N366AA

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 96,271 hrs · 15,058 cycles

LEFT ELEVATOR SKIN PUNCTURE 12 INCHES OTBD OF FUSELAGE & 32 INCHES FWD TE. COMPLIED WITH PERMANENT REPAIR IAW EA COMP-55-037779 DATED 12/16/14 & SRM 51-70-17-0G.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 96,271 hrs · 15,058 cycles

GOUGE IN UPPER FLANGE OF STRINGER 35 RT BETWEEN FS 303 & 325. REPAIRED STRINGER IAW SRM 53-00-03.

Part: SKIN — DENTED (CARGO DOOR) · airframe 96,271 hrs · 15,058 cycles

BULK CARGO COMPARTMENT DOOR OUTER SKIN IS DENTED OUTER AT LOWER FWD CORNER. REPAIRED SKIN IAW SRM 52-30-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 96,271 hrs · 15,058 cycles

FUSELAGE SKIN IS DENTED & CREASED BETWEEN STATIONS 1351 & 1395 FROM STRINGER 28 RT & 29 RT. REPAIRED SKIN IAW EA 53-037822 DATED 12/17/14 & SRM.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,271 hrs · 15,058 cycles

FORWARD CARGO COMPARTMENT FLOOR WEB CORRODED INSIDE STOP ASSEMBLY AT FS 610 & RBL 6. R & R WEB IAW SRM 51-40-02. FASTENER SUBSTITUTION IAW EA B767-53-037716 DATED 12/11/14.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 96,271 hrs · 15,058 cycles

RIGHT OTBD FLAP WEDGE UPPER SKIN HAS MULTIPLE AREAS OF DELAMINATION. REPAIRED DELAMINATION’S IAW SRM 51-70-06-0G.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 96,271 hrs · 15,058 cycles

CABIN SEAT TRACK NR 4 NICKED & WORN ON TOP SURFACE AT FS 1025. R & R NR 4 SEAT TRACK IAW AARD 51-00-05-1.

Part: WEB — CORRODED (FUSELAGE) · airframe 96,271 hrs · 15,058 cycles

CORROSION ON WEB UNDER SCUFF PLATE AT R4 DOOR ENTRY WAY. REPAIRED WEB IAW EA 53-037743 DATED 12/11/2014.

Part: WEB — DAMAGED (FUSELAGE) · airframe 96,271 hrs · 15,058 cycles

AFT CARGO COMPARTMENT WEB HAS TOOLING DAMAGE 7 INCHES BELOW FLOORBEAM AT FUSELAGE STATION 1175 & LBL 5. REPAIRED WEB IAW SRM 51-70-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,271 hrs · 15,058 cycles

AFT CARGO COMPARTMENT FLOORBEAM UPPER CHORD CORRODED AT FS 1197+22 & RBL 46. R & R UPPER CHORD IAW AARD 51-00-05.

Part: WIRE — BROKEN (CABIN) · airframe 96,187 hrs · 15,046 cycles

SEAT MOUNTED EMER LIGHT AT SEAT 31H INOPERATIVE. REPAIRED BROKEN WIRE IAW SWPM CHAPTER 20. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 94,802 hrs · 14,820 cycles

LEFT NR 4 DOOR EMER EXIT SIGN UPPER AFT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR UPPER AFT EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 94,802 hrs · 14,820 cycles

FS3 LAVATORY, LOWER EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR FS3 LAVATORY LOWER EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: SLIDE — MALFUNCTIONED (OVERWING EXIT) · airframe 94,374 hrs · 14,750 cycles

DURING THE OVERWING SLIDE REACT, RT OVERWING SLIDE DOOR DROPPED, SQUIBS DEPLOYED BUT SLIDE DID NOT DEPLOY. REPLACING ALL SQUIBS & RT OVERWING SLIDE.

