N127DL

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 80,180 hrs · 34,487 cycles

ANTENNA DOUBLER FOUND DAMAGED. REPAIRED IAW ERA 520703-14.

Part: CIRCUIT CARD — FAILED (FIRE WARNING) · airframe 79,649 hrs · 34,345 cycles

AT CRUISE, ABOUT TWO HOURS INTO FLIGHT "RT ENGINE O/H LP2" STATUS MESSAGE. R & R RT ENG OVERHEAT CARDS M690 & M10274 IAW AMM 26-10-01. OPS CHECKED GOOD.

Part: FAILSAFE — CRACKED (BS 955) · airframe 78,576 hrs · 34,037 cycles

UT INSPECTION, FOUND CRACK INDICATION ON FAILSAFE STRAP AT THE RT BULKHEAD AT BS 955. BS 955 AT RT BLKHD FAIL SAFE STRAP REPAIR CARRIED OUT IAW PRI 513478-14AD, REV 0, REV 1 & REV 2. PERMANENT REPAIR COMPARED AND COMPLIED WITH FINAL ERA 513478-14AD, REV ORIGINAL.

Part: FRAME — CORRODED (BS 977) · corrosion level 2 · airframe 78,543 hrs · 34,029 cycles

BS 977 FRAME WEB AT S21-22R CORRODED. FRAME WEB REPAIRED IAW PRI 514000-14, REV ORIGINAL, 1, 2, 3 AND 4.

Part: WEB — CRACKED (RT WING) · airframe 78,543 hrs · 34,029 cycles

RIGHT WING L/E STATION 674 NOSE BEAM CRACKED WEB CARRIED OUT REPAIR IAW PRI 514008-14, REV 0. THE REPAIR COMPARED AND COMPLIED WITH ER/A 514008-14, REV ORIGINAL.

Part: TEE FITTING — CORRODED (BS 955) · airframe 78,543 hrs · 34,029 cycles

FOUND LEFT TEE FITTING WITH CORROSION. R & R WITH NEW TEE FITTING IAW PRI 514001-14AD, REV 0.

Part: FAILSAFE — CRACKED (BS 955) · airframe 78,576 hrs · 34,037 cycles

UT INSPECTION FOUND CRACK INDICATION ON FAILSAFE STRAP AT THE REAR SPAR LT BULKHEAD AT BS 955. BS 955 LT BULKHEAD FAIL SAFE STRAP REPAIR CARRIED OUT IAW PRI 513476-14, AD REV 0, REV 1 & REV 2. PERMANENT REPAIR COMPARED AND COMPLIED WITH FINAL ERA 513476-14AD, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 1185) · corrosion level 2 · airframe 78,543 hrs · 34,029 cycles

AFT CARGO BAY AT APPROX BS 1185 S36R CORRODED STRINGER, TRIMMED OFF AND CARRIED OUT SECTION REPAIR IAW SRM 53-00-03, REPAIR 2, FIG 201, REV 92.00.

Part: STRINGER — CORRODED (BS 414 S35R) · corrosion level 2 · airframe 78,543 hrs · 34,029 cycles

FWD CARGO BS 414 FOUND STRINGER 35R CORRODED. REPLACED STRINGER.

Part: STRINGER SPLICE — CORRODED (BS 437) · corrosion level 2 · airframe 78,543 hrs · 34,029 cycles

FWD CARGO BS 437 S35L STRINGER SPLICE FOUND CORRODED. REPLACED DAMAGED STRINGER SPLICE.

Part: KEELBEAM — CORRODED (BS 870-915) · corrosion level 2 · airframe 78,543 hrs · 34,029 cycles

LOWER KEEL BEAM FOUND TO HAVE SEVERAL AREAS OF CORROSION BETWEEN BS 870-915. REPLACED SECTION.

