N135DL

Part: SKIN — DENTED (TE FLAP) · airframe 57,670 hrs · 25,930 cycles

HAIL DAMAGE DENTS FOUND ON UPPER SKIN OF INBOARD AFT FLAP DURING MTC. DENTS TOO CLOSE TO EXISTING DOUBLERS FOR NEW LOCAL REPAIRS. REPLACEMENT OF UPPER SKIN AND CORE WAS THEREFORE NECESSARY. REPAIRED PER ERA 473815-14.

Part: FITTING — FRACTURED (NR 2 PYLON) · airframe 55,946 hrs · 25,405 cycles

NR 2 PYLON INBOARD MIDSPAR FITTING WAS REPAIRED IAW ERA 472678-14. C/W 472678-14.

Part: FITTING — FRACTURED (NR 2 PYLON) · airframe 55,946 hrs · 25,405 cycles

DURING ACCOMPLISHMENT OF INSPECTIONS PER ROUTINE OPN 5281AD (EA 01-074944-12AD, ME-02) THE AFT MOST INBOARD BOLT THROUGH THE NR 2 PYLON INBOARD MIDSPAR FITTING WAS FOUND FRACTURED. THE BOLT WAS SUCCESSFULLY REMOVED. IN ADDITION, THE LOCK FASTENERS COMMON TO THE HORIZONTAL FLANGE WERE FOUND LOOSE. THE SUBJECT HOLES WERE INSPECTED AND OVERSIZED IN ACCORDANCE WITH S/B REQUIREMENTS IN COMPLIANCE WITH AD MANDATES. REPAIR IS DOCUMENTED IN ER/A 472678-14AD.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 55,848 hrs · 25,365 cycles

UPON ARRIVAL TO GATE T-1 IN ATL AFTER ENGINE SHUTDOWN AND BEFORE JETWAY ARRIVAL THE L-1 DOOR SLIDE DEPLOYED. FOUND L-1 DOOR SLIDE RIPPED BY JETWAY REMOVED AND REPLACED L-1 DOOR SLIDE PER AMM.

Part: SKIN — CRACKED (BS 1725 S7R) · airframe 51,981 hrs · 23,932 cycles

REPAIR REMOVED THAT WAS OUT OF SCOPE FOR AD2006-09-09. UNDERLYING CHORD FOUND CRACKED. DAMAGE WAS CUTOUT AND REPAIR DOUBLER AND TRIPLER WAS INSTALLED.

Part: SUPPORT BEAM — CORRODED (NR 4 FLAP) · airframe 51,981 hrs · 23,932 cycles

FROM NR 185 PSV 15, NUMBER 4 FLAP SUPPORT BEAM HAS PITTING IN FORWARD MOUNT HOLES. REPAIRED PER ERA 089397-14MA REV O.

Part: GRND AIR VALVE — OPEN (LEFT) · airframe 51,906 hrs · 23,912 cycles

AFTER TAKEOFF, GOT FWD EQPT OVHT EICAS WENT TO STBY AS PER QRH. 5 MINS LATER CAME BACK ON WENT TO OVRD AS PER QRH. AT 35K, ALT CABIN PRESS CLIMBED ABOVE 11K AND CABIN ALT EICAS WARNING CAME ON. AFTER PERFORMING IMMEDIATE ACTION ITEMS. EMERGENCY DESCENT TO 12K CABIN ALT WARNING LIGHT CAME ON PASSING 33K ON THE WAY DOWN. RAN BITE ON BOTH CABIN PRESS AND PACK CONTROLLERS NO FAULTS. PRESSURIZED A/C TO 4 PSI FOUND GRND AIR CONNECTION PART OPEN. NO OTHER LEAKS NOTED.

Part: ENGINE — MAKING METAL (NR 1) · airframe 50,146 hrs · 23,330 cycles

LT ENG INOP, ON DESCENT LOUD BOOM AND SERVERE VIBS-ENG CONT TO RUN UNTIL SHUTDOWN-THRUST LOST. FOUND METAL IN TAILPIPE. REMOVED AND REPLACED NR 1 ENGINE ON ROUNTINE CARD TRANSMITTAL.

