIMITS, ORIGINAL THICKNESS: 0.100 INCH, MATERIAL REMOVED: 0.044 INCH, MATERIAL REMAIN: 0.056 INCH AS PER SRM 53-20-00 FIGURE 13 VOLUME I.
Part: STIFFENER — CRACKED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
AFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 AFT SURFACE QUANTITY 01 STIFFENER AT X = -15.250 FOUND CRACKED APPROXIMATELY 0.5 INCH. EMPENNAGE, AFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 AFT SURFACE STIFFENER AT X = -15.250 REPAIRED AS PER EA 1-5310-122645 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 56,868 hrs · 11,615 cycles
DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOR CRACKED BOLT HOLES NR A, NR B, NR C AND NR D, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FITTING — CRACKED (DOOR FRAME) · airframe 56,868 hrs · 11,615 cycles
DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATION AT HOLE NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOR CRACKED BOLT HOLE NR C, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FITTING — CRACKED (ZONE 700) · airframe 56,868 hrs · 11,615 cycles
RIGHT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING FOUND CRACKED, CRACK LENGTH APPROXIMATELY : 1 INCH. RT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 (SHEET 1 OF 6). REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRE FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,868 hrs · 11,615 cycles
CABIN SEAT TRACK STATION 959 RIGHT X =-8.5 FOUND CORRODED. CABIN: CORRODED SEAT TRACK AT STATION 959, X =-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 949 TO STATION 969, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: FITTING — CRACKED (ZONE 700) · airframe 56,868 hrs · 11,615 cycles
LEFT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING FOUND CRACKED, CRACK LENGTH APPROXIMATELY: 3/4 INCH. LEFT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS.
Part: SKIN — CHAFED (ZONE 600) · airframe 56,868 hrs · 11,615 cycles
RIGHT WING LEADING EDGE SURFACE FOUND CHAFED AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA. RT WING LEADING EDGE CHAFED SURFACE AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA REPAIR CARRIED OUT AS PER EA NO 1-5740-122639 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
2007
Part: STRUCTURE — CORRODED (ZONE 100) · airframe 51,840 hrs · 10,573 cycles
CENTER CARGO BETWEEN STA 1559 AND STA 1565 LONGERON 48R FOUND CORROSION. [07-09-07] CENTER CARGO BETWEEN STA 1559 AND STA 1565 LONGERON 48R CARRIED OUT REPAIR AS PER SRM 53- 10-00 VOLUME I FIGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
Part: BUSHING — WORN (TE FLAPS) · airframe 51,840 hrs · 10,573 cycles
LEFT WING INBOARD FLAP VANE OUTBOARD TEE FITTING BUSHING FOUND WORN. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5750-112340, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: STRUCTURE — WORN (ZONE 600) · airframe 51,840 hrs · 10,573 cycles
RIGHT WING, AFTER REMOVING NR 3 SLAT FOUND OUTBOARD MOUNTING HOLE WORN. [07-06-07] WORN OUTBOARD MOUNTING HOLE AT RIGHT HAND WING NR 3 SLAT REWORKED AND INSTALLED WITH NEW FABRICATED BUSHING AS PER FEDEX E.A. 1-5740-112339, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: LONGERON — CRACKED (ZONE 100) · airframe 51,840 hrs · 10,573 cycles
CENTER CARGO AT STA 5-123 LONGERON 47R FOUND 1EA LOCK FASTENER HOLE CRACKED. [07-09-07] REMOVED SPLICE AT STA 5-123 STR 47R AS PER SRM 51-33-01 VOLUME II AND HFEC INSPECTION CARRIED OUT PER NDT SPM 06-10-01.001 REV 13 FOUND NO CRACK EVIDENT. INSTALLED EXISTING SPLICE AT CENTER CARGO AT 5-123 STR 47R AREA AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 500) · airframe 51,840 hrs · 10,573 cycles
LEFT WING FIXED LEADING EDGE, AT 3 SLAT ANTI-ICE TELESCOPE DUCT CUT-OUT, FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. 1-5710-112343, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SKIN — CRACKED (ZONE 600) · airframe 51,840 hrs · 10,573 cycles
RIGHT WING FIXED LEADING EDGE TELESCOPE DUCT CUTOUT FOUND CRACKED. [07-06-07] CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. #1-5710-112342, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: SPAR CAP — CORRODED (ZONE 600) · corrosion level 2 · airframe 51,840 hrs · 10,573 cycles
RT WING REAR SPAR UPPER CAP FOUND WITH CORROSION AT XORS 1043 - 1045. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-111132. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: STIFFENER — CRACKED (ZONE 500) · airframe 51,840 hrs · 10,573 cycles
LT WING FIXED LEADING EDGE CAVITY AT XOS = 665, STIFFENER FOUND WITH CRACK. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-111130. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.
