N175DN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,135 hrs · 20,687 cycles

SHIP 175 DOOR 1L LIGHT INDICATOR MISSING AT 1 LEFT FLIGHT ATTENDANT PANEL. CORRECTIVE ACTION: R/R 1L LIGHT SW ON FWD FA PANEL IAW B767 AMM 33-13. DOOR 1L ARMED INDICATION OPS NML. ALSO INSTALLED LENS IAW B767 AIPC 52- 11. NO "M" PROC. MEL & PLACARD REMOVED. (4373696)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,135 hrs · 20,687 cycles

SHIP 175 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. CORRECTIVE ACTION: SECURED ASSY AS REQ'D (0069800)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 139,608 hrs · 20,584 cycles

SHIP 0175 -ATO- DUE TO RT GEN OFF INDICATION. CORRECTIVE ACTION: REPLACED IDG PER AMM 24-11. (4613393)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 139,227 hrs · 20,525 cycles

SHIP 0175 - ATB/IFSD - AIRCRAFT RETURNED TO PRG DUE TO RIGHT ENGINE FAILURE AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN THE TAIL PIPE. ENGINE CHANGE COMPLETED.(5156318)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 139,180 hrs · 20,516 cycles

SHIP 175 SEAT 35 BA EMERG EXIT LIGHT BELOW SEAT DETATCHED, CORRECTIVE ACTION: RESECURED OK FOR SERVICE (4432170)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,991 hrs · 20,322 cycles

SHIP 175 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:20A. CORRECTIVE ACTION: FOUND MISSING LENS AND INSTALLED. OK FOR SVC. (2769397)

Part: UNKNOWN — UNKNOWN · airframe 137,316 hrs · 20,201 cycles

SHIP 175 R2 DOOR HARD TO ARM. CORRECTIVE ACTION: EXERCSIED DOOR HANDLE AND CLEARED DOOR TRACK. OPS CHECK OK PER B767-300 AMM 52-73. OK FOR SVC (4110656)

Part: NONE — NONE · airframe 137,210 hrs · 20,187 cycles

SHIP 175 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. CORRECTIVE ACTION: RESECURED LIGHT ASSY CKS OK (2660003)

Part: NONE — NONE · airframe 137,210 hrs · 20,187 cycles

SHIP 175 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED, CORRECTIVE ACTION: RESECURED LIGHT ASSY CKS OK (2660006)

Part: NONE — NONE · airframe 137,161 hrs · 20,178 cycles

SHIP 175 CABIN CIELING EXIT SIGN MISSING. CORRECTIVE ACTION: FOUND MISSING EXIT SIGN, RESTOWED. (4187087)

Part: NONE — NONE · airframe 137,088 hrs · 20,164 cycles

SHIP 175 LIGHT DANGLING BELOW SEAT 33F. CORRECTIVE ACTION: RESECURED LIGHT HOUSING @ SEAT 33F PER B767 33-50 (4187053)

Part: NONE — NONE · airframe 137,025 hrs · 20,151 cycles

SHIP 175 HARD TO ARM DOOR 1R. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR ATTACHMENT POINTS. OPS OK PER B767 AMM 25-66. (4187018)

Part: NONE — NONE · airframe 137,025 hrs · 20,151 cycles

SHIP 175 1R DOOR COULD NOT ARM. CORRECTIVE ACTION: ARMED AND DISARMED 1 R SLIDE OPS CK NML PER B767 AMM 25-66. (4187012)

Part: NONE — NONE · airframe 137,025 hrs · 20,151 cycles

SHIP 175 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:602. CORRECTIVE ACTION: ARMED AND DISARMED 1R DOOR SLIDE PER B767 AMM 25-66. NO PROBLEM FOUND. OK FOR SVC. (2631948)

Part: NONE — NONE · airframe 136,957 hrs · 20,138 cycles

SHIP 175 R1 DOOR REQUIRES EXCESS FORCE TO ARM. CORRECTIVE ACTION: T/S PER B767-300 FIM 52-11-00-815-804. LUBRICATED R1 DOOR GIRT BAR CARRIER ASSY PER B767-300 AMM 12-21. OPS NORMAL. (9918682)

Part: NONE — NONE (DOOR) · airframe 136,733 hrs · 20,097 cycles

ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:602. OPS CHK 1R DOOR ARMING PER B767-200/300 AMM 52-73. OPS CHK NML.

Part: LIGHT — UNSECURE (SEAT 37F) · airframe 136,540 hrs · 20,059 cycles

SEAT MOUNTED EMERGENCY LIGHT SEAT 37F UNSECURE. SECURED THE EMERGENCY LIGHT, CHECKED OK.

Part: DOOR — OBSTRUCTED (R1) · airframe 136,418 hrs · 20,037 cycles

R1 DOOR WILL NOT ARM SLIDE. CLEARED OBSTRUCTION. DOOR OPS CHK GOOD IAW AMM 52-11. ACFT OK FOR SERVICE.

Part: NONE — NONE · airframe 135,290 hrs · 19,817 cycles

SHIP 175 FLOOR TRIM CREW REST EMERGENCY EXIT CAME OFF. CORRECTIVE ACTION: RESECURED AS REQ. OPS CHK NML. (9205528)

Part: NONE — NONE · airframe 135,280 hrs · 19,815 cycles

SHIP 175 -ATB/FUME- DUE TO BURNING ODOR IN THE CABIN. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. R/R MULTIPLE MLG TIRE WHEELS DUE TO BLOWN FUSE PLUGS. R/R TWO RMLG BRAKES. ONE AXLE REQUIRES LANDING GEAR SHOP SUPPORT. R/R LT RECIRC FAN AND FILTER. (8991883)

Part: NONE — NONE · airframe 135,250 hrs · 19,809 cycles

SHIP 175 L EXIT ROW SIGN MISSING, CORRECTIVE ACTION: REPLACED L EXIT ROW SIGN AS REQUIRED. (8991877)

Part: BATTERY PACK — INOPERATIVE · airframe 134,666 hrs · 19,694 cycles

SHIP 175 FOUND EMERGANCY LIGHTS INOP, CORRECTIVE ACTION: FOUND POWER PACK INOP. R/R POWER PACK PER B767 AMM 33-51. OPS CHK NORMAL (8370070)

Part: LENS — MISSING · airframe 134,547 hrs · 19,671 cycles

SHIP 175 MID CABIN OVHD EMER EXIT LIGHT LENS MISSING, CORRECTIVE ACTION: INSTALLED NEW EMER EXIT LIGHT LENS. CHECKS OK. PER B767-300AMM 33-50. (8370026)

Part: COVER — UNSECURE · airframe 134,455 hrs · 19,641 cycles

SHIP 175 EXIT SIGN AT 16D KEEPS FALLING OFF. CORRECTIVE ACTION: SECURED EXIT SIGN LENS COVER PER B767-300 AMM 33-51-01. (8798842)

Part: COVER — MISSING · airframe 134,433 hrs · 19,633 cycles

SHIP 175 PASSENGER EXIT SIGN COVER FELL OFF, CORRECTIVE ACTION: REATTACHED PASSENGER EXIT SIGN COVER IAW B767-300 AMM 3351. OPS CHK GD (8798828)

