N10834

Part: STRINGER — CRACKED (HORIZONTAL STAB) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A 2 INCH CRACK IN HORIZONTAL STABILIZER DOG HOUSE STRINGER. THE CRACKED AREA WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 51-30-2, 53-01, AND 55-01, FIGURE 2.

Part: PAN — GOUGED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FORWARD CARGO DOOR TOP PAN FLANGE GOUGED AT STOP. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW 51-10-02, 51-30-02, 51-10-03, AND ECRA 5330-02819.

Part: RETAINER — CRACKED (NR 1 ENGINE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND NR 1 ENGINE APRON FORWARD UPPER SUPPORT (RETAINER) BENT WITH A SIX INCH CRACK. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR UPPER AFT INNER ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND AFT SIDE OF FRAME CORRODED AT STA 1309, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 2A, SHEET 1, PAGE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND SHEAR TIE CORRODED AT STA 1287, LONGERON 30 TO 29R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180 - 208, LONGERON 18L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-30-2.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND TWO 3 INCH CRACKS IN MID CARGO DOOR I/B SKIN. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, LBL 16 - 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A .5 INCH CRACK IN RT MLG I/B DOOR AFT LOWER CORNER AT REPAIR DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-1.

Part: PANEL — CORRODED (LT WING) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND LT LOWER FUEL PANEL NR 1363 CORRODED ON MOUNT FACE AND IN COUNTERSINK. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW MM 51-30-2.

Part: NUT PLATE — CORRODED (TORQUE BOX) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND CORROSION AROUND AND UNDER NUT PLATES INSIDE AFT CARGO LOWER TORQUE BOX AT FS 1183, LONGERON 27R AND 28R. THE TORQUE BOX WAS REPAIRED IAW ECRA 5310-04023.

Part: STRUCTURE — BENT (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND THE AFT LOWER CORNER OF AFT CARGO DOOR BENT. REPAIRED AREA IAW ECRA 5230-01557.

Part: PAN — GOUGED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND AFT CARGO DOOR PAN GOUGED AT STOP NR 5 ON FORWARD EDGE AND AT STOP NR 4 ON AFT EDGE. BOTH AREAS WERE REPAIRED IAW ECRA 5330-02819.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A .5 INCH CRACK IN SUPPORT AT TAIL COMPARTMENT RT SIDE IN CEILING JUST AFT OF FRAME STA 1380. THE CRACK WAS STOP DRILLED AND A STACKED ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 53-01.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND LT CARGO TIE DOWN TRACK IN AFT PIT CORRODED AROUND CLIP NUT HOLES AT FS 1155 - 1320, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4.

Part: STOP — GOUGED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FORWARD CARGO DOOR FORWARD SEAL FLANGE DOOR STOPS A-E GOUGED. REPAIRED AREAS IAW ECRA 5330-02819.

Part: SKIN — DENTED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED JUST ABOVE AFT ACCESS PANEL. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 1 AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND MID CARGO RT TRACK AFT OF DOOR CORRODED UNDER NUT CLIPS AT FS 683 - 786, LONGERON 27R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 24L. THE SKIN WAS REPAIRED IAW SRM 53-04, SHEETS 12 & 20.

Part: RIB — CRACKED (RT WING) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A 6 INCH CRACK IN RT WING L/E RIB AT TRACK NR 8, XRS 248. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A REPAIR ANGLE WAS INSTALLED IAW SRM 57-10, FIGURE 3 AND 51-30-2.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND SUPPORT CHANNELS CRACKED AT CENTER FLOOR PANEL BETWEEN FS 886 AND 946. THE CRACKS WERE 2 INCHES LONG. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30-1. THE SUPPORT CHANNELS WERE REMOVED AND NEW CHANNELS WERE INSTALLED IAW 51-10-4 AND 51-30-0. THE FLOOR PANEL WAS REINSTALLED IAW SRM 51-30-0.