Part: STRINGER — CORRODED (BS 420) · corrosion level 2 · airframe 78,543 hrs · 34,029 cycles

FOUND BS 420 STRINGER 36L CORRODED. STRINGER CUT AND DISCARDED. CARRIED OUT SECTION REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 325) · airframe 78,543 hrs · 34,029 cycles

CABIN FLOOR SUPPORT AT BS 325, RBL 50 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, REV 91.02. FOUND OUT OF LIMIT IAW SRM 53-00-51, FIG 101, REV 91.02. FLOOR SUPPORT TEE DAMAGED AREA CARRIED OUT REPAIR IAW SRM 53- 00-51, FIR 201, REPAIR 1.

Part: COFFEEMAKER — DAMAGED (AFT GALLEY) · airframe 77,966 hrs · 33,865 cycles

DOOR 2L COFFEEMAKER DAMAGED AND INOPERATIVE. COFFEEMAKER SPARKING FROM SIDES. COFFEEMAKER REMOVED IAW ERA 511387-14. BOLT SHEARED OFF. C/BS COLLARED AND WIRES SECURED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 74,906 hrs · 32,984 cycles

EMERGENCY ESCAPE PATH LIGHTS AT AFT RT LAVATORY RED LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SYSTEM OPS NORMAL.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,906 hrs · 32,984 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 2AB ARE INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS. SYSTEM OPS NORMAL.

Part: SILL — CORRODED (FS 1270) · airframe 74,340 hrs · 32,822 cycles

FUSELAGE AFT CARGO DOOR LOWER SILL FS 1270 UPPER CHORD. REPAIR IAW ERA 497875-14.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 69,621 hrs · 31,536 cycles

AFT RT DOOR RED EMERGENCY LIGHTS ARE INOPERATIVE. MX FOUND WIRES CUT ON LENS ASSY AND SPLICED AND SECURED WIRES. SYS OPS IS NORMAL.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 69,618 hrs · 31,535 cycles

AFT RT DOOR RED EMERGENCY LIGHTS INOP. FOUND WIRES CUT TO LENS ASSY. SPLICED WIRES AND SECURED. OPS CK GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 65,255 hrs · 30,237 cycles

ON DESCENT INTO ATL THE LEFT ENGINE ROLLED BACK. PERFORMED IN FLIGHT SHUTDOWN OF ENGINE. INSP INLET AND EXHAUST NTF. CHECKED CHIP DETECTORS NTF. RAN ENG IDLE AND T/O POWER ALL PARAMETERS NORMAL. SUMPED LEFT TANK BEF RUN NTF. REMOVED FUEL PUMP AND MEC. REMOVED FUEL OIL COOLER, REMOVED AND REPLACED NR 1 ENGINE PER TRANS 1T144.

Part: DUCT — SPLIT (APU SUPPLY) · airframe 63,154 hrs · 29,514 cycles

CREW REPORTED HEARING LOUD POP AND FELT EARS POP THEN GOT BODY DUCT LEAK LIGHT. AFT CABIN FILLED WITH SMOKE AND CABIN GOT VERY HOT. PASSENGER SEATED AT 42A GOT A BURN TO HER LEG. PBE AND HALON BOTTLES USED, FLT DIVERTED TO GSP. MTC FOUND PNEU DUCT LOCATED LT SIDE OF AFT B/B BLOWN/SPLIT, MPN 212T3119-17X. ALSO, HAD DAMAGE TO INSULATING BLANKETS AND SIDEWALL PANELS. DELTA MTC PERFORMING REPAIRS. VOICE RECORDER AND FLT REC PULLED AT REQUEST OF FLT SAFETY.

Part: RIB — CRACKED (RT WING) · airframe 60,887 hrs · 28,696 cycles

RT WING LES 688 AREA RIB SUPPORT FWD END CRACKED. RT WING LES 688 AREA RIB SUPPORT REPAIRED PER SRM 57-41-01 FIGURE 201 REPAIR 4.

Part: ANGLE — WORN (BS 1417) · airframe 60,887 hrs · 28,696 cycles

FS 1417 LEFT FLOOR SUPPORT ANGLE HAS AN ELONGATED FASTENER HOLE. BULK CARGO COMPT, BS1417, STR 36L AREA FLOOR SUPPORT ANGLES ELONGATED HOLE REPAIRED IAW ERA 462310-14AD REV ORG.

