N27610

Part: WIRE HARNESS — DEFECTIVE (APU BAY) · airframe 44,811 hrs · 24,025 cycles

APU FIRE INDICATION ON CLIMBOUT AT FL240. APU HANDLE WAS PULLED AND BOTTLE DISCHARGED. REPLACED HARNESS M/E 24-2611-3-0003 IAW WDM 26-11-31 RE N/R4479597. ALSO REPLACED M717 (APU TAILPIPE OVERHEAT DETECTOR P/N 10-61096-217) AND M515 (APU TAILPIPE DETECTOR P/N 10-61096-417) WDM 26-11-31 PG 2 REF N/R4479596. OP CHECK GOOD. REF N/R4479598 FOR OPS CHECK PER AMM 26-11-00. ALSO REPLACED APU FIRE BOTTLE DUE TO DISCHARGE 24-2622-9-9001, P/N 33007507, S/N 33336B1.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 44,527 hrs · 23,851 cycles

THEN GOT FULL FIRE WARNING LIGHT& BELLS RAN QRH DISCHARGED BOTTLES. FLT ATTENTANT CALLED UP, REPORTED SMELLED SMOKE, CALLED FOR FIREMEN AND WHEN THEY OPENED CARGO DOOR THEY SMELLED SMOKE. PERFORMED CONDITIONAL INSPECTION FOR SMOKE/ODOR IN CABIN/FLIGHT DECK IAW AMM 05-51-95-200-801C1, NO DEFECTS NOTED. ALSO SEE NON- ROUTINES 4482386, 4482383, 4482385 FOR CORRECTIVE ACTION.

Part: WARMER — ODOR (GALLEY) · airframe 42,965 hrs · 23,001 cycles

1.5 HR INTO FLT, F/A'S REPORT THE BURNT WIRE SMELL IS BACK. DOES NOT APPEAR TO BE COMING FROM AIR VENT BUT IS PRESENT IN ACFT GALLEY. COFFEEMAKERS & OVENS WERE OFF AND NOT USED. TURNED OFF GALLEY POWER. F/A REPORT SMELL LIGHTER NOW, 10-15 MINUTES LATER OPS CHECKED ALL AFT GALLEY LIGHTS, OVENS, AND COFFEEMAKERS AND FOUND NO DEFECTS OR ODORS. FOUND COFFEE WARMER 1 EMITTING STRONG "BURNT" ODOR. REPLACED SAME. ALSO REPLACED COFFEE WARMER 2 AS PRECAUTIONARY. OPS CHECK GOOD. NO ODORS IN AFT GALLEY. A/C OK FOR SERVICE.

Part: CONNECTOR — DEFECTIVE (FIRE LOOP) · airframe 41,257 hrs · 22,087 cycles

CLIMBING OUT OF AT 18,000FT STARTED TO GET INTERMITTENT APU FIRE WARNING FOLLOWED IMMEDIATE ACTION ITEMS & QRH. DECLARED AN EMERGENCY & RETURNED TO CLE. ON ARRIVAL, APU FIRE WARNING WAS GOING OFF INTERMITTENTLY AGAIN THRU LANDING. TROUBLESHOT APU FIRE DETECTION SYS. FOUND M334, M515 FIRE LOOPS FAILED. R&R IAW WDG 26-11-31.M.M. 26-15-14. ALSO FOUND KIDDE CONNECTORS 878581-01, D1446, D1448,D982 R&R IAW SWP 2062-16. OPS CHECK NORMAL, A/C OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

CORROSION ON FLOORBEAM AT STA 344 BETWEEN LBL 10 AND RBL 10 SEE WORK CARD MASTER PANEL CLOSE ZONE 107C SEQ 1007 FOR FLOOR PANELS INSTALLATION. REPAIRED CABIN FLOORBEAM STA 344 UPPER CORD BETWEEN BLL 10 AND RBL 10 PER ECRA 5310-01490.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

