N33817

Part: SPAR — CRACKED (VERT STAB) · airframe 55,172 hrs · 26,152 cycles

INSPECTION FOUND A 10 INCH CRACK IN VERTICAL STABILIZER L/H FRONT SPAR AT LOWER END AT CANTED BULKHEAD STA 1388. INSTALLED DOUBLERS IAW SRM 55-02, FIGURE 26.

Part: SEAT TRACK — CORRODED (STA 229) · airframe 55,172 hrs · 26,152 cycles

INSPECTION FOUND R/H O/B SEAT TRACK CORRODED AT STA 229. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 51-30-02.

Part: SEAT TRACK — CORRODED (STA 229) · airframe 55,172 hrs · 26,152 cycles

INSPECTION FOUND R/H INBOARD SEAT TRACK CORRODED AT STA 229. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 55,073 hrs · 26,094 cycles

INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT COCKPIT, FORWARD ENTRY CEILING, AND SERVICE ENTRY CEILING. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS GOOD.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 53,258 hrs · 25,171 cycles

SMOKE ENTERED THE CABIN WHILE AT CRUISE EN ROUTE TO TPA. THE RECIRCULATING FAN C/B'S ALSO POPPED. THE CABIN TEMP WAS LOWERED AND GALLEY POWER WAS REMOVED. THE SMOKE DISSIPATED AND THE AIRCRAFT LANDED SAFELY AT TPA. THE RECIRCULATING FAN WAS REMOVED AND REPLACED.

Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 52,334 hrs · 24,697 cycles

CABIN FORWARD SET OF EMERGENCY LIGHTS ON AFTER POWER TURNED OFF. EMERGENCY PACK BAD. REMOVED AND REPLACED BATTERY PACK AND BATTERIES PER MM 33-53-00. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,564 hrs · 24,297 cycles

THE FORWARD SERVICE AND FORWARD GALLEY AND COCKPIT OVERHEAD EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST. THE BATTERIES IN FORWARD DROP PANEL BATTERY PACK (STA 213) WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00.

Part: RIB — CRACKED (RT WING) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND RT WING LEADING EDGE I/B RIB AND DOUBLER CRACKED AT WS XRS 267-295. THE RIB WAS REMOVED AND TWO REPAIR DOUBLERS WERE INSTALLED IAW EA 9-5721-2-A0744 AND ECRA 5720-01810.

Part: RIB — CRACKED (RT WING) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A CRACK IN RT WING LEADING EDGE O/B RIB AT WS XRS 267-295. REPAIR ANGLE WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-05 AND 57-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-05, EA 9-5720-2-A0742, AND ECRA 5720-01810.

Part: RIB — CRACKED (RT WING SLAT) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A CRACK IN RT WING LEADING EDGE SLAT MID RIB AT WS XRS 267-295. THE RIB WAS REPAIRED IAW EA 9-5720-2-A0742 AND ECRA 5720-01810.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND DOUBLER CORRODED AT FS 693, L29L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND ECRA 5310-04033.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 1 INCH CRACK IN LEFT I/B LEADING EDGE HORIZONTAL STABILIZER FAIRING. THE OLD DOUBLER WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT CARGO FRAME CORRODED ON FORWARD AND AFT SIDES BELOW SUPPORT AT FS 1251. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED WITH SPLICE AND CHANNEL IAW SRM 53-03, FIGURE 2A, 51-30-08, AND 51-30-05.

Part: STRUCTURE — CORRODED (LAV SERVICE DOOR) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT LAV SERVICE DOOR CORRODED UNDER HINGE. THE SERVICE DOOR WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: PANEL — CRACKED (RT WING) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 5 INCH CRACK IN RIGHT WING REFUELING PANEL ON O/B END AT CAMLOCK. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, 51-30-02, AND 51-30-01.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT LAV SERVICE DOOR CUTOUT DOUBLER GOUGED, CHAFED, AND CORRODED AT FS 1308. THE AFT LAV SERVICE DOOR CUTOUT DOUBLER WAS REPAIRED IAW ECRA 5332-01008 AND EA 9-5332-2-A0735A.