Part: GASKET — OUT OF POSITION (NR 1 ENGINE) · airframe 47,770 hrs · 22,453 cycles

CLIMBING THROUGH 10000 FT LEFT ENGINE FAILED TO A NEAR FLIGHT IDLE CONDITION. OPENED ENGINE FOUND FUEL LEAK AT MANIFOLD TO FUEL/OIL COOLER REALIGNED GASKET PLATE TIGHTENED. RAN ENGINE IN NORMAL/ALTERNATE MODE. PERFORMED QUICK SNAP CHECK. ENGINE ACCELERATE/DECELERATE NORMAL. ALL ENGINE PARAMETERS NORMAL NO LEAKS LEFT ENGINE OK FOR SERVICE .

Part: ENGINE — LEAKING (NR 1) · airframe 47,474 hrs · 22,348 cycles

LEFT ENGINE HOC B SUMP LEAKING, ITEM WILL REQUIRE A ENGINE CHANGE. FOUND OIL LEAKING FROM NR 6 BEARING B-SUMP BREATHER EXHAUST REPLACED NR 1 ENG PER TRANS 1T144.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 46,334 hrs · 21,860 cycles

IN FLIGHT EICAS MESSAGES C-HYD PRESS AND C-HYD QTY SHOWED .07RF, LATER WENT TO ZERO. CENTER ELEC 1 AND 2 PRESS AND CENTER AIR PRESS LIGHTS ILLUMINATED. C/W QRH PROCEDURE. INSPECTED AND FOUND HYD LINE COMING FROM RT BRAKE METERING VALVE TO T FITTING CRACKED. REPLACED LINE. SERVICED CTR HYD TO FULL. PERFORMED LEAK CHECK. LEAK CHECKS GOOD.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 44,181 hrs · 20,971 cycles

NR 1 ENG WOULD NOT ACHIEVE T/O POWER WITH ANTI-ICE ON OR OFF. RETURNED TO GATE. REPLACED MAIN ENGINE CONTROLLER.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 42,231 hrs · 20,008 cycles

RT ENGINE EGT 950 ON TAKEOFF FOR LESS THAN ONE MINUTE. FOUND LPT BLADES DAMAGED AND BROKEN PER FIM. REPLACED NR 2 ENGINE PER JIC CARD DECK 1T145. C/W NR 2 ENGINE PREFLIGHT AND LEAK CHECKS, NO DISCREPANCIES NOTED.

Part: CHARGER — MALFUNCTIONED (MAIN E&E BAY) · airframe 42,070 hrs · 19,900 cycles

MAIN BATTERY CHARGER STATUS MSG. REPLACED MAIN BATTERY CHARGER PER M/M, NO HELP. REPLACED MAIN SHIPS BATTERY PER M/M. ALL CKS NORMAL PER M/M.

Part: CIRCUIT BREAKER — TRIPPED (FAN) · airframe 40,758 hrs · 19,167 cycles

AT CRUISE, F/A REPORTED ELECTRICAL ODOR THRU OUT CABIN. DID ELECTRICAL SMOKE CHECKLIST AND PULLED C/BS ON VIDEO SYS. TURNED OFF RT RECIR FAN, THAT WAS REPORTED TO BE CAUSING VIBRATION AND PULLED C/B ON GASPER FAN (OFF LIGHT APPEARED IN GASPER LIGHT SWITCH AND FAILED AFTER RESTTING. ELECTRICAL ODOR WENT AWAY AFTER TURNING OFF UTILITY BUSSES. FWD GASPER FAN MCO AND PLACARD PER MEL 21-24-01. REMOVED AND REPLACED GASPER FAN PER AMM. MCO / PLACARD REMOVED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,458 hrs · 18,547 cycles

EMERGENCY LIGHTS FROM ROW 34 AND BACK BOTH SIDES INOP. FOUND SHORTED SEAT HARNESS AT SEAT 36AB REPAIRED SAME. REPLACED PWR SUPPLY D9048 DUE TO BLOWN FUSE.

