N767TW

Part: SKIN — DENTED (APU DOOR) · airframe 71,141 hrs · 64,373 cycles

REPAIRED APU DOOR NONPRESSURIZED OUTER SKIN AT 2 LOCATIONS, FROM B/S 1098.5 TO 1108, AND FROM B/S 1113.5 TO B/S 1129.5 AT CENTER SECTION, DUE TO DENTS OUT OF LIMITS.

Part: SHEAR BEAM — CRACKED (RT MLG WW) · airframe 71,141 hrs · 64,373 cycles

RIGHT WHEEL WELL SHEAR BEAM REPAIRED DUE TO CRACK.

Part: SKIN — DENTED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO DENTS OUT OF LIMITS.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.

Part: SKIN — ELONGATED (NR 2 ENGINE) · airframe 71,141 hrs · 64,373 cycles

REPLACED RT WING TO NR 2 ENGINE AFT FAIRING IB SKIN PANEL DUE TO ELONGATED HOLES.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

REPAIRED MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE MAIN CARGO CABIN FLOOR BEAM UPPER CHORD DUE TO CORROSION.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE FORWARD GALLEY DOOR, UPPER AFT FRAME, DUE TO CRACK.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE AFT CARGO COMPARTMENT DOOR LOWER BEAM REPAIRED DUE TO CRACK.

Part: SKIN PANEL — DELAMINATED (RT WING) · airframe 71,141 hrs · 64,373 cycles

REPAIRED RIGHT WING TRAILING EDGE LOWER FIXED PANEL DUE TO DELAMINATION.

Part: SPAR — CORRODED (WING CENTER SEC) · airframe 71,141 hrs · 64,373 cycles

WING CENTER SECTION REAR SPAR LOWER CHORD WAS REPAIRED DUE TO CORROSION.

Part: FRAME — DENTED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE MAIN CARGO CABIN FITTING UNDERNEATH LONGITUDINAL FLOOR BEAM DUE TO MISSING MATERIAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

STRINGER SECTION WAS REPAIRED DUE TO CORROSION.

Part: SPOILER — DELAMINATED (LEFT) · airframe 71,141 hrs · 64,373 cycles

REPAIRED LEFT WING SPOILER #3 DUE TO DELAMINATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE AFT PRESSURE BULKHEAD WEB DUE TO CRACK.

Part: SKIN — CORRODED (BS 339-327) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO CORROSION.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE STRINGER REPAIRED DUE TO CRACK.

Part: SKIN — DENTED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO DENTS OUT OF LIMITS.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED NONPRESSURIZED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: SKIN — DAMAGED (MID FLAP) · airframe 71,141 hrs · 64,373 cycles

REPAIRED RIGHT WING OUTBOARD MID FLAP TRAILING EDGE LOWER SKIN DUE TO SHARP EDGE.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: WINDOW FRAME — CORRODED (CABIN) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE WINDOW FRAME AT TWO LOCATIONS, FROM B/S 688 TO 703.25, AND FROM B/S 727+3 TO 727+18.25, DUE TO CORROSION.

Part: WEB — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE MAIN CARGO CABIN LOWER JAMB FLOOR WEB DUE TO CORROSION.

Part: FITTING — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPLACED FUSELAGE BULKHEAD LEFT FITTING DUE TO CORROSION. ALSO REPAIRED FUSELAGE SKIN AND DOUBLER DUE TO CRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM WEB AND REPLACED PRODUCTION DOUBLER DUE TO CORROSION.

Part: SKIN — DENTED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE STRINGER REPAIRED DUE TO CORROSION.

Part: SKIN — CANNING (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO OIL CANNING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SHEAR TIE REPAIRED DUE TO CORROSION.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED -579 STIFFENER AND PERFORMED BLEND OUT IN THE AFT PRESSURE BULKHEAD "Y" CHORD DUE TO CORROSION. REPAIRED AFT PRESSURE BULKHEAD WEB AND RADIAL STIFFENER AND REPAIRED FUSELAGE SKIN DUE TO ACCESS TO REPAIR AREA.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: SKIN — DENTED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: SKIN — DENTED (ZONE 800) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FORWARD CARGO COMPARTMENT DOOR EXTERNAL SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: SKIN — DENTED (BS 240-255) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

REPAIRED MAIN CARGO CABIN TRANSVERSAL BEAM DUE TO CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 675-663) · airframe 71,141 hrs · 64,373 cycles

REPAIRED MAIN CARGO CABIN FLOOR SUPPORT CHANNEL DUE TO CORROSION.

