N16806

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 54,220 hrs · 31,157 cycles

INSPECTION FOUND A 3 INCH CRACK IN NR 1 SLAT INTERIOR SKIN BETWEEN NR 4 AND NR 5 SLAT TRACKS OF LT WING, STA XFS 167. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5752-01134, PART 1, STEP 13.

Part: SPLICE — CRACKED (WING) · airframe 54,220 hrs · 31,157 cycles

INSPECTION FOUND A 1 INCH CRACK IN WING SPLICE STRAP AT WING SPAR STA XRS 164 JUST O/B OF RIGHT VORTILION. THE WING SPLICE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

INSPECTION FOUND A 2.75 INCH CRACK IN LT VERTICAL STABILIZER ATTACH ANGLE AT STA 1474. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23B.

Part: BELTFRAME — CRACKED (STA) · airframe 54,220 hrs · 31,157 cycles

INSPECTION FOUND CANTED BELTFRAME CRACKED AT L2L, 3L, 2R, AND 3R, STA 1416. THE CRACKS WERE .25 INCH TO 4 INCHES LONG. THE CANTED BELTFRAME SECTION FROM L15R TO L15L WAS REMOVED AND REPLACED IAW SRM 51-30-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

INSPECTION FOUND A 1.25 INCH CRACK IN TAIL COMPARTMENT LONGERON 2L AT STA 1418. THE CRACK WAS LOCATED AT BELTFRAME FASTENER. THE CRACKED END OF LONGERON WAS CUT OFF AND A NEW END WAS SPLICED ON IAW SRM 53-02, FIGURE 18 AND ECRA 5311-01132.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

INTERCOSTAL BETWEEN STA 1287 AND 1309 CABIN FLOORBEAM CRACKED AT CLIP NUTS. INSTALLED INTERCOSTAL STA 1287 - 1309 AFT BAG BIN CABIN FLOORBEAM PER SRM 51-30-0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

SKIN FORMER AT STA 1451 UNDER LEFT VERTICAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED FORMER PER SRM 51-10-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

FRAME AT STA 1451 UNDER RIGHT VERTICAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED FORMER PER SRM 51-10-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

CRACK ON INNER SKIN FORWARD UPPER CORNER BY ROLLER ARM RIGHT MLG INNER DOOR. FABRICATED AND INSTALLED DOUBLER PER SRM 52-01 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

SKIN CRACKED AT RIVET STA 1418 JUST OUTBOARD OF LEFT VERTICAL ATTACH ANGLE. FABRICATED AND INSTALLED DOUBLER AT STA 1418 FUSELAGE SKIN PER SRM 53-04 FIG 4D SHEET 1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

AFT BAG BIN INTERCOSTAL FOR CABIN FLOORBEAM IS CRACKED AT STA 1041 CENTER LINE OF A/C. FABRICATED AND INSTALLED DOUBLER PER SRM 51-70-04 AND STOP DRILLED CRACK IN INTERCOSTAL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

INTERCOSTAL BETWEEN STA 1271 - 1287 CABIN FLOORBEAM CRACKED AT CLIP NUTS. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 FIG 2 SHEET 4.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,220 hrs · 31,157 cycles

STRINGER CRACKED AT STATION 1429 AT STRINGER 2 RIGHT (1 INCH). INSTALLED NEW STRINGER SECTION AND SPLICE PER EC/RA 5311-01132.

Part: HANDLE — LACK OF LUBE (TAILCONE) · airframe 53,840 hrs · 30,954 cycles

THE TAIL CONE HANDLE AFT ENTRY DOOR REQUIRED EXCESSIVE FORCE TO OPEN. THE DOOR HINGES AND HANDLE MECHANISM WERE LUBRICATED. A PULL TEST WAS PERFORMED IAW MM 53-53-00 AND OPERATIONAL CHECKS WERE GOOD.

Part: CABLE — OUT OF ADJUST (TAILCONE) · airframe 53,845 hrs · 30,957 cycles

THE TAIL CONE INNER RELEASE HANDLE REQUIRED EXCESSIVE FORCE TO PULL. THE TAIL CONE CABLE WAS ADJUSTED, CLEANED AND LUBRICATED IAW MM 53-53-00. AN OPERATIONAL CHECK WAS GOOD.