Part: NOT REPORTED — NOT REPORTED · airframe 134,151 hrs · 19,526 cycles

SHIP 175 R/H OVERWING SLIDE DOOR OPENING ACTUATORS OUT OF DATE. CORRECTIVE ACTION: R/R AFT RIGHT SLIDE DOOR OPENING ACTUATOR PER B767 W/C 2560-4232, R/R RH FWD OFF WING SLIDE DOOR OPEN ACTUATOR PER W/C 2560-4636. (2163987)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 , FWD CARGO DOOR CUT OUT OUTER CHORD FOUND CORROSION AT STA590,RBL40, CORRECTIVE ACTION: THE REWORKED AREA BLEND OUT REPAIR,COMPARED AND COMPLIED WITH ERA:596686-14. (2143254)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FWD CARGO DOOR CUTOUT BEAM FOUND CORROSION AT STA496, RBL40, CORRECTIVE ACTION: REPLACED DAMAGED SPLICE PER ERA 596823-14. (2143223)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND CABIN ABOVE MAIN LANDING GEAR AREA FRAME CORROSION AT STA977 LBL88.5, CORRECTIVE ACTION: PERFORMED SPLICE REPAIR AS PER PRI:596893. (2140961)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 ERA 596893-14 ISSUED FOR REPAIRS TO PN 145T1057-27 INNER CHORD AT STA 977, LBL 88.50, CORRECTIVE ACTION: AMOC REQUIRED FOR ALTERNATE INSPECTION DUE TO REPAIR AT OR BEFOR E 49999 TOTAL FLIGHT CYCLES, UPDATED MONITOR TITLE. (2140224)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 ERA 596893-14 ISSUED FOR REPAIRS TO PN 145T1057-27 INNER CHORD AT STA 977, LBL 88.50, CORRECTIVE ACTION: DTA DTE REQUIRED NO LATER THAN 36568 TOTAL FLIGHT CYCLES, UPDATED MONITOR TITLE. (2140222)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND RH NACELLE STRUT 426BR CUT OUT BOTH LOWER SIDE CRACK. CORRECTIVE ACTION: PERFORMED DOUBLER AND TRIPLER REPAIR AS PER PRI:271951-14 (2137175)

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 134,133 hrs · 19,522 cycles

ER/A 271951-14 REV E, DURING HCK AT STAG, CRACKING WAS FOUND ON THE #2 PYLON, RH SKIN AT NAC STA 156-172. CORECTIVE ACTION: PER ERA 271951-14 REV F, DTE ANALYSIS FOR THE SECTION III REPAIR COMPLETED. DAMAGE TOLERANCE ASSESSMENT HAS ESTABLISHED THAT THIS IS A CATEGORY A PERMANENT REPAIR, AND NO SPECIAL INSPECTIONS ARE REQUIRED.

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 ERA 596686-14 ISSUED FOR BLENDING TO FWD CARGO, OUTER CHORD BETW EEN STA 587-593. CORECTIVE ACTION: DTA DTE DUE NO LATER THAN 37499 TOTAL FLIGHT CYCLES. (2135368)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 ERA 596823-14 ISSUED FOR REPAIR TO FWD CARGO LOWER MAIN SILL SPL ICE, CORRECTIVE ACTION: AMOC TO AD 2014-14-04 REQUIRED NO LATER THAN 49999 TOTAL FLIGHT CYCLES. (2131515)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 ERA 596823-14 SECTION I ISSUED FOR REPAIR TO STA 472-616 FWD CAR GO, LOWER THRESHOLD INNER CHORD. CORRECTIVE ACTION: DTA DTE IS REQUIRED AT OR BEFORE 37499 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 00-596823 (2131499)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 AFT CARGO FLOOR FRAME ANCHOR NUT AREA FOUND CORROSION AT STA1153 RBL39. CORRECTIVE ACTION: PERFORMED SPLICE REPAIR AS PER PRI:596751-14 (2128840)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 BULK CARGO INNER SKIN FOUND CORROSION AT STA1543 BETWEEN S39R AND S39L, CORRECTIVE ACTION: DAMAGE AREA REPAIR AS PER PRI:596985. (2128498)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND CORRSION ON SEAT TRACK RBL88.5 BETWEEN STA1363 AND STA1373, CORRECTIVE ACTION: THE REWORKED AREA BLEND OUT REPAIR AS PER PRI:596787. (2128491)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 LOWER FUSELAGE SKIN AT AFT VACUUM BLOWER OUTLET PORT FOUND WITH CORROSION, CORRECTIVE ACTION: REPAIR AS PER B767-300 SRM53-60- 01-2R, TO C/O INSPECTION 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 6000 FLIGHT CYCLES. (2125940)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND CABIN FLOOR STRUCTURE CORROSION AT STA347 RBL33- RBL42.5, CORRECTIVE ACTION: THE REWORKED AREA BLEND OUT REPAIR AS PER PRI:596917-14. (2128564)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1543, S39L-39R. CORRECTIVE ACTION: ER/A REVISION IS REQUIRED PRIOR TO 37,500 TOTAL FLIGHT CYCLES IN ORDER TO ENSURE THIRD STAGE APPROVAL IS RECEIVED. (2125145)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540,BETWEEN S39L AND S39R, CORRECTIVE ACTION: PERFORMED REPAIR AS PER B767-300 SRM 53-00-07 & 51-40-02. (2124622)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1285,BETWEEN S39R AND S39L. CORRECTIVE ACTION: PERFORMED REPAIR AS PER B767-300 SRM 53-00-07 & 51-40-02. (2123602)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540,BETWEEN S38R AND S39R. CORRECTIVE ACTION: PERFORMED REPAIR AS PER B767-300 SRM 53-00-07 & 51-40-02. (2123626)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540,BETWEEN S36R AND S37R. CORRECTIVE ACTION: PERFORMED REPAIR AS PER B767-300 SRM 53-00-07 & 51-40-02. (2123639)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1307,BETWEEN S35L AND S36L. CORRECTIVE ACTION: PERFORMED REPAIR AS PER B767-300 SRM 53-00-07 & 51-40-02. (2123613)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1285,BETWEEN S36L AND S37L. CORRECTIVE ACTION: PERFORMED REPAIR AS PER B767-300 SRM 53-00-07 & 51-40-02. (2123596)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND PAX CABIN SEAT TRACK CORROSION AT STA346-STA434 LBL58. CORRECTIVE ACTION: REPAIRED AS PER B767-300 SRM 53-00-52 & 51-40-02 (2120204)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND SEAT TRACK CORROSION AT STA346-STA368 LBL11, CORRECTIVE ACTION: REPAIR AS PER B767-300 SRM 51-40-02 & 53-00-52. (2120243)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND PAX CABIN SEAT TRACK CORROSION AT STA346-STA434 RBL58.5, CORRECTIVE ACTION: REPAIR AS PER B767-300 SRM 51-40-02 & 53-00-52. (2120208)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FWD CARGO STRINGER FOUND CORROSION AT STA748 S34R, CORRECTIVE ACTION: PERFORMED SPLICE REPAIR AS PER B767-300 SRM53-00-03 (2120122)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 THS CTR BOX UPPER SURFACE FOUND CORROSION AT THS S3 RIB 1L-RIB 2L, CORRECTIVE ACTION: REPAIR AS PER B767-300 SRM 55-10-01 (2117829)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND A CRACK AT THE 3RD FASTENER FROM THE TOP OF THE INSPECTION AREA ON THE BS1725 BULKHEAD OUTER CHORD STRAP AT STR-7R, CORRECTIVE ACTION: DAMAGE AREA REPAIRED AS PER B767-300 SRM53-80-01 -2R REPAIR 5 (2117874)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND EXISTING REPAIR DOUBLER OBSTRUCT THE HFEC SURFACE INSPECTION OF RH LOWER WING SKIN AROUND THE FASTENERS AT STRINGER L-6.5 BETWEEN RIB 31-RIB 32, CORRECTIVE ACTION: REF TO REVISED ER/A 584203-14AD REV A AND RAISED JOB 232 LOG #2097598 AND PERFORMED THE ER/A SECTION III INSPECTION. (2109715)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 SEAT TRACK-FOUND PAX CABIN SEAT TRACK CORROSION AT STA346-STA423 LBL54.75. CORRECTIVE ACTION: DAMAGE AREA REPLACED AS PER B767- 300 SRM51-40 (2116999)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 SEAT TRACK-FOUND PAX CABIN SEAT TRACK CORROSION AT STA346-STA423, CORRECTIVE ACTION: DAMAGE AREA REPLACED AS PER B767- 300 SRM51-40. (2116983)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 FOUND CORROSION ON SEAT TRACK RBL88.5 BETWEEN STA 1197+50 AND STA 1197+59, CORRECTIVE ACTION: REPAIRED FROM STA 1197+33 TO STA 1208,RBL88.5, CUT AT STA 1197+33 AND REPLACED AS PER B767-300 SRM53-00 (2112132)