Part: LIGHT — DIRTY (R2 DOOR) · airframe 92,095 hrs · 14,389 cycles

RT NR 2 DOOR HANDLE ILLUMINATION LIGHT BULB INOPERATIVE. CLEANED & RESEATED LAMPS & CONTACTS ON LAMP HOLDER ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,095 hrs · 14,389 cycles

LT INNER AFT OVERWING LOWER EXIT MARKER 2 BULB SEGMENTS INOPERATIVE. REPLACED LAMPS FOR LT INNER AFT OVERWING LOWER EXIT MARKER. OPERATIONS CHECKED NORMAL.

Part: LENS — DETERIORATED (CABIN) · airframe 92,095 hrs · 14,389 cycles

AFT GALLEY BULKHEAD LT SIDE LOWER EXIT MARKER LENS IN POOR CONDITION. REPLACED LENS FOR AFT GALLEY BULKHEAD LT SIDE EXIT MARKER. OPERATIONS CHECKED NORMAL.

Part: LENS — DETERIORATED (CABIN) · airframe 92,095 hrs · 14,389 cycles

AFT GALLEY BULKHEAD RT LOWER EXIT MARKER LENS IN POOR CONDITION. REPLACED LENS FOR AFT BULKHEAD RT SIDE OVER EXIT MARKER. OPERATIONS CHECKED NORMAL.

Part: COMPUTER — FAULTY (EICAS) · airframe 90,979 hrs · 14,231 cycles

FORWARD CARGO COMPARTMENT FIRE INDICATION. CARGO FIRE BOTTLES WERE BLOWN. INSPECTION SHOWED NO INDICATION OF FIRE OR OVERHEAT CONDITION. PLACARDED COMPLETE CARGO FIRE EXTINGUISHING SYSTEM & CARGO SMOKE DETECTION IAW MEL. REPLACED LEFT EICAS COMPUTER THAT WAS FAULTY & CARGO FIRE BOTTLES AT ORD ON 07/20/2013. SYSTEM GROUND CHECKED NORMAL.

Part: CONTACT — DIRTY (EXTERIOR) · airframe 89,597 hrs · 14,022 cycles

LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS AND REPLACED LAMP FOR LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 89,597 hrs · 14,022 cycles

ICT INFLIGHT TUL-TUL (FCF). CREW REPORTED FIRE WARNING BELL WITH NO FIRE WARNING LIGHT INDICATION. FLIGHT DIVERTED ICT LANDED WITHOUT INCIDENT. RESET FIRE WARNING CIRCUIT BREAKERS AND ACCOMPLISHED FIRE WARNING TESTS. ALL TESTS NORMAL. REPLACED LEFT AFT LAVATORY SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — OUT OF ALIGNMENT (CARGO DOOR) · airframe 89,194 hrs · 13,948 cycles

STI - CREW REPORTED FORWARD CARGO DOOR OPEN LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED STI LANDED WITHOUT INCIDENT. REALIGNED CONNECTOR D4306P AND SECURED AT FORWARD ARM OF FORWARD CARGO DOOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RESOLVER — OUT OF LIMITS (TE FLAP) · airframe 89,097 hrs · 13,929 cycles

TUL - CREW REPORTED DURING ALT FLAP EXTENSION TRAILING EDGE DISAGREE LIGHT "T/E FLAP ASYM" DISPLAYED. EMERGENCY DECLARED FLIGHT LANDED TUL WITHOUT INCIDENT. ADJUSTED NUMBER FOUR RESOLVER THAT WAS OUT OF LIMITS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,097 hrs · 13,929 cycles

RIGHT FAILSAFE T FITTING LOWER ATTACH FASTENER LOCATION HAS EVIDENCE OF DEEP INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT T-FITTING PER ECO C3039AM 001 AND EA B767-53-027144.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,926 hrs · 13,906 cycles

RIGHT NUMBER 2 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR LOWER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,926 hrs · 13,906 cycles

LEFT NUMBER 1 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR LOWER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,926 hrs · 13,906 cycles