Part: BEAM — CRACKED (L1 DOOR) · airframe 48,181 hrs · 28,040 cycles

INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF L-1 DOOR UPPER INTERNAL BEAM. A T-ANGLE AND DOOR PAN WERE REMOVED FOR ACCESS IAW SRM 51-10-4 AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31, 51-10-4, AND 51-30-5.

Part: RIB — CHAFED (RT WING) · airframe 48,173 hrs · 28,035 cycles

RIGHT WING LEADING EDGE RIB INBOARD OF ANTI ICE DUCT IS CHAFED. REMOVED AND REPLACED RIB PER SRM 57-30-2, 51-30-2, AND 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

LEFT CABIN CUSP WEB IS HEAVILY CORRODED FS 1155-1174. REMOVED AND REPLACED CUSP WEB PER SRM 51-30-2, 51-30-5, 51-30-3, AND 51-30-0.

Part: FITTING — CRACKED (FLAP ACTUATOR) · airframe 48,173 hrs · 28,035 cycles

LEFT WHEEL WELL INBOARD FLAP ACTUATOR ATTACHMENT FITTING IS CRACKED (1 X .25 INCH). REMOVED AND REPLACED FITTING PER SRM 51-30-5 AND 51-10-4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

MID CARGO INTERCOSTAL HAS CORROSION AT FS 617-636 AT 29L. REMOVED DAMAGED SECTION. INSTALLED NEW INTERCOSTAL PER SRM 53-01 FIG 2 SHEET 3, 51-30-2, AND 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

L1 AFT TORQUE BOX WEB TANGS AT LONG 12 AND 15 ARE CRACKED. REPAIRED CRACKS. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS PER SRM 51-30-02 AND EC/RA 5310-04129.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

AFT CARGO INTERCOSTAL AT 28L FROM STATION 1309 - 1320 HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-02, 51-30-05, AND 51-10-3.

Part: BEARING — WORN (HORIZ STAB) · airframe 48,173 hrs · 28,035 cycles

RIGHT HORIZONTAL STAB SUPPORT BEARING HAS EXCESSIVE PLAY AND BOLT CORRODED. REMOVED HORIZONTAL STAB, REMOVED AND REPLACED STAB ATTACH PLATE BUSHINGS AND BEARINGS. REMOVED AND REPLACED HINGE PLATES PER 55-10-00 AND CARD 08-5530-1-0006.

Part: FRAME — CRACKED (FS1000/RBL60) · airframe 48,173 hrs · 28,035 cycles

RIGHT WHEEL WELL APPROX STATION 1000 RBL 60 MLG AFT FRAME IS WORN AND CRACKED. REMOVED AND REPLACED DAMAGED FRAME PER SRM 51-30-2, 51-10-4, 51-10-2, AND 51-30-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

MID CARGO INTERCOSTAL AT FS 769-786 OUTBOARD OF LONG 28R IS CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-3, 51-10-2, AND 51-10-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

LEFT FUSELAGE SKIN AFT OF GROUND FLOOD LIGHT CREASED. REPAIRED FUSELAGE SKIN PER SRM 53-04 FIG 12B.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

SHEAR TIE CRACKED AT STATION 1309 LGL 13 AND 14L. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER EA 9-5314-2-A0872 AND SRM 51-30-5.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 48,173 hrs · 28,035 cycles

MAIN CABIN FLOOR PANEL FS 1250 - 1309 CENTER HAS TORN INSERTS AND DAMAGED CORNERS. FABRICATED NEW FLOOR PANEL PER EC/RA 5320-01265. MATERIAL USED 4017T4000001BB-9.

Part: FITTING — CORRODED (CARGO BAY) · airframe 48,173 hrs · 28,035 cycles

AFT CARGO DOOR CUTOUT AREA AFT LOWER CORNER FITTING CORRODED. REMOVED FITTING FROM CORNER. FABRICATED AND INSTALLED FITTING PER SRM 51-30-5.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 48,173 hrs · 28,035 cycles

FORWARD CARGO DOOR AFT LOWER INNER STIFFENER UPPER SUPPORT IS CRACKED. REMOVED DAMAGED STIFFENER. FABRICATED AND INSTALLED NEW STIFFENER PER SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

LEFT CUSP ANGLE CORRODED AT STATION 1322-1338. CUSP ANGLE REPAIRED PER EA 9-5314-2-A0873. FABRICATED REPAIR ANGLE FROM .050 7075T6. INSTALLED PER SRM 51-30-02 AND EC/RA 5310-04134.