Part: STIFFENER — CRACKED (ZONE 500) · airframe 51,840 hrs · 10,573 cycles
LEFT WING FIXED LEADING EDGE CAVITY, AT XOS = 570, STIFFENER FOUND CRACKED. [07-06-07] REPAIRED AS PER FEDEX EA 1-5710-111129, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: RIB — CRACKED (ZONE 500) · airframe 51,840 hrs · 10,573 cycles
LT WING FIXED LEADING EDGE CAVITY AT XORS = 492 RIB STIFFENER FOUND CRACKED. [07-09-07] REMOVED CRACKED RIB STIFFENER AND FABRICATED NEW RIB STIFFENER AS PER DOUGLAS DRAWING ARB2931. INSTALLED NEW RIB STIFFENER AT LT WING FIXED LEADING EDGE CAVITY AT XORS 492. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
Part: RIB — CRACKED (ZONE 600) · airframe 51,840 hrs · 10,573 cycles
RIGHT WING FIXED LEADING EDGE RIB FOUND CRACKED AT XOS 911. [07-06-07] CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW RIB FABRICATED PER DOUGLAS DRAWING ARB2921. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
2006
Part: ADC — MALFUNCTIONED (NR 1) · airframe 48,078 hrs · 9,774 cycles
ON TAKEOFF, ALL AIRSPEED INDICATIONS LOST, RECEIVED SELECT FADEC OFF; AIRSPEED INDICATIONS CAME BACK BUT ERRONEOUS; LOST ALTITUDE INDICATION, LSAS ALL FAIL ALERT; YAW DAMP ALL FAIL. INFO NOTE: PER CREW DEBRIEF INDICATION LOSS ONLY ON CAPTAINS SIDE. FAULT REVIEW OF NR 1 ,NR 2 IRU NR 1 FCC ALL THREE COMPUTER REPORT NR 1 CADC FAIL AND NR 1 CADC FAULT BALL INDICATING YELLOW REF MM 34.16.01.04, MM 34.16.01.05. REPLACED NR 1 CADC PURGE NR 1 CADC PITOT STATIC LINES AND PERFORM LOW LEVEL LEAK CK AND NR 1 CADC CAT 3 RETURN TO SERVICE TEST OK, A/C REMAIN IN CAT 3B AND RVSM STATUS.
Part: STIFFENER — BROKEN (BS 525-595) · airframe 47,838 hrs · 9,705 cycles
DURING MODIFICATION FROM P TO F FOUND STIFFENER AT STA 525 TO STA 595, S28L TO STRINGER 36 LT BROKEN. REPLACE STIFFENER FOR DWG SP10530071 AND SRM 51-33-01 PAG 34/47.
2005
Part: FRAME — CRACKED (BS 1305) · airframe 47,838 hrs · 9,705 cycles
DURING AIRPLANE'S CONVERSION FROM P TO F: A CRACK 2.2" LONG HAS BEEN FOUND ON FRAME AT THE STA Y=1305 LT BETWEEN L=11 AND L=12. PERFORMED REPAIR IN ACCORDANCE WITH FEDEX EA N 1-5310-93785.
