N767AX

Part: LIFE VEST — EXPIRED (ZONE 200) · airframe 71,903 hrs · 46,878 cycles

FOUND CREW LIFE VEST IN STORAGE NEXT TO L1 DOOR EXPIRED DEFERRED LIFE VEST IAW MEL 25-62-1A. MAINTENANCE PROCEDURES C/W. PLACARDS INSTALLED. MBCB 03/13/2026 CLEARED 11/14/25 .REPLACED CREW LIFE VEST AS REQUIRED PLACARD REMOVED NO REACTIVATION PROCEDURES REQUIRED A/C IS IN SERVICE

Part: ANTI-ICE VALVE — DEFECTIVE (ZONE 600) · airframe 71,883 hrs · 46,865 cycles

DURIING TEST FLIGHT, RT WING ANTI-ICE VALVE WOULD NOT OPEN. AIRCRAFT DIVERTED TO DFW. REMOVED AND REPLACED R WING ANTI-ICE VALVE. OPS TEST GOOD IAW AMM 30-11-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIFE VEST — EXPIRED (ZONE 200) · airframe 71,775 hrs · 46,815 cycles

F/U LIFE VEST NEED TO BE REPLACE PER DUE DATE.  REMOVED AND REPLACED LIFE VEST IN THE CAPT'S SEAT, 1ST OBSERVERS SEAT AND 2ND OBSERVERS SEAT PER B767 SP'MMS 25-62-00. NO DEFECTS NOTEED AT THIS TIME. RETURNED TO SERVICE

Part: ESCAPE REEL — UNWANTED EXTEND (ZONE 200) · airframe 71,453 hrs · 46,701 cycles

THREE INERTIAL ESCAPE REELS DISCOVERED DROPPED TO FLOOR AFTER LANDING. DEFERRED INERTIAL ESCAPE REELS IAW MEL 25-61-1-1. REMOVED AND REPLACED 3 INERTIAL ESCAPE REELS AT F/D POS. #2, SN 20994, POS. #4, SN 17656, POS. #6 SN 17681, REF AMM 25-61-00. DI CLEARED MEL 25-61-1-1. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 71,350 hrs · 46,650 cycles

DURING PRE-D FOUND EMERGENCY LIGHTS (MULTIPLE) IN COCKPIT, SUPP AREA, EMER EXIT SIGNS AND EXT INOP. CONNECTED TO POWER SUPPLY M735. REMOVED "DEAD" EMERGENCY LIGHT POWER SUPPLY REPLACED WITH SERVICEABLE UNIT IAW B767 AMM 33-51-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 71,333 hrs · 46,641 cycles

DURING C 5 CHECK AT PEMCO, AMES NR 0155 - FOUND APU COMPARTMENT, INTERNAL, RH WALL AT STA. 1872, 30" UP FROM DOOR CUT OUT HAS GOUGE DAMAGE. EVALUATED DAMAGE, FOUND TO BE OUT OF LIMITS DEPTH .225 LENGTH 1.625 ORIGINAL MATERIAL 2 PLIES 0.016 LIMITS ARE 15% OF SKIN THICKNESS CUTOUT DAMAGE ARE FAB 1 EA FILLER AND 1 EA DOUBLER. INSTALLED NEW 1 EA FILLER AND 1 EA DOUBLER IAW B717-200 SRM 53-00-01. INSPECT 37,500 12,000 FLIGHT CYCLES 9,000 FLIGHT CYCLES. TOOL USED IA 21811 EAP 08/OCT/25. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — INOPERATIVE (RIGHT) · airframe 70,789 hrs · 46,385 cycles

ON PUSHBACK, RH PACK OFF LIGHT. ILLUMINATED RESET DID NOT RESTORE FUNCTION AC RETURNED TO GATE AND MTX GROUNDED AC . MTX DEFERRED RH PACK FOR DEPARTURE IAW MEL ABX 21-51-1-1 AND RETURNED AC TO SERVICE.

Part: MODULE — MALFUNCTIONED (ZONE 100) · airframe 70,748 hrs · 46,367 cycles

WHILE TURNING ON HYDRUALIC PUMPS FOR STARTUP CHECK LIST, RAT PRESSURE GREEN LIGHT ILLUMINATED AND AC WAS RETURNED TO A GATE TO BE WORKED , MTX GROUNDED AC AND TROUBLESHOT .MTX REPLACED RAT CHECKOUT MODULE IAW AMM-29-21-11 NO HYDRAULIC LEAKS NOTED . MTX RETURNED AC TO SERVICE .

Part: SEAT — MALFUNCTIONED (COCKPIT) · airframe 70,143 hrs · 46,068 cycles

DUURING TAXI CAPT SEAT WILL NOT REMAIN IN HORIZONTAL LOCKED POSITION AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . REMOVED AND REPLACED CAPTS. SEAT IAW AMM 25-11-01 OPS CHECK GOOD AC WAS RETURED TO SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 68,490 hrs · 45,356 cycles

DURING ROUTINE LINE MAINTENANNCE IN CVG IN JULY OF 2022 CORROSION DAMAGE WAS FOUND NEAR THE AFT LOWER CARGO DOOR AND WAS TEMPORARILY REPAIRED, WHEN A PERMANENT REPAIR COULD HAVE BEEN INSTALLED. THE AIRCRAFT IS NOW IN C-CHECK. THE PURPOSE OF THIS REA IS TO REPLACE TEMPORARY REPAIR. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED AND PERMANENT REPAIR INSTRUCTIONS PROVIDED. REPAIR WAS COMPLETED ON ABX-REA-5365-64956-01