Part: SKIN — DENTED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

EXTERNAL FUSELAGE. SKIN DENTED AT STA 256 LGL 30 BY DRAIN HOLE. CUT OUT DAMAGED AREA IAW 53-04 FIG 12B. FAB''D REPAIR DOUBLERS IAW 53-04 FIG 12B. DRILLED AND COUNTERSUNK IAW 51-10-04. TREATED AND PRIMED IAW 51-10-3 AND INSTALLED ALL PER 51-30-2, 4, 5.

Part: BRACKET — CORRODED (CARGO BAY) · airframe 48,173 hrs · 28,035 cycles

AFT PIT AFT TORQUE BOX WEB ATTACH BRACKET CORRODED. REMOVED, FABRICATED, AND INSTALLED NEW ATTACH BRACKET PER SRM 51-30-2, 51-10-4, AND 51-10-3 AND 5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,173 hrs · 280,235 cycles

AFT PIT FLOORBOARD SUPPORT IS CORRODED AT STATION 1193 - 1212 ABOVE THE TORQUE BOX WEB UPPER AND LOWER SIDES. REMOVED FLOOR SUPPORT. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-10-4. TREATED AND PRIMED PER SRM 51-30-2 AND 3.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 48,173 hrs · 28,035 cycles

FORWARD CARGO DOOR FORWARD LOWER INNER STRUCTURE BRACKET CRACKED (1 INCH). REMOVED BRACKET. FABRICATED NEW BRACKET AND ANGLE, INSTALLED PER SRM 51-30-2, 51-10-3, AND 51-30-5.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

AFT CARGO TORQUE WEB AFT OF DOOR CUTOUT FS 1215 HAS A HOLE PUNCTURED IN THE WEB. REMOVED AND REPLACED DAMAGED TORQUE WEB PER SRM 51-30-5, 51-10-4, AND 51-10-3.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 48,173 hrs · 28,035 cycles

FORWARD CARGO DOOR AFT LOWER CENTER INNER BRACKET IS CRACKED (1 INCH). REMOVED BRACKET. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-30-5, 51-10-4 AND 51-10-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

TAIL COMPARTMENT SHEAR TIE CRACKED AT STATION 1418 AND LONGERON 1. REMOVED SHEAR TIE, FABRICATED AND INSTALLED A SPLICE. TREATED AND PRIMED SHEAR TIE AND INSTALLED PER SRM 51-10-4, 53-03 FIG 3, 51-10-3, AND 51-30-5.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 48,173 hrs · 28,035 cycles

FORWARD CARGO DOOR AFT LOWER INNER STRUCTURE STIFFENER CRACKED (1 INCH). REMOVED DAMAGED STIFFENER. FABRICATED AND INSTALLED NEW STIFFENER PER SRM 51-30-2, 51-10-4, 51-30-5 AND 51-10-3.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

AFT ACCESSORY COMPARTMENT RIGHT LOWER END FS 1485 AND BELOW AFT STAIR TORQUE TUBE SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 51-30-1 AND 5.

Part: PAN — CORRODED (CARGO BAY) · airframe 48,173 hrs · 28,035 cycles

FOWARD CARGO PIT DOOR CUT-OUT LOWER PAN CORRODED. REMOVED AND REPLACED PAN PER SRM 53-05 FIG 44, 51-10-4, AND 51-10-3.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 48,173 hrs · 28,035 cycles

MID CARGO THRESHOLD SUPPORT IS CORRODED. REMOVED DAMEGED SUPPORT. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-30-1, 51-10-4, 51-10-3, AND 51-30-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

FLOORBEAM CORRODED AT AND UNDER NUT PLATE LOCATIONS AT STATION 1322 AND LBL 0 - LBL 54. REMOVED NUT PLATES AND CUT OUT DAMAGED AREAS. INSTALLED REPAIR ANGLES AND FILLERS PER SRM 51-30-2, 53-01 FIG 1, 53-05 FIG 204, 51-10-3, AND 53-05 FIG 202.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 48,173 hrs · 28,035 cycles

FORWARD CARGO DOOR EXTERNAL SKIN CRACKED AT LOWER FORWARD END (.5 INCH). STOP DRILLED CRACK. FABRICATED AND INSTALLED A REPAIR DOUBLER PER SRM 51-10-4, 51-30-3 AND 51-30-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER FLANGE IN FORWARD CARGO AREA AT FS 427-466, LONGERON 29R. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND LONGERON 30 IN E&E BAY UNDER BATTERY CHARGER CORRODED AT STA 110 - 120. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND SECOND I/B FROM LEFT SEAT TRACK CORRODED AT FS 1079 - 1309, LBL 44. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-3, AND 51-30-5.

