N351AA

Part: CONTACT — DIRTY (CABIN) · airframe 112,191 hrs · 18,446 cycles

CEILING EMER LIGHT AT 11H IS DIM. CLEANED LAMP CONTACT & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-04. SYS CHECKED NORMAL.

Part: LIGHT — DIM (CABIN) · airframe 112,191 hrs · 18,446 cycles

SEAT MOUNTED EMER LIGHT AT 22H IS DIM. R & R LIGHT ASSEMBLY IAW AMM 33-51-10. SYS CHECKED NORMAL.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 5 AT FS 531.71 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 1 AT FS 487.71 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 2 AT FS 500.29 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 9 AT FS 573.71 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 12 AT FS 608.29 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 4 AT FS 522.29 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 8 AT FS 564.29 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 3 AT FS 509.71 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 11 AT FS 595.71 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 7 AT FS 551.71 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 10 AT FS 586.29 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 111,192 hrs · 18,272 cycles

FORWARD CARGO DOOR FITTING NR 6 AT FS 544.29 CORRODED INSIDE PIN HOLE. R & R FITTING IAW AARD 51-00-05 & AMM 52-33-00.

Part: STIFFENER — CRACKED (NR 2 PYLON) · airframe 111,192 hrs · 18,272 cycles

FOUND DIAGONAL STIFFENER CRACKED ON THE NR 2 PYLON JUST FWD OF THE MID SPAR BULKHEAD. R & R STIFFENER IAW AARD 51-00-05-1 & DWG 311T2400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 111,192 hrs · 18,272 cycles

AFT CARGO COMPARTMENT INTERCOSTAL BETWEEN FS 1307 & 1329 AT RBL 12 IS CRACKED. R & R INTERCOSTAL IAW AARD 53-60-53-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 111,192 hrs · 18,272 cycles

AFT CARGO COMPARTMENT INTERCOSTAL BETWEEN FS 1285 & 1307 AT RBL 12 IS CRACKED. R & R INTERCOSTAL IAW AARD 53-60-53-01. .

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,192 hrs · 18,272 cycles

BULGING FUSELAGE SKIN AT STATIONS 434 BETWEEN STINGER 37 RT & 38 RT WAS FOUND TO BE CORROSION. REPAIRED SKIN IAW SRM 53-00-01 & EA 53-038386 DATED 2/15/2015.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 111,192 hrs · 18,272 cycles

FUSELAGE SKIN DAMAGED AT STRINGER 37 LT & STATION 1197+70. REPAIRED SKIN IAW SRM 53-00-01-2R, PROCEDURE 1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 111,013 hrs · 18,241 cycles

L4 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED THE L4 DOOR EXTERIOR EMER LIGHT. OPERATIONAL CHECKED GOOD IAW AMM 33-51-03.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 109,374 hrs · 17,960 cycles

LEFT NR 1 LOWER EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 1 LOWER EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,894 hrs · 17,878 cycles

EMERGENCY LIGHT AT SEAT 22H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 22H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,894 hrs · 17,878 cycles

EMERGENCY LIGHT AT SEAT 24H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 24H. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,894 hrs · 17,878 cycles

EMERGENCY LIGHT AT SEAT 23H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 23H. OPERATIONS CHECKED NORMAL.

Part: STIFFENER — CRACKED (LT PYLON) · airframe 108,430 hrs · 17,801 cycles

LEFT PYLON OTBD SIDE, STIFFENER CRACKED AT STATION 285. ACCOMPLISHED REPAIR IAW AARD 54-52-02-2.