Part: NONE — NONE · corrosion level 2 · airframe 134,133 hrs · 19,522 cycles

SHIP 175 MTC TASK-FOUND CABIN FLOOR STRUCTURE CORROSION AT STA325 RBL33 - RBL27. CORRECTIVE ACTION: REPAIR AS PER B767-300 SRM53-00. (2113088)

Part: NONE — NONE · airframe 134,133 hrs · 19,522 cycles

SHIP 175 ER/A 584203-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 175 IN THE RH WING SKIN AT STR L-6.5. FOLLOW ON ACTION IS REQUIRED FOR SECT. III INSPECTION. CORRECTIVE ACTION: ACCOMPLISH ER/A 584203-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR, FOLLOW ON ACTION IS REQUIRED. (2097598)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 132,311 hrs · 18,996 cycles

SHIP 175 DURING TEST MAINTENANCE FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY AND BATTERIES. SYSTEM OPERATION IS NORMAL. (LP 6820480)

Part: LENS — MISSING (PASS CABIN LIGHT) · airframe 132,175 hrs · 18,955 cycles

SHIP 175 - DURING SERVICE CHECK MAINTENANCE FOUND CEILING LIGHT LENSE ABOVE 5A MISSING AND INSTALLED NEW LENSE. SYSTEM OPERATION IS NORMAL.

Part: INDICATOR — ODOR (WX RADAR SYS) · airframe 132,147 hrs · 18,946 cycles

TCAS/RADAR DISPLAY WENT BLANK, 1 MINUTE LATER THERE WAS A STRONG ELECTRICAL BURNING SMELL. TURN DISPLAY OFF AND PULLED TCAS PLUS RADAR C/B,S. ODOR DISSAPATED, FAINT ELECTRICAL BURN SMELL FROM WEATHER RADAR INDICATOR. NO OTHER FAULTS NOTED. CORRECTIVE ACTION: REPLACED WEATHER INDICATOR AS PRECAUTION AND WEATHER TRANSCEIVER. SYSTEM OPERATION IS NORMAL. MCO/PLAC REMOVED.

Part: SKIN — WORN (TE FLAP) · airframe 130,741 hrs · 18,668 cycles

R/H WING I/B AFT FLAP HAS WORN AREA AT UPPER SURFACE AT I/B END OF FLAP. REPAIRED PER SRM 51-70-10. (LP 1436471)

Part: SKIN — CRACKED (NOT REPORTED) · airframe 136,733 hrs · 20,097 cycles

DURING INSPECTION PER WC 5724-01010-41B, EM 5724-01010, AD 2018- 11-14, A CRACK WAS FOUND IN HOLE NO. 1 & 2. THE CRACKS WERE REPAIRED PER ER/A 584203-14AD PER AN AMOC FROM BOEING. THE AMOC REQUIRES REPETITIVE INSPECTIONS. ER/A 584203-14AD REVISED TO REV. B. ACCOMPLISH ER/A 584203-14AD REV B SECTION II INSPECTIONS. STATE INSPECTION RESULTS ON THIS LOGPAGE.

Part: SKIN — CRACKED (RT WING) · airframe 130,741 hrs · 18,668 cycles

CRACK INDICATION NOTED AT HOLE NUMBER 1 ON RH WING LWR SKIN STRINGER L 6.5 INDICATION IS LOCATED AT APPROXIMATELY THE 6 O CLOCK. C/W ERA 584203-14 (LP 1437522)

Part: WEDGE — DENTED (LE SLAT) · airframe 130,741 hrs · 18,668 cycles

R/H WING #7 SLAT T/E WEDGE UPPER SURFACE HAS DENTED AREA 41 INSCHES FROM I/B END OF SLAT. REPAIRED PER SRM 57-43-02 (LP 1434018)

Part: SKIN — DEBONDED (LE SLAT) · airframe 130,741 hrs · 18,668 cycles

#11 SLAT UPPER SURFACE, OUTBOARD EDGE HAS A DISBONDED PREVIOUS REPAIR. REPAIRED PER SRM 57-43-02. (LP 1434040)

Part: SKIN — DEBONDED (LE SLAT) · airframe 130,741 hrs · 18,668 cycles

#12 SLAT UPPER SURFACE INBOARD EDGE HAS A DISBONDED PREVIOUS REPAIR. C/W SRM 57-43-02 (LP 1434031)

Part: LIGHT — SHORTED (ROWS 1-5) · airframe 130,698 hrs · 18,659 cycles

EMERGENCY PATH LIGHTS ROWS 1-5 INOPERATIVE ON LEFT SIDE. FOUND FORWARD LGITH ASSEMBLY AT SEAT 5 SHORTED AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 130,615 hrs · 18,640 cycles

DURING SERVICE CHECK FOUND SEATS 1A-5A EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED PACK CHARGER M9008. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 130,070 hrs · 18,542 cycles

FOUND BOTTOM EMERG LIGHTS FROM ROWS 1 TO 5 LT SIDE INOP. REPLACED EMERG BATTERY CHARGER/ PWR SUPPLY PER B767-300 AMM 33- 51.

Part: BULKHEAD — CRACKED (BS 1809) · airframe 126,139 hrs · 18,028 cycles

HFEC INSPECTION FOUND CRACK INDICATION ON STA 1809 BULKHEAD, RIGHT FORWARD OUTER CHORD STRINGER TR, APPROX 1/2" IN LENGTH AS MARKED. AREA REPAIRED PER SRM 53-80-08. (LP 852451)

Part: OVEN — SMOKE (GALLEY) · airframe 125,118 hrs · 17,888 cycles

SMOKE EMANATED FROM AFT GALLEY OVEN 1 AND 3 SMOKE DETECTOR IN AFT CREW REST WENT OFF, WARNING LIGHT ON OVERHEAD PANEL ILLUMINATED "AFT CR SMK DETCR" MASTER WARNING AND FIRE BELL. REPLACED NR 1 AND NR 3 OVENS AS PRECAUTION.

Part: SKIN — DAMAGED (BS 957) · corrosion level 2 · airframe 122,293 hrs · 17,521 cycles

AFTER REMOVAL OF LEVELING COMPOUND AT AFT LEFT SIDE OF PICKLE FORK AREA AT BS 957, DAMAGE WAS FOUND ON UNDERLYING STRUCTURE AT SEVERAL LOCATIONS. COMPLIED WITH ERA 565898-14.

Part: FRAME — CORRODED (BS 1562) · airframe 122,293 hrs · 17,521 cycles

FRAME BS 1562, CORRODED. DRAIN PATH HOLE, CORRODED AT 6:00 ON FRAME. COMPLIED WITH ERA 565949-14.

Part: TANK — CORRODED (BS 957) · corrosion level 2 · airframe 122,293 hrs · 17,521 cycles

CENTER TANK UPPER SKIN HAS CORROSION AT BS 957 FORWARD OF RT PICKLE FORK FITTING. REPAIRED.

