N526FE
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FedEx Corporation | Operator | on 2009-03-23 | Operator named in NTSB report |
Accident & incident history
Operated by FedEx Corporation (per NTSB report)
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.
84 reports on file, 2006-04-06 – 2007-10-24.
Part: FRAME — DENTED (ZONE 200) · airframe 35,898 hrs · 6,059 cycles
MAIN DECK CARGO COMPARTMENT, RIGHT STA 1681 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTION AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
Part: FRAME — DENTED (ZONE 200) · airframe 35,898 hrs · 6,059 cycles
MAIN DECK CARGO COMPARTMENT, RIGHT STA 1701 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
Part: FRAME — DENTED (ZONE 200) · airframe 35,898 hrs · 6,059 cycles
MAIN DECK CARGO COMPARTMENT, LEFT STA 1761 FRAME AT ABOUT STRINGER 12R AREA FOUND CRACKED. 11-07-07 MAIN DECK CARGO COMPARTMENT - LEFT HAND STA 1761 FRAME AT STRINGER 12L CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 3 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 12,000 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 8,000 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
Part: FRAME — DENTED (ZONE 200) · airframe 35,898 hrs · 6,059 cycles
MAIN DECK CARGO COMPARTMENT, RIGHT STA 1721 FRAME AT ABOUT STRINGER 12R AREA FOUND DENT. 11-05-07 CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.
Earlier reports · 2006 · 80 reports
2006
Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 31,941 hrs · 5,119 cycles
HORIZONTAL STABILIZER - INSPECT/REPAIR HORIZONTAL STABILIZER BARREL NUT HOLES. WORK ACCOMPLISHED AS PER EA 1-5510-94622 AIR WORTHINESS DIRECTIVE AD 2003-22-08- STABILIZERS - HORIZONTAL STABILIZER - EMBODIMENT OF HORIZONTAL STABILIZER S/B MD11-55-023 BARREL NUT INSPECTION REWORK.
Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 31,941 hrs · 5,119 cycles
FOUND RT WING NR 3 SLAT LE SURFACE FOUND DAMAGED. REPAIR CARRIED OUT ON RT WING NR 3 SLAT L/E SURFACE AS PER SRM 57-10-00 FIG.33 VOL.I.REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CRACKED (SLATS) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACKED FASTENER HOLE AT UPPER SURFACE OF RT WING DROOP LE SLAT. WORK CARRIED OUT AS PER E.A.1-5740-99695 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Part: SKIN — CRACKED (L/E SLAT) · airframe 31,941 hrs · 5,119 cycles
SNRM N02174: RT WING NR 7 SLAT INTERIOR SURFACE MID SECTION SUSPECT SKIN CRACK. REPAIRED AS PER SRM 57-10-00 FIG.10 VOL.I. REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100.
Part: SKIN PANEL — UNKNOWN (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
FOUND EXISTING FLUSH REPAIR FOUND AT RT FWD CORNER OF FUSELAGE CAC ACCESS DOOR CUTOUT (REF EO1-5100-7-5001). SKIN REPAIRED AS PER EA 1-5330-94701.
Part: LONGERON — CRACKED (ZONE 200) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACKED LONGERON 7L ON INTERCOSTAL AT BS 518 RT. INTERCOSTAL REPLACED AS PER SRM 51-35-01 VOL2 AND DRAWING AFA3086.