Part: CHANNEL — NICKED (FWD CARGO DOOR) · airframe 60,887 hrs · 28,696 cycles

FWD CARGO DR LWR EDGE FWD REPAIRED PATCH NICKED. FWD CARGO DOOR LOWER EDGE CHANNEL REPLACED SRM 51-10-02 PAGE 8.

Part: SPAR — CRACKED (LT WING) · airframe 60,887 hrs · 28,696 cycles

LT WING FRONT SPAR AT NR 8 RIB POST FOUND 1 FASTENER HOLE CRACKED AT RIB POST. LT WING FRONT SPAR NR 8 RIB AREA REWORKED AND FASTENER INSTALLED PER ERA 461699-14AD REV ORG.

Part: FRAME — DAMAGED (FS 1417) · airframe 60,887 hrs · 28,696 cycles

DURING THE CURRENT HMV IN HKG, A FASTENER HOLE WAS FOUND ELONGATED IN THE FS 1417 FRAME NEAR STRINGER 36L. A BOEING APPROVED REPAIR WAS INSTALLED PER 462310-14.

Part: BULKHEAD — CRACKED (BS 1809) · airframe 60,887 hrs · 28,696 cycles

ON HMV, FOUND BULKHEAD CRACKED. REPAIRED PER SRM 53-80-00. REPAIR NR 9 FIG 201. AREA OF REPAIR WAS BS 1809 BETWEEN STRINGER 4R AND 8R.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 60,887 hrs · 28,696 cycles

A CRACK INDICATION WAS FOUND DURING ACCOMPLISHMENT OF HORIZONTAL STABILIZER PIVOT FITTINGS PER OPN 5927AD, LHS OUTBOARD FITTING, LOWER RIB CHORD, AND LOWER SPLICE PLATE. BOEING WAS CONTACTED FOR REPAIR INSTRUCTIONS FOR HOLE OVERSIZING. THE REPAIR WAS APPROVED AND IS DOCUMENTED IN ERA 462304-14AD.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 60,887 hrs · 28,696 cycles

DURING INSPECTION PER SIP EO MOD, NR 1 PYLON BULKHEAD FITTING WAS FOUND CRACKED AT BOLT HOLE COMMON TO UPPER SPAR FITTING. THE DISCREPANT HOLE ON BULKHEAD FITTING WAS OVERSIZED TO A FINAL DIAMETER OF 1.125" UNTIL THE CRACK INDICATION WAS REMOVED. BOEING APPROVED REPAIR INSTALLED PER ERA 461699-14AD.

Part: SKIN — CRACKED (BS 1725 S7R) · airframe 60,887 hrs · 28,696 cycles

DURING INSPECTION OF THE FS 1725.5 SKIN AND CHORD STRAP AT S-7R WAS FOUND CRACKED THAT WAS OUTSIDE OF THE 767 SRM 53-80-01 REPAIR 5. BOEING APPROVED REPAIR WAS INSTALLED PER 462298-14AD.

Part: FITTING — DAMAGED (NACELLE) · airframe 60,887 hrs · 28,696 cycles

DURING INSPECTION OF THE AFT PITCH LOAD FITTING PER EA 01-074906-03AD, SEVERAL HOLES WERE FOUND TO BE OVERSIZED BEYOND THE ALLOWABLE LIMITS. BOEING WAS CONTACTED AND THEY ALLOWED THE OVERSIZED HOLES WITH CORRESPONDING MATCHING FASTENERS AS REFERENCED IN ERA 462299-14AD.

Part: FLOOR SUPPORT — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO FLOOR PANEL SUPPORT RIB AT STA 1197+66 LBL 38 CORRODED, REPAIRED ON AJN 51016 PER 53-00-07 FIGURE 201 REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO STA 1197+66 LBL10 TO LBL 30 FLOOR PNL SUPPORT RIB SIGN OF CORROSION REPAIRED ON AJN 51001 PER 53-00-07 REPAIR 4 FIG 201.

