N14337

Part: FLOORBEAM — CORRODED (BS 277) · airframe 57,850 hrs · 26,053 cycles

INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 19. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04464.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 57,850 hrs · 26,053 cycles

INSPECTION FOUND R-1 DOOR THRESHOLD DRAIN FRAME CORRODED AT STA 294-342, BL 0 TO RBL 36. A CHORD WAS INSTALLED IAW SRM 51-40-02 AND DRAWING 55-45875.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 57,850 hrs · 26,053 cycles

INSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, LBL 20. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04463.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,850 hrs · 26,053 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21, RBL 36, AND RBL 49. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,850 hrs · 26,053 cycles

INSPECTION FOUND FLOORBEAM CORRODED IN E&E COMPARTMENT ON RT SIDE ABOVE AIRFONE CONTROL BOX AT STA 312, RBL 21. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,850 hrs · 26,053 cycles

INSPECTION FOUND A 1.625 INCH CRACK IN FORWARD GALLEY FLOORBEAM WEB AT STA 312, RBL 18. THE WEB WAS REPAIRED IAW ECRA 5310-04462.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,689 hrs · 25,524 cycles

INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 264 ABOVE S19L. THE SKIN WAS REPAIRED IAW ECRA 5330-03366. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW PART III WITHIN 50 FLIGHT CYCLES.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,786 hrs · 25,103 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 540, RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5331-01146.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 55,786 hrs · 25,103 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00.

Part: SKIN — CRACKED (LT WING) · airframe 55,786 hrs · 25,103 cycles

INSPECTION FOUND A .5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-40-01, FIGURE 201, PROCEDURE 2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,786 hrs · 25,103 cycles

INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE FOR RIGHT RAM AIR INLET AT BS 540, S22R. THE CRACKED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 55,786 hrs · 25,103 cycles

THE RIGHT I/B SEAT TRACK UPPER LOBE BROKE DURING REMOVAL AT STA 827. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 55,786 hrs · 25,103 cycles

THE RIGHT O/B SEAT TRACK UPPER LOBE BROKE DURING SEAT REMOVAL AT STA 887, RBL 34. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,758 hrs · 25,086 cycles

THREE EMERGENCY LIGHTS OVER EMERGENCY ESCAPE HATCH ARE INOP. REPLACED BATTERY CHARGERS AND BATTERIES PER MM 33-51-51.

Part: SKIN — CRACKED (WINDOW POST) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1" CRACK IN CAPTAIN'S WINDSHIELD O/B POST OUTER SKIN AT UPPER CORNER. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-01104.

Part: SKIN — CRACKED (C-2 DOOR) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND TWO INCH CRACKS AT THE EDGES OF THREE LIGHTENING HOLES IN C-2 DOOR INNER SKIN OVER CENTER BALANCE SPRINGS. A 1" CRACK WAS FOUND AT THE EDGE OF A LIGHTENING HOLE IN C-2 DOOR INNER SKIN AT PULLEY ACCESS PANEL. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5230-01651 AND 5230-01652.

Part: SKIN — CRACKED (C-2 DOOR) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1.25" CRACK IN C-2 DOOR INNER SKIN AT AFT LOWER CORNER. THE SKIN WAS REPAIRED IAW ECRA 5230-01650.

Part: WEB — CRACKED (STA 1040) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1/2" CRACK IN WEB AT LIGHTENING HOLE AFT OF STA 1040 AND I/B OF TAIL COMPARTMENT ACCESS. A REPAIR WAS INSTALLED IAW ECRA 5320-01768.

Part: SPAR CAP — CRACKED (RW REAR SPAR) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1/2" CRACK AT HOLE IN SPAR CAP AT R/H WING MLG BEAM ATTACH FITTING. REPAIRED IAW ECRA 5740-02000. THE ITEM WAS PLACED ON DIP TO PERFORM AN HFEC INSPECTION ON THE R/H WING REAR SPAR AT MLG BEAM ATTACH FITTING AT THE LOCATION REFERENCED IN ECRA 5740-02000. THE INSPECTION IS TO BE PERFORMED AT "C" CHECK INTERVALS OR AT 4500 FLIGHT CYCLES AND ANY CRACK FOUND MUST BE REPAIRED.

Part: SKIN — CRACKED (RH HOR STAB) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 3" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR JUST I/B OF #4 ELEVATOR HINGE. A PERMANENT REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01584.

Part: KEELBEAM — CHAFED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND LT AFT UPPER SURFACE OF KEEL BEAM FLANGE HAD WORN HOLES ON UPPER SURFACE FROM PANEL ATTACH NUTS AT STA 719-727. REPAIRED IAW ECRA 5310-03740.

Part: SKIN — CRACKED (#4 SLAT) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.

Part: WEB — WORN (C-1 DR JAMB) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND C-1 AFT DOOR JAMB LOWER WEB WORN AROUND EDGES. A NEW WEB WAS INSTALLED IAW SRM 51-70-13.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOOR H-STRAP CORRODED AT STA 1022-1026, LBL 3. A NEW H-STRAP WAS INSTALLED IAW SRM 51-10-2 AND 51-30-3.

Part: SKIN — WORN (STA 867) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND UPPER FUSELAGE SKIN WORN AT STA 867, RBL 6. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 214.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 578, BBL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-2.