LEFT NUMBER 2 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR LOWER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,926 hrs · 13,906 cycles

RIGHT NUMBER 1 DOOR LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR LOWER EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: B-NUT — LOOSE (OIL SYSTEM) · airframe 88,907 hrs · 13,902 cycles

MIA - CREW REPORTED LEFT ENGINE OIL QUANTITY LOSS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND B-NUT ON OIL PRESSURE LINE ON BOTTOM OF OIL PUMP LOOSE. TIGHTENED B-NUT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 86,537 hrs · 13,516 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 22H MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT 22H. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,537 hrs · 13,516 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 22H INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 22H. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,537 hrs · 13,516 cycles

RIGHT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,548 hrs · 13,360 cycles

CORROSION ON FUSELAGE SKIN AT FUSE DRAIN PLUG HOLE AT TOP SIDE FORWARD END OF AFT CARGO BETWEEN STATIONS 1065 TO 1087 AT LEFT SIDE. ACCOMPLISHED HFEC WITH NO CRACKS FOUND. REMOVED CORROSION PER EA B767-53-020712.

Part: SPAR — CRACKED (LT PYLON) · airframe 85,548 hrs · 13,360 cycles

LEFT PYLON FORWARD MID SPAR WEB INBOARD EDGE AT STATION 211.25 TO 220 CRACKED. ACCOMPLISHED DOUBLER REPAIR PER EA 020755.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 85,548 hrs · 13,360 cycles

INTERCOSTAL CRACKED STATIONS 742 TO 764 AT LEFT BUTTLINE 40. REPLACED INTERCOSTAL PER AARD 53-30-00

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,548 hrs · 13,360 cycles

J-CAP STATION 1197 CORRODED. REPLACED J-CAP PER SRM 51-40-02.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 84,873 hrs · 13,262 cycles

BUSHINGS FOR LEFT PYLONS INBOARD AND OUTBOARD LUGS MIGRATED. CLEANED LUG BORES AND BUSHINGS AND RE-INSTALLED PER EA B767-54-019263.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 82,866 hrs · 12,960 cycles

JFK - CREW REPORTED CAPTAINS FORWARD WINDSHIELD SHATTERED. FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAINS FORWARD WINDOW AND WINDOW HEAT CONTROL UNIT (MPN 6240664). SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 79,663 hrs · 12,397 cycles

DEEP DENT ON THE FUSELAGE SKIN AT STATION 1366.5 BETWEEN STRINGERS 31 AND 32 RIGHT. INSTALLED DOUBLER PER EA B767-53-010270.

Part: SENSOR — FAULTY (LE SLAT) · airframe 78,215 hrs · 12,147 cycles

ON APPROACH INTO DFW WHEN EXTENDING FLAPS FROM 15-20, SLAT ASYMMETRY MESSAGE DISPLAYED ON EICAS. LANDED WITHOUT INCIDENT AT 160 KNOTS AMD NORMAL SINK RATE. REPEAT. REPLACED SENSORS S285 AND S286.

Part: FSEU — FAULTED (LE SLAT) · airframe 78,204 hrs · 12,146 cycles

ON APPROACH INTO CDG EXTENDED TRAILING EDGE FLAPS FROM 15 TO 20 DEGREES LEADING EDGE SLAT ASYMMETRY MESSAGE ILLUMINATED. LANDED WITHOUT INCIDENT AT 150 KNOTS. REPLACED FLAP SLAT ELECTRONIC UNIT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,895 hrs · 12,077 cycles

EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP AT LEFT NUMBER FOUR DOOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 74,300 hrs

MIA - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP AT RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 74,300 hrs

MIA - EXTERIOR EMERGENCY LIGHT AT L3 DOOR INOPERATIVE. REPLACED LAMP AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PSEU — FAULTED (SLATS)