Part: REPAIR — UNKNOWN · airframe 31,941 hrs · 5,119 cycles
REPAIR REQUIRED AT UNUSED MOUNTING BASE HOLES OF ANTENNA (P/N S65- 5366-890L QTY 04 EACH) AFTER ITS REMOVAL AS PER EA1-2310-94626 STEP 18 REQUIREMENT, SNRM N01696: SKIN REPAIR AT BS 839-879 LONGERON 51L-51R AND INNER DOUBLER AT BS 859-879 LONGERON 51R-52. INSTALLED AS PER SRM 53-20-00 FIG 6 SHEET 8 VOL 1. CATB REPAIR, INITIAL INSPECTION AT 7500 CYCLES AND REPETITIVE INSPECTION AT 4750 CYCLES.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION INBOARD HINGE (WING SIDE) LOWER ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-605 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION INBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
Part: BRACKET — CRACKED (ZONE 300) · airframe 31,941 hrs · 5,119 cycles
CRACK SUPPORT BRACKET FOR TAIL FUEL TRANSFER PIPE IN EMPERAGE.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT BARREL NUT BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT INBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION OUTBOARD HINGE (WING SIDE) SIDE LINK ATTACHMENT SPOT FACE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION INBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-08 PAGE 602-607 AND EA 1-5750-94697.
Part: ATTACH FITTING — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION OUTBOARD HINGE (WING SIDE) ACTUATOR ATTACHMENT OUTBOARD BORE OF OUTBOARD FLAP IN RIGHT WING. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94688.
Part: ATTACH FITTING — DAMAGED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
LT INBOARD AILERON ATTACH LUG FOUND DAMAGED AT 2 LOCATION ON THE INBOARD SURFACE OF THE LUG AT UPPER AND LOWER CORNER.
Part: SPAR — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
CORROSION LT WING REAR SPAR UPPER SURFACE BETWEEN BS 738-773. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
Part: SPAR — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 799-827. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
Part: FITTING — DAMAGED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
LEFT INBOARD FLAP AFT UPPER ROLLER SUPPORT STRUCTURE CENTER BOLT HOLE FOUND DAMAGED.
Part: WEDGE — SEVERED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
LT INBOARD FLAP TRAILING EDGE WEDGE ATTACH CHANNEL OUTBOARD REMOVABLE SEGMENT FOUND SEVERED AT THE OUTBOARD MOST 12 INCH (MATERIAL CLAD 2024-T42 SHEET 0.04 INCH).
Part: SKIN — DAMAGED (ZONE 300) · airframe 31,941 hrs · 5,119 cycles
RIGHT HORIZONTAL STAB LEADING EDGE SECTION FOUND DAMAGED AT STA XFS91.2.
Part: SPAR — CORRODED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 786-799. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
Part: SKIN — DENTED (BS 1997-2015) · airframe 31,941 hrs · 5,119 cycles
DENT FUSELAGE SKIN BETWEEN BS 1997-2015 AND S46L-47L. REPAIRED AS PER EA 1-5330-99714.
Part: WEB — DAMAGED (ZONE 200) · airframe 31,941 hrs · 5,119 cycles
FLIGHT DECK OBSERVER SEAT DOUBLE FLANGE LIGHTENING HOLE LOCATED UNDERNEATH THE SEAT IN THE COCKPIT SUBFLOOR STRUCTURE FOUND DAMAGED.
Part: RIB — DAMAGED (ZONE 300) · airframe 31,941 hrs · 5,119 cycles
RIGHT HORIZONTAL STAB INBOARD ELEVATOR ASSY OUTER RIB FOUND DAMAGED.
Part: STRUCTURE — DAMAGED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
LT INBOARD AILERON INBOARD TRAILING EDGE FOUND AN IMPACT DAMAGED.
Part: BRACKET — DENTED (ZONE 800) · airframe 31,941 hrs · 5,119 cycles
DENT AFT BRACKET AT DOOR 2R LOWER SIDE. REPLACED BRACKET AS PER DRAWING ADA3760 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).
Part: BRACKET — CRACKED (ZONE 800) · airframe 31,941 hrs · 5,119 cycles
CRACK FWD BRACKET AT DOOR 4R LOWER SIDE. REPLACED BRACKET AS PER DRAWING ADA3760 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).
Part: SKIN — DENTED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
MULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE INBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.
Part: SKIN — DENTED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
MULTIPLE DENTS FOUND AT RT WING INBOARD FLAP ASSY LOWER SURFACE OUTBOARD SEGMENT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1.