Part: STRAP — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND AFT CARGO COMPARTMENT LOWER TORQUE BOX REPAIR STRAP CORRODED AT FS 1155-1212, LONGERON 28R. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-05, 51-10-3, AND ECRA 5310-03027.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND THE THIRD I/B FROM LEFT SEAT TRACK CORRODED AT FS 1098 - 1309, LBL 22. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-01, 51-10-4, AND 51-10-3.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND AFT PIT INTERCOSTAL CRACKED AT FS 1332 BETWEEN LONGERON 27R AND 28R, BELOW RT CARGO TRACK. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-10-3, 51-10-4, AND 51-30-5.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1120 - 1220. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-1, 51-10-3, AND 53-05.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND SHEAR TIE ON AFT SIDE OF FRAME IN AFT PIT CORRODED AT STA 1155 BETWEEN LONGERON 30 AND 29R. A T-ANGLE WAS INSTALLED IAW 51-10-4, 51-10-3, AND 51-30-5.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND CABIN LEFT O/B SEAT TRACK CORRODED AT FS 1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND A 2 INCH CRACK IN LT CUSP WEB AT LIGHTENING HOLE, STA 1295. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 96, 51-10-4, 51-10-5, 51-30-2, AND 51-30-5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT AND UNDER NUT PLATES AT STA 1309, BL 0 TO LBL 54.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND R-1 DOOR RT CUSP ANGLE CORRODED AT FS 216. THE CORRODED SECTION OF CUSP ANGLE WAS REMOVED AND A NEW CUSP ANGLE AND SPLICES WERE INSTALLED IAW SRM 53-05, FIGURE 55.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND LT FLOOR PANEL DELAMINATED AT FS 1031 - 1155. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: SKIN — CRACKED (LT WING) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND A 2.3 INCH CRACK IN LT WING LEADING EDGE SKIN O/B OF NR 7 SLAT TRACK. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-30-5 AND ECRA 5721-01064.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND AFT END OF LEFT I/B FLOOR PANEL CORRODED AROUND SCREW HOLES AT FS 1003-1079. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND AFT PIT RT CUSP WEB CRACKED AT STA 1271-1287, RBL 56. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. A DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND RT CABIN FLOOR PANEL DELAMINATED AT FS 1250 - 1309. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: SKIN — DENTED (CARGO DOOR) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND AFT PIT DOOR EXTERNAL SKIN DENTED. THE DENTED AREA WAS CUTOUT AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR PANELS M, N, O, AND P DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND FLOOR PANELS DELAMINATED AT CENTER SECTION FS 1079 - 1174, RT SECTION AT FS 1117 - 1174, AND CENTER SECTION AT FS 1117 - 1174. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND CABIN FLOOR PANEL HAD CORRODED INSERTS. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND CABIN FLOOR PANEL BBB DELAMINATED. A NEW FLOOR PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND L-1 DOOR FUSELAGE EXTERNAL SURFACE OF GUST LOCK LATCH SKIN CRACKED. REMOVED REPAIR FASTENERS AND INSTALLED DOUBLERS IAW SRM 53-04, FIGURE 24, 51-10-4, AND 51-10-3.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND CENTER FLOOR PANEL DELAMINATED AT FS 1309 - 1322. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND LT CABIN FLOOR PANEL AT FS 1079-1124 HAD CORRODED INSERTS. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND MAIN CABIN FORWARD ENTRY FLOOR PANELS A, C, D, E, F, G, H, I, AND J DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND RT CABIN FLOOR PANEL AT FS 886-927 HAD TWO EDGE CRACKS AND WEAR IN CENTER OF PANEL. A NEW PANEL WAS INSTALLED IAW ECRA 5320-01265.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND LT CABIN FLOOR PANEL DELAMINATED AT FS 769 - 826. THE PANEL WAS REPLACED IAW ECRA 5320-01265.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND CENTER FLOOR PANEL AT STA 946 - 1003 DELAMINATED AND LT FLOOR PANEL DELAMINATED AT STA 927 - 1003. THE FLOOR PANELS WERE REMOVED AND REPLACED IAW ECRA 5320-01265.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND RT FLOOR PANEL AT STA 866 - 886 DELAMINATED AND FLOOR PANEL AT STA 886 - 946 DELAMINATED. THE FLOOR PANELS WERE REPLACED IAW ECRA 5320-01265.

