N743AX
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.
458 reports on file, 2008-02-03 – 2025-03-13.
Part: SKIN — CORRODED (ZONE 100) · airframe 97,545 hrs · 46,569 cycles
CARRIED OUT MAJOR REPAIR OF LH FUSELAGE SKIN FOR CORROSION BEHIND MAIN CARGO DECK SCUFF PLATE AT STA 588-654, STR 19-22LH
Part: STRINGER — CRACKED (ZONE 200) · airframe 97,545 hrs · 46,569 cycles
DURING AIRCRAFT MAINTENANCE, WAS ACCOMPLISHING HFEC INSPECTIONS AND FOUND CRACK DAMAGE ON THE STRINGERS S-2R & S-8R AT STA 676. THE STRINGERS ARE REPAIRABLE PER BOEING SRM 53-00-03, REPAIR 1; HOWEVER, THE DAMAGE LOCATION IS AFFECTED BY THE IAI FRIEGHTER CONVERSION STC IN THAT THERE ARE STRAPS INSTALLED ON S-2R THAT ARE PART OF THE IAI CONVERSION. ONE 1/2" CRACK ON S2R ON THE THIRD FASTNER FROM STA 676 AT THE FWD INBOARD ANGLE.TWO CRACKS ON S8R ON THE SECOND FASTNER FROM STA 676. ONE 1/3" CRACK AT THE FWD OTB ANGLE AND ONE 3/4" CRACK AT THE OTB AFT ANGLE. REPAIR - SEC 43, STA 654 - 698, STR S-2R & S-8R.
Earlier reports · 2008–2020 · 456 reports
2020
Part: WEDGE — CORRODED (NR 9 SLAT) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
#9 SLAT UPPER TE WEDGE AFT SURFACE IS CORRODED IN NUMEROUS AREAS. REPAIRED DAMAGE ON 39 SLAT TE WEDGE IAW SRM 57-43-02 REPAIR 1,51-70-10 PARA 7, 8, 14, 15, 18, 20, 21, 22.
Part: STRINGER — CORRODED (BS 390) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORRODED STR33L AT STA 390. REMOVED AND REPLACED STR 33L AT STA 390 I/A/W REA 47417REA19, B767 SRM 53-00-03 REPAIR 2,51-40-02.
Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON SHEAR TIE JUST AFT OF FRAME 742, BETWEEN STR 33L AND STR 34L. REMOVED AND REPLACED SHEAR TIE I/A/W B767 SRM 51-40-02.
Part: SUPPORT BRACKET — CORRODED (BS 581) · airframe 93,741 hrs · 44,878 cycles
MAIN DECK CARGO DOOR VIEW PORT CORRODED ON THE MOUNTING FLANGE. REPAIRES MAIN DECK CARGO DOOR VIEW PORT MOUNTING FLANGE I/A/W REA 47417REA20 AND NR 0669.
Part: FAILSAFE — CORRODED (BS 539) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
STA 539.5, STRINGER 31R FOUND CORROSION ON FAIL SAFE STRAP ON FLC CUT OUT. REPAIRED CORROSION AT STA 539.5 STR 31R ON REA 47417REA09 AND NR 0785.
Part: SHEAR TIE — CORRODED (BS 390) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
SHEAR TIE BETWEEN S33L-S34L AT STA 390 IS CORRODED. REMOVED CORROSION OUT OF LIMITS PER B767 SRM 53-00-07 DETAIL 2. FABRICATED AND INSTALLED NEW PER B767 DWG 114T1223 AND SRM 51-40-02 PARA 4 AND 7. REF NR 0693.
Part: SUPPORT BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON FWD SUPPORT BEAM FOR THE FLC DOOR FWD HINGE. CORRODED ON THE UPPER FLANGE JUSTFWD AND ABOVE THE FWD HINGE, JUST INSIDE THE FLC DOOR CUTOUT. REPAIRED THE FWD ACTUATOR SUPPORT BEAM JUST INSIDE FLC DOOR CUTOUT IAW REA 47417REA16 AND NR 0632.
Part: FLOOR SUPPORT — CORRODED (BS 742-764) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORRODED INTERCOSTAL, LOCATED AT BOTTOM OF UPPER CARGO FLOOR BEAM AT STA 764, RBL 12. REMOVED AND REPLACED INTERCOSTAL IAW SRM 53-30-50.
Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
LT WING UPPER AFT REAR SPAR CORRODED. REPAIRED ON REA 47417REA17 AND NR 0834.
Part: SKIN — DAMAGED (LT WING) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
LT WING LOWER SKIN HAS 34 HOLES THAT ARE OUT OF LIMITS IAW REA 47417REA18. REPAIRED ON REA 47417REA18. REF NR 0927 AND 0472
Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
L/W L/E AIR LOAD STRUT CORRODED UNDER ALL N/P'S AT WS. 785 NR 3 SLAT O/B AUX. TRK. AREA. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW B767 SRM 51-41-09 MAX 10% OF OT OF .071 REMAINING .059 REMOVED AND REPLACED AIR LOAD STRUT AT LW WS 785 IAW B767 SRM 51-40-02 PARA 9
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
SHEAR TIE CORRODED AT BS 1197, STRINGERS 32 - 33R. THE SHEAR TIE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL II. REPLACED THE SHEAR TIE IAW SRM 51-40-02, PARA 4 &7.
Part: STRINGER — CORRODED (BS 368) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON FAILSAFE CHORD, STR 32L AT STA390. REMOVED AND REPLACED DAMAGED S-32L IAW B767 SRM 53-00-03 REPAIR 2. S-32L OUT OF LIMITS IAW B767 SRM 53-00-03 DETAIL II.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERNAL SURFACE OF THE SKIN, ON THE RT HORIZONTAL STAB AT LEADING EADGE AT RIB 13. REPAIRED PER 47417REA15 AND NR 0201.
Part: WEB — CORRODED (BS 390) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON WEB AT BS 390, STRINGERS 29L-28L. REMOVED AND REPLACED WEB AT STA390 STR 29L-28L IAW BOENING DWG 14IT1223, AND SRM 51-40-02. REF CWO 123512-0020 AND AMES REA 47417 FAB 06.
Part: WINDOW FRAME — CORRODED (BS 522-612) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE FRAME, OF THE MDCD VIEWING WINDOWS, WINDOWS NR 3, 5, AND 11, ON THE INTERIOR LOWER EDGE OF THE MDCD. MDCD CORROSION OUT OF LIMITS. REPAIRED IAW 47417REA20.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
SHEAR TIE CORRODED AT BS 1197, STRINGERS 32-33 LT. REMOVED CORROSION, LOST .011, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.
Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON SHEAR TIE AT FRAME 1395, BTW STR.37L AND STR.38L. REMOVED DAMAGED SHEAR TIE AND INSTALLED NEW SHEAR TIE FABRICATED FROM 7075T6 .063 FROM PO-0145891 TAG#2583486 IAW BOEING DRAWING # 146T1215 AND B767-200 SRM 51-40-02 PARA 4.
Part: SHEAR TIE — CORRODED (BS 698) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
BS 698 HAD A CORRODED SHEAR TIE BETWEEN STRINGERS 36L AND 37L. THE SHEAR TIE WAS BLENDED IAW 53-00-07, ALLOWABLE 2.0G. THICKNESS .050", REMAINING .040", FOUND OUT OF LIMITS. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02, PARA 4 AND 7.
Part: STRINGER SPLICE — CORRODED (BS 1461) · airframe 93,741 hrs · 44,878 cycles
STRINGER SPLICE 23R IS CORRODED AND CRACKED, BELOW FRAME 1461. REMOVED DAMAGED STRINGER SPLICE ANGLE AND INSTALLED NEW ANGLE FABRICATED ON CWO 123512-0001, IAW DOCUMENT 47417FAB01 AND SRM 51-40-02 PARA 4 AND 7.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERIOR SURFACE OF SKIN ON RIGHT HORIZONTAL STAB AT RIB 8 TE. REPAIRED ON 47417REA 13.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE LEFT HOR. STAB. AT THE T/E, BTW RIB 3 AND RIB 4. REMOVED CORR. FOUND TO BE OUT OF LIMITS IAW B767 SRM 55-10-01 TABLE I WITH LOWEST POINT AT .120. REPAIRED AREA IAW REA 47417REA04.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE RIGHT HOR. STAB., AT STR.3, BTW RIB 3 AND RIB 4. BLENDED AREA IN QUESTION. LOWEST AREA FOUND .166" FOUND TO BE OUT OF LIMITS IAW B767 SRM 55-10-01 FIG 101 DETAIL V. COMPLETED REPAIR INSTRUCTIONS AS OUTLINED IN REA# 47417REA10 REV IR.
Part: STRINGER — CORRODED (BS 710-730) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON STRINGER 36L AT STRINGER CLIP STA 720. REMOVED CORROSION 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW 15767 SRM 53-00-03 REPAIR 2. REMOVED DAMAGED STRINGER AND INSTALLED REPAIRED SECTION IAW B767 SRM 53-00-07 AND B767 SRM 51-40-02, AND REA 47417REA19
Part: SHEAR TIE — CORRODED (BS 698) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
STA 698 HAS CORR SHEAR TIE BETWEEN STR 34L AND 35L. REMOVED CORROSION ORIGINAL THICKNESS .050 REMOVED .010 REMAINING THICKNESS .040 FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-07. REMOVED OLD SHEAR TIE AND REPLACED WITH NEW SHEAR TIE B767 SRM 51-40-02.
Part: SHEAR TIE — CORRODED (BS 632) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
BS 632 HAD A CORRODED SHEAR TIE BETWEEN STRINGERS 39L AND 39R FWD OF LAV SERVICE BOX. REMOVED CORROSION ORIGINAL THICKNESS .052 REMOVED .008 REMAINING .044. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL II. LOCATED AND DRILLED IAW DWG 143T1209 AND INSTALLED 51-40-02 IAW SRM.
Part: SHEAR TIE — CORRODED (BS 720) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
BS 720 SHEAR TIE CORRODED BETWEEN STRINGERS 36L - 37L. REMOVED CORROSION, ORIGINAL THICKNESS .060, REMOVED .015, REMAINING .045. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
RIGHT HORIZONTAL STAB UPPER EXTERIOR SKIN CORRODED AT RIB9 TE. REPAIRED ON 47417REA14.
Part: FLOOR SUPPORT — CRACKED (BS 1417) · airframe 93,741 hrs · 44,878 cycles
FLOOR STRINGER SUPPORT IS CRACKED AT THE UPPER RIVET, ON THE FWD SIDE OF FRAME 1417, ABOVE STR.38L, AT FRAME 1417 UPPER CHORD. REMOVED AND REPLACED FLOOR STRINGER SUPPORT ON THE FWD SIDE OF 1417 AT STR 38L IAW B767 SRM 51-40-02 PAR. 7
Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
AIR LOAD STRUT CORRODED AT NR 8 SLAT O/B AUX. TRK. AREA. AIR LOAD STRUT CORRODED OUT OF LIMITS IAW B767 57-41-09 REPLACED STRUT IAW B767 SRM 51-40-02 PARA 4 AND 7.
Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
R/W L/E AIR LOAD STRUT AND UPPER L/E FORMER ARE CORRODED NEAR #11 SLAT O/B AUX.TRK. AREA. AIR LOAD STRUT AND UPPER L/E FORMER CORRODED OUT OF LIMITS IAW B767 SRM 57-41-09. REPLACED IAW B767 SRM 51-40-02 PARA 4 AND 7 SEE REVERSE AND PARTIAL WORK SHEET 100 FOR PARTIAL WORK ACCOMPLISHED, REF CWO 123512-0017 FOR FABRICATION.
Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON SHEAR TIE ON THE AFT SIDE OF FRAME 1540, BTW STR.37R AND 38R. CORROSION ON SHEAR TIE ON THE AFT SIDE OF FRAME 1540 BLENDED FOUND TO BE OUT OF LIMITS FABRICATED NEW SHEAR TIE INSTALLED IAW B767 SRM 51-40-02 PAR 4 AND PAR 7.
Part: SHEAR TIE — CORRODED (BS 566) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON SHEAR TIE AT STA566 STR39L-38L. BLENDED SHEAR TIE. FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-07 FLAG NOTE D AND INSTALLED NEW SHEAR TIE IAW B767 SRM 51-40-02 PARA 7-4.
Part: STRINGER — CORRODED (BS 1087) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
STRINGER 32 LT, BS 1087 WAS CORRODED ON UPPER SIDE. REPLACED THE SECTION OF THE STRINGER IAW SRM 53-00-03, REPAIR 2, DETAIL IV, AND SRM 51-40-02.
Part: SHEAR TIE — CORRODED (BS 698) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
STA 698 HAS CORR SHEAR TIE BETWEEN STR 35L AND 36L. REMOVED CORROSION ORIGINAL THICKNESS .050, REMOVED .010, REMAINING .040 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.
Part: FAILSAFE — CORRODED (BS 390) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON FRAME FAIL SAFE CHORD AT STA 390 S33L - S34L. REPAIRED FAIL SAFE CHORD AT STA 390 S37L-S33L I/A/W AMES DOCUMENT 47417REA06.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN ON RIGHT HORIZ STAB AT RIB8 LEADING EDGE. REPAIRED ON 47417REA12.