Part: SPACER — CORRODED (CARGO DOOR JAMB) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT CARGO DOOR JAMB HAD AREAS OF CORROSION, AT FS 1211. REMOVED DOUBLER IAW SRM 51-30-5. A NEW SPACER WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 2.3 INCH CRACK IN LEFT UPPER WING TO BODY ATTACH BRACKET AT FS 927, LONGERON 18L. THE BRACKET WAS REMOVED AND A REPLACEMENT BRACKET WAS INSTALLED IAW SRM 51-30-2.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL ATTACH FITTING OF MID CARGO DOOR LOWER AFT STOP. THE T-ANGLE WAS ALSO FOUND CRACKED. THE ATTACH FITTING AND T-ANGLE WERE REMOVED AND A NEW ATTACH FITTING AND ANGLE WERE INSTALLED IAW SRM 51-10-4, 51-30-5, 51-30-1, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1155 - 1211. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: RIB — MISDRILLED (RT WING) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND RT WING TRAILING EDGE RT I/B (I/B SIDE) UPPER AND LOWER CLOSURE RIBS HAD NO EDGE DISTANCE ON TWO FORWARD HOLES. THE END ASSEMBLY WAS REMOVED IAW SRM 51-30-2. REPAIR PARTS WERE INSTALLED IAW SRM 51-10-4 AND 51-30-2.

Part: BEAM — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED AT FS 636 - 693, LONGERON 28R. A DOUBLER AND SPACER REPAIR WAS INSTALLED IAW SRM 51-30-5 AND ECRA 5310-03027.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CORROSION AROUND HI-LOKS AND LOWER SKIN AT FS 674, LONGERON 29R - 30R. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5332-01007.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND LT CARGO TRACK CORRODED AT STA 1007 - 1155, LONGERON 27L. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 53-05 AND 51-10-3.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT CARGO AFT RT TRACK CORRODED AROUND CLIP NUTS AT FS 1211 - 1320, LONGERON 27R. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: STRAP — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT CARGO FRAME STRAP ON TOP OF FRAME CORRODED AT STA 1231, LONGERON 28R. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND LT CARGO TRACK CORRODED AT FS 1211 - 1309, LONGERON 27L. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4G.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT CARGO DOOR AFT EDGE DENTED AND GOUGED AT CENTER TO LOWER STOP AREAS. THE DENTED AREA WAS REFORMED IAW SRM 51-10-4. THE GOUGED AREA WAS TRIMMED OUT AND A DOUBLER WAS INSTALLED IAW ECRA 5330-02819.

Part: STRAP — WORN (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND MID CARGO TORQUE BOX STRAP FASTENER HOLES WORN AT FS 636. THE TORQUE BOX WEB STRAP, FIVE INTERCOSTALS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. DAMAGED FRAME WAS REPAIRED IAW EA 9-5312-2-A0728. ANGLES, INTERCOSTALS, FILLER, STRAP, AND WEB WERE INSTALLED IAW SRM 51-10-3, 51-10-4, AND ECRA 5311-01102.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 2 INCH CRACK IN RT HORIZONTAL STABILIZER BANANA FAIRING. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 AND 55-01-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 886 - 1041, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 200, LBL 4 TO RBL 4. THE FLOOR SUPPORT WAS REMOVED AND NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FORWARD CARGO TIE DOWN TRACK CORRODED AT FS 218 - 522, LT SIDE. THE CARGO TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-3.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 4 INCH CRACK IN LT CUSP WEB AT FS 1288, LBL 58. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2, SECTION 3. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1, SECTION 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1136, LBL 56 AND AT FS 1138, LBL 55. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND LT CUSP WEB CORRODED AT FS 1098 - 1170. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-30-5, 51-10-3, AND 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294, LONGERON 18L. THE DENT WAS COLD WORKED. SHEAR TIE WAS REMOVED AND REPLACED AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2, 51-30-5, AND 53-04, FIGURE 38.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FORWARD ENTRY AREA SUPPORT CORRODED AT FS 200 - 218, LBL 14. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-02 AND 51-10-04.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FRAME LOWER LOBE CORRODED AROUND FASTENERS AT STA 1231, LONGERON 24R TO 24L. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-02 AND 51-30-05.

