N173DZ

Part: PITOT HEAD — DAMAGED (ZONE 100) · airframe 103,939 hrs · 22,137 cycles

IAS AND ALT DISAGREE WITH F/O AIR DATA INCORRECT. REPLACED RIGHT LOWER PITOT PROBE.(7676858)

Part: SKIN — CRACKED (ZONE 200) · airframe 103,606 hrs · 22,072 cycles

FWD PAX DOOR CUTOUT AFTER LOWER CORNER HOLE NO. 4 IS CRACKED. REPAIRED FWD PAX DOOR CUTOUT AFTER LOWER CORNER IAW B767 SRM 53- 10-01-2R REPAIR 1. (1219987)

Part: SKIN — CRACKED (ZONE 200) · airframe 103,606 hrs · 22,072 cycles

SHIP 1703 FWD SERVICE DOOR CUTOUT AFT LOWER CORNER HOLE NO. 4 IS CRACKED. CRACK WAS FOUND DURING NDI INSPECTION. REPAIR IS REQUIRED PRIOR TO FURTHER FLIGHT. AMOC TO AD 24-05-03 MAY BE REQUIRED. REFER TO AA 5331-01288. CORRECTIVE ACTION: REPAIRED FWD SERVICE DOOR CUTOUT AFT LOWER CORNER HOLE NO 4 IAW B767-300 SRM 53-10-01-2R-1 (1219980)

Part: SKIN — DENTED (ZONE 100) · airframe 103,599 hrs · 22,070 cycles

WHILE PERFORMING DENT DOT MONITOR INSPECTION FOR LOG PAGE 6784736, FOUND ADDITIONAL DAMAGE AT DENT LOCATION 13" AFT OF STA 1197+66 AND 3" BELOW STR 35L. REPAIRED PER B767 SRM 53-00-01-2R-12 DETAIL I. REPAIR IS CAT B. (1205512)

Part: LENS — BROKEN (ZONE 200) · airframe 103,319 hrs · 22,026 cycles

EMERGENCY SLIDE LIGHT BEHIND LEFT WING APPEARS TO HAVE A BROKEN/ MISSING LENS. R/R THE LEFT EMERGENCY LIGHT LENS PER B767-300 AMM 33-51. OPS CHECK GOOD. OK FOR SERVICE (7865963)

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 102,836 hrs · 21,958 cycles

SHIP 1703 L1 DOOR SLIDE ARM LIGHT NOT ILLUMINATED. CORRECTIVE ACTION: REMOVED AND REPLACED PROX BOX PER B767 AMM 32-0. (7315544).

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 101,530 hrs · 21,729 cycles

THE RIGHT LOWER EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED ALL FOUR FUSES WITHIN THE M733 POWER SUPPLY PER B767-300 WDM 33-51-21. OPERATIOANL CHECK WAS NORMAL. AIRCRAFT IS OK FOR SERVICE. (LP #7114623)

Part: MODULE — INOPERATIVE (ZONE 800) · airframe 100,785 hrs · 21,585 cycles

SHIP 1703 L1 DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE MODULE ASSY PER B767-300 AMM 52-73. SLIDE LIGHT OPERATES NORMAL. A/C OK FOR SERVICE. (6630538)

Part: INDICATOR — DAMAGED (ZONE 800) · airframe 100,074 hrs · 21,460 cycles

SHIP 1703 SLIDE INDICATOR LIGHT INOP OR DAMAGED. CORRECTIVE ACTION: R/R DOOR 1R SLIDE LIGHT INDICATOR ASSY. CHECKS OK PER B767-300ER AMM 52-73. (0640032)

Part: LAVATORY — UNDERSERVICED (ALL) · airframe 99,714 hrs · 21,400 cycles

SHIP 1703 -DIV- FLT DIV TO CDG DUE TO MULTIPLE LAVATORIES INOPERATIVE. CORRECTIVE ACTION: CDG MTC SERVICED LAVS. ALL WERE FUNCTIONAL. PHYSICAL CHECK OF POINT LEVEL SENSORS REVEALED UPPER PORTION OF TANK HEAVILY COVERED WITH DEBRIS. RINSE NOZZLE ROTATING HEAD MISSING. RPLCD SENSOR, LOGIC MODULE AND RINSE NOZZLE. (9994162)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 97,411 hrs · 21,076 cycles

SHIP 1703 - PRES- CABIN ALTITUDE WARNING WHILE AIRCRAFT HOLDING NEAR BOG. PERFORMED EMERGENCY DESCENT. NO PASSENGER OXYGEN MASKS DEPLOYED. CORRECTIVE ACTION: NO FAULTS ON CABIN PRESSURE CONTROLLERS. INSPECTED FUSELAGE, DOOR SEALS, PRESSURE RELIEF VALVES NO FAULT FOUND. PERFORMED OPS CHECK OF OUTFLOW VALVE. (5339544)

Part: LIGHT — UNKNOWN (L1 DOOR SLIDE) · airframe 96,790 hrs · 20,975 cycles

SHIP 1703 1L SLIDE LIGHT INOP. CORRECTIVE ACTION: LIGHT OPS NORMAL REF. B767-300 AMM 52-71-00 (5729278)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,939 hrs · 20,818 cycles

SHIP 1703 L FWD EMER DOOR EICAS MSG AFTER T/O. RAN QRH AND PRESSURE WAS NORMAL. CORRECTIVE ACTION: FWD LH FWD EMERG DOOR INDICATION TO MEL 51-71-01. C/W "M" PROC. (4613094)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,873 hrs · 20,807 cycles

SHIP 1703 L FWD EMER DOOR EICAS MESSAGE ON GROUND AFTER START. CORRECTIVE ACTION: R/R PSEU PER B767-300 AMM 32-09, OK FOR SERVICE. MEL PLACARD REMOVED NO " M" PROCEDURES TO REVERSE. (4613088)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,873 hrs · 20,807 cycles

SHIP 1703 L EMER DOOR EICAS MESSAGE INTERMITTENT AND AFTER TAKEOFF. QRH ACCOMPLISHED. MCC NOTIFIED. CORRECTIVE ACTION: ON ARRIVAL, NO L EMER DOOR EICAS MSG. CONFIRMED FIM B767 52-71- 00-990-812. BITE TEST OF PSEU & TEST OK. NO FAULT NOTED. A/C OK FOR SVC. (4613080)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,821 hrs · 20,798 cycles