Part: FLOORBEAM — CORRODED (BS 676) · airframe 60,887 hrs · 28,696 cycles

FWD CARGO BS 676 LBL42 FLOORBEAM ANCHOR NUT CORRODED ON BOTTOM SIDE, REPAIRED ON AJN 52957 PER 53-00-07 FIGURE 201 REPAIR 4.

Part: RIB — CRACKED (LT WING) · airframe 60,887 hrs · 28,696 cycles

DURING ACCOMPLISHMENT OF SIP EO, THE LHS WING FRONT SPAR AT RIB NR 8 WAS FOUND CRACKED AT A FASTENER HOLE. THE CRACK WAS APPROXIMATELY 0.030 INCH IN LENGTH. THE SUBJECT HOLE FROM WHICH THE CRACK EMANATED WAS ALREADY BEYOND THE EA ALLOWABLES. BOEING APPROVED REPAIR INSTALLED PER 461698-14AD.

Part: NUT CLIP — UNKNOWN (NACELLE) · airframe 60,887 hrs · 28,696 cycles

DURING ACCOMPLISHMENT OF EA 01-074906-03AD, NEED TEE CLIPS ARE ATTACHED TO THE SUBJECT PITCH LOAD FITTINGS, HOWEVER THEY HAD SHORT EDGE MARGIN. BACO GAVE AMOC APPROVAL FOR THE SHORT EDGE MARGIN CONDITION. REFERENCE ER/A 461700-14AD.

Part: SWIVEL FITTING — CORRODED (MLG) · airframe 60,887 hrs · 28,696 cycles

CORROSION WAS FOUND INSIDE THE LUG BORES AND ON THE BUSHINGS OF THE LT AND RT MLG SIDE STRUT SWIVEL FITTINGS. REPAIRED PER ERA 01-462303-14 REV ORG.

Part: FLOORBEAM — CORRODED (BS 1219) · airframe 60,887 hrs · 28,696 cycles

FOUND AFT CARGO FLOOR PLANEL SUPPORT RIB AT STA 1219 LBL 40 CORROSION. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON AJN 50830.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO COMPARTMENT STA 1197 BELOW FLOOR FRAME UPPER CORD LBL 11 UPPER AND LOWER SURFACES CORRODED REPAIRED ON AJN52893 PER 53-00-07 FIRURE 2O1 REPAIR 4.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO FLOOR PANEL SUPPORT RIB AT STA 1197+66 LBL 38 SIGN OF CORROSION. REPAIRED PER 53-00-07 FIGURE 201 REPAIR 4 ON AJN 51016.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO COMPT FLOOR PNL SUPPORT RIB RBL 42 AT STA 1197+88 HOLE CUTOUT SIGN OF CORROSION. REPAIRED PER 53-00-07 FIG 201 REPAIR 6 ON AJN 51468.

Part: FLOORBEAM — CORRODED (BS 434) · airframe 60,887 hrs · 28,696 cycles

FWD CARGO BS 434 RBL 41 TO RBL 45 FLOOR SUPPORT TOP SURFACE CORRODED. REPAIRED PER 53-00-07 FIGURE 201. REPAIR 4 ON AJN 52963.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO FLOOR PANEL SUPPORT RIB AT STA 1197+110 RBL 24 AND RBL 40 BOLT HOLE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON AJN 51009.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 60,887 hrs · 28,696 cycles

AFT CARGO COMPT -STA 1197+66 LBL 10 TO LBL 30 FLOOR PANEL SUPPORT RIB SIGN OF CORROSION. REPAIRED PER 53-00-01 REPAIR 4 FIGURE 201 ON NR AJN51001.

Part: PRESSURE PANEL — CRACKED (BS 977) · airframe 60,887 hrs · 28,696 cycles

CABIN BS 977 RBL 23 MLG PRESSURE WEB SKIN CRACKED AND REPAIRED PER 53-50-51 FIGURE 201 REPAIR 1 ON NR CARD AJN 53146.

Part: SEAT TRACK — CRACKED (BS 999) · airframe 60,887 hrs · 28,696 cycles

CABIN, STA 999 RBL54.75 SEAT TRACK FOUND CRACKED. REPAIRED ON NR 51787. REPAIRED PER 53-00-51 FIGURE 201 REPAIR 3.