Part: SHEAR TIE — CORRODED (BS 566) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON SHEAR TIE AT STA566 STR38L-37L. REMOVED CORROSION ORIGINAL THICKNESS .050 REMOVED .008 REMAINING .042 TAG # 14483 FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-07 DETAIL II. LOCATED AND DRILLED IAW DWG 143T1209 AND INSTALLED IAW B767 SRM 51-40-02 PAR 7, PAR 4.
Part: SHEAR TIE — CORRODED (BS 720) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
BS 720 SHEAR TIE CORRODED BETWEEN STRINGERS 35L-36L. REMOVED THE CORROSION, ORIGINAL THICKNESS .060, REMOVED .015, REMAINING THICKNESS .045, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE RIGHT HOR. STAB., AT STR.3, BTW RIB 4 AND RIB 5.BLENDED AREA IN QUESTION. LOWEST AREA FOUND WAS .130" FOUND TO BE OUT OF LIMITS IAW B767 SRM 55-10-01 FIG 101 DETAIL V. COMPLETED REPAIR INSTRUCTIONS AS OUTLINED IN REA# 47417REA10. REV IR
Part: STRINGER — CORRODED (BS 1188-1208) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
STRINGER 37 LT, BS 1197 WAS CORRODED. THE STRINGER AT BS 1197 WAS ALSO CRACKED, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REMOVED AND REPLACED THE STRINGER WITH REPAIR SECTION IAW SRM 53-00-03, REPAIR 2.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 93,741 hrs · 44,878 cycles
CORROSION ON THE UPPER EXTERIOR SURFACE OF THE SKIN, ON THE RIGHT HOR. STAB., AT THE L/E, AT RIB 7. CORROSION OUT OF LIMIT ON UPPER HORZ STAB SKIN 4E AT RIB 7, REPAIRED UPPER SKIN I/A/W AMES DOCUMENT 47417REA11.
Part: HYDRAULIC SYSTEM — LOW PRESSURE (C SYSTEM) · airframe 93,226 hrs · 44,638 cycles
AFTER GEAR DOWN AND FLAPS AT 2" C HYDRAULIC PRESSURE AT 2990
2019
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
RT MAIN FRAME CORRODED (PICKLE FORK).
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
NR 8 SLAT L/E SKIN CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs
BULK CARGO FLOORBEAM CORRODED.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,834 hrs · 42,309 cycles
WEB CORRODED.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STIFFENER ANGLE CORRODED.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,134 hrs · 43,909 cycles
TEAR STRAP CORRODED.
Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
LT WING T/E UPPER AFT BEAM CHORD CORRODED.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STIFFENER CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
BULK CARGO DOOR SKIN CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CRACKED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL FLANGE CORRODED.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
UPPER CHORD CORRODED.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CLIP IS CORRODED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TOP ANGLE OF WEB CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FUSE SKIN CORRODED.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR TIE CORRODED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STIFFENER ANGLES CORRODED.
Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
PRESSURE WEB CORRODED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
BATH TUB FITTING CORRODED.
Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
LONGERON SPLICE PLATE CORRODED.
Part: SUPPORT BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SUPPORT BEAM CORRODED.
Part: FITTING — CRACKED (PYLON) · airframe 9,142,934 hrs · 43,909 cycles
INTERCOASTAL PYLON FITTING CRACKED.
Part: FITTING — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
PYLON FITTING SIDE OF SEAT TRACK CRACKED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TRANSITION / STABILIZATION ANGLE IS CORRODED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STIFFENER ANGLE CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: LONGERON SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
LONGERON SPLICE PLATE CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED.
Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
END FITTING CRACKED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CRACKED.
Part: LINK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR LINK FWD END OF LONGERON IS CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SUPPORT BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SUPPORT BEAM CORRODED.
Part: FITTING — CRACKED (PYLON) · airframe 9,142,934 hrs · 43,909 cycles
PYLON FITTING CRACKED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FAIL SAFE STRAP CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOASTAL IS CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FUSELAGE SKIN CORRODED.
Part: SUPPORT FITTING — CRACKED (PYLON) · airframe 9,142,934 hrs · 43,909 cycles
LWR SUPPORT FITTING PYLON CRACKED.
Part: SPAR WEB — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
RHS AFT SPAR WEB IS CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: FITTING — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
PRESSURE DECK FITTING CRACKED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SUPPORT RIB — CORRODED (NR 9 SPOILER) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SUPPORT RIB AT #9 SPOILER CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL WEB CORRODED.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER FRAME CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SHEAR TIE — CORRODED (BS 1351) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR TIE CORRODED
Part: FRAME SPLICE — CORRODED (BS 1263) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FRAME SPLICE BRACKET CORRODED
Part: SEAT TRACK — CORRODED (BS 991-1070) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: FRAME SPLICE — CORRODED (BS 1263) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FRAME SPLICE CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (BS 445-665) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (BS 1207-1405) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SHEAR TIE — CORRODED (BS 1329) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR TIE IS CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SHEAR TIE — CORRODED (BS 1329) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR TIE CORRODED
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL CHORD CORRODED.
Part: SEAT TRACK — CORRODED (BS 665-756) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL CHORD CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (BS 929) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (BS 665-786) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SUPPORT FITTING CORRODED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER FITTING CORRODED.
Part: SKIN — CORRODED (BS 1175) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
WEB CORRODED.
Part: SEAT TRACK — CORRODED (BS 445-665) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRUCTURE — CORRODED (BS 764) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
AUX CHORD CORRODED
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
BULKHEAD FITTING CORRODED.
Part: TEAR STRAP — CORRODED (BS 1351) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TEAR STRAP CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
AIR LOAD STRUT CORRODED.
Part: SEAT TRACK — CORRODED (BS 445-665) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (BS 991-1070) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (BS 1208-1405) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FAIL SAFE STRAP CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: ANGLE — CORRODED (BS 1263) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
Z ANGLE FOR GILLNER CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SHEAR TIE — CORRODED (BS 1131) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR TIE CORRODED
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
ALC DOOR SILL CLOSE OUT WEB CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (BS 1207-1405) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (BS 991-1070) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (BS 786-911) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: STRAP — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL WEB STRAP CORRODED.
Part: SEAT TRACK — CORRODED (BS 1316-1405) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL CHORD CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL STIFFENER CORRODED.
Part: SEAT TRACK — CORRODED (BS 991-1070) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: STRINGER — CORRODED (BS 1307-1339) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL BEAM CORRODED.
