N12313

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 67,422 hrs · 34,569 cycles

DURING NR 3 SERVICE CHECK FOUND L2 DOOR ESCAPE SLIDE LATCH CABLE TO HAVE BROKEN STRANDS. INSTALLED NEW CABLE AND HARDWARE PER AMM 25-61-35.

Part: CLOSEOUT PANEL — CRACKED (BS 950) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .75 INCH CRACK IN CLOSEOUT PLATE JUST FORWARD OF L-2 DOOR CUTOUT AND BELOW DOOR ASSIST HANDLE ATTACH POINT, STA 950. THE CLOSEOUT PLATE WAS REMOVED AND REPLACED IAW ECRA 5311-01332.

Part: FRAME — CRACKED (BS 950) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .75 INCH CRACK IN L-2 DOOR FORWARD STUB FRAME AT STA 950 AT UPPER HINGE. THE CRACKED AREA WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01332.

Part: SKIN — CRACKED (BS 730) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT STA 730, S24R. A REPAIR WAS INSTALLED IAW ECRA 5330-03690.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON AFT HORSE COLLAR (FITTING) AT LOWER I/B NUT PLATE, FORWARD OF NR 6 FLAP TRACK. A NEW FITTING WAS INSTALLED IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (BS 294) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL CLIP AT STA 294.5, S10L. THE CLIP WAS REPLACED AND A DIP WAS INITIATED TO INSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 6000 FLIGHT CYCLES IAW ECRA 5311-01330.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND VERTICAL STABILIZER LEFT AFT I/B ATTACH LUG FORWARD FAILSAFE FITTING CORRODED ON FORWARD SIDE, STA 1088-1104. THE FAILSAFE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND VERTICAL STABILIZER LEFT AFT LUG FAILSAFE FITTING CORRODED AT STA 1088-1104. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 328) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R-1 DOOR, STA 328, S17R - S17L. THE CRACKED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-01.

Part: STRINGER — CORRODED (BS 878-890) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND STRINGER 17R CORRODED ON UPPER FLANGES AND BELOW ATTACHING WEBS AT STA 878-890, RBL 70. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPLACED IAW SRM 51-70-12.

Part: FRAME — CORRODED (BS 827) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND FRAME CORRODED AT RIGHT AFT BAGGAGE BIN, STA 827, S27R. THE FRAME WAS REPAIRED IAW SRM 53-00-07, REPAIR 3.

Part: FRAME — CRACKED (BS 807) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 807 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04637.

Part: FRAME — CRACKED (BS 767) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 767 BETWEEN STRINGERS 8R AND 9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04637.

Part: BEAM — CRACKED (L1 DOOR) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR AFT EDGE BEAM AT NR 7 FORWARD STOP. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5210-01938 AND SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 196-203) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 196-203, RBL 5.7, S28L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: SKIN — CRACKED (753) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 753, S25R. THE CRACKED AREA OF SKIN WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-00-01, REPAIR 31.

Part: FRAME — CRACKED (BS 847) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR CUTOUT AFT FRAME AT LOWER STOP FITTING, STA 847, S24R. A NEW FRAME WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 947) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR LOWER HINGE CUTOUT, STA 947.5, S14R. THE CRACKED AREA WAS REMOVED AND A DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 53-60-01.

Part: STRINGER — CORRODED (BS 967-986) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND STRINGER 25L CORRODED AT STA 967-986.5. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-00-03.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND FLOORBEAM AT STA 1016 CORRODED AROUND UPPER AND LOWER HOLES FROM LBL 20 TO O/B END. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 63,822 hrs · 32,899 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1016, RBL 20. A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,149 hrs · 32,147 cycles

A 1 INCH FUSELAGE STRINGER CRACK 25.5 INCHES AFT OF RT CARGO DOOR. REPAIRED IAW SRM 53-00-01 REPAIR 11.