Part: ANGLE — CRACKED (BS 999) · airframe 60,887 hrs · 28,696 cycles

CABIN STA 999 RBL 32 SUPPORT CRACKED. REPAIRED PER 53-00-51 FIGURE 201 ON NR 51788.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,887 hrs · 28,696 cycles

CABIN BS287, RBL 60-62 FLOORBEAM UPPER CORD CORRODED AS MARKED, REPAIRED PER 53-00-51D, FIG 201 ON AJN50915.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,887 hrs · 28,696 cycles

CABIN BS 287 , RBL 24-26 FLOORBEAM UPPER CHORD FOUND CORRODED AS MARKED, REPAIRED PER 53-00-51D FIG 201 ON NR AJN50902.

Part: WIRE — SHORTED (CARGO LOADING SY) · airframe 59,926 hrs · 28,347 cycles

FOUND C2 BAG BIN LOADING SYS INOP, 5 BREAKERS BLOWN. SUSPECT SHORT UNDER BAG BIN FLOOR. FOUND WIRE HARNESS MELTED BETWEEN 6L AND 6R PDU STA 1230. REPAIRED 10 EACH TRIPLE WIRE PDU POWER WIRES AND 9 EACH SINGLE PDU CONTROL WIRES UNDER 6L PDU PER BSWPM CHPT 20. AFT CARGO LOADING SYS OPS CK NORMAL. REMOVED MCO AND PLAC.

Part: ENGINE — MAKING METAL (NR 2) · airframe 56,103 hrs · 26,880 cycles

IN CRUISE, THE RT ENG HAD VIBRATION TO 5.0. DURING T/S IN FLT, THE ENG ANALYST AT HOME GOT A SMART SIGNAL THAT SHOWED A SHIFT IN F/F GET AND LOW N-2 ROTOR SPEED OCCURRED. CALLED THE MTC COORDINATOR WHILE ON THE RADIO PATCH AND ADVISED WHAT OBSERVED. ADVISED THE CREW TO RETURN TO ATL, METAL WAS FOUND IN THE TAIL PIPE AND ENGINE WAS REPLACED.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 53,874 hrs · 25,976 cycles

AFT LEFT FA JUMPSEAT EMERGENCY FLASHLIGHT STRAP BROKEN. REPLACED FLASHLIGHT AND STRAP.

Part: OVEN — ODOR (FWD GALLEY) · airframe 53,714 hrs · 25,897 cycles

FWD GALLEY LOWER OVEN HAS AN ODOR OF BURNING RUBBER WHEN ON. REPLACED OVEN, OPS CKECKS OK.

Part: POWER SUPPLY — DISCHARGED (RT EMERG EXIT) · airframe 53,551 hrs · 25,814 cycles

FOUND ON TRANSIT CHECK, EMERGENCY ESCAPE SQUIB TEST INOP IN BOTH TEST 1 AND 2. REPLACED POWER SUPPLY.

Part: FAN — FAILED (E/E BAY COOLING) · airframe 53,458 hrs · 25,762 cycles

ON DESCENT PASSING THRU APPROX 15,000 FEET COCKPIT CREW SMELLED ELECTRICAL FUMES. SHORTLY AFTER THE FWD EXHAUST EQUIP COOLING FAN C/B POPPED. CREW RAN SMOKE, FUMES, FIRE, ELECTRICAL CHECKLIST. FUMES SUBSIDED AFTER C/B POPPED. C/B AND WIRING CHECK GOOD, FAN MAKING A LOT OF NOISE. REPLACED FWD EXHAUST EQUIP COOLING FAN PER M/M. OPERATION CHECKS GOOD.

Part: TIRE — DAMAGED (RT MLG) · airframe 52,043 hrs · 25,060 cycles

FOUND ON ARRIVAL NR 3 MAIN TIRE WITHOUT TREAD. PERFORMED TIRE TREAD CONDITIONAL INSPECTION AND REPLACED TIRE PER AMM.