Part: SPOILER — CRACKED (WING) · airframe 9,142,934 hrs · 43,909 cycles
NR 5 SPOILER CRACKED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: SEAT TRACK — CORRODED (BS 1207-1316) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: STIFFENER — CORRODED (BS 445) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK SPLICE STIFFENER CORRODED
Part: STRINGER — CORRODED (BS 698) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED
Part: SEAT TRACK — CORRODED (BS 991-1070) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: WEB — CORRODED (BS 1109-1131) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
WEB IS CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL CHORD.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
CORROSION ON LOWER CHORD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: STRINGER — CRACKED (BS 1080) · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CRACKED
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEELBEAM CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (BS 1207-1405) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SKIN — CORRODED (BS 738) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FUSELAGE SKIN CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: STRINGER — CORRODED · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED
Part: TEAR STRAP — CORRODED (BS 1175) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TEAR STRAP CORRODED
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL CHORD CORRODED.
Part: SEAT TRACK — CORRODED (BS 445-665) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (BS 445-665) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
C-TRACK SPLICE CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CRACKED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: SEAT TRACK — CORRODED (BS 665-786) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
PANEL SUPPORT CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
CHORD CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL WEB CORRODED.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
CHORD CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
CHORD CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL WEB CORRODED.
Part: RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
RAIL CORRODED FLOOR SUPPORT.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,924 hrs · 43,909 cycles
TEAR STRAP CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FITTING CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL CORRODED.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL WEB CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
SHEAR PLATE CRACKED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TEAR STRAP CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,993 hrs · 43,909 cycles
INTERCOSTAL WEB CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL CHORD CORRODED.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TEAR STRAP CORRODED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
WEB CORRODED.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
WEB CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOORBEAM CORRODED.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
KEEL BEAM FAIRING SPLICE CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FRAME STATION 1175 HAS CORROSON ON WEB.
Part: SEAT TRACK — CORRODED (BS 1405-1605) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SEAT TRACK CORRODED
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED.
Part: STRINGER — CORRODED (BS 1080-1097) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLOOR PANEL ATTACHED TO ANGLE IS CORRODED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN TEAR STRAP CORRODED AT STRINGER.
Part: STRINGER — CORRODED (BS 368) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED
Part: STRINGER — CORRODED (BS 518-522) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED
Part: INTERCOSTAL — CORRODED (BS 1405) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
INTERCOSTAL CORRODED
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER AND FRAME CORRODED.
Part: FLOORBEAM — CORRODED (BS 676) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
UPPER CARGO FLOOR BEAM CORRODED
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
ALC UPPER FLOOR FRAME CAP CORRODED.
Part: STRINGER CLIP — CORRODED (BS 1087) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CLIP CORRODED BEYOND LIMITS
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FITTING BETWEEN STRINGER IS CORRODED.
Part: STRINGER — CORRODED (BS 858) · airframe 9,142,934 hrs · 43,909 cycles
UPPER CNTR WING SKIN AND STRINGER CORRODED
Part: SKIN — CORRODED (BS 1065-1067) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FUSELAGE SKIN CORRODED
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SHEAR TIE CORRODED AT STRINGER.
Part: FRAME — CORRODED (BS 1175) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FRAME SEGMENT CORRODED
Part: SKIN — CORRODED (BS 1087) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
SKIN CORRODED
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CRACKED.
Part: SKIN — CORRODED (BS 1395-1427) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
BULGING FUSELAGE SKIN
Part: STRINGER — CORRODED (BS 1087) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER CORRODED
Part: FLOORBEAM — CORRODED (BS 544) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
UPPER CARGO FLOOR BEAM CORRODED
Part: WEB — CORRODED (DOOR) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
ALC DOOR WEB CORRODED
Part: FITTING — CRACKED (FUSELAGE) · airframe 9,142,934 hrs · 43,909 cycles
ALC BULK HEAD FITTING IS CRACKED.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED.
Part: STRINGER — CORRODED (BS 1141-1207) · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED.
Part: BEAM — CORRODED (DOOR) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
ALC DOOR BEAM CORRODED
Part: BUTT JOINT — CORRODED (BS 858) · airframe 9,142,934 hrs · 43,909 cycles
UPPER CNTR WING SKIN BUTT SPLICE CORRODED
Part: FLOORBEAM — CORRODED (BS 588) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
UPPER CARGO FLOOR BEAM CORRODED
Part: STRINGER — CORRODED (BS 1163-1185) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
STRINGER IS CORRODED
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
ALC WEB ABOVE STRINGER CORRODED.
Part: FLOORBEAM — CORRODED (BS 610) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLC UPPER FLOOR BEAN UPPER CHORD CORRODED
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
TEAR STRAP CORRODED AT STRINGER.
Part: SPLICE PLATE — CORRODED (BS 789) · airframe 9,142,934 hrs · 43,909 cycles
CORRODED SPLICE PLATE
Part: FLOORBEAM — CORRODED (BS 698) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
UPPER CARGO FLOOR BEAM CORRODED
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
ALC UPPER FLOORBEAM SHEAR WEB CORRODED.
Part: PRESSURE DECK — CORRODED (BS 977) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
RWW CANTED PRESSURE DECK WEB AND ANGLE CORRODED
Part: DOOR SILL — CORRODED (BS 544) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLC DOOR UPPER AND LOWER SILL IS CORRODED
Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
CORRODED HORZ STAB CTR BOX INTERNAL
Part: FAILSAFE — CORRODED (BS 1351) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FAILSAFE STRAP ALC DOOR ENCLOSURE CORRODED
Part: FRAME — CORRODED (BS 955) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
RH MAIN FRAME PICKLE FORK CORRODED
Part: BULKHEAD WEB — CORRODED (BS 212.5) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FORWARD BULKHEAD PRESSURE PANEL CORRODED
Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
LW LOWER SPLICE PLATE CORRODED
Part: SKIN — CORRODED (RT WING TE) · airframe 9,142,934 hrs · 43,909 cycles
RW TRAILING EDGE CORRODED SKIN
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
LH WING LOWER SKIN HAS CORROSION
Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 914,934 hrs · 43,909 cycles
LW UPPER SPLICE PLATE CORRODED
Part: DOOR SILL — CORRODED (BS 544) · airframe 9,142,934 hrs · 43,909 cycles
FLC DOOR SILL CORRODED
Part: SKIN — CHAFED (BS 1809) · airframe 9,142,934 hrs · 43,909 cycles
AFT SIDE FUSELAGE SEAM DOUBLER CHAFED
Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
BULK CARGO DOOR INNER SURFACE CORRODED
Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
CORROSION HORIZ STAB CTR BOX INTERNAL
Part: KEELBEAM — CORRODED (LT MLG WW) · corrosion level 2 · airframe 9,142,934 hrs · 22,218 cycles
LEFT WHEEL WELL LEFT HAND KEEL BEAM LOWER O/B FLANGE CORRODED
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
L/W UPPER AND LOWER WING SKIN IS CORRODED
Part: SKIN — CORRODED (BS 1552) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
EXTERIOR FUSELAGE SKIN CORRODED
Part: SKIN — GOUGED (BS 1065-1087) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FUSELAGE SKIN HAS MULTIPLE GOUGES
Part: SKIN — CHAFED (BS 1809) · airframe 9,142,934 hrs · 43,909 cycles
AFT SIDE OF FUSELAGE SKIN SEAM DOUBLER CHAFED
Part: WEB — CORRODED (BS 592) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles
FLC DOOR ENCLOSURE WEB BETWEEN UPPER AND LOWER SILLS CORRODED
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RIGHT UPPER WING/SIDE AFT OF BODY SPLICE PLATE HAS 4 AREAS OF EXFOLIATION LOCATED ON THE LONGERON DOUBLER.
Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 91,429 hrs · 43,909 cycles
THE FWD FLANGE OF THE KEELBEAM IS CRACK LOCATED AT STA 786 RBL2 APPROX 0.5" LONG VERIFIED WITH HFEC.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT WW LT KEEL BEAM WEB UPPER SURFACE CORRODED STA 995 LBL 11.
Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT WING TE WS 597 UPPER PANEL ATTACH CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT KEEL BEAM STA 1005 RBL 11 I/B VERTICAL FLANGE CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 960 LBL 11 LOWER I/B FLANGE CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEELBEAM STA 918 LBL11 LOWER KEEL FLANGE CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 1000-1005 LBL 11 LOWER I/B FLANGE CORRODED.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
INTERNAL CENTER WING SECTION B STA 786 BULKHEAD RBL 15 FUEL MANIFOLD CUT OUT LWR SECTION CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT WW LT KEEL BEAM LOWER O/B FLANGE UPPER SURFACE CORRODED STA965-977 LBL11.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT KEEL BEAM STA 859 RBL11 LOWER I/B KEEL FLANGE CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 955 LBL11 LOWER I/B KEEL FLANGE CORRODED.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
ADJACENT TO THE RT UPPER/WING SIDE OF BODY SPLICE PLATE THERE ARE 6 AREAS OF CORROSION ON THE WING UPPER SURFACE.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT WW INTERNAL LONGERON O/B CHORD STA 1055 RBL 95 CORRODED ON UPPER VERTICAL CHORD FLANGE.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT KEEL BEAM STA 1005 RBL 11 LOWER I/B FLANGE CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT WW LT KEEL BEAM VERTICAL FLANGE STA 976 LBL11 CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 1044 LBL 11 LOWER I/B FLANGE CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 1020 LBL 11 LOWER I/B FLANGE CORRODED.
Part: BOLT — UNSECURE (TE FLAP) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT WING OB FLAP IB FLAP SUPPORT FITTING COMMON TO LOWER WING SKIN AS SEEN THRU ACCESS PANEL 572DB BOLT IS NOT SECURE. REMOVED AND REPLACE BOLTS TO LT WING OB FLAP IB FLAP SUPPORT IAW REA 47324 REA41.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT KEEL BEAM STA 790 RBL 11 IB SPLICE FITTING CORRODED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 800 LBL11 IB LOWER FLANGE CORRODED.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LEFT WING UPPER SKIN AT WING TO BODY SPLICE HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE FROM UPPER STRINGER 17 TO REAR SPAR, WS 97.5 TO APPROX 107.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LEFT FUSELAGE UPPER WING TO BODY SPLICE STA 785-955 CORRODED IN MULTIPLE AREAS.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
RT KEEL BEAM 790 RBL 11 OB SPLICE FITTING CORRODED.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,429 hrs · 43,909 cycles
LT KEEL BEAM STA 790 LBL11 IB SPLICE FITTING CORRODED.
2017
Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 89,914 hrs · 43,179 cycles
LEFT WING 720 AND 780 HAVE CORROSION JUST FWD OF THE FORWARD WING SPAR.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs
CLOSE OUT WEB CORRODED AT FS 1263 TO 1285 S33L. REPLACED IAW SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
INTERCOSTAL CORRODED AT FS 1263-1285 INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
S33 STRINGER IS CORRODED AT FS 1210 TO 1295. REPAIRED IAW SRM 53-00-03 REPAIR 2.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 89,615 hrs · 43,025 cycles
S37 STRINGER IS CRACKED AT FS 1263 TO 1285. REPAIRED IAW SRM 53-00-03 REPAIR 2.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
STRINGER 32L CORRODED FROM BS 1230 TO 1300. REPAIRED IAW SRM 53-00-03, REPAIR 2.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
S39L STRINGER IS CORRODED AT FS 1263 TO 1285. REPAIRED IAW B767 SRM 53-00-03 REPAIR 2.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
TEAR STRAP CORRODED AT FS 1236 26L TO 36L. INSTALLED NEW TEAR STRAP IAW SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
INTERCOSTAL CORRODED AT FS 1263-1285. INSTALL NEW INTERCOSTAL IAW SRM 51-40-02, 51-40-05.
Part: SKIN — CORRODED (BS 1260) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
FUSELAGE SKIN AT BS 1260 ABOVE STRINGER 31 HAS CORRODED HOLE IN SKIN. REPAIRED IAW REA 47284REA02 REVA ,767 SRM 51-40-02, 51-40-05.
Part: STRINGER — CORRODED (BS 1263-1307) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
STRINGER 34L CORRODED BS 1263 TO 1300. REPAIRED IAW SRM 53-00-03, REPAIR 2.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
INTERCOSTAL CORRODED AT FS 1263-1285 INSTALL NEW INTERCOSTAL IAW SRM 51-40-02, 51-40-05.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs
INTERCOSTAL CORRODED AT FS 1263 TO 1285 S26L. REPLACED INTERCOSTAL IAW SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
INTERCOSTAL CORRODED AT FS 1263 TO 1285 S33L REPLACED INTERCOSTAL IAW SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
SHEAR TIE CORRODED AT FS 1241 S30L. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
TEAR STRAP CORRODED AT FS 1263 S30L TO S33L. INSTALLED NEW TEAR STRAP IAW SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
SHEAR TIE CORRODED AT FS 1285 S29L-S33L. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.
Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
TEAR STRAP CORRODED AT FS 1241 S26-S36L. INSTALLED NEW TEAR STRAP IAW SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
S30L STRINGER CORRODED AT STATION 1270 TO 1306. REPAIR IAW SRM 53-00-03 REPAIR2.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,615 hrs · 43,025 cycles
S34L STRINGER CORRODED AT STATION 1230 TO 1250. REPAIR IAW SRM 53-00-03 REPAIR 2.
