N751AT

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 94,318 hrs · 40,078 cycles

AIRCRAFT 6901, SEAT 21R AND 27R ESCAPE LIGHT INOPERATIVE. FOUND CONNECTORS LOOSE ON BOTH SEAT HARNESSES. SECURED CONNECTORS, OPS OK.

Part: LIGHT — INOPERATIVE (SEAT 21) · airframe 93,960 hrs · 39,993 cycles

EMERGENCY LIGHT AT SEAT 21 RT, INOPERATIVE. R & R EMERGENCY LIGHT ASSY AT SEAT 21R. OPS CHECKED GOOD. OK FOR SERVICE.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,071 hrs · 39,723 cycles

ROW 37 SEAT MOUNTED EMERGENCY LIGHT LIGHT MODULE DAMAGED AND INOPERATIVE. R & R ROW 37 SEAT EMERGENCY LIGHT MODULE IAW AMM 33-51. OPS CHECK GOOD.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,071 hrs · 39,723 cycles

EMERGENCY ESCAPE PATH LIGHTS ON SEAT 36 ON BACK, AFT, INOPERATIVE R & R EMERGENCY LIGHT HARNESS AT SEAT 40 DEF IAW MM 20-10.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 92,966 hrs · 39,684 cycles

SEAT 36 RIGHT AND AFT EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT IAW WDM 33-51-21. FOUND CONNECTOR D9016 DAMAGED. REPAIRED CONNECTOR IAW SPWM 20-60. REPLACED BATTERY CHARGER. EMEGENCY LIGHTS CHECKED NORMAL IAW AMM 33-51.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,821 hrs · 39,132 cycles

DURING A CHECK, FOUND EMERGENCY LIGHTS AT ROWS 1-25 INOPERATIVE. R & R POWER SUPPLY AMM 33-51. OPS CHECKED NORMAL.

Part: STRUCTURE — CORRODED (L4 DOOR SEAL) · corrosion level 2 · airframe 89,532 hrs · 38,802 cycles

FOUND CORROSION ON L4 DOOR UPPER RT SEAL AREA. COMPLIED WITH PRI 526064-14 REV '0'. LEAK CHECKED DOOR TO 3 PSI. ALL PRI INSPECTIONS COMPLIED WITH IAW PRI 526064-14 REV 0, 1 AND 2. COMPLIED WITH SECTION I TIME-LIMITED REPAIR PER ER/A 526064-14 REV ORIGINAL.

Part: SKIN — CORRODED (BS 900) · corrosion level 2 · airframe 88,787 hrs · 38,616 cycles

DURING NR 5 -L2 CHECK, MAINTENANCE FOUND EVIDENCE OF CORROSION AT THE LT FRONT SPAR FRAME AT THE BS 900, SKIN SPLICE. DAMAGE IS LOCATED JUST BELOW THE WINDOW BELT BETWEEN S14-15L. REPAIRED IAW ERA 523726-14, REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,066 hrs · 37,916 cycles

EMEREGENCY LIGHT AT 35D IS INOPERATIVE.

Part: RESERVOIR — DISCHARGED (R4 DOOR) · airframe 85,536 hrs · 37,779 cycles

DURING DOOR SLIDE DOOR EMERGENCY POWER RESERVOIR DEPLETED. R & R R4 DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-11-30. RII COMPLETED.

Part: LIGHT — INOPERATIVE (SEAT 38 DEF) · airframe 85,191 hrs · 37,695 cycles

SEAT 38 DEF EMERGENCY WHITE LIGHT INOPERATIVE. R & R PAX SEAT 38DEF WHITE EMERGENCY LIGHT IAW AMM 33-51, OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 84,890 hrs · 37,617 cycles

MX FOUND EMERGENCY LIGHT INOPERATIVE A ROW 36. MX CONNECTED PATH LIGHT AT ROW 36. OPS OF LIGHT NOW CHECK OK.

Part: BOTTLE — EMPTY (L4 DOOR SLIDE) · airframe 81,652 hrs · 36,808 cycles

DURING LAYOVER MAINTENANCE FOUND L4 DOOR SLIDE BOTTLE IN THE RED. MAINTENANCE REPLACED DOOR SLIDE PER OPN 7809. INSPECTION ITEM COMPLETED QC2009.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 81,501 hrs · 36,768 cycles

DURING MAINTENANCE CHECK FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 1-25. MAINTENANCE REPAIRED SHORTED WIRE BETWEEN SEAT 5C AND 6C. OPERATION OF LIGHTS NOW CHECK OK.