Part: OVEN — ODOR (GALLEY) · airframe 119,805 hrs · 17,202 cycles

FA REPORTED STRONG ELECTRICAL ODOR FROM FWD GALLEY IAW QRH PROCEDURE, TURNED OFF UTILITY BUSSES AND ODOR DISAPATED. REPLACED THE OVEN ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (BS 1629-1654) · airframe 119,454 hrs · 17,157 cycles

DURING A PDC INSPECTION, FOUND THREE CRACKS IN THE SKIN, 1 INCH, AT BS 1629 - 1654, STRINGER 14. COMPLIED WITH ERA 559952-14 AND SRM 53-00-01.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 116,383 hrs · 16,777 cycles

ON SERVICE CHECK, FOUND SEAT 6-9D EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FUSE ON THE POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 1A) · airframe 116,264 hrs · 16,764 cycles

INTERNAL EMERGENCY LIGHTS AT SEAT 1A ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 116,264 hrs · 16,764 cycles

INTERNAL EMERGENCY LIGHTS AT SEATS 6D-9D ARE INOPERATIVE. MAINTENANCE FOUND A FUSE BLOWN IN POWER PACK M9011 AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 116,264 hrs · 16,764 cycles

EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE LAMPS. SYSTEM OPERATION IS NORMAL.

Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 112,627 hrs · 16,288 cycles

WING CENTER SECTION REAR SPAR UPPER CHORD BL 0 AT WS 955 FOUND CORROSION. REPAIRED IAW ERA 534292-14.

Part: FRAME — CRACKED (BS 903) · airframe 112,627 hrs · 16,288 cycles

HFEC INSPECTION FOUND 01EA CRACK ON RT 903.5 FRAME INNER CHORD TRANSITION RADIUS AND REPAIRED.

Part: FRAME — CRACKED (BS 903) · airframe 112,627 hrs · 16,288 cycles

HFEC INSPECTION FOUND 01 EA CRACK ON LT BS 903.5 FRAME INNER CHORD TRANSION RADIUS AND REPAIRED.

Part: STRINGER — CORRODED (BS 1540-1562) · corrosion level 2 · airframe 112,627 hrs · 16,288 cycles

AFT CARGO COMPARTMENT STRINGER AT BS 1540 TO BS 1562, S38L FOUND CORROSION. REPAIRED IAW SRM 53-00-03.

Part: STRINGER — CORRODED (BS 654) · corrosion level 2 · airframe 112,627 hrs · 16,288 cycles

FWD CARGO COMPARTMENT AT BS 654+22, S39L. FOUND STRINGER CORROSION. REPAIRED IAW SRM 53-00-03.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 112,627 hrs · 16,288 cycles

LEFT OTBD FLAP UPPER SURFACE INBD SIDE FOUND CRACKED. REPAIRED IAW SRM 57-53-01.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 112,627 hrs · 16,288 cycles

FOUND TWO DENTS ON THE LOWER INBD SURFACE OF THE RT WING OTBD FLAP. SURFACED REPAIRED IAW 57-53-01 & SRM 51-70-17.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 112,627 hrs · 16,288 cycles

FOUND LT WING OTBD FLAP LOWER CENTER SURFACE HAD A DENT. REPAIRED IAW SRM 57-53-01.

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 112,627 hrs · 16,288 cycles

AFT CARGO COMPARTMENT AT BS 1219, S37L TO S38L FOUND SHEAR TIE CORROSION. REPLACED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 112,627 hrs · 16,288 cycles

LEFT INBD MAIN FLAP OTBD SIDE LOWER SURFACE FOUND DENTED. REPAIRED IAW SRM 51-70-10 & 51-70-03.

Part: FRAME — CORRODED (BS 1348) · corrosion level 2 · airframe 112,627 hrs · 16,288 cycles

FOUND CORROSION-AFT CABIN RT FRAME AT BS 1348 BETWEEN S18R AND S20R FOUND CORROSION. REFER TO CPCP TASK 53-252-01L, OUT OF LIMITS IAW SRM 53-00-15. REPAIRED IAW ERA 534299-14.

Part: STRUCTURE — CRACKED · airframe 112,627 hrs · 16,288 cycles

THE RT FORWARD OUT CHORD CRACK AREA REPAIRED IAW SRM 53-80-08, REPAIR 9.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 112,594 hrs · 16,284 cycles

EMERGENCY LIGHT AT SEAT 21AC RED AND WHITE ARE INOPERATIVE. MAINTENANCE REPLACED SIDEWALL DISCONNECT MATE CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: FAILSAFE — CRACKED (BS 955) · airframe 103,233 hrs · 15,131 cycles

BS 955, RT FAILSAFE STRAP CRACKED, REPAIR CARRIED OUT WITH ERA 519778-14.

Part: STRUCTURE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 103,233 hrs · 15,131 cycles

RIGHT MLG WHEEL WELL FWD BS 955 CORRODED. REPAIR CARRIED OUT IAW ERA 19789-14AD.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 103,102 hrs · 15,113 cycles

BURNING ODOR IN THE CABIN, LOCATED AT SEAT 18A. MX FOUND INDIRECT CEILING LIGHT BALLAST WITH BURNED FUSE AND REPLACED SAME. SYSTEM CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 102,484 hrs · 15,035 cycles

EMERGENCY LIGHT 23ABFG ARE INOPERATIVE. REPLACED BATTERY POWER SUPPLY AND BATTERY PACKS. SYS OPS IS NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,614 hrs · 14,803 cycles

EMERGENCY LIGHTS AT SEAT 23AB ARE INOPERATIVE. MX REPLACED THE UNDERSEAT CONNECTOR. SYS OPERATION IS NORMAL.

Part: FLEX HOSE — UNKNOWN (COCKPIT OXYGEN) · airframe 97,299 hrs · 14,343 cycles

CREW OXYGEN SYSTEM HAS LOW PRESSURE, FLEX HOSE REPAIRED IAW EA 01-074935-03.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 96,161 hrs · 14,181 cycles

CABIN CREW REPORTS SEVERAL FWD CABIN LIGHTS WENT OUT ELECTRICAL SMELL IN CABIN. FOUND BAD BALLAST D02690 M00671. REPLACED BALLAST P/N 05814-16 PER AMM B767-300 33-21. PVHD PNL RE-INSTALLED FWD CABIN OVHD LIGHTS, OP NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: WIRE — DAMAGED (CABIN) · airframe 94,074 hrs · 13,909 cycles

EMERGENCY ESCAPE PATH LIGHTS AT 19AB ARE INOPERATIVE. MAINTENANCE REPAIRED WIRING. SYSTEM OPERATION IS NORMAL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 93,184 hrs · 13,798 cycles

EMERGENCY LIGHTS AT SEATS 21-31 AF/FG ARE INOPERATIVE. MAINTENANCE FOUND EEP LIGHTS HARNESS BAD AT SEAT 29AB AND REPLACED IT. SYSTEM OPERATION IS NOW NORMAL.

Part: FLOORBEAM — CORRODED (BS 286) · airframe 91,892 hrs · 13,615 cycles

CABIN FLOORBEAM STRUCTURE (EXISTING UPPER FLANGE REPAIRED T-CHORD) AT STA 286, RBL 71-74 FOUND CORRODED. CABIN FLOORBEAM STRUCTURE AT STA 286, RBL 44.5-83.5. PREVIOUS REPAIRED T-CHORD FOUND CORROSION EXCEEDED LIMITS IAW SRM 53-00-51, FIG 101 (OTIS). CORRODED T-CHORD REMOVED , NEW T-CHORD FABRICATED AND INSTALLED IAW SRM 53-00-51, FIG 201, REPAIR 1. (OTIS)

Part: SKIN — CRACKED (LT WING) · airframe 91,892 hrs · 13,615 cycles

HFEC OPEN HOLE INSP CARRIED OUT AND FOUND CRACK INDICATION ON LT WING PYLON SIDE LOAD FITTING MOST INBD HOLE WITH CRACK INDICATION ON WING SKIN TOP SURFACE AT APPROX 2 O'CLOCK BY PLAIN VIEW AS MARKED. REPAIR ON 01 EA HOLE ACCOMPLISHED IAW PRI 487833-14 AD, REV 2, DATED 01/04/11.