Part: SKIN — CRACKED (C-2 DOOR) · airframe 60,468 hrs · 31,351 cycles

INSPECTION FOUND A 1 INCH CRACK IN C-2 DOOR INNER SKIN AT LIGHTENING HOLE. REPAIRED IAW ECRA 5232-01074.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 60,468 hrs · 31,351 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON O/B ACCESS PANEL 5824R AT FORWARD UPPER CORNER OF PANEL. A PERMANENT REPAIR WAS PERFORMED IAW ECRA 5430-01204.

Part: FRAME — CORRODED (BS 807) · airframe 60,468 hrs · 31,351 cycles

INSPECTION FOUND FORWARD SIDE OF C-2 DOOR JAMB (FRAME) CORRODED AT DOOR LOCK RECEPTACLE, STA 807, RBL 43. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 727E) · airframe 60,314 hrs · 31,273 cycles

INSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN EIGHT INCHES AFT OF EMERGENCY LIGHT AND TWO INCHES BELOW STRINGER 23R AT STA 727E. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31, PROCEDURE 5, DETAIL 10.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 54,953 hrs · 28,499 cycles

MAINTENANCE DISCOVERED AN EXISTING REPAIR TO THE INNER SKIN OF THE FORWARD CARGO DOOR AT A LIGHTENING HOLE LOCATION. THE EXISTING REPAIR WAS NOT INSTALLED PER CURRENT FAA REQUIREMENTS. PREVIOUS ECRA 5232-01031 REPAIRED A LARGER AMOUNT OF DAMAGE TO THE SAME AREA AS THE CURRENT DAMAGE USING A DOUBLER INSTALLATION. A REPAIR DOUBLER WAS INSTALLED AS A PERMANENT REPAIR TO THE INNER SKIN IAW ECRA 5232-01036.

Part: SKIN — DAMAGED (RUDDER) · airframe 54,953 hrs · 28,499 cycles

THE RUDDER LT SIDE BONDED SKIN ASSEMBLY WAS FOUND DAMAGED AT APPROXIMATELY R STA 172. THE DAMAGE WAS REMOVED BY TAPER SANDING. A REPAIR WAS INSTALLED IAW ECRA 5540-01170.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 54,953 hrs · 28,499 cycles

MAINTENANCE DISCOVERED AN EXISTING REPAIR TO THE INNER SKIN OF THE FORWARD CARGO DOOR AT A LIGHTENING HOLE LOCATION THAT WAS NOT INSTALLED PER CURRENT FAA REQUIREMENTS. A PERMANENT REPAIR TO THE INNER SKIN WAS INSTALLED IAW ECRA 5232-01038.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 54,953 hrs · 28,499 cycles

MAINTENANCE DISCOVERED AN EXISTING TRIM-OUT TO THE INNER SKIN OF THE FORWARD CARGO DOOR AT AN UPPER LIGHTENING HOLE LOCATION. A PERMANENT REPAIR WAS INSTALLED TO THE INNER SKIN IAW ECRA 5232-01037.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND A .7500 INCH CRACK IN NR 6 SLAT LOWER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-43-01.

Part: WEB — CRACKED (RAM AIR INLET) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT WING RAM AIR INLET SUPPORT WEB AT STA 530. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13.

Part: SUPPORT ANGLE — CRACKED (FAIRING) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND A 2 INCH CRACK IN LT WING TO BODY FAIRING SUPPORT ANGLE AT BS 535. THE ANGLE WAS REPAIRED IAW ECRA 5350-01227.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND CENTER FLOOR RAIL CORRODED AT TOP AND INSIDE CHANNEL AT FLOOR STRAP AFT OF STA 847. THE FLOOR RAIL WAS REPAIRED IAW ECRA 5320-01603.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND A 3INCH CRACK IN NOSE WHEEL WELL RETRACT ACTUATOR SUPPORT TEE WEB AT STA 233. A WEB REPAIR WAS INSTALLED IAW SRM 51-70-13.

Part: STOP FITTING — CRACKED (L-1 DOOR) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR UPPER AFT STOP FITTING. THE STOP FITTING WAS REPLACED IAW SRM 51-10-2.