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND LEFT O/B CABIN FLOOR PANEL CRACKED AT EDGES, STA 541 - 617. THE CRACKED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4B. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 4B, 51-10-3, AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FORWARD ENTRY AREA SUPPORT CORRODED AT STA 160 - 170, LBL 48. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CUSP WEB CORRODED BETWEEN FS 1193 AND 1250, LT SIDE. THE CUSP WEB WAS REMOVED AND A NEW CUSP WEB WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-1, 51-30-2, AND 51-30-5.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CUSP WEB CORRODED AT FS 218, RBL 54. THE CORRODED AREA OF WEB WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, AND 53-01, FIGURE 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED AT FS 256, LBL 10 TO RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-05, 53-14-02, 51-10-04, AND 51-30-05.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN WINDOW FRAME AT UPPER AFT CORNER, STA 1003, LONGERON 11L. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-03 AND ECRA 5330-02569.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 160, RBL 10 AND AT STA 160 - 200, LBL 50. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-02, 51-10-04, 51-30-05, AND 51-10-03.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT AT FS 148, RBL 3. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01 AND 51-30-02.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A .75 INCH CRACK AND LOOSE RIVETS IN RT WING SLAT NR 3 AT AFT SIDE. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3 AND 51-10-04.

Part: SKIN — DENTED (CARGO DOOR) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND MID CARGO DOOR OUTER SKIN DENTED IN AFT UPPER SECTION. THE DENTED AREA WAS REMOVED. DOUBLER, FILLER, AND ANGLES WERE INSTALLED IAW SRM 52-05, FIGURE 5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1155 BETWEEN LEFT I/B AND O/B AND I/B SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FORWARD ENTRY AREA SUPPORTS CORRODED AT FS 160 - 200, LBL 5 AND LBL 40. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-01, 51-30-04, 51-10-03, AND 51-30-05.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOORBEAM CHAFED AT FS 653, RBL 22. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIGURE 86, 51-10-04, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FORWARD ENTRY AREA SUPPORT CORRODED AT FS 180, RBL 6 - 36. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, LBL 18 - 36 AND RBL 10 - 36. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-02, AND 51-30-05.

Part: FITTING — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FRAME FITTING AT FS 1139, LONGERON 18L CORRODED. THE FRAME FITTING WAS REMOVED AND A NEW FRAME FITTING WAS INSTALLED IAW SRM 51-10-04, 51-30-05, AND 51-30-01.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CUSP WEB CORRODED AT STA 160 - 200, LBL 5. A DOUBLER WAS INSTALLED IAW SRM 51-10-02, 51-10-04, 51-10-03, 51-20-0, AND 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1171, LBL 56. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND 51-30-02.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND TWO FLOOR STIFFENERS CORRODED AT STA 1145 - 1168, LBL 54. THE STIFFENERS WERE REMOVED AND NEW STIFFENERS WERE INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1079. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-05.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SKIN CORRODED AT FS 160, RBL 10. TWO FLOOR SUPPORTS WERE REMOVED TO FACILITATE MAINTENANCE. FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01 AND 51-10-04. THE FLOOR SUPPORTS WERE REINSTALLED IAW SRM 51-10-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CABIN LEFT I/B SEAT TRACK CORRODED AT FS 1117 - 1309. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01, 51-30-05, AND 53-05, FIGURE 4.

Part: ANGLE — CRACKED (NR 8 SLAT TRACK) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 12 INCH CRACK IN RT WING FIXED L/E RIB SUPPORT ANGLE AT PANEL O/B OF TRACK NR 8. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-05, 51-10-02, 51-10-04, AND 51-10-03.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CABIN FLOORBEAM CORRODED UNDER AND AROUND NUT PLATES AT FS 1322, RBL 22 - 58. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 20A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1170, LBL 55. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND GALLEY FITTING CORRODED AT FS 218, RBL 56. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-04 AND 51-30-02.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLIGHT COMPARTMENT FLOOR CUSP WEB PUNCTURED AT FS 150, RBL 3. THE PUNCTURED AREA WAS CUT OUT IAW SRM 53-01, FIGURE 4. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 51-10-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1249, LONGERON 21R. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-20, AND 51-30-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 3.5 INCH CRACK IN CUSP WEB AT FS 1032, RBL 44.5. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-14-3, FIGURE 12, 53-01, FIGURE 2, 51-10-3, AND 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND LT CARGO TRACK CORRODED UNDER NUT PLATES AT LOWER SURFACE, FS 522 - 788. THE TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS INSTALLED IAW SRM 51-30-01 AND 53-05, FIGURE 1C.