Part: SPAR — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING TOPSIDE FOUND CORROSION UNDER T/E PANEL JUST FWD OF O/B AILERON XORS 917.0 AND XORS 1040.0. REPAIR CARRIED OUT AS PER EA1-5710-87601.
Part: SKIN — DENTED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING LE PANEL 516EB , FOUND DENT EXTERIOR SURFACE AT STICKER. REPAIR CARRIED OUT AS PER EA1-5710-90127.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STAB BARREL NUT HOLE LT NR 27 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: FLOORBEAM — DAMAGED (CARGO BAY) · airframe 47,823 hrs · 9,702 cycles
AFT CARGO COMPARTMENT STA 1841 LOWER FRAME FLOORBEAM WEB FOUND DAMAGED, AS MARKED. REMOVED AS PER SRM 51-33-01 AND 51-35-01 VOL II. NEW WEB FABRICATED AS PER DRAWING AGA 7170 AND NEW WEB INSTALLED AS PER SRM 51-33-01 AND 51-35-01 VOL II. MINOR REPAIR AS PER GMMM 6-2-100.
Part: FLOORBEAM — DAMAGED (BS 1841) · airframe 47,823 hrs · 9,702 cycles
AFT CARGO COMPARTMENT, STA 1841 LOWER FRAME FLOORBEAM SKIN FOUND DAMAGED AS MARKED. AFT CARGO COMPARTMENT, LOWER FRAME FLOORBEAM WEB AT STA 1841, REMOVED AS PER SRM 51-33-01 AND 51-35-01 VOL II. NEW WEB FABRICATED AS PER DRAWING AGA 7170 AND NEW WEB INSTALLED AS PER SRM 51-33-01 AND 51-35-01 VOL II. MINOR REPAIR AS PER GMMM 6-2-100.
Part: RIVET — LOOSE (AILERON) · airframe 47,823 hrs · 9,702 cycles
LEFT WING TOPSIDE FIXED TRAILING EDGE ISLAND FWD AREA BETWEEN O/B FLAP AND I/B AILERON FOUND WORKING RIVETS ON FORWARD I/B CORNER. LEFT WING TOPSIDE FIXED TRAILING EDGE ISLAND FWD AREA BETWEEN O/B FLAP AND I/B AILERON I/B AND O/B CORNER SKIN TRIMMED. REPAIR FILLER AND DOUBLER FABRICATED AND MATERIAL USED AS PER DWG ARC 0583 AND SRM 51-71-00 PARAGRAPH 20B VOL II. HOT BOND REPAIR CARRIED OUT AS PER SRM 51-71-00 VOL II. MINOR REPAIR AS PER GMM 6-2-100.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1986 FRAME TO LONGERON 27L INTERSECTION, INTERCOSTAL FOUND CORRODED. WEB REMOVED, NEW WEB FABRICATED. INSTALLED AS PER SRM 51-31-01.
Part: INTERCOSTAL — CRACKED (CABIN) · airframe 47,823 hrs · 9,702 cycles
CABIN, STA 5-53 TO 5-73 LONGERON L-7 RT INTERCOSTAL FOUND CRACKED AS MARKED. INTERCOSTAL REMOVED AND FABRICATED IAW DWG A5A 7071. INSTALLED IAW SRM 51-35-01
Part: INTERCOSTAL — CRACKED (CABIN) · airframe 47,823 hrs · 9,702 cycles
CABIN, STA 1441 TO 1461 LONGERON L-9 RT INTERCOSTAL FOUND CRACKED AS MARKED. REMOVED AND FABRICATED IAW DWG AEA 7685. INSTALLED IAW SRM 51-35-01.
Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
LT HORIZONTAL STABILIZER HAS UPPER TRAILING EDGE PANEL WITH DELAMINATION, BETWEEN INBOARD AND OUTBOARD ELEVATOR ACTUATOR FORWARD ACCESS PANELS, STA XE 160. REPAIRED IAW CHP 51-62-01.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 05 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: FITTING — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
HFEC CARRIED OUT FOUND CRACKS 2 EACH AT LEFT NR 4 BANJO FITTING ON AFT LOWER HOLE 5 O'CLOCK (LOOKING I/B) APPROX .1875 INCH LONG AS MARKED. REPAIRED AS PER SRM 55-20-00.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 11 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 04 FOUND WITH CORROSION EXCEEDING LIMITS. BARREL NUT BORE REAMED TO 0.974 DIAMETER. BOTTOM BORED THRU FOUND CLEAN HOLE COND. C3 AND ACCEPTABLE PER EO 1-5510-7-5000 D1 PT1. INSP/REPAIR HORIZONTAL STAB.BARREL NUT HOLES AD 2003-22-08/SB MD11-55-023. (BUCKET BUSHING INSTALLED) MINOR REPAIR PER GMM 6-2-100.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 22 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 24 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 13 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 07 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 02 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 03 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 35 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RIGHT NR 15 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARRREL NUT HOLE RT NR 27 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LEFT NR 34 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: SKIN — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
EXTERIOR FUSELAGE SKIN HAS CORROSION AT STA 1674 LONGERON 52 BELOW ANTENNA MOUNT. EXTERIOR FUSELAGE SKIN AT STA 1674 LONGERON 52 BELOW LIGHT MOUNT INNER DOUBLER FINGER REMOVED AS PER SRM 51-35-01 VOL II. NEW INNER DOUBLER FINGER FABRICATED AS PER DRAWING AFA 3088 AND INSTALLED AS PER SRM 51-38-01 VOL II. NEW REPAIR DOUBLER AND FILLER INSTALLED AS PER SRM 53-20-00 VOL I FIG 2. MAJOR REPAIR AS PER GMM 6-2-100.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 26 FOUND WITH CORROSION EXCEEDING LIMITS. CORRODED FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 51-38-01 VOL II AND SRM 51-33-01 VOL II. MINOR REPAIR PER GMM 6-2-100.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 32 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 09 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 19 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 28 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 35 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO COMPARTMENT HAS STA 1787 RT LONGERON 45 CRACKED. REMOVED AND REPLACED AS PER DRAWING AFA7097 AND SRM 51-31-01.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 30 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 29 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 31 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RH NR 14 FOUND WITH CORROSION EXCEEDING LIMITS. REMOVED AND REPLACED WITH NEW SPLICE FITTING PER SRM 51-38-01.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 26 FOUND WITH CORROSION EXCEEDING LIMITS. CORRODED FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 51-38-01 VOL II AND SRM 51-33-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 20 FOUND WITH CORROSION EXCEEDING. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 07 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 25 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 13 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 08 FOUND WITH CORROSION EXCEEDING LIMITS. OPEN
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 36 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 28 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 30 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 14 FOUND WITH CORROSION EXCEEDING LIMITS. FITTING REMOVED AND NEW FITTING INSTALLED PER SRM 57-38-01. (CLOSED)
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 23 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 15 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 29 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 27 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED AS PER EA1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 10 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 1 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 24 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 21 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 16 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 19 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: WEB — DAMAGED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
TO PROVIDE ACCESS AT HORIZONTAL STABILIZER CUT OUT UPPER TORQUE BOX WEB FOR REPAIR OF 36L BARREL NUT HOLE. REPAIRED PER EA 1-5310-87589. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 22 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 33 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 3 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE LT NR 31 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 12 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
TO PROVIDE ACCESS AT HORIZONTAL STAB UPPER TORQUE BOX TO REPAIR HORIZONTAL STAB BARREL NUT HOLE NR 36R. REPAIRED PER EA 1-5310-87589. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 02 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 04 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE NR 36R FOUND WITH CORROSION. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 47,823 hrs · 9,702 cycles
HORIZONTAL STABILIZER BARREL NUT HOLE RT NR 06 FOUND WITH CORROSION EXCEEDING LIMITS. REPAIRED IAW EA 1-5510-87597. [CLOSED]
Part: BRACKET — CORRODED (A/C BAY) · airframe 47,823 hrs · 9,702 cycles
LT NR 1 AIR CONDITIONING BAY, LOWER LONGITUDINAL BRACKET ASSY FOUND WITH CORROSION AS MARKED. INTERCOSTAL FABRICATED AND INSTALLED AS PER DWG ACA3816 AND SRM 51-31-01 VOL 2 RESPECTIVELY.
Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, ALONG STA 1887 TO STA 2007 RBL 24 FLOOR SUPPORT STRUCTURE FOUND CORRODED. REMOVED AND REWORKED NEW FLOOR SUPPORT FROM S3932107-12400 AS PER DWG AGA 7497. NEW FLOOR SUPPORT PAINTED, PART MARKED AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN AT STA 2007 LBL 59 SUPPORT BRACKET ATTACHED TO BULKHEAD FOUND CORRODED. DISPREPANT SUPPORT BRACKET REMOVED. NEW SUPPORT BRACKET REWORKED FROM S2272071X7075T6511 AS PER DRAWING NJC6040. NEW SUPPORT PAINTED, PART MARKED AND INSTALLED AS PER SRM 51-22-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED.
Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 47,823 hrs · 9,702 cycles
RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-443. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87612.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING-O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 602-607. REPAIR CARRIED OUT AS PER CMM 57-44-08.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87610. (CLOSED)
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1887 ALONG RBL 38.5 TO RBL 53.5 FLOOR SUPPORT STRUCTURE FOUND CORRODED. SUPPORT REPLACED AS PER DWG AGA8027 AND SRM 51-31-01 VOL2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1986 ALONG LBL 1 TO LBL 19 FLOOR SUPPORT STRUCTURE FOUND CORRODED.
Part: HINGE — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING-O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 612-615.
Part: HINGE — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING-O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5750-87605.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED IAW CMM 57-44-09 PG 402-407.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1887 ALONG RBL 60 TO RBL 88 FLOORBEAM STRUCTURE FOUND CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AT STA 1821 ALONG LBL 38.5 TO LBL 65 FLOORBEAM STRUCTURE FOUND CORRODED. REMOVED AND REPLACED. NEW FLOOR SUPPORT REWORKED IAW DWG AGA 7028. NEW SUPPORT PAINTED, PART MARKED AND INSTALLED IAW SRM 51-35-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 47,823 hrs · 9,702 cycles
CABIN STA 1887 RBL 54 FLOOR SUPPORT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II. MATERIAL THK: 0.125", MATERIAL REMAINED: 0.113" AND MATERIAL REMOVED: 0.012" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 4 VOL I. REWORKED AREA PAINTED AS PER SRM 51-21-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AT STA 1964 LBL 10 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2929169X7075T6511 AS PER DRAWING AGA 7091 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AT STA 1821 ALONG LBL 10 TO LBL 25.5 FLOORBEAM STRUCTURE FOUND CORRODED. DISCREPANT FLOOR SUPPORT REMOVED, NEW FLOOR SUPPORT REWORKED FROM S2929169X7075T6511 AS PER DRAWING AGA 3814 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR AS PER GMM 6-2-100.
Part: SKIN — DENTED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT I/B FLAP UPPER SKIN BETWEEN XIFN 151.300 TO 159.300, FOUND WITH EXISTING DENTS, 3 PLACES, AS MARKED. DENT AREA TRIMMED AND REPAIR DOUBLER FABRICATED AND MATERIAL USED AS PER SRM 57-10-00 FIG 34 VOL I AND DRAWING ARC 2740. REPAIR DOUBLER INSTALLED AS PER SRM 51-35-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87605.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE, FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-407. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87608.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, ALONG STA 1887 TO 2007 RBL 19 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REMOVED AND REWORKED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN AT STA 1887 RBL 35 FLOORBEAM STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II. MATERIAL THK: 0.080" ,THK REMAINED: 0.072" AND MATERIAL REMOVED: 0.008" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 4 VOL I. REWORKED AREA PAINTED AS PER SRM 51-21-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 2003 RBL 57 FLOOR SUPPORT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AT STA 1836 ALONG LBL 10.5 TO LBL 26 FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2929348X7075T6511 AS PER DRAWING AGA 7975 AND INSTALLED AS PER SRM 51-31-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING , O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87608.