Part: LINK — CRACKED (NR 1 ENGINE) · airframe 49,276 hrs · 23,612 cycles

A/C LOG E302036 ITEM 007 DETAILS REPLACEMENT OF AFT MOUNT O/B TANGENTAL LINK DUE TO CRACK THROUGH ONE SIDE OF LINK EVEN WITH CENTERLINE OF BEARING. CRACK WAS FOUND BY MTC ON WALK AROUND AND REPLACED. NO OPERATIONAL PROBLEMS WERE NOTED BEFORE OR AFTER REPLACMENT. REPLACED CRACKED LINK ON O/B AFT MOUNT NR 1 ENG PER MM.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 48,881 hrs · 23,406 cycles

THE FUSELAGE SKIN WAS DAMAGED FROM A LIGHTNING STRIKE AT FS 1219 AND STRINGER 3R. THE DAMAGED SECTION OF SKIN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS. THE UNDERLYING STRINGER WAS CUT AND A NEW SECTION SPLICED IN PER B767-300 SRM. THE REPAIR WAS DOCUMENTED PER ER/A 384955-14.

Part: ENGINE — LEAKING (NR 1) · airframe 48,857 hrs · 23,393 cycles

ENROUTE TO EWR LT ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DROP. QUANTITY REACHED 0.SHUT DOWN ENGINE WHEN LOW OIL PRESSURE LIGHT CAME ON AT APPROXIMATELY 10-11 PSI. FOUND OIL LEAK FROM OIL INLET PRESSURE TUBE. REMOVED AND REPLACED SCAVENGE TUBE ON NBR 6 BEARING HOUSING PER MM . LE CK GOOD.

Part: LINE — LEAKING (RT ACMP TO FLTR) · airframe 46,743 hrs · 22,379 cycles

RT HYD QUANITY SYSTEM TO ZERO RETURN TO LAS VEGAS CA FND LINE TO RT ACMP LEAKING, RPLD SAME.

Part: IDG — LACK OF LUBE (NR 1 ENGINE) · airframe 46,026 hrs · 22,041 cycles

LT GEN DRIVE EICAS MESSAGE ILLUMINATED WHEN TAKEOFF POWER APPLIED. LIGHT WENT OUT WHEN THROTTLES RETURNED TO IDLE. TAKEOFF ABORTED BELOW 80 KTS. SERVICED IDG, RAN NR 1 ENG, PUT GEN ONLINE, LOADED GEN TO .67 PERCENT VOLTS AND FREQS CHECK NORMAL. OIL TEMP NORMAL. OPN NORMAL, LEAK CHECK OK.

Part: DUCT — DAMAGED (RT WING) · airframe 45,846 hrs · 21,933 cycles

L/E SLAT ASYM MESSAGE AND LEADING EDGE LIGHT ON AFTER LANDING WHILE BRINGING FLAPS UP. REPLACED TAI DUCT AND TORQUE TUBE. REPAIRED SLAT PANELS.

Part: MANIFOLD — LEAKING (#2 ENGINE) · airframe 45,137 hrs · 21,580 cycles

IR - LOST R ENG OIL PRESS (PRESS INDICATING 4 PSI) ENG SHUTDOWN 20 MIN BEFORE LNDG. (4 PSI INDICATING WHILE WINDMILLING. CA - FOUND FUEL POURING FROM FUEL MANIFOLD AT 5 OCLOCK POS. FROM UPPER BRANCH (SECOND NOZZLE BELLOW LOWER IGNITOR PLUG).REMOVED AND REPLACED FUEL MANIFOLD LEAK CHECK AND IDLE RUN OK. PERFORMED TEST 4 TAKE OFF POWER CHK PFHB. HIGH POWER RUN UP OK.

