N36NE

Part: SKIN — DENTED (ZONE 100) · airframe 100,961 hrs · 16,223 cycles

REASSESS DENT 20 RH FUSELAGE STATION 368+6INCHES STRINGER 26+4INCHES. FOUND TO BE OUTSIDE OF ALLOWABLE DAMAGE LIMITS IAW B767-300 SRM 53-00-01-1A-1 REV 128.

Part: STRINGER — DENTED (ZONE 100) · airframe 100,961 hrs · 16,223 cycles

DENT #13, REPAIRED ON STRINGER 19L BETWEEN STATION 368-388 IAW B767-300 SRM 53-00-03-2R-1 REV128.

Part: SKIN — DEBONDED (ZONE 500) · airframe 100,961 hrs · 16,223 cycles

DISBOND AROUND HOIST POINT ATTACH POINT L/H WING UPPER SURFACE.

Part: SKIN — GOUGED (ZONE 300) · airframe 100,961 hrs · 16,223 cycles

GOUGES ON LH H-STAB LOWER INSPAR SKIN AT S-2 AND STA 226.605 (RIB 12 CENTERLINE).

Part: CASE — CORRODED (NR 2 ENGINE FAN) · corrosion level 2 · airframe 100,961 hrs · 16,223 cycles

DURING C CHECK, CORROSION WAS FOUND ON THE NR 2 ENGINE FWD AND AFT CASE AROUND THE EXTERIOR AND INTERIOR SKIN. IT WAS FOUND TO BE OUT OF REPAIRABLE LIMITS FOR THE FWD FAN CASE PER AMM 72-32-00 AND OUT OF FLYABLE LIMITS PER AMM 72-00-00. THE ENGINE WAS REMOVED AND SENT FOR REPAIR. WHILE AT GA TELESIS IT WAS FOUND BY THE ENGINE SHOP THAT THE AFT FAN CASE WAS ALSO BEYOND REPAIR. THE FWD AND AFT FAN CASE WERE CHANGED AT GA TELESIS ON WO#1155. AFTER REPAIR THE ENGINE WAS SENT BACK AND INSTALLED BACK ON N36NE AT THE #2 POSITION.

Part: SKIN — DENTED (ZONE 100) · airframe 100,961 hrs · 16,223 cycles

DENT NR 12 LT FUSELAGE STATION 368 +8 INCHES, STRINGER 17L +4 INCHES. DURING SCHEDULED MAINTENANCE, TWO DENT DAMAGES WERE FOUND COMMON TO THE LOWER FUSELAGE SKIN BETWEEN STA 368 - STA 390 AND STGR 17L - STGR 19L..

Part: SPAR — DAMAGED (ZONE 300) · airframe 100,981 hrs · 16,223 cycles

DURING C-CHECK AT YHM, THE RH HORIZONTAL STABILIZER AUXILIARY SPAR WEB NEAR OUTBOARD CLOSURE RIB AT HSBL 357.442 WAS FOUND TO HAVE TOOLING MARKS, AFTER BLENDING OUT OF THE DAMAGED AREAS, TWO CRACKS OF 0.300" AND 0.250" LONG WERE FOUND.

Part: NONE — NONE · airframe 99,827 hrs · 15,883 cycles

DURING SERVICE CHCK IT WAS NOTED THE EMERGENCY LIGHT DO NOT WORK. REPLACED 4 EMERGENCY LT BATTERY IAW 33-51-07. OPS CHECK GOOD. A/C RETURN TO SERVICE.

Part: WIRE HARNESS — DAMAGED (TEMP CONTROL) · airframe 99,748 hrs · 15,840 cycles

TEMP CONTROL - NO TEMP CONTROL WITH ANY CONTROLS. CORRECTIVE ACTION: FOUND WIRE BUNDLE W1200-1204 DAMAGE, REPAIRED WIRE BUNDLE ACCORDING WITH STANDARD WIRE PRACTICE MANUAL. OPS CHECK NORMAL

Part: ACCESS DOOR — MISSING (RT NACELLE) · airframe 99,652 hrs · 15,796 cycles

UPON PREFLIGHT WALK-AROUND MAINTENANCE FOUND R/H ENGINE PYLON INBOARD NACELLE STRUT ACCESS DOOR MISSING. MAINTENANCE TRANSFERRED TO DMI 36N-21-0002, CDL 54-53-02. EXP 07/15/21 PLACARD INSTALLED PER GMM-002 UPDATED.

Part: CONTROL MODULE — FAILED (LAVATORY) · airframe 99,613 hrs · 15,783 cycles

AFT LAV LIGHT ILLUMINATED AND WILL NOT CLEAR.