INFLIGHT - CREW REPORTED INTERMITTENT SLAT ASYMMETRY INDICATION ON FINAL APPROACH. LANDED BOS WITHOUT INCIDENT. FOUND PROXIMITY SENSOR ELECTRONIC UNIT FAULT ON CARD 13 AND FAULT ON FLAP HANDLE. ADJUSTED FLAP HANDLE AND REPLACED PROXIMITY SENSOR ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (BS 440 S36) · airframe 73,847 hrs · 11,430 cycles

AFW - FUSELAGE SKIN AT STATION 440 AT STRINGER 36 JUST AFT OF THE SECTION 41/43 BUTT SPLICE AND ABOVE A SKIN LAP JOINT HAS CORROSION BLENDED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767 3337.

Part: SKIN — CORRODED (BS 437 S36) · airframe 73,847 hrs · 11,430 cycles

AFW - FUSELAGE SKIN AT STATION 437 AT STRINGER 36 JUST AFT OF THE SECTION 41/43 BUTT SPLICE AND ABOVE A SKIN LAP JOINT HAS CORROSION BLENDED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767 3337.

Part: SKIN — CORRODED (BS 1087) · corrosion level 2 · airframe 73,847 hrs · 11,430 cycles

AFW - CORROSION WAS FOUND AT THREE LOCATIONS JUST AFT OF STATION 1087 ON THE INTERIOR SURFACE OF FUSELAGE SKIN. BLENDING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767-3333.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,847 hrs · 11,430 cycles

AFW - OUTER CHORD LOWER MAIN SILL AT FORWARD CARGO DOOR CORRODED. REMOVED AND REPAIRED CORROSION BY BLENDING AREA PER SRM 51-10-02 AND MRB 767-3335.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 73,847 hrs · 11,430 cycles

AFW - FORWARD CARGO DOOR SILL WEB HAD CORROSION BLENDED AT LOWER FORWARD OUTBOARD SIDE AT STATION 615. REPAIRED IN ACCORDANCE WITH MRB 767 3336.

Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 73,847 hrs · 11,430 cycles

AFW - FLOORBEAM AT STATION 325 HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767 3334.

Part: GASKET — LEAKING (NR 2 ENGINE) · airframe 71,413 hrs

CDG - ON ARRIVAL FOUND NUMBER TWO ENGINE FUEL LEAK. REPLACED GASKET BETWEEN NUMBER TWO ENGINE FUEL PUMP AND FUEL INLET HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 36H)

JFK - EMERGENCY LIGHT AT SEAT 36H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (HYD SYSTEM)

LHR INFLIGHT T83/17DEC FRA TO ORD - LEFT HYDRAULIC QUANTITY INDICATION AND LOSS OF LEFT HYDRAULIC PUMP DURING CRUISE. DIVERTED TO LHR AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE PRIMARY HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STIFFENER — DAMAGED (BS 1045-1060)

AFW - PRESSURE DECK LONGITUDINAL STIFFENER HAS TWO HOLES IN THE UPPER FLANGE AT RIGHT BUTTLINE 5.75 STATION 1045 AND 1060. REPAIRED HOLES FOR THE PRESSURE DECK LONGITUDINAL STIFFENER IN THE UPPER FLANGE AT RIGHT BUTTLINE 5.75 STATION 1045 AND 1060.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LEFT OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY CEILING LIGHT AT SEATS 28AB INOPERATIVE. RELAMPED EMERGENCY CEILING LIGHT AT SEATS 28AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT ON BACK BULKHEAD OF MID GALLEY DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY ON BACK BULKHEAD OF MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 40H INOPERATIVE. SECURED LIGHT CABLE FOR EMERGENCY LIGHT AT SEAT 40H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHTS DAMAGED AT SEATS 28H/29H/31H. REPAIRED EMERGENCY LIGHT ASSEMBLY AT SEATS 28H/29H/31H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — DAMAGED (FUSELAGE)