Part: FRAME — DAMAGED (FUSELUGE) · airframe 80,656 hrs · 36,546 cycles

WHILE ACCOMP OPN 50321AD SEVERAL FASTENER HOLES WERE OVERSIZED AND 1/8 BLIND FASTENERS WERE PREVIOUSLY INSTALLED IN C-1 AFT FRAME (FS 620) COMMON SEAL RETAINER. REPAIRED PER ERA 501847-14AD REV ORIGINAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,656 hrs · 36,546 cycles

WHILE ACCOMPLISHING ERA 501847-14, A CRACK INDICATION WAS FOUND IN THE 143N3420-4 SKIN AT A FASTENER HOLE COMMON TO THE STA 620 CARGO DOOR AFT FRAME ABOVE STR 25R. THE DISCREPANT HOLE WAS STEPPED UP TO .215" IN THE SKIN, BEAR STRAP AND OTHER FRAME CORD. C/W ERA 502160-14AD.

Part: FRAME — DAMAGED (CARGO BAY) · airframe 80,656 hrs · 36,546 cycles

WHILE ACCOMPLISHING OPN 50321AD, MTC FOUND THAT SEVERAL FASTENER HOLES WHERE OVERSIZED AND 1/8 BLIND FASTENERS WERE PREVIOUSLY INSTALLED. THESE FASTENERS ARE BEYOND THE REQUIREMENTS OF AD 2002-24-02. ACCOMPLISHED PERMANENT REPAIR PER ERA 501775-14 REV 2 TO RETURN AIRCRAFT TO AD CONDITION.

Part: PIN — LOOSE (LIGHT SOCKET) · airframe 80,153 hrs · 36,415 cycles

LINE MAINTENANCE FOUND EMERGENCY PATH LIGHTING INOPERATIVE AT SEAT 24D. LOOSE PIN IN LIGHT SOCKET RE-SEATED. LIGHT OPERATION NORMAL.

Part: LANYARD — TORN (EVAC SLIDE) · airframe 79,273 hrs · 36,207 cycles

BY MAINTENANCE FOUND 4L SLIDE LANYARD TORN REMOVED AND REPLACED 4L SLIDE ASSEMBLY. INSPECTED PER OPN 7809. NO ISSUES NOTED. SAFETY PINS REMOVED AND STOWED. LANYARD WAS UNDER GIRT BAR. NO HISTORY. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

WHILE PERFORMING PRI 485379-14AD REV 1 FOUND 1 EA ELONGATD HOLE ON STR 17L STA 627 AND 1 EA HOLE OVERSIZED ON STR 17L STA 630. COMPLIED WITH ERA 486176-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 170978 (DL75E102745).

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

(UNIQUE CONTROL NUMBER SUPPLEMENTAL INFORMATION) WHILE PERFORMING PRI 485379-14AD REV 1 FOUND 1 EA ELONGATD HOLE ON STR 17L STA 627 AND 1 EA HOLE OVERSIZED ON STR 17L STA 630. COMPLIED WITH ERA 486176-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 170978 (DL75E102745).

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

AFTER FRAME REMOVED FROM AFT CARGO COMP FOUND SHEAR TIE AND ATTACH BRACKET WITH ELONGATED HOLE, STA 1420 AND I/B OF DOOR LOWER SILL. REMOVED AND REPLACED SHEAR TIE AND BRACKET DURING HMV AT ST AEROSPACE ON NON ROUTINE CARD 169189. (DL75E102750)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

WHILE WORKING FLOORBEAM STA 365 IN MAIN CABIN PERFORMING PRI FOUND FRAME CUT AT STA 365 BELOW FLOOR AT STR 17 DUE TO PREVIOUS REPAIR. COMPLIED WITH ERO 485381-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 169190 (DL75E102742).