Part: HINGE — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 612-615 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
Part: HINGE — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, ACTUATOR ATTACHMENT OUTBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.
Part: STRUCTURE — CRACKED (ZONE 800) · airframe 31,941 hrs · 5,119 cycles
CRACK LOWER FWD CORNER OF AFT CARGO DOOR. REPAIRED AS PER SRM 52-10-00 FIG. 17 VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: HINGE — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, SIDE LINK ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-09 PAGE 402-407 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0503 AND REPAIRED AS PER CMM 57-44-09.
Part: NONE — NONE · airframe 31,941 hrs · 5,119 cycles
EXISTING REPAIR FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED ABOUT 76 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).
Part: HINGE — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, LOWER ATTACHMENT SPOT FACE AT LT WING OUTBD FLAP INBD HINGE ON THE WING SIDE. CORROSION REMOVED AS PER CMM 57-44-08 PAGE 602-607 AND FOUND WITHIN LIMIT AS PER DAG DRAWING ARC0502 AND REPAIRED AS PER CMM 57-44-08.
Part: HINGE — CORRODED (TE FLAP) · airframe 31,941 hrs · 5,119 cycles
CORROSION PIVOT BORE AT RT WING INBOARD FLAP OUTBOARD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-07 PAGE 403-404 AND EA 1-5750- 94700.
Part: HINGE — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, LOWER ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.
Part: HINGE — CORRODED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, ACTUATOR ATTACHMENT INBD BORE AT LT WING OUTBD FLAP OUTBD HINGE ON THE WING SIDE. REPAIRED AS PER CMM 57-44-09 PAGE 402-408 AND EA 1-5750-94681.
Part: SKIN — DENTED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
EXISTING DENT FOUND AT LT WING INBOARD FLAP LOWER SURFACE LOCATED 69 INCHES FROM OUTBOARD AND 6 INCHES FROM AFT. DENT REPAIRED AS PER SRM 57-10-00 FIG2 VOL1 (MAJOR REPAIR).
Part: SKIN — DAMAGED (ZONE 100) · airframe 31,941 hrs · 5,119 cycles
FUSELAGE EXTERIOR SKIN FOUND DAMAGED BETWEEN BS 1951-1961 LONGERON 38R-39R. REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK.0.068" REMOVED 0.006"X L=3"X W=3" REMAIN 0.062" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: SKIN — DENTED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
EXISTING DENT FOUND AT LT WING INBD FLAP ASSY UPP SURFACE LOCATED 37 INCH FROM INBD AND 30 INCH FROM AFT. FOUND EXCEED LIMIT AND REPAIRED AS PER SRM 57-10-00 FIG. 34 VOL.I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.
Part: SKIN — DAMAGED (ZONE 100) · airframe 31,941 hrs · 5,119 cycles
FOUND DAMAGED SKIN INNER SIDE AT BS 1781-1801 BETWEEN STRINGER 32 AT AFT DOOR JAMB OF CENTER CARGO DOOR.
Part: DOUBLER — CRACKED (ZONE 100) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACK-MACHINED DOUBLER LOCATED BETWEEN RT WALL (ADJACENT TO RT SPOILER MIXER OUTPUT ROD) AND RT WHEEL WELL CUTOUT OF CENTER LANDING GEAR WHEEL WELL. CRACKED DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: DOUBLER — CRACKED (ZONE 100) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACK-MACHINED DOUBLER LOCATED BETWEEN LT WALL (ADJACENT TO LT SPOILER MIXER OUTPUT ROD) AND LT WHEEL WELL CUTOUT OF CENTER LANDING GEAR WHEEL WELL. CRACKED DOUBLER REMOVED AND REPLACED AS PER 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
Part: REPAIR — UNKNOWN (ZONE 100) · airframe 31,941 hrs · 5,119 cycles
FOUND SKIN EXTERIOR SIDE WITH EXTERNAL LONGITUDIANL REPAIR DOUBLER AT PACK 2 ACCESS DOOR 113AL (REF EO 1-5100-7-5001).