Part: STRAP — CORRODED (PAX DOOR) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND R-1 DOOR THRESHOLD COVER STRAP CORRODED. THE THRESHOLD COVER STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-05.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND AFT RT MID PIT CARGO TRACK CORRODED UNDER CLIP NUTS. THE CARGO TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS INSTALLED IAW SRM 51-30-01 AND 53-05, FIGURE 1C.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT FS 1338, LBL 20 TO LBL 50 AND AT FS 1322, LBL 20 TO LT SIDE WALL. THE CORRODED AREAS WERE CUT OUT AND BLENDED IAW SRM 53-05, FIGURE 20A. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW SRM 51-10-04, 51-10-03, 51-30-05, AND 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1309 TO AFT DOOR JAMB, LBL 20 AND RBL 20. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-01, 51-10-04, 51-10-03, AND 51-30-07.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND INTERCOSTAL CORRODED ON LOWER LEG AT FS 1145 - 1155, LONGERON 30. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW 51-10-04, 51-10-03, 51-30-02, 51-30-05.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CUSP WEB CORRODED AT FS 160 - 190, RBL 48. THE AREA WAS REPAIRED IAW SRM 53-01, FIGURE 2. TWO FLOOR SUPPORTS WERE REINSTALLED IAW SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT R-1 DOOR LOWER JAMB AFT PANEL, FS 200 - 210. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-05, 51-30-0, AND 51-30-01.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND R-1 DOOR FORWARD AND AFT GIRT BAR ATTACH FITTINGS CORRODED. THE GIRT BAR FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 223 BETWEEN LONGERON 17L AND 18L. THE DENTED AREA OF SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, 51-30-5, AND ECRA 5330-02471.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237, LONGERON 7L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 1/2 INCH CRACK IN ANGLE AT AFT RT SIDE OF FRAME, STA 1322. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-24-0, 51-10-03, AND 51-30-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT FITTING CORRODED AT FS 160, LBL 14. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-05, 51-10-04, AND 51-10-03.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO CUSP WEB AT FS 218, RBL 40. THE CUSP WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-04, 51-30-02, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160-200, RBL 5. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1211, LONGERON 27 LT - 27 RT. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-04 AND 51-30-02.

Part: FLOOR SUPPORT — CORRODED (FS 180-218) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 180, LBL 12 - 24 AND AT FS 218, LBL 10 - RBL 10. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,001 hrs · 22,919 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AT FS 1134, LBL 30. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: RIB — CRACKED (WS 270-289)

INSPECTION FOUND THREE .75 INCH CRACKS IN RT WING LEADING EDGE RIBS AT STA XRS 276.5, XRS 270, AND XRS 289. THE RIBS WERE REMOVED AND NEW RIBS WERE INSTALLED IAW ECRA 5721-01008.

Part: FRAME — CORRODED (BS 1271)

INSPECTION FOUND BELTFRAME CORRODED IN AFT BAGGAGE BIN AT STA 1271, LONGERON 30. A BELTFRAME AND SPLICES WERE INSTALLED IAW SRM 53-03, FIGURE 2A.

Part: SKIN — DAMAGED (BS 1065)

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 1065 BETWEEN LONGERON 2L AND 3L. THE SKIN WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 38.

Part: JAMB — CORRODED (CARGO DOORWAY)

INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR JAMB PAN CORRODED. THE CORRODED SECTION OF PAN WAS REMOVED. REPAIR SPLICES WERE FABRICATED AND THE NEW SECTION OF PAN WAS INSTALLED IAW SRM 53-05, FIGURE 44.

Part: FRAME — CORRODED (BS 1309)

INSPECTION FOUND AFT BAGGAGE BIN BELTFRAME CORRODED AT STA 1309 FROM LONGERON 27L TO 27R. A NEW BELTFRAME WAS INSTALLED IAW SRM 53-03.