Part: STIFFENER — CRACKED (CTR WNG) · airframe 43,357 hrs · 20,746 cycles

CRACKS DISCOVERED IN THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE WING CENTER SECTION FRONT SPAR. THE DAMAGE IS IN THE WEB OF EACH OF THE STIFFENERS AT THE OVERWING LONGITUDINAL FLOORBEAM TO STIFFENER JOINT. ER/A 397596-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,357 hrs · 20,746 cycles

SKIN DAMAGE AT STA 368 AND STRINGER 33R. ER/A 397613-14.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 41,963 hrs · 20,055 cycles

LEFT_SIDE EXTERIOR EMERGENCY LIGHTS AT L-1 DOOR AND OVERWINGEXIT INOP// REPLACED BATTERY

Part: ENGINE — FOD (NR 1) · airframe 41,858 hrs · 20,009 cycles

NR 1 ENGINE SUSTAINED DAMAGE TO 7 FANS BLADES DURING TAKEOFF FROM PBI. DEPARTMENT OF AIRPORTS FOUND 2 PARTIAL REMAINS OF TURKEY VULTURES NEAR END OF RUNWAY. ENGINE WAS NOT SHUT DOWN IN FLIGHT. ENGINE WILL REQUIRE REPLACEMENT BEFORE FURTHER FLIGHT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,709 hrs · 19,482 cycles

THE FUSELAGE SKIN WAS FOUND CORRODED ALONG THE AFT EDGE OF THE LAVATORY SERVICE CUTOUT AT FS 1582. THE CORROSION WAS REMOVED WITH A 5 X 4 INCH SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 377820-14, REV A.

Part: LINE — WORN (NR 1 ENGINE) · airframe 40,422 hrs · 19,351 cycles

DURING CLIMB FROM DFW, HYD QTY EICAS MSG WITH DECREASING QTY LEFT HYD INDICATED. ONCE LEFT ENG PRIMARY PUMP WAS TURNED OFF LEFT HYD QTY STABILIZED AT .40. FOUND HYD LINE OFF OF EDP WORN THROUGH. REPLACED AND REPOSITIONED LINE SVC SYSTEM, OPS CHECK NORMAL. OK FOR SVC.

Part: WIRE — SHORTED (GALLEY)

AT ENGINE SHUTDOWN MID GALLEY FLIGHT ATTENDANT REPORTED SHE SAW SMOKE AND ARCING WIRE UNDER THE COFFEEMAKER, PBE AND HALON BOTTLE USED. SMOKE DISSIPATED AFTER A FEW SECONDS. FOUND WIRING TO AFT MOST MID GALLEY LEFT HAND FLUORESCENT COUNTER LIGHT SHORTED. FWD GALLEY COUNTER LIGHTS TO MCO PER MEL 33-21-01A. PULLED AND COLLARED C/B FOR COUNTER LIGHTS. HALON BOTTLE PIN PULLED BUT NOT USED. INSTALLED NEW PBE AND STOWED HALON BOTTLE.

Part: SKIN — DELAMINATED (NR 9/11/12 SLAT)

THE NR 9, 11 AND 12 SLATS WERE FOUND WITH AREAS OF DELAMINATION ON THE TRAILING EDGE WEDGES. THE DAMAGED AREAS WERE TRIMMED OUT AND REPAIRED PER THE B767 SRM, 57-43-02. THE REPAIRS WERE DOCUMENTED PER ER/A 365088-14AD. (S/N 000222).

Part: SLIDE — MALFUNCTIONED (L-2 DOOR)

L2 SERV DOOR ESCAPE SLIDE PACK FELL OUT OF DOOR UPON OPENING OF DOOR SLIDE. DID NOT FALL ENOUGH TO DEPLOY, DOOR WAS NOT FULLY OPENED. REPLACED L2 DOOR SLIDE ASSY, ARM/DIARM CKS NML. DOOR NOT FULLY DISARMED BY FLT ATTEND.

Part: TE WEDGE — DELAMINATED (NR 5 LE SLAT)

THE NR 5 SLAT T/E WEDGE WAS FOUND DELAMINATED. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER THE B-767-300 SRM 51-70-10 FIG 9 PARAGRAPH 2K.

Part: TRACK LIGHT — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHT AT 32AB AND 41AB OUT. RELAMPED, OPERATION NORMAL.

Part: POWER SUPPLY — FAILED (CABIN)

OVERHEAD EMERGENCY LIGHTS FROM 17AB TO 36AB OUT AND TWO OVERHEAD EXIT SIGNS OUT. REPLACED POWER SUPPLY, OPERATION NORMAL.