Part: PANEL — DELAMINATED (CARGO BAY) · airframe 99,613 hrs · 15,783 cycles

FWD CARGO PANEL HAS SEVERAL DELAMINATION SPOTS (P/N 453T1822-44).

Part: SUPPORT BRACKET — CUT (NR 2 COWLING) · airframe 99,613 hrs · 15,783 cycles

NR 2 ENGINE NOSE COWL, AFT WEB, OTBD LOWER SUPPORT BRACKET IS CUT.

Part: CONTROL UNIT — DAMAGED (ZONE 200) · airframe 99,613 hrs · 15,783 cycles

DAMAGED ECLU FOUND IN THE FWD GALLEY.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 99,613 hrs · 15,783 cycles

FORWARD CARGO DOOR CUTOUT, LOWER SILL UPPER SURFACE HAS CORROSION (REPAIRED).

Part: LINK — WORN (LT AILERON) · airframe 99,613 hrs · 15,783 cycles

LT INBD AILERON OTBD PCA HAS PLAY AT HANGAR ATTACH POINT.

Part: SEAL — TORN (ZONE 600) · airframe 99,613 hrs · 15,783 cycles

SEAL ON PANEL 661BB IS TORN.

Part: PANEL — DAMAGED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

PANEL 122AW HAS COMPOSITE DAMAGE.

Part: SEAL — TORN (RT MLG DOOR) · airframe 99,613 hrs · 15,783 cycles

SEAL IS TORN ON THE FORWARD END OF THE RT MLG TRUNNION DOOR.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 99,613 hrs · 15,783 cycles

LH INBD UPPER FLAP, INTERNAL SKIN HAS COMPOSITE DELAMINATION (REPAIRED).

Part: SEAL — WORN (RT WING) · airframe 99,613 hrs · 15,783 cycles

SEAL ON LT WING PANEL 561BB IS WORN.

Part: BUSHING — MISSING (TE FLAP) · airframe 99,613 hrs · 15,783 cycles

FLAP FAIRING PANEL 671AB HAS A BUSHING MISSING FROM THE MOUNTING BRACKET.

Part: SEAL — WORN (TE FLAP) · airframe 99,613 hrs · 15,783 cycles

FLAP FAIRING PANEL 61AB HAS A WORN SEAL.

Part: PROBE — DAMAGED (PITOT/STATIC SYS) · airframe 99,613 hrs · 15,783 cycles

RT UPPER PITOT PROBE FAILED DETAILED INSPECTION (TIP OF PROBE IS FLARED).

Part: FRAME — CHAFED (NR 1 COWLING) · airframe 99,613 hrs · 15,783 cycles

NR 1 ENGINE OTBD CORE COWL INTERIOR 2ND FRAME IS CHAFFED (REPAIRED).

Part: THRUST REVERSER — DAMAGED (NR 1 ENGINE) · airframe 99,613 hrs · 15,783 cycles

NR 1 ENGINE OTBD T/R HALF ABLATIVE MATERIAL IS DAMAGED ON THE AFT SECTION 6" FROM THE EDGE (REPAIRED).

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 99,613 hrs · 15,783 cycles

FLOOR PANEL AT SEAT 25-27 RH SIDE IS DAMAGED.

Part: PLATE — CRACKED (FUSELAGE) · airframe 99,613 hrs · 15,783 cycles

AFT CARGO DOOR SILL PLATE IS CRACKED (REPAIRED).

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 99,613 hrs · 15,783 cycles

RT FWD OVERWING EMERGENCY EXIT DOOR HAS DAMAGE ON THE UPPER AFT CORNER.

Part: RUB STRIP — DAMAGED (RT MLG DOOR) · airframe 99,613 hrs · 15,783 cycles

RH MLG POP UP DOOR RUB/WEAR STRIP HAS A SECTION MISSING.

Part: HINGE — WORN (THRUST REVERSER) · airframe 99,613 hrs · 15,783 cycles

NR 1 ENGINE, INBD T/R NR 12 BLOCKER DOOR UPPER HINGE IS LOOSE / WORN.

Part: SEAL — TORN (TE FLAP) · airframe 99,613 hrs · 15,783 cycles

INBD FLAP FAIRING PANEL 671DB HAS A TORN SEAL.

Part: HINGE — WORN (THRUST REVERSER) · airframe 99,613 hrs · 15,783 cycles

NR 1 ENGINE INBD T/R NR 7 BLOCKER DOOR LOWER HINGE IS LOOSE/WORN.