Part: HINGE — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87605.
Part: FLOORBEAM — BROKEN (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1986 RBL 61 FLOORBEAM STRUCTURE FOUND BROKEN. DISPREPANT FLOOR SUPPORT REMOVED. NEW FLOOOR SUPPORT REWORKED FROM S2929169X7075T6511 AS PER DRAWING AGA 7091 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING - I/B FLAP O/B HINGE (FLAP SIDE ), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-443. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87606.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1887 RBL 30.5 FLOOR SUPPORT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II. MATERIAL THK 0.070", MATERIAL REMAINED 0.063" AND MATERIAL REMOVED 0.007" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG 1A VOL I. REWORKED AREA PAINTED AS PER SRM 51-21-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LT WING-O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B BORE FOUND CORRODED. REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. FABRICATED BUSHING AND INSTALLED IAW EA 1-5750-87605.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1908 ALONG LBL 60 TO LBL 86.5 FLOOR SUPPORT STRUCTURE FOUND CORRODED. SUPPORT REMOVED AND REPLACED.
Part: HINGE — CORRODED (RT WING) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-407. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87609.
Part: HINGE — CORRODED (LT WING) · airframe 47,823 hrs · 9,702 cycles
LEFT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. REPAIR CARRIED OUT AS PER EA 1-5750-87605.
Part: SPLICE — DAMAGED (CTR CARGO BAY) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY RT STA 5-113, LONGERON 44 SPLICE FITTING FOUND WITH EXISTING ENLONGATED HOLE AFTER REMOVAL SPLICE FITTING. REMOVED AND REPLACED NEW SPLICE FITTING AS PER SRM 51-33-01 VOL. II. MINOR REPAIR AS GMM 6-2-100.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407. REPAIR CARRIED OUT AS PER CMM 57-44-09.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER CMM 57-44-09 P402-407 AND EA 1-5750-87592A.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87592A.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87590.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED IAW EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87590.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT ASPER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.
Part: BRACKET — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AFT CARGO BAY STA 1841 LOWER FRAME FWD FLOOR PANEL SUPPORTING BRACKET FOUND CORRODED AS MARKED. AFT CARGO COMPARTMENT, STA 1841 LOWER FRAME FWD FLOOR PANEL SUPPORTING BRACKET REMOVED AS PER SRM 51-33-01 VOL II. NEW STIFFENER FABRICATED AS PER DRAWING AGA 7170 AND NEW STIFFENER INSTALLED AS PER SRM 51-33-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WIN, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AFT CARGO BAY AT STA 1967, AFT CENTER CEILING TOP STRINGER ASSY FOUND DAMAGED AS MARKED. DAMAGED FLOOR SUPPORT REMOVED. NEW FLOOR SUPPORT REWORKED FROM S2922781- 1X2024T42 AS PER DWG ACA 7149 AND INSTALLED AS PER SRM 51-31-01 VOL.II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.
Part: HINGE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
RT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587.
Part: HINGE — CORRODED (LT WING TE FLAP) · airframe 47,823 hrs · 9,702 cycles
LT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587.
Part: HINGE — CORRODED (LT WING TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED A PER EA 1-5750-87588.
Part: HINGE — CORRODED (LT WING TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIRED AS PER CMM 20-11-02 AND EA 1-5750- 87588.
Part: HINGE — CORRODED (LT WING TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588.
Part: STRUCTURE — CORRODED (TE FLAPS) · airframe 47,823 hrs · 9,702 cycles
LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED.