Part: SUPPORT BRACKET — CRACKED (FAIRING) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A .5 INCH CRACK IN EXTERNAL FUSELAGE LOWER SURFACE WING TO BODY FAIRING SUPPORT TEE AT FS 916. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-5.

Part: SKIN — CANNING (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND RIGHT FUSELAGE SKIN OIL CANNING AT STA 484, LONGERON 23R-24R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED WITH A .5 INCH CRACK AT FS 315 BETWEEN LONGERON 22L AND 23L. THE DENT WAS BLENDED OUT IAW SRM 53-04, FIGURE 38. THE CRACK WAS CUT OUT AND A FINGER DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51-30-2.

Part: PAN — GOUGED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FORWARD CARGO DOOR FORWARD PAN FLANGE STOPS H-L GOUGED. THE GOUGED AREAS WERE TRIMMED OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-02819, SRM 51-10-3, 51-10-4, AND 51-30-2.

Part: VANE — CRACKED (RT WING) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A .25 INCH CRACK IN NR 2 RT FIXED VANE I/B LOWER SURFACE. REPAIRED AND BONDED DOUBLER WITH RIVETS IAW SRM 57-04 AND 51-71-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT FS 1032 - 1309, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, AND 51-10-3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND LT AFT UPPER FUSELAGE SKIN CORRODED AROUND FASTENERS JUST BELOW DORSAL FIN AT STA 1429 - 1435. A REPAIR STRAP WAS INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND MID CARGO TIE DOWN TRACK CORRODED AT FS 595 - 785, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1088 - 1231. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 4.

Part: PAN — CRACKED (CARGO DOOR) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD DOOR CAM AREA. THE OLD DOUBLER WAS REMOVED AND A NEW DOOR PAN DOUBLER WAS INSTALLED IAW SRM 51-30-2, 52-05, FIGURE 26A, 51-10-4, 51-10-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 218 - 238. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-3, 51-10-4, 51-30-1, 51-30-5, AND 51-30-6.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT FS 670, RBL 22.5. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, FIGURE 4F, AND 51-10-3.

Part: MOUNT — CORRODED (GALLEY) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND G-2 GALLEY I/B FORWARD MOUNT FITTING CORRODED. THE FITTING WAS REMOVED AND AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,691 hrs · 19,773 cycles

INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-4.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND HOLE PUNCTURED IN RT CUSP WEB UNDER FLOOR SUPPORT AT FS 200, RBL 44. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2. THE FLOOR SUPPORT WAS REINSTALLED IAW SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, LBL 44.5 AND STA 180, LBL 16 - 36. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,691 hrs · 19,773 cycles

INSPECTION FOUND SEAT TRACK LUGS CORRODED AT FS 378, RBL 22.5. THE SEAT TRACK WAS REMOVED AND NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 53-05-4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 200 AND 250, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5.

Part: ATTACH ANGLE — CRACKED (THRESHOLD) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND R-1 DOOR THRESHOLD AFT ATTACH ANGLE CRACKED AND CORRODED. THE ANGLE AND DOUBLER WERE REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND FLOOR SUPPORT AT L-2 DOOR, STA 1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.

Part: RIB — CRACKED (TE FLAP) · airframe 41,690 hrs · 19,773 cycles

INSPECTION FOUND A 3 INCH CRACK IN I/B RIB OF RIGHT FLAP WEDGE ASSEMBLY NR 6. THE CRACK WAS DRILLED OUT AND A NEW RIB WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5.

Part: TAIL CONE — WARPED (AFT FUSELAGE)

THE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00.

Part: SKIN — DENTED (BS 229-237)

INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229-237 ABOVE CUSP LINE. A REPAIR WAS INSTALLED IAW ECRA 5330-02687.

Part: BEAM — CORRODED (BS 636/1155)

INSPECTION FOUND CORROSION ON MID BAG BIN Z BEAM AT THRESHOLD, STA 636-693. CORROSION WAS ALSO FOUND ON AFT BAG BIN Z BEAM AT THRESHOLD STA 1155-1212. REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 63.