Part: SILL — CORRODED (BS 566.48-571.52) · airframe 91,892 hrs · 13,615 cycles

FWD CARGO-LOWER SILL STRUCTURE, INNER CHORD FAILSAFE STRAP AT NR3 ROLLOUT STOP MOUNT BOLT LOCATION CORRODED. FWD CARGO DOOR LOWER SILL CORROSION ON LOWER SURFACE OF THE FAILSAFE STRAP LOCATED BETWN STA 566.48 - STA 571.52, CORROSION REMOVED IAW SRM 511002, FOUND EXCEEDED LIMIT IAW SRM 53-00-15. REPAIR ACCOMPLISHED IAW PRI 487847-14 REV 0.

Part: FITTING — DAMAGED (LT WING) · airframe 91,892 hrs · 13,615 cycles

LT WING INBD MIDSPAR UNDERWING FITTING INBD HOLE FOUND DIAMENTER SIZE = 0.902" WHICH IS GREATER THAN 0.8750"-0.8770". REPAIR CARRIED OUT IAW PRI 487833-14AD, REV.2, DATED 01/04/11.

Part: SILL — CORRODED (FUSELAGE) · airframe 91,892 hrs · 13,615 cycles

FWD CGO-DOOR CUTOUT, NR3 ROLLOUT STOP MOUNTING STRUCTURE, INTERNAL SIDE FOUND CORRODED. FWD CARGO-DOOR CUTOUT, NR3 ROLLOUT STO STRUCTURE, LOWER SILL CHORD BLENDOUT ACCOMPLISHED IAW SRM 51-10-02 OTIS AND FOUND EXCEEDED LIMIT.

Part: SPAR — CRACKED (NR2 ENGINE STRUT) · airframe 91,892 hrs · 13,615 cycles

ONE HOLE CRACK FOUND DURING HFEC INSP ON NR2 ENGINE STRUT MIDSPAR WEB LT SIDE CLOSE TO AFT BULKHEAD WITH LENGTH OF APPROX. .2500" LONG AS MARKED. REPAIR ON 01 EA HOLE ACCOMPLISHED IAW PRI 487826-14 REV 1, DATED 12/03/10.

Part: SPAR — DAMAGED (NR 1 STRUT) · airframe 91,892 hrs · 13,615 cycles

DURING ACCOMPLISHMENT OF EA01-074965-03, AD OPN 0306 WITH REF SB767-54-0080, FIG 10, FOUND NR 1 STRUT UPPER SPAR WEB, PN 311T4100-55, HAS EXISTING REPAIR DOUBLER INTERFERE WITH NEW STIFFENER 311T3040-11 AND RING DOUBLER 311T3040-13. IN ADDITION FOUND WEB HAS 02EA ELONGATED HOLES. WEB REPAIR ACCOMPLISHED IAW PRI 81632 REV.0, DATED 12/30/10.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 91,892 hrs · 13,615 cycles

LT WING NR 6 SLAT OTBD UPPER SURFACE FOUND DENTED AS MARKED. DENTED UPPER SURFACE REPAIRED PERMANENT IAW SRM 57-43-01, FIG 201.

Part: SKIN — CRACKED (BS 654 S1R) · airframe 91,892 hrs · 13,615 cycles

DURING HFEC INSP ON UPPER VHF ANTENNA MOUNTING AREA EXT SKIN BETWN BS 654+22 TO BS 654+44 AND STR 01R, 02 EA CRACK INDICATION FOUND 0.4" LONG AND CRACK ENDS MARKED OUT. REPAIR ACCOMPLISHED.

Part: SILL — CORRODED (FUSELAGE) · airframe 91,892 hrs · 13,615 cycles

FWD CARGO-DOOR CUTOUT, NR4 ROLLOUT STOP MOUNTING STRUCTURE, INTERNAL SIDE FOUND CORRODED. FWD CARGO-DOOR CUTOUT, NR4 ROLLOUT STOP STRUCTURE, LOWER SILL CHORD BLENDOUT ACCOMPLISHED IAW SRM 51-10-02 AND FOUND EXCEEDED LIMIT IAW SRM 53-00-15 , REPAIR ACCOMPLISHED IAW PRI 487832-14, REV 0.

Part: FAILSAFE — CRACKED (BS 955) · airframe 91,892 hrs · 13,615 cycles

CRACK INDICATION FOUND DURING ULTRASONIC INSP ON LT BS 955 FAILSAFE STRAP AT FWD SIDE OF THE BOLT HOLE. FAILSAFE STRAP REPAIRED IAW SB 767-53A0100, FIG 15, REV 2.

Part: FAILSAFE — CRACKED (BS 955) · airframe 91,892 hrs · 13,615 cycles

CRACK INDICATION FOUND DURING ULTRASONIC INSP ON LT SIDE STA 955, FAILSAFE STRAP AT FWD SIDE OF BOLT HOLE. FAILSAFE STRAP REPAIRED IAW BS B767-53A100, REV 2, FIG 15 IAW ERA 487824-14AD.

Part: RESISTOR — FAILED (BPCU) · airframe 90,803 hrs · 13,469 cycles

ON TAXI OUT LT ENG GEN WOULD NOT PICK UP RT BUSS WHEN APU WAS SHUTDOWN FOR CROSSBLEED START. BITE CHECK OF BPCU FAULTED AUX CONTACTS/BPCU/GCU. ORDERED L C/B IAW FIM. REPLACED R531 IN P34 IAW WDM. PWR CKS GOOD MM. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: ENGINE — FAILED (APU) · airframe 90,767 hrs · 13,464 cycles

WHILE AT GATE APU SHUTOFF. PFMD BITE TEST OF APU SHOWS OVERSPEED SHUTDOWN. PFMD VISUAL INSP OF APU FOUND SENSOR TS8 DISCONNECTED AND FULL OF OIL AND APU HAS ZERO OIL QTY. REMOVED AND REPLACED APU.

Part: CONTROL PANEL — INTERMITTENT (COCKPIT) · airframe 90,551 hrs · 13,436 cycles

WITH LEFT GEN RUNNING RT AC BUS OFF MSG. REPLACED BPCU SINCE FAULTED, NO HELP. T/S PER FIM REMOVED AND REPLACED APU BTB, NO HELP. FURTHER T/S SHOWED THE STBY PWR PANEL INTERMITTENT. REMOVED AND REPLACED STBY PWR PNL. RAN LT ENGINE, CHECKS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: UNKNOWN — ODOR (CABIN) · airframe 88,926 hrs · 13,221 cycles

ON TAXI OUT, FLIGHT ATTENDANT NOTICED A RUBBER ODOR IN MID-CABIN. IN ADDITION, PARKING BRAKE HANDLE HAS DIFFICULTY RELEASING IT TOOK EXCESSIVE POWER TO INITIATE TAXI. FINALLY RECEIVED AN ANTISKID/AUTOBRAKES STATUS MESSAGE. ON ACFT ARRIVAL ALL MLG TEMP SENSORS HAD NML INDICATIONS. ALL ONES. PERFORMED BITE CHECK ON ANTISKID/AUTOBRAKE LRU AS PER FIM. NO MSGS NOTED. VISUALLY CONFIRMED BRAKES COMPRESSED AND RELEASED NORMALLY. RAN PACKS AND FANS NO ODOR NOTED. ALL TIRES AND BRAKES IN ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: CIRCUIT CARD — FAILED (L ENG SPEED) · airframe 88,688 hrs · 13,188 cycles

AFTER ENGINE START LT CTR FUEL PUMP LOW PRESSURE LIGHT. REMAINED ILLUMINATED. REPLACED ENGINE SPEED CARD.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 88,671 hrs · 13,185 cycles

FOUND AT PSV, THE NR 2 PYLON UPPER SPAR WEB CRACKED AT THE CUTOUTS FOR HYDRAULIC DRAIN AND SUPPLY LINES, AND THE PRESSURIZED FUEL LINE.