SHIP 1703 FOUND BY MTC - 1L DOOR ARMED INDICATOR ON FAP INOP/ SWITCH STUCK. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR ARMED INDICATOR PER B767-300 WDM 52 -73-11. OPS NML. MEL AND PLAC RMVD. M PROCEDURES C/W. (4613058)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 CHECK FOUND MULTIPLE NICKS OF R HORI-STAB L/E PNL 342CR SURFACE. CORRECTIVE ACTION: THE NICKS REPAIRED OF R HORI-STAB L/E PNL 342CR SURFACE AS PER PRI 612883-14.REV.0. (0041360)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 CHECK FOUND MULTIPLE NICKS OF R HORI-STAB L/E PNL 342BR SURFACE. CORRECTIVE ACTION: COMPARE AND COMPLIANCE WITH THE ER/A 612883-14 REV. (0041350)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 LHW NO.1 ACTUATORCRANK INRUT SHAFT SUPPORT ROLLER BEARING FOUND CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED LHW NO.1 ACTUATOR CRANK ARM O/B SUPPORT RIB BEARING, AS PER B767-300 AMM:27-51-21 (0040012)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 FOUND WORN ON FUSELAGE EXTERIOR SKIN AT 321BR AREA. CORRECTIVE ACTION: THE CHAFING BLENT OUT REPAIR AS PER PRI:612806-14 REV. O COMPARED AND COMPLIED WITH ER/A:612806 (0036771)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 AGING AIRCRAFT INSPECTION ITEM- CHAFING MARKS ON PREVIOUS REPAIR , KEEL BEAM CENTER WEB, STATION 992, WATER LINE 150.REFERENCE ERA 555767-14 REV A. CORRECTIVE ACTION: THE DAMAGE TRIPLER AND DOUBLER REMOVED AND REPLACED AS PER ER/A 555767-14 REV.A AND B767-300 SRM 51-40-02 (0036751)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 FOUND CORROSION ON THE GAPAREAR BETWEEN THE LH SIDE WING CENTER SECTION REAR SPAR WEB AND SIDE FRAME BULKHEAD FITTING. CORRECTIVE ACTION: THE LH SIDE FRAME FITTING AND REAR SPAR WEB CORROSION BLENT OUT REPAIR AS PER PRI 612413-14 REV. (0033643)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 ERA 612806-14 ISSUED FOR REPAIR TO FUSELAGE SKIN AT STA 1582-162 9, S2R. DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED NO LATER THAN 3749 9 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 00-612806 (0032798)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 CABIN LH FRAME END FITTING CRACK AT FUEL TANK UPPER SURFACE AT 927. CORRECTIVE ACTION: PERFROMED REPAIR PER B767-300 SRM 51-40-02. (0030775)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 FOUND THE CABIN SEAT TRACK CRACK WHEN INSTALLING SEATS AT STA 1131,RBL11. CORRECTIVE ACTION: THE CABIN SEAT TRACK CUT AT STA 1143 RBL 11 AND REPAIRED AS PER B767-300 SRM53-00-52 (0030785)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 ER/A 612413-14, DURING H-CHK AT STAG, CORROSION WAS FOUND COMMON TO THE WING REAR SPAR WEB AND LH PICKLE FORK. CORRECTIVE ACTION: PERFROMED REPAIR PER ER/A 612413-14. (0031643)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 BULK CARGO SHEAR TIE FOUND CRACK AT STA 1562 BETWEEN S39L AND S39R. CORRECTIVE ACTION: PERFROMED REPAIR PER B767-300 SRM51-40 (0030801)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 CABIN RH FRAME END FITTING CRACK AT FUEL TANK UPPER SURFACE AT 852. CORRECTIVE ACTION: PERFROMED REPAIR PER B767-300 SRM51-40 (0030809)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 BULK CARGO LOWER CHORD FOUND CORROSION AT STA1564 BETWEEN S39L AND S39R. CORRECTIVE ACTION: PERFROMED REPAIR PER B767-300 SRM51-40 (0030739)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 RHW NO.7 SPOILER LOWER SURFACE PUNCTURED. CORRECTIVE ACTION: RHW NO.7 SPOILER LOWER SURFACE REPAIRED AS PER B767-300 SRM 57- 70-01-2R-1&SRM 51-70-04. (0030311)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 FOUND L/H WING #6 SLAT INTERNAL SURFACE ONE GOUGE FROM O/B EDGE 22.5 INCH AND UPPER EDGE 6 INCH. CORRECTIVE ACTION: L/H WING #6 SLAT INTERNAL SURFACE REPAIRED FROM O/B EDGE 22.5 INCH AND UPPER EDGE 6 INCH AS PER B767-300 SRM 57-43 (0030318)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 NO.2 PYLON I/B ACCESS DOOR 442AL CUTOUT UPPER EDGE CRACK. CORRECTIVE ACTION: THE CRACK SKIN AT NO.2 PYLON I/B ACCESS HOLE 442AL AFT UPPER EDGE REMOVED AND APPLY DOUBLER REPAIR WITH MATERIAL:15-5PH-0.090 " AS PER PRI 612706-14 REV 0. (0026135)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540 BETWEEN S38L-S37L. CORRECTIVE ACTION: PERFROMED REPAIR PER PERFROMED REPAIR PER B767-300 SRM51-40 (0024337)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540 BETWEEN S38R-S37R, CORRECTIVE ACTION: PERFROMED REPAIR PER B767-300 SRM51-40 (0024542)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540 BETWEEN S39L-39R, CORRECTIVE ACTION: PERFROMED REPAIR PER B767-300 SRM51-40 (0024534)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 SEAT TRACK-CABIN SEAT TRACK FOUND CRACK AT LBL 11,STA1109. CORRECTIVE ACTION: CUTTED AND REMOVED THE DAMAGE SECTION OF SEAT TRACK BETWEEN STA1065-STA1142 LBL11 AND REPAIRED AS PER B767-300 SRM 53-00-52 (0013375)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

AORCRAFT 1703, AD/EM-EO TASK-HFEC INSPECTION OF THE LH BS883.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS FOUND 01EA CRACK LENGTH APPROXIMATELY 2MM. CORRECTIVE ACTION: THE LH BS883.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS CRACK (01EA) TRIMMED AND REPAIRED REFER TO A.A WORKCARD 5311-01195-09C FOR WORK DETAILS. (LP 0008490)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,582 hrs · 20,763 cycles

SHIP 1703 -MISC/DE- DUE TO LT HYD QTY DECREASE DURING FLIGHT. C/W QRH AND LANDED AND TAXIED IN NORMALLY. CORRECTIVE ACTION: LOCATED LEAK IN LT PYLON. REPLACED PACKING AND DPI OF THE LT EDP FILTER MODULE. CHECKED AND REPLACED FILTERS. FLUSHED AND SERVICED HYD SYS. (4599932)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,642 hrs · 20,626 cycles

SHIP 1703 1L ENTRY DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: 1L SLIDE LIGHT OPS GOOD AT THIS TIME. REF B767 AMM 52-73 OK FOR SVC. (4195306)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,818 hrs · 20,511 cycles

MAIN ENTRY/SERVICE DOOR ARMED INDICATORS 2L DOOR. CORRECTIVE ACTION: FOUND LT ASSEMBLY INTERMITTENT. R/R SLIDE ARMED LT ASSY PER B767 WDM 52-73. ALL OPS CHKS GOOD PER B767 AMM 52-73.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,589 hrs · 20,480 cycles

SHIP 1703 -RVSM- FIRST OFFICERS ALTIMETER FLUCUATED +/- 250 FEET DURING CRUISE AT FL380. CORRECTIVE ACTION: R/R F/O'S ALTIMETER PER. B763 AMM 34-12. CKS GOOD. OK FOR SVC. (9447444)