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACKED INTERCOSTAL AT BS1621-1641 LONGERON 7R IN AFT CABIN. REPLACED INTERCOSTAL AS PER DRAWING AFA7761 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).
Part: SKIN — DENTED (ZONE 200) · airframe 31,941 hrs · 5,119 cycles
FOUND BENT-SKIN OUTER SIDE AT UPPER FWD CORNER OF CABIN DOOR 2R. REPAIRED SKIN AS PER DRAWING AFA7761 AND SRM 52-10-00 FIG4 VOL1 & SRM 51-31-01 VOL2 (MAJOR REPAIR).
Part: STRUCTURE — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACKED-DROOPED LEADING EDGE IN LT WING. SKIN REPLACED AS PER DRAWING ACA3822 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).
Part: REPAIR — UNKNOWN · airframe 31,941 hrs · 5,119 cycles
EXISTING FLUSH REPAIR FOUND AT FUSELAGE ADJACENT TO BS435 BILGE BETWEEN LONGERON 51L TO 51R (REF EO 1-5100-7-5001). SKIN REPAIRED AS PER SRM 53-20-00 FIG6 SHEET8 VOL1 CATB REPAIR-INITIAL INSPECTION AT 7500 CYCLES AND REPETITIVE INSPECTION AT 4750 CYCLES (FLIGHT HOUR/CYCLE: 31941/5119) (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 42 END (LENGTH ABOUT 1 INCH) AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT2 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 14 END (LENGTH ABOUT 12 INCH) AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT1 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACK STRINGER 10 END, LENGTH ABOUT 9.5 INCH, AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT3 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 44 END (LENGTH ABOUT 0.75 INCH) AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT2 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACK STRINGER 11 END, LENGTH ABOUT 13.5 INCH, AT RT WING TANK. STRINGER REPAIRED AS PER SRM 57-20-00 FIG10 OPT1 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
CRACK STRINGER 11 END (LENGTH ABOUT 9 INCHES) AT LT WING TANK. CRACK SLOTTED OUT AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. HFEC INSPECTION CARRIED OUT AND FOUND NO CRACK EVIDENT AND REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: STRINGER — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
CRACK STRINGER 41 PROPAGATED FROM THE FIRST OUTBOARD FASTENER HOLE TO THE INBOARD FASTENER HOLE (LENGTH ABOUT 0.5 INCHES) AT LT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 13 END (LENGTH ABOUT 3.5 INCH) AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT3 VOL1 AND STRINGER CLIP REPLACED EA 1-5720-94687.
Part: STRINGER — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
CRACK STRINGER 9 (TOTAL LENGTH ABOUT 12.5 INCHES) AT LT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT3 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
CRACK STRINGER 10 END (LENGTH ABOUT 13 INCHES) AT LT WING TANK. CRACK SLOTTED OUT AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. HFEC INSPECTION CARRIED OUT AND FOUND NO CRACK EVIDENT AND REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: STRINGER — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 12 END (LENGTH ABOUT 9.5 INCH) AT LT WING TANK. CRACK SLOTTED OUT AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I HFEC INSPECTION CARRIED OUT AND FOUND NO CRACK EVIDENT AND REPAIRED AS PER SRM 57-20-00 FIG.10 OPT 3 VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACK STRINGER 9 END, LENGTH ABOUT 12.5 INCH, AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT3 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 12 END (LENGTH ABOUT 9 INCH) AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT3 VOL1 (MAJOR REPAIR).
Part: STRINGER — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
CRACK - STRINGER 43 (TWO LENGTH ABOUT 0.5 INCH EACH) AT RT WING TANK. REPAIRED AS PER SRM 57-20-00 FIG10 OPT1 VOL1 (MAJOR REPAIR).
