N1610D

Part: FRAME — CRACKED (BS 903.5) · airframe 84,102 hrs · 10,843 cycles

HFEC INSPECTION FOUND 01 EA CRACK AT LH BS903.5 FRAME INNER CHORD AS MARKED AND REPAIRED. (LP 0876277)

Part: FRAME — CRACKED (BS 903) · airframe 84,102 hrs · 10,843 cycles

FUSELAGE AT STA903 LEFT SIDE INNER CHORD LOWER CORNER SUSPECT CRACK AND REPAIRED. (LP0876275)

Part: SHEAR TIE — CORRODED (BS 632) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 -FWD CARGO COMPARTMENT SHEAR TIE FOUND CORROSION AT BS 632 BETWEEN STRINGER S-35R AND S-36R FOUND OUT OF LIMITS AND INSTALLED NEW SHEAR TIE. (LP 0876286)

Part: SKIN — CORRODED (BS 995) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

WING CENTER SECTION UPPER SKIN AT STA955 RBL78 FOUND CORROSION. C/W ERA 573864-14. (LP 0875020)

Part: SEAT TRACK — CORRODED (BS 1428-1439) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT LBL88.5 FROM STA1428 TO STA1439 FOUND CORROSION OUT OF LIMITS AND REPLACED. (LP 0872731)

Part: SEAT TRACK — CORRODED (BS 859-933) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT RBL88.5 FROM STA859 TO STA933 FOUND CORROSION. REPAIRED PATS AND NEW SPLICES INSTALLED. (LP 0868995)

Part: SEAT TRACK — CORRODED (BS 1362-1428) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT LBL88.5 FROM STA1362 TO STA1428 FOUND CORROSION OUT OF LIMITS AND REPAIRED. (LP 0868743)

Part: SEAT TRACK — CORRODED (BS 859-955) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT LBL88.5 FROM STA859 TO STA955 FOUND CORROSION OUT OF LIMITS. REPAIRED PER SRM 53-00-52 AND 51-10-02. (LP 0865235)

Part: SEAT TRACK — CORRODED (BS 1098-1230) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT LBL88.5 FROM STA1098 TO STA1230 FOUND CORROSION FOUND OUT OF LIMITS AND REPAIRED. (LP 0865232)

Part: SEAT TRACK — CORRODED (BS 1098-1197) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT RBL88.5 FROM STA1098 TO STA1197+ 33. FOUND CORROSION. REPARIED PER SRM 53-00-52 AND 51-10-02. (LP 0865240)

Part: SEAT TRACK — CORRODED (BS 1208-1428) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT RBL88.5 FROM STA1208 TO STA1428 FOUND CORROSION OUT OF LIMITS AND REPAIRED. (LP 086537)

Part: SEAT TRACK — CORRODED (BS 1197-1208) · corrosion level 2 · airframe 84,102 hrs · 10,843 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT RBL88.5 FROM STA1197+33 TO STA1208 FOUND CORROSION OUT OF LIMITS AND REPAIRED. (LP 0865243)

Part: WIRE — PULLED (CABIN) · airframe 83,578 hrs · 10,793 cycles

EMERGENCY LIGHTS AT SEAT 22AB ARE INOPERATIVE WIRE PULLED OUT OF SOCKET. MAINTENANCE RETERMINATED WIRE AND SECURED SOCKET.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 82,003 hrs · 10,632 cycles

EMERGENCY LIGHTS AT SEAT 22AB WERE INOPERATIVE. REPLACED THE A BROKEN SIDEWALL ELECTRICAL CONNECTOR. SYSTEM OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,003 hrs · 10,632 cycles

L2 AND R2 EMERGENCY DOOR EXTERIOR LIGHTS WERE INOPERATIVE. THE BATTERY PACK WAS FOUND BAD. REPLACED THE BATTERY PACK, AND REPLACED THE LAMPS . SYSTEM OPS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 81,526 hrs · 10,583 cycles

DURING SERVICE CHECK, EMERGENCY LIGHTS, RIGHT SIDE WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN PIN AND SOCKET. REPAIRED THE WIRE AND REPLACED PIN. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,391 hrs · 10,569 cycles

DURING A SERVICE CHECK, THE EMERGENCY LIGHTS AT SEATS 23 - 23 ABC WERE FOUND INOPERATIVE. REPLACED THE BATTERY POWER SUPPLY UNIT.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 79,255 hrs · 10,364 cycles

EMERGENCY PATH LIGHTS AT SEAT 21AB, 22FG, 33FG INOPERATIVE. SECURED CONNECTORS. SYSTEM OPERATION IS NORMAL.