Part: UNKNOWN — UNKNOWN · airframe 93,246 hrs · 20,425 cycles

SHIP 1703 JS 01 DOOR 1R ARMED LIGHT INOP ON F/A PANEL. CORRECTIVE ACTION: OOR 1R CLOSED AND ARMED IAW AMM TASK 52-11-00-862-004 AND ARMED LIGHT ILLUMINATES ON F/A PANEL AND 'ARMED' ILLUMINATES NEXT D1R HANDLE. (4195814)

Part: UNKNOWN — UNKNOWN · airframe 93,190 hrs · 20,417 cycles

SHIP 1703 LH FWD OFF WING SLIDE OPEN ACTUATOR FOUND BAD DURING SLIDE LATCH INSP. CORRECTIVE ACTION: REPLACED LH FWD OFF WING SLIDE ACTUATOR REF AMDS 2560-4232 (9914254)

Part: NONE — NONE · airframe 93,143 hrs · 20,411 cycles

SHIP 1703 RH AFT OFF WING SLIDE OPEN ACTUATOR FOUND BAD DURING SLIDE LATCH INSP. CORRECTIVE ACTION: REPLACED RH AFT OFF WING SLIDE OPEN ACTUATOR REF AMDS 2560-4232 (9914255)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 92,807 hrs · 20,357 cycles

SHIP 1703 ELECTRICAL BURNING SMELL MID AIRCRAFT AND GETS STRONGER IN THE AFT GALLEY. CORRECTIVE ACTION: FOUND SOURCE OF ODOR FROM BULK CARGO VENT FAN. DEFFERED PER MEL 21-40-01C (4136714)

Part: A/C PACK — INOPERATIVE (RIGHT) · airframe 92,524 hrs · 20,306 cycles

ATO DUE TO RIGHT PACK TEMP MESSAGE. A/C RETURNED TO THE GATE. MEL APPLIED FOR RIGHT PACK INOP. 01/04 ATL. REPLACED RIGHT PACK OVERHEAT SWITCH. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,147 hrs · 20,244 cycles

SHIP 1703 LOWER LOB CRUISE REST GREEN CORNER EMERGENCY RUN LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED LOWER LOB CRUSE REST GREEN CORNER EMERGENCY RUN LIGHT PER B767-300 AMM 33-51-01. CKS GOOD. (9712941)

Part: NONE — NONE · airframe 91,848 hrs · 20,197 cycles

SHIP 1703 FLIGHT ATTENDANTS REPORTED A DIRTY SOCK SMELL OCCURED RIGHT AFTER TAKEOFF. DISSIPATED WITHIN 5 MINUTESCORRECTIVE ACTION: WITH R ENG RUNNING R PACK OPS NORMAL WITH NO ORDORS PRESENT IN CABIN. REF B767-300 AMM 21-51. ALSO PERFORMED R ENG OIL LEAK GVI PER B767-300 AMM 79-00 NO LEAKS NOTED. INLET/EXHAUST AND COWLS CLEAN. OK FOR SERVICE. (9438196)

Part: NONE — NONE · airframe 91,357 hrs · 20,118 cycles

SHIP 1703 DOOR 2R SLIDE ARM LIGHT INOP, CORRECTIVE ACTION: 2R DOOR HAS NO ISSUE 1R DOOR SLIDE LIGHT IS THE ISSUE RELAMPED 1R DOOR SLIDE LIGHT AS PER B767-300 AMM 52-73 VERIFIED SLIDE ARMS AND DISARMS PER SAME AMM MEL + PLACARD RMVD (9619045)

Part: NONE — NONE · airframe 91,277 hrs · 20,108 cycles

' SUPPLEMENTAL INFOMATION' SHIP 1703 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601, CORRECTIVE ACTION: FOUND SLIDE LIGHT INOP AT THE FA PANEL, REPLACED BULB, OPS CHECKS GOOD (2407894)

Part: NONE — NONE · airframe 91,103 hrs · 20,076 cycles

SHIP 1703 -ATB/IFSD- 30 MINUTES AFTER TAKE OFF OUT OF ATL FLIGHT CREW OBSERVED LEFT ENGINE HIGH OIL TEMP MESSAGE WITH ASSOCIATED OIL QUANTITY ZERO. ENGINE SHUT DOWN PER QRH, TURNED BACK TO ATL. OIL TANK FOUND TO BE EMPTY ANDNO VISUAL EXTERNAL OIL LEAKS FOUND. DFDR SHOWS OIL TEMP REACHED 192 DEGREES, QUANTITY INDICATED ZERO AND POSSIBLE N2 ROTOR SEIZED. ENGINE REPLACED. (9069210)

Part: SIGN — INOPERATIVE · airframe 90,415 hrs · 19,966 cycles

SHIP 1703 CREW REST COMMON AREA EMERGENCY EXIT SIGN/ RUNNING MAN INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSY PER B767 MM 33-51. OPS NML. (8686497)

Part: NONE — NONE · airframe 90,407 hrs · 19,963 cycles

SHIP 1703 COCKPIT EMERGENCY EXIT SIGN GOES OFF IN SEVERAL SECONDS. CORRECTIVE ACTION: REPLACED BATTERIES IN SIGN ASSY PER B767 MM 33-51 OPS NORMAL (8686496)

Part: NONE — NONE · airframe 89,858 hrs · 19,872 cycles

SHIP 1703 DURING SVC FOUND 2 EA CREW REST EMERGENCY EXIT SIGNS INOP. CORRECTIVE ACTION: OK TO DEFER AND PLACARD IAW MEL 33-51-01D. "M" PROC CW. (8868448)

Part: MANIFOLD — LEAKING · airframe 89,685 hrs · 19,847 cycles

A/C 1703 **SMOKE SMELL EVENT** CABIN CREW ADVISES OF A CHEMICAL SMELL IN THE CABIN. FLIGHT IS CONTINUED TO JFK. CREW DONNED OXYGEN NO EMERGENCY DECLARED. FUMES DISSIPATED IN CRUISE, FLIGHT ATTENDANT COMPLAINED ABOUT HEADACHES. FLIGHT ATTENDANT WAS GIVEN OXYGEN IN COCKPIT / CORRECTIVE ACTION: MTC FOUND #1 OIL MANIFOLD SEAL LEAKING. REPLACED SEAL. (8870054)

Part: NONE — NONE · airframe 89,275 hrs · 19,765 cycles

SHIP 1703 2L CONTROL PANEL SLIDE LIGHT INOP, CORRECTIVE ACTION: C/W OPS CK OF THE 2L DOOR SLIDE LIGHT AS PER B767-300 AMM 52-11. OPS CK GOOD. (8755771)

Part: LIGHT — NOT SEATED (R1 DOOR) · airframe 89,251 hrs · 19,760 cycles

SHIP 1703 1R ARMED LIGHT WONT STAY ON. CORRECTIVE ACTION: RE-SEATED ARMED LIGHT ON 1R DOOR. OPS OK. OK FOR SERVICE. (8755754)