Part: SKIN — CORRODED (BS 544-566) · airframe 89,615 hrs · 43,025 cycles
SKIN CRACK AT BS 544 - 566 STRINGERS 37 - 38L. REPAIRED IAW REA4728REA01
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
ALC S32 LT IS CORRODED AT FS 1263 - 1285.
Part: STRINGER — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 32L FOUND CORRODED AT BS 1263 - 1285.
Part: STRINGER — SPLIT (BS 1263-1285) · airframe 89,630 hrs · 43,031 cycles
STRINGER 37L, BS 1263 - 1285 SPLIT.
Part: STRINGER — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 33L IS CORRODED AT BS 1263 - 1285.
Part: STRINGER — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 33L IS CORRODED, BS 1263 - 1285.
Part: STRINGER — CORRODED (BS 1263) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 39R AT BS 1263 IS EXFOILATED.
Part: FLOOR SUPPORT — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
FLOOR SUPPORT, BS 1263 - 1285, RBL 16.4 CORRODED.
Part: STRINGER — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 39L, BS 1263 - 1285 IS CORRODED.
Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
SHEAR TIE CORRODED AT BS 1307, STRINGERS 30-33L.
Part: TEAR STRAP — CORRODED (BS 1236) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
TEAR STRAP AT BS 1236 BETWEEN STRINGERS 26 & 36L CORRODED
Part: TEAR STRAP — CRACKED (BS 1241) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
TEAR STRAP AT BS 1241, STRINGER 33L IS CORRODED AND CRACKED
Part: TEAR STRAP — CORRODED (BS 1263) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
TEAR STRAP CORRODED AT BS 1285 STRINGERS 30-33L.
Part: STRINGER — CORRODED (BS 1241) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 34L, BS 1241 IS CORRODED.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
SHEAR TIE CORRODED AT BS 1241 STRINGERS 30-33L.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
ALC S31 LT IS CORRODED AT FS 1263 - 1307.
Part: STRINGER — CORRODED (BS 1263-1307) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
STRINGER 31L FOUND CORRODED AT BS 1263 - 1307.
Part: FLOOR SUPPORT — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
CORROSION ON FLOOR SUPPORT BETWEEN BS 1263 - 1285, LBL 26.
Part: FLOOR SUPPORT — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
CORROSION FOUND ON FLOOR SUPPORT BETWEEN BS 1263 - 1285, LBL 33.
Part: CLOSEOUT PANEL — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
CLOSE OUT PANEL AT BS 1263 - 1285, RBL 33 - 42 HAS A HOLE CORRODED THRU IT.
Part: SKIN — CORRODED (BS 1238) · corrosion level 2 · airframe 89,630 hrs · 43,031 cycles
INTERNAL FUSEAGE SKIN CORRODED AT BS 1238, STRINGERS 32-33L.
Part: SKIN — CRACKED (BS 544-566) · airframe 89,630 hrs · 43,031 cycles
CRACK ON SKIN BETWEEN BS 544 - 566, STRINGERS 30 TO 37L.
Part: FIRE WARNING — FALSE ACTIVATION (NR 2 ENGINE) · airframe 89,421 hrs · 42,919 cycles
THE LEFT ENGINE FIRE WARNING, THE ENGINE WAS SHUTDOWN IAW THE ENGINE SECURING CHECKLIST. THE FIRE WARNING EXTINGUISHED AFTER THE DISCHARGE OF THE SECOND FIRE BOTTLE. THE OIL PRESSURE WAS NORMAL. THE ENGINE WINDMILLED FOR APPROXIMATELY 28 MINUTES.
Part: STRINGER — CORRODED (BS 1809-1829) · corrosion level 2 · airframe 89,300 hrs · 42,853 cycles
A STRINGER 32, BS 1809- 1829 WAS CORRODED BEYOND SRM LIMITS. REPLACED THE STRINGER IAW SRM 51-40-02 AND DRAWING 148T3000.
Part: STRINGER — CORRODED (BS 1809) · corrosion level 2 · airframe 89,300 hrs · 42,853 cycles
STRINGER 32L, BS 1809 WAS FOUND CORRODED BEYOND SRM LIMITS. REPLACED THE STRINGER IAW SRM 51-40-02, AND DRAWING 148T3000.
2015
Part: ENGINE — POWER LOSS (RIGHT) · airframe 85,691 hrs · 40,939 cycles
TAKEOFF CANCELLED AT 70 KNOTS DUE TO POWER LOSS RT ENG. PRIOR TO POWER LOSS, ENG PARAMETERS LOOKED NORMAL.
2014
Part: SKIN — CORRODED (BS 1087) · airframe 84,627 hrs · 40,388 cycles
FUSELAGE INNER SKIN CORRODED BS 1087 S31L.
Part: STRINGER — CORRODED (BS 1542-1582) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 38R BS 1542-1582 CORRODED.
Part: STRINGER — CORRODED (BS 1329-1417) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 35L, CORRODED BETWEEN BS 1329 - 1417.
Part: STRINGER — CORRODED (BS 1510-1540) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 26L CORRODED BETWEEN BS 1510.5 - 1540.
Part: STRINGER — CRACKED (BS 1490-1540) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 35L, CRACKED THREE INCHES BETWEEN BS 1490 - 1540.
Part: SKIN — CORRODED (BS 1087-1109) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY SKIN CORRODED BETWEEN BS 1087 AND 1109 S39L AND 39R.
Part: STRINGER — CORRODED (BS 1285-1307) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 37L CORRODED BETWEEN BS 1285 AND 1307.
Part: STRINGER — CORRODED (BS 1285-1307) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 36L CORRODED BETWEEN BS 1285 AND 1307.
Part: STRINGER — CORRODED (BS 1536) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 37R CORRODED BS 1536.
Part: STRINGER — CORRODED (BS 1535) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 37L CORRODED BS 1535.
Part: SPLICE — CORRODED (BS 434) · airframe 84,627 hrs · 40,388 cycles
FWD CARGO BAY SECTION 43 FWD CARGO SPLICE CORRODED BS 434 S33R.
Part: STRINGER — CORRODED (BS 1307-1329) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 36L CORRODED BETWEEN BS 1307 AND 1329.
Part: STRINGER — CORRODED (BS 1395-1417) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 31R CORRODED BETWEEN BS 1395 - 1417.
Part: STRINGER — CORRODED (BS 1395-1417) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 32R CORRODED BETWEEN BS 1395 AND 1417.