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,490 hrs · 45,356 cycles

DURING C CHECK CORROSION WAS FOUND ON CARGO TRACK P/N: 96FS667847-104 INSTALLED IN THE AFT CARGO COMPARTMENT BETWEEN STA 1263 AND STA 1307 AND RBL 33. DAMAGE REMOVED PER 767-200 SRM 51-10-02, THE REMAINING THICKNESS IS 0.082 IN STA 1263 AND 0.064 IN STA 1295 SEE FIGURE 1. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED AND PERMANENT REPAIR. INSTRUCTIONS WERE APPROVED. INSTRUCTIONS WERE PROVIDED FOR REPAIR ON ABX-REA-5360-64959-00

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,490 hrs · 45,356 cycles

DURING C CHECK DENT ON FUSELAGE AT STA 361 BETWEEN S25L AND S26LWAS FOUND. SKIN DENT IS OUT OF LIMITS PER SRM 53-00-01 FIG. 101 DETAIL 3. THE DENT IS CLOSE TO IAI STC STRAP DOUBLER P/N: 368-53-11-60695-201 APRROX. .85” SEE FIGURE 1 SHEET 1 OF THIS EA. FLIGHT VEHICLES CONSULTING INC. WAS CONTACTED AND PERMANENT REPAIR INSTRUCTIONS WERE APPROVED. INSTRUCTIONS WERE PROVIDED FOR REPAIR ON ABX-REA-5315-64958-00

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 68,008 hrs · 45,143 cycles

AFTER T/O LEFT GEAR DID NOT COME UP. REMAINS GREEN AND DOWN. LOWERED GEAR  FOR LANDING AND GEAR DOOR LIGHT REMAINED ILLUMINATED. DURING APPROACH THE GEAR DOOR LIGHT EXTINGUISHED.THE LANDING WAS OVERWEIGHT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT FURTHER INCIDENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OVERWEIGHT LANDING INSPECTION AND NO DEFECTS WERE FOUND. MAINTENANCE DEFERRED THE LANDING GEAR RETRACTION SYSTEM IAW B767 MEL 32-30-1. PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — BROKEN (SHUTOFF SWITCH) · airframe 67,971 hrs · 45,130 cycles

UNABLE TO GET LEFT FUEL CUT OFF SWITCH TO GO INTO RUN DETENT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED DEBRIS AND REPLACED LIGHT PLATE IAW AMM 76-11-09. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — SEIZED (HYD SYSTEM) · airframe 67,911 hrs · 45,096 cycles

ON CLIMB OUT L PRIM HYD OVHTEICAS ILLUM WITH L DEM PUMP INOP RETURNED TO LAND. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED EDP FILTERS IAW B767 AMM 29-11-05 AND REPLACED EDP IAW 29-11-05. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 67,421 hrs · 44,907 cycles

DURING ROUTINE LINE OPERATIONS AT CVG (CINCINNATI/N. KY INTERNATIONAL AIRPORT), AIRBORNE MAINTENANCE DISCOVERED CORROSION DAMAGE (SHOWN IN FIGURE 1) TO THE BEAR STRAP SURROUNDING THE AFT LOWER CARGO DOOR CUTOUT (P/N 146T8521-1), WHICH EXCEEDED THE ALLOWABLE DAMAGE LIMITS GIVEN IN B767-200 SRM 53-60-01. THE DAMAGE WAS LOCATED BETWEEN STA 1373 AND 1380 AT STR 34R. THE DAMAGE TO THE BEARSTRAP WAS TRIMMED OUT, AS WELL AS A PORTION OF THE FUSELAGE SKIN (146T8531-2) IN ORDER TO ACCESS THE BEARSTRAP, LEAVING A 9” X 7” CUTOUT IN THE FUSELAGE (SHOWN IN FIGURE 2). THE BEARSTRAP IS MADE FROM 0.212” 2024-T3 BARE ALUMINUM SHEET AND THE AFFECTED SKIN PANEL IS MADE FROM 0.210” 2024-T3 CLAD ALUMINUM SHEET. AS NO SRM REPAIR EXISTED FOR THE SUBJECT DAMAGE, ABX AIR MAINTENANCE CONTROL CONTACTED AMES ENGINEERING FOR DAMAGE EVALUATION AND A REPAIR SOLUTION. THIS REA ALLOWS FOR THE DAMAGED AREA TO BE REPAIRED USING ALUMINUM DOUBLERS. AMES ENGINEERING CONTACTED FLIGHT VEHICLES CONSULTING (FVCI), INC. FOR EVALUATION AND APPROVAL OF THE PROPOSED REPAIR. AIRCRAFT REPAIR COMPLETED AND AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE · airframe 67,333 hrs · 44,876 cycles

LAV SERVICE DOOR WAS DISCOVERED OPEN DURING PUSH BACK. GROUND PERSONNEL WERE UNABLE TO CLOSE THE DOOR. MAINTENANCE WAS CALLED TO SECURE DOOR PRIOR TO AIRCAFT DEPARTURE.

Part: CABLE — BROKEN (LEFT ENGINE) · airframe 66,622 hrs · 44,587 cycles

DURING CLIMB PASSING 350, NOTICED LEFT EGT WAS LESS THAN 1/2 OF NORMAL. SEI SHOWED 40-46 REGARDLESS OF POWER SETTING.AIRCRAFT PROCEEDED WITH A AIR TURNBACK WITHOUT EVENT. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE FOUND THERMOCOUPLE HARNESS CONNECTOR BROKEN AT 11'OCLOCK POSITION. REMOVED AND REPLACED UPPER HARNESS IAW B767 77-21-03.CONDUCTED L ENGINE RUN FOR EGT INDICATION CHECK PER ABX ERU/TAXI CHECKLIST AND AMM 77-21-00. NO HELP. DISCONNECTED STANDBY ENGINE INDICATOR, EICAS EGT NORMAL. FOUND PUSHED PIN ON SEI L/H ENGINE CONNECTOR TO GROUND. RESEATED PIN, ALL EGT INDICATIONS NORMAL AND MATCHING. REF WDM 77-21-11 AND AMM 77-41-01. SEI OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSMITTER — FAULTED (RT AILERON) · airframe 66,202 hrs · 44,387 cycles

RT AILERON EICAS POSITION INDICATOR DOES NOT INDICATE FULL DEFLECTION DURING BEFORE TAKE-OFF CHECK.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DETERMINED THAT THE PROBLEM WAS THE POSITION TRANSMITTER AND THAT THE AILERON HAD FULL MOVEMENT. THE AILERON POSITION SYSTEM WAS PACED ON DEFERRAL IAW MEL 27-08-01 AND THE AIRCRAFT WAS RELEASED FOR FLIGHT.