Part: SWITCH — LOOSE (COCKPIT) · airframe 36,600 hrs · 17,168 cycles

STANDY BY POWER SWITCH LOOSE INTERNALLY CAUSING ALL THREE IRS'S TO FAIL . THIS HAPPENED IN FLIGHT ON PREV LEG. REF LOG SHEETS 792866 ITEM 2 AND 792871 ITEM 1 FOUND THAT WIGGLING STNBY PWR CAUSED TROUBLE REPLCD STBY POW PANEL IRUS OPS NML OFF SN ON SN DPN 1 D00812 D00547 311701501

Part: PIN — BACKED OUT (LIGHT HARNESS) · airframe 33,566 hrs · 15,683 cycles

PAX SEAT 31A EMERGENCY LIGHTS WON`T TEST. FOUND PULLED/BACKED OUT PIN IN SEAT HARNESS. REPAIRED SAME.

Part: GASKET — LEAKING (THERMOCOUPLE) · airframe 33,475 hrs · 15,635 cycles

LT ENG FIRE INDICATIONS SHORTLY AFTER TAKEOFF THROTTLE. RETARDED TO IDLE AND FIRE INDICATION WENT OUT. FOUND ALL THERMOCOUPLE GASKETS LEAKING. REPLACED GASKETS, CK OK ON RUN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,034 hrs · 15,426 cycles

FOUND RED EMERGENCY LIGHT INOP AT AFT R/H LAV. RELAMPED SAME OPS CK. GOOD.

Part: BULKHEAD CHORD — CRACKED (BS 1809.5)

THE FS 1809.5 BULKHEAD OUTER CAP WAS FOUND WITH A CRACK TYPICAL OF BAC S/B 767-53-0078. THE CRACKED UPPER END OF THE CHORD WAS CUT AND REMOVED. A NEW SECTION WAS SPLICED IN PER THE PROCEDURES OUTLINED IN S/B 767-53-0078 AND PER ER/A 368357-14.

Part: SHUTOFF VALVE — CRACKED (NR 10 SPOILER)

CENTER HYDRAULIC RESERVIOR NEEDS FLUID. FOUND NR 10 SPOILER ELECTRONIC SHUTOFF VALVE LEAKING. REPLACED SAME.

Part: ENGINE — FAILED (NR 1)

LEFT ENGINE FAILED AT 6,000 FT. CLIMBOUT EGT REACHED 1,100, LITE ENGINE VIBRATION FELT FOLLOWED BY EGT SPIKE. REPLACED ENGINE.

Part: SWITCH — DIRTY (LT MLG DOOR)

ON T/O, THE AMBER GEAR DOOR LIGHT REMAINED ILLUM FOR A UNUSUALLY LONG TIME AFTER GEAR RETRACT. ON APPROACH WITH GEAR EXTENDED AND THREE GREEN THE AMBER GEAR DOOR LIGHT REMAINED ILLUM THROUGH TOUCHDOWN. LIGHT EXTINGUISHED AFTER TOUCHDOWN. PERFORMED BITE OF PSEU LAST FLT FAULTED SW S260 AND S238 LT LOCK LATCH SYS. CHECKED SWITCHES, TARGETS AND WIRING ALL OK CYCLED GEAR DOORS SEVERAL TIMES, SYS OP AND INDICATION NML.

Part: SKIN — CRACKED (BS 1197-1221)

A CRACK WAS FOUND IN THE FUSELAGE SKIN NEAR AN EXISTING REPAIR. A SECTION OF SKIN PANEL IN THIS REGION WAS REMOVED AND A NEW ONE SPLICED IN BETWEEN STA 1197+77 AND 1197+124 AND BETWEEN STR 36L AND 36R.

Part: SKIN — TORN (BS 1197-1307)

THE FUSELAGE SKIN AT FS 1197+110 WAS BADLY DAMAGED BY AN IMPACT FROM GROUND EQUIPMENT. THE SKIN WAS CUTOUT BETWEEN STR 35R AND 39L RESULTING IN A 15.5 X 19.5 CUTOUT. THE DAMAGED SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PER ER/A 364390-14, REV A.