Part: TEE FITTING — DAMAGED (FAILSAFE) · airframe 76,082 hrs · 9,993 cycles

LEFT FAILSAFE STRAP, FOUND TEE FITTING HAS TWO HOLES DAMAGED. REPLACED THE TEE FITTING.

Part: FAILSAFE — CRACKED · airframe 76,082 hrs · 9,993 cycles

LEFT FAILSAFE STRAP INDICATES A CRACK DURING A HOLE EDDY CURRENT INSPECTION. CRACK INDICATIONS ALSO IN FUSELAGE, SKIN AND STRAP. REPAIRED THE FAILSAFE STRAP IAW EM 5312-01170 SECTION 10A.

Part: FAILSAFE — CRACKED · airframe 76,082 hrs · 9,993 cycles

DURING OPEN HOLE HFEC INSPECTION OF THE FAIL-SAFE STRAP, FOUND CRACK INDICATIONS IN ALL THREE HOLES. INDICATIONS ARE IN ALL THREE LAYERS OF THE FITTING, SKIN AND STRAP. REPAIRED IAW ERA 556293-14.

Part: FAILSAFE — CRACKED · airframe 76,082 hrs · 9,993 cycles

DURING OPEN HOLE INSPECTION OF THE FAIL-SAFE STRAP, FOUND CRACK INDICATIONS IN ALL THREE HOLES. INDICATIONS ARE IN ALL LAYERS OF FITTING, SKIN AND STRAP.

Part: FAILSAFE — CRACKED · airframe 76,082 hrs · 9,993 cycles

RIGHT FAILSAFE STRAP INDICATES A CRACK, FOUND DURING OPEN HOLE EDDY CURRENT INSPECTION, REPAIRED THE FAILSAFE STRAP IAW EM 5312-01170 SECTION 10B.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 68,979 hrs · 9,116 cycles

OVERHEAD PANEL EMERGENCY LIGHTS WIRE IS LOOSE. MAINTENACE RESECURED WIRE. SYS OPERATION IS NORMAL.

Part: SKIN — MECHANIC ERROR (LT WING) · airframe 67,378 hrs · 8,928 cycles

TOOLING DAMAGE LT WING STR 9.5L AT RIB 32 AFT .2500" HOLE, ERA 386382-14AD, REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,585 hrs · 7,914 cycles

EMERGENCY LIGHT ROW 19A/B INOPERATIVE. HAVE 6 VOLTS TO CEILING PANEL PLUG. ONLY 3 VOLTS AT LIGHT ASSY.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 57,557 hrs · 7,801 cycles

RT WING INBD MAIN FLAP L/E OTBD FAIRING IS DELAMINATED. REPAIRED IAW SRM 57-53-01, FIG 201 AND SRM 51-70-07, PAR 5A.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 57,557 hrs · 7,801 cycles

RT WING OTBD FLAP LWR SURFACE T/E INBD AREA IS DENTED. REPAIRED IAW SRM 57-53-01, FIG 201 AND SRM 51-70-07, PAR 5A.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 57,557 hrs · 7,801 cycles

LT WING INBD MAIN FLAP IS DELAMINATED AND REPAIRED IAW SRM 57-53-01, FIG 201 AND SRM 51-70-05, PAR 5A.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 57,108 hrs · 7,756 cycles

FOUND ONE EMERGENCY LIGHT ON CEILING ABOVE SEAT 19B INOPERATIVE. REPAIRED THE TERMINAL OF LIGHT ASSY IAW SWPM AND REINSTALLED THE LIGHT ASSY IAW AMM 33-51. OPS CHECKED OK.

Part: OVEN — ODOR (FWD GALLEY) · airframe 54,611 hrs · 7,441 cycles

AFTER TAKEOFF, BURNING ODOR VICINITY FWD OVENS, NR 2 OVEN FAULT LIGHT ILLUMINATED OVEN STOPPED WORKING ODOR DIMINISHED PULLED NR 2 OVEN CIRCUIT BREAKER AND CONTINUED FLIGHT. OPEN

Part: SKIN — BULGED (LE SLAT) · airframe 52,758 hrs · 7,203 cycles

LEFT WING NR 1 SLAT EXTERIOR SKIN FOUND BULGE ADJACENT TO O/B AUX TRACK AND THE SUBJECT DEFECTIVE SKIN AREA. REPAIRED PER ERA 497662-14 REV ORIG.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 52,758 hrs · 7,203 cycles

LEFT WING I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-03 PAR. 5A FIG 5.

Part: WEDGE — CHAFED (LE SLAT) · airframe 52,758 hrs · 7,203 cycles

NR 12 SLAT T/E WEDGE LWR SURFACE IS CHAFED NEAR I/B AUX TRACK AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202 SHT 8.