Part: TIEDOWN RAIL — CORRODED (BS 1212-1231)

INSPECTION FOUND AFT BAGGAGE BIN LEFT TIE DOWN RAIL AT SPLICE BETWEEN STA 1212 AND 1231 CORRODED AROUND NUT PLATE HOLES. A REPAIR WAS INSTALLED IAW ECRA 5320-01523.

Part: SKIN — DENTED (BS 275-294)

INSPECTION FOUND FUSELAGE SKIN DENTED IN FORWARD LAV SERVICE AREA BETWEEN STA 275 AND 294 ABOVE LONGERON 21L. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION FOUND A 1.375 INCH CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: T4 BLADE — FAILED (NR 2 ENGINE)

TAKEOFF WAS ABORTED AT APPROXIMATELY 50 KNOTS AFTER THE NR 2 ENGINE LOST POWER. THE POWER LOSS WAS ACCOMPANIED BY A LOUD POP. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE NR 2 ENGINE TURBINE HAD FAILED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED A T-4 BLADE FAILURE.

Part: CENT SWITCH — INOPERATIVE (APU)

THE APU HAD A HISTORY OF AUTO SHUTDOWN DURING CLIMB PORTION OF FLIGHT AROUND FL250. THE APU HAD BEEN TEMPORARILY PLACARDED INOPERATIVE. WHILE TROUBLESHOOTING PROBLEM IN EWR, THE APU CENTRIFUGAL SWITCH WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD AND THE PLACARD WAS REMOVED. THE AIRCRAFT HAS FLOWN OVER EIGHT FLIGHTS WITHOUT A REPEAT OF APU PROBLEMS SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED.

Part: BATTERIES — DISCHARGED (CABIN)

INSPECTION FOUND FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND THE OPERATION OF THE LIGHTS WAS RESTORED.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.

Part: FRAME — WORN (BS 1380)

INSPECTION FOUND FRAME WEB REPAIR DOUBLER WORN IN TAIL COMPARTMENT AT STA 1380, LONGERON 5L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-01.

Part: STOP PAD — CORRODED (CARGO DOOR)

INSPECTION FOUND MID CARGO DOOR LOWER AFT STOP PAD CORRODED. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05.

Part: CIRCUMFERENTIAL — CORRODED (BS 1231)

INSPECTION FOUND CIRCUMFERENTIAL CORRODED AT STA 1231 BETWEEN LONGERON 27R AND 27L. THE CORRODED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 2A.

Part: SILL — CORRODED (AFT CARGO DR)

INSPECTION FOUND THE AFT CARGO DOOR SILL FORWARD FACE CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63.

Part: FITTING — CORRODED (BS 1155)

INSPECTION FOUND AFT CARGO FITTING CRACKED AND CORRODED AT STA 1155, LONGERON 29R TO 30R. A REPLACEMENT FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-00 AND 51-10-3.

Part: WEB — CORRODED (BS 198)

INSPECTION FOUND MAIN ENTRY FLOOR WEB CRACKED AT STA 198, LBL 60 WITH CORROSION UNDER CIRCUMFERENTIAL FRAME AT STA 200L. THE CORRODED AREA WAS CUT OUT, A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5310-03285.

Part: FITTING — CORRODED (DOOR CUTOUT)

INSPECTION FOUND CORNER FITTING CORRODED AT LOWER FORWARD CORNER OF CENTER PIT DOOR CUTOUT. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-10-3.

Part: ANGLE — CRACKED (BS 522)

INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF VERTICAL ANGLE AT AFT SIDE OF STA 522 BULKHEAD ABOVE LONGERON 24L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-20 AND 51-10-3.

Part: FRAME — PUNCTURED (BS 522)

INSPECTION FOUND LOWER FRAME AT AFT SIDE OF STA 522 BULKHEAD PUNCTURED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01.

Part: FLAP VANE — GOUGED (RT TE FLAP)

INSPECTION FOUND RT WING OUTBOARD FLAP MIDDLE VANE LOWER LEADING EDGE SKIN GOUGED. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-70-2.

Part: SUPPORT — CORRODED (BS 140-200)

INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 140 TO 200, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-05, 53-00 AND 51-10-3.

