N63305

Part: CABLE — FRAYED (R2 DOOR SLIDE) · airframe 67,129 hrs · 36,015 cycles

R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED R2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW AMM 25-61-35.

Part: BRACKET — CORRODED (BS 986.5-1016) · airframe 64,031 hrs · 34,611 cycles

INSPECTION FOUND INTERGRANULAR CORROSION ON AFT LAV SERVICE SUPPORT HAT BRACKET AT STA 986.5-1016, S24R TO 25R. THE BRACKET ASSEMBLY WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BAC DRAWING 69-36677.

Part: CHANNEL — CORRODED (BS 967-986.5) · airframe 64,031 hrs · 34,611 cycles

INSPECTION FOUND AFT DRAIN MAST MOUNTING CHANNEL CORRODED FROM STA 967-986.5 BETWEEN S24L AND S25L. THE DRAIN MAST CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BAC DRAWING 65-55843.

Part: STRINGER — CORRODED (BS 907-1016 S26L) · airframe 64,031 hrs · 34,611 cycles

INSPECTION FOUND STRINGER 26L CORRODED AT STA 907-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02, PAGE 1.

Part: SHEAR TIE — CORRODED (BS 1006 S27L) · airframe 64,031 hrs · 34,611 cycles

INSPECTION FOUND FUSELAGE SKIN BULGED WITH RIVETS PULLED TO THE RIGHT OF STRINGER 27L AT STA 1006. A CORRODED SKIN CLIP WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: STRINGER — CORRODED (BS 980-996 S27L) · airframe 64,031 hrs · 34,611 cycles

INSPECTION FOUND STRINGER 27L CORRODED AT STA 980-996. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1.

Part: STRINGER — CORRODED (BS 960-980 S25L) · airframe 64,031 hrs · 34,611 cycles

INSPECTION FOUND STRINGER 25L CORRODED AT STA 960-980. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, REPAIR 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND SHEAR TIE CORRODED AT STA 460 BETWEEN STRINGERS 27R AND S28R. THE SHEAR TIE WAS REPAIRED IAW SRM 53-00-07.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND O/B SIDE OF STRINGER 27L CORRODED APPROXIMATELY 2 INCHES FORWARD OF STA 500D IN FORWARD BAGGAGE BIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 5331-01336.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 767, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN RIGHT FUSELAGE SKIN ABOVE SKIN LAP S25R APPROXIMATELY 6 INCHES FORWARD OF STA 887. THE SKIN WAS REPAIRED IAW SRM 53-00-01, PRODECURE 5, PAGE 203, REPAIR 31.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 480, S9R. REPAIRED IAW ECRA 5110-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 787, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 847, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 887, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN STRINGER 14L AT STA 360. REPAIRED IAW ECRA 5311-01346.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND AFT BAGGAGE BIN FRAME CORRODED AT STA 794.3, S25R TO S26R. A NEW FRAME WAS INSTALLED IAW SRM 51-40-02.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN STRINGER SPLICE AT STA 359, S15L. REPAIRED IAW ECRA 5311-01346.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 380, S9R. REPAIRED IAW ECRA 5310-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 867, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND LEFT KEEL BEAM CORRODED ON O/B FLANGE IN FORWARD BAGGAGE BIN AT STA 520, S28L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT RIVET THAT ATTACHES AIR GRILL, STA 400, S9L. A FRAME REPAIR WAS INSTALLED IAW ECRA 5310-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 887, S9R. REPAIRED IAW ECRA 5310-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 727D, S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04643.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 867, S9R. REPAIRED IAW ECRA 5310-04643.

Part: SKIN — BURNED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A BURN SPOT ON FUSELAGE SKIN 2.25 INCHES AFT OF STA 727 AND 2.25 INCHES ABOVE S23L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31, PAGE 231.

Part: CHANNEL — CORRODED (BS 727D) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND AFT BAGGAGE BIN FLOOR CHANNEL CORRODED AT STA 727D + 8 INCHES, RBL 3. REPAIRED IAW SRM 53-00-53.

Part: RAIL — CRACKED (BS 727E) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A 1 INCH CRACK IN AFT BAGGAGE BIN TIE DOWN RAIL AT STA 727E, S27R. THE TIE DOWN RAIL WAS REMOVED AND A NEW SECTION OF TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53, REPAIR 2, PAGE 202.