Part: FAIRING — CRACKED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE WING TO BODY FAIRING FORMER REPAIRED DUE TO CRACK.

Part: SKIN — CRACKED (ZONE 100) · airframe 71,141 hrs · 64,373 cycles

REPAIRED FUSELAGE SKIN SECTION DUE TO CRACK.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.

Part: SKIN — OUT OF LIMITS (BS 320-365) · airframe 71,141 hrs · 64,373 cycles

LOWER FUSELAGE E/E COMPARTMENT CUTOUT SKIN REPAIRED DUE TO SKIN HOLE EDGE DISTANCE OUT OF LIMITS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

CARGO CABIN FLOOR SUPPORT CORRODED.

Part: SPOILER — DELAMINATED (NR 3) · airframe 71,141 hrs · 64,373 cycles

REPAIRED LEFT WING NR 3 SPOILER DUE TO DELAMINATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

MAIN CABIN CARGO FLOOR SUPPORT CHANNEL CORRODED.

Part: SKIN PANEL — DELAMINATED (RT WING) · airframe 71,141 hrs · 64,373 cycles

RIGHT WING TRAILING EDGE LOWER PANEL DELAMINATED

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,141 hrs · 64,373 cycles

MAIN CARGO CABIN SUPPORT STRAP CRACKED AT MAIN DOOR LOWER SECTION.

Part: DOOR — NOT CLOSED (L1) · airframe 70,448 hrs · 63,977 cycles

AIRCRAFT FAILED TO PRESSURIZE ON CLIMB-OUT.

Part: SKIN — DELAMINATED · airframe 70,063 hrs · 63,743 cycles

DURING A-CHECK INSPECTION, FOUND TAIL CONE WITH AN APPROXIMATELY 8 INCH BY 7 INCH SECTION OF DELAMINATION.

Part: CHANNEL — CORRODED (RT WING)

RT WING TRAILING EDGE CAVITY UPPER FIXED PANEL CHANNEL CORRODED.

Part: CHANNEL — CRACKED (MLG)

RT MAIN LANDING GEAR CHANNEL.

Part: WEB — WORN (HORIZONTAL STAB)

RT HORIZONTAL STABILIZER TRAILING EDGE, HINGE RIB, WEB WITH WEAR.

Part: SKIN — DELAMINATED (RT WING AILERON)

RT WING, AILERON (PN-65-46454-2) SN 305, SKIN DELAMINATED.

Part: SKIN — DELAMINATED (SPOILER)

RT WING, FLIGHT SPOILER NR 7 UPPER SURFACE DELAMINATED.

Part: CARRIAGE — DAMAGED (TE FLAPS)

LT AND RT INBOARD MIDFLAP (PN 6571902-11/12) CARRIAGE ASSY PN 65-52246-9/10 AND 11/12 DAMAGED.

Part: SKIN — DELAMINATED (RT WING SPOILER)

RT WING, IB GROUND SPOILER (PN 65-79952-6) SN MA358, DELAMINATED.

Part: RIB — CRACKED (RT WING)

RT WING, FSS 266 LEADING EDGE RIB CRACKED.

Part: SKIN — CORRODED (NR 2 NACELLE)

NR 2 ENGINE OB COWLING EXTERNAL SKIN CORRODED.

Part: ANGLE — CORRODED (RT WING)

RT WING, TRAILING EDGE - RSS486, ANGLE CORRODED.

Part: RIB — CRACKED (RT WING)

RT WING, FSS 263 LEADING EDGE RIB CRACKED.

Part: CHANNEL — CRACKED (LT MLG)

LT MAIN LANDING GEAR CHANNEL, CRACKED.

Part: THRUST BEARING — DAMAGED (RT AND LT WING)

RT AND LT WING, OB MIDFLAP THRUST BEARING DAMAGED.

Part: FLAP TRACK — CORRODED (LT WING)

LT WING, FLAP TRACK NR 2 CORRODED.

Part: SPLICE — CRACKED (RT WING)

RT WING, REAR SPAR LOWER CHORD SECTION, OUTBOARD SPLICE PN 6550821144 CORRODED AND CRACKED.

Part: SPAR — CRACKED (RT WING)

RT WING, REAR SPAR LOWER CHORD SECTION, FROM WBL 113 INCHES TO WBL 130 INCH OB SPLICE PN 65-50821-142.

Part: SEAL — CRACKED (HORIZONTAL STAB)

LT HORIZONTAL STABILIZER BLADE SEAL CRACKED.

Part: PANEL — DELAMINATED (RT WING)

RT WING, FIXED PANEL PN 65-50820-142, TMC-284 DELAMINATED.