RIGHT O/B SEAT TRACK 6 INCHES FWD OF STA 807 IS DAMAGED. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION OF TRACK REF SRM 53-00-52 REPAIR 4 OPTION 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME STA 360 CRACKED BETWEEN STR 8L&9L AT A/C OUTLET EXTRUSION ATTACHMENT REPAIRED CABIN FRAME STA 360 L/T PER ECRA 5311-01488 AND GENERATED DIP PER PER ECRA 5311-01488 STEP 11 ON N/R LOG PAGE 9716560, SEQ N00714 STEP 12 ON N/R LOG PAGE 9716559, SEQ N00715 ATTACH FORM 44.0008 PAGE 1 TO PAGE 2 ITEM 1 TO ITEM 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK - FRAME WEB OVAL HOLE CRACKED .5 INCH LONG AT STA BS 303.9 AND STRINGER S16L AREA. TRIMMED OUT CRACKED SECTION OF FRAME & SPLICED IN NEW SECTION PER EA5310-04659 OP 2.

Part: BEAM — CORRODED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

CORROSION AT L1 DOOR LWR SILL BEAM DOOR CHORD BETWEEN STA 300 AND 360. INSTALLED NEW CHORD AT L1 DOOR LWR SILL BEAM AREA REF SRM 51-40-02.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 41,058 hrs · 21,982 cycles

L-1 DOOR JAMB, LOWER HINGE FITTING CRACKED ABOVE WL 236.68 AND JUST AFT OF STA 303.9. REMOVED AND REPLACED L-1 DOOR LOWER HINGE FITTING PER SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

CRACK FUSELAGE BETWEEN S-8L AND S-9L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 400 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 400 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK PAX CABIN FRAME STA 440 BETWEEN SRT 8R AND 9R HAS CRACKED INDICATION WHEN PERFORMED HFEC INSPECTION PER EA 5310-04498 OP20. FRAME AT STA 440 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662 CORRECTIVE ACTION SHOULD STATE THE LOCATION AS STA 440 STR 8R&9R 440.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK PAX CABIN FRAME AT STA 440 BETWEEN STR 8L AND 9L HAS CRACKED INDICATION WHEN PERFORMED HFEC PER EA 5310-04498 OP2. FRAME AT STA 440 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 867 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 867 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 380 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). FRAME AT STA 380 STR 8R&9R REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 907 CRACKED BETWEEN S-8L & S-9L AT A/C OUTLET EXTRUSION ATTACHMENT(MARKED). FRAME AT STA 907 STR 8L&9L REPAIRED PER EA5310-04498 OP2 DIP REQUIRED BY EA5310-04498 STEP 35 ON L/P9716468 SEQ N00662.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK PAX CABIN FRAME STA 727B BETWEEN STR 8R AND 9R HAS CRACKED INDICATION WHEN PERFORMED HFEC PER EA 5310-04498 OP 2. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS (ANGLES), TREATED AND PRIMED REF EA 5310-04498.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED AT DOOR STOP ATTACHMENT HOLE AT S-22R REFERENCE EA 5310-0444E REV C. REMOVED AND REPLACED CRACKED FRAME PER SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK B737-53-4-0010 L-1 DOOR LOWER SILL WEB IS CORRODED BETWEEN STA 312 & 344. REMOVED AND REPLACED L1 DOOR LOWER SILL WEB REF SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 827 CRACKED BETWEEN S-8L & S9L AT A/C OUTLET EXTRUSION ATTACHMENT. REPAIRED FRAME 827 LT PER EC/RA 5311-01489.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 827 CRACKED BETWEEN S-8R &S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED CRACKED FRAME 827 RT PER EC/RA 5311-01489.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME CRACKED BETWEEN S-8R & S9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED FRAME 787 BETWEEN S-8R AND S-9R REF EA 5310-014498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 867 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA 5310-04498, OP. O2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 907 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET T EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA5310-04498,OP 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

SUPPORT TASK PER EA 5310-04498 OP.2, FRAME CRACKED STA 727B BETWEEN S8L AND 9SL. REPAIRED FRAME STA 727B BETWEEN S-8L AND S9-L REF EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 747 CRACKED BETWEEN S-8R AND S-9R AT OUTLET EXTRUSION ATTACHMENT (MARKED). REPAIRED FRAME STA 747R BETWEEN S-8R AND S-9R REF EA 5310-0449 8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,058 hrs · 21,982 cycles