Part: NONE — NONE · airframe 89,141 hrs · 19,736 cycles

SHIP 1703 2L DOOR SLIDE ARMED LIGHT AT DOOR AFTER ARMING. CORRECTIVE ACTION: REPLACED LIGHT ASSY PER B767-300 AMM 52-73. CHKS GOOD MEL/PLAC RMVD (2157075)

Part: NONE — NONE · airframe 88,746 hrs · 19,659 cycles

SHIP 1703 -ATB/IFSD- DUE TO RIGHT ENGINE FAILURE AND UN-COMMANDED SHUTDOWN. FOUND EXTENSIVE TURBINE DAMAGE AND METAL IN THE TAILPIPE. DAMAGE TO RIGHT INBOARD AILERON AND LEADING EDGE OF HORIZONTAL STABILIZER. CORRECTIVE ACTION: ENGINE CHANGED. (8918566)

Part: NONE — NONE · airframe 88,724 hrs · 19,656 cycles

SHIP 1703 RT HORIZONTAL STAB LOWER SKIN 3 DENTS ON BOTTOM MID BETWEEN AUX AND FRONT SPAR. CORRECTIVE ACTION: BLENDED DENTS. INSPECTION C/W PER B767-300 SRM 55-10-01-1A-1 TABLE 101. WITHIN LIMITS. TREATED. FWD TO PNT. (8918575)

Part: NONE — NONE · airframe 88,724 hrs · 19,656 cycles

SHIP 1703 RT HORIZONTAL STAB HAS ONE DENT ON LOWER SKIN MID BETWEEN AFT AND FWD SPAR. CORRECTIVE ACTION: BLENDED DENT. INSPECTION C/W PER B767-300 SRM 55-10-01-1A-1 TABLE 101. WITHIN ALLOWABLE LIMITS. TREATED. FWD TO PAINT. (8918576)

Part: UNKNOWN — ODOR (CABIN) · airframe 88,648 hrs · 19,641 cycles

SHIP 1703 UPON SETTIING THRUST FOR TAKEOFF A STRONG BURNING OIL/ DIRTY SOCK ODOR CAME THROUGH THE PACKS/ AIR ODOR REMAINED THROUGH FL190. CORRECTIVE ACTION: PERFORMED GVI OF BOTH PACK BAYS, #1 AND #2 ENG CORE FOR LEAKS. NO LEAKS NOTED PER B767 AMM 78-31. REFERENCE LOG # 2056396 MD LOG FOR OIL SMELL ODI STEPS COMPLIED WITH. (7988592)

Part: NONE — NONE · airframe 88,573 hrs · 19,625 cycles

SHIP 1703 FOUND THE WEB PUNCHED A HOLE AT STA 1654.5,S35R TO S36R. CORRECTIVE ACTION: CLEAN UP DAMAGE AREA AND DO THE REPAIR AS PER B767-300 SRM 53 -00 (2010670)

Part: NONE — NONE · airframe 88,573 hrs · 19,625 cycles

SHIP 1703 HFEC INSPECTION FOUND 02 EA CRACKS (FWD:0.315" AND AFT0.250") ON THE LH FUSELAGE SKIN BELOW THE NO.8 AND NO.9 STRINGER-ATTACH RIVENTS. CORRECTIVE ACTION: 02 EA CRACKS(FWD: 0.315" AND AFT 0.250") DOUBLER REPAIR AS PER B767-300 SRM 53-80 (2005165)

Part: BULB — DAMAGED (COCKPIT LIGHT) · airframe 88,335 hrs · 19,579 cycles

SHIP 1703 ON DESCENT C 9000' FUMES IN COCKPIT. LASTED ABOUT 1 MINUTE. CALLED CABIN. NOT IN CABIN. NO EICAS MSGS. NO SMOKE IN SIGHT IN COCKPIT. CORRECTIVE ACTION: DURING INSP OF COCKPIT INSTRUMENTS, NOTICED CTR FLOOD LIGHT INOPERATIVE. FOUND BULB IN POOR CONDITION. INSPECTED LIGHT ASSEMBLY TERMINALS & ADJUSTED SAME. INSTALLED NEW BULB. SUSPECT THIS WAS ROOT CAUSE FOR SMELL. OPERATED PACKS FOR SEVERAL HOURS AND NO SMELL PRESENT. SYSTEM OPERATION IS NORMAL. (LP 8034780)

Part: TARGET — OUT OF ADJUST (LT PAX DOOR) · airframe 88,051 hrs · 19,531 cycles

SHIP 1703 FOUND LEFT FWD ENTRY DOOR EICAS MESSAGE AFTER LANDING, SLIDE LIGHT AT ENTRY DOOR WAS FLASHING. CORRECTIVE ACTION: ADJUSTED S194 TARGET. SYSTEM OPERATION IS NORMAL. (LP 8008930)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,794 hrs · 19,482 cycles

SHIP 1703 EMERGENCY LIGHTS AT ROW 13-20 ARE INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTTERY PACK M1209. SYSTEM OPERATION IS NORMAL. (LP 7359485)

Part: WINDSHIELD — CRAZED (COCKPIT) · airframe 85,678 hrs · 18,985 cycles

DIVERTED TO YHZ DUE TO RT WINDSHIELD OUTER PANE CRAZED AND MISSING SECTION WITH INNER PANE SHOWING DEFORMATION. CORRECTIVE ACTION: REPLACED WINDSHIELD AND RT WINDOW HEAT CONTROLLER.

Part: PSEU — MALFUNCTIONED (EMERGENCY EXIT) · airframe 85,546 hrs · 18,952 cycles

RIGHT FORWARD EMERGENCY DOOR EICAS MESSAGE. CORRECTIVE ACTION: REPLACED PSEU MCO/PLAC REMOVED. SYSTEM OPERATION IS NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,792 hrs · 20,791 cycles

SHIP 1703 DURING CCK AND WHILE ACOMCPLISHING EM 5724-01010- 41B A CRACKED FASTENER HOLE WAS FOUND IN THE RHW LOWER SKIN PANE L. A REPAIR WAS ACOCMPLISHED PER SECT I OF ERA 582280-14AD. CORRECTIVE ACTION: PERFORMED RH WING LWR WING SKIN INCLUDE THE REPAIRED LOCATION WITH THE FREEZE PLUG ALONG STRINGER L-6.5 HFEC INSPECTION ,AS PER ERA 582280-14AD (1329684)

Part: LENS — MISSING (CABIN) · airframe 82,370 hrs · 18,392 cycles

FAA INSPECTOR FOUND RED EMERGENCY LIGHT LENS MISSING FROM AISLE EMERGENCY LIGHT FORWARD OF F/L LAV LEFT SIDE FLOOR LEVEL. REPLACED EMERGENCY PROXIMITY LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: FAN — FAILED (E/E COOLING) · airframe 76,889 hrs · 17,653 cycles

DURING DEPARTURE, COCKPIT CREW NOTICED SMOKE ODOR WITH AN ASSOCIATED FWD EQUIP SUPPLY EICAS MESSAGE. REPLACED THE FWD EQUIPMENT COOLING SUPPLY FAN 1. SYSTEM OPS NORMAL.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 76,566 hrs · 17,606 cycles

ON SERVICE CHECK, FOUND THE EMERGENCY LIGHTS WERE INOPERATIVE AT 21AB - 31AB AND 21GF-31GF. BATTERY WAS WEAK AND REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,107 hrs · 17,537 cycles

AISLE EMERGENCY LIGHTS DIDN`T TEST AT ROWS 21-31 ON BOTH SIDES. REPLACED THE BATTERY PACK. SYSTEM OPS NORMAL.