Part: HINGE — WORN (THRUST REVERSER) · airframe 99,613 hrs · 15,783 cycles

NR 1 ENGINE, INBD TR NR 11 BLOCKER DOOR, LOWER HINGE WORN/LOOSE.

Part: SEAL — WORN (LE SLAT) · airframe 99,613 hrs · 15,783 cycles

NR 3 SLAT, OTBD LOWER TRAILING EDGE VERTICAL SEAL HAS FABRIC WORN AWAY.

Part: PANEL — DELAMINATED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

FILLET PANEL 193ML IS DELAMINATED ON THE INNER SURFACE. REPAIRED.

Part: INDICATOR — WORN (LAVATORY) · airframe 99,613 hrs · 15,783 cycles

FORWARD LH LAVATORY (FS3) WASTE COMPARTMENT TEMPERATURE INDICATOR NEEDS REPLACEMENT.

Part: SEAL — TORN (PANEL) · airframe 99,613 hrs · 15,783 cycles

LEFT FILLET PANEL 191EL HAS A TORN SEAL.

Part: SENSOR — FAILED (AC BAY) · airframe 99,613 hrs · 15,783 cycles

LEFT PACK STAND-BY TEMPERATURE SENSOR FAILED FUNCTIONAL CHECK.

Part: PANEL — DELAMINATED (CARGO BAY) · airframe 99,613 hrs · 15,783 cycles

CARGO PANEL HAS DELAMINATION SPOTS (REPAIRED)

Part: DOOR — PUNCTURED (FUELING) · airframe 99,613 hrs · 15,783 cycles

FUELING PANEL DOOR HAS A SMALL PUNCTURE ON THE INNER SURFACE. REPAIRED.

Part: HOUSING — WORN (LT WING TE FLAP) · airframe 99,613 hrs · 15,783 cycles

FLAP TORQUE TUBE CARRIER BEARING HAS UP & DOWN PLAY IN THE HOUSING (LH SIDE).

Part: RIB — GOUGED (RT WING) · airframe 99,613 hrs · 15,783 cycles

RH WING RIB FOUND GOUGED (REPAIRED).

Part: SIDEWALL PANEL — DAMAGED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

FWD CARGO PANEL HAS SEVERAL DELAMINATION SPOTS & A HOLE IN IT (REPAIRED).

Part: SIDEWALL PANEL — DAMAGED (AFT CARGO) · airframe 99,613 hrs · 15,783 cycles

AFT LOWER CARGO, FWD WALL HAS COMPOSITE DAMAGE (RH SIDE).

Part: FAIRING — CRACKED (RT WING) · airframe 99,613 hrs · 15,783 cycles

RH INBD FLAP FAIRING PANEL 671DB IS CRACKED ON THE AFT END IN TWO SPOTS (REPAIRED).

Part: PANEL — DELAMINATED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

R/H FILLET PANEL 194NR IS DELAMINATED ON INNER SURFACE (REPAIRED)

Part: SEAL — TORN (RT PANEL) · airframe 99,613 hrs · 15,783 cycles

RIGHT FILLET PANEL 196DR HAS A TORN SEAL.

Part: PANEL — DAMAGED (RT WING) · airframe 99,613 hrs · 15,783 cycles

RH WING LEADING EDGE PANEL HAS COMPOSITE DAMAGE. REPAIRED.

Part: SKIN — CORRODED (LT WING) · airframe 99,613 hrs · 15,783 cycles

CORROSION FOUND ON UPPER SKIN OF LEFT WING AT W.S. 292. (REPAIRED)

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 99,613 hrs · 15,783 cycles

PANEL 324BL HAS A DELAMINATION SPOT ON THE INSIDE OF THE PANEL.

Part: RETAINER — CHAFED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

ANGLE(SEAL RETAINER) CHAFED BEHIND PANEL 196DR.

Part: HOUSING — WORN (LT WING TE FLAP) · airframe 99,613 hrs · 15,783 cycles

FLAP TORQUE TUBE CARRIER BEARING BELOW NUMBER 6 SPOILER HAS UP/DOWN PLAY IN HOUSING.

Part: SKIN — CORRODED (HORZONTAL STAB) · airframe 99,613 hrs · 15,783 cycles

HORIZONTAL STABILIZER CENTER SECTION TORSION BOX EXTERNAL SURFACE IS CORRODED AT FWD RH SIDE.(REPAIRED)

Part: BEARING — WORN (LT TORQUE TUBE) · airframe 99,613 hrs · 15,783 cycles

FLAP TORQUE TUBE CARRIER BEARING BELOW NUMBER 6 SPOILER HAS UP/DOWN PLAY IN HOUSING.