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

UPON WORKING N/R 171032 FOUND VHF ANTENNA MOUNT STRUCTURE CORRODED BETWEEN FS 1460 TO 1480, STR 29R - STR 30. REMOVED AND REPLACED DOUBLER AND TRIPLER AT ANTENNA MOUNT LOCATION AT ST AEROSPACE SAT ON NON ROUTINE 169182. (DL75E102731)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFTER INTERCOSTAL REMOVED TO FOM FOUND IT CORRODED THRU OUT, RBL 23, STA 1540-1560. REMOVED, FABRICATED AND RE-INSTALLED INTERCOSTAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 169186 (DL75E102783).

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

UPON REMOVAL OF CORR ON STRINGER 29L STA 1407 FOUND ON MACHINE STR 29L (KEEL) AT STA 1410 APPROX. COMPLIED WITH ER/A 485747-14 REV ORIGINAL AT ST AEROSPACE SAT REF NON ROUTINE 170853 (DL75E102733).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

SEAT TRACK GOUGE AND CORRODED BETWEEN STA 1180-1320 AND RBL 45 THROUGHOUT. REMOVED DAMAGED SEAT TRACK, FABRICATED AND INSTALLED DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 171169 (DL75E102824).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

SEAT TRACK CORRODED THRU OUT STA STA 700-780 RBL 24.7. REMOVED AND REPLACED DAMAGED SEAT TRACK DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 179230. (DL75E102818)

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

EMPENNAGE EXTERNAL DENT STA 1720-1743.85 S16R-17R DENT IS OVAL 9.0L 4.0W AT WIDEST POINT. COMPLIED WITH ERA 485744-14 REV ORIG DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 167265 (DL75E102785).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO FRAME CORRODED STA 1600 STR 29R-30. COMPLED WITH ERA 486174-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 171047 (DL75E102749).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO FRAME CORRODED STA 1480 STR 26L-26R. REMOVED AND REPLACED FRAME, STIFFENERS, FAIL SAFE CHORD AT STA AEROSPACE SAT ON NON ROUTINE CARD 171030 (DL75E102736).

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

LT WING TO BODY STA 760 TO 780 LBL 24 TO BL 0, FAIRING LANDING HAS CORROSION. COMPLIED WITH ERA 485728-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 167278 (DL75E102739).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1600-1620 BETWEEN STR 29L & 30. REMOVED, FABRICATED NEW AND INSTALLED INTERCOSTAL DURING HMV AT STA AEROSPACE SAT ON NON ROUTINE CARD 171049. (DL75E102822)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1600-1620 BETWEEN STR 29R & 30. REMOVED, FABRICATED NEW INTERCOSTAL AND INSTALLED DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 171048 (DL75E102815).

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO SHEAR TIE CORRODED STA 1640 BETWEEN STR 22 & 23 RT. REMOVED AND REPLACED SHEAR TIE AT STA AEROSPACE SAT ON NON ROUTINE CARD 171052. (DL75E102735)

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO STRINGER SPLICE CORRODED STA 1452-1466 STR 28L. REMOVED AND REPLACE AFT CARGO STRINGER SPLICE DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 168395 (DL75E102783).

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO STRINGER CORRODED SA 1407 STR 29L. REMOVED AND REPLACED STRINGER 29L DURING HMV AT ST AEROSPACE SAT ON NON ROTINE CARD 178896. (DL75E102781)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO FRAME CORRODED STA 1520 STR 26L-26R. REPAIRED CARGO FRAME DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 171039 (DL75E102748).

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

AFT CARGO STRINGER AND STRINGER CLIP CORRODED STA 1390-1400 STR 28R STRINGER DOES NOT CONFORM TO DWG DIMENSIONAL REQUIREMENTS, DRAWN DOWN (CLECO) HAS GAPS AT FS 1400 & 1440 STRAPS & IS NOT SYMMETRICAL DOES NOT ALIGN WITH AIRCRAFT CENTERLINE. REMOVED AND REPLACED STRINGER DURING HMV AT ST AEROSPACE ON NON ROUTINE CARD 178893 (DL75E102751).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

FLOORBEAM HAS UPPER FLANGE CORRODED AT STA 365 BETWEEN RBL 1 AND RBL 16 INCLUDING LBL 24. COMPLIED WITH ERA 485737-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 179222 (DL75E102743).