Part: SKIN — DAMAGED (AILERON) · airframe 47,823 hrs · 9,702 cycles
RT WING I/B AILERON BOTTOM SURFACE HAS MULTIPLE SHARP ABRASIONS.
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1345 RBL 98 AS MARKED. REMOVED AND INSTALLED AS PER SRM 52-57-12.
Part: SKIN — CANNING (VERTICAL STAB) · airframe 47,823 hrs · 9,702 cycles
VERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BL. REPAIR DOUBLER INSTALLED IAW SRM 51-35-01. [CLOSED]
Part: SKIN — CANNING (VERTICAL STAB) · airframe 47,823 hrs · 9,702 cycles
VERTICAL STABILIZER HAS OIL CANNING ON SKIN JUST ABOVE 373BR. RIGHT I/B FLAP UPPER SKIN BETWEEN 140.6 TO 147.3, 03 EACH EXISTING DENTS SMOOTHENED OUT AND REPROTECTED AS PER SRM 51-21-01 VOL II, DEEPEST DENT IS 0.025", DIAMETER: 1/2" FOUND WITHIN LIMIT AS PER SRM 51-80-01 PAGE 1 ITEM 2E VOL II. MINOR REPAIR AS PER GMM 6-2-100.
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
OVERWING STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1352 RBL 98 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL.II AND NEW STIFFENER REPLACED PER DWG APB7242. NEW STIFFENER REWORKED PER DWG APB7242. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. [CLOSED]
Part: SUPPORT — CORRODED (LAVATORY MOUNT) · airframe 47,823 hrs · 9,702 cycles
CABIN AT STA 1834 LBL 36.25 LAVATORY MOUNTING SUPPORT STRUCTURE AT TOP FOUND CORRODED. (OPEN)
Part: STIFFENER — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1332 RBL 98 AS MARKED. CORRODED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY, RT STA 1641 AFT LONGERON 44 FOUND WITH CORROSION AS MARKED. FABRICATED AS PER DWG AFA7127 AND SPICED REPAIR AS PER SRM 53-10-00 VOL1 FIG1. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 47,823 hrs · 9,702 cycles
STA 912 RBL 8.5 SEAT TRACK BASE FOUND CORRODED. (OPEN)
Part: STIFFENER — CORRODED (OVERWING EXIT) · airframe 47,823 hrs · 9,702 cycles
CABIN OVERWING EXTERIOR STIFFENER FOR UPPER AUX TANK FOUND CORRODED AT STA 1339 RBL 98 AS MARKED. REMOVED AS PER SRM 51-31-01 VOL.II AND NEW STIFFENER INSTALLED AS PER DRAWING APB 7242.NEW STIFFENER REWORKED PER DWG 7242. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. [CLOSED]
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
FLOOR SUPPORT FOUND CRACKED AT STA 5-11 AT RBL 69 AS MARKED. CORRECTIVE ACTION: SNRM N1342: DISPREPANT FLOOR SUPPORT REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS PER DRAWING ACA 3762 AND INSTALLLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: SPLICE — CRACKED (LONGERON) · airframe 47,823 hrs · 9,702 cycles
STA 6-90 TO 1139 LONGERON SPLICE FOUND CRACKED AT L-12 RT AS MARKED. SPLICE FABRICATED AS PER DWG AFA7112 AND INSTALLED AS PER SRM 51-33-01 VOL2. [CLOSED]
Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY RT STA 1641 LONGERON SPLICE FITTING 44 , FOUND CORRODED AS MARKED. CENTER CARGO COMPARTMENT R/H STA 1641 LONGERON 44 SPLICE FITTING REMOVED AND REPLACED NEW SPLICE FITTING AS PER DRAWING AFA 7105 AND SRM 51-33-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY. RT STA 1641 LONGERON 44 , FOUND CORRODED AS MARKED. CENTER CARGO COMPT. R/H STA 1641 LONGERON 44 ,NEW LONGERON 44 FABRICATED AS PER DRAWING AFA 7779 AND NEW SPLICE REPAIRED AS PER SRM 53-10-00 VOL I AND AS PER SRM 51-32-01 VOL II. MAJOR REPAIR AS PER GMM 6-2-100.