Part: SKIN — LOOSE (LE SLAT) · airframe 52,758 hrs · 7,203 cycles

NR 4 SLAT T/E WEDGE CORNER SKIN IS LOOSE AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202 SHT 1.

Part: LIGHT — NOT SEATED (CABIN) · airframe 52,357 hrs · 7,157 cycles

EMERGENCY AISLE CEILING LIGHTS AT SEAT 37FG ARE INOPERATIVE. MAINTENANCE RESEATED BULB AND INSPECTED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 47,982 hrs · 6,635 cycles

PILOT RECEIVED AN EICAS WARNING THAT THE LEFT FORWARD WINDSHIELD HEAT WAS INOPERATIVE. CAPTAIN THEN NOTICED THAT THE WINDOW WAS CRACKED BUT NO SIGN OF LEAKAGE WAS IDENTIFIED. THE FLIGHT LANDED WITHOUT INCIDENT AND MAINTENANCE REPLACED THE NR 1 WINDSHIELD PER MM 56-11-01 AND REPLACED THE WINDOW HEAT CONTROLLER. (DL76G102877)

Part: UNKNOWN — ODOR (CABIN) · airframe 39,648 hrs · 5,736 cycles

INTERMITTENT BURNING RUBBER/PLASTIC ODOR IN MID CABIN DURING CRUISE. ODOR CENTERED AT ROW 17 CAME FROM AIR VENTS. STRONGER ON LEFT SIDE OF CABIN BARELY NOTICEABLE ON RIGHT SIDE. TURNED GASPER FAN OFF ODOR DISSIPATED. NOTIFIED ATL MTC ACARS 1825Z. RAN RECIRC FANS AND GASPER CANNOT DUPLICATE ODOR. NO ODOR NOTICED.

Part: BRAKE ASSY — DAMAGED (MLG) · airframe 32,876 hrs · 4,941 cycles

OUTSIDE REAR LT BRAKE TEMP EXTREMELY HOT REACHING 9 MLG TIRE 5 FOUND DEFLATED UPON ARRIVAL. AFTER TIRE REMOVAL FOUND BRAKE ASSY DAMAGED BRAKE PAD FALLING APART ACP CONDITIONAL INSPECTION AS PER AMM 05-51-14-212-094. NOTHING ABNORMAL FOUND. REPLACED BRAKE ASSEMBLY AS PER AMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,166 hrs · 4,722 cycles

THE FUSELAGE SKIN WAS GOUGED AND DENTED BETWEEN STA 325 AND 347, S-34L-35L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: DISPLAY — FAILED (COCKPIT) · airframe 29,967 hrs · 4,584 cycles

RIGHT FMC INOP ON TAXI OUT. REMOVED AND REPLACED RIGHT MCDU PER AMM, OPS CHECK NORMAL

Part: WINDOW — FAILED (COCKPIT) · airframe 26,688 hrs · 4,182 cycles

APPROX 1 HOUR NORTH OF JFK CREW REPORTED RT FWD WINDSHIELD HEAT INOP FOLLOWED BY OUTER PANE SHATTERED. NO AIR LEAKS, JUST OUTER PANE BROKEN. REPLACED WINDSHIELD AND HEAT CONTROLLER.

Part: BLADES — TORN (NR 1 ENGINE) · airframe 25,199 hrs · 3,983 cycles

DURING TAXI AND NR 1 ENGINE START EGT WENT TO 849 ANALOG A/C ADVISED TO RTB. DURING T/S, N2 WENT TO ONLY 42.9 PERCENT AND EGT WAS ABOVE 750 FOR 2.5 MIN DAMAGE FOUND TO 1ST AND 3RD HPC. REPLACED ENGINE.

Part: BOTTLE — DISCHARGED (OXYGEN SYSTEM) · airframe 22,906 hrs · 3,657 cycles

CREW OXYGEN PRESS INDICATED ZERO ON EICAS EN ROUTE TO ATL. DIVERTED TO SJU. REMOVED AND REPLACED CREW O2 BOTTLE. LEAK CHECK GOOD. MAINTAINED PRESSURE. OKAY FOR SERVICE. INSPECTED MASKS AT ALL 4 STATIONS, CHECKS OK.

Part: COMPUTER — INOPERATIVE (FLT DIRECTOR) · airframe 22,753 hrs · 3,634 cycles

DURING DIVERSION FOR WEATHER INTO SKG, CAPT PITOT MSG ILLUMINATED ON FINAL. AFTER GO AROUND - AILERON LOCKOUT MSG RUDDER RATIO MSG LT AND RT EEC MSG ILLUM. F/O FLT DIR STOPPED WORKING. DISCOVERED C/B K-15 ON P6-3 PANEL POPPED. RESET, ALL RETURNED TO NORMAL. RUDDER RATIO LIGHT FIM PROCEDURE 27-21-00 PG 107 AND 27-09-00 PG 107 CHECK OUT OF SYS OK. AIL LOCKOUT FIM 27-11-00 CHECK OUT OK. PIMU LT AND RT BITE OK. REMAIN GROUND RUN UP FOR SYS VERIFICATION GOOD.

Part: SWITCH — OUT OF RIG (NR 3 SLAT) · airframe 19,427 hrs · 3,155 cycles

L/E ASSYM ON T/O AT 1000 AGL RETURNING TO LGW. FOUND SLAT ASSYM SWITCH 284 OUT OF ADJUSTMENT. RESHIMMED PROX SWITCH 284 ON NR 3 SLAT.

Part: SENSOR — UNSERVICEABLE (SLAT) · airframe 13,954 hrs · 2,310 cycles

DURING CLIMBOUT, CLEAN CONFIGURATION, LE SLAT ASYM EICAS MSGACOMPLISHED QRH PROCEDURE. AIRCRAFT LANDED WITH ZERO SLATS AND 20 DEG FLAPS. 173 KT LANDING SPEED. REPLACED S279 PROX SENSOR. CHECKS OK. PERFORMED HIGH ENERGY STOP INSPECTION NO DEFECTS.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 13,622 hrs · 2,245 cycles

SEAT ROWS 1-7 LT SIDE EMERGENCY LIGHTS HAVE SEVERAL LIGHTS INOP. FWD TO MCO AND PLACARD PER MEL 33-51-03, CONNECTORS DISCONNECTED AT 6AB, 1AB, 2AB.

Part: FSEU — FAILED (E/E BAY) · airframe 11,462 hrs · 1,868 cycles

AFTER T/O LEADING EDGE SLAT ASSYM LIGHT ON. FLAP GAUGE WOULD NOT COME FULL UP. INDICATOR STUCK BETWEEN 1 AND UP. PERFORMED BITE TEST OF FLAP/SLAT ELEC UNIT. REPLACED FSEU.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 5,451 hrs · 888 cycles

CAPTS WINDSHIELD OUTER LAYER SHATTERED. REPLACED LT FWD WINDSHIELD AND WINDOW HEAT CONTROLLER PER M/M TORQUED PER ERA 388709-14. ALL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 4,278 hrs · 716 cycles

LT EXTERIOR AFT OVER WING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. LIGHT OPS NML

Part: UNKNOWN — ODOR (AFT GALLEY) · airframe 3,499 hrs · 591 cycles

CREW REPORTED ELEC ODOR IN AFT CABIN AROUND SEAT ROW 37. CHECKED CABIN AREA, FWD AND AFT CARGO BAYS APU BATTERY AREA AND WATER COMPRESSOR AND SURROUNDING AREA. ALSO CHECKED E & E BAY AND COMPONENTS. ALL CHECKS WERE OK, NO UNUSUAL ODORS WERE NOTED. PERFORMED POWER RUN-UP AND RAN PACKS, NOTHING FOUND. A/C PUT BACK IN SERVICE.

Part: ENGINE — SEIZED (NR 2) · airframe 2,693 hrs · 458 cycles

ON TAXI OUT NR 2 ENGINE N2 SPUN DOWN WHILE OIL PRESSURE DROPPED TO 10 PSI. EGT WENT ABOVE 900 DEGREES. THE ENGINE WAS THEN SHUT DOWN. MTC FOUND METAL AND NON METAL MATERIAL IN THE TAIL PIPE. REMOVED AND REPLACED ENGINE

Part: UNKNOWN — FUMES (CABIN) · airframe 2,229 hrs · 384 cycles

AT GATE WITH APU AND PACKS ON, A SLIGHT HAZE AND SMOKE ODOR IN CABIN. FOUND UTILITIES BUSS IN OFF POSITION AND RECIRC FANS OFF. RESET SYSTEM AND TURNED PACKS ON, NO SMELL OR HAZE.

Part: OVEN — ODOR (GALLEY) · airframe 1,188 hrs · 204 cycles

FLIGHT ATTENDANTS NOTICED ELECTRICAL SMELL COMING FROM ABOVE AFT GALLEY OVEN NR 2. SMELL WENT AWAY WITH POWER REMOVED. FOUND MELTED PLASTIC BAG MATERIAL INSIDE OF OVEN NR 2. REMOVED AND CLEANED SAME. OPERATED OVENS, NO SMELL NOTED.