Part: SUPPORT — CORRODED (BS 160-200)

INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 160 TO 200, LBL 60. THE FLOORBOARD SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-3.

Part: SKIN — GOUGED (BS 1316)

INSPECTION FOUND RT FUSELAGE SKIN GOUGED AT STA 1316, 8 INCHES BELOW CUSP LINE. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-04.

Part: SKIN — GOUGED (BS 207)

INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 207, LONGERON 13L. A DOUBLER WAS INSTALLED IAW SRM 53-04, PAGE 218F.

Part: SKIN — DENTED (BS 262)

INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 262 BETWEEN LONGERONS 23 AND 24L. THE DAMAGED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, PAGE 218.

Part: VANE — GOUGED (LT TE FLAP)

INSPECTION FOUND LT INBOARD FLAP VANE LOWER SURFACE GOUGED AND DENTED. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-70-2.

Part: PANEL — CRACKED (RT WING TE)

INSPECTION FOUND A 10 INCH CRACK AT OUTBOARD END OF RT WING UPPER TRAILING EDGE PANEL LOWER SURFACE, AFT OF RIGHT GEAR. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: SKIN — DENTED (BS 229-237)

INSPECTION FOUND LT FUSELAGE SKIN DENTED IN THREE PLACES ABOVE CUSP LINE AT STA 229 TO 237. THE DAMAGED AREA WAS CUT OUT AND A FLUSH REPAIR WAS INSTALLED IAW ECRA 5330-02410.

Part: SKIN — DENTED (BS 219-229)

INSPECTION FOUND LT FUSELAGE SKIN DENTED IN THREE PLACES ABOVE CUSP LINE BETWEEN STA 219 TO 229, LONGERON 17L AND 18L. THE DAMAGED AREA WAS CUT OUT AND A FLUSH REPAIR WAS INSTALLED IAW ECRA 5330-02410.

Part: ANGLE — CRACKED (WS 270)

INSPECTION FOUND A .5 INCH CRACK IN RIB SUPPORT ANGLE INSIDE LEADING EDGE, 13 INCHES OUTBOARD OF NR 8 SLAT TRACK AT XRS 270. A SUPPORT ANGLE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-01.

Part: RIB — CRACKED (LE FLAP)

INSPECTION FOUND A 1.25 INCH CRACK AT INBOARD ROOT RIB OF RT WING SLAT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-02, FIGURE 2.

Part: GEN CONTL PANEL — INOPERATIVE (OVERHEAD PANEL)

FLT NR 1994 - IAH - THE LEFT GENERATOR TRIPPED OFF FOLLOWED BY ILLUMINATION OF THE DC EMERGENCY BUS OFF LIGHT. THE GENERATOR BUS OFF LIGHT PROCEDURES WERE FOLLOWED AND THE DC BUS CROSSTIE SWITCH WAS CLOSED. THE DC EMERGENCY BUS LIGHT CAME ON AND THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND THE LEFT GCU AT FAULT. THE LEFT GCU WAS REMOVED AND REPLACED. THE ENGINES WERE RUN AND THE SYSTEM CHECKED GOOD. (M)

Part: FIRELOOP — CHAFED (LT ENGINE)

FLT NR 0499 - IAH - THE LEFT ENGINE 'A' LOOP FIRE DETECTION LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO IAH. THE ENGINE WAS BROUGHT TO IDLE AND THE AIRCRAFT LANDED AT IAH. THE ENGINE WAS SHUTDOWN AND BOTH FIRE BOTTLES WERE DISCHARGED AFTER LANDING. MX FOUND NO EVIDENCE OF FIRE. CHAFED WIRES WERE FOUND ON THE LEFT ENGINE FIRELOOP. THE WIRES WERE INSULATED AND SECURED. IN ADDITION, A PRBC LINE WAS FOUND LOOSE AND BLOWING ABOVE PYLON LOOP. THE PRBS LINE WAS SECURED. THE ENGINES WERE RUN AT TAKEOFF POWER FOR FIVE MINUTES AND NO DEFECTS WERE NOTED. BOTH ENGINE FIRE BOTTLES WERE REPLACED. (M)