Part: WEB — CORRODED (FUSELAGE) · airframe 48,173 hrs · 28,035 cycles

INSPECTION FOUND FORWARD ENTRY SUBFLOOR CORRODED AT FS 218 - 225, LBL 42. A DOUBLER WAS INSTALLED IAW SRM 53-20-0 AND 51-30-2.

Part: BATTERY — DISCHARGED (ROW 22)

THE CEILING EMERGENCY LIGHTS AT ROW 23-32, EXIT SIGNS AT AFT SERVICE DOOR, LEFT AFT LAV WALL, AND THE CATWALK WOULD NOT TEST. THE BATTERY AT OVERHEAD BINS 25 AND 29 WAS REPLACED. REPLACED BLOWN FUSE AT AFT BATTERY CHARGER. REPAIRED WIRE AT AFT SERVICE DOOR SIGN. OPERATION OF ALL EMERGENCY LIGHTS CHECKED GOOD.

Part: RIB — CRACKED (NR 5 SLAT)

INSPECTION FOUND A 0.085 CRACK AT FASTENER HOLE OF LT O/B NR 5 SLAT SEAL RETAINING RIB. THE RIB WAS REMOVED IAW SRM 51-30-0. THE RIB WAS REPAIRED AND REINSTALLED IAW SRM 51-30-0, ECRA 5750-03253, AND EA 9-2780-2-AO467.

Part: SKIN — CRACKED (WS 286)

INSPECTION FOUND A 4 CRACK IN RT WING L/E UPPER SKIN AT NR 8 L/E SLAT TRACK, STA XOS 286. AN INTERNAL DOUBLER WAS INSTALLED AND A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION EVERY SERVICE CHECK AND PENETRANT EVERY SEVEN DAYS WITH A PERMANENT REPAIR TO BE INSTALLED AT NEXT 1/4D CHECK PER ECRA 5720-01725.

Part: RIB — CRACKED (LT WING)

INSPECTION FOUND A .5 CRACK IN LT WING L/E RIB APPROXIMATELY 12 INCHES O/B OF NR 8 SLAT TRACK AT TOP AFT ATTACH POINT TO SPAR. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-03 AND 51-30-0.

Part: SEAT TRACK — CORRODED (BS 1197)

INSPECTION FOUND RIGHT O/B SEAT TRACK GOUGED AT STA 1197, RBL 54. A NEW SEAT TRACK AND FITTINGS WERE INSTALLED SRM 53-05.

Part: FRAME — CORRODED (BS 1271)

INSPECTION FOUND AFT FACE OF CIRCUMFERENTIAL FRAME CORRODED AT FS 1271, LONGERON 27L TO 27R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 5.

Part: SKIN — DENTED (BS 47-68)

INSPECTION FOUND RT FUSELAGE EXTERNAL SKIN DENTED AT FS 47-68, STRINGER 19R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.

Part: SKIN — CRACKED (RT WING)

INSPECTION FOUND A 4 INCH CRACK IN RT WING LEADING EDGE UPPER SKIN AT NR 8 L/E SLAT TRACK. THE AREA WAS REPAIRED IAW ECRA 5720-01725. A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION EVERY SERVICE CHECK AND PENETRANT EVERY SEVEN DAYS WITH PERMANENT REPAIR AT NEXT 1/4D CHECK.

Part: OIL PUMP — FAILED (NR 2 ENGINE)

THE NR 2 ENGINE LOST OIL PRESSURE WHILE IN FLIGHT AND THE RIGHT OIL PRESSURE LIGHT ILLUMINATED. THE NR 2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* ANALYSIS REVEALED OIL PUMP BEARING FAILURE.