Part: STRINGER — CORRODED (BS 1241-1263) · airframe 84,627 hrs · 40,388 cycles
AFT LOWER CARGO BAY STRINGER 35L CORRODED BETWEEN BS 1241 AND 1263.
Part: WEB — CORRODED (BS 1395) · airframe 84,627 hrs · 40,388 cycles
AFT LOWER CARGO BAY WEB CORRODED BS 1395 BETWEEN STRINGERS 38L AND 38R.
Part: STRINGER — CORRODED (BS 1442-1502) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 36L CORRODED BS 1442 AND 1502.5.
Part: STRINGER — CORRODED (BS 1263) · airframe 84,627 hrs · 40,388 cycles
AFT LOWER CARGO BAY STRINGER 39R CORRODED AT BS 1263.
Part: STRINGER SPLICE — CORRODED (BS 1351-1373) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER SPLICE 31R CORRODED BETWEEN BS 1351 AND 1373.
Part: FLOORBEAM — BROKEN (BS 1461) · airframe 84,627 hrs · 40,388 cycles
AFTCARGO BAY FLOORBEAM WEB BROKEN 2.5 INCHES AND 3 INCHES, BS 1461, LBL 3 AND RBL 4.
Part: STRINGER — CORRODED (BS 1439-1461) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 30R CORRODED BETWEEN BS 1439 AND 1461.
Part: STRINGER — CORRODED (BS 1241-1263) · airframe 84,627 hrs · 40,388 cycles
AFT LOWER CARGO BAY STRINGER 34L CORRODED BS 1241 AND 1263.
Part: STRINGER — CORRODED (BS 1439-1461) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 29R CORRODED BETWEEN BS 1439 AND 1461.
Part: SKIN — CORRODED (CARGO BAY) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY SKIN CORRODED.
Part: STRINGER — CORRODED (BS 1263) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY TRINGER 32L CORRODED BS 1263.
Part: STRINGER — CORRODED (BS 1109) · airframe 84,627 hrs · 40,388 cycles
AFT LOWER CARGO BAY STRINGER 33L CORRODED BS 1109.
Part: STRINGER — CORRODED (BS 1461-1480) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY STRINGER 33R CORRODED BETWEEN BS 1461 AND 1480.
Part: FLOORBEAM — CORRODED (BS 1219) · airframe 84,627 hrs · 40,388 cycles
AFT CARGO BAY FLOORBEAM LOWER TEE CORRODED BS 1219, WL 200, LBL 13.
Part: STRINGER — CORRODED (BS 1307-1329) · airframe 84,627 hrs · 40,388 cycles
AFT LOWER CARGO BAY STRINGER 33L CORRODED BETWEEN BS 1307 AND 1329.
Part: STRINGER — CORRODED (BS 1173) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 28L CORRODED BS 1173.
Part: STRINGER — CORRODED (BS 1109) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 32L CORRODED BS 1109.
Part: STRINGER FITTING — CRACKED · airframe 84,627 hrs · 40,388 cycles
LEFT UNDER WING STRINGER FITTING CRACKED 0.600 LENGTH.
Part: FLOORBEAM — CORRODED (BS 1153) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY CARGO FLOORBEAM UPPER HORIZONTAL FLANGE CORRODED BS 1153, RBL 25 & RBL 39.
Part: STRINGER SPLICE — CORRODED (BS 434) · airframe 84,627 hrs · 40,388 cycles
SECTION 43, FWD CARGO STRINGER SPLICE 33L CORRODED BS 434.
Part: STRINGER — CORRODED (BS 1405) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 39R CORRODED BS 1405.
Part: STRINGER — CORRODED (BS 1395) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 39L CORRODED BS 1395.
Part: STRINGER — CORRODED (BS 434-544) · airframe 84,627 hrs · 40,388 cycles
LOWER CARGO BAY SECTION 43, STRINGER 32L CORRODED, BS 434 - 544.
Part: FLOORBEAM — CORRODED (BS 1219) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY CARGO FLOORBEAM UPPER HORIZONTAL FRAME CORRODED BS 1219, LBL 8 - 20
Part: STRINGER — CORRODED (BS 1087-1109) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 31L CORRODED BETWEEN BS 1087 - 1109.
Part: STRINGER SPLICE — CORRODED (BS 434) · airframe 84,627 hrs · 40,388 cycles
LOWER CARGO BAY SECTION 43, STRINGER SPLICE 31L CORRODED BS 434.
Part: STRINGER SPLICE — CORRODED (BS 434) · airframe 84,627 hrs · 40,388 cycles
LOWER CARGO BAY SECTION 43, STRINGER AND SPLICE 35L CORRODED BS 434.
Part: STRINGER FITTING — CORRODED (BS 1153-1175) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY STRINGER 28L, FITTING CORRODED BETWEEN BS 1153 - 1175.
Part: SKIN — CORRODED (BS 1241-1263) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY SKIN CORRODED BETWEEN BS 1241 - 1263, S30-32L.
Part: INTERCOSTAL — CORRODED (BS 1153-1175) · airframe 84,627 hrs · 40,388 cycles
AFTER CARGO BAY INTERCOSTAL CORRODED FROM BS 1153 - 1175.
Part: SKIN SPLICE — CORRODED (BS 434) · airframe 84,627 hrs · 40,388 cycles
LOWER CARGO BAY SECTION 43, FWD SKIN SPLICE CORRODED S34L BS 434.
Part: SKIN — CORRODED (BS 1263-1285) · airframe 84,627 hrs · 40,388 cycles
FUSELAGE EXTERIOR LOWER SKIN CORRODED FROM BS 1263 - 1285.
2013
Part: SILL — CRACKED (EMERGENCY EXIT) · airframe 80,220 hrs · 38,118 cycles
DURING ROUTINE C-CHECK INSPECTION, LT OVERWING EMERGENCY EXIT DOOR HATCH LOWER MAIN SILL HAS A CRACK 0.400" LENGTH AT STA 883.500, REF NR N0390.
Part: ANGLE — CRACKED (LT NACELLE) · airframe 80,220 hrs · 38,118 cycles
DURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE. LT CORE COWL LOWER ANGLE CRACKED AT NAC STA 293.50, REF NR N0306.
Part: SKIN — CORRODED (BS 1351) · airframe 80,220 hrs · 38,118 cycles
DURING ROUTINE C-CHECK INSPECTION, FUSELAGE INTERNAL SKIN CORRODED BETWEEN STA 1351 AND 1373, S33L.
Part: SKIN — CRACKED (BS 1387) · airframe 80,220 hrs · 38,118 cycles
DURING ROUTINE C-CHECK INSPECTION, FUSELAGE EXTERIOR SKIN CRACKED BS 1387 S34-35L.