Part: FRAME — DENTED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY AT STA 1841 RT LOWER FRAME PATCH REPAIR FOUND DENTED AS MARKED. CENTER CARGO COMPARTMENT,LOWER FRAME AT STA 1841 RH WEB REMOVED AS PER SRM 51-53-01 VOL II. NEW WEB FABRICATED AS PER DRAWING AGA 7170, NEW WEB INSTALLED AS PER SRM 51-53-01 VOL II. MINOR REPAIR AS PER GMM 6-2-100.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY RT STA 1531 LONGERON 47 FOUND WITH HAIR LINE CRACK AS MARKED. 47 REMOVED IAW SRM 51-33-01 VOL.II. NEW LONGERON FABRICATED AS PER DWG AFA 0618 AND NEW SPLICE REPAIR FABRICATED IAW SRM 53-10-00 FIG.2 VOL I. NEW LONGERON AND NEW SPLICE REPAIR INSTALLED IAW SRM 51-33-01 VOL II. MAJOR REPAIR PER GMM 6-2-100.
Part: SPLICE — CRACKED (LONGERON) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY RT STA 1531 LONGERON SPLICE 44 FOUND WITH A HAIR LINE CRACK AS MARKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AS PER SRM 51-33-01. [CLOSED]
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
BELOW FLOOR PANEL 271CF AT STA 1381 LBL 36.5 FLOOR SUPPORT STRUCTURE FOUND CRACKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS PER DRAWING ACA 3762 AND INSTALLED AS PER SRM 51-31-01 VOL II. CLASSIFIED MINOR AS PER GMM 6-2-100.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
BELOW FLOOR PANEL 271CF AT STA 1401 LBL 36.5 FLOOR SUPPORT STRUCTURE FOUND CRACKED. REMOVED AS PER SRM 51-31-01 VOL II. NEW FLOOR SUPPORT REWORKED FROM S2932222T12000 AS DRAWING ACA 3762 AND INSTALLED AS PER SRM 51-31- 01 VOL II. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY, RT STA 1531 LONGERON 45 FOUND WITH HAIR LINE CRACK AS MARKED. LONGERON REMOVED IAW SRM 51-32-01. NEW LONGERON AND SPLICE REPAIR INSTALLED IAW SRM 53-10-01. [CLOSED]
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
STA 1909 TO STA 2007 LBL 60 ALONG FLOOR SUPPORT STRUCTURE FOUND CORRODED. FLOOR SUPPORT REWORKED IAW DWG AGA7496 AND INSTALLED IAW SRM 51-31-01.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CENTER CARGO BAY, RT STA 1531 LONGERON 44 FOUND WITH HAIR LINE CRACK AS MARKED. LONGERON REMOVED IAW SRM 51-33-01. NEW LONGERON FABRICATED IAW DWG AGA 7028 & NEW LONGERON & SPLICE REPAIR INSTALLED IAW SRM 52-10-00. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
ALONG STA 1821 TO STA 1887 LBL 8.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, ALONG STA 1821 TO STA 1887 RBL 27.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
AT STATION 1964 LBL 78 SEAT TRACK CROWN, BASE AND FLANGE FOUND CORRODED. REMOVED AND REPAIRED IAW SRM 53-70-00. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 47,823 hrs · 9,702 cycles
ALONG STA 1821 TO STA 1887 RBL 8.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, AT STA 1837 RBL 98.5 SEAT TRACK BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00 AND INSTALLED AS PER SRM 51-31-01. [CLOSED]
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,823 hrs · 9,702 cycles
CABIN, ALONG STA 1821 TO STA 1887 LBL 27.75 SEAT TRACK CROWN AND BASE FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00. [CLOSED]