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO SHEAR TIE CORRODED STA 1480 BETWEEN STR 29R & 30. REMOVED AND REPLACED DAMAGED SHEAR TIE DURING HMV AT ST AEROSPACE ON NON ROUTINE CARD 171032 (DL75E102828).

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

SKIN CRACKED AND PULLING THROUGH AROUND TCAS ANTENNA MOUNT FASTENERS BETWEEN STA 418-440 FROM S-1 TO S-2R. COMPLIED WITH ER/A 485734-14 REV ORIG AT ST AEROSPACE SAT ON NON ROUTINE CARD 179218 (DL75E102729).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO INTERCOSTAL CORRODED ON WEB AND LOWER LEG STA 1460-1480 I/B OF STR 28R. REMOVED AND REPLACED INTERCOSTAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 171028. (DL75E102740)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO INTERCOSTAL CORRODED ON LOWER LEG STA 1400-1420 BETWEEN STR 29L & 30. REMOVED AND REPLACED INTERCOSTAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 178900 (DL75E102755).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1300-1320 O/B STR 28L. REMOVED AND REPLACED INTERCOSTAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 178882 (DL75E102826).

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

AFT CARGO STR 28L CORRODED STA 1480-1520. REMOVED AND REPLACED STRINGER 28L SECTION FROM STA 1479-1550 AT ST AEROSPACE SAT ON NON ROUTINE 171033 (DL75E102732).

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

UPON REMOVAL OF LT WING UPPER FIXED T/E PNL 551 FOUND CORROSION ON REAR SPAR UPPER CAP AFT SIDE BETWEEN WBL 79 TO WBL 130. COMPLIED WITH ERA 485384-14 REV ORIGINAL AT ST AEROSPACE SAT ON NON ROUTINE CARD 167257. (DL75E102737)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1420-1440 BETWEEN STR 28 & 29L. REMOVED AND REPLACED INTERCOSTAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 168383 (DL75E102752).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

FLOORBEAM HAS UPPER CAP CORRODED AT STA 1640 BETWEEN BL 0 AND LBL 20 INCLUDING AREA AT LBL 58. REPAIRED UPPER FLOORBEAM DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 179150 (DL75E102738).

Part: SKIN — DENTED (LE SLAT) · airframe 74,661 hrs · 35,018 cycles

NR 9 SLAT OSS 617 L/E UPPER SURFACE HAS A DENT. COMPLIED WITH ER/A 485746-14 REV B AT ST AEROSPACE SAT ON NON ROUTINE CARD 178931 (DL75E102730).

Part: CHANNEL — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

LT AFT EMERGENCY EXIT HATCH LWR INNER SKIN NUT PLATE CHANNEL HAS CORROSION. REMOVED AND REPLACED NUT PLATE CHANNEL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 179025 (DL75E102838).

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 74,661 hrs · 35,018 cycles

FUSELAGE EXTERNAL FS 1500-1520 S28L-29L AIR PHONE ANTENNA ATTACH POINT HAS CORROSION PITTING AND SCRIBE MARKS. COMPLIED WITH ERA 485373-14 REV A DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 178912. (DL75E102754)

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

LOWER EXTERIOR FUSELAGE AT APPROX 660 STRINGER 17L SKIN SURFACE HAS 1EA DENT. COMPLIED WITH ERA 485383-14 REV ORIGINAL DURING HMV AT ST AEROSPACE ON NON ROUTINE CARD 168279 (DL75E102744).

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

DENT AT APPROX STA 700 BELOW R2 DOOR BETWEEN STR 20 & 21R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 178739 (DL75E102784).

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

DENT ON EXTERNAL FUSELAGE SKIN STA 1558 BELOW S26R. COMPLIED WITH ERA 485378-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 169337 (DL75E102746).

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

FUSELAGE DENTED STA 1710 BELOW STR 15L. WORK ACCOMPLISHED ON NON ROUTINE CARD 168309 AND ERA 485738-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT REF NON ROUTINE 168312 (DL75E102756).