Part: SKIN — CORRODED (CARGO DOORWAY)

INSPECTION FOUND MID AND AFT CARGO DOOR CUTOUTS CORRODED AT LOWER END. THE CORROSION WAS REMOVED AND REPAIRS WERE INSTALLED IAW ECRA 5310-03027.

Part: ANGLE — CORRODED (L 1 ENTRY)

INSPECTION FOUND ANGLE AND WEB CORRODED JUST INSIDE THRESHOLD AREA OF L-1 ENTRYWAY. THE ANGLE WAS REMOVED AND THE WEB WAS CUT OUT, A NEW WEB AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-01 AND 51-30-02.

Part: DOUBLER — CRACKED (BS 946)

INSPECTION FOUND A .25 INCH CRACK AT WINDOW FRAME DOUBLER, FS 946, LONGERON 11L. THE CRACK WAS STOP DRILLED, A DOUBLER AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-01 AND ECRA 5330-02568.

Part: DOUBLER — CRACKED (BS 883)

INSPECTION FOUND A .25 INCH CRACK THROUGH FASTENER HOLE AT WINDOW FRAME DOUBLER, FS 883, LONGERON 11L. REMOVED FASTENERS, FABRICATED AND INSTALLED ANGLE IAW SRM 53-01, FIGURE 2, SHEET 3 AND ECRA 5330-02568.

Part: FRAME — CRACKED (FWD ENTRY DOOR)

INSPECTION FOUND A 1.5 INCH CRACK IN LOWER FORWARD CORNER OF FORWARD ENTRY DOOR FRAME. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05.

Part: O-RING — LEAKING (FUEL LINE)

A STRONG SMELL OF KEROSENE WAS OBSERVED IN THE CABIN NEAR AFT JUMPSEAT AND GALLEY JUMPSEAT ON LANDING. MAINTENANCE FOUND FUEL LEAKING FROM FUEL LINE UNION/ELBOW AT THE APU ATOMIZER. THE O-RING WAS REPLACED AND NO LEAKS WERE NOTED DURING OPERATION OF APU.

Part: CLIPS — OUT OF ADJUST (TAILCONE)

HOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLED FROM CLIPS AT 45 POUNDS. THE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00. (M)

Part: SKIN — CRACKED (NR 1 LE FLAP)

HOU - DURING INSPECTION, FOUND A 3 INCH CRACK IN NR 1 SLAT SKIN ON THE LOWER SIDE. THE SLAT WAS REPAIRED IAW ECRA 5750-02346. (M)

Part: BELTFRAME — CORRODED (BS 598)

HOU - INSPECTION FOUND CORROSION ON BELTFRAME IN MID CARGO BIN AT STATION 598. THE BELTFRAME WAS REPAIRED BY REMOVING CORROSION IAW SRM 53-01, FIGURE 1. (M)

Part: BELTFRAME — CORRODED (BS 636)

HOU - INSPECTION FOUND CORROSION ON BELTFRAME IN AFT CARGO BIN AT STATION 636. THE BELTFRAME WAS REPAIRED BY REMOVING CORROSION IAW SRM 53-01, FIGURE 1. (M)

Part: SKIN — DENTED (RUDDER TAB)

HOU - DURING INSPECTION, FOUND THREE DENTS ON RIGHT SIDE OF RUDDER TAB. THE DENTS WERE REPAIRED PER SRM 55-04 AND 55-40-1. (M)

Part: TE PANEL — DELAMINATED (NR 1 TE FLAP)

HOU - INSPECTION FOUND THE LOWER TRAILING EDGE PANEL DELAMINATED JUST OUTBOARD OF NR 1 FLAP HINGE. THE PANEL WAS REPAIRED PER SRM 51-90-0. (M)

Part: SKIN — DENTED (BS 207-256)

HOU - DURING INSPECTION, FOUND SEVERAL DENTS IN SKIN AT STATION 207 TO 256, LONGERONS 15, 16, AND 17. THE DENTS WERE REPAIRED IAW ECRA 5330-02309. (M)

Part: TE SKIN — DELAMINATED (RUDDER TAB)

HOU - INSPECTION FOUND THE UPPER TRAILING EDGE OF RUDDER TAB DELAMINATED THE RUDDER TAB WAS REPAIRED IAW SRM 55-04. (M)