Part: SOCKET — DIRTY (EXTERIOR LIGHT) · airframe 108,427 hrs · 17,800 cycles

RIGHT NR 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED SOCKET & REPLACED LAMP, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,042 hrs · 17,743 cycles

29H SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 29H SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,042 hrs · 17,743 cycles

26B SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR 26B SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — NOT SEATED (EXIT SIGN) · airframe 108,042 hrs · 17,743 cycles

21A OVERWING EXIT SIGN IS DIM. RESEATED LAMP, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,042 hrs · 17,743 cycles

41H SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 41H SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,042 hrs · 17,743 cycles

29B SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 29B SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,042 hrs · 17,743 cycles

25H SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 25H SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,042 hrs · 17,743 cycles

28H SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR 28H SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 108,042 hrs · 17,743 cycles

21A EXIT IDENTIFIER SIGN IS DIM. REPLACED LAMP FOR 21A EXIT IDENTIFIER SIGN, OPERATIONS CHECKED NORMAL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 107,547 hrs · 17,660 cycles

MEM INFLIGHT MIA-SFO. CREW REPORTED BIRD STRIKE TO CAPTAINS LT FWD WINDSHIELD. EMERGENCY DECLARED FLIGHT DIVERTED MEM LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAINS LT FWD WINDSHIELD. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 107,274 hrs · 17,613 cycles

FUSELAGE SKIN AT STATION 347 & STRINGER 22 RT DAMAGED. INSTALLED PERMANENT REPAIR IAW EA B767-53-032830.

Part: LENS — LOOSE (CABIN) · airframe 106,360 hrs · 17,469 cycles

EMERGENCY LIGHT COVER LOOSE AT LT NR 1 DOOR. RESECURED EMERGENCY LIGHT COVER AT LT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 106,217 hrs · 17,447 cycles

DENT ON FS AT STATION 1228 & STRINGER 36 LT. DENT DAMAGE IS OVER A LAP SPLICE. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R REPAIR 12.

Part: CONNECTOR — LOOSE (CABIN) · airframe 104,142 hrs · 17,115 cycles

SEATS 30AB AND 31AB EMERGENCY LIGHTS INOPERATIVE. REPOSITIONED AND SECURED CONNECTOR AT SEAT 31AB. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,497 hrs · 17,011 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,489 hrs · 17,010 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 30B INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 30B. OPS CHECK NORMAL.

Part: LIGHT — UNSECURE (EXIT SIGN) · airframe 103,489 hrs · 17,010 cycles

LEFT NUMBER 1 EXIT SIGN BOTTOM LIGHTS INOPERATIVE. SECURED LEFT NUMBER 1 EXIT SIGN BOTTOM LIGHTS HOLDER. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,489 hrs · 17,010 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 31B INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 31B. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 103,489 hrs · 17,010 cycles

RIGHT NUMBER 1 EXIT SIGN BOTTOM LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 EXIT SIGN BOTTOM LIGHT. OPS CHECK NORMAL.

Part: PROCESSOR — INOPERATIVE (FUEL SYSTEM) · airframe 102,247 hrs · 16,802 cycles

ORD INFLIGHT DFW-FRA. CREW REPORTED CENTER FUEL QUANTITY INDICATOR AND TOTAL QUANTITY INDICATOR INOPERATIVE. EMERGENCY DECLARED FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE FUEL QUANTITY PROCESSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 102,135 hrs · 16,787 cycles

DENT WITH GOUGE AT STATION 356, 1/2 INCH ABOVE STRINGER 22 RIGHT. INSTALLED DOUBLER REPAIR PER FEA AFW7867.

Part: SKIN — BULGED (FUSELAGE) · airframe 100,162 hrs · 16,440 cycles

UPPER FUSELAGE SKIN BULGING AROUND FASTENER AT STATION 446 ON STRINGER 6 RIGHT. REMOVED FASTENER AT STRINGER 6 RIGHT STATION 446 AND REMOVED EXCESS MATERIAL FROM BETWEEN STRINGER AND SKIN WHICH RELIEVED BULGE IN SKIN. HFEC HOLE INSPECTION REVEALED INDICATIONS OF A CRACK, REAMED HOLE TO .2782 PER EA B767-53-021441, SUBSEQUENT HFEC REVEALED NO CRACK. INSTALLED FASTENER PER EA B767-53-021441.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 100,162 hrs · 16,440 cycles

ULTRASONIC INSPECTION OF NUMBER 5 SLAT TRAILING EDGE WEDGE SHOWS A DISBOND INDICATION AT 1 INCH TO 1.75 INCH FROM INBOARD END AND 2 INCHES TO 3.5 INCHES FORWARD OF TRAILING EDGE. INSTALLED REPAIR DOUBLER PER SRM 51-70-10-29.

