N929FR

Part: LEVER — STUCK (ESCAPE SLIDE) · airframe 31,475 hrs · 15,399 cycles

RIGHT EMERGENCY EXIT SLIDE RELEASE LEVER ON DOOR WILL NOT RETURN TO NORMAL POSITION. INSTALLED RELEASE CABLE TEST TOOL AND PERFORMED TEST NUMEROUS TIMES. CABLE RELEASE LEVER NOW RETURNS TO NORMAL POSITION IAW AMM 25-62-43-400-003-A, PG 10 & 11 STEPS(B) THUR C.(5). OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 303 hrs · 14,831 cycles

EMERGENCY LIGHT EPSU BATTERY 10WL FAILED TEST, HEAVY SERVICE. R & R BATTERY FOR 10WL EPSU. OPS CHECK OK, REF AMM 33-51 -38-000-002A AND 33-51-38-400-002A.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0768. MULTIPLE EMERGENCY LIGHTS FOR SEAT ROWS INOPERATIVE. R & R EMERGENCY LIGHT HARNESS AT SEAT ROW 18 ABC IAW ESPM 20-33-11. R & R DEFECTIVE EPSU AT POSITION 11WL AND POSITION 13WL IAW AMM 33-51-38 PAGE BLOCK 401.

Part: TRANSITION PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0685 AFT CARGO COMPARTMENT TRANSITION PANEL 161CF HAS NUMEROUS DENTS AND BULGES THROUGHOUT PANEL. R & R PANEL 161CF IAW MCG IRM 9701 REV G.

Part: TRANSITION PANEL — PUNCTURED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF C-CHECK NON ROUTINE N0686. AFT CARGO COMPARTMENT TRANSITION PANEL 161BF HAS (2) PUNCTURES. OFF ACFT PART. FABRICATED REPLACEMENT TRANSITION PANEL 161BF IAW IRM 9701 REV G.

Part: TRANSITION PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF C-CHECK NON ROUTINE N0682. AFT CARGO COMPARTMENT TRANSITION PANEL 151BE HAS (2) PUNCTURES AND NUMEROUS DENTS THROUGHOUT ENTIRE PANEL. OFF ACFT PART. FABRICATED REPLACEMENT PANEL 151BE IAW MCG IRM 9701 REV G.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF HEAVY MX NON ROUTINE N0689. AFT CARGO PIT PANEL 151UG HAS NUMEROUS DENTS. OFF ACFT PART. FABRICATED PANEL 151UG IAW IRM 9701 REV G.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF HEAVY MX NON-ROUTINE N0679. AFT CARGO PANEL 151DE HAS NUMEROUS DENTS THROUGHOUT PANEL. R & R PANEL.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF HEAVY MX NON-ROUTINE N0687. AFT CARGO PIT PANEL 152TG HAS SEVERAL AREAS OF EDGE DELAMINATION AND SEVERAL SMALL DENTS. OFF ACFT PART. FABRICATED PANEL 152TG IAW IRM 9701 REV G.

Part: TRANSITION PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

HEAVY MX NON-ROUTINE N0688. AFT CARGO PIT TRANSITION PANEL 152UG HAS NUMEROUS DENTS THROUGHOUT ENTIRE PANEL . OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE HEAVY MX NON-ROUTINE N00680. AFT CARGO PIT PANEL 162BF HAS AREAS OF DELAMINATION AROUND EDGE OF PANEL. FABRICATED PANEL IAW IRM 9701 REV G.

Part: TRANSITION PANEL — DELAMINATED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF HEAVY MX NON-ROUTINE N0678. AFT CARGO TRANSITION PANEL 151FE HAS DELAMINATION AROUND EDGE. OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF C-CHECK NON ROUTINE N0587. CABIN FLOOR PANEL 222CF IS DELAMINATED. OFF ACFT PART. FABRICATED REPLACEMENT CABIN FLOOR PANEL 222CF IAW IRM 9701 REV G.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF C-CHECK NON ROUTINE N0478. CORROSION IN (2) AREAS OF FLOORBEAM -Y765 AT FRAME 68. R & R FLOORBEAM IAW A319 SRM 51-42-11 PAGE 11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 21,469 hrs · 10,442 cycles

REFERENCE HEAVY MX NON-ROUTINE N0534. CORROSION DISCOVERED ON NUTPLATE HOLES ON FLOORBEAM Y1292. R & R FLOORBEAM.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0481. CORROSION ON PREVIOUS REPAIR AT FLOORBEAM, Y1292, FRAME 66. R & R FLOORBEAM IAW SRM 51-72-11, SHEETS 1 THROUGH 6.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

CORROSION ON FLOORBEAM JUST INBD OF Y765 AT FRAME 68. R & R FLOORBEAM IAW A319 SRM 51-42-11, PAGE 1, STEP A, 51-44-11, PAGE 1 AND 51-21-11 PAGE 1 TABLE 1.