FRAME 400 CRACKED BETWEEN S-8R & S-9R AT A/C OUTLET EXTRUSION ATTACHMENT (MARKED). PERFORMED REPAIR PER EA5310-04498, OP.02.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 39,958 hrs · 21,411 cycles

ON APPROACH WHILE SETTING THE FLAPS TO 30, GOT A SPLIT FLAPS 17 TO 24. ON G/A PLACED FLAPS TO 15 DEGREES AND FLAPS STAYED AT 17 AND 24, ON DOWNWIND FLAPS CAME UP TO BETWEEN 10 AND 15. PUT FLAPS TO 10 WITH NORMAL INDICATIONS. QAR SHOWED A DELAY FROM FLAP XMTR RT SIDE. CHANGED FLAP RIGHT XMTR PER AMM 27-58-12, ADJUSTED BOTH LT AND RT XMTRS. VISUALLY INSPECTED FLAP ASSY FOR GENERAL CONDITION AND OPERATION. PERFORMED LAND VERIFY 22-03-10, PASSED. AIRCRAFT REMAINS CAT II AUTOLAND. ROTATABLE PARTS CHANGE WAS INDICATED - TT 1283315, S/N OFF 02820, TRANSMITTER, FLAP OFF 03-2762-9-0002 2820 ON 03-2762-9-0002 0505.

Part: SILL — CORRODED (FUSELAGE) · airframe 36,314 hrs · 19,511 cycles

INSPECTION FOUND R-1 DOOR SILL LOWER CHORD CORRODED AT STA 277-360, RBL 113. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,426 hrs · 16,405 cycles

INSPECTION FOUND AFT ENTRY FLOORBEAM CORRODED AT FASTENER HOLES, STA 986.5, LBL 54 TO RBL 54. REPAIRED IAW ECRA 5310-04461.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,728 hrs · 15,500 cycles

INSPECTION FOUND FUSELAGE SKIN CORRODED AFT OF FORWARD BAG BIN DOOR CUTOUT AT STA 452, S22R. A REPAIR WAS INSTALLED IAW ECRA 5330-03351.

Part: SKIN — DENTED (HORIZ STAB) · airframe 28,728 hrs · 15,500 cycles

INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5510-01741.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 25,495 hrs · 13,769 cycles

INSPECTION FOUND A 7 INCH CRACK IN TIE DOWN RAIL AT STA 807, RBL 14. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202.

Part: SKIN — CRACKED (W/S POST) · airframe 25,495 hrs · 13,769 cycles

INSPECTION FOUND A 1/8" CRACK IN SKIN OF CO-PILOT'S WINDSHIELD POST AT UPPER R/H CORNER. A DOUBLER WAS INSTALLED IAW SRM 53-10-01.

Part: WEB — CRACKED (STA 344-360) · airframe 25,495 hrs · 13,769 cycles

INSPECTION FOUND A 2" CRACK IN WEB AT STA 344-360, BL 0. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (STA 344-360) · airframe 25,495 hrs · 13,769 cycles

INSPECTION FOUND A 1" CRACK IN ANGLE AT STA 344-360, LBL 12. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (STA 500-520) · airframe 25,495 hrs · 13,769 cycles

INSPECTION FOUND A 1" CRACK IN ANGLE AT STA 500-520, BL O. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — DENTED (STA 360) · airframe 25,495 hrs · 13,769 cycles

A DENT WAS DISCOVERED IN FUSELAGE SKIN AT STA 360 ABOUT 3" ABOVE CUSP LINE AND 22" AFT OF L-1 DOOR. INSTALLED DOUBLER IAW SRM 53-00-01.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 24,541 hrs · 13,172 cycles

THE WHITE EMERGENCY PATH LIGHT AT SEAT 18C WAS FOUND INOPERATIVE DUE TO A PULLED WIRE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-81.

Part: WINDOW — OUT OF ADJ (COCKPIT) · airframe 18,954 hrs · 10,112 cycles

THE R-2 SLIDING COCKPIT WINDOW REQUIRED EXCESS FORCE TO LATCH AND UNLATCH. THE R-2 SLIDING WINDOW WAS ADJUSTED IAW MM 56-12-11, PAGE 501-511.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT RIGHT OVERWING AND AISLE RIGHT SIDE, ROW 7 AND 8. THE BATTERY PACK WAS REMOVED AND REPLACED.