N35832

Part: LONGERON — CRACKED (STA 1415) · airframe 48,566 hrs · 23,371 cycles

INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT AFT SIDE OF BELTFRAME, STA 1415. A LONGERON SPLICE WAS INSTALLED IAW SRM 53-02.

Part: INTERCOSTAL — CORRODED (STA 1174) · airframe 45,556 hrs · 21,793 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER SECTION OF AFT BAGGAGE BIN DOOR CUTOUT, STA 1174. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-01, FIGURE 1 AND 51-30-2.

Part: SKIN — CRACKED (WS XOS 286) · airframe 45,556 hrs · 21,793 cycles

INSPECTION FOUND A 1.5" CRACK IN R/H WING UPPER L/E SKIN BETWEEN #2 & #3 SLAT PANELS AT WS XOS 286. A SKIN DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01731.

Part: CHANNEL — CORRODED (LT WING PANEL) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND DOME NUT GANG CHANNEL AND OUTER SHIM OF LT WING LOWER FUEL TANK OPENING (PANEL 1371C) CORRODED. THE RUB STRIP AND GANG CHANNEL WERE REMOVED AND REPLACED IAW SRM 51-22-2 AND ECRA 5100-02063.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND THE LT NR 5 SLAT LEADING EDGE DENTED. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, SRM 57-06, FIGURE 1, AND 51-30-2.

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A .5 INCH CRACK AT LAST RIVET HOLE IN THE FIXED SECTION ON O/B SIDE OF RT HORIZONTAL STABILIZER ELEVATOR ACCESS TO ELEVATOR GEAR TAB MECHANISM 3616A. THE PUSH ROD AND CONDUIT WERE REMOVED TO GAIN ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2 AND 51-30-8, THE PUSH ROD AND CONDUIT WERE REINSTALLED IAW SRM 51-30-2.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND R-1 ENTRYWAY FLOOR PANEL CORRODED AT FS 148 - 200. THE CORRODED FLOOR PANEL AREA WAS REPAIRED IAW SRM 53-24-0, FIGURE 3, 51-10-3, AND ECRA 5100-01844.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LT WING FUEL ACCESS PANELS 1303C, 1355C, AND 1363C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING FUEL ACCESS PANELS 1410C, 1409C, AND 1436C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.

Part: SLAT TRACK — GOUGED (NR 5 SLAT) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING NR 5 SLAT TRACK GOUGED. THE SLAT TRACK WAS REMOVED AND REPLACED IAW MM 27-80-01.

Part: PANEL — GOUGED (LT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LT WING LOWER SURFACE FUEL ACCESS PANEL NR 2 GOUGED. THE PANEL WAS REPAIRED IAW SRM 5730-01688 AND SRM 51-30-2.

Part: ACCESS PANEL — GOUGED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FUEL ACCESS PANELS NR 1, 6 AND 7 GOUGED AND CORRODED ON RT WING LOWER SURFACE. THE PANELS WERE REPAIRED IAW ECRA 5730-01688 AND SRM 51-30-2.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AND DENTED AT STA 1211 - 1231. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 53-24-0, FIGURE 1A, 51-10-2, AND 51-60-0, PAGE 5.

Part: FITTING — CRACKED (NR 5 SLAT) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND TWO 1 INCH CRACKS AT FASTENER HOLE OF RT WING NR 5 SLAT END FITTING. THE SEAL AND RETAINER ON END FITTING WERE REMOVED IAW SRM 51-30-3. THE CRACKS WERE WELDED IAW DPS 10.225. THE SEAL AND RETAINER WERE REINSTALLED IAW SRM 51-30-2.

Part: FITTING — CORRODED (SPOILER) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LEFT O/B FLIGHT SPOILER CENTER FITTING CORRODED. THE SPOILER WAS REMOVED IAW MM 27-62-01. THE HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27-61-10 AND THE SPOILER WAS REINSTALLED IAW MM 27-61-01.

Part: FITTING — CORRODED (NR 4 GALLEY) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND NR 4 GALLEY ATTACH MOUNT FITTINGS (2) CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW ECRA 2530-01257.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AT FS 1211 - 1231. THE FLOOR PANEL WAS REPLACED IAW SRM 53-24-0, FIGURE 11A, 51-10-2, AND 51-60-0, PAGE 5.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 6 INCH CRACK IN MID CARGO BAY FIBERGLASS FLOOR SUPPORT ANGLE AT STA 617, LONGERON 26R TO 27R. THE FLOOR SUPPORT ANGLE WAS REMOVED, REPAIRED WITH FIBERGLASS OVERLAY, AND REINSTALLED IAW SRM 51-70-1, FIGURE 4 AND 51-30-5.

Part: WEB — CRACKED (AIRSTAIR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 4.5 INCH CRACK IN AFT AIRSTAIR LT SIDE WEB. THE CRACKED AREA WAS CUT OUT IAW SRM 52-01, FIGURE 2. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 2, 51-30-2, AND 51-10-3.

Part: FAIRING — GOUGED (RT WING TE FLAP) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING NR 3 AFT LOWER FLAP HINGE FAIRING GOUGED. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 57-50-14, FIGURE 4.

Part: FAIRING — CRACKED (RT WING TE FLAP) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 4 INCH CRACK IN RT WING O/B FLAP HINGE FAIRING LOWER HALF. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-50-14 AND 51-30-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FITTING CORRODED AT STA 160 - 196, LBL 55. THE FLOOR SUPPORT FITTING WAS REMOVED AND A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-15-1, AND 51-30-5.

Part: ANGLE — CRACKED (NR 2 T/R FAIRING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FOUR INCH CRACKS IN TWO ANGLES ON I/B FAIRING OF NR 2 ENGINE UPPER T/R BUCKET. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.

Part: ATTACH ANGLE — CRACKED (CARGO BAY) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 3 INCH CRACK IN MID CARGO LT SIDEWALL FORWARD ATTACH ANGLE AT STA 524. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 53-24-0, FIGURE 9.

Part: WEB — CRACKED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 6 INCH CRACK IN SUBFLOOR WEB AT STA 1170, LBL 56. THE CRACKED AREA OF WEB WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-3, FIGURE 12, AND 51-30-2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO TRACK CORRODED AT NUT CLIP HOLES. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-24-0, FIGURE 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FRAME OF THE FORWARD LAV TOILET SERVICING UNIT AT STA 240, LT SIDE. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-34-0, FIGURE 2, AND 51-30-1.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RIGHT I/B FLAP MOVEABLE VANE GOUGED. THE GOUGED AREA OF SKIN WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-70-2, FIGURE 72 AND PARAGRAPH 22C.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LEFT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE LEFT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.

Part: ANGLE — CRACKED (NR 1 T/R FAIRING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CRACKS IN FIRST AND THIRD ANGLES ON INBOARD T/R FAIRING ON UPPER BUCKET OF NR 1 ENGINE. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.

Part: PANEL — GOUGED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING FUEL PANEL 1472C GOUGED. THE FUEL PANEL WAS REMOVED AND REPLACED IAW ECRA 5730-01688.

Part: PANEL — CORRODED (LT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LT WING FUEL PANELS 1311C AND 1307C CORRODED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.

Part: GALLEY TRACK — CORRODED (GALLEY) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD GALLEY I/B LOWER MOUNT FITTING CORRODED. A REPLACEMENT MOUNT FITTING WAS INSTALLED IAW ECRA 2530-01257.

Part: PANEL — CORRODED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING FUEL PANEL 1414C CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RIGHT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE RIGHT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND THREE DENTS IN NR 1 SLAT T/E BETWEEN XOS 166 AND XOS 147. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5750-03426.

Part: SKIN — BULGED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN BULGED AT STA 389, LONGERON 16L-17L. THE EXISTING REPAIR WAS REMOVED IAW SRM 51-30-2. AN EXTERNAL AND INTERNAL DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38, 51-30-2, 51-30-5, AND ECRA 5330-02944.

Part: SHIM — CORRODED (CARGO DOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND SHIMS UNDER STRAPS OF DOOR STOP NUMBER 11 & 12 OF AFT CARGO DOOR CORRODED. THE SHIMS WERE REMOVED AND REPLACEMENT SHIMS WERE INSTALLED. THE STRAPS WERE REINSTALLED. WORK WAS PERFORMED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR CORRODED AT STA 170 - 184, LBL 55. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2.

Part: VANE — DENTED (TE FLAP) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LT WING O/B FLAP O/B NR 2 FIXED VANE DENTED ON LEADING EDGE. THE DENTED AREA WAS REMOVED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 57-50-14 AND 51-70-2.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND THE UPPER FLANGE OF THE RIGHT CARGO TIE DOWN TRACK IN THE MID CARGO PIT CORRODED AROUND FASTENER HOLES ON UPPER AND LOWER SURFACES AT STA 579 - 598. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-30-1, 53-05, FIGURE 4C, 51-30-1, AND 51-10-4.

Part: PANEL — GOUGED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING LOWER FUEL PANEL NR 1244C GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-3, 51-30-2, AND DRAWING 9937483.

Part: FITTING — BENT (CARGO DOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND MID CARGO DOOR FRAME LOWER BEAM TEE FITTING BENT. THE TEE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-1, 51-30-5, AND 51-10-3.

Part: PANEL — GOUGED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT WING LOWER PANEL NR 1222C GOUGED. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 57-30-3, FIGURE 3 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO DOOR JAMB FLOOR SUPPORT CORRODED AT STA 1155 - 1211, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO DOOR JAMB CENTER LOWER SECTION CORRODED. THE DOOR JAMB CENTER LOWER SECTION WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5, 53-05, FIGURE 63, 51-10-3, AND 51-30-4.

Part: WEB — CORRODED (CARGO DOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD CARGO PIT FORWARD DOOR FRAME TORQUE BOX WEB CORRODED. A DOUBLER AND CONICAL WASHERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-1, 51-30-8, AND 51-30-2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND SUPPORT SPLICE UNDER CABIN FLOOR HAD 7 CRACKS AT STA 826 - 886. THE CRACKS WERE 4 - 6 INCHES LONG. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED IN CHANNEL AT FS 568 - 576, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F AND 51-30-5.

Part: SKIN — BULGED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND LOWER FORWARD FUSELAGE SKIN BULGED AT STA 389, LONGERON 16L AND 17L. THE EXISTING REPAIR WAS REMOVED FROM SKIN IAW SRM 51-30-2. AN EXTERNAL AND INTERNAL DOUBLER AND FILLER REPAIR WAS INSTALLED IAW ECRA 5330-02944, SRM 53-04, FIGURE 38, 51-30-2, AND 51-30-5.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT ELEVATOR ANTI-FLOAT TAB DELAMINATED AT O/B UPPER SIDE. THE DELAMINATED AREA WAS CUT OUT IAW SRM 51-70-2. REPAIR CORE AND WEDGE DOUBLER WERE BONDED IAW SRM 51-70-2. DEFLASHED BOND AND APPLIED FILLET SEAL IAW SRM 51-70-2. BALANCED TAB IAW MD80 SRM 55-20-2.

Part: BRACKET — BROKEN (CARGO DOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO DOOR OPEN UPLATCHING LOCK MECHANISM MOUNTED IN CEILING HAD A BROKEN AND BENT L BRACKET. BOTH THE FORE AND AFT BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-5 AND 51-10-2.

Part: DOUBLER — CORRODED (RADAR ANTENNA) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FWD MID RADAR/ALT ANTENNA SKIN CUTOUT MOUNT CORRODED ON FLANGE SURFACE. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND MID CARGO DOOR FRAME LOWER BEAM CORRODED. THE MID CARGO DOOR LOWER BEAM WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.

Part: PAN — CORRODED (DOOR FRAME) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD CARGO DOOR LOWER DOOR JAMB PAN CORRODED AROUND FASTENER HOLES. THE LOWER DOOR JAMB PAN WAS REMOVED AND REPLACED IAW SRM 53-05.

Part: FITTING — CORRODED (GIRT BAR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD SERVICE DOOR GIRT BAR MOUNT FITTINGS CORRODED. THE MOUNT FITTINGS WERE REMOVED AND NEW MOUNT FITTINGS WERE INSTALLED IAW SRM 51-10-4 AND 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK SECTIONS CORRODED AT STA 667 - 698, 726 - 750, AND 788 - 843, RBL 56. THE SEAT TRACK SECTIONS WERE REMOVED AND NEW SECTIONS OF TRACK WERE INSTALLED IAW SRM 53-05, FIGURE 4F, 51-30-5, AND 51-30-1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 237, LONGERON 17L-18L AND AT STA 218, LONGERON 19L. THE DAMAGED SECTIONS OF SKIN WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-04, FIGURE 25 AND ECRA 5330-02445.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED IN FORWARD GALLEY AREA AT FS 216, RBL 6. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3, 51-30-5, AND 53-14-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RIGHT AFT FUSELAGE EXTERNAL SKIN DENTED AT STA 1309, LONGERON 19R. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 148 - 196, LBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED USING TWO SHIMS IAW SRM 51-30-1 AND 53-14-1, FIGURE 11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED IN CHANNEL AT FS 1114 - 1117, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-1, 51-30-2, AND 53-05, FIGURE 4F.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FITTING CORRODED AT STA 196 - 242, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, 53-14-1, AND 51-30-1.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RIGHT O/B FLOOR WEB CORRODED AT STA 636 - 712. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED IN FORWARD GALLEY AREA AT STA 160, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, FIGURE 11, AND 51-30-5, PAGE 1.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR WEB CORRODED AT AFT LT CORNER, STA 196 LBL 2 - LBL 7. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-14-1, 53-01, FIGURE 2, 51-30-2, 51-10-3, AND 51-20-0.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 1060 - 1174, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4 AND 51-30-1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK SECTIONS CORRODED AT STA 651 - 688 AND STA 696 - 767, LBL 56. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND NEW SECTIONS OF SEAT TRACK WERE INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 4F.

Part: FITTING — CORRODED (NR 3 FLAP) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT NR 3 FLAP HINGE FITTING UPPER AFT FAYING SURFACE CORRODED. THE CORROSION WAS REMOVED AND FLAP PEENED UPPER AFT SURFACE IAW OHM 27-50-5 AND 20-10-03. A BUSHING WAS INSTALLED IN UPPER MOUNT HOLES OF NR 3 FLAP HINGE IAW OHM 27-50-5 AND 20-10-7. A REPAIR SHIM WAS INSTALLED IAW OHM 27-50-5.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED IN TRACK CHANNEL AT FS 1166 - 1169, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 4F.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A CRACK IN RADIUS OF FORWARD MOUNTING FLANGE AT UPPER RT HORIZONTAL STABILIZER FAIRING. REMOVED ANGLE FROM FAIRING AND INSTALLED A NEW ANGLE IAW SRM 51-30-2, 51-10-2, 55-12-0, FIGURE 7A, 51-10-3, 51-30-0, AND 51-20-0.

Part: BRACKET — CORRODED (SERVICE DOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT LT SERVICE DOOR AFT SCUFF PLATE SUPPORT BRACKET CORRODED. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2, 51-10-3, AND 51-20-0.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN FLOOR SUPPORT CRACKED AT FASTENER HOLE, STA 845, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 53-14-3, FIGURE 10.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 42,567 hrs · 20,118 cycles

INSPECTION FOUND THAT CABIN FLOOR PANEL AT FS 674 - 693, RBL 24 - 44 HAD CRACKED INSERTS AND LOOSE FASTENERS. THE FLOOR PANEL WAS REMOVED, BUILT UP, AND INSTALLED IAW ECRA 5320-01265 AND MM 53-20-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED IN TRACK CHANNEL AT FS 439 - 443, LBL 56. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED WITH REPAIR STRAPS IAW SRM 51-30-7, 53-05, FIGURE 4F, 51-30-5, AND 51-30-1.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND AFT CARGO DOOR JAMB FLOOR SUPPORT BRACKET CORRODED AT STA 1155, RBL 13. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-05 AND 53-14-3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A CREASE IN FUSELAGE SKIN SURFACE AT STA 315 - 351, LONGERON 19R AND AT STA 446 - 465, LONGERON 19R & 20R. THE DAMAGED AREAS WERE CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-04, FIGURE 12B AND ECRA 5331-01077.

Part: BRACKET — CRACKED (FAIRING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 2 INCH CRACK IN RIGHT WING I/B MOST LEADING EDGE FAIRING UPPER C BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-20-0.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 148 - 196, RBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1, FIGURE 11, 51-10-4, AND 51-30-1.

Part: PANEL — GOUGED (RT WING) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND RT LOWER WING PANEL 1211C GOUGED AND SCRATCHED. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-4.

Part: STRUCTURE — CORRODED (CABIN FLOOR) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND SUB FLOOR CORRODED AT STA 196, LBL 8. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-14-1, FIGURE 11 AND 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED AT G-3 GALLEY FASTENER HOLE AND SURROUNDING TRACK AREA, FS 1101 - 1104, LBL 44. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 44 & 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 1222 - 1338, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-01, 51-10-3, AND 53-05, FIGURE 4F & 4H.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND ATTACH ANGLE FROM CUSP WEB TO FUSELAGE SKIN CORRODED AT STA 510, LONGERON 18L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5 AND 53-14-2, FIGURE 4.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CRACKS ON SEAT TRACK EDGES AT STA 1166 - 1260, LBL 44. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 53-05, FIGURE 4F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT ANGLE CORRODED AT STA 160 - 196, RBL 44. THE SUPPORT ANGLE WAS REMOVED AND A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 53-11-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 196, LBL 5 TO RBL 5. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2, 53-14, AND ECRA 5100-01844.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SIDEWALL LOWER SUPPORT ANGLE CORRODED AT STA 1117 - 1136. THE SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 53-01, FIGURE 1, 51-10-2, AND ECRA 5100-01844.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 1063 - 1169, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF SEAT TRACK WAS INSTALLED USING TWO SPLICES AND SPLICE PLATES IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 4F.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND A 3 INCH CRACK IN L-ANGLE BENEATH THE CARGO TIE DOWN TRACK IN THE FORWARD CARGO PIT AT STA 237, RBL 17. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND CABIN SEAT TRACK CORRODED AND GOUGED AT FS 1203 - 1206, LBL 44. THE SEAT TRACK WAS REPLACED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FRAME ANGLE CORRODED AT STA 176, RBL 9 - 43. THE FRAME ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 53-14-1, AND 51-10-3.

Part: FITTING — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY DOOR SUPPORT FITTING CORRODED FROM STA 160 - 196, LBL 44. THE SUPPORT FITTING WAS REMOVED AND A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 53-14-1, 53-04, 51-30-2, AND 51-30-10.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY AREA SUBFLOOR WEB CORRODED AT FS 160 - 200, LBL 48 - 59. THE CORRODED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-1, 51-10-3, AND 51-30-2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FRAME ANGLE CORRODED AT STA 176, RBL 9. THE FRAME ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 53-14-1, AND 51-10-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT STA 196, LBL 9 - 14. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR PANEL CORRODED ON SURFACE AT STA 196, LBL 14. THE CORRODED AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 2, 53-14-1, FIGURE 1 & 2, AND 51-30-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,467 hrs · 20,118 cycles

INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT ANGLE CORRODED AT STA 186, LBL 53. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-02 AND 53-14-1.

Part: DE-ICE DUCT — BLOWN (NR 2 ENGINE)

THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMBOUT. THE NR 2 ENGINE WAS RETARDED TO IDLE AND THE FIRE WARNING CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE NOSE COWL ANTI-ICE DUCT BLOWN WITH DAMAGE TO THE UPPER COWL. THE ANTI-ICE DUCT AND UPPER COWL WERE REPLACED. IN ADDITION, THE ANTI-ICE VALVE WAS REPLACED DUE TO METAL PARTICLES FOUND IN THE VALVE. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: CABLES — OUT OF ADJMT (TAIL CONE)

THE TAIL CONE RELEASE PULLED HIGH FROM EXTERIOR HANDLE. THE LATCH LEVERS, LEVER CABLES, AND EXTERNAL RELEASE CABLE SYSTEM WERE ADJUSTED IAW MM 53-53-00, PARAGRAPH A.

Part: DOUBLER — CORRODED (BAGGAGE COMPT)

INSPECTION FOUND AFT BAGGAGE BIN Z-ANGLE REPAIR DOUBLER CORRODED. THE Z-ANGLE DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63.

Part: TIE DOWN — CORRODED (BS 1007-1155)

INSPECTION FOUND AFT CARGO RT SIDE FLOOR TIE DOWN STRIP CORRODED WITH SHEARED SCREWS AND CRACKED FLANGE FROM STA 1007 TO 1155. THE CORRODED AREA WAS CUT OUT, REPAIR SPLICES WERE INSTALLED IAW ECRA 5320-01521.

Part: LONGERON — CORRODED (BS 239)

INSPECTION FOUND LONGERON 30 CORRODED AT STA 239 IN FORWARD BAGGAGE BIN. THE CORRODED AREA WAS REMOVED AND A LONGERON REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18.

Part: JAMB — CORRODED (BAGG COMPT)

INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR JAMB PAN CORRODED AT STA 370 TO 427. THE DOOR JAMB PAN WAS REPLACED IAW SRM 53-05-44.

Part: SKIN — PUNCTURED (BS 253)

INSPECTION FOUND A 2 DIAMETER HOLE IN FUSELAGE SKIN SIXTEEN INCHES ABOVE AND TWO INCHES AFT OF FORWARD LEFT LAV SERVICE PANEL (STA 253, LONGERON 18-19L). A DOUBLER WAS INSTALLED IAW SRM 53-04, CLASS II, PAGE 33, FIGURE 12B, SHEET 1 AND A DIP WAS INITIATED FOR REPETITIVE INSPECTION.

Part: PLATES — CORRODED (LT/RT HORIZ STAB)

INSPECTION FOUND LT HORIZONTAL STABILIZER PIVOT OUTBOARD PLATES AND RT HORIZONTAL STABILIZER PIVOT OUTBOARD PLATES CORRODED. THE PLATES WERE REPLACED IAW SRM 51-30-00.

Part: GEAR HANDLE — MALFUNCTIONED (LANDING GEAR)

THE LANDING GEAR HANDLE WOULD NOT MOVE DOWN UPON INITIAL ATTEMPT TO LOWER, WHILE ON APPROACH. ALTERNATE GEAR EXTENSION WAS USED, AND THEN CREW WAS ABLE TO MOVE GEAR HANDLE DOWN AFTER EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS JACKED IAW MM 7-11-00 AND THE GEAR HANDLE WAS CYCLED EIGHT TIMES AND ALL GEAR FUNCTIONS WERE NORMAL WITH SMOOTH GEAR HANDLE OPERATION.

Part: SKIN — PUNCTURED (FUSELAGE)

A 2 INCH HOLE WAS FOUND IN FUSELAGE SIXTEEN INCHES ABOVE AND TWO INCHES AFT OF FORWARD LEFT LAV SERVICE PANEL. A DOUBLER WAS INSTALLED IAW SRM 53-04, CLASS II, PAGE 33, FIGURE 12B, SHEET 1. A DIP WAS ISSUED FOR REPETITIVE INSPECTIONS AND TO INSTALL A CLASS I REPAIR WITHIN 40,000 LANDINGS.

Part: PROX SWITCH — INOPERATIVE (NLG)

THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED, BUT WENT OFF AND ON INTERMITTENTLY DURING CRUISE. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SWITCH CONTROL AND TIGHTENED THE NOSE GEAR LOCK SENSOR TARGET. THE NOSE GEAR WAS SWUNG SEVERAL TIMES WITH NORMAL OPERATION AND INDICATIONS.

Part: DUCT — BLOWN (NR 1 ENGINE)

THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB-OUT OF MIA. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE ANTI-ICE DUCT FROM NOSE COWL TO SADDLE DUCT BLOWN. THE DUCT WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: CABLES — OUT OF ADJUST (TAILCONE)

THE TAILCONE INTERIOR AND EXTERIOR HANDLES PULLED AT 50 POUNDS TO OPEN LATCHES. THE TAILCONE CABLE PULL TENSION WAS ADJUSTED IAW MM 53-53-00.

Part: BULKHEAD PANELS — CORRODED (BS 786.5)

INSPECTION FOUND BULKHEAD PANELS IN MID BIN CORRODED AT STA 786.5. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01.

Part: FRAME — CRACKED (BS 1418)

INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 1418, LONGERON 2R AND A 1 INCH CRACK WAS FOUND AT LONGERON 2L. REPAIRS WERE INSTALLED IAW SRM 53-03-32.

Part: SUPPORT — CORRODED (BS 160-200)

INSPECTION FOUND Z-ANGLE FLOOR SUPPORT CORRODED TEN INCHES FROM FORWARD ENTRY DOOR AT STA 160 TO 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01-01.

Part: THRESHOLD — PUNCTURED (FWD SERV DOOR)

INSPECTION FOUND HOLES PUNCTURED INTO FORWARD SERVICE DOOR THRESHOLD. A NEW DOOR PAN WAS INSTALLED IAW SRM 53-05-01.

Part: JAMB WEB — CRACKED (PAX DOOR)

INSPECTION FOUND A 2 INCH CRACK IN FORWARD ENTRY DOOR JAMB WEB AT STA 207, LONGERON 15L. A DOUBLER WAS INSTALLED IAW SRM 53-01-01.

Part: SUPPORT — CRACKED (BS 886)

INSPECTION FOUND A 2.5 INCH CRACK IN KEEL BEAM T-ANGLE SUPPORT FOR ADF PANELS AT STA 886. THE T-ANGLE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0.