Part: SUPPORT FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0551. RIGHT HAND CABIN FLOOR SHEAR PLATE EXTRUSION IS CORRODED. REPLACED EXTRUSION REF A319 SRM 41-42-11, SRM 51-21-11 AND 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0479. CORROSION ON NUT PLATE HOLES AT SPLICE ON FLOORBEAM AT Y-1292 FRAME 69. UPPER AND LOWER SIDES OF BEAM. R & R FLOORBEAM IAW SRM 51-72-11.

Part: SILL — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0480. CORROSION ON L-2 DOOR SILL PLATE AT SPLICE FRAME 66. REPAIRED L-2 DOOR SILL PLATE IAW SRM 53-41-11 FIGURE 201 REPAIR PRINCIPLE 6.

Part: SILL — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

C-CHECK NON ROUTINE N0482. CORROSION ON R-2 DOORSILL PLATE AT FRAME 66 SPLICE. R & R DOOR SILL AND 3 EACH SCUFF PLATES IAW SRM 51-72-11 AND AMM 53-45-15-400-001.

Part: TRANSITION PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE HEAVY MX NON ROUTINE N0319. FWD CARGO PIT TRANSITION PANEL HAS NUMEROUS DENTS THROUGHOUT ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT PANEL IAW IRM9701 REV G. R & R PANEL.

Part: BRACKET — CRACKED (ZONE 500) · airframe 21,469 hrs · 10,442 cycles

REF C4/SI CHECK NON-ROUTINE N0215. LT WING L/E TAI DUCT CUT OUT UPPER SURFACE OTBD PANEL ATTACH ANGLE HAS A 1.5 INCH CRACK. R & R BRACKET.

Part: TRANSITION PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF C-CHECK NON ROUTINE N0299. FWD CARGO COMPARTMENT TRANSITION PANEL 131DG HAS NUMEROUS DENTS ACCROSS ENTIRE LENGTH OF PANEL. OFF ACFT PART. FABRICATED TRANSITION PANEL 131DG IAW MCG IRM 9701 REV G.

Part: TRANSITION PANEL — DELAMINATED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF AERO FRAME HEAVY MX NON-ROUTINE N0336. TRANSITION PANEL 131BF HAS AREAS OF PUNCTURES DENTS AND EDGE DELAMINATION. OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE C-CHECK NON ROUTINE N0318. SHEAR PLATE AT FRAME 69 TO FRAME 70 BETWEEN STRINGER 23 RT AND 24 RT HAS CORROSION IN 15 AREAS. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 AND 7 AND EO A0-53EO-31434.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REF C-CHECK NON ROUTINE N0317. SHEAR PLATE AT FRAME 69 TO 70 BETWEEN STRINGER 23 LT AND STRINGER 24 LT HAS 6 SQUARE INCHES OF CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 AND 7 AND EO NR A0-53EO-31434.

Part: FLOOR PANEL — DENTED (ZONE 100) · airframe 21,469 hrs · 10,442 cycles

REFERENCE HEAVY MX NON-ROUTINE N0684. AFT CARGO PIT FLOOR PANEL 162CF HAS NUMEROUS DENTS. R & R PANEL.

Part: SERVO CONTROL — INOPERATIVE (SPOILERS) · airframe 18,476 hrs · 8,987 cycles

FLIGHT CREW MADE AN UNSCHEDULED LANDING IN RSW DUE TO "SPOILER FAULT 4". THE AIRCRAFT RETURNED TO DEN ON A SPECIAL FLIGHT PERMIT. MAINTENANCE REMOVED AND REPLACED THE NR 4 RIGHT SPOILER SERVO AND PERFORMED RIG, OPERATIONAL AND LEAK CHECK PER AMM 27-64-51 PB 401.