Part: SEAT TRACK — CORRODED (STA) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 910-927. THE SEAT TRACK WAS REMOVED AND REPLACED USING SPLICES AND FILLER IAW SRM 53-00-52, FIGURE 204.

Part: SKIN — WORN (FUSELAGE) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND EXTERIOR FUSELAGE SKIN WORN AT FORWARD DORSAL FIN FAIRING, TOP OF FUSELAGE STARTING AT BL 0, BS 860 THROUGH L & R BL6, BS 885. THE SKIN WAS REPAIRED USING A DOUBLER REPAIR IAW SRM 53-00-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND RT IB CABIN SEAT TRACK CORRODED AT STA 916-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,953 hrs · 28,499 cycles

INSPECTION FOUND A .5 INCH CRACK AT FASTENER IN RT FRAME AT STA 616. REPAIRED IAW ECRA 5311-01158.

Part: SKIN — CRACKED (AFT CARGO DR) · airframe 53,861 hrs · 27,888 cycles

MAINTENANCE NOTED DAMAGE TO THE INNER SKIN AT AN ACCESS PANEL LOCATION DURING REPAIR OF AN AFT CARGO DOOR THAT HAD BEEN REMOVED FROM AIRCRAFT.. THE DAMAGE CONSISTED OF A 1.1" AND 0.5" CRACK AND AN AREA OF DEFORMED SKIN. THE SKIN WAS REPAIRED IAW ECRA 5230-01717.

Part: FLOORBEAM — CORRODED (BS 1006) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND FLOORBEAM SCREW HOLES CORRODED AT TOP AND BOTTOM OF UPPER CAP AT BS 1006, LBBL 16.5, 20, AND 27.75. REMOVED AND REPLACED T-CAP IAW SRM 51-20-02 AND PERFORMED SPLICE REPAIR IAW ECRA 5310-03851.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND LT AFT LAV FORWARD WALL SUPPORT HAT SECTION CORRODED AT NUT PLATES. INSTALLED A NEW SECTION OF WALL SUPPORT HAT SECTION IAW SRM 51-40-01.

Part: FLOORBEAM — CORRODED (STA 986) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND AFT GALLEY FLOORBEAM CORRODED AT FORWARD AND AFT FLANGES AT STA 986, LBL 10 TO RBL 20. REMOVED AND REPLACED T-CAP IAW SRM 51-20-02.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND A 1 INCH CRACK IN RT PRESSURE DECK AT STA 664. REPAIRED IAW SRM 53-60-51.

Part: FLOORBEAM — CORRODED (STA 312) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED ON TOP SURFACE AT NUTPLATE AND LOWER SURFACE AT STA 312, RBL 20 TO RBL 31. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, PAGE 205, 51-40-02, AND 51-20-01.

Part: FLOORBEAM — CORRODED (STA 328) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT NUTPLATES ON FORWARD FLANGE AT STA 328, RBL 15 TO RBL 23. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, PAGE 205, 51-20-01, AND 51-40-02.

Part: FLOORBEAM — CORRODED (STA 344) · airframe 53,861 hrs · 27,888 cycles

INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED ON FORWARD AND AFT FLANGES AT STA 344, RBL 12 TO LBL 12. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-5, FIGURE 205.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 14,434 hrs · 7,292 cycles

MAINTENANCE FOUND THE AFT CARGO DOOR LOWER BEAM TEE CHORD CRACKED. TWO CRACKS WERE EMANATING FROM A RIVET HOLE. THE CRACKS WERE 0.4 INCH LONG AND 0.8 INCH LONG. THE AREA WAS REPAIRED IAW ECRA 5230-01715. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND FOUR 1/2 INCH CRACKS IN SEAT TRACK FRAME AT STA 727B. A STRAP REPAIR WAS INSTALLED AT EACH LOCATION IAW ECRA 5321-01122.

Part: STRINGER — CORRODED (STA 1016) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND STRINGER 26R CORRODED AT STA 1016. THE STRINGER WAS REPLACED IAW SRM 51-10-02.

Part: SHEAR TIE — CORRODED (STA 1006) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND BELTFRAME SHEAR TIE CORRODED AT STA 1006 BETWEEN STRINGERS 25R AND 27R. THE SHEAR TIE WAS REPLACED IAW SRM 51-10-02.

Part: WEB — CORRODED (STA 787-827) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND WEB CORRODED BETWEEN FLOOR SUPPORT RAILS IN AFT BAGGAGE BIN AT STA 787-827, S28R. A NEW WEB WAS INSTALLED IAW SRM 51-10-02.

Part: FRAME — CORRODED (STA 727E) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND BELT FRAME CORRODED BELOW FLOOR OF AFT BAGGAGE BIN AT STA 727E. REPAIRED IAW SRM 53-00-07, FIGURE 203, SHEETS 1-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND SIX FLOOR SUPPORTS CORRODED AT STA 767. A DOUBLER WAS INSTALLED AT EACH FLOOR SUPPORT IAW ECRA 5320-01603.

Part: SKIN — CRACKED (#4 SLAT) · airframe 51,090 hrs · 26,418 cycles

INSPECTION FOUND A 1/2" CRACK IN R/H WING #4 SLAT SKIN LOWER AREA, BELOW ACTUATOR ATTACHMENT TO SLAT. THE CRACKED AREA WAS CUTOUT. REPAIR FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.

Part: FLOORBEAM — CORRODED (BS 360)

INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 360, RBL 50. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW ECRA 5311-01074.

Part: SKIN — CRACKED (NR 2 ENGINE)

INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON SKIN UPPER SURFACE. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.

Part: INTERCOSTAL — CRACKED (BS 328)

INSPECTION FOUND A 1 CRACK IN INTERCOSTAL AT R-1 DOORWAY, STA 328, STRINGER 8A. A DOUBLER WAS INSTALLED IAW SRM 51-40-2 AND DRAWING NR 65C33288-1.

Part: FRAME — CRACKED (BS 328)

INSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR AFT FRAME AT STRINGER 8A, STA 328. STRINGER 8A HAD A .5 INCH CRACK. THE FRAME AND STRINGER WERE REMOVED AND REPLACED IAW SRM 51-40-2.

Part: FRAME — CRACKED (L1 WINDOW)

INSPECTION FOUND A .5 INCH CRACK IN COCKPIT L-1 WINDOW FRAME. A REPAIR WAS INSTALLED IAW ECRA 5330-02876.

Part: ANGLE — CORRODED (BS 967-986)

INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-986, LOWER DOOR JAMB AREA. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 294)

INSPECTION FOUND FORWARD LAV/GALLEY AREA FLOORBEAM CORRODED AT STA 294, LBL 18 TO RBL 12. A FLOORBEAM UPPER TEE CHORD REPAIR WAS INSTALLED IAW SRM 53-10-51.

Part: BATTERY — DISCHARGED (CABIN)

THE R-1 INSIDE OVERDOOR LIGHT, L-1 OUTSIDE SLIDE LIGHT, AND INSIDE FRONT STANDBY LIGHTS FAILED BATTERY CHECK. REPLACED BATTERY PACK AND OPERATION CHECKED GOOD.

Part: BATTERY — INOPERATIVE (CABIN)

THE R-2 INSIDE OVER DOOR LIGHT, L-2 OUTSIDE SLIDE LIGHT, AND CENTER BACK OVERHEAD LIGHTS FAILED BATTERY CHECK. REPLACED BATTERY PACK AND OPERATION CHECKED GOOD.

Part: LOGIC CARDS — INOPERATIVE (NLG)

THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLING THE GEAR PRODUCED NO CHANGE. A VISUAL CHECK WAS PERFORMED THROUGH VIEW PORT AND GEAR WAS OBSERVED TO BE UP AND DOORS APPEARED CLOSED. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE M983 AND M1215 NLG LOGIC CARDS AND THE NOSE GEAR LOCK SENSOR. OPERATION AND INDICATIONS CHECKED GOOD.

Part: CIRCUIT CARD — FAILED (NLG)

THE RED NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. A LOOK THROUGH THE VIEWPORT EVIDENCED THAT GEAR AND DOORS WERE RETRACTED. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE M983 AND M1215 CIRCUIT CARDS WERE REMOVED AND REPLACED. THE NOSE GEAR WAS SWUNG AND OPERATION AND INDICATIONS CHECKED GOOD.

Part: SKIN — DENTED (BS 847)

GSO - INSPECTION FOUND THE FUSELAGE SKIN DENTED ON RIGHT SIDE AT STATION 847 ABOVE STRINGER 19R. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-20-01, AND 51-40-02. (M)

Part: FLOOR BEAM — CORRODED (BS 312)

GSO - INSPECTION FOUND FLOOR BEAM CORRODED AT STATION 312 FROM RBL 30 TO LBL 11. THE UPPER T-CAP WAS REMOVED FROM LBL 11 TO RIGHT CUSP. A NEW T-CAP SEGMENT WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-70-12, 51-20-01, AND 51-40-00. (M)

Part: SKIN — DENTED (CARGO DOOR)

GSO - INSPECTION FOUND THE C-1 DOOR SKIN DENTED AND CREASED IN SEVERAL PLACES ABOVE DOOR HANDLE LEVEL. THE DAMAGED AREA OF SKIN WAS CUT OUT. DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 52-00-01, 51-20-01, AND 51-40-00. (M)

Part: FLOOR WEB — CORRODED (RT AFT LAV)

GSO - INSPECTION FOUND RIGHT AFT LAV FLOOR WEB CORRODED AT ATTACH AREAS, RBL 8 AND RBL 15. THE CORRODED AREAS WERE REMOVED. A REPLACEMENT WEB AND ATTACH ANGLE WERE FABRICATED AND INSTALLED IAW BAC DRAWING 65-52457 AND SRM 51-40-02. (M)

Part: SKIN — GOUGED (BS 847)

GSO - INSPECTION FOUND THREE GOUGES IN RIGHT SIDE FUSELAGE SKIN AT STATION 847 BETWEEN STRINGER 20R AND STRINGER 21R. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 201, 51-20-01, AND 51-40-02. (M)

Part: FLOOR BEAM — CORRODED (BS 940-986)

GSO - INSPECTION FOUND L-2 DOOR THRESHOLD FLOOR BEAM CHORD CORRODED FROM STATION 940 TO STATION 986. THE CHORD SEGMENT WAS REMOVED FROM STATION 910 TO 1006 AND A NEW CHORD WAS INSTALLED IAW SRM 51-40-02 AND BAC DRAWING 65C80735. (M)

Part: SKIN — GOUGED (CARGO DOR)

GSO - INSPECTION FOUND TWO GOUGES IN C-2 DOOR EXTERNAL SKIN. THE GOUGED AREAS WERE CUT OUT. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 52-30-01. (M)

Part: FLOOR BEAM — CORRODED (FS 986.5)

GSO - INSPECTION FOUND FS 986.5 MAIN CABIN FLOOR BEAM UPPER CHORD CORRODED AT RBL 37, RBL 23, RBL 10, LBL 6.5, LBL 19.5 AND LBL 32. THE UPPER CHORD SECTION WAS CUT OFF FROM CUSP TO CUSP. A 'T' ANGLE WAS INSTALLED IAW SRM 53-00-51 AND A 'T' CHORD UPPER SEGMENT WAS INSTALLED IN TWO SECTIONS IAW SRM 51-40-02. (M)

Part: DOOR — CRACKED (CARGO COMPT)

CLE - INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR, ZONE 209. AN REINFORCEMENT ANGLE WAS INSTALLED ON THE CARGO DOOR IAW DRAWING SA005-5230-01027. (M)