Part: WEB — CRACKED (LT PYLON) · airframe 100,162 hrs · 16,440 cycles

LEFT PYLON LOWER TORQUE BOX SKIN AT GENERATOR FEEDER CABLE PASS THROUGH HAS A POSSIBLE CRACK ON THE INBOARD FORWARD CORNER. INSTALLED DOUBLER REPAIR PER EA COMP767-54-021544.

Part: SKIN — CRACKED (PYLON) · airframe 100,162 hrs · 16,440 cycles

PYLON HAS VISUAL CRACK INDICATIONS IN THE UPPER PYLON SKIN AT THE GENERATOR CABLE FEED THRU LOCATION. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.

Part: WEB — CRACKED (PYLON) · airframe 100,162 hrs · 16,440 cycles

CRACK IN PYLON AT PASS THROUGH FOR INTEGRATED DRIVE GENERATOR FEEDER CABLES. REPAIRED PER AARD 54-52-01-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 100,162 hrs · 16,440 cycles

INTERCOSTAL AT STATION 760 RIGHT BUTTLINE 72 CRACKED. INSTALLED DOUBLER REPAIR PER SRM 51-70-13.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 100,162 hrs · 16,440 cycles

NUMBER 9 SLAT TRAILING EDGE WEDGE SHOWS DISBOND INDICATION. INSTALLED HOT BOND REPAIR DOUBLER PER SRM 51-70-10-2R.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 100,162 hrs · 16,440 cycles

NUMBER 10 SLAT TRAILING EDGE WEDGE SHOWS DISBOND INDICATION. INSTALLED DOUBLER PER SRM 51-70-10.

Part: FLAP — DEBONDED (RT WING) · airframe 100,162 hrs · 16,440 cycles

RIGHT TRAILING EDGE OUTBOARD FLAP HAS SMALL DELAMINATION 172 INCHES FROM OUTBOARD END. ACCOMPLISHED HOT BONDED REPAIR PER SRM 57-53-01.

Part: FLAP — DEBONDED (RT WING) · airframe 100,162 hrs · 16,440 cycles

RIGHT TRAILING EDGE OUTBOARD FLAP HAS SMALL DELAMINATION 80 INCHES FROM OUTBOARD END. ACCOMPLISHED HOT BONDED REPAIR PER SRM 57-53-01.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 100,162 hrs · 16,440 cycles

NUMBER 1 SLAT TRAILING EDGE WEDGE INBOARD END SHOWS DISBOND INDICATION. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.

Part: SKIN — DEBONDED (TE FLAP) · airframe 100,162 hrs · 16,440 cycles

LEFT OUTBOARD FLAP, LOWER SURFACE JUST OUTBOARD OF MID CANOE DISBONDED. REMOVED DAMAGE AND REPAIRED AREA PER SRM 51-70-07-0G.

Part: SLAT — DEBONDED (LT WING) · airframe 100,162 hrs · 16,440 cycles

NUMBER 8 SLAT TRAILING EDGE INBOARD END DISBONDED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 99,474 hrs · 16,322 cycles

TUL - CREW REPORTED LEFT ENGINE COMPRESSOR STALLED DURING DECELERATION. MULTIPLE, RAPID POPS WERE HEARD. LEFT EXHAUST GAS TEMPERATURE WAS HIGHER THAN RIGHT BUT NOT OUT OF LIMITS. EMERGANCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT TUL ON 10/30/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GCU — FAILED (RIGHT) · airframe 95,200 hrs · 15,651 cycles

JFK - INFLIGHT DFW-LHR. CREW REPORTED RIGHT ENGINE GENERATOR FAILED IN FLIGHT. EMERGENCY DECLARED DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,160 hrs · 15,645 cycles