Part: LONGERON — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION LONGERON 52 BETWEEN BS 1761 AND BS 1781 IN CENTER CARGO COMPARTMENT. REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK. 0.125" REMOVED 0.005"X L=20"X W=1" REMAIN 0.120" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: SUPPORT — CRACKED (L/E SLAT) · airframe 31,941 hrs · 5,119 cycles
CRACKED ANGLE SUPPORT AT RIGHT WING NR 2 L/E SLAT OUTBOARD. REMOVED AS PER SRM 51-31-01 VOL.II. NEW ANGLE FABRICATED AS PER DWG ARB 1647 AND INSTALLED AS PER SRM 51-35-01 AND 51-35-02 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION AFT SHEAR TIES AT FRAME BS 1741 BETWEEN LONGERON 52 AND 51L IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK. 0.071" REMOVED 0.004" X L=6"X W=2" RETAIN 0.067" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG. 1A VOL.I. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION LONGERON 51R BETWEEN BS 1721 AND BS 1741 IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. MATERIAL ORIGINAL THK. 0.125" REMAIN 0.121" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION SHEAR TIES AT FRAME BS 1721 BETWEEN LONGERON 52 AND 51L IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK. 0.090" REMOVED 0.006"X L=8"X W=3" REMAIN 0.084" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION AFT SHEAR TIES AT FRAME BS 1741 BETWEEN LONGERON 52 AND 51R IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION FORWARD SHEAR TIES AT FRAME BS 1741 BETWEEN LONGERON 52 AND 51L IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. MATERIAL THK.0.071",REMAINED 0.066" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION SKIN DOUBLER BETWEEN BS 1721 AND BS 1741 BETWEEN LONGERON 51L AND 51R IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II.
Part: FRAME — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION FRAME CHORD AT BS 1781 BETWEEN LONGERON 50L AND 50R IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK. 0.090" REMOVED 0.006"X L=20"X W=1.25", REMAIN 0.084" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION DOUBLER ATTACHED ANCHOR NUTS BETWEEN BS 1721 AND BS 1741 BETWEEN LONGERON 52 AND 51L IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II.
Part: STRUCTURE — CORRODED (ZONE 200) · airframe 31,941 hrs · 5,119 cycles
FOUND CORROSION, STRUCTURE ALONG BS 1741 LONGERON 52 IN CENTER CARGO COMPARTMENT. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II.
Part: FRAME — CORRODED (FUSELAGE) · airframe 31,941 hrs · 5,119 cycles
CORROSION FRAME CHORD AT BS 1741 BETWEEN LONGERON 50R AND 52 IN CENTER CARGO COMPARTMENT. ORROSION REMOVED AS PER SRM 51-21-01 VOL.II. ORIGINAL MATERIAL THK. 0.090" REMOVED 0.006"X L=10"X W=1.25" REMAIN 0.084" FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIG.1A VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: SKIN — DAMAGED (ZONE 200) · airframe 31,941 hrs · 5,119 cycles
FOUND NR 3L PLUG DOOR FWD UPPER FOUND SIDE SKIN DAMAGED WITH RIVETS SHEARED. REPAIRED AS PER SRM 52-10-00 FIG.10 VOL.I. CLASSIFIED MINOR REPAIR PER GMM 6-2-100.
Part: RIB — CRACKED (ZONE 500) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACKED INBOARD SUPPORT RIB AT LT WING SLAT TRACK NR 16. RIB REPLACED AS PER DOUGLAS DRAWING ARB2850 AND SRM 51-31-01 VOL2 AND SRM 51-33-01 VOL2 (MAJOR REPAIR).
Part: RIB — CRACKED (ZONE 600) · airframe 31,941 hrs · 5,119 cycles
FOUND CRACKED INBOARD SUPPORT RIB AT RT WING SLAT TRACK NR 16. RIB REPLACED AS PER DRAWING ARB2850 AND ARB1129 AND ARB1323 AND SRM 51-31-01 VOL2 AND 51-33-01 VOL2 (MAJOR REPAIR).