Part: LIGHT — DAMAGED (SEAT 33F) · airframe 74,696 hrs · 17,341 cycles

EMERGENCY SEAT MOUNTED LIGHTS AT 33F ARE DAMAGED. SECURED LOOSE HARDWARE. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 33F) · airframe 74,696 hrs · 17,341 cycles

EMERGENCY SEAT MOUNTED LIGHTING AT 33F ARE INOPERATIVE. FOUND LOOSE HARDWARE AND SECURED.

Part: ANGLE — CRACKED (BS 1480) · airframe 74,172 hrs · 17,266 cycles

BULK CARGO BAY STRUCTURE. INNER ANGLE HAS A CRACK AT BS 1480. BETWEEN STRINGERS 23R AND 24R REPAIRED IAW ERA 562578-14.

Part: FAILSAFE — CRACKED (BS 955) · airframe 74,172 hrs · 17,266 cycles

OPEN HOLE INSPECTION FOUND THE FAILSAFE STRAP WITH ONE HOLE CRACKED AT BS 955 LOWER OF THE THREE FASTENER HOLES. REPAIRED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 74,172 hrs · 17,266 cycles

HFEC SURFACE INSPECTION, FOUND ONE CRACK APPROX 0.100 IN LENGTH ON THE RT BS 955 FAILSAFE STRAP WHICH IS STARTING FROM THE LOWER OF THE THREE FASTENER HOLES ON THE FAILSAFE STRAP. REPAIR CARRIED OUT.

Part: SEAT TRACK — CORRODED (BS 1098-1208) · airframe 74,172 hrs · 17,266 cycles

CORROSION FOUND ON THE SEAT TRACK, RBL 88.5, BETWEEN BS 1098 AND 1208. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 753-1098) · airframe 74,172 hrs · 17,266 cycles

CORROSION FOUND ON THE SEAT TRACK, LBL 88.5, BETWEEN BS 753 AND 1098, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 753-1098) · airframe 74,172 hrs · 17,266 cycles

CORROSION FOUND ON THE SEAT TRACK, RBL 88.5, BETWEEN BS 753 AND 1098, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 1428-1444) · corrosion level 2 · airframe 74,172 hrs · 17,266 cycles

CORROSION FOUND ON THE SEAT TRACK RBL 88.5 BETWEEN BS 1428 AND 1444 AND IS OUT OF LIMITS. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 74,172 hrs · 17,266 cycles

BULK CARGO SHEAR TIE HAS CORROSION AT BS 1540 BETWEEN STRINGERS 39L AND 38L AND FOUND OUT OF LIMITS. THE DAMAGED SHEAR TIE WAS REPLACED IAW SRM 51-40-17.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 74,172 hrs · 17,266 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT SHEAR TIE HAS CORROSION AT BS1395 BETWEEN S-39L AND 39R IS OUT OF LIMITS PER SRM 53-00-07 AND REPLACED PER SRM 51-40-02. (LP 0239556)

Part: SHEAR TIE — CORRODED (BS 544) · corrosion level 2 · airframe 74,172 hrs · 17,266 cycles

FWD CARGO LOWER SHEAR TIE HAS CORROSION AT BS 544, BETWEEN STRINGERS 35 - 36L AND WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 1208-1428) · airframe 74,172 hrs · 17,266 cycles

CORROSION FOUND ON THE SEAT TRACK, RBL 88.5, BETWEEN BS 1208 AND 1428, FOUND TO BE OUT OF LIMITS. THE SEAT TRACK WAS REPLACED.

Part: ANGLE — CRACKED (NLG WW BLKHD) · airframe 74,172 hrs · 17,266 cycles

DURING HFEC INSPECTION, FOUND ONE CRACK ON THE RT NOSE WHEEL WELL BULKHEAD ANGLE. REPAIRED.

Part: SMOKE DETECTOR — MALFUNCTIONED (CREW REST) · airframe 73,937 hrs · 17,237 cycles

SMOKE ALARM IN F/A CREW REST SOUNDS INTERMITTENTLY. PERFORMED TEST SYSTEM OPERATION IS NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 73,580 hrs · 17,188 cycles

ACRID ODOR REPORTED ON RIGHT SIDE OF JET. COULDN'T DETECT ANY UNUSUAL ODORS DURING WALK THROUGH OF CABIN RIGHT SIDE ROWS 28-30.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,576 hrs · 16,170 cycles

COCKPIT EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. SYSTEM CHECKS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 62,423 hrs · 15,790 cycles

LEFT WINGLET LOWER SKIN FASTENER HOLES NR 1 & NR 2 STILL SHOW CRACK INDICATIONS AT .282, REF; 5724-01010-03B, STEP 2 C, ERA NR 533600-14AD, REV 0, MATCHES PRI 533600-14AD, REV 2, DATED 28, FEB 15, 1345E.

Part: SKIN — CRACKED (RT WING) · airframe 62,423 hrs · 15,790 cycles

RIGHT WING LOWER IN SPAR SKIN WS 990, STRINGER 9.5 CRACKED. REPAIRED IAW ERA 533881-14.

Part: SKIN — CRACKED (RT WING) · airframe 62,423 hrs · 15,790 cycles

RIGHT WINGLET LOWER SKIN FASTENER HOLES NR 1 & NR 2 STILL SHOW CRACK INDICATIONS AT .282, REF; 5724-01010-04B, STEP 2 C. ERA 533600-14AD, REV 0, MATCHES PRI 533600-14AD, REV 1, DATED 02 MAR 15, 10:45E.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,662 hrs · 14,670 cycles

EMERGENCY SEAT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY M9009 AND BATTERY PACK IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,623 hrs · 14,665 cycles

PATH LIGHTING CEILING LIGHTS OUT LT AISLE BETWEEN SEAT ROW17 AND 29. REPLACED BATTERY PACK IAW AMM 33-51.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,579 hrs · 14,659 cycles

RT WING INBD MAIN FLAP LWR SURFACE AFT PANEL WAS DENTED AND REPAIRED IAW SRM 57-53-01 REPAIR 1, FIG 201 AND 51-70-10, FIG 201, SHT 1.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 53,579 hrs · 14,659 cycles

RT WING INBD AFT FLAP UPPER OTBD SURFACE WAS CHAFED AND REPAIRED IAW SRM 57-53-01 REPAIR 1, FIG 201 AND 51-70-10, FIG 201, SHT 1.