AFW - FUSELAGE FRAME WEB IN FORWARD CARGO COMPARTMENT HAD HEAT DAMAGE CAUSED BY FIRE. AREA AFFECTED WAS 31 INCHES BY 16 INCHES AT STATION 654 AND 88. REPAIRED FRAME PER MRB 767-2717.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

SFO - RIGHT HAND OVERWING SLIDE BOTTLE PRESSURE IS LOW. REPLACED RIGHT HAND OVERWING SLIDE BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: INDICATOR — INOPERATIVE (COCKPIT)

FIRST OFFICERS HSI DISPLAY INOPERATIVE SHORTLY AFTER TAKEOFF DISPLAY INTERMITTENT FOR .5 OF FLIGHT, INOPERATIVE REMAINDER OF FLIGHT. TROUBLESHOT FOUND FAULTY SYMBOL GENERATOR. REPLACED RIGHT SYSTEM GEN AS PER MM. ACCOMPLISHED ALL REQ CHECKS OPS CHECKED NORMAL OF EHSI SYSTEM. (M)

Part: INDICATOR — FAILED (COCKPIT)

FIRST OFFICERS HSI NAV DISPLAY INOPERATIVE. WHEN AIRCRAFT POWER SWITCHED TO APU DISPLAY CAME BACK ON. RE-RACKED FIRST OFFICERS HSI, OPS CHECK NORMAL. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - UPPER SURFACE OF FLOORBEAM STATION 764 HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION PER REF B. VERIFY CORROSION COMPLETELY REMOVED. FABRICATE AND INSTALLED REPAIR STRAP. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 347 HAS CORROSION ON UPPER SURFACE REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS, REQUEST ENGINEER APPROVAL TO REPAIR PER SKETCH. REMOVED EXISTING REPAIR STRAPS TO INCORPORATE SINGLE STRAP. REMOVED CORROSION PER REF B AND VERIFIED COMPLETELY REMOVED. FABRICATED REPAIR STRAP AND ENSURED 3 ROWS OF FASTENERS. ALODINED AND PRIMED. FILLED BLEND. INSTALLED REPAIR STRAP WITH SEALANT. (M)

Part: INVERTER — OVERHEATED (E/E BAY)

AFW - AT SOME TIME DURING IN SERVICE, APPARENT OVERHEAT OF STATIC INVERTER CAUSE SMOKE AND HEAT DISCOLORATION TO C3-1 RACK AND WIRING. REF E-58 NR 3687296, REMOVED, INSPECTED, REINSTALLED AND 0A5 CK E3-1 RACK. NO APPARENT DAMAGE FOUND JUST DISCOLORATION. (M)

Part: WIRE — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, PATH LIGHT AT SEAT 38H INOPERATIVE. REPAIRED EMERGENCY PATH LIGHTING WIRE AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HOUSING — DEFECTIVE (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE LIGHTS AT SEAT 22A INOPERATIVE. REPLACED EMERGENCY LIGHT HOUSING ASSEMBLY AT SEAT 22A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, FOUND LEFT SIDE EMERGENCY ESCAPE LIGHTS AT ROW 2 THROUGH ROW 8 INOPERATIVE. REPLACED EMERGENCY ESCAPE LIGHTS AT ROW 2 THROUGH ROW 8 BATTERY PACK AND POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — MALFUNCTIONED (L/E SLAT)

MIA - FLT 1772 - EN ROUTE SJU-JFK, AIRCRAFT EXPERIENCED L/E ASYMMETRIC MESSAGE ON EICAS. DIVERTED FLIGHT TO MIA LANDING WITHOUT INCIDENT, NON-OVERWEIGHT. MIA ACCOMPLISHED FIM TASK 32-09-03 FAULT CODE 10 AND 285 WAS DETECTED. REPLACED PSEU DUE TO CODE 10 PROCEDURES AND INSPECTED LEFT NR 4 SLAT PROP SENSORS. NO FAULTS NOTED. OPERATIONAL CHECK PERFORMED ON FLAP/SLATS. SYSTEM CHECKED NORMAL. (M)