Part: RAIL — CORRODED (BS 1060-1155)

INSPECTION FOUND RT TIEDOWN RAIL CORRODED AT STA 1060-1155. A NEW TIEDOWN RAIL WAS INSTALLED IAW SRM 51-30-0.

Part: DOOR BEAM — CRACKED (PAX DOOR)

INSPECTION FOUND A .375 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-0.

Part: BEAM — CRACKED (SERVICE DOOR)

INSPECTION FOUND A .75 INCH CRACK IN NR 4 HORIZONTAL BEAM OF FORWARD SERVICE DOOR. A NEW BEAM WAS INSTALLED IAW SRM 51-60-0.

Part: VANE CLUSTER — FAILED (NR 1 ENGINE)

THE NR 1 ENGINE GAVE OFF A LOUD POP AND ART FIRED DURING CLIMBOUT AT 1,000 FEET. THE ENGINE EPR WAS AT 1.12 AND VIBRATION WAS STEADY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. *S/D* TEARDOWN REVEALED FAILURE OF T-2 VANE CLUSTER.

Part: SKIN — DENTED (PAX DOOR)

INSPECTION FOUND SKIN DENTED ALONG BOTTOM OF MAIN CABIN DOOR. THE DENTED SKIN WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 37.

Part: HINGE PLATES — CORRODED (LT HOR STAB)

INSPECTION FOUND INBOARD AND OUTBOARD HINGE PLATES FOR LT HORIZONTAL STABILIZER CORRODED. THE HINGE PLATES WERE REMOVED AND NEW PLATES WERE INSTALLED IAW SRM 51-30-5.

Part: SKIN — DENTED (BS 313)

A TEMPORARY REPAIR DOUBLER HAD BEEN INSTALLED DUE TO DENTED FUSELAGE SKIN AT STA 313 LEFT. A PERMANENT CLASS I REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B.

Part: ANGLE — CORRODED (BS 160-200)

INSPECTION FOUND FLOOR Z-ANGLE CORRODED INBOARD OF FLOOR PANEL-K AT STA 160 TO 200. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CRACKED (BS 905)

INSPECTION FOUND FLOOR SUPPORT CRACKED AT STA 905 LEFT. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: CUSP MEMBRANE — CORRODED (BS 1134/1135)

INSPECTION FOUND CORROSION ON CUSP MEMBRANE AT STA 1134 AND 1135, LT SIDE IN AFT BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 53-01.

Part: INTERCOSTAL — CRACKED (BS 1287)

INSPECTION FOUND CRACKS AT NUTPLATE HOLES OF INTERCOSTAL IN AFT BAGGAGE BIN, BOTH FORWARD AND AFT OF STA 1287. THE AREA WAS REPAIRED IAW SRM 51-30-2.

Part: SKIN — TORN (LT ELEVATOR)

INSPECTION FOUND A 2 INCH TEAR IN SKIN AT LT ELEVATOR LEADING EDGE INBOARD NR 1 HINGE. THE TORN SECTION OF SKIN WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30 AND 55-20-0, ITEM 1.

Part: CUSP MEMBRANE — CORRODED (BS 1174)

INSPECTION FOUND CUSP MEMBRANE CORRODED FORWARD AND AFT OF STA 1174 IN AFT BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 53-01.

Part: SKIN — DAMAGED (FUSELAGE)

A TEMPORARY REPAIR DOUBLER HAD BEEN INSTALLED DUE TO SKIN DAMAGE AFT OF LT FORWARD WATER SERVICE PANEL. A PERMANENT CLASS I REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B.

Part: ANGLE — CORRODED (BS 198-200)

INSPECTION FOUND FLOOR SUPPORT ANGLE AT AFT LOWER CORNER OF FORWARD ENTRY DOOR STA 198 TO 200 CORRODED. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 53-30-5.

Part: ANGLE — CORRODED (BS 200)

INSPECTION FOUND FLOOR PANEL SUPPORT Z-ANGLE CORRODED AT FLOOR PANEL-H, STA 200. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.