Part: STRUCTURE — CORRODED (BS 227.8) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND LOWER FUSELAGE O/B CHORD CORRODED AT STA 227.8, LBL5.7 TO RBL 5.7. REPAIRED IAW ECRA 5311-01345.

Part: CHANNEL — CRACKED (BS 500-500A) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 1 VHF ANTENNA MOUNT CHANNEL ON BOTH ENDS AT STA 500-500A, S29R TO 29L. THE ANTENNA CHANNEL WAS REPLACED IAW SRM 51-40-02.

Part: FRAME — CORRODED (BS 847 S26R) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND FRAME CORRODED AT STA 847, S25R TO S26R. THE FRAME WAS REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 947) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN ABOVE L-2 DOOR UPPER HINGE, STA 947.5, S11L T0 14L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-60-01.

Part: INTERCOSTAL — CRACKED (BS 357) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL WEB AT STA 357, S16L. REPAIR PARTS WERE INSTALLED IAW SRM 53-10-04.

Part: SEAT TRACK — CORRODED (BS 328-360) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND FORWARD ENTRY RIGHT I/B SEAT TRACK CORRODED BETWEEN STA 328 AND 360, RBL 20. A REPAIR WAS INSTALLED IAW SRM 53-00-52.

Part: ANGLE — CORRODED (BS 294.5-360) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED IN SEVERAL AREAS FROM STA 294.5 TO 360, RBL 48. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 328-360) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND THE FORWARD ENTRY RIGHT O/B SEAT TRACK CORRODED BETWEEN STA 328 AND 360, RBL 36. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF R-1 DOOR CUTOUT OUTER SKIN, STA 344-360, S16R TO S17R. THE SKIN WAS REPAIRED IAW SRM 53-10-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 344, LBL 17 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED THE ENTIRE LENGTH, AT STA 328, LBL 45 TO RBL 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A CRACK IN THE AFT CARGO DOOR CUTOUT STA 794.3 FRAME. THE FRAME WAS REPAIRED IAW ECRA 5311-01344.

Part: SKIN — CRACKED (BS 947.5-967) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN BELOW R-2 DOOR LOWER HINGE AT STA 947.5-967, S13R TO S14R.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 26 TO RBL 30. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW ECRA 5310-03851.

Part: FRAME — CRACKED (BS 616) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND A .25 INCH CRACK IN MAIN FRAME AT STA 616, LBL 55. A REPAIR WAS INSTALLED IAW ECRA 5311-01158.

Part: SEAT TRACK — CORRODED (BS 887-927) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 887-927, RBL 20. A REPAIR SPLICE SEAT TRACK WAS INSTALLED IAW SRM 53-00-52, REPAIR 3, FIGURE 201.

Part: SEAT TRACK — CORRODED (BS 867-947) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 867-947, LBL 40. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52, REPAIR 3, FIGURE 201.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 63,357 hrs · 34,281 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, S17R TO 17L. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851.

Part: SKIN — CRACKED (BS 727D-727E) · airframe 62,611 hrs · 33,944 cycles

INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727D-727E, S23L (AT LEFT AFT EMERGENCY LIGHT). REPAIRED IAW ECRA 5330-03658.

Part: SKIN — CRACKED (BS 727E-727D) · airframe 62,611 hrs · 33,944 cycles

INSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT STA 727E-727D, S23R (AT WING AFT EMERGENCY LIGHT). DOUBLERS WERE INSTALLED IAW ECRA 5330-03659, REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,214 hrs · 33,285 cycles

FUSELAGE CRACK AT STA 747, 12 INCHES BELOW WATER LINE. REPAIRED IAW SRM 53-00-01 REPAIR 31 FIG 201.

Part: KEELBEAM — CORRODED (STA 690-727) · airframe 58,584 hrs · 31,986 cycles

INSPECTION FOUND RT WHEEL WELL LOWER KEEL BEAM MILDLY CORRODED AT STA 690-727, S28R. REPAIRED IAW ECRA 5311-01237.

Part: SHEAR TIE — CORRODED (BS 847) · airframe 58,584 hrs · 31,986 cycles

INSPECTION FOUND SHEAR TIE AT STA 847 BETWEEN S27L AND S27R, LBL 6 TO RBL 6 CORRODED. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 208.