Part: BLADE — FAILED (NR 1 ENGINE) · airframe 88,012 hrs · 13,101 cycles

FAILED OP 50103 7TH STAGE BLADE INSPECTION. BLADE TEAR. ENGINE CHANGE IN PROGRESS.

Part: STARTER — MALFUNCTIONED (NR 2 ENGINE) · airframe 87,545 hrs · 13,043 cycles

ON TAXI OUT NR 2 ENG DURING START NO ROTATION. ATTEMPTED MANUAL START - NO HELP. REMOVED AND REPLACED NR 2 ENG STARTER PER M/M. CHECKS NORMAL.

Part: STARTER — DAMAGED (NR 1 ENGINE) · airframe 87,469 hrs · 13,033 cycles

ON FIRST START ATTEMPT ON LEFT ENGINE IT HUNG START AT ABOUT 48 PERCENT N2. SUBSEQUENT ATTEMPTS HAD NO N2 ROTATION AND A STARTER VALVE LIGHT AND L STARTER EICAS MESSAGE. REMOVED AND REPLACED NR 1 ENG STARTER PER AMM MFN 774860A4, FOUND STARTER/GEARBOX COUPLING SHEARED. REPLACED SAME PER M/M. STARTED ENG, ALL CHECKS NORMAL.

Part: A/C PACK — INOPERATIVE (LEFT) · airframe 87,016 hrs · 12,977 cycles

L PACK TEMP EICAS MESSAGE WITH LEFT PACK INOP LIGHT RESET PER QRH WITH SAME RESULT. NO AUTO EVEN GENERATED. BITE PACK CONTROLLER NO FAULTS OPENED PACK BAY AND INSPECTED AREA FOR DUCT LEAKS WHILE OPERATING PACK. PACKS OPERATE NORMAL COULD NOT REPRODUCE PROBLEM NO HISTORY.

Part: WARNING MESSAGE — ILLUMINATED (COCKPIT) · airframe 84,872 hrs · 12,721 cycles

MULTIPLE STATUS MSGS AND RT EEC ALTN LIGHT. FOUND C/B ON P6-3 PANEL 115 VAC RT XFR BUS PULLED. RESET BREAKER AND ALL MSGS CLEARED. RAN RT ENG AS PRECAUTIONARY. NO EEC MSGS.

Part: VALVE — OVERHEATED · airframe 83,851 hrs · 12,597 cycles

AFTER T/O AT JFK, AFT AND MID SMOKE DET WENT OFF, SMELL ALL OVER CABIN WAS NOTICED STRONG ENOUGH TO RETURN TO JFK. SMOKE AND FUMES REMOVAL AND ELEC SMOKE CKLIST RUN TO NO AVAIL. ELECTRICAL SYS TURNED OFF, NO EFFECT TAXIED TO GATE. INSP GALLEYS/CHILLERS-COFFEE MAKERS-OVENS-LAVS. REMOVED AFT AND FWD CARGO AFT BULKHEADS. INSP EXHAUST FANS, LAV WASTE VENT FANS-RECIRC FANS-GASPER FAN, NO PROBLEM FOUND. INSPECTED A/C BAYS, FOUND LEFT BAY MID ZONE TRIM VLV OVERHEATED. REMOVED AND REPLACED MID ZONE TRIM VLV. OPS CK OK. TAXIED A/C NO FAULT FOUND. PERF IFSDCK 1/2 ENGS. NO FAULT FOUND.

Part: PROCESSOR — INOPERATIVE (TCAS) · airframe 83,591 hrs · 12,565 cycles

TCAS INOP. REPLACED TCAS PROCESSOR. OPS CK GOOD. CK CB ALL OK.

Part: ANGLE — CRACKED (NACELLE) · airframe 82,518 hrs · 12,424 cycles

CRACKED CLOSEOUT ANGLE FOUND DURING AD 2005-19-23 INSPECTIONS. INSPECTED AND REPLACED ANGLE PER B/P.

Part: SKIN — DENTED (BS 179, LBL 28) · airframe 82,518 hrs · 12,424 cycles

FUSELAGE SKIN HAS A DENT AT STA 179, LBL 28. CUTOUT THE DAMAGED SKIN AN INSTALLED A REPAIR DOUBLER/TRIPLER.

Part: WHEEL — DAMAGED (MLG) · airframe 82,217 hrs · 12,387 cycles

RTB - ON TAXI SHORT OF RUNWAY, TOWER INFORMED OF POSSIBLE FLAT TIRE TAXIED CLEAR OF RUNWAY. INFORMED OF SMOKE FROM WHEEL WELL STOPPED A/C BRAKES INDICATIONS NORMAL INFORMED A/C HAVE TWO FLAT TIRES/C PERFORMED INSPECTION PER MM 05-51-16-201. FLAT TIRE LOSS MAINT PRACTICES CK OK. REPLACED NR 7 AND 8 WHEEL ASSY AND BRAKES.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 81,081 hrs · 12,250 cycles

LEFT ENG OIL LOSS IN 2 HOURS INDICATION WENT FROM 11 DOWN TO3. ABOUT 20 MINS LATER DROPPED TO 2. CHANGING THROTTLE SETTING AND EICAS COMPUTERS, NO HELP. RETURNING TO JFK. OPENED NR 1 ENG PRESSURIZED GEARBOX THROUGH BREATHER. FOUND LEAKING FROM IDG CARBON SEAL NEEDS NEW CARBON SEAL. REMOVED AND REPLACED IDG CARBON SEAL PER AMM. RAN ENG AT T/O PWR. PERFORMED ENG LEAK CK. NO LEAKS FOUND. IDG OPS OK. CHIP DETECTORS OK.

Part: ENGINE — MALFUNCTIONED (APU) · airframe 80,739 hrs · 12,212 cycles

APU SHUTDOWN DURING ENG START. RESTARTED APU ELECT OK. REPLACED APU ASSY PER AMM. OP AND LK CKS GOOD. REMOVED MCO/PLAC.

Part: CDU — FAILED (COCKPIT) · airframe 80,577 hrs · 12,193 cycles

RT FMC CDU WENT BLANK PRIOR TO TAKEOFF. RESET A COUPLE OF TIMES AND DID NOT FIX. REPLACED RT CDU. OPS NORMAL.

Part: BULKHEAD — LEAKING (FUSELAGE) · airframe 80,461 hrs · 12,177 cycles

ON APPROACH, HEARD A LOUD BANG FROM THE TAIL AREA WITH VIBRATIONS IN AIRFRAME AND YOKE. REQUIRED A/P DISCONNECT TO CORRECT AIRCRAFT PITCH. PERFORMED TESTS MCDP 1 8 9 65 68 69, NO INBOUND FAULTS NO TEST FAULTS 481481. PUMPED UP ELEV FEEL COMP BLED ELEV FEEL LINE PER MM 431329. INSP CABLES AND FOUND EVIDENCE OF WATER LEAK ON CABLES IN AREA OF LT P DOME FEED THRUS. CLEARED CLOGGED FLOOR DRAINS SEE ITEM 8 AND DISASSEMBLED/CLEAN FEED THRU AI SEALS REF SB 767-27AD192. LEAK AND OPS CK GOOD 930900.