Part: NONE — NONE · airframe 66,165 hrs · 44,376 cycles

ON TAKE OFF ROLL RIGHT REV (AMBER) LIGHT ILLUMINATED. ABORTED TAKE OFF AND RETURNED TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. RIGHT REVERSER WAS DEFERRED IAW ABX MEL 78-31-1A. AIRCRAFT RETURNED TO SERVICE.

Part: SHUTOFF VALVE — FAULTED (LT ENG FUEL) · airframe 65,953 hrs · 44,288 cycles

DURING LT ENGINE START NO FUEL FLOW WITH A LT ENG FUEL VALVE EICAS MSG DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.REPLACED ENG FUEL SPAR SHUTOFF VALVE ADAPT/SHAFT IAW AMM 28-20-0.AIRCRAFT RELEASED FOR FLIGHT.

Part: WARNING MESSAGE — ILLUMINATED (L1 DOOR) · airframe 65,911 hrs · 44,269 cycles

L1 DOOR EICAS MESSAGE INDICATION ON PUSHBACK AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE, THE L1 DOOR INDICATION WAS PLACED ON DEFERRAL. IAW MEL52-71-1-1 AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (RT A/C PACK) · airframe 65,865 hrs · 44,252 cycles

RT PACK OFF LIGHT ANNUNCIATED , RESET NO HELP. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. RT. A/C PACK WAS DEFERRED IAW MEL 21-51-1-1. MAINTENANCE PROCEDURES COMPLIED WITH. PLACARD INSTALLED AND AIRCRAFT RELEASED FOR FLIGHT.

Part: IDG — FAULTY (RIGHT) · airframe 65,843 hrs · 44,245 cycles

IN FLIGHT EICAS MSG "R GEN DRIVE" DISPLAYED WITH DRIVE LIGHT ON DISCONECT SWITCH. DISCONNECTED PER THE QRH PROCEDURE. THE APU WAS DEFERRED AND THE APU GENERATOR COULD NOT BE USED. THE CREW DECIDED TO DIVERT TO KMEM INSTEAD OF CONTIMUING TO KDEN. THE AIRCRAFT LANDED AND WAS GROUNDED BY MAINTENACE. MAINTENANCE REMOVED AND REPLACED THE RIGHT IDG IAW AMM 24-11-01. AIRCRAFT WAS RETURNED TO SERVICE

Part: WARNING MESSAGE — FAULT MESSAGE (AILERON LOCKOUT) · airframe 65,468 hrs · 44,091 cycles

AILERON LOCKOUT EICAS MESSAGE AND LIGHT ON DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. AILERON LOCKOUT SYSTEM PLACED ON DEFERRAL AND AIRCRAFT RELEASED FOR FLIGHT.

Part: PSEU — FAULTED (MLG HANDLE) · airframe 65,411 hrs · 44,066 cycles

ON INITIAL TAKEOFF GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION.  GEAR HANDLE THEN MOVED TO THE UP POSITION WITH "LOCK OVERRIDE" BUTTON PUSHED. AIRCRAFT PERFORMED AIR TURN BACK. AIRCRAFT WAS GROUNDED BY MAINTENANCE. PSEU FAILED, PSEU REMOVED AND REPLACED. NOSE LANDING GEAR SENSORS ADJUSTED, WIRING CHECKED, OPS CHECKED GOOD.

Part: SUPPORT — CORRODED (RT TRUNNION) · corrosion level 2 · airframe 65,411 hrs · 44,064 cycles

LMLG H-BLOCK MOUNT UPPER I/B BUSHING HAS CORROSION AROUND AND UNDER THE O/B SIDE OF BUSHING.  THERE IS ALSO A GOUGE IN THE STRUCTURE BELOW THE BUSHING. REMOVED, REPAIRED AND REPLACED LMG H BLOCK UPPER I/B BUSHING IAW ABX-REA 5727-64355-00

Part: STRINGER — CRACKED (BS 676-678 S24L) · airframe 65,411 hrs · 44,064 cycles

FUSELAGE STRINGER 24L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S24L IAW B767 SRM 53-00-03 REPAIR 2.

Part: STRINGER — CRACKED (BS 676-677 S23L) · airframe 65,411 hrs · 44,064 cycles

FUSELAGE STRINGER 23L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S23L @ F.S. 676 IAW B767 SRM 53-00-03 REPAIR 2

Part: PANEL — DELAMINATED (RT WING) · corrosion level 2 · airframe 65,411 hrs · 44,064 cycles

THERE IS DELAMINATION ON THE CORNERS OF 2 RIGHT WING UPPER T/E PANELS, FWD OF THE RIGHT O/B AILERON AT W.S.1030. REMOVED I/B AND O/B TE PANELS AT W/S 1030, REMOVED CORROSION BY .025" FROM NOMINAL .080" AND FOUND REMAINING .055" FOUND TO BE OUT OF LIMITS IAW B767 SRM 57-51-02 VII TAG# 3310 REPAIRED IAW REA# ABX-REA-5725-64336-00

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 65,411 hrs · 44,064 cycles

WHILE IN C-CHECK, THERE IS CORROSION ON THE INTERIOR STRUCTURE OF THE ALC DOOR, AROUND LIGHTENING HOLES, AROUND NUTPLATE HOLES, AND INSIDE ALL OF THE LIGHTENING HOLES AT THE TOP OF THE ALC DOOR, MARKED. THE CORROSION WAS FOUND TO BE OUT OF LIMITS ON VARIOUS STRUCTURES ON DOOR. THE DOOR WAS REPLACED WITH A NEW DOOR

Part: STRINGER — CRACKED (BS 676 S21L) · airframe 65,411 hrs · 44,064 cycles

WHILE IN C CHECK, FUSELAGE STRINGER 21L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S21L @ FS 676 IAW B767 SRM 53-00-03 REPAIR 2 AND SB #368-53-038

Part: STRINGER — CRACKED (BS 676 S22L) · airframe 65,411 hrs · 44,064 cycles

DURING C CHECK, FUSELAGE STRINGER 22L STA 676 IS CRACKED AT THE IAI STRINGER SPLICE. REPAIRED S22L @ F.S. 676 IAW B767 SRM 53-00-03 REPAIR 2.

