N197DN

Part: WIRE — BROKEN (ZONE 200) · airframe 118,353 hrs · 17,688 cycles

SEAT MOUNTED WHITE EPATH LIGHT INOP AT 53 RIGHT. T/S PER B767 WDM 33-51-31, FOUND BROKEN WIRE AT 53G. REPAIRED AND SPLICED WIRE AS PER B767 SWPM 20-30, OPS CHECK OK. MEL AND PLACARD REMOVED. (8054695)

Part: SENSOR — OUT OF TOLERANCE (ZONE 800) · airframe 118,033 hrs · 17,633 cycles

1L DOOR INTERMITTENTLY SHOWS AS OPEN W/DOOR CLOSED AND ARMED ENTRY DOOR LIGHT ILLUMINATED IN COCKPIT. FOUND S194 "DOOR CLOSED SENSOR" OUT OF SPECIFICATION. ADDED TARGET SHIM, MEASUREMENT OF S194 NOW WITHIN LIMITS. ALL WORK DONE PER B767 AMM. 52-71. (8171956)

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 117,814 hrs · 17,589 cycles

L1 DOOR INDICATES OPEN UNTIL BOTH ENGS. ARE RUNNING. SLIDE LIGHT FLASHES UNTIL BOTH ENGS ARE RUNNING. R&R PROX BOX DUE TO HISTORY IAW B767-300 AMM 32-09-04. OPS CK GOOD, (7925528)

Part: SKIN — DAMAGED (ZONE 100) · airframe 115,566 hrs · 17,230 cycles

GROUND DAMAGE ON FUSELAGE BOTTOM AT APPROX STATION 412-420, BETWEEN STRINGERS LBL 537 AND RBL 537. REF NR LOG #0921831 FOR PRI COMPLIANCE ERA 625864-14 REV O. REPAIRED DAMAGE IAW PRI/ERA 625902-14 REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. VERIFIED PRI 625902-14 REV 1, 2, 3, 4, 5, 6, 7, 8, & 9 AND ERA 625902-14 REV A MATCH. RII COMPLETE (QC5284). ASSOCIATED ER/A 14-625902 ADDED FOR AC 0197. (LP #7148830)

Part: SKIN — DAMAGED (ZONE 100) · airframe 115,566 hrs · 17,230 cycles

FOUND SEVERAL HOLES OUT OF ROUND AND UNINSPECTABLE. 7 HOLES AT S-37L, 2 HOLES AT S-37R, AND 1 HOLE AT STA 421 ABOVE S-37R. MARKED. COMPLIED WITH E/RA 625902-14 REV A. PRI REVREV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625902-14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL - FUSELAGE / STA. 412 - 420 / 37L - 37R / GROUND DAMAGE - E/RA 625902-14 REV. A. SECTION I PERMANENT REPAIR INSTRUCTIONAL STEPS . COMPLIED WITH E/RA 625902-14 REV. A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625902-14 REV. A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REP AIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL - FUSELAGE STA 412 - 420 / 37L - 37R GROUND DAMAGE. E/RA 625902-14 REV A. SECTION I PERMANENT REPAIR INSTRUCTIONAL STEPS.

Part: SKIN — GROUND DAMAGE · airframe 115,566 hrs · 17,230 cycles

GROUND DAMAGE. COMPLIED WITH E/RA 625902-14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9 REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625902-14 REV A. PRI REV. 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9. REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL.

Part: SKIN — DAMAGED (ZONE 200) · airframe 115,566 hrs · 17,230 cycles

AT STR 37R STA 421 (MARKED). SUMMARY SEE NRC 003-0001:0520-8130/013 00013: COMPLIED WITH E/RA 625902-14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9, REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625902 -14 REV A. PRI REV 0, 1, 2, 3, 4, 5, 6, 7, 8, & 9 REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL. FUSELAGE STA 412 - 420 / 37L - 37R GROUND DAMAGE. E/RA 625902-14 REV A. SECTION I PERMANENT REPAIR INSTRUCTIONAL STEPS.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 115,546 hrs · 17,227 cycles

LEFT OVERWING FWD EMERGENCY EGRESS LIGHT IS INOPERATIVE. TROUBLE SHOT PER B767 WDM 33-51-21, SUSPECT BATTERY CHARGER M736 IS BAD. FWD TO MEL 33-51-02. PLACARD INSTALLED. DAYLIGHT FLIGHTS ONLY. MAINTENANCE REPLACED THE BATTERY CHARGER M376 PER B767 AMM 33-51-07. ALL LIGHTS IN CIRCUIT ILLUMINATE. PLACARD WAS REMOVED AND LOG PAGE WAS CLOSED. (LP #7148833)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 115,546 hrs · 17,227 cycles

L1 DOOR EMERGENCY GROUND ILLUMINATION LIGHT IS INOPERATIVE. REFER TO LOG #7148833, AS THIS LIGHT IS ALSO CONNECTED TO BATTERY CHARGER M736. FWD TO MEL 33-51-02. PLACARD INSTALLED. DAYLIGHT FLIGHTS ONLY. REFERENCE LOG 7148833 FOR CORRECTIVE ACTION. CLOSED LOG AND REMOVED PLACARD. (LP #7148840)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 115,546 hrs · 17,227 cycles

MULTIPLE EMERGENCY CEILING LIGHTS ARE INOPERATIVE FROM ROWS 36-42 RH SIDE. MAINTENANCE REPLACED THE BATTERY PACK M734 PER B767 AMM 33-51. OERATIONAL TEST STEP E, AFTER 90 MINUTE CHARGE, FAILED. REINSTALLED EMRGENCY BATTERY PACK AT M734. INSTALLED NEW BATTERY PACK AT M732. OERATIONAL TEST STILL FAILS. REPLACE BATTERY PACK M732 PER B767 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7148834)

Part: LATCH — OUT OF DATE (ZONE 200) · airframe 113,793 hrs · 16,902 cycles

SHIP 197 CHECK FOUND RH OFF WING SLIDE DOOR LATCH ACTUATOR MANUFACTURE DATE PAST DUE. CORRECTIVE ACTION: REMOVED AND REPLACED RH OFF WING SLIDE DOOR LATCH ACTUATOR AS PER B767-300 AMM 25-65-11 (0614706)

Part: SKIN — DELAMINATED (ZONE 300) · airframe 113,788 hrs · 16,901 cycles

SHIP 197 LH VERTICAL STABILIZER EXTERNAL SURFACE DELAMINATION FROM FUSELAGE 16 INCH AND FROM L/E 34INCH. CORRECTIVE ACTION: REPAIRED LH VERTICAL STABILIZER EXTERNAL SURFACE DELAMINATION FROM FUSELAGE 16 INCH AND FROM L/E 34 INCH AS PER PRI 621518-14. (0611758)

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 113,772 hrs · 16,898 cycles

SHIP 197 HFEC INSPECTION FOUND 01EA CRACK APPROX. 13MM IN LENGTH ON LH NOSE WHEEL WELL BULKHEAD CHORDS ABOVE WL159 AS MARK, AND THE CRACK DO NOT EXTEND BELOW WL159. CORRECTIVE ACTION: ACCOMPLISHED REPAIR REFER TO JOB CARD 5312-01165-0701. (0601245)

Part: DOOR — DENTED (ZONE 800) · airframe 113,772 hrs · 16,898 cycles

SHIP 197 FOUND BULK DOOR HAVE A DENT, "FROM THE LOWER EDGE 3" AND FROM THE FWD EDGE 5". CORRECTIVE ACTION: REMOVED THE PREVIOUS DOUBLER AS PER B767-300 SRM 51-40-02 REV .126.00-AUG-22-2024.RE-DID THE REPAIR AS PER ER/A 487030-14 REV B SECTION I. FOR THE FURTHER INSPECTION, REFER TO ER/A 487030-14 (0599856)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 113,462 hrs · 16,852 cycles

SHIP 197 1 EMERG LIGHT NOT WORKING ON SEAT 2A, CORRECTIVE ACTION: R/R OF LENS AND LAMPS IAW B767 AMM 33-51. OPS CHECK GOOD. MEL + PLACARD REMOVED. (6174997)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 113,531 hrs · 16,861 cycles

SHIP 197 1 EMERG LIGHT NOT WORKING ON SEAT 1D, CORRECTIVE ACTION: REMOVED AND REPLACED1D FWD ESCAPE PATH LIGHT ASSY. REF B767-300 CMM 25-25-09. OPS CHK GOOD. (6174996)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 113,010 hrs · 16,786 cycles

SHIP 197 UPON PDC FOUND 2L AND 2R EMERGENCY DOOR EXIT SIGNS NOT ILLUMINATED. CORRECTIVE ACTION: R/R BATTERY PACK PER B767-300 AMM 33-51. ALL OPS GOOD. A/C OK FOR SVC. (5708737)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 112,964 hrs · 16,780 cycles

SHIP 197 LOWER RUNNING EMERGENCY LIGHT OUT AT DOOR 1R. CORRECTIVE ACTION: R/R LIGHT ASSY, REF B767 AMM 33-52 (5708700)

Part: DOOR — UNKNOWN · airframe 112,964 hrs · 16,780 cycles

SHIP 197 FA'S ADVISED DOORS 2L AND 2R ARE HARD TO ARM. CORRECTIVE ACTION: OPS CHK 2L AND 2R SLIDE ARMING PER B767-300 AMM 52-73-00. CHKS NML NO DEFECTS FOUND (6076292)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 110,784 hrs · 16,437 cycles

SHIP 197 FOUND EMERGENC AISLE PATH LIGHTING ON SEAT 4D &. 5D INOP. CORRECTIVE ACTION: T/S PER B767 WDM 33-51-12, FOUND CONNECTOR D09J DISCONNECTED. RESECURED CONNECTOR, EMERGENCY LIGHTS AT 4D AND 5D OPERATE (5008374)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,509 hrs · 16,386 cycles

SHIP 197 F/A REPORTS 2R DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED 2R DOOR OPEN AND CLOSED AND ARMING. ALL OPS NML REF B767 AMM 52-11 & 52-73 (5032104)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,441 hrs · 16,231 cycles

SHIP 197 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101. CORRECTIVE ACTION: RE-SEATED SLIDE INDICATOR LIGHT AT SWITCH. OP'S NML. OK FOR SVC. (2962663)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,480 hrs · 16,236 cycles

SHIP 197 DURING PDC FOUND ON R/H BOTTOM OUTBOARD ACCESS LUBRICATION PANEL 621AJB MISSING. CORRECTIVE ACTION: REINSTALLED NEW PANEL AS PER B767-300 AMM 57-41. CDL REMOVED. OK FOR SVC. (4570612)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,083 hrs · 16,179 cycles

SHIP 197 REPAIR TO FRAME INNER CHORD AT STA 859.5 RBL 89, WL200. DTA COMPLETE. REQUIRES DTA SUPPLEMENTAL INSPECTIONS PER ERA 602721- 14AD REV A. CORRECTIVE ACTION: PER ERA 602721-14AD REV A, DTA COMPLETE. ACCOMPLISH SECTION II INSPECTIONS AT OR BEFORE 37,500 TOTAL AIRFRAME FLIGHT CYCLES. REPEAT SECTION II WITHIN EVERY 12,000 FLIGHT CYCLES THEREAFTER. (2922797)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,413 hrs · 15,942 cycles

SHIP 197 EXT EMERG LIGHT FWD OF AFT CARGO DOOR OUT. CORRECTIVE ACTION: R/R EMERG BATTERY CHARGER 00733 PER B767-300 AMM 33-51. OK FOR SVC. (9897376)

Part: NONE — NONE · airframe 106,791 hrs · 15,852 cycles

SHIP 197 RH OFF-WING SLIDE BOTTLE FAILED TO INFLATE. CORRECTIVE ACTION: ADJUSTED CABLE PER AMDS WORKCARD 2561-4723-RH. (2653981)

Part: NONE — NONE · airframe 106,760 hrs · 15,843 cycles

SHIP 0197 -DIV- DIVERSION TO PIK DUE TO RIGHT ENGINE VIBRATION FELT AT TAKEOFF FOLLOWED BY ERRATIC RIGHT ENGINE INDICATIONS. CORRECTIVE ACTION: MAINTENANCE CONFIRMED METAL IN TAIL PIPE. ENGINE CHANGE REQUIRED. MAINTENANCE IN PROGRESS. (A007992)

Part: NONE — NONE · airframe 106,760 hrs · 15,843 cycles

SHIP 0197 -DIV- DIVERSION TO PIK DUE TO RIGHT ENGINE VIBRATION FELT AT TAKEOFF FOLLOWED BY ERRATIC RIGHT ENGINE INDICATIONS. CORRECTIVE ACTION: MAINTENANCE CONFIRMED METAL IN TAIL PIPE. REPLACE ENGINE PER W/C 7210-40001-02. (9918880)

Part: NONE — NONE (NONE) · airframe 106,429 hrs · 15,781 cycles

L1 DOOR SLIDE INDICATOR LIGHT INOP OR DAMAGED. COULD NOT DUPLICATE FAULT ON GND. NO 90 DAY HISTORY. OK FOR SVC.

Part: SIGN — INOPERATIVE (CABIN) · airframe 106,266 hrs · 15,757 cycles

CREW REST SMALL RUNNING MAN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN ASSY. CKS GOOD REF AMM 33-51.

Part: INDICATOR — MALFUNCTIONED (ALTIMETER) · airframe 106,065 hrs · 15,723 cycles

-RVSM- SHIP 197 ALT DISAGREE EICAS MESSAGE AT FL320 CA AND FO ALTIMETERS OFF BY 200 FT. FO ALTIMETER WAS ERRATIC DURING FLIGHT, FO ALTIMETER SHOWED FL315 AND STBY 325. INSPECTED PITOT STATIC AND AOA VANES FOR DEFECTS. NONE FOUND. PERFORMED ADC L AND R TEST IAW AMM 34-12. TEST PASSED. BOTH ALTIMETERS FUNCTION NORMALLY.

Part: SIGN — INOPERATIVE · airframe 105,976 hrs · 15,711 cycles

SHIP 197 AT CREW REST FWD SMALL RUNNING MAN/ EXIT SING INOP. CORRECTIVE ACTION: REMOVED AND REPLACED CREW REST RUNNING LEFT LED EXIT SING P/N BR9795-001 ROBBED FROM SHIP 1813. OPS CHECK GOOD. PER B767 AMM 33-51 (4293181)

Part: NOT REPORTED — NOT REPORTED (EMERGENCY EXIT) · airframe 105,814 hrs · 15,685 cycles

SHIP 197 EMER EXIT ARMED PLACARD NOT EXTENDING. CORRECTIVE ACTION: FWD TO MCO/ PLACARD PER MEL 52-11-01. (M) PROCEDURES C/W, PLACARD INSTALLED (4293111)

Part: FITTING — CORRODED (BS 955 FRAME) · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 FOUND CORROSION AT BODY STATION 955 REF TO CPCP TASK W/C 53-524- 00. CORRECTIVE ACTION: LH W/W AT STA 955 SIDE FRAME FITTING AND REAR SPAR WEB CORROSION REPAIRED AS PER PRI: 602469-14. (2468608)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1329, BETWEEN STG39L AND STG38L,REFER TO CPCP TASK 53-550-00. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2467393)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+88, BETWEEN STG37R AND STG36R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2465810)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1153, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2465901)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+132, BETWEEN STG37R AND STG36R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2465802)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+66, BETWEEN STG37R AND STG36R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2465828)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+88, BETWEEN STG36R AND STG35R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2465865)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1153, BETWEEN STG38R AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2465914)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+88, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464495)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+132, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464448)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+66, BETWEEN STG38R AND STG37R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464485)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG38R AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464461)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+66, BETWEEN STG39R AND STG38R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464491)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 HFEC INSPECTION OF THE FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AT STATION 883.5, LBL89, BELOW WL 200 FOUND CRACK APPOXIMATELY LENGTH 3MM. CORRECTIVE ACTION: CUT OUT THE CRACK AND REPAIRED REF TO W/C: 5311-01195-09C. (2464545)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1307, BETWEEN STG38L AND STG37L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464419)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA197+22, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464490)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1241, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464404)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 HFEC INSPECTION OF THE FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AT STATION 859.5, LBL89, BELOW WL 200 FOUND CRACK APPROXIMATELY LENGTH 2MM. CORRECTIVE ACTION: CUT OUT THE CRACK AND REPAIRED REF TO W/C: 5311-01195-09A. (2464549)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+66, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464456)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+110, BETWEEN STG38R AND STG37R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464438)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1263, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464567)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 FWD CARGO SHEAR TIE FOUND CORROSION AT STA742,BETWEEN STG37R AND STG36R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464564)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CAGRO SHEAR TIE FOUND CORROSION AT STA1175, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464416)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG37R AND STG36R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464589)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG36L AND STG35L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464423)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+110, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464446)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG38R AND STG37R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464504)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 WHILE ACCOMPLISH W/C:5311-01195-10B STEP 5, NEED TO SUBMIT APPENDIX A - FILLER DATE REPORT TO LIAISON ENGINEERING. CORRECTIVE ACTION: FINAL REPAIRED REF TO W/C : 5311-01195-09B AND W/C: 5311-01195-10B. (2461538)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 FWD CARGO SHEAR TIE FOUND CORROSION AT STA742,BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461640)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+66, BETWEEN STG36L AND STG35L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461685)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+132, BETWEEN STG38R AND STG37R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461674)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461587)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA 1197+88, BETTWEEN STG38L AND STG37L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461567)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461627)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 PERFORM FQIS WIRING AND BONDING INSPECTION LEFT WING FOUND THE CONNECTOR M1944 FAILED .FURTHER INSPECTION OF THE CONNECTOR SHOWED THE CONNECTOR BACKSHELL TO BE SEVERELY CORRODED. CORRECTIVE ACTION: COMPLY WITH THE ER/A 602722-14AD REV ORIGINAL FOR DISPOSITON. (2461220)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1329, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461693)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHARE TIE FOUND CORROSION AT STA1241, BETWEEN STG36R AND STG35R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461680)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+44, BETWEEN STG37L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461589)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHARE TIE FOUND CORROSION AT STA1285, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461676)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHARE TIE FOUND CORROSION AT STA1197, BETWEEN STG39L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461574)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO STG39L FOUND CORROSION BETWEEN STA1219 AND STA1241. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 53-00-03 (2461216)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA 1197+22, BETWEEN ST 38R AND STG 39 R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2459807)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHARE TIE FOUND CORROSION AT STA1263, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461297)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHARE TIE FOUND CORROSION AT STA1197+66, BETWEEN STG37L AND STG38L, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461282)

Part: CONNECTOR — FAILED · airframe 105,744 hrs · 15,666 cycles

SHIP 197 PERFORM FQIS WIRING AND BONDING INSPECTION LEFT WING FOUND THE CONNECTOR M1944 FAILED. FURTHER INSPECTION OF THE CONNECTOR SHOWED THE CONNECTOR BACKSHELL TO BE SEVERELY CORRODED. CORRECTIVE ACTION: COMPLY WITH THE ER/A 602722-14A0 REV ORIGINAL FOR DISPOSITION ASSOCIATED ER/A 14-602722 (2471560)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+88, BETWEEN STG38R AND STG37R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461663)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 THE VERTICAL STABILIZER LH FWD SURFACE FOUND DELAMINATION AT FSS 195.390 TO FSS 270.784. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI 602519-14 REV.0 AND PRI 602519-14 REV.1 (2458388)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 THE VERTICAL STABILIZER LH FWD SURFACE FOUND DELAMINATION AT FSS 92.250 TO FSS 145.128. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 55-30-01-2R-1 & SRM 51-70-10-2R-4.FIG 201 & SRM 51-70-10-2R- 0. (2458348)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 -THE VERTICAL STABILIZER RH FWD SURFACE FOUND DELAMINATION AT FSS 11.787 TO FSS 39.250. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 55-30-01-2R-1 & SRM 51-70-10-2R-0 & SRM 51-70-10-2R-4. (2458367)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 THE VERTICAL STABILIZER RH FWD SURFACE FOUND DELAMINATION AT FSS 195.390 TO FSS 270.784. CORRECTIVE ACTION: THE VERTICAL STABILIZER RH FWD SURFACE REPAIRED AS PER B767-300 SRM 55-30-01-2R-1 & SRM 51-70-10-2R-4.FIG 201 & SRM 51-70-10-2R- 0. (2458359)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 HFEC INSPECTION FOUND 01EA CRACK ON RH LOWER UNDER-WING LONGERON FITTING AS MARK, CORRECTIVE ACTION: RH LOWER UNDER WING LONGERON FITTING 01EA CRACK LENGTH:0.160" REMOVED AND REPLACED REF TO W/C:5711-01042-04. (2460160)

Part: NONE — NONE · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AMOC REQUIRED TO AD 14-14-04: ERA 602721-14AD ISSUED FOR REPAIR TO STA 859.5, RBL 89 BULKHEAD. CORRECTIVE ACTION: AMOC TO AD 14-14-04 REQUIRED AT OR BEFORE 50,000 TOTAL FLIGHT CY CLES. (2447508)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1197+132, BETWEEN STG39L AND STG39R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2464221)

Part: NONE — NONE · corrosion level 2 · airframe 105,744 hrs · 15,666 cycles

SHIP 197 AFT CARGO SHARE TIE FOUND CORROSION AT STA1197+22, BETWEEN STG38R AND STG37R, CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (2461235)

Part: NONE — NONE · airframe 105,183 hrs · 15,567 cycles

AIRCRAFT 0197, FOUND #01 OVERWING SLIDE DOOR LATCH WORN. CORRECTIVE ACTION: REPLACED #1 OVERWING DOOR LATCH ON R/T SIDE. (8907164)

Part: NONE — NONE · airframe 105,183 hrs · 15,567 cycles

AIRCRAFT 0197, FOUND #04 OVERWING SLIDE DOOR LATCH WORN. CORRECTIVE ACTION: REPLACED #4 OVERWING DOOR LATCH ON R/T SIDE. CORRECTIVE ACTION: (8907165)

Part: CONNECTOR — FAULTED · airframe 104,927 hrs · 15,517 cycles

SHIP 0197 - DIV - TO LAX DUE TO DECREASING RIGHT HYD SYSTEM QUANTITY INDICATION. CORRECTIVE ACTION: CHECKED FOR EXTERNAL HYDRAULIC LEAKS AND HYDRAULIC SYSTEM HEAT EXCHANGER INTEGRITY. NO LEAKS NOTED. CHECKED HYDRAULIC QUANTITY INDICATION SYSTEM WIRING AND REPLACED CONNECTOR D60 DUE TO FAULT. A/C RTS. (9264056)

Part: BULB — NOT SEATED · airframe 104,507 hrs · 15,448 cycles

SHIP 197 2R SLIDE LIGHT REPORTED INOP, CORRECTIVE ACTION: RESEATED BULBS CKS NML (8826370)

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 103,996 hrs · 15,341 cycles

SHIP 197 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1L. CORRECTIVE ACTION: REPLACED SLIDE LIGHT LAMPS AND LAMP HOLDER PER B767 AMM 52-73. CHKD OK. PLACARD RMVD. (2167255)

Part: NONE — NONE · airframe 103,746 hrs · 15,289 cycles

SHIP 197 2R SLIDE LIGHT BLINKING. CORRECTIVE ACTION: REPOSITIONED SLIDE LIGHT BRACKET OPS CHECK WITH ARM/DISARM CHKS OK. (8528980)

Part: NONE — NONE · airframe 103,386 hrs · 15,196 cycles

SHIP 197 DOOR R2 SLIDE IND LIGHT INOP. FLICKERS. CORRECTIVE ACTION: R/R 2R ALARM SIGNAL MODULE PER B767 MM 52-73. (8230894)

Part: NONE — NONE · airframe 103,365 hrs · 15,189 cycles

SHIP 197 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS: 1L. CORRECTIVE ACTION: REINSTALLED AND CKS GOOD (2063947)

Part: NONE — NONE · airframe 102,973 hrs · 15,079 cycles

SHIP 197 EMERGENCY PATHWAY LIGHTS ROWS 13-20 WILL NOT ILLUMINATE DURING TEST. CORRECTIVE ACTION: REPLACED POWER SUPPLY M9011 PER B767 AMM 33-51. EPATH LIGHTS ROW 13-20 NOW TEST GOOD.(7989662)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,880 hrs · 14,811 cycles

SHIP 197 EMERGENCY EXIT LIGHT ON FORWARD LEFT LAV AND L!/RQ UPPER EXIT SIGN ARE INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY IN M1208 POWER SUPPLY. SYSTEM OPERATION IS NORMAL. (LP 7758720)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 101,756 hrs · 14,782 cycles

SHIP 197 (2) CLEAR EMERGENCY LIGHT LENSES ON THE AISLE ACROSS FROM SEAT 1B, 1C AND 1 RED LENS ON THE AISLE BY FORWARD RIGHT LAV ARE MISSING. CORRECTIVE ACTION: LENSES REPLACED. (LP 7347842)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 101,159 hrs · 14,628 cycles

SHIP 197 LOWER LOBE CREW REST VERTICAL EMERGENCY PATH LIGHT IS INOPERATIVE. MAINTENANCE RELAMPED 5 BULBS. SYSTEM OPERATION IS NORMAL. (LP 7594549)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 101,154 hrs · 14,626 cycles

SHIP 197 LOWER LOBE CREW REST HORIZONTAL EXIT SIGN IS INOPERATIVE. RELAMPED 8 BULBS. SYSTEM OPERATION IS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 101,154 hrs · 14,626 cycles

SHIP 197 LOWER LOBE CREW REST VERTICAL EXIT SIGN IS INOPERATIVE. MAINTENANCE RE-LAMPED 16 BULBS. SYSTEM OPERATION IS NORMAL. (LP 7594547)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,094 hrs · 14,611 cycles

DURING SERVICE CHECK FOUND SECTION OF FLOOR PATHWAY EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY CHARGER. SYSTEM OPERATION IS NORMAL. (LP 7594517)

Part: POWER SUPPLY — NO TEST (SLIDE SQUIBS) · airframe 100,797 hrs · 14,533 cycles

OVER WING SQUIBS WILL NOT TEST. MAINTENANCE REPLACED POWER SUPPLIES AND BATTERIES. SYSTEM OPERATION IS NORMAL.

Part: ACCESS DOOR — MISSING (RT WING) · airframe 100,797 hrs · 14,533 cycles

DURING WALK AROUND FOUND RIGHT WING LEADING EDGE SLATE LUBRICATION ACCESS DOOR MISSING. MAINTENANCE INSTALLED MISSING DOOR.

Part: SIGN — MISSING (CABIN) · airframe 100,388 hrs · 14,427 cycles

OVERHEAD EMERGENCY EXIT SIGN MISSING AT L2. MAINTENANCE RE-INSTALLED EXIT SIGN. SYSTEM OPERATION IS NORMAL.

Part: BOWL — LEAKING (HYD PUMP FILTER) · airframe 99,805 hrs · 14,341 cycles

FLIGHT 109, DECLARED EMERGENCY AND PERFORMED AN ATB DUE TO LOSS OF CENTER HYDRAULIC SYSTEM FLUID. MAINTENANCE FOUND THE C-1 ELECTRIC PUMP FILTER BOWL LEAKING AND REPLACED THE MODULE ASSEMBLY AND FILTERS. SYSTEM OPERATION IS NORMAL.

Part: PIN — DAMAGED (LIGHT CONNECTOR) · airframe 97,710 hrs · 14,039 cycles

EMERGECY FLOOR PATH LIGHTS ROW 29 LEFT, 15 RIGHT, 17 RIGHT AND 21 RIGHT LIGHTS WON'T TURN ON UPON SERVICE CHECK FOUND OPEN WIRE & CONNECTOR. REPLACED PINS AND RECONNECTED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 96,926 hrs · 13,932 cycles

SHIP 0197 - DIV - DIVERTED TO DTW DUE TO AUTO CABIN PRESSURIZATION FAILED. CREW WAS ABLE TO CONTROL THE CABIN PRESSURE MANUALLY PER QRH. CREW DECIDED TO DIVERT TO A STATESIDE HUB WITH OCC AND MCC CONCURRENCE. NO EMERGENCY WAS DECLARED; FLIGHT DIVERTED TO DTW. CORRECTIVE ACTION: MAINTENANCE REPLACED NR 1 AND 2 CABIN PRESSURE CONTROLLER. LP 6279710

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,829 hrs · 16,285 cycles

SHIP 197 WING / LOWER SKIN / LH WSTA 906.2-962.2 / CRACKED FASTENER HOLE #45 AT STR L-9.5. CORRECITVE ACTION: REPAIRED PER ERA 574301-14AD REV. ORIG. (0897391)

Part: WEDGE — GOUGED (LE SLAT) · airframe 95,563 hrs · 13,729 cycles

NR 6 INBOARD SLAT T/E WEDGE I/B END, GOUGED REPAIRED PER SRM 57-53-02. (LP 0893617)

Part: SKIN PANEL — PUNCTURED (RT HORIZ STAB) · airframe 95,563 hrs · 13,729 cycles

RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SKIN PANEL PUNCTURE. REPAIR C/W ER/A 564950-14. (LP 0890489)

Part: CONNECTOR — BROKEN (CABIN) · airframe 94,249 hrs · 13,556 cycles

EMERGENCY LIGHTS AT SEAT 17FG ARE INOPERATIVE. MAINTENANCE FOUND ELECTRICAL CONNECTOR AT SEAT BROKEN AND REPLACED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 92,995 hrs · 13,385 cycles

EMERGENCY LIGHTS ROWS 31-46 WERE INOPERATIVE. FOUND THE FUSE AT M9010 CHARGER TO BE BLOWN, REPLACED AND THE SYSTEM OPS NORMAL.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 92,336 hrs · 13,291 cycles

PASSING THRU APPROX. 9000 FT, THE CREW NOTICED A STRONG ODOR LIKE DANK, DIRTY SOCKS, THROUGHOUT THE CABIN AND FLIGHT DECK. ENGINE AND ALL OTHER INDICATIONS WERE NORMAL THE ODOR WAS MUCH STRONGER IN THE AFT CABIN. THE ODOR DISSIPATED DURING TAXI IN. APU & BOTH ENGINES PNEU SYSTEMS RAN WITH NO RESIDUAL ODOR. REPLACED BOTH RECIRCULATION FILTERS. NO OIL CONTAMINATION OR ODOR IN ANY PART OF THE CABIN .

Part: LIGHT — MISSING (CABIN) · airframe 92,087 hrs · 13,250 cycles

EMERGENCY LIGHT AT 41G MISSING. REPLACED DAMAGED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 91,422 hrs · 13,151 cycles

DURING A SERVICE CHECK, FOUND DAMAGE ON THE RIGHT STABILIZER LEADING EDGE AT HSS 211. REPAIRED IAW ERA 495014-56.

Part: SKIN — PUNCTURED (HORIZONTAL STAB) · airframe 91,422 hrs · 13,151 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE HAD A SKIN PUNCTURE. REPAIRED IAW 564950-14.

Part: UNKNOWN — ODOR (CABIN) · airframe 91,174 hrs · 13,115 cycles

BURNING ELECTRICAL ODOR NOTICED IN CABIN FROM ROW 28 TO BACK OF AIRCRAFT. NO SIGNS OF SMOKE NOTICED. ODOR APPROX 1 HR OUT FROM LANDING. RAN NR 1 AND 2 ENGINES INDEPENDENTLY WITH PACKS RUNNING. NO SMOKE OR ANY BURNING ODOR. CHECKED READING LIGHTS IAW MCC FOR SHORTING AND ARCING. NO SIGNS OF SHORTING AND ARCING. CHECKED OVENS AND COFFEEMAKERS, NO EVIDENCE OF BURNING OR ARCING NOTED.

Part: HOLDER — BROKEN (CABIN) · airframe 91,073 hrs · 13,102 cycles

EMERGENCY PATH LIGHTS AT 30B ARE BROKEN AND HANGING FROM THE SEAT. FOUND BROKEN SIDE PANEL WHICH HOLDS DIFFUSER COVER. REPLACED AISLE BUMPER TRIM AND EMERGENCY PATH LIGHT HOLDER. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 90,908 hrs · 13,073 cycles

EMERGENCY LIGHTS AT SEAT 41F IS INOPERATIVE. RESECURED SEAT MOUNTS. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 90,974 hrs · 13,082 cycles

EMERGENCY SEAT MOUNTED LIGHTING AT 30B IS INOPERATIVE. SECURED EMERGENCY SEAT LIGHT. SYSTEM OPERATION IS NORMAL.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 90,384 hrs · 12,996 cycles

AFT EMERGENCY EXIT LIGHTS ARE BURNED OUT. REPLACED THE BULBS.

Part: STIFFENER — NOT REPORTED (BS 246) · airframe 88,072 hrs · 12,640 cycles

CABIN FLOORBEAM STIFFENER BS 246, LBL 40. REPAIRED IAW SRM 53-10-51.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,437 hrs · 12,549 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE. REINSTALLED SEAT BRACKET. SYSTEM OPERATION IS NORMAL.

Part: FUEL TANK — CORRODED (BS 955) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

CABIN AREA CENTER TANK UPPER SURFACE AT BS 955 LBL 70 FOUND CORRODED. REPAIRED IAW ERA 551294.

Part: FUEL CELL — CORRODED (BS 955) · airframe 87,225 hrs · 12,516 cycles

BS 955, RBL 88.5 CENTER TANK CORRODED. REPAIRED IAW ERA 551296-14.

Part: FUEL CELL — CORRODED (BS 955) · corrosion level 2 · airframe 87,225 hrs · 12,516 cycles

CABIN AREA CENTER TANK UPPER SURFACE AT BS 955, LBL 88 FOUND CORRODED. COMPLIED WITH ERA 551297-14.

Part: FUEL TANK — CORRODED (BS 955) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

CABN AREA CENTER TANK UPPER SURFACE AT BS 955 RBL 88, FOUND CORRODED. REPAIRED IAW ERA 551296-14.

Part: SKIN — CORRODED (FUEL TANK) · airframe 87,225 hrs · 12,516 cycles

CORROSION LEVEL: 2 CABIN AREA CENTER TANK UPPER SURFACE AT STA 955 RBL 70 CORRODED AND REPAIRED PER ERA 551298-14.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

CORROSION LEVEL 2 AFT CARGO AT STA1395 STR39L, LT STIFFENER FOUND CORRODED AND REPLACED.

Part: SHEAR TIE — CORRODED (BS 1241) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

AFT CARGO AT BS 1241 BETWEEN STRINGERS 38-39L SHEAR TIE CORRODED AND REPLACED.

Part: BRACKET — CORRODED (BS 1395) · airframe 87,212 hrs · 12,513 cycles

AFT CARGO AT BS 1395 STRINGER 39L FOUND THE BRACKET CORRODED. REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

CORROSION LEVEL 2, AFT CARGO AT STA1197 BETWEEN STR39L-39R FOUND SHEAR TIE CORRODED AND REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 87,212 hrs · 12,513 cycles

AFT CARGO SHEAR TIE AT BS 1197+132 BETWEEN STRINGERS 37 - 38L FOUND CORRODED. REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

AFT CARGO AT BS 1395 BETWEEN STRINGERS 38 - 39R FOUND THE SHEAR TIE CORRODED. REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 87,212 hrs · 12,513 cycles

CORROSION ON AFT CARGO SHEAR TIE BS 1197+66 BETWEEN STRINGERS 39L-39R. REMOVED AND REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 87,212 hrs · 12,513 cycles

AFT CARGO AT BS 1197+110 BETWEEN STRINGERS 37-38L FOUND THE SHEAR TIE CORRODED. REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 87,212 hrs · 12,513 cycles

AFT CARGO AT BS 1197+22 BETWEEN STRINGERS 38-39L FOUND THE SHEAR TIE CORRODED. REPLACED.

Part: SKIN — CRACKED (RT WING) · airframe 76,244 hrs · 10,937 cycles

RT WING LOWER SKIN AT RWS 967.4 AND S9.5 FOUND CRACKED. REMOVED DAMAGED SKIN AREA AND INSTALLED REPAIR SHIMS AND DOUBLERS IAW ERA 526893-14AD.

Part: SKIN — CRACKED (LT WING) · airframe 76,244 hrs · 10,937 cycles

LEFT WING LOWER SKIN AT LWS 967.4 AND S9.5 FOUND CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR SHIM AND DOUBLERS IAW ERA 526893-14AD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 70,290 hrs · 10,055 cycles

EMERGENCY PATH LIGHTS AT SEAT 27F ARE INOPERATIVE. REPAIRED WIRE AT CONNECTOR UNDER SEAT. OPS CHECKED NORMAL.

Part: FLOORBEAM — DAMAGED (FS 1502 LBL 2) · airframe 69,903 hrs · 9,979 cycles

CABIN FLOORBEAM AT LBL 2, HAS TWO FASTENER HOLES WITH SHORT EDGE MARGIN AND WAS REPAIRED IAW ERA 509170-14, REV A.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 69,903 hrs · 9,979 cycles

BS 720, RBL 11, FLOORBEAM UPPER SURFACE CORRODED. REPAIRED IAW SRM 53-00-51 FIG 201, REPAIR 1.

Part: LIGHT — DAMAGED (SEAT 30AB) · airframe 66,313 hrs · 9,508 cycles

EMERGENCY LIGHT ASSY AT 30AB IS DAMAGED. MAINTENANCE REPLACE 30AB ASSY 2012-D0175.

Part: PIN — LOOSE (CONNECTOR) · airframe 63,879 hrs · 9,183 cycles

MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT 22AB. MAINTENANCE ADJUSTED AND SECURED A CONNECTOR PIN AT THE SAME LOCATION.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 61,363 hrs · 8,868 cycles

BULK CARGO DOOR SKIN PUNCTURED AT LWR FWD CORNER AND REPAIRED IAW ERA 487030-14.

Part: FRAME — CRACKED (FS 903) · airframe 61,355 hrs · 8,867 cycles

RT FS 903, FRAME INNER CHORD CRACKED BETWEEN STR 20 & 21R AND REPAIRED IAW ERA 487046.

Part: FRAME — CRACKED (FS 903) · airframe 61,355 hrs · 8,867 cycles

LT FS 903, FRAME INNER CHORD CRACKED BETWEEN STR 20 & 21 LT AND REPAIRED IAW ERA 480431-14.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,355 hrs · 8,867 cycles

RT WING INBD MAIN FLAP OTBD END L/E FAIRING DELAMINATED AND REPAIRED IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: SKIN — DELAMINATED (LT WING AILERON) · airframe 61,355 hrs · 8,867 cycles

LT WING INBD AILERON PANEL L/E 556CB FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-60-01, REPAIR 1 AND SRM 51-70-05, PARA 5D, FIG 6.

Part: WEDGE — DEFORMED (NR 4 SLAT) · airframe 61,355 hrs · 8,867 cycles

LT WING NR 4 SLAT WEDGE AREA INBD EDGE FOUND DEFORMED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10. REPAIR 4, FIG 202 AND SRM 57-43-02 REPAIR 1, FIG 201.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 61,355 hrs · 8,867 cycles

RT WING OTBD FLAP L/E MID AREA FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: UNKNOWN — ODOR (GALLEY) · airframe 60,928 hrs · 8,812 cycles

AN ELECTRICAL SMELL IN THE MID GALLEY WHEN UTILITY BUSES WERE TURNED ON, MAINTENANCE FOUND SMELL COMING FROM MID GALLEY COFFEEMAKERS. DEACTIVATED MID GALLEY COFFEEMAKERS 1 AND 2 PER NEF 253.08. MAINTENANCE CLEANED OVERFLOW SENSOR AT COFFEEMAKERS 1 AND 2. SYSTEM OPERATION IS NORMAL. (2010-D1348) (DL76L103069)

Part: WIRE — PULLED (CABIN) · airframe 60,746 hrs · 8,788 cycles

EMERGENCY LIGHTS AT SEAT 22AB ARE INOPERATIVE. MAINTENANCE FOUND PULLED WIRING FROM THE SIDEWALL AND RE-TERMINATED NEW HARNESS. SYSTEM OPERATION IS NORMAL. (2010-D1294) (DL76L102973)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 59,616 hrs · 8,651 cycles

EMERGENCY PATH LIGHT AT ROW 24AB IS INOPERATIVE. MX FOUND THE CONNECTOR AT SIDEWALL BUSTED AND RE-SPLICED, INSTALLED A NEW HARNESS. SYS OPS IS NORMAL.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHTS) · airframe 59,227 hrs · 8,601 cycles

ON DRC CHECK FOUND EMERGENCY LIGHTS FROM 24ABC TO 30ABC INOPERATIVE. MX REPAIRED LOOSE WIRE HARNESS AND REPLACED 24AB BATTERY PACK AND BATTERY PACK CHARGER. SYS OPS IS NORMAL. (2010-D0875)(DL76L101948)

Part: TRAY — DEFECTIVE (CABIN) · airframe 59,147 hrs · 8,591 cycles

EMERGENCY LIGHTS ROWS 6FG-19FG ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY TRAY. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,085 hrs · 8,584 cycles

EMERGENCY LIGHTS INOP ROW 6 -23 FG R & R BATTERY CHARGER, SEAT 14 AB. (DL76L101664)

Part: TRANSMITTER — INOPERATIVE (ELEVATORS) · airframe 56,697 hrs · 8,285 cycles

LT ELEVATOR POSITION INDICATION INOP AFTER TAXI OUT. FWD TO MCO AND PLACARD IAW MEL 27-08-01. RESET ELEV POS IND C/B NO HELP. VERIFIED LT ELEV MOVEMENT. REMOVED & REPLACED LT ELEV POSITION TRANSMITTER IAW AMM CKS GOOD MCO AND PLACARD REMOVED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 56,158 hrs · 8,212 cycles

AFTER STARTING LEFT ENGINE - L-GEN DRIVE MESSAGE AND DRIVE LIGHT ON OVERHEAD PANEL. REMAINED ILLUMINATED. LEFT GENERATOR SYS INOP. FWD TO MCO PER MEL 24-00-0. CHECKED, BPCU -IDG/PRESS SW WIRING- NOTED. MAINT PROC COMPLIED WITH, REPETITIVE APU OIL QTY CHECK REQUIRED. APU QTY CHECKED AND FULL. MCC NOTIFIED. PLACARD INSTALLED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: COMPUTER — MALFUNCTIONED (E&E BAY) · airframe 55,969 hrs · 8,188 cycles

A/C RETURNED TO BLOCKS DUE TO NO ETA OR FUEL INFO ON PROGRESS PAGE. RELOADED FMS NAV DATABASE USING DL3-0910-002 FLIGHT PLAN AND FMS NOW CHECK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 55,011 hrs · 8,067 cycles

L ENG CONTROL AND L ENG EEC 1 MSG AFTER ENG START - RTB. PIMU BIT - CH A/CNTRL. CH A/FAULT CAT 1. CH B/UNIT FAULT. CHB/CNTRL. FAULT CAT 1/CAT 2. CHB P2 LINE. T2/P2 PROBE HT. CH B LOST POWER. CH B XLINK FAIL. INSPECTED EEC AND LINES. ERASED MSGS RAN ENG ON IDLE, NO FAULTS NOTED. NO MTC AND STATUS MSGS.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 54,956 hrs · 8,061 cycles

LEFT ENG EEC MODE SWAPPED CHANNEL. PERFORMED BIT ON LEFT ENG PIMU NO FAULT. RAN ENG NO FAULTS

Part: STARTER — INOPERATIVE (NR 1 ENGINE) · airframe 54,486 hrs · 7,999 cycles

APU DUCT PRESSURE NORMAL. LEFT ENG N2 SHOWS ZERO DURING START. START VALVE INDICATED OPEN. NO OIL PRESSURE RISE. LEFT ENG STARTER MOTOR REPLACED AND OIL SERVICED IAW M/M. NOW OPS NML.

Part: SEAL — DAMAGED (NR 1 ENGINE) · airframe 54,334 hrs · 7,979 cycles

DURING IN FLT SHUTDOWN CHECK, FOUND 4TH STAGE STATOR MISSING SEALANT CAUSING DAMAGE TO INSULATION TO REAR FRAME OF ENG. MIP REPLACING ENGINE. NO PROCEDURE TO REPAIR MISSING SEALANT OR FOR REPAIR TO INSULATION. AT LEAST 7 STATORS HAVE THE SEALANT MISSING. C/W NR 1 ENG CHG PER TRANS 1T148.

Part: MODULE — MALFUNCTIONED (LT VHF RADIO) · airframe 54,252 hrs · 7,969 cycles

LT VHF WILL TRANSMIT, REC ONLY HISTORY. REMOVED AND REPLACED SWITCHING MODULE IAW MM. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: INDICATOR — INOPERATIVE (LT ELEVATOR) · airframe 53,984 hrs · 7,937 cycles

LEFT ELEVATOR INDICATION INOP, FWD TO MCO AND PLACARD PER MEL 27-08-01. REP CHK C/W OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (LT ELEVATOR) · airframe 53,880 hrs · 7,924 cycles

RTB DUE TO LT ELEV POSITION INDICATOR INOP ON TAXI-OUT. T/S PER FIM 27-31-01-101 OPS NML.

Part: IRU — FAULTED (LEFT) · airframe 53,480 hrs · 7,873 cycles

LT IRU FAULT INDICATION DURING TAXI. REMOVED AND REPLACED LT IRU PER AMM TEST AND OPS CK GOOD.

Part: INDICATION SYS — INOPERATIVE (LT ELEVATOR) · airframe 53,447 hrs · 7,869 cycles

RTB DUE TO LT ELEV INDICATION INOP. FWD TO MCO AND PLAC MEL 27-08-01.

Part: TRANSMITTER — MALFUNCTIONED (LEFT ELEVATOR) · airframe 53,282 hrs · 7,848 cycles

LEFT ELEV IND SYS ON EICAS PANEL UNRESPONSIVE TO CONTROL COLUMN MOVEMENT W HYD SYS PRESSURIZED NOTED DURING FLT CONTROL CHECK. RETURN TO GATE. FWD TO MCO AND PLACARD PER MEL 27-08-01.

Part: OVEN — ODOR (FWD GALLEY) · airframe 52,945 hrs · 7,810 cycles

UNUSUAL ODOR FORWARD GALLEY. OPERATED ALL EQUIPMENT IN FWD GALLEY FND FAINT PLASTIC ODOR FROM UPPER OVEN. AS PRECAUTION FOUND BOTH OVENS TO NEF PER 253.30 C/B`S PULLED COLLARED OVEN.

Part: OVEN — ODOR (GALLEY) · airframe 52,929 hrs · 7,806 cycles

UNUSUAL ODOR FORWARD GALLEY. OPERATED ALL EQUIPMENT IN FWD GALLEY FND FAINT PLASTIC ODOR FROM UPPER OVEN. AS PRECATUION FWD BOTH OVENS TO NEF PER 253.30 C/B`S PULLED COLLARED OVEN.

Part: WARNING LIGHT — FALSE ACTIVATION (LT GENERATOR) · airframe 52,673 hrs · 7,775 cycles

LEFT ENG GEN DID NOT COME ON LINE AFTER ENG START ALSO HAD LT ENG EEC MODE CAUTION ILLUMINATED. LT GEN FIELD LIGHT ILLUM WAS ILLUM RESET FIELD RAN ENG OPS CHECKS OK. FOUND GEN FIELD LIGHT ILLUM RESET FIELD RAN ENGINE OPS OK.

Part: TRANSMITTER — OUT OF LIMITS (TE FLAP) · airframe 52,446 hrs · 7,749 cycles

ON TAXI OUT RECEIVED FLAP T/E SHUTDOWN MSG. COULD NOT CLEAR MSG. FOUND THE NR 4 FLAP POSITION TRANSMITTER OUT LIMITS. REPLACED NR 4 FLAP POS T/E AND INSTALLED A -16 FSEU PER AMM PERFORMED ADJ TEST PER AMM CKS OK.

Part: FLAP — MALFUNCTIONED (WING) · airframe 52,323 hrs · 7,733 cycles

ON TAXI OUT WITH FLAPS 5 RECEIVED STATUS MESSAGE T/E FLAP SHUTDOWN. PERFORMED WALK AROUND. NO DAMAGE NOTED TO FLAPS. BIT FSEU. SHOWED NO CURRENT FAULTS. T/E FLAP SHUTDOWN SHOWED INTERMITTENTLY BUT FLAPS STILL MOVED. CHECKED FLAP HANDLE RVDTS M603 AND M604 ON FSEU ALL VALUES GOOD AND NOMINAL FROM ZERO TO THIRTY. REPLACED RELAYS K350 AND K623 AS PRECAUTION. RAN FLAPS ELECTRICALLY AND HYDRAULICALLY CHECKS GOOD. MCC NOTIFIED.

Part: STATOR — DAMAGED (NR 2 ENGINE) · airframe 51,998 hrs · 7,694 cycles

DURING ACCOMPLISHMENT OF EA 51-470869-12 REV H MAINTENACE FOUND PMA STATOR HAD INTERNAL DAMAGE AND REPLACED THE STATOR, STATOR PN 2710540-1 WITH DEPT 335 AS PRIME SHOP. FAA HAS REQUESTED SDR AND QA FOLLOW-UP WITH VENDOR TO CONFIRM DAMAGE AND DETERMINE IT'S SOURCE.

Part: WIRE — BROKEN (SLAT SENSOR) · airframe 48,544 hrs · 7,283 cycles

L/E SLAT ASYM MESSAGE DURING SLAT RETRACTION. SLAT LOCKED BETWEEN 1 AND UP. RETURNED TO ATL. MIP SUSPECTING NR 5 SLAT SENSOR OR TARGET. FOUND BROKEN WIRE AT SENSOR S280 REPAIRED SAME AND OPS CK GOOD.

Part: WIRE — BROKEN (L/E SLAT) · airframe 48,544 hrs · 7,283 cycles

AFTER T/O DURING FLAP RETRACTION, EICAS MESSAGE LE SLAT ASSY WITH TE FLAP INDICATOR BETWEEN 0 AND 1. BITE TEST OF FSEU NR 5 SLAT O/B SENSOR FAULTING FOUND BROKEN RED WIRE AT S280 SPLICE REPAIRED SAME CHECKS GOOD PER AMM.

Part: CASE — CRACKED (NR 1 FAN) · airframe 48,543 hrs · 7,282 cycles

NR 1 ENG CHANGE DUE TO FAN CASE CRACK.

Part: PUMP — LOW PRESSURE (HYD SYSTEM) · airframe 45,789 hrs · 6,941 cycles

LEFT PRIMARY HYD PUMP EICAS MSG CAME ON. LOW SYSTEM PRESSURE. LOW ENG HYD PUMP OUTPUT. REMOVED AND REPLACED LEFT ENG EDP PER AMM. REMOVED AND REPLACED PRESSURE AND CASE DRAIN FILTER PER AMM. OP AND LEAK CHECK OKAY.

Part: TIRE — FAILED (MLG) · airframe 45,382 hrs · 6,892 cycles

DURING T/O ROLL NOTICED VIBRATION FROM LEFT SIDE. ABORTED T/O AND PULLED OF ACTIVE RNWY 22R ONTO RNWY 31L. ABORT SPEEDLESS THAN 105 KTS. FOUND BOTH 5 AND 6 MAIN TIRES BLOWN. ACFT SITTING ON RIMS (5 AND 6). BRAKE TEMPS LESS THAN 2 ON ALL WHEELS. REPLACED NR 5 AND 6 MAIN WHEEL ASSY AND BRAKE ASSY PER AMM.

Part: UNKNOWN — UNKNOWN · airframe 45,234 hrs · 6,875 cycles

RT ENG VALVE AND SPAR VALVE FAIL TO OPEN DURING START. RESET SPAR VALVE C/B, VISUAL INSP SPAR VALVE OK. RESET FIRE HANDLE ENG RUN TEST GOOD.

Part: VALVE — UNKNOWN (RIGHT) · airframe 45,234 hrs · 6,875 cycles

RT ENG VLV AND SPAR VLV FAIL TO OPEN DURING START. RESET SPAR VLV C/B, VISUAL INSP SPAR VLV OK, RESET. FIREHANDLE ENG RUN TEST GOOD.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 45,145 hrs · 6,863 cycles

AFTER ENG START ON NR 2 ENG RT ENG BLEED LIGHT REMAINED ILLUMINATED WITH EICAS MSG. NO RT DUCT PRESSURE. RAN POWER UP RECYCLED SWITCHES SHUTDOWN AND RESTARTED ENGINE WITH NO CHANGE. REPLACED RT PRV VALVE IAW MM 254267. ALSO REPLACED CONTROLLER FOR PRV VALVE. OPS GOOD ON GROUND ENGINE RUN.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 45,145 hrs · 6,863 cycles

AFTER ENG START NR 2 ENG RT ENG BLEED LIGHT REMAINED ILLUM WITH EICAS MSG. NO DUCT PRESSURE. RAN POWER UP-RECYCLED SWITCHES-SHUTDOWN AND RESTARTED ENGINE. NO HELP. REPLACED RT PRV AND PRV CONTROLLER. OPS GOOD ON ENGINE RUN.

Part: STARTER — SPARKS (NR 2 ENGINE) · airframe 44,332 hrs · 6,765 cycles

DURING TAXI AND START OF RT ENG, HAD NO ROTATION AND SPARKS FROM STARTER AREA AFTER START VALVE OPENED. STARTER FAILED AND ALSO DAMAGED THE START VALVE. REPLACED STARTER AND START VALVE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 44,033 hrs · 6,728 cycles

EMERGENCY LIGHTS STAY ON WHEN COCKPIT SWITCH SET TO OFF. REPAIRED PUSHED BACK PIN AT PIN 33 OF PLUG D1650 AFT FLT ATTENDANT PANEL. EMERGENCY LIGHTS OPS CHK OK.

Part: PROJECTOR — OVERHEATED (CABIN) · airframe 42,158 hrs · 6,497 cycles

DURING TURN AROUND VIDEO PROJECTOR AT 24CDE CAUSING SMOKE. REPLACED PROJECT AT SEAT 24CDE, OPS CKS NORMAL MCO AND PLAC REMOVED.

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 41,337 hrs · 6,398 cycles

NR 2 ENG WOULD NOT START AFTER SELECTION OF NR 2 START VLV TO GND. NO NR 2 ENGINES INDICATIONS NOTED. REPLACED NR 2 ENG STARTER PER MM SPUN ENGINE. OPS NORMAL.

Part: VALVE — UNSERVICEABLE (NR 1 ENGINE) · airframe 41,160 hrs · 6,375 cycles

LT IDG VALVE STATUS LIGHT FWD TO MCO PER MEL 75-21-01C LOCKED VALVE DISP APPROVED. REMOVED IDG AIR OIL HEAT EXCHANGER AND VALVE PER AMM. INSTALLED IDG AIR OIL HEAT EXCHANGER VALVE PER MM NEEDS LEAK CK RAN ENG LEAK CK GOOD VOLTS FREQS GOOD MSG CLEARED MCO AND PLACARD REMOVED.

Part: BATTERY — MALFUNCTIONED (MASTER) · airframe 40,690 hrs · 6,314 cycles

MAIN BATTERY CHARGER STATUS MESSAGE DURING ENGINE START. REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER ASSYS. SYSTEM OPS TEST NORMAL. STATUS MESSAGE CLEARED.

Part: CONTROL VALVE — FAILED (RT) · airframe 40,643 hrs · 6,309 cycles

RTB DUE PRIOR TO TAKEOFF WITH RT BLEED PROVIDING AIR TO RT PACK OFF LIGHT ILLUMINATED WITH THRUST LEVER IN IDLE TO 85 PERCENT. REPLACED PACK FLOW CONTROL VLV AND THE RT PRSOV.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 37,372 hrs · 5,902 cycles

SIGNIFICANT WATER LEAK AFT GALLEY BEHIND OVENS. RTB. REMOVED OVENS LT SIDE OF AFT GALLEY. INSPECTED AREA AROUND OVENS, FOUND SMALL AMOUNT OF WATER IN OVENS BUT NOT OUTSIDE OF OVENS. CLEANED UP AREA. NO LEAKS NOTED.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 36,610 hrs · 5,796 cycles

AT T/O CREW REPORTED LEFT DUCT PSI FLUX ALONG WITH L-2 DOOR AREA HAVING VIBRATION AND VIBRATION WAS FELT IN CONTROL COLUMN ROLL MODE. RETURNED TO JFK FOR REPAIRS. INSPECTED LEFT ENGINE FOR BIRD STRIKE. BOROSCOPED AND VIBE SURVEYED. REPLACED PRSOV FOR HISTORY OF BLEED FLUX.

Part: WIRE — DAMAGED (CABIN) · airframe 34,844 hrs · 5,553 cycles

AFT CARGO PDU INOP. FOUND C/B OUT. RESET SAME AND SPARKS STARTED FLYING IN P-39 PANEL. NUMEROUS WIRES (30-40) BURNED INSIDE PANEL. REPAIRED WIRING.

Part: ENGINE — MAKING METAL (NR 2) · airframe 34,477 hrs · 5,500 cycles

NR 2 ENGINE REPLACED DUE METAL FOUND IN NR 3 MCD.

Part: OVEN — DIRTY (AFT GALLEY) · airframe 34,201 hrs · 5,457 cycles

SLIGHT ELECTRICAL ODOR NOTICED IN AFT GALLEY WITH NO VISIBLE SMOKE. PULLED ALL GALLEY C/B INCLUDING AFT GALLEY LEFT AND RIGHT BREAKERS IN COCKPIT. ODOR DISSIPATED AND FLIGHT CONTINUE WITH NO FURTHER USE OF AFT GALLEY. ALSO ALL AFT GALLEY LIGHTS WERE TURNED OFF. CHECK ALL LIGHTS AND OVEN AND COFFEEMAKER FOR OPS AND ODOR, ALL OK. NOTIFY CABIN SVC TO CLEAN ALL OVEN AREA. RAN BOTH PACK AND GALLEY VENT FANS, ALL NORMAL.

Part: SWITCH — OVERHEATED (COCKPIT) · airframe 33,553 hrs · 5,369 cycles

ON APPROACH LATCHED THE EGPWS INHIBIT SWITCH, HAD ELECTRICAL ODOR IN COCKPIT. SVO FOUND INHIBIT SWITCH WARM WHEN LATCHED IN. REPLACED P3-1 PANEL.

Part: CONTROL UNIT — MALFUNCTIONED (SLATS) · airframe 26,437 hrs · 4,293 cycles

LEADING EDGE SLAT ASSY EICAS ON SLAT RETRACTION. AIR RETURN TO ATL. REPLACED S301 PER M/M. ACFT RETURNED TO ETOPS STATUS AFTER VERIFICATION FLIGHT. L/E SLATS OPERATED NORMAL.

Part: TRANSMITTER — FAILED (NR 2 ENGINE) · airframe 24,653 hrs · 3,980 cycles

AFTER T/O AND REACHING FL230 GOT EICAS CAUTION MSG, RT ENG FUEL FILTER. NO CHANGE WITH POWER REDUCTION. REPLACED FUEL FILTER AND PRESSURE TRANSMITTER.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 23,602 hrs · 3,785 cycles

DURING ETOPS L/O CHECK, FOUND L391 EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED M733 EMERGENCY EXIT LIGHT POWER SUPPLY. CHECKS GOOD.

Part: O-RING — FAILED (SPOILER) · airframe 22,585 hrs · 3,602 cycles

DURING CRUISE AT FL350 GOT R HYD QTY EICAS MSG AND R HYD RVSR LT ON OVERHEAD PANEL. R HYD QTY AT .47. FOLLOWED PROCEDURE AND TURNED OFF R ENG HYD PUMP AND R DEMAND PUMP. R HYD QTY STAB AT .37 REST OF FLIGHT. FOUND O-RING ON PLUG AT NR 13 SPOILER BLOWN OUT. REPLACED O-RING ON NR 13 SPOILER ACR PLUG. SERVICED HYD SYSTEM. RAN FLT CONTROLS. NO FURTHER LEAKS NOTED. CHECKS OK.

Part: FAN — FAULTY (E/E BAY) · airframe 16,847 hrs · 2,669 cycles

ACFT DIVERTED INTO KEF DUE TO SMOKE IN COCKPIT. REPLACED FWD EXH FAN PER M/M 21-58-06-4. LEAK CK AND OPS CKS O.K. NO FAULT INDICATIONS

Part: SKIN — DENTED (NR 1 SLAT) · airframe 16,554 hrs · 2,621 cycles

OUTBOARD MOST 54 INCHES OF THE LE SKIN OF THE NR 1 SLAT WAS FOUND DAMAGED BY IMPACT. REPAIR PER ER/A 371936-14 REV B

Part: FAN — SEIZED (CABIN) · airframe 14,590 hrs · 2,303 cycles

STRONG ELECTRICAL SMELL WAS NOTED THROUGHOUT THE CABIN AND COCKPIT AT 0420Z FOR ABOUT 1 MIN AND SMELL DISSIPATED. AT THE SAME F/A PLUGGED IN THE ENTERTAINMENT WIRE AT 21F, 1.5 HR LATER THE SMELL REOCCURRED MOMENTARILY. ON FINAL APP SMELL RETURNED VERY STRONG. 02 FOUND LT RECIRCULATION FAN INOP AND CIRCIUT BREAKER POPPED. FAN SEIZED UP. FWD TO MCO AND PLACARD PER MEL 21-25-01A. C/B PULLED AND COLLARED.

Part: SYMBOL GENERATOR — MALFUNCTIONED (E/E BAY) · airframe 11,705 hrs · 1,806 cycles

CO-PILOTS ND HAD MAP FAIL FLAG. ISOLATED CAUSE TO SYMBOL GENERATOR AND VERIFIED. CTR SYMBOL GENERATOR FWD TO MCO AND AIRCRAFT WAS DISPATCHED FROM MAD NON ETOPS PER MEL 34-22-05A. FOUND WIRE ON NORM/TRUE SWITCH.

Part: HARNESS — ARCING (SEAT 4)

ELECTRICAL BURNING SMELL AT SEATS 4C AND E. SEATS DEACTIVATED. REPLACED WIRE BUNDLE.

Part: BATTERY — DISCHARGED (EMER EXIT SLIDE)

DURING PDC OVERWING SLIDE SQUIBS WOULD NOT TEST. REPLACED BOTH OVERWING SQUIB BATTERIES M961 AND M962. TEST OPS NORMAL.

Part: PRSOV — FAILED (NR 1 ENGINE)

AFTER TAKEOFF, NO BLEED AIR FROM LEFT ENG. ELECTED TO BRING A/C BACK TO ATL FOR REPAIRS. REPLACED PRSOV, SYSTEM CHECKS NORMAL.

Part: COMPRESSOR — OVERHEATED (WATER SYS)

ELECTRICAL SMELL DETECTED CLOSE TO RT AFT ENTRY DOOR. FOUND WATER COMPRESSOR OVERHEATED CAUSING SMELL. DISCONNECTED AND TIED BACK C/P AT WATER COMPRESSOR AND PULLED AND COLLARED CBMCO AND PLACARD INSTALLED.

Part: PUMP — FAILED (C HYD SYS)

FIFTEEN MIN AFTER T/O, LT HYD PUMP PRIM 1 EICAS MSG ILLUM WITH LIGHT. DIVERTED TO FRA. PLACED PUMP ON MCO. ATB TO FRA. REPLACED NR 1 ELEC PUMP AND CASE RETURN FILTER. REMOVED MCO, SYSTEM OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (RT EMER EXIT)

DURING OW2 CHECK, SLIDE/SPOILER SQUIB TEST FAILED. FOUND VOLTAGE OF RIGHT ESCAPE BATTERY LOW. REPLACED BATTERY AND PERFORMED GOOD TEST OF SQUIBS.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING MTC, FOUND THAT RT AND LT OVERWING SLIDE SQUIBS WOULD NOT TEST. REPLACED THE BATTERY PACKS FOR THE OVERWING SLIDE POWER SUPPLYS. THE SQUIBS THEN TESTED NORMALLY.

Part: LIGHT — MISSING (CABIN)

EMERGENCY ESCAPE PATH LIGHT (1 WHITE) MISSING AT SEAT 10B. REPLACED MISSING LIGHT ASSY AT 10B, OPS CKS GOOD.

Part: COFFEEMAKER — ODOR (GALLEY)

STRONG ODOR IN ALL GALLEYS, VERY UNCOMFORTABLE TO WORK IN FOR THE FLIGHT ATTENDANTS. FLIGHT ATTENDANTS ALSO REPORT THAT THERE IS NO DEFINABLE SOURSE AND IT SMELLS LIKE BURNED PAPER OR A HOT IRON. FOUND FIBERGLASS TAPE INSTALLED ON THE LOWER COVER PLATE OF ALL 8 GALLEY COFFEEMAKER. MODIFIED COFFEEMAKERS PER ERA 310476-14.