FORWARD CARGO DOOR CUTOUT LOWER SILL INNER CHORD BETWEEN STATIONS 504 AND 506 CORRODED. ACCOMPLISHED BORE/FASTENER REWORK PER EA 767-53-012752.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,160 hrs · 15,645 cycles

CORROSION WAS FOUND ON THE LEFT NUMBER 2 DOOR INNER CHORD 146T8022-10 UPPER SURFACE COMMON TO THE SPLASH GUARD INSTALLATION BETWEEN APPROXIMATELY STATION 1506 AND STATION 1528. THE CORROSION WAS BLENDED AND REPAIR WAS ACCOMPLISHED PER EA B767-53-012784.

Part: ALTIMETER — FAULTY (COCKPIT) · airframe 91,792 hrs · 15,060 cycles

AT FLIGHT LEVEL 310 AND FLIGHT LEVEL 280 CAPTAINS ALTIMETER WAS ON ASSIGNED FLIGHT LEVEL. FIRST OFFICERS ALTIMETER WAS 160 FEET LOWER. CENTER ALTIMETER WAS 400 FEET HIGHER. AIRCRAFT AIR INTERRUPTED INTO MIA. LANDED OVERWEIGHT BUT SMOOTH. OVERWEIGHT INSPECTION ACCOMPLISHED WITH NO ANOMALIES NOTED. REPLACED FIRST OFFICERS PITOT STATIC PROBE, ALTIMETER INDICATOR, AND RIGHT AIR DATA COMPUTER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 90,404 hrs

SFO - RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,404 hrs

SFO - RIGHT EMERGENCY EXIT AFT OF WHEEL WELL INOPERATIVE. REPLACED LAMP FOR RIGHT EMERGENCY EXIT AFT OF WHEEL WELL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT IN AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN AFT GALLEY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

MIA - LEFT AISLE FIRST CLASS EMERGENCY LIGHT IN CEILING INOPERATIVE. REPLACED LAMP IN LEFT AISLE FIRST CLASS CEILING.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT IN AFT AT SEAT 4A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN AFT AT SEAT 4A.

Part: FSEU — INOPERATIVE (TE FLAPS) · 87,551 cycles

HNL INFLIGHT T5/19SEP. CREW REPORTED FLAPS WOULD NOT EXTEND DURING DESCENT. LANDED HNL WITHOUT INCIDENT. REPLACED FLAP SLAT ELECTRONICS UNIT (FSEU). SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 85,935 hrs

DFW - EMERGENCY LIGHT AT SEATS 10H AND 11H INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEATS 10H AND 11H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CIRCUIT CARD — INOPERATIVE (FIRE DETECTOR)

CDG INFLIGHT T065/28DEC ZRH TO JFK - FIRE OVERHEAT SYSTEM WARNING FAILED. NUMBER TWO ENGINE FIRE DETECTION LOOP 2 PREVIOUSLY PLACARDED. CREW UNABLE TO RESET. LANDED CDG WITHOUT INCIDENT. REPLACED FIRE DETECTOR SYSTEM CARD 644501 AND TEMP CONTROL CARD 285T0094-6 AS PRECAUTIONARY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SILL — CORRODED (CARGO DOORWAY)

AFW FORWARD CARGO DOOR CUTOUT LOWER MAIN SILL, OUTER CHORD HAS CORROSION REMOVAL ON INBOARD SURFACE OF VERTICAL LEG. AREA IS 1 INCH BY 2.2 INCHES WITH A DEPTH OF 0.098 AND 0.100 INCH. BLEND CORROSION OVERSIZE FASTENER HOLES. PERFORM 10 TIMES VISUAL AND HIGH FREQUENCY EDDY CURRENT INSPECTIONS. SPOTFACE BOLT HOLES AND BLEND AREAS, ALODINE, PRIME, AND INSTALL SPOTFACE WASHER AND ALUMINUM FASTENER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT AFT DOOR M10722 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT AFT DOOR M10722. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