Part: BULB — FAILED (CABIN)

LT AFT OVERWING EMERGENCY LIGHT OUT. RELAMPED SAME, OPS CK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHTS BETWEEN SEATS 10 AND 13 BOTH SIDES ARE OUT. REPLACED EMERGENCY FLOOR TRACK LIGHTS POWER SUPPLY ASSY M9008, OPS CK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

LEFT WING SLIDE EMERGENCY ILLUMINATION LIGHTS AT STATION 1197, 1230 AND LEFT AFT DOOR EMERGENCY ILLUMINATION LIGHT INOP. REPLACED M738 POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD PER MM.

Part: SKIN — DENTED (NR 6 LE SLAT)

DURING SHOP VISIT, NR 6 L/E SLAT WEDGE WAS REPLACED DUE TO HAIL DAMAGE PER CMM 57-43-61.

Part: TE WEDGE — DENTED (NR 4 LE SLAT)

T/E WEDGE DENTED TOP SURFACE. INSTALLED WEDGE PER CMM 57-43-55, FOR NR 4 L/E SLAT AT SHOP INSPECTION.

Part: TE WEDGE — DENTED (RT LE SLAT)

DURING SHOP INSPECTION, RT WING L/E SLAT PANEL WAS FOUND WITH HAIL DAMAGE TO T/E WEDGE. REPLACED WEDGE PER MM 57-43-55.

Part: SKIN — DELAMINATED (LT TE FLAP)

LT WING O/B AFT FLAP T/E WEDGE HAS SEVERAL DELAMINATED AREAS UPPER SURFACE. MADE REPAIRS PER SRM 51-70-17 REF 57-53-01 AND COMPLY WITH ERA 270849-14. DAMAGE FROM HAIL.

Part: SKIN — DAMAGED (RT ELEV)

RT INBOARD ELEVATOR UPPER SURFACE DAMAGED BY HAIL. MADE BONDING REPAIRS. REPAIRED PER ERA 270806-14. DAMAGE FROM HAIL.

Part: SKIN — DENTED (NR 11 TE SLAT)

NR 11 SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61.

Part: SKIN — DENTED (RT AILERON)

DAMAGE FOUND DURING GROUND INSPECTION AFTER HAIL STORM IN DFW. DAMAGE WAS FOUND ON UPPER SURFACE O/B RT AILIRON IN VARIOUS AREAS. REPAIR WAS PERFORMED BY SRM 51-70-03 REF SRM 57-60-02.

Part: WEDGE — DENTED (NR 1 SLAT)

DURING INSPECITON NR 1 SLAT WEDGE WAS FOUND DENTED FROM HAIL. REPLACED WEDGE PER SRM 57-43-61.

Part: SKIN — DENTED (NR 3 LE SLAT)

SLAT T/E WEDGE HAIL DAMAGED. REPAIRED PER CMM 57-43-61, FOR NR 3 L/E SLAT DURING SHOP VISIT.

Part: TE WEDGE — DENTED (NR 2 LE FLAP)

NR 2 L/E SLAT FOUND TO HAVE DENTS APPARENTLY CAUSED BY HAIL. REPLACED TRAILING EDGE WEDGE AS PER CMM 57-43-61.

Part: SKIN — DENTED (NR 10 SPOILER)

UPON GROUND INSPECTION AT DFW AFTER HAIL STORM FOUND A DENT IN NUMBER 10 SPOILER ON THE UPPER SURFACE. REPAIRED PER SRM 57-70-01 REFERENCE TO SRM 51-70-17.

Part: SKIN — DENTED (NR 7 SPOILER)

UPON GROUND INSP, IN DFW AFTER HAIL STORM UPPER SURFACE WAS FOUND TO BE DENTED ON THE NR 7 SPOILER. REPAIRED PER SRM 51-70-17.

Part: SKIN — DENTED (NR 8 SPOILER)

RT WING UPPER SURFACE NR 8 SPOILER DENTED, REMOVED. REPAIRED PER B767 SRM 57-70-01 REF 51-70-17. DAMAGE FROM HAIL.

Part: SKIN — DENTED (RT TE FLAP)

RT WING I/B AFT FLAP UPPER SURFACE DENTED. REPAIRED TWO BONDED AREAS PER SRM 57-53-01 REF 51-70-10. FILLED AND SANDED ALL OTHER DENTS AND ALODINED PER 51-70-01. DAMAGE FROM HAIL.