Part: WIRE HARNESS — SHORTED (LT FLAP WELL) · airframe 57,062 hrs · 31,232 cycles

THE NR 1 ENGINE WAS SLOW TO SPOOL AND THEN FLAMED OUT ON TAXI OUT IN PHL. THE AIRCRAFT WAS RETURNED TO THE GATE. THE DAMAGED WIRES WERE REPLACED. BOEING EXAMINED THE WIRE HARNESS & FOUND THE INSULATION ON THE WIRES DETERIORATED TO THE EXTENT THAT THE WIRE CONDUCTORS HAD BEEN EXPOSED. THE MOST SIGNIFICANT INSULATION DAMAGE WAS OBSERVED AT AN AREA OF THE HARNESS WHERE THE WIRES TRANSITION FROM BEING COVERED WITH A SLEEVED FABRIC TO PLAIN WIRE. MOISTURE BEING RETAINED BY THE SLEEVING & A BEND IN THE WIRE HARNESS IS BELIEVED TO BE THE CAUSE OF THE DETERIORATION AT THE TRANSITION POINT.

Part: SKIN — CRACKED (FUSLEAGE) · airframe 54,961 hrs · 30,123 cycles

INSPECTION FOUND A 2 INCH CRACK IN RIGHT FUSELAGE SKIN AT BS 727E, S18R ABOVE EMERGENCY EXIT LIGHT AT WATERLINE. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.

Part: SUPPORT ANGLE — CRACKED (FLAP FAIRING) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND A 2 INCHES CRACK IN NR 3 FLAP FAIRING AFT SUPPORT ANGLE THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 520, LBL 48. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02

Part: ANGLE — CORRODED (R1 DOOR) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND RT AFT LAV WALL SUPPORT HAT SECTION CORRODED. THE WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED ON LOWER SIDE OF FLOOR SUPPORT AT STA 967-986, LBL 17.

Part: STRAP — CRACKED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND E&E COMPARTMENT CEILING STRAP CRACKED BETWEEN STA 312 AND 328, BL 0. REPAIRED IAW SRM 51-70-13.

Part: BEAM — CRACKED (L-1 DOOR) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND A CRACK AT LOWER FORWARD CORNER OF LOWER BEAM OF L-1 DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND FLOORBEAM CORRODED IN AFT LAV AREA AT STA 1016, RBL 10. INSTALLED REPAIR STRAP IAW SRM 53-00-51, FIGURE 203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 16. REPAIRED IAW SRM 51-10-02.

Part: SUPPORT — CORRODED (RT AFT LAV) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND RIGHT AFT LAV WALL SUPPORT CORRODED. THE LAV WALL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND AFT CABIN FLOORBEAM CORRODED AT STA 986.5, RBL 46. REPAIRED IAW SRM 53-00-51, FIGURE 203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND AFT CABIN FLOORBEAM CORRODED AT STA 1006, LBL 15. A STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND CROSS SUPPORT IN AFT LAV AREA CORRODED BETWEEN STA 1006 AND 1016, RBL 16. A CROSS SUPPORT ANGLE WAS INSTALLED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND FLOOR SUPPORT IN RT LAV AREA CORRODED AT STA 986.5-1006, RBL 42. A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND FLOORBEAM CORRODED IN FORWARD GALLEY AREA AT STA 328, RBL 29. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW SRM 53-00-51.

Part: SKIN — DENTED (T/E FLAP) · airframe 53,580 hrs · 29,376 cycles

INSPECTION FOUND TWO DENTS ON BOTTOM I/B SURFACE OF LEFT AFT NR 2 T/E FLAP. REPAIRED PER SRM 57-53-02, 51-70-10.

Part: INDICATOR — INOPERATIVE (RMI/DME) · airframe 53,485 hrs · 29,328 cycles

SMOKE BEGAN COMING FROM THE F/O'S RMI WHILE EN ROUTE TO ATL. THE APPROPRIATE C/B WAS PULLED AND THE SMOKE CEASED. THE AIRCRAFT LANDED SAFELY AT ATL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RMI AT FAULT. THE F/O'S RMI/DME(DUAL UNIT) WAS REMOVED AND REPLACED IAW MM 34-28-81. A SYSTEM TEST WAS PERFORMED AND OPERATION CHECKED NORMAL. ALL C/P'S AND WIRES WERE INSPECTED WITH NO DEFECTS NOTED.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A 2 INCH CRACK IN RIGHT WING L/E CUTOUT AT O/B AUX TRACK NR 5 SLAT PANEL. REPAIRED IAW SRM 51-70-16.