Part: GENERATOR — SHUTDOWN (RIGHT) · airframe 65,321 hrs · 44,018 cycles

WHILE ON GROUND AND LEFT ENGINE SHUTDOWN RIGHT GENERATOR DROPPED OFFLINE. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE PERFORMED MANUAL RESET OF #2 ENG. FIELD IAW B767 AMM 24-11-00. RESET SUCCESSFUL. AIRCRAFT RELEASED FOR FLIGHT.

Part: HYDRAULIC SYSTEM — LEAKING (RIGHT) · airframe 65,059 hrs · 43,902 cycles

ON TAXI OUT, RIGHT HAND HYDRAULIC FLUID QTY LOSS ON EICAS. AIRCRAFT BACK TO BLOCK AND GROUNDED. MAINTENANCE PLACED HYDRAULIC QTY ON DEFERRAL AND AIRCRAFT RELEASED TO RESUME FLIGHT OPERATIONS.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 64,857 hrs · 43,812 cycles

SPEED FLAGS ON BOTH CA/FO PED'S. AIRCRAFT BACK TO BLOCKS AND GROUNDED BY MAINTENANCE. RESET TMC FLAG CLEARED. NO MESSAGE, OK FOR SERVICE, FIM 22-32 FT 804. A/C DOWNGRADED TO CAT 1 PENDING 30 + 40 TEST.

Part: WARNING FLAG — FALSE ACTIVATION (ATTITUDE IND) · airframe 66,440 hrs · 43,637 cycles

SPEED FLAG APPEARED ON ATTITUDE INDICATOR. AIRCRAFT WAS GROUNDED. CYCLED THRUST MANAGEMENT COMPUTER C/BS F-14,15, SPEED FLAGS DISAPPEARED PER FIM 22-32-00 A/C RALM STATUS DOWN GRADED TO CAT 1.

Part: WARNING MESSAGE — ILLUMINATED (FWD CARGO DOOR) · airframe 64,237 hrs · 43,546 cycles

FORWARD CARGO DOOR EICAS MESSAGE ON DISPLAY.AIRCRAFT WAS GROUNDED.

Part: SENSOR — DEFECTIVE (COMPRESSOR INLET) · airframe 64,095 hrs · 43,469 cycles

LEFT ENGINE SLOW TO SPOOL WITH SOME STRANGE INDICATION COMPARED TO RIGHT ENGINE WITH N1'S MATCHED N2 (LEFT ENGINE) IS 10% HIGHER, OIL TEMP IS 10 DEGREES C HIGHER, OIL PRESSURE IS 10 PSI HIGHER AND N1 SHOWS A COMMAND BOX INDICATION FUEL FLOW WAS SLIGHTLY HIGHER TOO (ROUGHLY 800 LBS/ HR HIGHER. THE AIRPLANE WAS GROUNDED.

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 62,633 hrs · 42,799 cycles

THE FLIGHT DECK HAD A WHEEL WELL FIRE INDICATION AT FLIGHT LEVEL 260. THE CREW EXTENDED THE GEAR AND THE INDICATION WENT OFF. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELLS WERE INSPECTED WITH NO DEFECTS FOUND. THE WHEEL WELL FIRE CIRCUIT CARD M691 WAS REPLACED. THE CAUSE OF THE FIRE INDICATION IS UNKNOWN.

Part: TRANSDUCER — FAULTY · airframe 62,622 hrs · 42,793 cycles

DURING TAKEOFF, NEITHER ENGINE REACHED TAKEOFF N1 SPEED (109.7). THE RIGHT ENGINE N1 INDICATED 108.8 AND THE RIGHT EGT INDICATED 925 CELSIUS. THE LEFT ENGINE N1 INDICATED 107.9. THE CREW ABORTED THE TAKEOFF AT 125 KIAS. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND BOTH ENGINES WERE VISUALLY INSPECTED ALONG WITH THE CHIP DETECTORS. NO DAMAGE WAS FOUND. THE RIGHT THRUST LEVER ANGLE TRANSDUCER AND THE RIGHT POWER LEVER ANGLE TRANSDUCER WERE REPLACED. THE LEFT AND RIGHT THRUST LEVER ANGLE TRANSDUCERS, THE RIGHT POWER LEVER ANGLE TRANSDUCER, AND THE SPECIFIC GRAVITY SETTING ON THE LEFT AND RIGHT MAIN ENGINE CONTROLS WERE ADJUSTED. A HIGH POWER ENGINE RUN WITH THE ELECTRONIC ENGINE CONTROLS ON WAS PERFORMED. PARAMETERS WERE WITHIN LIMITS. A HIGH ENERGY STOP CONDITIONAL INSPECTION WAS PERFORMED WITH NO FINDINGS. THE CAUSE OF THE BOTH ENGINES NOT REACHING TAKEOFF N1 IS UNKNOWN.