Part: SKIN — DAMAGED (RT ELEV)

RT ELEVATOR UPPER SURFACE DAMAGED, OUTBOARD ELEVATOR. SEALED AND POTTED AREAS OF DAMAGE AS PER SRM 59-70-00. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL.

Part: SKIN — DAMAGED (RT ELEV)

RT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER ERA 270814-14 AND SRM 55-70-01. DAMAGE FROM HAIL.

Part: SKIN — DENTED (NR 6 SPOILER)

LT WING UPPER SURFACE OF NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL, REMOVED DAMAGE AND FABRICATED REPLACEMENT AS PER SRM 51070-17. REPAIRED PER 51-70-17. DAMAGE FROM HAIL.

Part: SKIN — DAMAGED (WING)

UPON GROUND INSPECTION DFW AFTER HAIL STORM, FOUND HOLES ON UPPER SURFACE OF NR 9 SPOILER. REPAIRED PER SRM 57-70-01 REF 51-17-17.

Part: SKIN — DAMAGED (RT ELEV)

RT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER SRM 55-70-01. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL.

Part: SKIN — DENTED (LT AILERON)

LT WING UPPER SURFACE OF I/B AILERON DENTED. REPAIRED AS PER SRM 57-60-01 REF 51-70-17. DAMAGE FROM HAIL.

Part: SKIN — DENTED (LT ELEV)

DURING GROUND INSPECTION, DAMAGE FOUND TO UPPER SURFACE OF LT I/B ELEVATOR. REPAIRD PER SRM 55-20-01 REF 51-70-17.

Part: SKIN — DENTED (NR 6 SPOILER)

LT WING UPPER SURFACE NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL. REMOVED DAMAGE AND FABRICATED REPLACEMENT CORE AS PER SRM 51-70-17. REPAIRED PER 51-70-17. DAMAGE FROM HAIL.

Part: SKIN — DENTED (NR 2 SPOILER)

LT WING UPPER SURFACE OF NR 2 SPOILER DENTED. REPAIRED PER SRM 57-70-01. DAMAGE FROM HAIL.

Part: SKIN — DENTED (RT AILERON)

DURING GROUND INSPECTION DAMAGE FOUND ON UPPER SURFACE OF RT I/B AILERON. REPAIRED PER SRM 57-60-01 REF 51-70-17.

Part: SKIN — DAMAGED (NR 9 LE SLAT)

DURING SHOP INSPECTION, NR 9 L/E SLAT T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE. REPAIRS ACCOMPLISHED PER SMR 57-43-55.

Part: SKIN — DENTED (NR 2 SPOILER)

DURING SHOP INSPECTION, NR 2 SPOILER HAD A DENT FROM HAIL DAMAGE AND WAS REPAIRED PER 57-70-01.

Part: TE WEDGE — DENTED (NR 8 LE FLAP)

RT WING NR 8 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED TRAILING EDGE WEDGE PER CMM 57-43-61.

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

NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED T/E WEDGE PER CMM 57-43-61.

Part: SKIN — DENTED (RT TE FLAP)

RT WING O/B AFT FLAP UPPER SURFACE DENTED. REPAIRED AS PER SRM 51-70-06. DAMAGE FROM HAIL.

Part: SKIN — DENTED (NR 5 SPOILER)

LT WING UPPER SURFACE NR 5 SPOILER DENTED. REMOVED AND REPAIRED PER SRM 51-70-17 REF FROM 57-70-01. DAMAGE FROM HAIL.

Part: TE WEDGE — DENTED (NR 7 LE SLAT)

RT WING NR 7 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61.

Part: COOLING FAN — MALFUNCTIONED (FWD CARGO)

JUST PRIOR TO DESCENT, HEAVY SMELL OF ELECTICAL WIRE HEATING. FOUND 6H21 EXHAUST FAN C/B OUT. SELECTED OVERIDE ON EQUIPMENT COOLING, AND SMELL WENT AWAY. FWD TO MCO AND PLACARD MEL 21-58-04B C/B COLLARD. REPLACED FWD EQUIPMENT COOLING FAN, OPERATION NORMAL.