Part: SKIN — CORRODED (STA 520) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 520, S28R. A DOUBLER WAS INSTALLED IAW ECRA 5311-01111.

Part: STRINGER — CORRODED (BS 520-540) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND STRINGER S28R CORRODED AT BS 520-540. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-00 AND ECRA 5311-01111.

Part: FITTING — CRACKED (R OB MLG BEAM) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A 1/16" CRACK IN R/H O/B MLG BEAM FITTING. THE FITTING WAS REPLACED IAW TASK CARD 03-5743-1-0002 AND 03-5743-1-0004, SEQ 579, AND EA 5743-01022.

Part: FITTING — CRACKED (L OB MLG BEAM) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A 1/16" CRACK IN L/H O/B MLG BEAM FITTING. THE FITTING WAS REPLACED IAW TASK CARD 03-5743-1-0003 AND EA 5743-01022.

Part: SKIN — CRACKED (#2 ENG PYLON) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND THE #2 ENGINE PYLON ACCESS PLATE #5824R CUTOUT CRACKED AT FORWARD UPPER AND AFT LOWER AREAS. THE CRACKS WERE 1.6" LONG. A DOUBLER AND ANGLE WERE INSTALLED IAW ECRA 5430-01204.

Part: CAP — CORRODED (FUSELAGE) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND END CAP CORRODED AT STA 540, LONGERON 27R. A NEW END CAP WAS INSTALLED IAW SRM 51-10-2.

Part: SKIN — CRACKED (LT WING) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A 1 INCH CRACK ABOVE NR 3 SLAT ACTUATOR IN LT WING LEADING EDGE CUTOUT. THE LEADING EDGE WAS REPAIRED IAW MM 51-70-17.

Part: BEAM — CORRODED (LT MLG) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND LT MLG ACTUATOR WALKING BEAM HANGER AND BRACKET HARDWARE CORRODED. A NEW WALKING BEAM HANGER AND BRACKET HARDWARE WERE INSTALLED IAW MM 57-15-00.

Part: SKIN — CRACKED (LT PYLON) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A .75 INCH CRACK IN LT ENGINE UPPER PYLON SKIN AT PANEL CUTOUT 5727L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.

Part: SKIN — CRACKED (#6 SLAT) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A 1/4" CRACK IN R/H WING #6 SLAT PANEL SKIN. REPAIRED IAW SRM 57-43-01.

Part: FRAME — CORRODED (STA 500) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND FRAME CORRODED AT STA 500, L27R. REPAIRED IAW SRM 51-70-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,932 hrs · 27,470 cycles

INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 500-500A, L27R. REPAIRED IAW SRM 51-70-11.

Part: DOOR — CRACKED (FWD CARGO) · airframe 47,838 hrs · 26,402 cycles

INSPECTION FOUND TWO 4.5" CRACKS IN FORWARD CARGO DOOR AT LOWER AFT CORNER. THE FORWARD CARGO DOOR WAS REMOVED AND REPLACED IAW MM 52-31-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,577 hrs · 25,780 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT R-2 GIRT BAR MOUNT STA 986.5, RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851 AND SRM 53-60-51.

Part: STRINGER — CRACKED (BS 390)

INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 390. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-03.

Part: STRINGER — CRACKED (BS 500)

INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16R AT BS 500C. REPAIRED IAW SRM 53-00-03.

Part: FLOORBEAM — CORRODED (BS 328)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328, LBL 15 TO RBL 50. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 344, RBL 10 TO LBL 50. REPAIRED FLOORBEAM IAW SRM 53-10-51.