Part: BEAR STRAP — CORRODED (BS 859-871) · corrosion level 2 · airframe 62,434 hrs · 42,711 cycles

CORROSION ON THE LOWER (INTERNAL SURFACE) BEAR STRAP, RIGHT OVERWING EMERGENCY EXIT, STA 859.5 – 871.5, STR 16AR – 18R. THE BEAR STRAP WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1297-1307) · corrosion level 2 · airframe 62,434 hrs · 42,711 cycles

CORROSION ON STRINGER 36L, AT FUSELAGE STATION 1297 - 1307. THE STRINGER WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: CARABINER — MISSING (FORWARD CABIN) · airframe 60,241 hrs · 41,675 cycles

THREE EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), THREE NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS UNKNOWN.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,940 hrs · 41,482 cycles

CRACK AND DAMAGE IN WEB AT RIGHT MAINTENANCE EQUIPMENT TUNNEL FLOOR SUPPORT, FUSELAGE STATION 246. WEB WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (BS 1120) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION UNDER NUT PLATE ON INTERCOSTAL IN THE UPPER CARGO BAY AT BS 1120. THE INTERCOSTAL WAS REPLACED. THE ACFT WAS GROUNDED.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,940 hrs · 41,482 cycles

CRACK AND DAMAGE IN WEB AT LEFT MAINTENANCE EQUIPMENT TUNNEL FLOOR SUPPORT, FUSELAGE STATION 246. WEB WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: RIB — CRACKED (RT WING) · airframe 59,940 hrs · 41,482 cycles

CRACK IN LEADING EDGE NOSE RIB AT RIGHT WING STATION 456. THE RIB WAS REPLACED. THE ACFT WAS GROUNDED.

Part: FAILSAFE — CORRODED (BS 1346) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON UPPER FAILSAFE STRAP AT AFT LOWER CARGO DOOR CUTOUT AFT EDGE FRAME, BS 1346. THE FAILSAFE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 59,940 hrs · 41,482 cycles

CRACK IN AFT LOWER CARGO DOOR NR 7 BEAM REPAIR STRAP. REPAIRED. AIRPLANE WAS GROUNDED.

Part: COVER — CRACKED (RT WING) · airframe 59,940 hrs · 41,482 cycles

CRACK IN OUTBOARD AILERON INBOARD WEIGHT COVER AT RIGHT WING STATION 923. COVER WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FITTING — CRACKED (RT WING SPOILERS) · airframe 59,940 hrs · 41,482 cycles

CRACK IN THE NR 11 SPOILER ACTUATOR INBOARD SUPPORT FITTING AT THE RIGHT WING STATION 700. FITTING WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: WEB — CORRODED (RT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON LEADING EDGE WEB AT RIGHT WING STATION 730. WEB WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (BS 955) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON SKIN COMMON TO LEFT FAILSAFE STRAP AT BS 955. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: RIB — CRACKED (RT WING) · airframe 59,940 hrs · 41,482 cycles

CRACK IN UPPER SECTION OF THE PYLON CANTED RIB, RIGHT WING STATION 404.4. CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON LOWER END FITTING OF STRINGER 7L IN THE LEFT HORIZONTAL STABILIZER AT REAR SPAR HSS 0.00. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: RIB — CRACKED (RT WING) · airframe 59,940 hrs · 41,482 cycles

CRACK IN LEADING EDGE RIB AT RIGHT WING STATION 500. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,940 hrs · 41,482 cycles

CORROSION ON SEAT TRACK BETWEEN FUSELAGE STATIONS 999 AND 1175. SEAT TRACK WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (SUBFLOOR) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON SUBFLOOR IN AFT LOWER CARGO COMPARTMENT, BS 1285 - 1307. REPLACED. AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (BS 676) · airframe 59,940 hrs · 41,482 cycles

CORROSION AROUND NUT PLATES ON STRUCTURE AT BS 676, LBL 21 IN LOWER CARGO BAY. THE STRUCTURE WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON REAR SPAR TO TRAILING EDGE LOWER PANEL ATTACH TEE AT LEFT WING STATION 1076. TEE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON UPPER TRAILING EDGE SKIN FORWARD OF OUTBOARD AILERON BENEATH BONDED PANEL AT LEFT WING STATION 1030. SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: STRAP — CORRODED (BS 1480) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON STRAP AND FRAME AT BS 1480. THE STRAP WAS REPLACED. THE FRAME WAS REPAIRED. THE ACFT WAS GROUNDED.

Part: STRINGER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON LOWER END FITTING OF STRINGER 6L IN THE LEFT HORIZONTAL STABILIZER AT REAR HSS 0.00. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: FAILSAFE — CORRODED (BS 1270) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON UPPER FAILSAFE STRAP AT AFT LOWER CARGO DOOR CUTOUT FORWARD EDGE FRAME BS 1270. THE FAILSAFE STRAP WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: TEE FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON REAR SPAR TO TRAILING EDGE LOWER PANEL ATTACH TEE FROM LEFT WING STATION 138 TO STATION 220. TEE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON RIB AT RIGHT WING STATION 631. RIB WAS REPLACED. ACFT WAS GROUNDED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 59,940 hrs · 41,482 cycles

CRACK IN FAILSAFE STRAP AT LEFT BS 955. THE FAILSAFE WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (LT WING AILERON) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION AROUND NUT PLATES ON UPPER STRUCTURE OF THE LEFT INBOARD AILERON, INBOARD RIB, AT WING STATION 431.97. THE STRUCTURE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: STRUCTURE — CORRODED (BS 544-610) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON FORWARD LOWER CARGO DOOR INTERNAL STRUCTURE BELOW LIGHT ASSEMBLY, BS 544 - 610. THE STRUCTURE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SUPPORT ANGLE — CORRODED (BS 1065) · corrosion level 3 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON SUPPORT ANGLE AT AFT LOWER CARGO COMPARTMENT BULKHEAD, BS 1065. THE SUPPORT ANGLE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 1540-1562) · airframe 59,940 hrs · 41,482 cycles

CORROSION ON OUTER FLOOR SUPPORT JUST AFT OF R2 DOOR BETWEEN BS 1540 AND 1562. THE FLOOR SUPPORT WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: TEE FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON REAR SPAR TO TRAILING EDGE LOWER PANEL ATTACH TEE AT LEFT WING STATION 936. TEE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON REAR SPAR TO TRAILING EDGE LOWER PANEL ATTACH TEE AT LEFT WING STATION 1087. TEE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: TEE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON REAR SPAR TO TRAILING EDGE LOWER PANEL ATTACH TEE AT RIGHT WING STATION 1106. TEE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: STRINGER — CORRODED (BS 1351) · airframe 59,940 hrs · 41,482 cycles

CORROSION ON STRINGER 39L AT BS 1351. THE STRINGER WAS REPAIRED. THE ACFT WAS GROUNDED.