JFK - EXTERIOR EMERGENCY LIGHT AT AFT RIGHT SIDE OF AIRCRAFT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT AFT RIGHT SIDE OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

SFO EXTERIOR EMERGENCY LIGHT AT RIGHT HAND SIDE OVERWING INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT AT RIGHT HAND SIDE OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

MIA - EMERGENCY PATH LIGHTS AT LEFT SEAT ROWS 30 TO 34 INOPERATIVE. RELAMPED EMERGENCY PATH LIGHTS AT LEFT ROWS 30 TO 34. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (L/E SLAT)

AFW - NUMBER EIGHT SLAT LEADING EDGE SKIN INBOARD EDGE HAD SMALL CRACK AT STATION OSS418.426. AREA IS 1 11/16 INCH BY 15/16 INCH AND 1 AND 11/16 INCHES LONG. CUTOUT DAMAGE. INSPECT CUTOUT EDGES FOR CRACKS. ENSURE CUTOUT DOES NOT EXCEED CONDITION DESCRIPTION. FABRICATE A DOUBLER FOR CUTOUT USING 0.071 INCH 7075T6 CLAD PER THE B767 SRM 57 43 01 2R FIG 201 WITH THE FOLLOWING DEVIATION. MAKE DOUBLER EXTERNAL ONLY AND SIZE IT TO EXTEND A MINIMUM OF THREE ROWS AROUND CUTOUT. AERO TAPER THE EDGES OF DOUBLER PER B767 SRM 51 10 01 0G. INSTALL DOUBLER USING THE B767 SRM 57 43 01 2R FIG 201. EXCEPT USING A MINIMUM OF THREE ROWS OF FASTENERS. DO NOT USE ANY FASTENERS WEAKER THAN A D RIVIT.

Part: SPAR CAP — CORRODED (T/E FLAP)

AFW - LEFT HAND INBOARD MAIN FLAP LOWER AFT SPAR LOWER SURFACE AT IFS 19 HAD CORROSION. AREA WAS FOUR INCHES BY 1.7 INCHES WITH A DEPTH OF .027 INCH. VERIFY THE CORROSION WAS COMPLETELY REMOVED. ACCOMPLISH EDDY CURRENT INSPECTION ON BLENDED AREA FOR CRACKS. ROTOPEEN BLENDED AREA. REFINISH THE BLENDED AREA WITH ALODINE AND TWO COATS BMS 10 11 PRIMER AND RETURN TO SERVICE WITH NOTED CONDITIONS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS AT ROWS 20AB TO 24AB INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR EMERGENCY LIGHTS AT ROWS 20AB TO 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: NUT — LOOSE (SCAV PUMP)

DFW - ABOUT 150 MILES FROM DFW OIL QUANTITY WENT TO ZERO AND OIL PRESSURE WENT TO APPROXIMATELY 23 PSI IN THE AMBER BAND. SECURED RIGHT HAND ENGINE PER QHR AS A PRECAUTION. NO OIL TEMPERATURE OR ENGINE TEMPERATURE ON ENGINE TEMPERATURE RED INDICATIONS. LANDED DFW WITHOUT INCIDENT. FOUND LOOSE NUTS ON OIL SCAVANGER PUMP. TIGHTENED LOOSE NUTS AND REFILLED OIL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPAR — PUNCTURED (RT WING)

AFW - RIGHT WING FORWARD SPAR PUNCTURED AT STATION 1028. AREA IS 1 INCH BY 0.125 INCH. TRIMMED OUT THE DAMAGED PORTIONS OF SPAR WEB BETWEEN FSS 1022 AND 1032 AND SPLICED IN A NEW WEB SEGMENT FABRICATED FROM 0.140 INCH THINK 2024T3 ALUMINUM. TWO 0.080 INCH THICK 2024T3 SPLICE PLATES ARE INSTALLED AT EACH SPLICE LOCATION. BOTH SPLICE PLATES PICK UP A MINIMUM OF TWO ROWS OF FASTENERS ON EACH SIDE OF THE WEB CUT LINES AND THE SPLICE PLATE ADJACENT TO THE WEB PICKS UP 1 ADDITIONAL ROW OF FASTENERS ON EACH SIDE OF WEB CUT LINES. ALL REPAIR STRAPS AND WEB SECTIONS WERE ALODINED AND PRIMED WITH A MINIMUM OF 2 COATS OF BMS1020 AND INSTALLED WET WITH BMS526.