Part: CHANNEL — CORRODED (L-1 DOOR)

INSPECTION FOUND L-1 DOOR THRESHOLD Z-CHANNEL CORRODED. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: ANGLE — CORRODED (R-2 DOOR)

INSPECTION FOUND Z-ANGLE CORRODED AT R-2 DOOR. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: BLKHD STIFFENER — CORRODED (AFT PRESS BLKHD)

INSPECTION FOUND BOTTOM CENTER RT STIFFENER CORRODED AT AFT PRESSURE BULKHEAD SIDE. REPAIRED IAW SRM 51-70-11, FIGURE 1.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AND EDGES AT STA 986.5. A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW ECRA 5310-03851.

Part: FLOORBEAM — CORRODED (BS 947.5)

INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AROUND NUT PLATE HOLES AT STA 947.5, LBL 15 TO RBL 8. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-00-51, PAGE 207-209.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 10 TO RBL 25. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: BATTERY PACK — DISCHARGED (BS 326,629,753)

THE EMERGENCY LIGHT BATTERY PACKS AT M1133 STA 326L, M1134 STA 629L, AND M1136 STA 753L FAILED 10 MINUTE DURATION TEST. THE BATTERY PACKS WERE REPLACED.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN MID CABIN. MAINTENANCE FOUND BATTERY PACK IN MID CABIN NOT TESTING. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATION WAS NORMAL.

Part: WIRE — BROKEN (LT EMER EXIT)

INSPECTION FOUND LOWER EMERGENCY LOCATOR SIGN AT RT OVERWING EXIT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO LIGHT ASSEMBLY AND OPERATION CHECKED GOOD.

Part: SOCKET — CORRODED (CABIN)

INSPECTION FOUND THE RT AFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE LIGHT SOCKET WAS REPLACED DUE TO CORROSION.

Part: SLIDE — LOW PRESSURE (R 1 DOOR)

INSPECTION FOUND THE R-1 DOOR SLIDE PRESSURE LOW. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED.

Part: BRACE — CRACKED (NR 2 PYLON)

INSPECTION FOUND NR 2 ENGINE PYLON STRUT TO WING DIAGONAL BRACE CRACKED THROUGH THE LOWER LUG RADIUS(1 INCH LONG BY .75 INCH DEEP). THE BRACE WAS REMOVED AND REPLACED IAW MM 54-10-01.

Part: FILTER — LEAKING (A-HYD SYS)

MCO - FLT 0259 - THE A-SYSTEM HYRAULIC QUANTITY WENT TO ONE-HALF FULL INDICATION DURING CLIMB-OUT. THE INDICATION SLOWLY DECREASED TO LESS AND ONE-QUARTER FULL DURING THE FLIGHT. THE A-SYSTEM HYDRAULIC ENGINE PUMP LOW PRESSURE LIGHT ILLUMINATED DURING DESCENT INTO MCO. THE PUMP WAS TURNED OFF PER THE 'ABNORMAL' CHECK LIST. MAINTENANCE FOUND THE A-SYSTEM ELECTRIC PUMP ACOUSTICAL FILTER LEAKING FROM UPPER FITTING. THE ACOUSTICAL FILTER ASSEMBLY WAS REMOVED AND REPLACED. THE A-HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECK WAS GOOD. (X)

Part: UPLOCK FITTING — CORRODED (BS 685)

YVR - INSPECTION FOUND THE LEFT MLG FORWARD ATTACH LUG (BODY LUG AT STATION 685) CORRODED IN AND AROUND THE BORE. THE BORE WAS REAMED, UNEVEN AREAS WERE REAMED, AND FACES SPOTFACED. SHOT PEENED AND FABRICATED AND INSTALLED REPAIR SLEEVE. SPOTFACED FILLERS, FABRICATED AND INSTALLED. (M)

Part: UPLOCK FITTING — CORRODED (BS 685)

YVR - THE RIGHT MLG FORWARD UPLOCK BODY LUG, STATION 685, WAS FOUND CORRODED. BORE REAMED, BLENDED UNEVEN AREAS, AND FACES SPOTFACED. SHOT PEENED AND FABRICATED AND INSTALLED REPAIR SLEEVE. SPOT FACED FILLERS AND FABRICATED AND INSTALLED. (M)

Part: CARGO TRACK — CRACKED (BS 460-480)

YVR - INSPECTION FOUND A 20 INCH CRACK IN FORWARD CARGO FLOOR TRACK AT STATION 460-480, RBL 14. THE TRACK WAS REPLACED AND SPLICED PER DRAWING 50D53-28185 AND ECRA 5320-01387. (M)