2012
Part: SKIN — CORRODED (FUSELAGE) · 37,348 cycles
FOUND CORROSION AT BODY STATION 764 BETWEEN STRINGER 34R AND 36R.
Part: SKIN — DAMAGED (BS 1373) · corrosion level 2 · airframe 77,998 hrs · 37,055 cycles
FUSELAGE SKIN DAMAGE AT BS 1373 BETWEEN S19 AND 20 LEFT.
2011
Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
CORROSION INSIDE OF BULK CARGO DOOR LWR THRESHOLD FWN LIGHTENING HOLE AT STA 1423 AND AFT LIGHTENING HOLE AT STA 1455. REPLACED "T" CAP AND SPLICE STRAP IAW B767 SRM.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
LWW T FITING CORRODED AROUND FASTENER HOLE. REPLACED T FITTING IAW B767 SRM AND REA 46868REA09.
Part: GUSSET — CHAFED (NR 2 PYLON) · airframe 49,655 hrs · 38,568 cycles
NR 2 PYLON UPPER SKIN LT AND RT FWD GUSSETS CHAFED. REPAIRED IAW B767 SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 8L CRACKED AT STA 676. REPAIRED IAW B767 SRM.
Part: BOLT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
BOLTS 10, 11, 12, 13 REQUIRE REPLACEMENT IN THE LOWER LEG OF THE LT PICKLE FORK. REPLACED BOLTS IAW REA 46868REA07.
Part: STRAP — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
RT FAILSAFE STRAP CRACKED. REPAIRED IAW REA 46868REA01.
Part: SKIN — CRACKED (NR 2 PYLON) · airframe 49,655 hrs · 38,568 cycles
NR 2 PYLON UPPER FWD SKIN CRACKED. REPAIRED IAW B767 SRM.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
RIGHT T FITTING COMMON TO FAILSAFE STRAP CORRODED AT FWD HOLE. REPLACED FITTING IAW B767 SRM AND REA 46868REA01.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 17L CRACKED AT STA 676. REPAIRED STRINGER IAW B767 SRM AND REA 46854REA04.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 13L CRACKED AT STA 676. REPAIRED STRINGER IAW B767 SRM AND REA 46854REA04.
Part: FITTING — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
S3R SHEAR CLIP CRACKED AT STA 1654.5. REPLACED SHEAR CLIP IAW B767 SRM.
Part: STRAP — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
LT FAILSAFE STRAP CRACKED. REPLACED FAILSAFE STRAP IAW REA 46868REA09.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
THE "I" BEAM AT STA 955 RBL 85 CORRODED. REPAIRED IAW REA 46868REA08.
Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
RIGHT PRESSURE DECK WEB CORRODED. REPLACED WEB IAW REA 46868REA01.
Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
MAIN CARGO DOOR MAIN LATCH FITTING NR 9 CORRODED IN BORE FOR LATCH CAM PIN. REPAIRED IAW REA 46854REA06.
Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
PRESSURE DECK WEB STA 977 LT WHEEL WELL HAS DOUBLE DRILLED AND PLUGGED HOLES. REPAIRED IAW REA 46854REA07.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 10L CRACKED AT BS 676. REPAIRED IAW B767 SRM.
Part: SKIN — CHAFED (NR 2 PYLON) · airframe 49,655 hrs · 38,568 cycles
NR 2 PYLON L/E CHAFED. REPAIRED IAW B767 SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 11 CRACKED AT BS 676. REPAIRED IAW B767 SRM.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 49,655 hrs · 38,568 cycles
RIGHT NLG CHORD CRACKED AT STA 287 RBL 25. REPAIRED IAW B767 SRM.
Part: STRAP — DAMAGED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
MACHINED STRAP AT STA 977 LT WHEEL WELL PRESSURE PANEL DOUBLE DRILLED. REPAIRED IAW REA 46854REA07.
Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
PRESSURE DECK WEB CORRODED AT LEFT PICKLE FORK UPPER SIDE. REPLACED WEB IAW REA 46868REA09.
Part: STIFFENER — CRACKED (NACELLE) · airframe 49,655 hrs · 38,568 cycles
INBOARD HYD BAY INSIDE STIFFENER CRACKED ON INBOARD AFT END. REPAIRED IAW B767 SRM.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 49,655 hrs · 38,568 cycles
LEFT NLG CHORD CRACKED AT STA 287 BL 25. REPAIRED IAW B767 SRM.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
LEFT KEEL BEAM CORRODED AT STA 1032. REPAIRED IAW B767 SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 9L CRACKED AT STA 676.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
FITTING AT STA 1082 FWD BULKHEAD LBL 11.5 CORRODED ON LOWER FLANGE. REPAIRED IAW B767 SRM.
Part: SUPPORT BRACKET — BROKEN (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
BROKEN SUPPORT BRACKET LT SLANT PANEL AREA AT STA 566. REPAIRED IAW B767 SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
STRINGER 19L CRACKED AT STA 676. REPAIRED IAW B767 SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 49,655 hrs · 38,568 cycles
TWO CRACKS IN FUSELAGE SKIN AT BS 1654.5 BETWEEN STRINGERS 2R AND 5R. REPAIRED IAW B767 SRM.
Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
MAIN CARGO DOOR LATCH FITTING NR 5 CORRODED IN BORE FOR LATCH CAM PIN. REPAIRED IAW REA 46854REA06.
Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 49,655 hrs · 38,568 cycles
MAIN CARGO DOOR MAIN LATCH FITTING NR 3 CORRODED IN BORE FOR LATCH CAM PIN. REPAIRED IAW REA 46854REA06.
2009
Part: RIB — CORRODED (RT WING) · airframe 72,249 hrs · 34,610 cycles
CORROSION MIGRATING OUT FROM BENEATH L/E RIB AT WING LOWER SPAR NR 8 SLAT INBOARD AUX TRACK INBOARD SUPPORT RIB.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 72,249 hrs · 34,610 cycles
CRACKED STRINGER AFT OF AFT PRESS BULKHEAD APPROX S35L BETWEEN STA BS 1620-1605.
Part: RIB — CORRODED (RT WING) · airframe 72,249 hrs · 34,610 cycles
CORROSION MIGRATING OUT FROM BENEATH L/E RIB AT WING LWR SPAR NR 8 SLAT INBOARD AUX TRACK.
2008
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 69,570 hrs · 33,584 cycles
EMERGENCY LIGHT NR 9023 IN SUPERNUMERARY INOPERATIVE, SECOND LIGHT INBOARD OF MAIN ENTRY DOOR. REMOVED AND REPLACED M736 BATTERY PACK WITH SPARE BATTERY PACK M734 IAW B767 MM 33-51-07. OPS CHECKED GOOD.