Part: LAMP — LOOSE (COCKPIT) · airframe 68,368 hrs · 62,677 cycles

SMOKE/ELEC FUMES FROM MASTER CAUTION ANNUNCIATOR PANEL ON CAPTAINS SIDE. STOPPED AFTER 2 MINUTES.FOUND GLARESHIELD FLOURESCENT TUBE NEAR CAPTAINS MASTER CAUTION PANEL DISPLACED FROM SOCKET. THIS ARCED WITH SLIGHT MOVEMENT. CLEANED SOCKET AND TUBE AND RESEATED AND SECURED. OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (L/E SLAT)

LEFT WING, SLAT NR 1, PN 65-46421-165, SN 132 UPPER SKIN DELAMINATED.

Part: LONGERON — CRACKED (NR 2 PYLON)

ENGINE NR 2, FORWARD FIREWALL-LONGERON, PN 65-53558-54 CRACKED.

Part: SKIN — DELAMINATED (T/E FLAP)

RIGHT WING, OUTBOARD AFT FLAP PN 65-46435-236, SN 333, UPPER SKIN DELAMINATED.

Part: SKIN — DELAMINATED (T/E FLAP)

RIGHT WING, INBOARD FORE FLAP, PN 65-46430, SN BN803, UPPER SKIN DELAMINATED.

Part: SKIN — DELAMINATED (T/E FLAP)

LEFT WING, INBOARD AFT FLAP, PN 65ND27301-1, SN BN-2. LOWER AND UPPER SKIN DELAMINATED.

Part: SKIN — DELAMINATED (T/E FLAP)

RIGHT WING, INBOARD AFT FLAP PN 65ND-27301-2, SN BN2, LOWER AND UPPER SKIN DELAMINATED.

Part: SKIN — DELAMINATED (SPOILER)

RIGHT WING, FLIGHT SPOILER NR 8 PN 65-79952-7, MA-532, UPPER SKIN DELAMINATED.

Part: SKIN — DELAMINATED (SPOILER)

LEFT WING, GROUND SPOILER NR 4, PN 6579952-5 DHL, MD-364 UPPER SKIN DELAMINATED.

Part: SKIN — DELAMINATED (FUSELAGE)

FUSELAGE SKIN FROM BS 847 TO BS 867 BETWEEN STR 22R AND STR 23R WITH DELAMINATION.

Part: BULKHEAD — CRACKED (FUSELAGE)

BULKHEAD WEB SECTION CRACKED, AT LBL 10, BETWEEN WL 237.25 AND WL 230.5.

Part: DOUBLER — DELAMINATED (FUSELAGE)

FUSELAGE SKIN DOUBLER FROM BS 639 TO BS 663 BETWEEN STR 9L AND 10L WITH DELAMINATION.

Part: SKIN — DEBONDED (FUSELAGE)

FUSELAGE SKIN SECTION FROM BS 330 TO BS 350 BETWEEN STR 21L AND 23L WITH DISBONDING.

Part: RIB — CRACKED (LT WING)

LEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 394, NR2 SLAT OUTBOARD MAIN TRACK SUPPORT.

Part: BULKHEAD — CRACKED (FUSELAGE)

BULKHEAD WEB SECTION CRACKED, RBL 10, BETWEEN WL 237.25 AND WL 230.5

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE SKIN FROM BS 500B+6 TO BS 500B+10 AT STR 19R UPPER SKIN WITH CRACK INDICATION.

Part: SKIN — DELAMINATED (FUSELAGE)

FUSELAGE SKIN FROM BS 950 TO BS 955 BETWEEN STR 5R AND STR 6R DELAMINATED.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN AT BS 340 AT STR 24L WITH CORROSION.

Part: SKIN — DELAMINATED (FUSELAGE)

FUSELAGE SKIN SECTION FROM BS 635 TO BS 663 BETWEEN STR 14R AND 15R WITH DELAMINATION.

Part: RIB — CRACKED (LT WING)

LEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 267, NR3 SLAT INBOARD MAIN TRACK SUPPORT.

Part: DOUBLER — DEBONDED (FUSELAGE)

FUSELAGE SKIN FROM BS 335 TO BS 350 BETWEEN STR 24L AND STR 25L WITH DOUBLER DEBONDED.

Part: PROXIMITY SWITCH — OUT OF ADJ (NR 3 LE FLAP) · airframe 65,659 hrs · 61,028 cycles

WITH FLAPS SELECTED TO FLAP 1, L/E FLAP LIGHT REMAINED INTRANSIT ON FWD INSTRUMENT PANEL.