Part: ATTACH FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON REAR SPAR TO TRAILING EDGE LOWER PANEL ATTACH TEE AT LEFT WING STATION 1046. TEE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON SHEAR TIE AT OUTLFOW VALVE CUTOUT, BS 1540. THE SHEAR TIE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 59,940 hrs · 41,482 cycles

CRACK IN FAILSAFE STRAP AT RIGHT BS 955. CRACK AT LOWER FASTENER HOLE COMMON TO TEE-FITTING. THE FAILSAFE STRAP WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 1417-1540) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON BULK CARGO RIGHT OUTBOARD FLOOR SUPPORT BETWEEN BS 1417 AND 1540. FLOOR SUPPORT WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: FRAME — CORRODED (BS 955) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON RIGHT SIDE FRAME FITTING AT BS 955. THE FRAME FITTING WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON UPPER INTERCOSTAL AT AFT LOWER CARGO DOOR CUTOUT, BS 1329 - 1351. THE INTERCOSTAL WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (BS 955) · corrosion level 2 · airframe 59,940 hrs · 41,482 cycles

CORROSION ON RIGHT SKIN COMMON TO TEE FITTING AT BS 955. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: PANEL SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 56,537 hrs · 39,924 cycles

PANEL SUPPORT IN RT MLG WW CORRODED & SPLIT OUT APPROX 200 WS. R & R CHORD PART 113T1023-158 IN RT MLG WW AT APPROX STATION 200 IAW SRM 51-40-02. SDR INFO, CORRODED PN 113T1623-158, PART NAME CHORD, SN NSN, WS FROM 200 TO 200. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (WING) · corrosion level 2 · airframe 56,537 hrs · 39,924 cycles

PANEL ATTACH LOWER CHORD FROM WING REAR SPAR TO TE AT WS 1054 CORRODED. LOWER CHORD AT TE WS 1054 CORRODED BEYOND LIMITS IAW SRM CH 57-51-02. INSTALL NEW CHORD PN 113T1676-21 IAW SRM CH 51-40-02. PART NUMBER 113T1676-21, PART NAME CHORD, SN NSN, WS LOC: 1054. ACFT WAS GDED.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 56,537 hrs · 39,924 cycles

LEFT WING UPPER SPLICE PLATE REQUIRES A REPLACEMENT SECTION INSTALLED FOR COI61410-001, REA B657-61466. REPLACED SPLICE PLATE IAW B657-61466. SDR INFO, CORRODED PN 114T0223-19, PART NAME SPLICE PLATE, SN NSN, STRINGER & WS LOCATION FROM 446 TO 519. ACFT WAS GNDED.

Part: UNKNOWN — ODOR · airframe 56,492 hrs · 39,902 cycles

HEAVY FUEL ODOR IN FLIGHT DECK WITH BOTH PACKS ON AFTER LANDING. PERFORMED FIM 21-00-801. GND CHECKED LT & RT PACK, INSPECTED PACKS. CHECKED FLIGHT DECK WITH PACK ON, NO FUEL ODOR NOTED. GND CHECKED GOOD. CAUSE OF REPORTED FUEL ODOR WAS NOT DETERMINED.

Part: BRACKET — CRACKED (ZONE 600) · airframe 54,270 hrs · 38,773 cycles

RT WING BRACKET ATTACHING INBD L/E STRUCTURE TO FWD UPPER SPAR AT WING STA 155 IS CRACKED. R & R BRACKET IAW SRM 51-40-02. LEAK CHECK GOOD IAW AMM 28-11-00. WS LOC; ACFT WAS GROUNDED.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 54,270 hrs · 38,773 cycles

L/E VERTICAL STABILIZER FWD ANGLE HAS CRACKED INSIDE LT SIDE OF VERTICAL STABILIZER AT VERTICAL FUSE BOXED STRUCTURE INSIDE OF LOWEST PANEL OPENING. R & R FWD ANGLE INSIDE LEFT VERTICAL STABILIZER AT VERTICAL FUSE BOX IAW DWG 173T1215 AND SRM 51-40-02. ACFT WAS GROUNDED.

Part: STRUT — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

NR 5 SLAT OTBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R STRUT AT OTBD SIDE OF OTBD AUX. TRACK IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

FRAME CORRODED AT APU EXHAUST DUCT SUPPORT FUSELAGE, BS 1943.5. CLEANED UP CORROSION, SPLICED IN NEW SECTION OF FRAME AT STA 1943.5 IAW REA B653-60618, ACFT GROUNDED.

Part: SUPPORT — CRACKED (NACELLE) · airframe 54,270 hrs · 38,773 cycles

INBD VERTICAL STRUCTURE FOR PNEUMATIC DUCT UPPER FWD ADJUSTABLE ROD FITTING HAS A CRACK COMING OUT OF TOP FASTENER, UNDER PANEL 441AT. R & R INBD VERTICAL STRUCTURE FOR ANTI ICE DUCT UPPER FWD ADJUSTABLE ROD IAW SRM 51-40-02 AND DWG 311T151510, ACFT WAS GROUNDED.

Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

NR 2 SLAT ON LT WING OTBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R NR 2 SLAT OTBD AUX TRACK AND OTBD LOWER STRUT IAW SRM 51-40-02, PARA 7B AND REA B657-60610, ACFT GROUNDED.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

CORROSION ON RIB AND FRONT SPAR LOWER TEE FRAME AT NR 9 SLAT INBD AUX TRACK OTBD RIB. R & R AIRLOAD RIB AT NR 9 SLAT INBD AUX TRACK IAW SRM 51-40-02 AND REA B657-60613, ACFT WAS GROUNDED.

Part: STRUT — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 54,270 hrs · 38,770 cycles

NR 5 SLAT INBD AUX TRACK OTBD LOWER STRUT HAS CORROSION AROUND NUTPLATES. R & R NR 5 SLAT INBD AWS TRACK OTBD LOWER STRUT IAW SRM 51-40-02, AND EA B657-60615.

Part: RIB — CORRODED (ZONE 500) · airframe 54,270 hrs · 38,773 cycles

NR 5 SLAT ANTI-ICE TELESCOPING DUCT INBD STRUT CORRODED AROUND NUTPLATES. REMOVED CORRODED AIR LOAD RIB, INSTALLED NEW AIR LOAD RIB IAW REA 657-60614 AND SRM 51-40-02. INSTALLED NR 5 SLAT & TELESCOPING DUCT IAW AMM 20-11-00-2, FIG 209 & SRM 51-40-02 AMM 30-11-05-4, ACFT WAS GROUNDED.

Part: STRUT — CORRODED (NR 8 SLAT) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

CORROSION AROUND NUTPLATES ON LOWER STRUT OF NR 8 SLAT OTBD AUX TRACK OTBD STRUT. R & R LOWER STRUT OF NR 8 SLAT OTBD AUX TRACK OTBD STRUT IAW SRM 51-40-02 AND REA B657-60609, ACFT WAS GROUNDED.

Part: BEAM — CHAFED (PYLON) · airframe 54,270 hrs · 38,773 cycles

CHAFE ON BACKSIDE OF FWD ATTACHING FLANGE FOR ACCESS PANEL 447BR AT BS 298-RT NACELLE STA 410, RT PYLON OTBD SIDE. R & R NR 2 OTBD PYLON BEAM IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: STRUCTURE — CORRODED (RT WING) · airframe 54,270 hrs · 38,773 cycles

CORROSION UNDER NUTPLATE ON WING L/E AFT OF NR 8 SLAT LES 466. R & R OUT OF LIMIT DAMAGE. IAW SRM 51-70-11, DETAIL II. ACFT WAS GROUNDED.

Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

NR 3 SLAT OTBD AUX TRACK INBD LOWER STRUT CORRODED AT FORWARD END. R & R STRUT IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: STRUT — CORRODED (LT WING) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

NR 2 SLAT INBD AUX TRACK OTBD LOWER STRUT CORRODED AROUND NUTPLATES. R & R INBD AUX TRACK OTBD STRUT ON NR 2 SLAT IAW DWG 114T2222, REV D, ACFT GROUNDED.

Part: WEB — CRACKED (ZONE 500) · airframe 54,270 hrs · 38,773 cycles

NR 1 SLAT WEB ON L/E OF WING AT OTBD AUX TRACK INBD STRUT ATTACH POINT SPLIT FROM CORROSION. REPAIRED NOSE BEAM WEB IAW SRM 57-41-13, FIG 201, REPAIR 1, ACFT WAS GROUNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

CORROSION AROUND NUTPLATE ON WING L/E AT L/E S682 AFT OF INBD END OF NR 10 SLAT. REPAIRED AREA IAW SRM 51-70-11, REPAIRED AREA IAW SRM 51-70-11, ACFT WAS GROUNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 54,270 hrs · 38,773 cycles

CORROSION ON WING L/E WEB AT LES 695 AFT OF NR 10 SLAT. REPLACED NOSE BEAM IAW SRM 51-40-02, ACFT WAS GROUNDED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,754 hrs · 37,962 cycles

SKIN HAS LIGHTNING STRIKE DAMAGE AT FS 476 AT S26L. REPAIRED AREA IAW REA NO B653-59821-MR, ACFT WAS GROUNDED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,754 hrs · 37,962 cycles

SKIN HAS LIGHTNING STRIKE DAMAGE AT FS 368 AT S31L. REPAIRED DAMAGE AT FUSELAGE STR 368 AT 331L IAW REA B653-59814-MR, ACFT WAS GROUNDED.

Part: SUPPORT — CORRODED (RT MLG) · airframe 52,108 hrs · 37,706 cycles

RIGHT GEAR FORWARD TRUNNION BEARING SUPPORT "H" BLOCK UNDER LOWER INBD BUSHING CORRODED AT FACE OF LUG 12 O'CLOCK POSITION. REPAIRED FORWARD TRUNNION BEARNG SUPPORT IAW REA B657-59562-MR, AWG.

Part: BUSHING — CORRODED (RT MLG) · airframe 52,108 hrs · 37,706 cycles

RIGHT GEAR AFT BEARING RACE HAS CORROSION BLEEDING OUT OF RACE ON AFT SIDE. REMOVED BUSHING, CLEANED UP CORROSION, REWORKED AREA AND INSTALLED OVERSIZED BUSHING IAW B767 CMM 57-54-13, AWG.

Part: SPAR — CORRODED (LT WING) · airframe 52,081 hrs · 37,700 cycles

LW FWD UPPER SPAR IS CORRODED EXTERIOR SURFACE AT LES698. REPAIRED UPPER SPAR IAW B657-59256. CORROSION 3.5" X 1.2" X .062.