Part: FLOORBEAM — CORRODED (STA 986) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOORBEAM CORRODED ABOVE AND BELOW NUT CLIP HOLES AT STA 986, RBL 46 TO LBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851.

Part: SKIN — CRACKED (FLAP FAIRING) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1/2" CRACK IN R/H WING #6 FLAP FAIRING LOWER SKIN WITH RIVETS PULLING THROUGH. A STIFFENER WAS INSTALLED IAW SRM 51-10-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1006-1016, LBL 7 AND RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-02-01.

Part: COLLAR — CRACKED (FLAP FAIRING) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 FLAP FAIRING HORSE COLLAR. A NEW COLLAR WAS INSTALLED IAW SRM 51-10-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A RT AND LT LAV FLOOR SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 44, AND LBL 14 TO LBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT STA 986-1006. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.

Part: ANGLE — CORRODED (STA 927) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR JAMB, STA 927. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-05.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 663.75, LBL 65. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: WEB — CRACKED (STA 270) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1/2" CRACK IN WEB AT STA 270, S14R. A WEB INTERCOSTAL WAS INSTALLED IAW SRM 51-10-02.

Part: STRINGER — CRACKED (STA 500C) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 1" CRACK IN STRINGER 16L AFT OF STA 500C. REPAIRED STRINGER IAW SRM 53-00-03, FIGURE 201.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 50,301 hrs · 22,525 cycles

INSPECTION FOUND A 2 INCH CRACK IN AC BAY FLOOR SUPPORT AT STA 559, RBL 24, IN FORWARD BAGGAGE BIN. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (STA 1016) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 1016, RBL 37 TO LBL 37. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851.

Part: ANGLE — CRACKED (STA 927-947) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND A 3" CRACK IN ANGLE AT STA 927-947, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-03.

Part: FLOORBEAM — CORRODED (STA 967) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 967, LBL 50 TO RBL 50 AND AT RBL 18 TO LBL 18. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 202.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 951, LBL 14 TO LBL 16 AND AT LBL 18 TO LBL 24. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947-967, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: TRACK — CORRODED (STA 280-294) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND CABIN FLOOR R/H FORWARD GALLEY ATTACH TRACK CORRODED AT STA 280-294, RBL43. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 294-312, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-70-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,332 hrs · 22,544 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 328-344, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: BRAKE ASSY — FAILED (MLG) · airframe 46,135 hrs · 20,748 cycles

BRAKES FAILED ON TAXI TO GATE. CHECKED BRAKE SYSTEM PER MAINTENANCE MANUAL 32-41-00 ADJ / TEST. ALL SYSTEMS CHECK NORMAL.

Part: MODULE — INOP (E & E COMPT)

THE FIRE WARNING LIGHT AND BELL ACTIVATED WHILE ON SHORT FINAL INTO EWR. THE WARNING WAS ON THE GLARESHIELD WITH NO INDICATIONS IN T-HANDLE ON THROTTLE CONSOLE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND THE FIRE DETECTION MODULE AT FAULT. THE MODULE WAS REMOVED AND REPLACED. BITE CHECK WAS GOOD WITH NO OTHER DEFECTS NOTED.

Part: FIRE WARNING — ACTIVATED (APU)

WHEN THE APU WAS STARTED ON DESCENT INTO SAT, THE APU FIRE WARNING LIGHT AND BELL ACTIVATED. THERE WERE NO LIGHTS IN APU FIRE HANDLE OR FOR ENGINES AND NO OTHER ABNORMAL INDICATIONS WERE NOTED. THE APU RAN NORMALLY AND THE LIGHT AND BELL WERE SILENCED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND NO FAULTS. A FIRE WARNING TEST WAS PERFORMED IAW MM 26-11-00 AND NO FAULTS WERE NOTED. THE APU WAS RUN FULLY LOADED FOR 20 MINUTES WITH NO TROUBLE FOUND. THE PROBLEM COULD NOT BE DUPLICATED.

Part: BATTERY — DISCHARGED (CABIN)

THE FORWARD SERVICE DOOR EXIT SIGN FAILED TEN MINUTE BURN DURATION TEST. THE BATTERY WAS REPLACED AND A WIRE WAS RECONNECTED, OPERATIONAL TEST WAS GOOD.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 5 TO LBL 40. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, FIGURE 205.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 312 FROM LBL 20 TO RBL 20. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-10-51, PAGE 220-223.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN FS 967 AND 986.5 LEFT SIDE, 22 INCHES FROM CENTERLINE. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND FLOORBEAM CORRODED AT BOTH SIDES OF SCREW HOLES TO EDGE OF T-CAP AT STA 986.5. REPAIRED IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (BS 967)

INSPECTION FOUND FLOORBEAM CORRODED AT BS 967 UPPER T-CAP, LBL24. REPAIRED IAW SRM 53-00-51, FIGURE 202.

Part: O-RING — LEAKING (B-HYD SYST)

AIRCRAFT LOST B-SYSTEM HYDRAULIC FLUID AND PRESSURE ON APPROACH. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC PUMP LOW PRESSURE LIGHT. MAINTENANCE FOUND ELBOW LOOSE AND A BAD O-RING ON LOWER END OF ACOUSTIC FILTER. THE O-RING WAS REMOVED AND REPLACED AND THE ELBOW WAS TIGHTENED. LEAK AND OPERATIONAL CHECKS WERE GOOD.