Part: VALVE — UNSERVICEABLE (APU) · airframe 80,342 hrs · 12,163 cycles

A/C RTN TO STAND LOW AIR PRESS FROM APU ENG WOULD NOT START APU AIR SUPPLY INOP MCO/PLACARD, INSTALLED PER MEL 49-11-01C. FOUND SURGE BLEED VLV STUCK IN OPEN POSITION CHANGED SAME, OP NOW NORMAL.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 80,062 hrs · 12,125 cycles

EMERGENCY LIGHTS IN SEATS 23GH THRU 30GH INOP. TRIED SEVERAL NEW BULBS NO HELP, TRIED NEW BATTERY CHARGER NO HELP RE-INSTALLED ORIG. FOUND WIRE LOOSE AT SEAT 23GH SIDE PANEL LOOSE, RESECURED WIRE, EMERGENCY LIGHTS CK'S NORMAL.

Part: CIRCUIT CARD — UNKNOWN (ENGINE SPEED) · airframe 79,919 hrs · 12,109 cycles

AFTER STARTING, THE RIGHT CENTER PUMP PRESS LIGHT ILLUMINATED WITH THE RIGHT CTR PUMP ON. REMOVED AND REPLACED THE RT ENG SPEED CARD.

Part: ENGINE — FAILED (APU) · airframe 79,535 hrs · 12,065 cycles

THE APU FAILED TO START WHILE TAXIING IN AT BU. THE APU FAULT LIGHT ILLUMINATED. REPLACED APU AND APU ECU AS PER AMM RAN APU NO LEAKS NOTED. ECU SHOWS NML SHUTDOWN NO FAULTS NOTED.

Part: CIRCUIT BREAKER — FAILED (APU) · airframe 78,933 hrs · 11,984 cycles

DUE RT A/C BUSS FAILURE DURING TAXI. T/S PER SSM NTF. REMOVED AND REPLACED AUX POWER BREAKER C905 PER MM. NORMAL RT/LT APU BUSS ISOLATION OPS NORMAL.

Part: IDG — OVERSERVICED (NR 1 ENGINE) · airframe 78,553 hrs · 11,937 cycles

LT ENG DRIVE LT CAME ON INTERMITTENT FOR ABOUT 3 MINS THEN STEADY ON CLIMB-OUT DISCONNECTED GEN IAW QRA LT IDG OUT TEMP AND IDG RISE TEMP BOTH 178. FLT DECK IND T GEN DRIVE AND MTC MSG LT TEMP SENSOR. OPENED LT ENG SERVICED IDG DRAINED APPROX 2 PINTS OF OIL-RECONNECTED IDG PERF ENG RUN GEN FIELD RESET VOLTS/FREQ NML. REMOVED, CLEANED TEMP SENSOR C/PLUGS IND NML AND MTC MSG ERASED. OPENED RT ENG PRECAUTIONARY FOUND IDG OVER SERVICED APPROX 2 PINTS RETURNED A/C TO NML

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 78,018 hrs · 11,875 cycles

ON TAXI OUT, LT AFT FUEL PUMP PRESSURE LIGHT ON DISP APPROVED BUT RETURNED TO GATE TO REMOVE CARGO AND BOARDFUEL. RECYCLED PUMP AND C/B AND PRESS LIGHT OPS OK.

Part: BPCU — FAILED (E/E BAY) · airframe 76,580 hrs · 11,703 cycles

AFTER PUSHBACK STARTED ENGINES LOST GALLEY POWER. R/R BPCU RAN ENG ALL OPS NML.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 73,633 hrs · 11,331 cycles

LT HYD QUANTITY DROPPED TO 0.17. REPLACED CRACKED LINE.

Part: ENGINE — FAILED (NR 2) · airframe 73,575 hrs · 11,325 cycles

PASSING THRU 7K FEET ABOUT 4 MINS AFTER T/O, THE RIGHT ENG EXPERIENCED A VIOLENT SURGE WITH VIBRATIONS. THROTTLE PULLEDBACK TO IDLE AND EGT CONTINUED TO CLIMB. ENG SHUTDOWN WITH FUEL CUTOFF SWITCH. EGT REACHED 722 DEGS BEFORE SHUTDOWN AND N1 ROLLED BACK. MX FOUND METAL IN THE TAILPIPE. 4 TIRES BLOWN AFTER PULLING OFF THE RUNWAY.

Part: BATTERY — DISCHARGED (2L DOOR) · airframe 70,968 hrs · 10,976 cycles

FLIGHT ATTENDANT 2L DOOR FLASHLIGHT INOP. BATTERY LOW, REPLACED SAME.

Part: ODOR — DETECTED (A/C COMPARTMENT) · airframe 69,247 hrs · 10,735 cycles

AFTER APU STARTED ON THE GROUND BOTH PACKS WERE TURNED ON. AN OILY SMELL WAS EVIDENT IN THE COCKPIT. AFTER TAKEOFF THE SMOKE DETECTOR IN THE FWD MID CABIN LAV CAME ON AND THE SAME OILY SMELL WAS EVIDENT IN BOTH THE CABIN AND COCKPIT. OILY SMELL DISSIPATED AFTER APPROX 15 MIN OF FLT. RAN APU AND PACKS FOR 1 HR, NO OILY SMELL DETECTED.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 69,185 hrs · 10,727 cycles

WHILE PERFORMING ELEVATOR PCA BELLCRANK CHECK MX FOUND UPPER SURFACE OF LEFT INBD ELEVATOR WITH SLIGHT DAMAGE. REPAIRED PER SRM 55-20-01 AND 51-70-17.

Part: VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 67,374 hrs · 10,462 cycles

CLIMBING THROUGH 7000 FT HEARD THUMP FROM RT SIDE OF CABIN. CABIN RATE OF CLIMB WENT TO 2000 FT/MIN UP. COULD NOT CONTROL PRESSURIZATION. REPLACED EQUIPMENT COOLING EXHAUST VALVE.

Part: CONTROL PANEL — SMOKE (COCKPIT) · airframe 67,066 hrs · 10,420 cycles

AT PUSHBACK SMELLED SMOKE IN COCKPIT FROM OVERHEAD PANEL. FOUND ELECTRICAL ODOR COMING FROM YAW DAMPER/ANTI-SKID PANEL DAL P/N 311701432, S/N D00125. REPLACED PANEL.

Part: ENGINE — FAILED (NR 1) · airframe 66,362 hrs · 10,326 cycles

T/O ROLL 70 KNTS FELT STALL AND LOST OIL PRESS. EXAMINED TAILPIPE FOUND METAL N1 WON`T TURN. REPLACED ENGINE.

Part: ENGINE — MAKING METAL (NR 1) · airframe 61,962 hrs · 9,649 cycles

L OIL FILTER CAUTION AND STATUS MESSAGE CAME ON IN FLIGHT WHILE CRUISING AT FL350. REPLACED NR 1 ENGINE. FOUND MCD COVERED WITH BEARING METAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: LINE — LEAKING (LAVATORY) · airframe 58,610 hrs · 9,054 cycles

F/C LAV LEAKED WATER INTO E/E COMPARTMENT CAUSING DAMAGE TO ELECTRICAL COMPONENTS. REPAIRED LEAK.

Part: METERING VALVE — FAILED (LT MLG WW) · airframe 58,534 hrs · 9,041 cycles

AIRCRAFT RETURNED TO BLOCK DUE TO RIGHT HYDRAULIC SYSTEM PRESSURE LIGHT, QUANTITY LIGHT AND EICAS QUANTITY READING 0.03. IRREGULARITY OCCURRED ON RIGHT ENGINE START. FOUND LT WHEEL WELL BRAKE METERING VALVE FAILED. VALVE BODY END CAP SHEARED AWAY FROM COMPONENT. THREE OF FOUR ATTACHING FASTENERS FAILED. REPLACED VALVE, LEAK CKS GOOD.