Part: B-NUT — DAMAGED (OXYGEN LINE) · airframe 99,613 hrs · 15,783 cycles

CAPTAIN'S OXYGEN SUPPLY LINE B NUT THREADS ARE DAMAGED.

Part: DOOR SILL — GOUGED (FUSELAGE) · airframe 99,613 hrs · 15,783 cycles

UPPER SURFACE OF THE LOWER FORWARD CARGO DOOR SILL HAS SEVERAL AREAS OF LIGHT GOUGING.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 99,613 hrs · 15,783 cycles

GOUGE FOUND ON FUSELAGE SKIN BEHIND SLIDE PANEL 196ER.

Part: BRACKET — CRACKED (ZONE 400) · airframe 99,613 hrs · 15,783 cycles

OUTBOARD BRACKETS ON SKATE ANGLES ATTACHING PANEL 437DB ARE CRACKED AT THE HI-LOCS.

Part: BRACKET — CRACKED (ZONE 400) · airframe 99,613 hrs · 15,783 cycles

INBOARD BRACKETS ON SKATE ANGLES ATTACHING PANEL 437DB ARE CRACKED AT THE HI=LOCS.

Part: DOOR — DAMAGED (RT MLG) · airframe 99,613 hrs · 15,783 cycles

RT MLG DOOR HAS PUNCTURE DAMAGE (REPAIRED).

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

SUPPORT BRACKET CRACKED UNDER THE NOSE STEERING PULLY.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 99,613 hrs · 15,783 cycles

PANEL 198AR HAS DAMAGE ON THE INNER SURFACE (COMPOSITE REPAIR).

Part: DOOR — PUNCTURED (LT MLG) · airframe 99,613 hrs · 15,783 cycles

LT MLG DOOR HAS PUNCTURE DAMAGE (REPAIRED).

Part: FIRE SEAL — DAMAGED (THRUST REVERSER) · airframe 99,613 hrs · 15,783 cycles

NR 2 ENGINE OUTBOARD THRUST REVERSER UPPER FIRE SEAL IS DAMAGED.

Part: HINGE — WORN (LE SLAT) · airframe 99,613 hrs · 15,783 cycles

RT WING, NR 8 SLAT TAI DUCT DOOR AFT HINGES ARE WORN.

Part: CHANNEL — WORN (LE SLAT) · airframe 99,613 hrs · 15,783 cycles

RT SLAT NR 8, ANTI ICE DUCT HINGE GANG CHANNEL REQUIRES REPLACEMENT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 99,613 hrs · 15,783 cycles

SMALL AREA OF CORROSION ON THE FUSELAGE EXTERNAL SKIN UNDER RT FWD UPPER WING FILLET PANEL (192CR).

Part: ROD — FAILED (ZONE 300) · airframe 99,613 hrs · 15,783 cycles

EMPENNAGE PANEL 313AL STOW ROD WILL NOT STOW OPEN.

Part: BUSHING — WORN (TE FLAP) · airframe 99,613 hrs · 15,783 cycles

FLAP TORQUE TUBE ATTACH BRACKET DIAGONAL LINK HAS UP/DOWN PLAY AT BRACKET ATTACH POINT.

Part: PANEL — CHAFED (NR 1 PYLON) · airframe 99,613 hrs · 15,783 cycles

NR 1 PYLON PANEL 437AL IS CHAFED ON THE INTERIOR SIDE.

Part: DOOR SEAL — TORN (RT MLG DOOR) · airframe 99,613 hrs · 15,783 cycles

SEAL TORN ON RT MAIN LANDING GEAR DOOR ENCLOSURE.

Part: LONGERON CLIP — CRACKED (FUSELAGE) · airframe 99,613 hrs · 15,783 cycles

CLIP FROM BODY LONGERON CHORD TO SKIN AT STA 1746 LT STAB FUSELAGE CUTOUT IS CRACKED.

Part: HINGE — WORN (LE SLAT) · airframe 99,613 hrs · 15,783 cycles

RT WING, NR 8 SLAT TAI DUCT DOOR FWD HINGES ARE WORN.

Part: SKIN PANEL — CHAFED (ZONE 300) · airframe 99,613 hrs · 15,783 cycles

EMPENAGE PANEL 148T3150-1 CHAFED.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 99,613 hrs · 15,783 cycles

CAPTAIN'S AFT INBOARD SEAT TRACK HAS ELONGATED HOLES.

Part: RETAINER — BENT (PAX DOOR SEAL) · airframe 99,613 hrs · 15,783 cycles

FORWARD LEFT CABIN DOOR UPPER SEAL RETAINER IS BENT AND CRACKED.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 99,613 hrs · 15,783 cycles

CORROSION AROUND NUTPLATES AND NUTPLATE HOLES ON BOTH SIDES OF THE PANEL SUPPORT FASTENED TO KEEP PANEL.