Part: TERMINAL — BROKEN (R2 DOOR)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT TERMINAL END AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — DEFECTIVE (FUEL SYSTEM)

DFW - FLT 911 - EN ROUTE LAX-MIA - THIRTY MINUTES INTO FLIGHT RIGHT FUEL TANK INDICATED 2000 LBS FUEL IMBALANCE. DETERMINED CROSSFEED VALVE PROBLEM AND DIVERTED TO DFW. LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND REPLACED LEFT DEFUEL ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2H THROUGH 8H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

LHR - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT AT SIDE WALL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPS. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LHR - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPS. (M)

Part: SMOKE — DETECTED (CABIN)

LAX - FLT 34 - DURING INITIAL CLIMB, FLIGHT ATTENDANT REPORTED SMOKE SMELL IN CABIN. DECLARED EMERGENCY, RETURNED AND LANDED LAX WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT AND RAN ENGINES. NO SMELL NOTED. UNABLE TO DUPLICATE SMOKE SMELL. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT ROW 26H INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT SEAT LIGHT AT ROW 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROW 19)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 19 INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DISCONNECTED (ROW 23)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23 INOPERATIVE. CONNECTED EMERGENCY EXIT LIGHT WIRE AT SEAT 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

ORY - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTING AT SEAT 24B INOPERATIVE. REPAIRED EMERGENCY EXIT ESCAPE LIGHTING WIRE AT SEAT BASE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (LT ENGINE)

SFO - FLT 0037 - LT BLEED DUCT LEAK LIGHT ON TAKEOFF. LIGHT EXTINGUISHED AFTER ENGINE BLEED VALVE CLOSED. INSPECTED AND FOUND AFT GROUND AIR SUPPLY CHECK VALVE OPEN. REMOVED AND REPLACED GROUND AIR SUPPLY CHECK VALVE. LEAK CHECK GOOD. ACCOMPLISHED HIGH POWER RUN. NO PROBLEMS NOTED. (X)

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT)

MVD - GOT FORWARD EQUIPMENT VALVE EICAS WITH EQUIPMENT COOLING VALVE LEFT ON OVERHEAD PANEL AFTER TAKEOFF. VALVE REMAINED ILLUMINATED WHEN EQUPMENT COOLING SWITCH WAS PLACED TO STANDBY, SHORTLY AFTER FORWARD EQUIPMENT OVERHEAT EICAS ILLUM. FOUND ON PANEL P6-3 C/B POPPED, LT BUS SECT 1 115V AC. RESET C/B ERASED. RAN ENGINES ALL SYSTEMS NORMAL. NO STATUS MSG EQUIP COOLING NORMAL. BPCU BITE PASSED OK. ALL SYSTEMS NORMAL OK FOR SERVICE. (M)

Part: IDG — FAILED (LT ENGINE)

ORD - FIVE HOURS INTO FLIGHT AT FL340, THE LEFT GEN DRIVE DISCONNECTED WITH THE LEFT GEN FIELD. STARTED APU TO RESTORE UTILITY/GALLEY BUSES. REPLACED LEFT IDG PER MM CPT 24, GROUND RUN OP CHECK NORMAL. NO LEAKS DISCONNECT CHECK OK. (M)

Part: FRAME — CORRODED (BS 1197/110)

AFW - FOUND AND BLENDED OUT AN AREA OF CORROSION ON THE LOWER SURFACE OF THE FRAME INNER CHORD FORWARD FLANGE IN THE AFT CARGO COMPARTMENT. THE BLEND-OUT EXCEEDS SRM MAXIMUM LIMITS. REFINISHED BLENDED AREA PER SRM 53-00-07. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1479. TST: 27,633.03 HOURS. CYCLES: 4,256. (X)