Part: CONNECTOR — DIRTY (SLIDE)

SFO - MAINTENANCE ENTRY SQUIB NR 1 RIGHT OVERWING ESCAPE WILL NOT TEST. FOUND D1128 CONNECTOR IN NEED OF CLEANING. CLEANED D1128 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 29 ABC INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT ASSEMBLY AT SEAT 29 ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2H CUBICLE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 2H CUBICLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT LENS AT SEAT 29B IS INOPERATIVE. REPLACED SHIP TO CONNECTOR AT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: CONNECTOR — LOOSE (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 30H, INOPERATIVE. TIGHTENED LOOSE CONNECTOR AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IDG — FAILED (RT ENGINE)

FLT 96 - THREE HOURS INTO FLIGHT RIGHT GEN DRIVE LIGHT CAME ON STEADY. DISCONNECTED RIGHT GEN IAW PROCEDURES. PART NIS AT MXP. ENTERED IN MIC SERVICED BOTH IDGS. ADDED 2 PTS ON RIGHT AND 0 FOR THE LEFT IDG. BPCU TEST SHOWN IDG/OIL IN BULB WIRING. REPLACED RIGHT IDG. LEAK AND OPS CHECKED OK. (M)

Part: PIN — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR PIN AT ROW 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GENERATOR — FAILED (RT ENG GEARBOX)

JFK - FLT 24 - EN ROUTE FL330 LIGHT TO MODERATE TURBULENCE, RIGHT ENGINE DRIVEN GENERATOR FAILED. GENERATOR WOULD NOT RESET, FIELD OFF LIGHT ILLUMINATED CHECK STATUS MESSAGES. APU REQUIRED 2 ATTEMPTS TO START. REPLACED PER B767MM RIGHT ENGINE GENERATOR. OPS CHECK LEAK CHECK OK FOR SERVICE. BITE CHECK EB, NO FAULTS NOTED. APU STARTED FIRST ATTEMPTS.(M)

Part: WIRE — SHORTED (SIGN)

BOS - FLT 68 - EN ROUTE MIA-MAD - BURNING ELECTRICAL SMELL OCCURRED IN THE FIRST CLASS CABIN NEAR SEATS 3A AND 3B. DISSIPATED AFTER A FEW MINUTES. AFTER SMELL RETURNED, CREW TURNED OFF UTILITY BUSSES AND RECIRCULATING FAN. DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. REPAIRED WIRE AT FIRST CLASS LAV F2 RETURN TO SEAT SIGN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SOCKET — DEFECTIVE (ROW 11AB)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 11AB INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT SOCKET AT SEAT 11AB. SYSTEM CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FIRE DETECTOR — MALFUNCTIONED (LT ENGINE)

LGW - 50 - LT ENG OH LP 1 STATUS MESSGE ANNUNCIATED ON LOWER EICAS. PERFORMED TROUBLESHOOTING AS PER MM 26-11-00-1 OH LOOP 1 FOUND INOPERATIVE NIL SPARES LGW ITEM DEF PER MEL 26-02B AU 2-364D-A ENT IN MICS PLACARDED RAISED. TROUBLESHOT SYSTEM AND REPLACED FAULTY L ENG OVERHEAD LOOP DETECTOR ASSY PER MM 26-11-02-4 OVERHEAT DET TEST OK ON EICAS. REMOVED PLAC 2-364D-A. CLEARED MIC SHEET. (M)

Part: BOOST PUMP — FAILED (LT AFT WING)