Part: RETAINER — BENT (FWD CARGO DOOR) · airframe 99,613 hrs · 15,783 cycles

FORWARD LOWER CARGO DOOR, FWD UPPER CARGO SEAL RETAINER BENT AND GOUGED.

Part: LENS — CORRODED (BEACON)

CORROSION FOUND ON THE LOWER BEACON LIGHT FRAME.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 99,613 hrs · 15,783 cycles

FIRST OFFICER'S AFT INBOARD SEAT TRACK HAS ELONGATED HOLES.

Part: PROXIMITY SENSOR — FAULTED (ZONE 700) · airframe 99,613 hrs · 15,783 cycles

LANDING GEAR DOORS MAINTENANCE MESSAGE SHOWN ON EICAS, S264 SENSOR FAULT ON PSEU.

Part: DISPLAY — INOPERATIVE (ZONE 200) · airframe 99,586 hrs · 15,783 cycles

#2 FMS (TIMEOUT) MESSAGE & FMS WOULD NOT AUTO SEQUENCE ON THE POSITION REPORT PAGE.

Part: CURTAIN — TORN (RT WING) · airframe 99,586 hrs · 15,783 cycles

NR 5 SLAT TAI DUCT CURTAIN IS TORN.

Part: PROXIMITY SWITCH — FAILED (ZONE 700) · airframe 99,586 hrs · 15,783 cycles

AIR/GROUND DISAGREE

Part: SEAL — MISSING (LAVATORY SERVICE) · airframe 99,575 hrs · 15,776 cycles

FWD F1 LAVATORY WASTE DOOR MISSING UPPER AND LOWER SEALS.

Part: PACKING — LEAKING (VALVE STEM) · airframe 99,575 hrs · 15,776 cycles

#5 TIRE HAS A SLOW LEAK FOR THE VALVE STEM AT BASE.

Part: SEAL — MISSING (LAVATORY SERVICE) · airframe 99,575 hrs · 15,776 cycles

FWD F1 LAVATORY WASTE DOOR MISSING UPPER AND LOWER SEALS.

Part: LOCK — WORN (SEAT10K) · airframe 99,575 hrs · 15,776 cycles

SEAT LOCK IN SEAT 10K IS WORN.

Part: LOCK — WORN (SEAT 22C) · airframe 99,575 hrs · 15,776 cycles

SEAT LOCK IN SEAT 22C IS WORN.

Part: LOCK — WORN (SEAT 25H) · airframe 99,575 hrs · 15,776 cycles

SEAT LOCK IN SEAT 25H IS WORN.

Part: STATIC WICK — MISSING (RT WING) · airframe 99,575 hrs · 15,776 cycles

STATIC WICK MISSING ON THE TRAINING EDGE OF THE RH WING.

Part: LOCK — WORN (SEAT 21H) · airframe 99,575 hrs · 15,776 cycles

SEAT LOCK IN SEAT 21H IS WORN.

Part: SHUTOFF VALVE — LEAKING (LT WING FUEL) · airframe 99,575 hrs · 15,776 cycles

FUEL LEAKING INTO CENTER TANK WHEN FUEL IS ABOVE 20,000 FT. WHEN IT IS COLD OUTSIDE.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 99,575 hrs · 15,776 cycles

HPSOV VALVE IS STUCK IN THE OPEN POSITION

Part: SHUTOFF VALVE — LEAKING (CENTER FUEL TANK) · airframe 99,575 hrs · 15,776 cycles

FUEL LEAKING INTO CENTER TANK WHEN FUEL IS ABOVE 20,000 FT. WHEN IT IS COLD OUTSIDE.

Part: LOCK — WORN (SEAT 17H) · airframe 99,575 hrs · 15,776 cycles

SEAT LOCK IN SEAT 17H IS WORN.

Part: WIRE HARNESS — BROKEN (RT FIRE LOOP) · airframe 99,548 hrs · 15,750 cycles

RH ENGINE FIRE LOOP 1 DISPLAYED ON EICAS ON PREFLIGHT CHECK. TROUBLESHOT PER BOEING 767 FIM, FOUND A TERMINAL ON THE WIRE HARNESS WAS BROKEN. REMOVED AND REPLACED TERMINAL ON WIRE 5534-001R-16. COMPLIED WITH FIRE DETECTION OPERATIONAL CHECK IN ACCORDANCE WITH BOEING 767 AMM 26-11-00-715-075-003. OPERATIONAL CHECK WAS GOOD.