Part: FAN — MALFUNCTIONED (LEFT) · airframe 55,594 hrs · 8,532 cycles

ODOR IN THE COCKPIT SMELLED LIKE HOT INSULATION, AT THE SAME TIME THE LEFT RECIRC FAN INOP LIGHT CAME ON WITH EICAS MSG. TURNED OFF LEFT RECIRC FAN AND SMELL WENT AWAY. T/S AS PER AMM FOUND LEFT RECIRC INOP AND RED RUBBER SEAL BETWEEN FILTER AND FAN DAMAGED. PARTS NIS MUC FWD TO MCO AS PER MEL 21-25-01A. PLACARD INSTALLED. C/B R14 PULLED AND SECURED.

Part: GENERATOR — FAILED (RT ENGINE) · airframe 52,027 hrs · 7,977 cycles

RT GENERATOR OFF LIGHT AND EICAS MESSAGE CAME ON AFTER T/O. STARTED APU AND GOT A GOOD ELEC FROM THE GENERATOR. REPLACED RT GEN PER M/M. OPS CHECK NORMAL.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 49,493 hrs · 7,543 cycles

WITH PWR ON ELECTRICAL ODOR COMING FROM COFFEEMAKERS IN FWD GALLEY. ODOR DISSIPATED WITH POWER OFF. FOUND HEAVY ACCUMULATION OF COFFEE RESIDUE. NO BURNT WIRES. REPLACED BOTH COFFEEMAKERS AS PRECAUTION. CK''D, NO SMELL OF BURNING.

Part: LIGHT — INOPERATIVE (ROW 37) · airframe 49,241 hrs · 7,500 cycles

SEAT MOUNTED PROXMITY ESCAPE PATH LIGHT INOP AT SEAT ROW 37FG. FOUND ILLUMINATOR CONNECTOR PIN PULLED LOOSE AT SEAT HARNESS. REMOVED AND REPLACED ILLUMINATOR ASSY. OPERATIONAL CHECK NOWOK.

Part: LIGHT — INOP (ROW 30FG)

SEAT MOUNTED PROXIMITY LIGHTS INOP AT SEAT ROW 30 F, G. REMOVED AND REPLACED LUMINATOR AT 30 F, G, LIGHT OPS CKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

JUMP SEAT AFT CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY PACK.

Part: SKIN — PUNCTURED (BS 618)

A SKIN PUNCTURE WAS FOUND AFT OF THE NR 1 CARGO DOOR AT FS 618 BETWEEN STR 29R AND 30R. THE SKIN WAS CRACKED APPROX 1.5 AND HAD A 3.5 GOUGE. THE DAMAGE CLEANUP RESULTED IN A 1.75 BY 2.75 CUTOUT IN THE FUS SKIN ONLY WITH THE REMAINING GOUGE BLENDED WITHIN SRM LIMITS. NO DAMAGE TO INTERNAL STRUCTURE. DOUBLER FROM 0.100 CLAD 2024-T3, TRIPLER FROM 0.063 CLAD 2024-T3.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

RT ENG COMPRESSOR STALL DURING REVERSE THRUST AT FAIRLY, HIGH RPM SLOWING THROUGH 70 KTS, NO ENGINE EXCEEDENCES. BORESCOPED NR 2 ENGINE, NO PROBLEMS DETECTED. RAN ENGINE, OPS CHECK GOOD.

Part: APU — FAILED (TAIL)

DURING GROUND OPERATIONS, APU AUTO SHUTDOWN DUE WITH TAILPIPE FIRE. INSPECTION REVEALED GEARBOX OIL IN TAILPIPE CAUSING FIRE. REPLACED APU.

Part: EEC SW PANEL — FAULTY (NR 2 ENGINE)

AFTER T/O, RT ENG EEC ALTN LIGHT CAME ON, EPR NORMAL NO EICAS MSG. REPLACED EEC SWITCH LIGHT PANEL, OPS CHECK OK.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

LEFT ENGINE COMPRESSOR STALL IMMEDIATELY AFTER T/O. MADE SUCCESSFUL LANDING WITH LEFT ENGINE AT IDLE. REPLACED ENGINE.

Part: WIRE — CHAFED (PAX SEAT)

WIRING FOR F/C SEAT 2-A AND OTHER SEATS ON CIRCUIT SHORTED AND BURNED THROUGH. PULLED ASSOCIATED CIRCUIT BREAKERS, P-36 AND P-37 IN E/E COMPARTMENT PER MTC CO-ORDINATOR. REPAIRED CHAFED WIRE. SYSTEM OPS CHECK GOOD.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE)

FLIGHT OUT OF FRA - RT IDG DRIVE LIGHT CAME ON STEADY. APU STARTED AND RT IDG DISCONNECTED. APPROXIMATELY 1 HR LATER - APU OIL QTY - EICAS STATUS MSG. APPROXIMATELY 45 MINUTES LATER - APU AUTO SHUTDOWN. FLIGHT DIVERTED TO SNN. REPLACED RT IDG.

Part: UPPER SPAR — CRACKED (NR 1 PYLON)

TWO CRACKS WERE FOUND IN THE NR 1 ENGINE PYLON UPPER SPAR WEB AT THE OUTBOARD DRAIN HOLE AT NAC STA 156 AND WL 149.21. THE CRACKS WERE STOP DRILLED AND REINFORCED WITH A FILLER AND DOUBLER PER DL ERA 273499-14, REV A.

Part: SKIN — CRACKED (NR 2 PYLON)

TWO CRACK LOCATIONS HAVE BEEN REPORTED IN THE NR 2 ENGINE PYLON OUT'BD STRUT SKIN. THE CRACKS START FROM THE FWD TORQUE BOX ACCESS HOLE. A 1 INCH CRACK IS IN THE UPPER FWD CORNER AT NAC STA 158. SECOND CRACK IS IN THE UPPER AFT CORNER AT NAC STA 192 AND IS 2 INCHES LONG. BOTH CRACKS EXTEND THROUGH BOTH SHEETS OF 0.080 PLUS 0.080 2024-T3 BONDED SKIN ASSEMBLY. THE AFT CRACK TERMINATES IN AN EXISTING FASTENER HOLE. ACCOMPLISHED REPAIRS PER DL ERA 271951-14 REV, D.

Part: ENGINE — MALFUNCTIONED (NR 2)

PERFORMED ENGINE STABILITY RUN, FOUND LOW STALL MARGIN. ENGINE WAS REMOVED AND ROUTED TO SHOP FOR COMPLETION OF EO SI-690053. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: FUEL PUMP — CRACKED (NR 1 ENG)

DIFFERENCE BETWEEN CALCULATED AND TOTALIZER FUEL GREW TO 4,000 LBS. CALCULATED WAS GREATER, NO FUEL LEAK OBSERVED DURING FLT. FOUND NR 1 ENGINE FUEL PUMP HOUSING CRACKED. REPLACED PUMP, OPERATION NORMAL.

Part: SKIN — CRACKED (NR 2 PYLON)

TWO CRACKS HAVE BEEN REPORTED IN THE NR 2 ENGINE PYLON O/B STRUT SKIN. THEY BOTH GO THROUGH BOTH SHEETS OF THE BONDED SKIN ASSEMBLY. REPAIRED PER DL ERA 271951-14.

Part: WIRE — BURNED (FWD CABIN)

DURING L/O CHECK, SMOKE WAS SEEN COMING FROM FORWARD CABIN AREA, GROUND POWER WAS IMMEDIATELY DISCONNCTED, FOUND THREE SHORTED WIRES INSIDE LEFT SEAT ATTACH TRACK AT SEAT LOCATIONS 1C AND 2C. SHORT CAUSED MINOR BURN DAMAGE TO AREA. REPAIRED SHORTED WIRING FOR SEAT FOOT REST MOTOR AND REPLACED ADJACENT DAMAGED CABLE ASSEMBLY.