Part: FLOORBEAM — ELONGATED (BS 764) · airframe 53,579 hrs · 14,659 cycles

M/D BS 764, LBL 14, FLOORBEAM MOUNTING HOLE ELONGATED. REPAIRED IAW SRM 53-00-51, FIG 201 REPAIR 1.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 53,579 hrs · 14,659 cycles

RBL 20, FLOORBEAM CORRODED. REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 1.

Part: TIRE — FAILED (MLG) · airframe 51,982 hrs · 14,429 cycles

MLG WHEEL TIRE NR 7 BLOWN ON TAKEOFF. REPLACED NR 7 MAIN WHEEL ASSY IAW AMM 32-45-01. .

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 51,817 hrs · 14,407 cycles

SEAT 18B EMERGENCY ESCAPE PATH MARKING LIGHT INOPERATIVE. RESEATED PINS ON18B SEAT HARNESS LIGHT NOW OK.

Part: FLAP — DENTED (RT WING) · airframe 48,099 hrs · 13,922 cycles

TWO DENTS ON THE RIGHT I/B TRAILING EDGE FLAP UNDERNEATH. DENTS MEASURE ARE 4 INCH WIDTH AND 0.05 DEEP. SECOND DENT 3 INCH WIDTH AND 0.04 DEEP. PERFORMED METAL HOT BOND REPAIR PER B767-300 SRM 51-70-10 REPAIR 4 FIG 201 AND SRM 57-53-01 REPAIR 1 FIG 201.

Part: PANEL — DAMAGED (NR 2 PYLON) · airframe 48,099 hrs · 13,922 cycles

NR 2 PYLON PNL 446CR HAS ELONGATED HOLES AND IS BEING REPAIRED ON A PRI WHICH IS LISTED AS A MAJOR REPAIR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 48,099 hrs · 13,922 cycles

C2 DOOR REAR LWR EDGE IS DENTED AND IS MAJOR REPAIR AS PER PRI. REPAIRED IAW ER/A 496350-14 REV O.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 48,099 hrs · 13,922 cycles

FS 478 STR 23R FWD CARGO DOOR CUT OUT FRAME WEB IS CRACKED AND REPAIR IS LISTED AS MAJOR ON PRI. REPAIRED IAW ER/A 496355-14 REV O.

Part: ACCESS PANEL — WORN (NR 1 ENGINE) · airframe 48,099 hrs · 13,922 cycles

NR 1 ENG RT C-DUCT LWR REAR ACCESS PNL INTERIOR REAR EDGE WORN. LISTED AS MAJOR REPAIR ON PRI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 48,099 hrs · 13,922 cycles

FLOORBEAM UPPER CHORD CRACKED AT FS 654+44 LBL 13 IN FWD CARGO COMP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,099 hrs · 13,922 cycles

FS 903 LT AT STR 21L FRAME INNER CHORD IS CRACKED. REPAIRED IAW ER/A 496353-14AD REV 0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,099 hrs · 13,922 cycles

FS 903 RT AT STR 21R FRAME INNER CHORD IS CRACKED. REPAIRED IAW ER/A 496354-14AD REV O.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 48,099 hrs · 13,922 cycles

FS 927 RT FRAME LWR ATTACH SUPPORT FITTING IS CRACKED.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 48,099 hrs · 13,922 cycles

LEFT WING O/B FLAP LEADING EDGE FAIRING FOUND DELAMINATED AREA AT O/B OF NR 2 FLAP TRACK AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AT DELAM AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 48,099 hrs · 13,922 cycles

LEFT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 48,099 hrs · 13,922 cycles

RIGHT WING I/B MAIN FLAP O/B LEADING EDGE MAIN FLAP O/B LEADING EDGE FAIRING DELAM. COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 48,099 hrs · 13,922 cycles

LEFT WING O/B FLAP LEADING EDGE FAIRING FOUND DELAMINATED AT I/B OF NR 1 FLAP TRACK AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AT DELAM AREA AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PARA 5A(1) FIG 5.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,628 hrs · 13,862 cycles

MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT BEHIND THE WING ON THE RIGHT SIDE TO BE INOPERATIVE. THE CHARGER WAS REPLACED AND THE SYSTEM NOW OPERATES NORMALLY.

Part: WIRE — PULLED (CABIN) · airframe 44,103 hrs · 13,383 cycles

DURING EMERGENCY LIGHT CHECK MAINTENANCE FOUND PULLED WIRE FROM THE CONNECTOR OF THE EMERGENCY LIGHT AT 17GF AND RE-TERMINATED. SYSTEM OPERATION IS NORMAL. (2010-D1304) (DL76G103009)

Part: WIRE — OUT OF POSITION (PSU) · airframe 44,004 hrs · 13,371 cycles

A PASSENGER SMELLED BURNING PLASTIC AT SEATS 30-33ABC WITH READING LIGHTS DIMMING. THE READING LIGHTS WERE TURNED OFF AND THE SMELL DISSIPATED. MAINTENANCE FOUNDS WIRING HARNESS ABOVE ROW 30AB PSU AREA LOOSE FROM ATTACHED CLIPS AND HAD BEEN LAYING ON BACK SHELLS OF THE LIGHT ASSEMBLY AND REROUTED THE HARNESS, SECURED THE CLIPS FOR CLEARANCE AND RE-LAMPED THE READING LIGHT IN ROWS 30-33AB. NO SMELL NOTED. SYSTEM OPERATION IS NORMAL. (2010-D1283) (DL76G102954)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,743 hrs · 13,338 cycles

DURING DRC MX, FOUND EMERGENCY ESCAPE PATH MARKING LIGHT OUT AT SEAT 22AB AND FORWARDED IAW MEL 33-51-03A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,052 hrs · 13,124 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEATS 21AB THROUGH 31AB ARE INOPERATIVE. MX REPLACED BATTERY PACK M9009. SYS OPS IS NORMAL. (DL76G101417)

Part: PROCESSOR — MALFUNCTIONED (TCAS) · airframe 40,199 hrs · 12,894 cycles

NO TCAS ON RADAR FOR 45 MIN. PULLED F12 C/B WAITED FOR 5 MIN AND THEN TRIED 10 MIN WOULD NO RESET. CAME ON BRIEFLY FOR ABOUT 5 MIN THEN WENT OUT AGAIN FOR 15 MIN, COME ON AGAIN ENROUTE. REPLACED TCAS PROCESSOR IAW AMM. ALSO SHOOK DOWN WIRING AT CONTROL PANEL AND RACK CONNECTOR. RMVD RT ATC XPONDER AND CKD PINS DUE TO PREV REPORT OF PUSHED BACK PIN. ALL OPS CKS GOOD.