Part: FLOOR BEAM — CORRODED (BS 1480)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE MAIN CABIN FLOOR BEAM. THE BLEND-OUTS EXCEED SRM 53-00-51 MAXIMUM LIMITS. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 1/2 HARD STAINLESS STEEL. PRIMED REPAIR STRAP AND FLOOR BEAM. APPROVED BY ENGINEERING PER MRB 767-1471. TST: 27,633.03 HOURS. CYCLES: 4,256. (X)

Part: SILL — CORRODED (CARGO DOORWAY)

AFW - FOUND AND BLENDED OUT AN AREA OF CORROSION ON THE INNER SURFACE OF THE FWD CARGO DOOR SILL OUTER CHORD. THE BLEND-OUT EXCEEDS MAXIMUM LIMITS OF SRM 53-00-15, FIGURE 101. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRR 767-1477. TST: 27,633.03 HOURS. CYCLES, 4,256. (X)

Part: SILL — CORRODED (BS 590)

AFW - FOUND AND BLENDED OUT CORROSION ON THE INNER SURFACE OF THE FORWARD CARGO DOOR SILL OUTER CHORD. THE BLEND-OUT EXCEEDS SRM MAXIMUM LIMITS. REFINISHED THE BLENDED AREA PER SRM 53-00-15. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1480. TST: 27,633.03 HOURS. CYCLES: 4,256. (X)

Part: SUPPORT — CORRODED (L2 DOORWAY)

AFW - FOUND AND BLENDED OUT TWO AREAS OF CORROSION ON THE FLOOR SUPPORT TEE AT THE L2 DOOR LOWER SILL. BLEND-OUTS EXCEED SRM MAXIMUM LIMITS. FILLED AND REFINISHED BLENDED AREAS PER SRM 53-00-15. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1472. TST: 27,633.05 HOURS. CYCLES: 4,256. (X)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLENDING. FABRICATE .050 STRAP FROM 301 STAINLESS AND INSTALL WET WITH BMS 5095 PER ENGINEERING MRB 767-1476. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLENDING. FABRICATED .050 STRAP FROM 301 STAINLESS AND INSTALLED WET WITH BMS 5095 PER ENGINEERING MRB 767-1475. (M)

Part: FLOOR BEAM — CORRODED (BS 390)

AFW - FOUND AND BLENDED CORROSION ON THE UPPER SURFACE OF THE UPPER FLANGE OF THE FLOOR BEAM. REFINISHED BLENDED AREA PER SRM 53-00-51. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1485. CYCLES: 4,256. (X)

Part: FLOOR BEAM — CORRODED (BS 894-999)

AFW - FLOOR BEAM AT LBL 33 HAD CORROSION AT TWO LOCATIONS BEYOND SRM LIMITS. REPAIRED PER MRB NBR 767-1229. (M)

Part: WIRE — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY LIGHT INOPERATIVE IN BUSINESS CLASS CABIN LEFT SIDE ROWS 7 THROUGH 12 AND IN MAIN CABIN LEFT SIDE ROWS 37 THROUGH 42. RESECURED LOOSE EMERGENCY LIGHT WIRES AT ROW 12 AND ROW 42. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 7H AND 12H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 7H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RIGHT AISLE BETWEEN PASSENGER SEAT ROWS 7 AND 12 INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INVERTER — DEFECTIVE (CABIN)

LHR - FLT 0096 - EN ROUTE ORD/MXP, ELECTRICAL SMOKE OF UNKNOWN SOURCE WAS DETECTED IN THE CABIN. AIR INTERRUPTED AND LANDED LHR WITHOUT INCIDENT. REPLACED STATIC INVERTER PER MM24-33-03-04. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT AFT FLIGHT ATTENDANT STATION AND 36H-37H INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTORS AT AFT PARTITION AND 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, SEAT MOUNTED EMERGENCY EXIT LIGHT WIRING HARNESS BROKEN AT PAX SEAT 12J. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 12J. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS INOPERATIVE FROM PAX SEAT ROWS 8AB TO 23AB. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)