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

DENT ON EXTERNAL FUSELAGE SKIN AT STA 1562 ABOVE 25L. REMOVED DAMAGE AND INSTALLED REPAIR DURING HMV AT ST AEROSPACE ON NON ROUTINE CARD 169340. (DL75E102787)

Part: SKIN — BUCKLED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

FUSELAGE SKIN BUCKLED BETWEEN STA 1700 & 1720 BETWEEN STR 12 & 13 LT, COMPLIED WITH ERA 485366-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 168313(DL75E102763)

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

EXTERIOR FUSELAGE AT APPROX STA 630 STRINGER 17L SKIN SURFACE HAS 2 EA DENTS. COMPLIED WITH ERA 485379-14 REV A DURING HMV AT STA AEROSPACE SAT ON NON ROUTINE CARD 168280. (DL75E102741)

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

FUSELAGE DENTED AFT OF L4 DOOR BETWEEN STR 14&15L STA 1690. ALL WORK ACCOMPLISHED ON NRC 168309 AND ERA 485738-14 REV ORIGINAL DURING HMV AT ST AEROSPACE REF NON ROUTINE CARD 168310 (DL75E102757).

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 38,018 cycles

LOWER EXTERIOR FUSELAGE AT APPROX STA 1620 BETWEEN STRINGER 17L-18L FUSELAGE SKIN HAS 2 EA DENTS. ACCOMPLISHED ERA 485374-14 REV 1 DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 168278. (DL75E102771)

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

EXTERIOR FUSELAGE AT APPROX STA 600 STRINGER 17L SKIN SURFACE HAS 2 EA DENTS. COMPLIED WITH ERA 485379-14 REV A DURING HMV AT ST AEROSPACE ON NON ROUTINE CARD 168281.

Part: SKIN — DENTED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

EXTERIOR FUSELAGE AT APPROX 540-560 STRINGER 18L SKIN SURFACE PREVIOUSLY INDENTIFIED DENTS (2EA) ID TAG HAVE BEEN PAINTED OVER. REMOVED AND REPLACED DOUBLER DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 168283. (DL75E102786)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,661 hrs · 35,018 cycles

FUSELAGE SKIN SCRAPED AND DENTED STA 1704 FROM BELOW STR 16L TO BELOW STR 15L. COMPLIED WITH ERA 485738-14 REV ORIG AT ST AEROSPACE SAT ON NON ROUTINE CARD 168309. (DL75E102734)

Part: UNKNOWN — DAMAGED (DOOR) · airframe 74,661 hrs · 35,018 cycles

ACCOMPLISH PERM REPAIR PER ERA 473400-14, REV ORIG, CODE 6-52-11 ACTL 2300 "PSGR DOOR L1, R1 R2, L4, R4 CAM PLATES ALTERNATE FINISH" (REF OMI LOG W/CN C03039056). COMPLIED WITH ERA 473400-14 REV A DURING HMV AT ST AEROSPACE SAT ON NON ROUTINE CARD 174891(DL75E102823).

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,807 hrs · 34,316 cycles

ACCOMPLISHED THIS ERA 477691-14 REV A TO REPAIR AREA OF CORROSION ALONG LOWER SKIN JUST BELOW LAP SPLICE AT STR 14L BETWEEN FS 1290-1459.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,807 hrs · 34,316 cycles

ACCOMPLISHED THIS ERA 477740-14 REV A TO REPAIR AREA OF CORROSION ALONG LOWER SKIN JUST BELOW LAP SPLICE AT STR 14L BETWEEN FS 1459-1621.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,807 hrs · 34,316 cycles

ACCOMPLISHED THIS ERA 477689-14 REV A TO REPAIR AREA OF CORROSION ALONG LOWER SKIN JUST BELOW LAP SPLICE AT STR 14R BETWEEN FS 1459-1621.

Part: SKIN — GOUGED (FUSELAGE) · airframe 71,807 hrs · 34,316 cycles

ACCOMPLISHED ERA-477621-14- REV 1 TO REPAIR A SKIN GOUGE AT S-14R LAP JOINT STA 660. LOWER SKIN WAS GOUGED AND HAD PITTING CORROSION.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,807 hrs · 34,316 cycles

ACCOMPLISHING THIS ERA (477585-14) TO REPAIR A SKIN CUTOUT. C/W PER ERA (477391-14) AT S-19L / STA 660. SAMPLE CUTOUT WAS TAKEN DUE TO FINDINGS OF PITTING CORROSION ALONG THE LOWER SKIN AT THE LAP JOINT WHILE ACCOMPLISHING SCRIBE LINE INSPECTIONS.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,807 hrs · 34,316 cycles

ACCOMPLISHED THIS ERA (477583-14) TO REPAIR A DENT AT S-19L/ STA 609. PITTING CORROSION WAS ALSO FOUND ALONG THE LOWER SKIN AT THE LAP NEAR THE DENT.

Part: FUSE — LEAKING (BRAKE MANIFOLD) · airframe 71,032 hrs · 34,118 cycles

AFTER STARTING RT ENGINE COMPLETE HYD SYSTEM FAIL. FLUID DUMPED OUT ON TAXI WAY CURRENTLY SHOWS .25RF. FOUND UPPER BRAKE MANIFOLD FUSE LEAKING. REPLACED WITH BORROWED PART FROM CAL PER AMM 32-42-03-44-030 REF IPC 32-42-02-01.

Part: ENGINE — INOPERATIVE (APU) · airframe 68,419 hrs · 33,423 cycles

ATTEMPTED 3 APU STARTS AT FL 370, APU WOULD NOT START, DISPLAYED APU FAULT EICAS MSG AFTER EACH ATTEMPT, APU STARTED OK ON GRND. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 68,156 hrs · 33,339 cycles

ON TAXI OUT BOTH CABIN MODE ALT SELECTS AUTO INOP. RTB. BOTH SHOWED AC MOTOR RESET RAN VERIFY CKS GOOD MSG ERASED, NO HISTORY.

Part: TIRE — CUT (MLG) · airframe 66,613 hrs · 32,884 cycles

NR 8 MLG TIRE HAS DEEP CUT. REPLACED NR 8 MLG WHEEL ASSY PER AMM.

Part: LIGHT — SHORTED (CABIN 19DEF) · airframe 60,689 hrs · 30,623 cycles

EMERGENCY LIGHT INOP RT MID CABIN. FOUND SHORTED LIGHT ASSY AT SEAT 19 DEF OVERHEAD. EMERGENCY EXIT SIGN OPS NORMAL. FWD LIGHT ASSY AT 19DEF TO MCO/PLAC MEL 33-51-01. COVER REPLACED.

Part: SKIN — DENTED (BS 600-630 S17L) · airframe 58,639 hrs · 29,967 cycles

THE FUSELAGE SKIN WAS DENTED FORWARD OF THE L2 DOOR BY JETWAY. DENT IS AT BS 610 ABOVE S17L AND IS 1.75 INCH DIA BY 1.1 INCH DEEP. INSTALLED DOUBLER PER ER/A 451214-14 AND INCORPORATED EXISTING REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,266 hrs · 29,120 cycles

FUSELAGE SKIN DENTED AND REPAIR REPLACEMENT AT STATION 1505 AND STR 28L. REPAIRED IAW ERA 095225-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,266 hrs · 29,120 cycles

FUSELAGE SKIN CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. REPAIRED IAW ERA 095131-14AD.

Part: INVERTER — FAILED (E/E BAY) · airframe 52,918 hrs · 27,942 cycles

STANDBY INVERTER INOP. REPLACED STANDBY INVERTER.

Part: WIRE — BURNED (CARGO DOOR) · airframe 52,533 hrs · 27,786 cycles

IRR: FWD AND AFT CARGO DOORS INOPERATIVE. FOUND BURNT WIRE BEHIND AFT CARGO DOOR SWITCH. REPLACED SAME. REPLACED K101 AND PSEU. SLACK IN WIRES ENOUGH WHEN CUT BACK TO REINSTALL ON NEW SWITCH. K101 AND PSEU DAMAGED WHEN WIRE SHORTED OUT.

Part: COOLER — LEAKING (NR 2 ENGINE) · airframe 46,802 hrs · 25,340 cycles

ACFT DIVERTED TO MIA EN ROUTE TO BOG DUE TO RT ENG LOW OIL QTY. FOUND ENG FUEL OIL COOLER. F/O COOLER LEAKING AT ENG OIL INLET ELBOW ADAPTER. REPLACED F/O COOLER. LEAK CHECK NORMAL.

Part: SKIN — DENTED (FS 620, S-16L) · airframe 46,796 hrs · 25,336 cycles

FUSELAGE / SKIN / FS 620 / STRG. 16L-17L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS NEAR FS 620 AND STRINGERS 16L & 17L. THE DENTS WERE REMOVED WITH A 7" X 6" CUTOUT AND A 2.5" X 3.5" CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER PER ER/A 380995-14, REV A.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 46,796 hrs · 25,336 cycles

THE C2 DOOR SURROUND BEARSTRAP AT FS 1380 WAS FOUND WITH TWO AREAS OF CORROSION AT STRINGERS 22R AND 23R.

Part: FRAME — CUT (FS 620, S-25R) · airframe 46,796 hrs · 25,336 cycles

FUSELAGE / C1 DOOR OPENING / FRAME / FS 620 / STRG. 25R-26R:FRAME WEB AND OUTER CHORD SPLICE REPAIR THE C1 DOOR OPENING LOWER SILL OUTER CHORD REQUIRED REPLACEMENT DUE TO CORROSION. TO FACILITATE REMOVAL AND INSTALLATION OF A NEW CHORD, THE OUTER CHORD AND WEB OF THE FS 620 FRAME WERE CUT BETWEEN STRINGERS 25R & 26R. THE WEB WAS SPLICED BACK TOGETHER WITH AN ALUMINUM DOUBLER AND THE CHORD WITH 2 ALUMINUM ANGLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 381025-14, REV A.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,796 hrs · 25,336 cycles

THE LOWER SILL CAP OF THE C2 DOOR SURROUND STRUCTURE WAS BADLY CORRODED AND REQUIRED REPLACEMENT.

Part: ACTUATOR — INOPERATIVE (NLG) · airframe 42,710 hrs · 23,697 cycles

AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. RETURNED TO SLC. REPLACED NG ACTUATOR AND BYPASS SEQ VALVE.

Part: AIR DIST — ODOR (CABIN)

DIVERT TO DFW DUE TO FUMES IN CABIN NEAR MID GALLEY FUMES. RESEMBLED TURPENTINE/SOLVENT. INSPECTED LEFT AND RIGHT AC BAY FOR LEAKS. ALL CHECKS OK. INSPECTED FWD BAG BIN. BAG BIN CHECKS OK. INSPECTED PASSENGER CABIN ON ARRIVAL. NO FUMES NOTED. RAN NR 1 AND NR 2 ENG W/2 PACKS. STILL NO FUMES. OK FOR SERVICE.

Part: BATTERY — DRAINED (4R DOOR)

FLASHLIGHT AT 4R DOOR NOT FLASHING. REPLACED BATTERY, CHECK NORMAL.

Part: BULB — FAILED (CABIN)

ON L/O, FOUND FIRST CLASS EMERGENCY LIGHTS INOP. FOUND SHORTED BULB AT SEAT 2AB. REPLACED SAME. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

FLASHLIGHT AT FWD INBD F/A JUMPSEAT USED. FOUND FLASHLIGHT BACKWARD IN HOLDER, BATTERY DEAD. INSTALLED NEW FLASHLIGHT ASSY.

Part: BATTERY PACK — DISCHARGED (CABIN)

L3 EMERGENCY EXIT LIGHT, INTERIOR AND EXTERIOR INOP. REPLACED PACK AND RACK.

Part: GATE ASSY — CORRODED (R1 DOOR)

LOUD SQUEAL COMING FROM R1 DOOR. FOUND LOWER GATE ASSY CORRODED. REPLACED SAME OP AND LEAK CKS NORMAL.

Part: FUEL PUMP — LEAKING (ENGINE NR 1)

DTW - ON A CHECK, FOUND FUEL LEAK FROM NR 1 ENGINE FUEL PUMP PAD SEAL DRAIN. REMOVED AND REPLACED NR 1 FUEL PUMP IAW MM73-11-01. OPS CHECK GOOD. NO LEAKS NOTED.

Part: FUEL CONTROL — FAILED (LT ENGINE)

LAX - IN-FLIGHT ENGINE FAILURE (LT ENGINE). REMOVED AND REPLACED LT ENGINE FUEL CONTROL UNIT. ENGINE RUN-UP CHECK OKAY.