EZE - FLT 998 - DURING CLIMB-OUT, APPROACHING LEVEL OFF AT FL410, LT AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED WITH EICAS MSG. APPROX 30 SECONDS LATER LT FWD FUEL BOOST PUMP LOW PRESS LIGHT ILLUMINATED WITH EICAS MSG L FUEL SYS PRESS. OPENED FUEL CROSSFEED VALVE. LEFT FWD AND AFT FUEL BOOST PUMP LOW PRESS LIGHTS EXTINGUISHED AFTER ABOUT 1 MIN FUEL X-FEED VALVE LEFT IN OPEN POSITION. REMOVED FUEL FROM TANKS. OPENED ACCESS PANELS AND INSPECTED FUEL TANK LINES FOR OBSTRUCTIONS NO DISCREPANCIES. REPLACED LEFT AFT AND FWD FUEL BOOST PUMPS PER MM. REPLACED LEFT AFT AND FWD FUEL BOOST PUMPS PRESSURE SW PER MM. REFILLED TANKS AND CHECKED FOR LEAKS, NO LEAKS DETECTED. (M)

Part: MOUNT — CORRODED (G6 GALLEY)

AFW - GALLEY MOUNT M-M FOUND CORRODED. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR FITTING USING 7075-T6511 EXTRUSION. APPROVED BY ENGINEERING PER MRB 767-1505. (M)

Part: MOUNT — CORRODED (G7 GALLEY)

AFW - GALLEY MOUNT N-N FOUND CORRODED. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR FITTING USING 7075-T6511 EXTRUSION. APPROVED BY ENGINEERING PER MRB 767-1506. (M)

Part: MOUNT — CORRODED (G6 GALLEY)

AFW - GALLEY MOUNT N-N CORRODED. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR FITTING USING 7075-T6511 EXTRUSION AND SHEET ALUMINUM. APPROVED BY ENGINEERING PER MRB 767-1504. (M)

Part: MOUNT — CORRODED (G7 GALLEY)

AFW - G-7 GALLEY MOUNT FOUND CORRODED, GALLEY MOUNT M-M. FABRICATED AND INSTALLED REPAIR FITTING USING 7075-T6 EXTRUSION AND .071 INCH SHEET ALUMINUM AFTER REMOVAL OF ALL CORROSION. ALODINED, PRIMED AND PAINTED. APPROVED BY ENGINEERING PER MRB 767-1503. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, MID-GALLEY RT SIDEWALL EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REPAIRED BROKEN WIRE SPLICE FOR MID-GALLEY RT SIDEWALL EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LT ENGINE)

LHR - FLT 71 - LEFT GEN OFF LIGHT ILLUMINATED IN FLIGHT. LEFT GEN DISCONNECTED IAW PROCEDURE. REMOVED AND REPLACED LEFT IDG PER MM. OPS CHECK AND LEAK CHECK OK. REMOVED PLACARD MEL 24-1, 6337DC-B CLEARED MIC SHEET. (M)

Part: OVEN — NEEDED CLEANING (GALLEY)

MXP - FLT 96 - EN ROUTE ORD-MXP - DURING CRUISE, F/C GALLEY NR 1 OVEN PRODUCED SLIGHT SMOKE WHEN HEATED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED MXP, LANDING WITHOUT INCIDENT. CHECK OF THE OVEN REVEALED HEATING ELEMENT VERY DIRTY. PLACARDED F/C GALLEY NR 1 OVEN INOPERATIVE. SUBEQUENTLY REPLACED F/C GALLEY NR 1 OVEN AT LAX AND REMOVED PLACARD. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE NOTED. (M)

Part: AIR DISTR — ODOR (GALLEY)