Part: JACKSCREW — GOUGED (HORIZ STAB) · airframe 50,772 hrs · 36,808 cycles

DURING C-CHECK INSPECTION, FOUND HORIZONTAL STABILIZER JACKSCREW HAD GOUGE ON THREAD ABOUT 11 INCHES FROM LOWER END. JACKSCREW ASSEMBLY WAS REPLACED. STABILIZER TRIM ACTUATOR ASSEMBLY WAS SENT OUT ON R/O 501590675 TO REPAIR VENDOR DELTA AIRLINES INC. REPAIR ORDER IS OPEN AT THIS TIME.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 46,910 hrs · 35,447 cycles

L-2 DOOR SLIDE ASSY WAS LOOSE FROM PACKBOARD. DEFERRED DI 51091. REMOVED SLIDE ASSY FROM PACKBOARD AND INSTALLED BALLAST ASSY PER MM PROCEDURE REF 52-11-4-2. DEFERRED L2 DOOR SLIDE ASSY PER MEL 52-11-4-2D, CAT B, CODE 8. PLACARD INSTALLED ON GREEN ARMING LEVER. MBCB JULY 31, 2006. CLEAR DI 51091 REMOVED BALLAST AND INSTALLED SLIDE ASSY IAW B767 AMM 25-66-01. REMOVED PLACARD CLEARED DI.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,392 hrs · 35,241 cycles

EMERGENCY LIGHTS FAIL SATURDAY AM DEEP CYCLE TEST. REPLACED EMERGENCY LIGHTS MAIN BATTERY PACK IAW B767 AMM 33-51-07-2. CHECKS AND TESTS GOOD AS PER SAME.

Part: DOOR — STIFF (MAIN PAX) · airframe 45,751 hrs · 34,973 cycles

MAIN ENTRY DOOR WOULD NOT OPEN ABOVE FLIGHT. ADJUSTED BUSTLE AS NEEDED. OPS CHECKED DOOR SIX TIMES. OPS CHECKED GOOD.

Part: SLIDE — DAMAGED (PAX DOOR) · airframe 45,596 hrs · 34,918 cycles

EMERGENCY SLIDE ON MAIN PASSENGER DOOR WOULD NOT STAY IN POSITION. REMOVED AND REPLACED DOOR ESCAPE SLIDE IAW B767 AMM 25-66-01-4. PLACARD REMOVED.

Part: ACTUATOR — DEFECTIVE (MLG) · airframe 44,333 hrs · 34,482 cycles

ON DEPARTURE FROM ILN, LANDING GEAR DISAGREE AND GEAR DOORS EICAS MSG WITH GEAR HANDLE UP. REPLACED LEFT MAIN LANDING GEAR SIDE STRUT ACTUATOR IAW B767 MM 32-32-02-4. PERFORMED GEAR SWING, GEAR SWINGS OK.

Part: BRACKET — MISINSTALLED (MLG) · airframe 43,797 hrs · 34,255 cycles

GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. CAPTAIN'S DISCRETION TO NOT USE LOCK OVERRIDE SWITCH. MAINTENANCE TROUBLESHOT AIR/GROUND RELAY SYSTEM PER B767 WDM 32-09 AND FOUND RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET INCORRECTLY INSTALLED. REPOSITIONED THE RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET PER B767 MM 32-09-09 AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST PER B767 MM 32-32-10 AND SYSTEM CHECKED GOOD.

Part: BOLT — SHEARED (VERTICAL STAB) · airframe 43,794 hrs · 34,253 cycles

WHILE ACCOMPLISHING INSPECTION OF AD2001-19-04, FOUND 1 VERTICAL STAB ATTACH BOLT SHEARED AT FS 1654 LEFT SIDE. REMOVED AND REPLACED ALL 16 VERTICAL ATTACH BOLTS AND NUTS IAW ABX EA 53420014-001.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,334 hrs · 33,742 cycles

AFTER CLOSING ENTRY DOOR, ENTRY DOOR ANNUNCIATOR LIGHT ON. WENT TO RESECURE DOOR AND UPON OPENING, EMERGENCY SLIDE BEGAN TO FALL OUT OF DOOR. MAINTENANCE INSPECTED GIRT BAR MECHANISM. NO DEFECTS NOTED AT THIS TIME. REPLACED L1 SLIDE ASSEMBLY IAW B767 MM 25-66-01-4. DOOR OPENED AND CLOSED AND SLIDE ARMED SMOOTHLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,046 hrs · 33,638 cycles

DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT SPARE BATTERY PACK INOP. REPLACED EMERGENCY LIGHT SPARE BATTERY IAW 33-51-00-5. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,035 hrs · 33,634 cycles

DURING MAINTENANCE INSPECTION, FOUND BATTERY PACK DEAD. REPLACED BATTERY PACK IAW 33-51-00-2.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,637 hrs · 33,137 cycles

PANEL SPLICE TEE BRACKETS UNDER PANELS 139CL AND 139DL WERE FOUND TO BE CORRODED BEYOND LIMITS. REPAIRED AREA IAW REA B653-44780.

Part: FITTING — DEFECTIVE (T/E FLAP) · airframe 39,558 hrs · 32,807 cycles

RIGHT OUTBOARD FLAP, OUTBOARD 3-10 LINK, AFT FITTING, WOULD NOT TAKE GREASE WHILE PERFORMING AD 2002-01-15. REMOVED AND REPLACED FITTING IAW B767 MM 27-51-274.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 38,584 hrs · 32,491 cycles

PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY WAS FLICKERING ABOVE THE CREW DOOR. REPLACED THE PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY IAW B767 AMM 33-51-00. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (COCKPIT) · airframe 38,064 hrs · 32,326 cycles

THE COCKPIT EMERGENCY EXIT LIGHT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT LIGHT SIGN.

Part: REGULATOR — MALFUNCTIONED (COCKPIT)

CAPTAIN'S AND FIRST OFFICER'S OXYGEN REGULATOR ABNORMAL OPERATION. REPLACED LOWER OXYGEN BOTTLE REGULATOR. PRESSURIZED AIRCRAFT AND CHECKED OXYGEN REGULATOR AND MASKS FOR FLOW. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLIGHT DECK EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK.