N183DN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 129,733 hrs · 18,769 cycles

SHIP 183 DURING SVC FOUND PANEL 436BL ON #1 ENG MISSING. CORRECTIVE ACTION: REPLACED PANEL IAW B767 AMM 54-53. P/N 311T3065-253. (4528055)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 129,739 hrs · 18,770 cycles

SHIP 183 UPPER RED LED EMERGENCY LIGHT INOP ON LCCR STAIRS. CORRECTIVE ACTION: FOUND CONNECTOR WITH LOOSE PIN, RESECURED PIN & CONNECTOR REF B767-300 AMM 33-51. (4528046)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 129,287 hrs · 18,673 cycles

SHIP 183 ON WALKAROUND FOUND STEP ON LEFT EMERGENCY ESCAPE HANGING BELOW THE WINDOW. CORRECTIVE ACTION: REMOVED RT AFT EMER EXIT DOOR, SECURED OUTTER STEP. REINSTALLED DOOR. WORK DONE PER B767 AMM 25-65. ALL ARM AND DISARM C/W IAW B767 AMM 25-65. (5018650)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 129,023 hrs · 18,626 cycles

SHIP 183 L 2 PAX DOOR ARM LIGHT FLASHING. OPS CKS FINE CYCLED NUMEROUS TIMES. NO TROUBLE FOUND, REMOVED PLACARD AND RETURNED TO SERVICE. (4521580)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 128,733 hrs · 18,571 cycles

SHIP 183 DOOR 2L SLIDE LIGHT BLINKS. DOOR IS DISARMED, BUT SLIDE LIGHT BLINKING. CORRECTIVE ACTION: REINSTALLED SLIDE LIGHT MECHANISM PER B767 AMM 33-50 (4526922)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 128,566 hrs · 18,545 cycles

SHIP 183 DURING SVC FOUND OVERHEAD EMERGENCY COVER MISSING BEHIND FIRST CLASS ON LEFT HAND SIDE. CORRECTIVE ACTION: REPLACED OVERHEAD EMERGECY COVER BEHIND FISRT CLASS ON LEFT HAND SIDE. REF. B767 AMM 3351. CHECKS GOOD. (4922868)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 127,759 hrs · 18,415 cycles

SHIP 183 EMERGANCY LIGHT EXIT LENS OVER ISLE SEAT 16C MISSING. CORRECTIVE ACTION: EMERGANCY "EXIT" LENS FOUND AND REINSTALED. (4871046)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 127,590 hrs · 18,389 cycles

SHIP 183 LEFT AFT DOOR SLIDE LIGHT KEEPS FLASHING. CORRECTIVE ACTION: R/R LT AFT DOOR SLIDE LIGHT ASSY PER B767-300 AMM 52-73. OPS CHK NORMAL. (4911266)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 127,299 hrs · 18,340 cycles

SHIP 183 R1 EMERGENCY LIGHT LENS COVER FOR EMERGENCY DOOR ROBBED FOR A/C 192 CORRECTIVE ACTION: INSTALLED RIGHT EMERGENCY DOOR EXIT SIGN IAW B 767-300 AMM 33-51 (4538812)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 126,975 hrs · 18,284 cycles

SHIP 183 FOUND WHITE EMERGANCY PATH LIGHT AT SEAT 36B INOP, CORRECTIVE ACTION: FOUND WIRES FROM TERMINALS REMOVED. REPLACED TERMINALS PER B767 WDM 33-51-31 AND SWPM 20-30 OPS CHECK GOOD. (9695456)

Part: NONE — NONE · airframe 126,531 hrs · 18,207 cycles

SHIP 183 L1 DOOR WOULD NOT ARM IN LAX. MX WAS CALLED AND THE DOOR WOULD ONLY ARM WHEN HE PUSHED THE HANDLE IN FROM OUTSIDE. CORRECTIVE ACTION: CLEANED DEBRIS FROM GIRTBAR & TRACKS. OPENED, CYCLED, CLOSED L1 DOOR MULTIPLE TIMES FROM INSIDE IAW B767-300 AMM 52-11. ALL ARMED INDICATORS COME ON & TURN OFF WHEN SUPPOSED TO. (4188848)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 125,807 hrs · 18,072 cycles

DURING SERVICE CHECK FOUND EXIT SIGN LENS MISSING FOR OVERHEAD SIGN AT ROLL 16 RT SIDE. CORRECTIVE ACTION: REPLACED CROSS AISLE EXIT SIGN LENS AT ROLL 16 RT SIDE IAW AMM 33-51 OPS NORMAL OK FOR SERVICE.

Part: SIGN — MISSING · airframe 125,513 hrs · 18,013 cycles

SHIP 183 EXIT SIGN ROW 16CMISSINGBACK. CORRECTIVE ACTION: REINSTALLED EXIT SIGN ON THE BACK SIDE AT ROW 16C. OPS CKS NORMAL. (2498255)

Part: WARNING MESSAGE — FALSE ACTIVATION (LE SLATS) · airframe 125,473 hrs · 18,005 cycles

FCNT/DE- DUE TO LE DISAGREE INDICATION DURING APPROACH. CREW PERFORMED GO AROUND AND DECLARED EMERGENCY. C/W QRH AND DISAGREE CLEARED. UNABLE TO DUPLICATE. CHECKED LVDT RIGS. ALL NORMAL. RTS.

Part: NONE — NONE · airframe 125,395 hrs · 17,990 cycles

SHIP 183 EXIT SIGN BEHIND ROW 9, FO SIDE FELL OFF, CORRECTIVE ACTION: SECURED EXIT LENS AT LOC 802 - CKS SECURED (8582898)

Part: NONE — NONE · airframe 125,395 hrs · 17,990 cycles

SHIP 183 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:607. CORRECTIVE ACTION: RE-SECURED LIGHT ASSY. 2L SLIDE INDICATION CKS OK (2482380)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 125,169 hrs · 17,946 cycles

SHIP 183 FOUND LTEXTERIOR EGRESS OVERWING LIGHT INOP CORRECTIVE ACTION: RELAMPED NO HELP. REF B767 AMM 33-51. R/R LT EXTERIOR EGRESS OVERWING LIGHT REFLECTOR ASSY PER B 767 AMM 33-51. (8582806)

Part: NONE — NONE · airframe 124,925 hrs · 17,895 cycles

SHIP 183 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101, CORRECTIVE ACTION: SLIDE LIGHT @ 2L DOOR OPS CHK NML. UNABLE TO DUPLICATE FAULT. LIGHT FUNCTIONS WELL PER B767 300 AMM 52-73. A/C OK FOR SVC. (2408117)

Part: NONE — NONE · airframe 124,925 hrs · 17,895 cycles

SHIP 183 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:16C, CORRECTIVE ACTION: RE-INSTALLED EMERGENCY EXIT SIGN COVER AT ROW 16. CKS OK. (2407624)

Part: NONE — NONE · airframe 124,925 hrs · 17,895 cycles

SHIP 183 FRC256001 EMERGENCY EXIT SIGN BEHIND ROW 16 FELL OFF. CORRECTIVE ACTION: RE-INSTALLED EMERGENCY EXIT SIGN COVER AT ROW 16.CKS OK. (9206676)

Part: NONE — NONE · airframe 125,115 hrs · 17,933 cycles

'SUPPLAMENTAL INFOMATION' SHIP 183 ON PRE FLIGHT SMALL PANEL MISSING ON RT ENGINE OUTBOARD PYLON MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. CORRECTIVE ACTION: REPLACED RT ENGINE OUTBOARD NACELLE STRUT ACCESS DOOR IAW B767 AMM 54-53. OK FOR SVC. CDL AND PLACARD REMOVED. (9206602)

Part: NONE — NONE · airframe 124,521 hrs · 17,815 cycles

'SUPPLEMENTAL INFOMATION' SHIP 183 AFT LH DOOR SLIDE LIGHT INTERMITTANT, CORRECTIVE ACTION: FWD TO MEL 52-73-01 & PLACARD INSTALLED. FOUND LIGHT ASSY LENS NOT FULLY SEATER SECURED SAME OPS CHK NML. REF B767-300. AMM 52-73. (9023146)

Part: HARNESS — MISSING · airframe 124,444 hrs · 17,800 cycles

SHIP 183 LLCR ESCAPE HARNESS MISSING (2EA). CORRECTIVE ACTION: REPLACED MISSING LLCR ESCAPE HARNESS. MEL & PLAC REMOVED. (9023109)

Part: NONE — NONE · airframe 124,168 hrs · 17,745 cycles

SHIP 183 DURING SVC CHECK FOUND EMERGENCY LIGHTS INOP AT ROWS 21AB-30AB AND 21GF-31GF, CORRECTIVE ACTION: R/R BATT CHARGER M9009 NO HELP. R/R BATT NO HELP. FOUND DAMAGED WIRE AT SEAT 21AB. ALL LIGHTS NOW CK GOOD. WORK DONE PER B767 AMM 33-51 AND SWPM CH. 20. (8684986)

Part: LENS — DAMAGED · airframe 124,008 hrs · 17,711 cycles

SHIP 183 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING, CORRECTIVE ACTION: FOUND EMERGENCY LIGHT LENS AND RE-ATTACHED. CKS OKAY. (2287823)

Part: COVER — MISSING · airframe 123,984 hrs · 17,705 cycles

SHIP 183 EMERGENCY EXIT SIGN COVER MISSING 16BC. CORRECTIVE ACTION: RESECURED COVER. OK FOR SVC (8611156)

Part: POWER SUPPLY — INOPERATIVE · airframe 123,829 hrs · 17,673 cycles

SHIP 183 EXTERIOR EMERGENCY LIGHTING SYSTEM /BATTERY POWERED/ MEL NUMBER ADDED FOR DISPATCH RELEASE, CORRECTIVE ACTION: R/R POWER SUPPLY UNIT PER B767-300 AMM 33-52 OPS CHECK GOOD (9213548)

Part: SCREW — BACKED OUT · airframe 123,743 hrs · 17,656 cycles

SHIP 183 1L DOOR SLIDE WILL NOT ARM, CORRECTIVE ACTION: FOUND SCREW IN FLOOR FITTING FROM SLIDE COVER ON DOOR. SECURED SAME SLIDE OPS OK (8807196)

Part: SIGN — BROKEN · airframe 123,670 hrs · 17,621 cycles

SHIP 183 EXIT SIGN @ 16C FELL OFF, CORRECTIVE ACTION: REINSTALLED EXIT SIGN 16C PER B767-300 33-51. OK FOR SVC. (8171367)

Part: BOTTLE — INOPERATIVE · airframe 123,618 hrs · 17,600 cycles

SHIP 183 L/H OVERWING EXIT BOTTLE, C BALL BELOW CLIPS, CORRECTIVE ACTION: REPLACED L/H OVERWING SLIDE BOTTLE PER WORK CARD 2561-4723 (7340939)

Part: STABILATOR — DELAMINATED · airframe 123,597 hrs · 17,591 cycles

SHIP 183 VERTICAL STABILIZER BETWEEN ZONE 3A ?WITH EVIDENT DELAMINATION. CORRECTIVE ACTION: VERTICAL STABILIZER RH SIDE ZONE 3A PANEL P/N 175T2001-2 LOWER AREA WAS REPAIRED I.A.W B767-300 SRM 55-30 AND SRM 51-70. (2208386)

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 122,464 hrs · 17,371 cycles

SHIP 183; FLIGHT 423 JFK-LAX PERFORMED AN ATO DUE TAKE OFF CONFIG WARNING FLAPS BELOW 80KTS. CORRECTIVE ACTION: REPLACED FSEU AND TESTED TAKE OFF CONFIG WARNING SYSTEM. SYSTEM OPERATION IS NORMAL.

Part: ELBOW — LEAKING (OXYGEN LINE) · airframe 122,453 hrs · 17,369 cycles

SHIP 183 - DIV - DIVERTED TO DTW DUE CREW REPORT OF CREW O2 PRESSURE DROPPED TO ZERO AFTER 2.5 HOURS OF FLIGHT. CORRECTIVE ACTION: FOUND SLOW LEAK AT ELBOW ON MASK SUPPLY LINE IN CAPTAIN'S O2 BOX. TIGHTENED LINE. NO LEAKS NOTED. REPLACED O2 BOTTLE. NO-GO ODI PROCEDURE COMPLIED WITH. LP 6652772

Part: ACCESS DOOR — MISSING (LT WING) · airframe 122,336 hrs · 17,345 cycles

2 ACCESS DOORS MISSING FROM LEFT WING JUST OUTBOARD OF ENGINE. INSTALLED NEW ACCESS DOOR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,960 hrs · 17,281 cycles

ALL LLCR EMERGENCY LIGHTS ALL BURNT. REPLACED ALL LLCR EMERGENCY LIGHT BULBS PER B767-300 AMM 33-52. CKS OK. (LP6352180)

Part: LIGHT — DAMAGED (CABIN) · airframe 118,731 hrs · 16,859 cycles

EMERGENCY ESCAPE PATH LIGHT DAMAGED AT SEAT 41F. MAINTENANCE REATTACHED PATH LIGHTS TO SEAT. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 118,019 hrs · 16,755 cycles

LT WING LOWER SKIN, STRINGER L-9.5 WSTA906.20 TO WSTA934.20. ONE CRACKED HOLE REPAIRED PER ER/A 572983-14.

Part: SKIN — DAMAGED (RT WING) · airframe 118,019 hrs · 16,755 cycles

RT LOWER WING SKIN STRINGER L-6.5. BETWEEN WSTA990.2 AND WSTA1018.2. DIAMETER:0.625" HOLE REPAIRED PER ER/A 572984-14.

Part: DOUBLER — NOT REPORTED (RT WING) · airframe 126,079 hrs · 18,120 cycles

SHIP 183 RH LOWER WING SKIN EXTERNAL DOUBLER REPAIR AT STR 6.5 AND STA 990. CORRECTIVE ACTION: ER/A 572984-14AD REVISED TO REV. A. ACCOMPLISH ER/A 572984-14AD REV A SECTION II INSPECTIONS. (0850550)

Part: FITTING — CRACKED (RT WING) · airframe 118,019 hrs · 16,755 cycles

HFEC INSPECTION FOUND 01 EA CRACK ON RT WING LOWER UNDERWING LONGERON FITTING AND REPLACED.

Part: STRAP — NOT REPORTED (FUSELAGE) · airframe 118,019 hrs · 16,755 cycles

STA 955 FAIL-SAFE STRAP REPAIRED.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 118,019 hrs · 16,755 cycles

LH WING I/B FLAP MAIN FLAP UPPER SURFACE FOUND BULGE SKIN. REPAIRED BULGE AREA SRM 57-53-01 AND 51-70-17. (LP 0844807)

Part: SKIN — DAMAGED (BS 133-172) · airframe 118,019 hrs · 16,755 cycles

LH FUSELAGE SKIN AT STA 133 TO 172 2 EACH LIGHTING AREA DAMAGED. REPAIRED PER SRM 53-00-01. (LP 0843644)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+44 BETWEEN S-39R AND S-39L. CORRODED AREA REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197 BETWEEN S-39R AND S-39L. SHEAR TIE REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+88 BETWEEN S-39R AND S-38R. SHEAR TIE REPLACED.

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03 EA SHEAR TIE SURFACE CORROSION AT STA 1285 , BETWEEN S-38L AND S-35L AND REPLACED. (LP 0844791)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA 1307 BETWEEN S-39R AND S-39L AND REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 118,064 hrs · 16,762 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+88. BETWEEN S-38L AND S-37L AND REPLACED. (LP 0847073)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1197+22 BETWEEN S-39R AND S-39L AND REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 1219 BETWEEN S-39R AND S-38R AND REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+110 BETWEEN S-39R AND S-39L AND REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+66 BETWEEN S-38L AND S-37L. SHEAR TIE REPLACED.

Part: SHEAR TIE — CORRODED (BS 1241) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2- AFT CARGO COMPARTMENT FOUND 03 EA SHEAR TIE SURFACE CORROSION AT STA 1241, BETWEEN S-38L AND S-35L AND REPLACED. (LP 0844798)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1219 AND REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA1197+132 , BETWEEN S-38L AND S-37L AND REPLACED. (LP 0844794)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 04EA SHEAR TIE SURFACE CORROSION AT STA 1307 BETWEEN S-38L AND S-34L, SHEAR TIE REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE SURFACE CORROSION AT STA1241 BETWEEN S-36R AND S-35R. CORRODED AREA REPLACED.

Part: STRINGER — CORRODED (BS 830) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CORROSION ON STRINGER ON STA 830,STR-18L. REPAIRED PER ERA 573051-14. (LP 0839823)

Part: STRINGER CLIP — CORRODED (BS 1197) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON CLIP ATTACHED ON STR-16R AND FRAME AT STA1197+110. REPLACED CORRODED AREA. (LP 0839457)

Part: STRINGER — CORRODED (BS 925) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 STRINGER 20R FOUND CORRODED AT STA925 AND REPAIRED. (LP 0839816)

Part: STRINGER CLIP — CORRODED (BS 1175) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CLIPS FOUND CORRODED ON STA1175,STR-16L AND REPLACED. (LP 0839588)

Part: STRINGER CLIP — CORRODED (BS 1263) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON CLIP ON STA1263,STR-17R AND REPLACED. (LP 0839461)

Part: STRINGER CLIP — CORRODED (BS 1197) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CLIP ATTACHED ON STR 16R AND FRAME AT STA 1197+88 FOUND CORRODED AND REPLACED. (LP 0839479)

Part: SEAT TRACK — CORRODED (BS 753-1098) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 SEAT TRACK CORROSION FOUND ON CABIN SEAT TRACKS AROUND STA753 TO STA1098, RBL88.5 AND REPAIRED. (LP 0839741)

Part: ATTACH ANGLE — CORRODED (BS 1326) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

LEVEL 2 CORROSION: CORRIOSN FOUND ON FRAME ATTACHED ANGLE ON STA 1326. CORRODED AREA WAS REPLACED. (LP 0839556)

Part: TRUSS — CORRODED (BS 654) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 TRUSS FOUND CORRODED AT STA654+55,STR-20L. CORRODED AREA REPLACED. (LP 0839480)

Part: STRINGER CLIP — CORRODED (BS 1153) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CLIP FOUND CORRODED ON STA1153,STR-16L AND REPLACED. (LP 0839577)

Part: STRINGER CLIP — CORRODED (BS 1263) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CLIP FOUND CORRODED ON STA1263,STR-16L. REPLACED AREA. (LP 0839600)

Part: SEAT TRACK — CORRODED (BS 998-1070) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 SEAT TRACK-CORROSION FOUND ON CABIN SEAT TRACKS AROUND STA998 TO STA1070, LBL1. REPLACED CORRODED AREA. (LP 0839443)

Part: SEAT TRACK — CORRODED (BS 1098-1208) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 SEAT TRACK-CORROSION FOUND ON CABIN SEAT TRACKS AROUND STA1098 TO STA1208, RBL88.5. REPAIRED PER SRM 51-10-02 AND 53-00-52. (LP 0839745)

Part: SEAT TRACK — CORRODED (BS 1208-1428) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 SEAT TRACK-CORROSION FOUND ON CABIN SEAT TRACKS AROUND STA1208 TO STA1428, RBL88 AND REPLACED. (LP 0839749)

Part: SKIN — CORRODED (BS 925) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON FUSELAGE SKIN ON STA925 AND 2 INCH ABOVE THE FLOOR LEVEL. REPAIRED PER ERA 573021-14. (LP 0839762)

Part: TRUSS — CORRODED (BS 1230) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 TRUSS FOUND CORRODED ON STA 1230,STR-20L AND REPLACED. (LP 0839473)

Part: SEAT TRACK — CORRODED (BS 1098-1230) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 SEAT TRACK-CORROSION FOUND ON CABIN SEAT TRACKS AROUND STA1098 TO STA1230, LBL88.5 AND REPAIRED. (LP 0839730)

Part: FLANGE — CORRODED (BS 1197) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 FOUND CORRORED ON UPPER & LOWER FLANGES AROUND STA 1197+113 OUT OF LIMITS AND REPAIRED. (LP 0838308)

Part: SKIN — CRACKED (BS 1725) · airframe 118,019 hrs · 16,755 cycles

RH FUSELAGE SKIN FOUND 01EA CRACK AT BS1725. SKIN REPAIRED PER SRM 53-80-01. (LP 0838599)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+110 , BETWEEN S-38L AND S-37L AND REPLACED. (LP 0844806)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 118,019 hrs · 16,755 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA1197+110 BETWEEN S-39L AND S-38L AND REPLACED.

Part: SKIN — CRACKED (BS 1633) · airframe 118,019 hrs · 16,755 cycles

FUSELAGE AT STA 1633 S-14R.EXTERNAL CRACKED SKIN REPAIRED (LP 0835521)

Part: SKIN — CRACKED (RT WING) · airframe 118,073 hrs · 16,763 cycles

RIGHT WINGS UPPER SKIN PANEL OUTBOARD UPPER LINK PITCH LOAD FITTING AREA CRACKED FASTENER LOCATIONS C/W ERA 507538-14 (LP 0829134)

Part: SMOKE WARNING — FALSE ACTIVATION (AFT CARGO) · airframe 116,967 hrs · 16,609 cycles

AFT CARGO SMOKE DETECTOR WARNING MESSAGE DURING CRUISE. NO VISIBLE EVIDENCE OR ODOR OF SMOKE. SYSTEM RESET AT AFT CARGO AND WARNING CLEARED. SYSTEM OPS NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 116,656 hrs · 16,569 cycles

EMERGENCY LIGHT AT SEAT 25G IS INOPERATIVE. FOUND FEMALE CONNECTOR DAMAGED. REINSTALLED CONNECTOR AND SECURED HARNESS, MCO/PLACARD REMOVED. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (BS 1654-1678) · airframe 114,856 hrs · 16,329 cycles

DURING INSPECTION OF THE TAIL, SURFACE CRACKS WERE FOUND BETWEEN BS 1654 AND 1678 AT STRINGER 13A, THE CRACKS WERE REPAIRED IAW SRM 53-80-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 114,635 hrs · 16,297 cycles

LLCR EMERGENCY LIGHTS THE BULBS ARE BURNED OUT. REPLACED THE BULBS, SYSTEM OPERATION IS NORMAL.

Part: SIGN — DEGRADED (EMERGENCY LIGHTS) · airframe 114,264 hrs · 16,246 cycles

R1 DOOR EXIT SIGN IN POOR CONDITION. REPLACED THE SIGN.

Part: LIGHT — BURNED (CABIN) · airframe 113,855 hrs · 16,190 cycles

EMERGENCY LIGHTS ALL BURNED. REPLACED THE EMERGENCY LIGHTS.

Part: LINE — DAMAGED (PRESSURE) · airframe 109,755 hrs · 15,656 cycles

DURING TAXI OUT , THE RIGHT ENGINE SHUTDOWN BY ITSELF AFTER BEING STABILIZED AT IDLE. ANOTHER AIRCRAFT REPORTED SMALL TAIL PIPE FIRE AFTER THE ENGINE HAD SHUT DOWN. REPLACED THE RIGHT FCU, INSPECTED INLET AND EXHAUST. SYSTEM OPERATION IS NORMAL. AS FOLLOW UP, FOUND THE BURNER PRESSURE FLEX LINE DAMAGED NEAR THE EEC. REMOVED AND REPLACED THE BURNER PRESSURE FLEX LINE, CHECKS GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 123,586 hrs · 17,589 cycles

WHILE IN FOR A C-CHECK IN ATL, MTC FOUND CRACKS IN THE LOWER INSPAR SKIN OF THE LT WING EXTENDING FROM A FASTENER IN GROUP A COMMON TO STR L-9.5. C/W ER/A 532227-14AD.

Part: SKIN — CRACKED (LT WING) · airframe 123,586 hrs · 17,589 cycles

WHILE IN FOR A C-CHECK IN ATL, MTC FOUND CRACKS IN THE LOWER, INSPAR SKIN OF THE LT WING EXTENDING FROM A FASTENER IN GROUP A COMMON TO STR L-9.5. C/W ERA 532227-14AD.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 117,366 hrs · 16,661 cycles

CRACK WHEEL WELL PRESSURE DECK APPROXIMATE 16" LONG. REPAIR PER SRM 53-50-51 REPAIR 5 AND ERA 552418-14 REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 109,030 hrs · 15,566 cycles

LEFT SIDE CEILING EMERGENCY LIGHTS INOPERATIVE AFT OF ROW 9 AND RIGHT SIDE CEILING EMERGENCY LIGHTS FOR FOR 17-21 ARE INOPERATIVE. REPAIRED BROKEN WIRE AT L321, RESET C/B, CHARGED BATTERIES, REPLACED M9009 BATTERY AND CHARGER. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (WING) · airframe 100,629 hrs · 14,537 cycles

HFEC INSPECTION SHOWS A CRACK INDICATION AT FASTENER HOLE NR 1. FASTENER HOLE HAS BEEN STEPPED UP TO 0.5775 AND CRACK INDICATION REMAINS. REPAIRED FASTNER HOLE IAW 532227-14.

Part: BRAKE — FIRE (NR 8) · airframe 92,904 hrs · 13,546 cycles

AFTER ARRIVAL AT GATE AND RELEASE OF PARKING BRAKE A SMALL FIRE IGNITED ON TOP OF BRAKE NR 8. INSPECTED IAW AMM, REPLACED WHEEL ASSY AND BRAKE. ACFT RETURNED TO SERVICE.

Part: BRAKE — FIRE (LEFT MLG) · airframe 91,391 hrs · 13,341 cycles

RAMP REPORTED NR 5 BRAKE WAS ON FIRE INDICATING SEVEN IN THE FLIGHT DECK. R & R NR 5 BRAKE AND WHEEL ASSY. INSPECTED AXLE AND NO DEFECTS NOTED ACFT WAS THEN RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 91,279 hrs · 13,324 cycles

EMERGENCY LIGHTS AT 17B ARE INOPERATIVE. NO POWER AT WALL MOUNT. MX SECURED PIN IN PLUG. SYS OPS IS NORMAL.

Part: BUSHING — CRACKED (NR 1 PYLON) · airframe 91,128 hrs · 13,306 cycles

NR 1 PYLON STRUT LOWER SPAR FITTING BUSHINGS HAVE SEALANT CRACKED AND BUSHINGS REPLACED IAW SRM 54-53-90, FIG 201.

Part: BUSHING — CRACKED (NR 2 PYLON) · airframe 91,128 hrs · 13,306 cycles

NR 2 PYLON STRUT LOWER SPAR FITTING BUSHINGS HAVE SEALANT CRACKED AND BUSHINGS REPLACED IAW SRM 54-53-90, FIG 201.

Part: FITTING — SCRATCHED (RT WING) · airframe 91,128 hrs · 13,306 cycles

RT WING, UNDERWING SIDE LOAD FITTING OTBD HOLE IS SCRATCHED AND REPAIRED IAW SB 767-54-0069, FIG 3 AND EO 01-074904-03AD REV D.

Part: FLOORBEAM — CORRODED (FS 1197) · airframe 91,128 hrs · 13,306 cycles

AFT CARGO FLOORBEAM AT FS 1197 IS CORRODED AT LBL 18-42 AND RBL 24-48 ON THE UPPER CHORD AND THE CHORD IS REPLACED IAW SRM 51-10-02 AND DWG 146T1206, FRAME 3.

Part: FITTING — DAMAGED (RT WING) · airframe 91,128 hrs · 13,306 cycles

RT WING UPPER PITCH LOAD FITTING INBD TEE CLIP HAS SHORT EDGE MARGIN ON FASTENERS AND HAS BEEN REPLACED IAW ERA 507545-14AD.

Part: BUSHING — CRACKED (NR1 PYLON) · airframe 91,128 hrs · 13,306 cycles

NR 1 PYLON STRUT FWD UPPER SPAR FITTING BUSHING HAS SEALANT CRACKED AROUND BUSHING AND THE BUSHING HAS BEEN REPLACED IAW SRM 54-53-90, FIG 201.

Part: TEE FITTING — DAMAGED (LT WING) · airframe 91,128 hrs · 13,306 cycles

LEFT WING UPPER PITCH LOAD FITTING INBD TEE FITTING HAS SHORT EDGE MARGIN ON FASTENERS AND HAS BEEN REPLACED IAW ERA 507544-14AD, REV ORG.

Part: BUSHING — CRACKED (NR 2 PYLON) · airframe 91,128 hrs · 13,306 cycles

NR 2 PYLON STRUT FWD UPPER SPAR FITTING BUSHINGS HAS SEALANT CRACKED AND HAVE BEEN REPLACED IAW SRM 54-53-90, FIG 201.

Part: SKIN — CRACKED (LT WING) · airframe 91,128 hrs · 13,306 cycles

RT WING AFT PITCH LOAD FITTING FWD TENSION BOLT AREA OTBD HOLE FOUND CRACKED. REPAIRED IAW ERA 507540-14AD, REV ORIG.

Part: SKIN — CRACKED (LT WING) · airframe 91,128 hrs · 13,306 cycles

LT WING AFT PITCH LOAD FITTING FOUND TENSION BOLT HOLE AREA CRACKED AT WING LWR SKIN. FREEZE PLUG REPAIR IAW ERA 507539-14, REVO.

Part: FLOORBEAM — CORRODED (BS 1439) · airframe 91,128 hrs · 13,306 cycles

CABIN RT BS 1439 RBL 94 FLOORBEAM UPPER FLANGE CORRODED. REPAIRED IAW ERA 507543-14 REV0.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 91,128 hrs · 13,306 cycles

LT WING OTBD FLAP L/E FAIRING AREA ADJACENT NR 1 FLAP TRACK INBD FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-07, PARA 5A, FIG 9.

Part: FRAME — CRACKED (BS 903 S21R) · airframe 91,128 hrs · 13,306 cycles

BS 903 FRAME CRACKED AT S21R. REPAIRED IAW ERA 507534-14 REV0.

Part: FAILSAFE — CRACKED (BS 955) · airframe 91,128 hrs · 13,306 cycles

FUSELAGE RT BS 955 REAR SPAR BULKHEAD FAIL-SAFE STRAP FASTENER HOLE CRACKED. REPAIR IAW ERA 507532-14AD, REV 0.

Part: STRINGER — CORRODED (BS 1415 S20L) · airframe 91,128 hrs · 13,306 cycles

BS 1415, S20L UPPER FLANGE OF STRINGER CORRODED. REMOVED AND REWORKED AREA AND SHOT PEENED ACCOMPLISHED IAW ERA 507542-14 REV0.

Part: FRAME — CORRODED (BS 1439) · airframe 91,128 hrs · 13,306 cycles

BS 1439, S16 TO 18L FRAME OTBD FLANGE CORRODED. AREA TRIMMED OUT AND REPAIRED IAW ERA 507547-14 REV 0.

Part: FRAME — CRACKED (BS 903) · airframe 91,128 hrs · 13,306 cycles

BS 903 FRAME CRACKED AT S21L. REPAIRED IAW ERA 507533-14 REV0.

Part: SKIN — CRACKED (RT WING) · airframe 91,128 hrs · 13,306 cycles

RT WING AFT PITCH LOAD FITTING FWD TENSION BOLT AREA INBD HOLE FOUND CRACKED. REPAIRED IAW ERA 507540AD, REV ORIG.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 91,128 hrs · 13,306 cycles

RT WING INBD MAIIN FLAP OTBD L/E AREA FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-05, PARA 5A, FIG 5.

Part: TEE FITTING — DAMAGED (LT WING) · airframe 91,128 hrs · 13,306 cycles

LT WING SIDE LINK FITTING INBD AND OTBD LOWER TEE CLIPS FASTENER HOLES SHORT EDGE MARGIN. REPAIRED IAW ERA 507544-14AD, REV ORIG SECTION I.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 91,128 hrs · 13,306 cycles

RT WING OTBD T/E FLAP LWR SURFACE INBD T/E AREA FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-07, PARA 5A, FIG 9.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 91,128 hrs · 13,306 cycles

LT WING INBD MAIN FLAP OTBD L/E AREA FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-53-01, REPAIR 1, FIG 201 AND SRM 51-70-05, PARA 5A, FIG 5, NRC 5105159.

Part: ACCESS PANEL — DAMAGED (HORIZONTAL STAB) · airframe 91,128 hrs · 13,306 cycles

LT HORIZONTAL STAB L/E ACCESS PANEL 332BL HAS SCREW HOLE ELONGATED. PERFORMED METAL HOT BOND REPAIR PERFORMED IAW PRI 507537-14 AND ERA 507537-14.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 91,128 hrs · 13,306 cycles

LT WING OTBD LOWER SURFACE AT OTBD T/E AREA FOUND DELAMINATED. PERFORMED PREPEG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-07, PARA 5A, FIG 9.

Part: TEE FITTING — DAMAGED (RT WING SPAR) · airframe 91,128 hrs · 13,306 cycles

RT WING SIDE LINK FITTING INBD AND OTBD LWR TEE CLIPS FASTENER HOLES SEM. REPAIRED IAW ERA 507545-14AD, REV ORIG SECTION I.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 91,128 hrs · 13,306 cycles

MAIN DECK BS 287, RBL 14 TO RBL 19 FLOORBEAM UPPER FLANGE CORRODED. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: ACCESS PANEL — DELAMINATED (HORIZONTAL STAB) · airframe 91,128 hrs · 13,306 cycles

LEFT HORIZONTAL STAB L/E ACCESS PANEL 332DL SURFACE DELAMINATED. METAL HOT BOND REPAIR PERFORMED AT DELAMINATED AREA IAW SRM 55-10-01, REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 202.

Part: FITTING — CRACKED (RT WING) · airframe 91,128 hrs · 13,306 cycles

RIGHT WING UPPER LINK PITCH LOAD FITTING AND WING UPPER SKIN PANEL HOLE CRACKED. REPAIRED IAW ERA 507538-14AD, REV ORIG.

Part: ATTACH FITTING — DAMAGED (ESCAPE SLIDE) · airframe 91,128 hrs · 13,306 cycles

DURING INSPECTION TASK OPN 50150, ON RT OVERWING ESCAPE SLIDE FOUND TORQUE TUBE AND ASSOCIATED ATTACH CLAMPS BROKEN OFF OF SLIDE PACK. GENERATED NRC TO REPLACE SLIDE PACK.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 91,128 hrs · 13,306 cycles

NR 2 PYLON PANEL 442AL ACCESS CUTOUT SKIN AND DOUBLER CRACKED. AREA TRIMMED OFF AND REPAIRED IAW ERA 507546-14, REV ORIG.

Part: STRUCTURE — CRACKED (BS 1809.5) · airframe 89,672 hrs · 13,103 cycles

LEFT FWD OUTER CHORD AT BS 1809.5 NEAR THE AFT PRESSURE BULKHEAD WAS FOUND TO HAVE TWO FASTENER HOLES SHOWING CRACKS AND TWO WERE OBLONG. REPAIRS WERE MADE PER ERA 505173-14AD REV ORIG.

Part: TEE FITTING — DAMAGED (RT WING) · airframe 87,089 hrs · 12,763 cycles

RT WING UPPER PITCH LOAD FITTING INBD TEE FITTING HAS SHORT EDGE MARGIN ON FASTENERS AND HAS BEEN REPLACED IAW ERA 507545-14AD, REV ORG NR 52474.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 84,644 hrs · 12,439 cycles

AT CRUISE ALTITUDE CREW REPORTED LT FWD WINDOW HEAT EICAS LIGHT ON OVERHEAD PANEL. SMALL PUFF OF SMOKE OBSERVED NEAR CONNECTION. FOLLOWED QRH, TURNED OFF WINDOW HEAT, SMOKE QUICWINDOW AND RIGHT SIDE WINDOW CONTROLLER AND L1 WINDSHIELD OPERATION IS NORMAL.

Part: SOCKET — DAMAGED (CABIN) · airframe 83,975 hrs · 12,348 cycles

EMERGENCY LIGHTS AT SEAT 24F ARE INOPERATIVE. MAINTENANCE FOUND A DAMAGED SOCKET AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 83,948 hrs · 12,344 cycles

DURING DRC FOUND EMERGENCY EXIT PATH LIGHTS AT SEAT 1B ARE INOPERATIVE. MAINTENANCE FOUND LIGHT HARNESS WAS DISCONNECTED AND RE-SECURED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 83,948 hrs · 12,344 cycles

DURING DRC FOUND EXIT ROW LIGHTS ROWS 1-5 INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER.

Part: CONNECTOR — LOOSE (CABIN) · airframe 83,948 hrs · 12,344 cycles

DURING DRC FOUND EMERGENCY PATH LIGHTS AT SEAT 24F HARNESS CONNECTOR LOOSE. MAINTENANCE RE-SECURED THE WIRING HARNESS. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 81,891 hrs · 12,082 cycles

EMERGENCY PATH LIGHTS AT SEAT 6B ARE OPERATIVE. MX RECONNECTED A LOOSE CONNECTOR. SYS OPS IS NORMAL.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 79,738 hrs · 11,792 cycles

EMERGENCY EXIT LIGHTS AT 30AB, 33AB AND 36AB INOP. REPLACED EMERGENCY LIGHT SOCKET AND REPAIRED WIRING AT 30AB, 33AB AND 36AB. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 79,738 hrs · 11,792 cycles

EXIT EMERGENCY LIGHTS L644, L391, L392, L393 INOP. REPLACED M731 POWER SUPPLY AND BATTERY. EMERGENCY LIGHTS OPS NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 78,480 hrs · 11,627 cycles

CABIN ALT AUTO 1 AND 2 MSG AFTER POWER SWAP. PERFORMED CABIN CONTROLLER BITE CLEARED MSG PERFORMED CHECK GROUND SYSTEM OKAY AS PER AMM. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 77,878 hrs · 11,541 cycles

RTN TO GATE - R GEN DRIVE MESSAGE AND GEN DRIVE DISC R. DRIVE ILLUMINATED TAKING RUNWAY. ALL OTHER END INDICATIONS NORMAL. INSPECTED RT IDG. SERVICED RT IDG PER AMM. SPUN THEN RAN NR 2 ENG AT GATE. NO LEAKS NOTED. ALL ENG PARAMETER NORMAL DURING ENG RUN. SUSPECT SERVICING CONNECTOR O-RING UNSEATED. NO OTHER DEFECTS NOTED. OK FOR SERVICE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WARNING MESSAGE — FALSE ACTIVATION (VALVE) · airframe 76,431 hrs · 11,363 cycles

AFTER ENGINE START FWD EQPT VAL MSG ANNUNCIATED. WHEN AIRCRAFT ARRIVED AT GATE, NO STATUS MSG NO LIGHT ANNUNCIATED CYCLED FROM AUTO TO STANDBY COULD NOT DUPLICATE AIRFLOW NORMAL EXHAUST DOOR OPS NORMAL. OK FOR SVC.

Part: SHUTOFF VALVE — LOCKED (RIGHT) · airframe 75,671 hrs · 11,268 cycles

ON CLIMB-OUT, JFK RT ENG HPSOV EICAS FWD TO MCO/PLAC PER MEL 36-11-02. RT ENG HPSOV LOCKED OUT. JUMPER INSTALLED.

Part: WARNING SYSTEM — INTERMITTENT (TAIL SKID) · airframe 73,470 hrs · 10,996 cycles

TAIL SKID LIGHT INTERMITTANT AT DEPARTURE. PERFORMED CHECK OF TAIL SKID AS PER MEL 32-71-02B OPS OK AT TAIL SKID YELLOW PLACARD INSTALLED PER MEL.

Part: WIRE — DISCONNECTED (PTU) · airframe 70,463 hrs · 10,634 cycles

ON TAXI OUT, EICAS CAUTION L HYD SYS PRESS ILLUMINATED. SELECTED DEMAND PUMP TO ON. LIGHT REMAINED ILLUMINATED. ON ARRIVAL LIGHT EXTINGUISHED. VERIFY LT PUMP WORKS BOTH IN AUTO AND IN ON. SUSPECT INTERMITTENT PRESS SWITCH. FWD TO MCO AND PLAC PER MEL 29-31-01A. ACTIVATED FLT CONTROLS PRESSURE CHKS OK. PTU SIGNAL WIRE HAS BEEN DISCONNECTED AND MUST BE RECONNECTED BEFORE MCO IS CLEARED.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 68,802 hrs · 10,434 cycles

CRACK AT FACTORY CUTOUT ON INBOARD SKIN OF NR 2 PYLON. CRACK WAS STOP DRILLED AND DOUBLERS INSTALLED.

Part: TRANSMITTER — MALFUNCTIONED (NR 2 ENG OIL SYS) · airframe 68,063 hrs · 10,339 cycles

RTB DUE TO RT ENG OIL QTY DROPPED TO 6 AFTER ENG START. FWD OIL QTY INDICATION TO MCO PER MEL 79-31-01. VERIFIED OIL TANK FULL. NO OIL WAS ADDED. REPLACED OIL QUANTITY TRANSMITTER T 675 PER M/M RAN NR 2 ENG PER PFHB OIL TEMP ROSE OIL PRESSURE GOOD AFTER ENG SHUTDOWN CHECKED OIL LEVEL ENG REQUIRED 11 PINTS TO BRING TO FULL MC AND PLACARD REMOVED.

Part: ENGINE — FAILED (APU) · airframe 66,546 hrs · 10,148 cycles

APU HISTORY OF NO START AND NOT ENOUGH AIR FOR MEC. BITE CK OF ECU SHOWS 143 CODE EGT TRIM MODE WILL REQUIRE APU CHANGE. REMOVED AND REPLACED APU. PERFORMED OPS CHECK AND PNEU CHECK, ALL NORMAL.

Part: ACOUSTIC PANEL — DELAMINATED (NR 2 NACELLE) · airframe 66,509 hrs · 10,142 cycles

NR 2 ENGINE AFT ACOUSTIC PANEL AT APPROX 3:30 POSITION IS DELAMINATED. REPAIRED BY REMOVING DELAM AREA AND POTTING AREA IAW B767 - 300 SRM 54-00-01 REPAIR AND FIG 201. WORKED ON N/R20439 DURING HMV IN GSO.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 66,509 hrs · 10,142 cycles

NR 1 PYLON UPPER WEB WHERE WIRE HARNESS RUNS THROUGH, CRACKED 2 PLACES. INSTALLED NEW STIFFENER AND INSTALLED DOUBLERS AND FILLERS PER B767 SRM 54-53-02. ITEM WORKED DURING HMV IN GSO ON N/R CARD 20538.

Part: FLOORBEAM — CORRODED (BS 1483 LBL11-45) · airframe 66,509 hrs · 10,142 cycles

FOUND DURING HMV IN GSO, MAIN CABIN FLOORBEAM HAS CORROSION GS 1483 LBL 1 - LBL 45. REPAIRED FLOORBEAM IAW SRM 53-00-51D FIG 201. WORK ACCOMPLISHED ON N/R 24135.

Part: TORQUE BOX — CRACKED (NR 2 NACELLE) · airframe 66,509 hrs · 10,142 cycles

FOUND DURING HMV AT GSO, NR 2 PYLON NACELLE STRUT MID TORQUE BOX UPPER WEB IS CRACKED. REPAIRED IQW B767 SRM 54-53-02 FIG 201 REPAIR 2.

Part: SKIN — DENTED (BS 1461 S27-28L) · airframe 66,509 hrs · 10,142 cycles

FOUND DURING HMV AT GSO, DENT ON LT LOWER SKIN FS 1461 BETWEEN S27L AND S28L. REPAIRED PER EA 460909-14 REV 1R DATED 3-30-07. PERMANENT CATAGORY A REPAIR, WORKED ON N/R 24044.

Part: ACOUSTIC PANEL — CRACKED (NR 1 NACELLE) · airframe 66,509 hrs · 10,142 cycles

FOUND DURING HMV AT GSO, NR 1 ENG FAN COWL ACOUSTICAL PANEL HAS A CRACK INSIDE OF A DENT AT THE 4 O`CLOCK POSITION JUST FWD OF THE FAN BLADES. REPAIRED BY REMOVING CRACKED AREA AND POTTING AREA IAW B 767 SRM 51-00-01 REPAIR NR 1 ENGINE 201.

Part: FLOOR SUPPORT — WORN (FS 933-1087) · airframe 66,509 hrs · 10,142 cycles

FOUND DURING HMV AT GSO, MAIN CABIN RT SIDE AT STA 933-1087 RBL 33 FLOOR SUPPORT T CAP AND LONGITUDINAL SUPPORT HOLE ELONGATED FASTENER HOLES/ CHAFING AROUND FASTENERS. REMOVED FLOOR SUPPORT FROM STA 999-1087 RBL 33 IAW B767 - 300 SRM 51-40-02. FAB`D AND INSTALLED REPAIR STRAPS IAW B767 SRM 53-00-51 FIG 201 REPAIR 4 AND B767 SRM 51-40-01. FAB'D AND INSTALLED FLOOR SUPPORT AND REPAIR ANGLES IAW B767 SRM 51-70-12 AND 51-40-02. WORKED ON N/R 24143.

Part: PUMP — MALFUNCTIONED (APU) · airframe 66,497 hrs · 10,139 cycles

ON ENG START APU FAULT LIGHT ILLUM AND AUTO S/D ON PUSH BACK. APU ECU FAULTED LOW OIL PRESS SW PREV REPLACED. REPLACED OIL LUBE PUMP AND ECU APU NOW STARTS AND RUNS. ATTEMPTED ENG ST WAS SUCCESSFUL LEAK CHECK OK A/C RTS WITH FULL SERVICE APU PUMP MFG NR 3880190-10.

Part: CONTROLLER — MALFUNCTIONED (NR 1 AND 2) · airframe 65,583 hrs · 10,027 cycles

DURING TAXI OUT, CABIN AUTO INOP MSG CAME ON RETURN TO GATE. PERFORMED BITE ON CABIN PRESS CONTROLLERS 1 AND 2 NO FAULT BITE MESSAGE DISAPPEARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,630 hrs · 9,672 cycles

SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOP. RELAMPED, OPS OK NOW.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 62,519 hrs · 9,660 cycles

TRIED TO RESET APU AFTER PUSHBACK AND GOT APU DOOR EICAS MSG AND APU FAULT. SUBSEQUENT APU DOOR STATUS MSG WOULD NOT CLEAR AND APU WOULD NOT START. CYCLED APU INLET ACTUATOR C/B. STARTED AND SHUTDOWN APU SUCCESSFUL. APU ECU TESTS OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,346 hrs · 9,639 cycles

EXTERIOR EMERGENCY EXIT LIGHTS LT SIDE JUST AFT OF OVERWING EXITS CENTER DOUBLE LIGHT ASSY FWD BULB INOP. ALSO SINGLE LIGHT ASSY JUST AFT OF WING INOP. RELAMPED 2 LT SIDE EXTERIOR EMERGENCY LIGHT. LIGHTS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,346 hrs · 9,639 cycles

EMERGENCY ESCAPE PATH LIGHTS ATA SEATS 38AB AND 34FG INOP. RELAMPED 38AB OPS OK. RELAMPED 34FG NO HELP. FOUND WIRE PULLED OUT FROM CONNECTOR UNDER SEAT. REATTACHED CONNECTOR CKS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,346 hrs · 9,639 cycles

EMERGENCY ESCAPE PATH LIGHTS INOP AND COVER MISSING AT SEAT 3AB AFT ASSY, 4AB FWD ASSY, 5AB AFT ASSY. RELAMED ALL SEATS AND REPLACED COVERS, OPS CK NML 3AB 4AB AND 5AB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,346 hrs · 9,639 cycles

EXTERIOR EMERGENCY EXIT LIGHT RT SIDE JUST ABOVE FLAP LAST DOUBLE LIGHT ASSY FWD BULB INOP.

Part: STARTER — UNSERVICEABLE (NR 2 ENGINE) · airframe 62,261 hrs · 9,628 cycles

DURING RIGHT ENG START N2 INCREASED NORMALLY TO APPROX 18 PERCENT N2 ALL INDICATIONS WERE NORMAL UNTIL 18 PERCENT N2 WHEN START VALVE LIGHT ILLUM AND N2 BEGAN TO DECAY. OCCURRED DURING BOTH APU AND CROSSBLEED START ATTEMPTS. REPLACED RT ENG STARTER PER M/M CHKS GOOD.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 60,127 hrs · 9,357 cycles

THE NR 2 PYLON MID SPAR CLOSEOUT ANGLE WAS FOUND CRACKED. MID SPAR FITTING WAS INSPECTED AND CLOSEOUT ANGLE REPLACED PER ER/A 451663-14AD, REF AD 2005-19-23, 01-074944-12AD.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 60,127 hrs · 9,357 cycles

THE NR 1 PYLON MID SPAR FITTING CLOSEOUT ANGLES WAS FOUND CRACKED. THE MID SPAR FITTINGS WERE INSPECTED AND THE CLOSEOUT ANGLES WERE REPLACED, REF AD 2005-19-23, 01-074944-12AD.

Part: ALTIMETER — INOPERATIVE (COCKPIT) · airframe 59,454 hrs · 9,253 cycles

RTB, DUE CAPT ALT INDICATOR FLAG IN VIEW. AFTER POWER RESET FLAG RETRACTED AND IND OK. AFTER TAKEOFF BRU, CAPT ALTIMETER FLAG IN VIEW FLT DIV TO FRA FOR REPAIRS. FRA MTC REPLACED THE CAPT ALTIMETER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,642 hrs · 9,139 cycles

EMERGENCY LIGHT INOP LOCATED LT FUSELAGE AFT OF T/E OF LT WING, RELAMPED.

Part: TIRE — FAILED (MLG) · airframe 58,406 hrs · 9,106 cycles

MLG TIRE RECAP FAILED. FOUND DAMAGE TO NR 1 AND NR 5 MLG TIRES. REMOVED AND REPLACED NR 1 AND NR 5 WHEEL ASSYS. LEFT I/B AFT FLAP DAMAGE FROM NR 1 MAIN TIRE FOD. REPAIRED DAMAGE PER ERA 099530-14.

Part: SEAT — SPARKS (COCKPIT) · airframe 57,466 hrs · 8,977 cycles

F/O SEAT ADJUST INOP ELEC BURNING SMELL NOTED. REPLACED SEAT ASSY.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 56,331 hrs · 8,812 cycles

ON TAKEOFF ROLL APPROX 95 KNOTS, LT ENG HPSOV EICAS MESSAGE ILLUMINATED. AFTER AIRBORNE DID QRH PROCEDURES TALK WITH MX AND RETURNED TO JFK. REPLACED HPSOV.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 55,150 hrs · 8,649 cycles

DID NOT PRESSURIZE DURING CLIMBOUT WITH EQUIP COOLING OVERHEAT MESSAGE. QRH PROCEDURE PERFORMED. CABIN OUTFLOW VALVE FULLY CLOSED. DIFF PRESS .08 MAX. C.A.T HAD FWD DK SUP FLOW AND FWD EQU SUP FLOW EICAS MSG. FOUND OVERBOARD EXHAUST VALVE NOT LOCKED CLOSED OVERCENTER AFTER EXTENSIVE T/S PER FIM 21-58-00. PRESSURIZED AIRCRAFT WITH APU AIR 3 LBS POSITIVE. NO LEAKS FOUND. OUTFLOW VALVE OPN NORMAL IN STDBY AND AUTO 1 AND AUTO 2. EXHAUST VALVE IS ON MCO/PLACARD PER MEL 21-58-01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,156 hrs · 8,355 cycles

EMERGENCY SEAT LIGHTING ROWS 1-5 WILL NOT TEST. FOUND M90003 POWER SUPPLY AND BATTERY BAD. REPLACED BOTH, OPS CHECKS NORMAL.

Part: SEAT — MALFUNCTIONED (COCKPIT) · airframe 50,141 hrs · 7,923 cycles

DURING OPERATION OF CAPT SEAT WHEN REACHING THE AFT MOST POSITION THE ELEC SWITCH REMAINED ON AND THE MOTOR EMITTED AN ELEC SMELL AND THE P6 CB POPPED. THE SEAT COULD NOT BE MOVED MANUALLY AND REMAINS IN THE AFT POSITION. REMOVED AND REPLACED CAPTS SEAT. OPS CHECK GOOD.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 48,297 hrs · 7,640 cycles

APPROX 3 HRS INTO FLT F/A REPORTED STRONG ODOR IN AFT GALLEY. ODOR WAS STRONGEST IN VICINITY OF CAPT SIDE LAVATORY/ AISLE AIR VENTS. ODOR WAS ELECTRICAL IN NATURE AND DISSIPATED AFTER 10 MIN. FOUND CEILING LIGHT BALLAST AT 41A, B OVERHEAD INOP AND WITH STRONG ODOR. REPLACED BALLAST AT 41 A, B. CHECKS GOOD NO MORE ODOR,

Part: PHONE — INTERMITTENT (CABIN) · airframe 42,348 hrs · 6,571 cycles

INBOARD FLT ATTENDANT REPORTED HOT ELECT SMELL IN AREA OVERHEAD SEATS 3AB AND 4AB. PERFORMED THOROUGH INSPECTION OF FWD CABIN AREA. UNABLE TO DUPLICATE ANY ELECT SMELLS. SUSPECT POSSIBLE AIR PHONE PROBLEM DUE INTERMITTENT AT TIME OF REPORT. DEACTIVATED AIR PHONE SYS BY PULLING C/B.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 41,624 hrs · 6,430 cycles

SEAT 1-5AB EMERGENCY INOP. REPLACED POWER SUPPLY, OPS CHECK GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 40,466 hrs · 6,255 cycles

ON T/O FROM BRU REPORTED SMOKE IN CABIN.CLEARED AFTER 15 MINUTES OF FLT.ATL MTC FOUND OIL LEAKING FROM SPINNER. REPLACED ENGINE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 40,322 hrs · 6,235 cycles

HEARD A THUMP ON RIGHT SIDE DURING APPROACH. PASSENGER ON RIGHT SIDE SAW A FLASH OF LIGHT AT THE SAME TIME. NO ABNORMAL ENGINE INDICATIONS, BUT SUSPECT SMALL COMPRESSOR STALL. REMOVED AND REPLACED RIGHT ENGINE PER ROUTINE CARD DECK 1-27.

Part: FAN — OVERHEATED (E/E BAY) · airframe 38,735 hrs · 5,986 cycles

AFTER APPROX 5 HRS FLT TIME AT FL 310 NOTICED VERY FAINT ELECTRICAL SMELL. 5 MINS LATER L REC FAN EICAS MSG AND INOP LT IN LT RECIRC FAN SW CAME ON CB DNOT POP. CA - FOUND CB BOPPED ON CB PANEL IN MEC RMVD AND REPLD LT RECIFAN OPS CK GOOD ALL CBS RESET.

Part: SWITCH — FAILED (LIGHTS) · airframe 36,887 hrs · 5,673 cycles

DURING EMERGENCY LIGHT CHECK OUT PER LAYOVER, FOUND EMERGENCY LIGHTS ON WITH COCKPIT SWITCH IN THE OFF POSITION. REPLACED FWD FLIGHT ATTENDANT''S EMERGENCY LIGHT SWITCH. EMERGENCY LIGHTS CHECK NORMAL.

Part: CHARGER — FAILED (E/E BAY) · airframe 35,848 hrs · 5,517 cycles

MAIN BATTERY CHARGE STATUS MSG INFLT. REPLACED ACFT MAIN BATTERY AND BATTERY CHARGER. PERFORMED MSG RESET. CHECK BATTERY VOLTAGE. CHECK OK.

Part: ENGINE — STALLED (RIGHT)

FLT 47 ARN/JFK AIR TURNBACK, DUE RT ENG STALLED TWICE ON ROTATION A/C LANDED HEAVY. FUEL WAS NOT DUMPED. RT FWD BRAKE OVERHEATED AND HAD A SMALL FIRE. FIRE WENT OUT BY ITSELF WITH NO DAMAGE TIRES DID NOT DEFLATE. RT ENG EGT WENT TO 758 FOR 17 SECS. ENG CHANGE WAS CALLED. ETOPS CATEGORY 'C': UNCOMMANDED PWR CHANGES,SURGES,OR STALLS

Part: SENSOR — MALFUNCTIONED (RT BLEED AIR)

EICAS MESS RT ENG BLEED OFF AND RT BLEED OVERHEAT OFF. LANDED JFK FOR MTC. FOUND FAN AIR VALVE TEMP SENSOR AT FAULT. LOCKED FAN AIR VLV INTO INTERMEDIATE POSTION AND FWD TO MCO PER MEL 36-12-02A. REPLACED FAN AIR SENSOR AND OPS CHECKED IN VIE. SYSTEM CHECKS NORMAL, REMOVED MCO.

Part: WATER VALVE — LEAKING (AFT LAVATORY)

WATER LEAK IN AFT LEFT LAV 3 WATER VALVES WERE CLOSED. REPLACED TOILET ASSEMBLY, SYSTEM CHECKS GOOD.

Part: ENGINE — FAILED (NR 1)

LEFT ENGINE STALLED AT CRUISE, ENGINE WAS SHUTDOWN. A/C MADE AN UNSCHEDULED LANDING IN YYR. NR 1 ENGINE CHANGE.

Part: FAN — DAMAGED (NR 1 ENGINE)

DURING LAYOVER, ENGINE FAN BLADES WERE FOUND WITH FOD EROSION DAMAGE. BORESCOPED ENGINE, NO DAMAGE FOUND. REPLACED ENGINE FAN BLADE SET.

Part: FAN — DAMAGED (NR 2 ENGINE)

DURING LAYOVER, FOUND NR 2 ENGINE WAS FOUND WITH FOD EROSION DAMAGE TO FAN BLADES. BORESCOPED ENGINE, NO DAMAGE FOUND. REPLACED ENGINE FAN BLADE SET.

Part: ENGINE — MALFUNCTIONED (NR 2)

NR 2 ENG CHANGE DUE TO HIGH OIL CONSUMPTION.

Part: WIRE — BROKEN (AIL LOCK ACT)

AILERON LOCKOUT MSG ON EICAS, DIVERTED CVG. FOUND BROKEN WIRE ON CANNON PLUG FOR RT AILERON LOCK ACTUATOR. REPAIRED WIRE, OPERATION NORMAL.

Part: EEL BULB — FAILED (CABIN)

DURING S/C, FOUND 2 LAMPS INOP AT FWD CROSS AISLE PATH LIGHT. RELAMPED, OPERATION NORMAL.

Part: ACTUATOR — LEAKING (YAW DAMPER)

DURING CRUISE, HAD LEFT HYDRAULIC QUANTITY EICAS MSSG WITH ASSOCIATED LEFT HYD RSVR LIGHT. RETURNED JFK, FOUND LEFT YAW DAMPENER ACTUATOR LEAKING. REPLACED ACTUATOR, OPERATION NORMAL.