Part: FIRE WARNING — MALFUNCTIONED (LT ENGINE) · airframe 39,873 hrs · 12,849 cycles

ON TAXI LT ENG FIRE LP 1 STATUS MSG. UNABLE TO DISPATCH ON 120. THEN LATER APPROVED. T/S PER FIM SWAPPED CARDS M681 AND 682, NO HELP SWAPPED BACK, SAME SWAPPED CARDS M10224 AND M10274 NO HELP, SWAPPED BACK T SAME OUT OF TIME ATL FWD TO MCO/PLAC PER MEL 26-11-01. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 39,414 hrs · 12,791 cycles

ATC REPORTED NO SIGNAL FROM A/C. UNABLE TO RESOLVE, RTB. REMOVED AND REPLACED ATC CONTROL PANEL SYS CHECKS GOOD USING TIC 48 BOX PER AMM. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: FAN — FAILED (E/E BAY) · airframe 37,159 hrs · 12,515 cycles

ON TAXI OUT, ALARM SOUNDED FROM BELOW FLOOR. EQUIPMENT COOLING OVERHEAT LIGHT ILLUMINATED WITH FWD EQ SUP FAN 1 STATUS MSG. PULLED/COLLARED FWD EQ SUPPLY FAN 1 CB, FWD TO MCO/PLAC PER MEL 21-58-03. REMOVED AND REPLACED FWD EQUIP COOLING SUPPLY FAN NR 1 P AMM. OPS CHECK OK. MCO AND PLACARD REMOVED.

Part: SENSOR — MALFUNCTIONED (#2 ENGINE) · airframe 36,580 hrs · 12,439 cycles

ON TAKEOFF RIGHT ENGINE SURGING N1 +/- 10 PERCENT. ALL OTHER ENGINE PARAMETERS ALSO FLUCTUATING. DECLARED AN EMERGENCY AND RETURNED TO JFK. LANDED OVERWEIGHT. MX IN PROGRESS. PIMU FAULT 352-15A/B AND EEC CONTROL MSG. REPLACING CIT SENSOR, N1 PROBE AND PERFORM HPC BORO.

Part: SENSOR — CONTAMINATED (NR 2 ENGINE) · airframe 36,580 hrs · 12,439 cycles

ON CLIMB-OUT FROM JFK PASSING 8000 FT RT ENG STARTED SURGING. STATUS MSG R ENG CONTROL. DECLARED EMERGENCY AND RETURNED TO JFK. ENG WAS NOT S/D. OVERWEIGHT LANDING. R PIMU FAULTS T2.5 SNSR. (CIT) REPLACED SAME. REMOVED AND REPLACED N1 PROBE. BOROSCOPE HPC NTF, ENG R/U OK.

Part: VALVE — WARNING LIGHT · airframe 35,083 hrs · 12,256 cycles

AFTER SECOND ENGINE START NR 2 ENG, FWD EQUIPT VAL EICAS MSG WITH ASSOCIATED VALVE LIGHT ON EQUIPMENT COOLING PANEL. WENT TO STANDBY, NO HELP. RETURN TO GATE. VALVE LIGHT AND EICAS MSG WENT OUT WHEN NR 1 ENG SHUT DOWN. FWD TO MCO AND PLACARD PER MEL 21-58-07. VALVE LOCKED CLOSED T/S FWD EQUIP VALVE MSG PER FIM. NO FAULTS FOUND. EQUIPMENT COOLING SYS CKS GOOD.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 35,091 hrs · 12,257 cycles

ATB - DUE TO ALTIMETER SPLITS.

Part: VALVE — INTERMITTENT (RT A/C PACK) · airframe 35,026 hrs · 12,249 cycles

DURING TAXI OUT OF BCN RT PACK VALVE WOULD NOT OPEN AFTER TURNED OFF FOR ENG START. RTB, SWAPPED PACK CONTROL CARDS NO HELP. RESEATED FCV CONNECTOR. NOW OPN NORMAL.

Part: TIRE — FAILED (MLG) · airframe 33,123 hrs · 12,025 cycles

FLIGHT 74/12 MEDICAL DIVERTED INTO ORF AND IN THE PROCESS BLEW 4 MAIN TIRES. SENT AMT'S FROM ATL TO REPLACE AND INSPECT.

Part: INDICATOR — OVERHEATED (WX RADAR SYS) · airframe 32,386 hrs · 11,936 cycles

IN FLIGHT HEATED ELECTRICAL WIRE SMELL FROM WX RADAR LOST DISPLAY BOTH C/B`S PULLED. FOUND WX RADAR SCREEN OVERHEATED. COOLING TUBE FOR WX RADAR SCREEN RACK BROKEN NEEDS NEW COOLING TUBE AND WX RADAR SCREEN. REPLACED COOLING TUBE. REPLACED WX RADAR DISPLAY PER M/M.

Part: BRAKE — OVERHEATED (RT MLG) · airframe 31,423 hrs · 11,812 cycles

ON ARRIVAL, RT MAIN GEAR BRAKES REPORTED SMOKING BY TOWER ON TAXI IN. WHEN ARRIVED AT GATE RIGHT BRAKES INSPECTED WITH NO HYDRAULIC LEAKS EVIDENT. BRAKE CYCLED SEVERAL TIMES WITH NO FAULT. SUSPECT DE-ICE FLUID CONTAMINATION.

Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 31,313 hrs · 11,798 cycles

WHILE WORKING OPN 58118 FINAL ESCAPE SYSTEM CHECK FOUND FOUND SLIDE WAS PARTIALLY DE-LACED AND BOTH FWD AND AFT DEPLOYMENT CABLES AND AND DEPLOYMENT CABLE RETRACTORS WERE NOT INSTALLED ON THE A/C. PARTS WERE ORDERED AND DISCREPANCY CORRECTED.

Part: VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 30,385 hrs · 11,679 cycles

RTO FOR LEFT ENG PRV MESSAGE. REMOVED L ENG PRV. REMOVED AND REPLACED LT ENG PRV CONTROLLER PER AMM. INSTAL LT ENG PRV VLV AND REPLACED MUSCLE AIR FLEX LINE. PERFORMED ENG RUN-UP SYSTEM OPS CK OK PER MM.

Part: PRESSURE SWITCH — UNKNOWN (NR 2 ENGINE) · airframe 30,228 hrs · 11,658 cycles

RTO DUE TO PRV VALVE STATUS MSG. REPLACED OVER PRESS SWITCH.

Part: SWITCH — UNKNOWN (NR 2 ENGINE) · airframe 30,228 hrs · 11,658 cycles

ANNUNCIATED AS ADVANCED POWER FOR T/O, DISC TO AT 74 KTS. NO LIGHT ON RECALL. T/S PER FIM. PRV CHECKED NORMAL. REPLACED OVERPRESSURE SWITCH PER AMM.