GIG - FLT 904 - EN ROUTE CNF/GIG DURING CRUISE, ELECTRICAL ODOR NOTED IN B/C GALLEY. AIRCRAFT PROCEEDED GIG AND LANDED WITHOUT INCIDENT. CHECKED ALL GALLEY ELECTRICAL FUNCTIONS WITH NO DEFECTS NOTED. CHECKED MAIN WHEEL WELL AREAS, CEILING AREA OVER B/C GALLEY AND E/E COMPARTMENT WITH NO DEFECTS FOUND. ACCOMP GROUND ENGINE RUN AND OPERATED PNEUMATIC SYSTEM WITH APU OFF WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE PROBLEM. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEMS OPERATIONAL CHECKED NORMAL AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRAP — CORRODED (FUSELAGE)

AFW - FOUND FAIL/SAFE STRAP CORRODED. AFTER BLENDING FOUND 7 BLENDOUTS BEYOND SRM LIMITS. ALODINED AND REFINISHED DAMAGED AREA. APPROVED BY ENGINEERING PER MRB 767-1221. (M)

Part: CHORD — CORRODED (BS 568-570)

AFW - FORWARD CARGO LOWER DOOR CHORD CORRODED AROUND TWO HOLES ON INBOARD SIDE, FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND REFINISHED BLENDED AREAS. APPROVED BY ENGINEERING PER MRB 767-1222. (M)

Part: WEB — CORRODED (BS 611)

AFW - FOUND SMALL AREA OF CORROSION ON WEB. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED, PRIMED AND BLENDED AREA. APPROVED BY ENGINEERING PER MRB 767-1224. (M)

Part: FRAME — CORRODED (BS 1417)

AFW - FOUND FUSELAGE FRAME WEB IN AFT CARGO CORRODED AROUND NUT PLATE HOLE HAS DAMAGE BEYOND SRM LIMITS. REMOVED CORROSION, ALODINED AND PRIMED DAMAGED AREA. APPROVED BY ENGINEERING PER MRB 767-1225. (M)

Part: FITTING — WORN (RT DOOR FIG)

AFW - FOUND INBOARD SIDE OF RIGHT TRUNNION DOOR FITTING BEYOND SRM LIMITS AFTER BLENDING. ROTOPEENED, ALODINED AND PAINTED WORN AREA. APPROVED BY ENGINNERING PER MRB 767-1220. (M)

Part: STRAP — NOTCHED (BS 1244-1305)

AFW - FOUND AFT CABIN CARGO STRAP NOTCHED IN 3 PLACES. BLENDED CUT NOTCHES. ROTOPEENED, ALODINED AND PRIMED. APPROVED BY ENGINEERING PER MRB 767-1227. (M)

Part: CHORD — CORRODED (BS 127.6)

AFW - FOUND INTERGRANULAR CORROSION AROUND OUTBOARD FASTENER HOLE. FOUND TWO CORROSION AREAS BEYOND SRM LIMITS AFTER BLENDING. COUNTERBORED REAMED AND INSTALLED FREEZE PLUG IN AREA OF INTERGRANULAR CORROSION. ALODINED AND REFINISHED TWO BLENDOUTS. (M)

Part: SKIN — GOUGED (PAX DOOR CUTOUT)

AFW - FOUND TWO GOUGES ON SKIN LAP AFT APPROX 7 INCHES OF L-2 DOOR. FOUND BEYOND SRM LIMITS AFTER BLENDING. EDDY CURRENT CHECKED. NO CRACKS FOUND. COUNTERSINKED AND REPLACED FASTENERS. APPROVED BY ENGINEERING PER MRB 767-1219. (M)

Part: STRAP — CORRODED (FUSELAGE)

AFW - FOUND FORWARD CARGO DOOR FRAME FAIL/SAFE STRAP CORRODED BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREA. APPROVED BY ENGINEERING PER MRB 767-1217. (M)

Part: WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING LEFT SIDE IN FIRST CLASS INOPERATIVE. RECONNECTED WIRES ON EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT FORWARD LEFT FIRST CLASS SEAT INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR FOR FORWARD LEFT FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — NEEDED RESECURE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LEFT AISLE BETWWEN PASSENGER SEAT ROWS 3 THROUGH 8 INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGNECY EXIT LIGHTS BY MID-GALLEY INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGT WIRE AT LEFT SIDE OF MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)