Part: SCAVENGE PUMP — UNSERVICEABLE (NR 1 ENGINE) · airframe 29,687 hrs · 11,594 cycles

AIRCRAFT 173 FLIGHT 161/15 DIVERTED TO SANTIAGO SPAIN, AFTER DEPARTING FROM ROME DUE TO LEFT ENGINE LOSS OF OIL QTY AND PRESSURE. ENGINE WAS SHUTDOWN PRIOR TO REACHING RED LINE. PERFORMED WINDMILL INSP, NO DEFECTS FOUND. REPLACED LUBE AND SCAVENGE OIL PUMP PER MM. WINDMILLED ENG, NO LEAKING NOTED. RAN ENG FOR 5 MIN. INSPECTED MAIL OIL FILTER CLEANED BOWL RT ENG AGAIN 5 MIN TEMP PRESS NO LEAKS ALL OK. FILTER AND BOW CLEAN CHIP DETECTORS CLEAN. RESERVICED OIL TANK.

Part: RELAY — FAILED (UNKNOWN) · airframe 29,123 hrs · 11,524 cycles

RTB FWD CARGO OVERHEAT EICAS MSG. REPLACED RELAY K231 PER FIM.

Part: STARTER — INOPERATIVE (NR 1 ENGINE) · airframe 28,255 hrs · 11,413 cycles

NR N2 ROTATION NR 1 ENG. REMOVED AND REPLACED NR 1 ENG STARTER AND START VALVE PER M/M OPN NML.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 27,429 hrs · 11,313 cycles

WHEN PUSHING UP THROTTLES FOR T/O LEFT GEN DROPPED OFF, LT BUSS ISOLATION AND TRU MESSAGE. RETURNED TO BLOCKS. MTC IN PROGRESS. SWAPPED TO 1601. MEGGED FEEDER CABLES CKD OK. CHANGED IDG. RAN ENG UP TO 90 PCT N1. LOADED GEN TO 75 PCT LOAD. ALL OPS NORMAL, NO FAULTS.

Part: OVEN — INOPERATIVE (AFT GALLEY) · airframe 27,155 hrs · 11,279 cycles

FOUND GALLEY REAR CENTER OVEN INOP, FWD TO MCO AND PLACARD PER MEL 25-20-01H CB PULLED AND COLLARED DUE TO AFT GALLEY OVEN NR 6 CB POPPED WITH REPORT OF VISABLE ELECTRIC FLASH. REPLACED OVEN CKS GOOD REMOVED MCO AND PLAC.

Part: ANTENNA — INOPERATIVE (WX RADAR SYS) · airframe 27,054 hrs · 11,267 cycles

RECEIVED NO GROUND OR WEATHER RETURNS ON WX RADAR INFLT. REPLACED T/R NO HELP. REPLACED WXR ANTENNA, NO HELP. TRIED ANOTHER TRANSCEIVER. SYS CHECKS OK.

Part: WIRE — SHORTED (COCKPIT) · airframe 26,836 hrs · 11,234 cycles

RTB DUE TO NO DATA FROM LEFT IRU. FOUND W161-9009B-22 SHORTED TO SHIELD AT D4769P. REPLACED WIRE IRUS FMC TCAS, ALL CK NORMAL.

Part: ENGINE — FAILED (APU) · airframe 24,839 hrs · 10,985 cycles

APU FAILED TO START ON GROUND. REPLACED APU.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 24,672 hrs · 10,966 cycles

LEFT GEN FAILED ON GROUND. REPLACED LEFT ENG IDG PER AMM. LEAK CHECK OK GROUND OPS OK.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 22,219 hrs · 10,258 cycles

RT HORIZONTAL STABILIZER / UPPER SKIN AT RIB 12, S-5 / REPAIR OF GROUND DAMAGE. GOUGE DUE TO GROUND DAMAGE WAS CUT OUT OF THE RT HORIZONTAL STABILIZER UPPER SKIN AT RIB 12 AND S-5. AN ALUMINUM EXTERNAL DOUBLER IS INSTALLED WITH HI-LOKS TO REPAIR THE DAMAGE.

Part: ACTUATOR — INOPERATIVE (RUDDER TRIM) · airframe 22,005 hrs · 10,170 cycles

RUDDER TRIM INOP. REPLACED RUDDER TRIM ACTUATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,180 hrs · 8,527 cycles

OVERHEAD EMERGENCY LIGHTS AT FWD F/A POSITION MID GALLEY AND SEAT ROW 47 INOP. RELAMPED, ALL CHECKED GOOD PER MM33.

Part: FAN — ODOR (RIGHT) · airframe 16,882 hrs · 7,893 cycles

DISTINCT HOT ODOR OCCURRED 3 SEPARATE TIMES DURING FLIGHT. FWD RT RECIRCULATION FAN TO MCO/PLAC PER MEL 21-25-01A. REPLACED RT RECIRCULATION FAN PER M/M, REMOVED MCO/PLAC.

Part: FAIRING — SEPARATED (NR 2 ENGINE) · airframe 8,991 hrs · 4,322 cycles

DURING FLT BALL CAP FAIRING DEPARTED A/C CAUSING DAMAGE TO THE NR 7/8 SLATS AND STRUCTURE UNDERNEATH FAIRING. INSPECTED AREA REPLACED UPPER RT FWD PYLON FAIRING AND REPAIRED DAMAGE ON NR CARDS 1-11. REPLACED 8 SLAT ON N/R CARD 10 A ROUTINE JIC OPN 7008AD ON CARDS 1-2. ON, OFF A 271004046 30 825.

Part: RELAY — FAILED (IGNITION PANEL) · airframe 6,259 hrs · 3,005 cycles

ON FINAL APPROACH (APPROX 10 MILES OUT) RIGHT ENGINE STARTED TO ROLL BACK. UPON SELECTING FLT WITH IGNITION SWITCH THE ENGINE RETURNED TO SET THRUST AND RAN NORMALLY THROUGH TOUCHDOWN AND TAXI. T/S AND TESTED IGNITION SYSTEM PER M/M 74-00-00-5-H-02. FOUND NO IGNITION ON NR 2 ENG WITH SLATS EXTENDED IGN IN SINGLE AND AUTO AS SHOULD. FOUND RELAY K2 ON PANEL M49 IGNITION SELECTOR PANEL BAD. DUE TO POSSIBLE PENDING FLAME-OUT T/S PER FIM 73-21-00 FIG 105. NO RELATED PIMU FAULTS FOUND. REMOVED AND REPLACED IGN SELECT PANEL, ALL MM TEST TASK CKD NORMAL.

Part: UNKNOWN — ODOR (CABIN)

FLT ATTN REPORTED HEAVY ELEC SMELL FROM MID GALLEY AREA AFTER TAKEOFF. SMELL DISSIPATED DURING APPROACH. CHECKED ACFT WITH ALL SYSTEMS TURNED ON, NO PROBLEMS FOUND. REPLACED BALLASTS AT RT MID LAV MIRROR LGT AND M1325 AND M1323 IN MID GALLEY ABOVE CEILING. CHECKS OK ON VERIFICATION FLT.

Part: SKIN — DAMAGED (BS 654-687)

THE FUSELAGE SKIN AT FS 654+33 WAS STRUCK BY GROUND EQUIPMENT RESULTING IN MULTIPLE PUNCTURES AND GOUGES BETWEEN STRINGER 37R AND BL 0. THE DAMAGED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER ER/A 367045-14, REV A.