Part: COMPUTER — SMOKE (ZONE 200) · airframe 17,444 hrs · 8,460 cycles

DURING THE BOARDING PROCESS, BOTH PILOTS DETECTED ELECTRONIC OVERHEAT ODOR. MAINTENANCE PERFORMED TROUBLESHOOTING USING REFERENCE TSM 24-00-00-810-823, ELECTRICAL BURNING SMELL OR FUMES FOUND IN THE CABIN, COCKPIT, CARGO, OR AVIONICS COMPARTMENT AND IDENTIFIED THE SMOKE ODOR COMING FROM THE NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER. MAINTENANCE REMOVED AND REPLACED THE FLT MANAGEMENT GUIDANCE COMPUTER AND PERFORMED OPERATIONAL TEST, REFERENCE AMM 22-83-34 PB 401.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 15,674 hrs · 7,553 cycles

REF: NON ROUTINE C050752. DURING C3 C-CHECK, INSPECTION FOUND (1) MOUNT BUSHING CORRODED ON FLOOR PANEL 261DE. MAINTENANCE REMOVED AND REPLACED MOUNT BUSHING ON C-CHECK CARD NR C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,674 hrs · 7,553 cycles

REF NON ROUTINE C050600. DURING C3 C-CHECK, INSPECTION NOTED FWD NUT PLATE HOLE ON FRAME Y-1292 AT FRAME 66, HAD CORROSION. MAINT REMOVED CORROSION FROM HOLE, FABRICATED REPAIR BUSHING AND INSTALLED IAW WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9-53R-30598. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,674 hrs · 7,553 cycles

DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,674 hrs · 7,553 cycles

REF: NON ROUTINE C050602. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68, HAD CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K)

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050515. DURING C3 C-CHECK INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12 PB 401. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050370. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51UG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050368. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51TG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050372. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51FF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,674 hrs · 7,553 cycles

REF NON ROUTINE C050605. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68, HAD CORROSION. MAINT REMOVED CORROSION FROM HOLES, FABRICATED REPAIR PROFILE AND FILLER, AND INSTALLED IAW THE REQUIREMENTS OF EA NR A9-53R-30604 AND A 319 SRM 53-00-14, FIGURE 214. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050458. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131CF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050366. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I52UG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050457. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131EG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050375. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161CF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050374. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161BF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,674 hrs · 7,553 cycles

REFERENCE NON ROUTINE C050516. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12 PB 401. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: HINGE — DAMAGED (RT WING SPOILER) · airframe 15,674 hrs · 7,553 cycles

REF: NOT ROUTINE C050745. DURING C3 C-CHECK, INSPECTION FOUND DAMAGE ON THE RT NR (2) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLATE AND PROTECTED AREA IAW ENGINEERING AUTHORIZATION NR A9-57R-30610. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K)

Part: HINGE — DAMAGED (RT WING SPOILER) · airframe 15,674 hrs · 7,553 cycles

REF NON ROUTINE C050746. DURING C3 C-CHECK, INSP FOUND DAMAGE ON THE RT NR (4) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLATE AND PROTECTED AREA IAW EA NR A9-57R-30609. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K)

Part: UNKNOWN — ODOR (CABIN) · airframe 15,062 hrs · 7,233 cycles

DURING FLIGHT, FLIGHT CREW NOTED AN ODOR OF GAS IN AFT GALLEY. MAINT INSPECTED AC FOR UNSATISFACTORY CABIN AIR QUALITY IAW TSM 21-00-00-810-802. NO ODOR OR SOURCE OF ODOR WAS NOTED. FIRE DEPARTMENT AND HAZMAT CREW INSPECTED THE CABIN AND CARGO COMPARTMENT, AND ALL LUGGAGE. NO ODOR OR SOURCE OF ODOR WAS NOTED AND AC CONTINUED SERVICE. (A)

Part: WARNING LIGHT — MALFUNCTIONED (EVAC SLIDE) · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED RT WING OVERWING EXIT SLIDE ARMED LIGHT INOP. UNABLE TO REPRODUCE FAULT PER OPS TEST IAW AMM 52-73-00-710-002.

Part: PIN — BACKED OUT (WIRING HARNESS) · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED EMERGENCY EXIT LIGHT AT ROW 3 INOP. FOUND PIN PUSHED BACK ON WIRE HARNESS 350WL2 AT SEAT ROW 2. REPLACED WIRE HARNESS IAW 33-51-06, PG 003, SHEET 2. PERFORMED OPS CHECK IAW AMM 33-51-00-710-009. CHECKED GOOD.

Part: HOSE — DAMAGED (HYD SYSTEM) · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED LT ENG HYDRAULIC PRESSURE HOSE ASSY HAD A DEEP RUB MARK FROM CLAMP AT CENTER ATTACHMENT BRACKET (APPROX. 7:00 O'CLOCK POSITION). REPLACED HYDRAULIC PRESSURE HOSE/TUBE ASSY IAW MM 29-11-49-400-002.

Part: PIN — CORRODED (RYLON PANEL) · corrosion level 2 · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED RT PYLON PANEL 483BL ONE ALIGNMENT PIN CORRODED. REPLACED PIN IAW AMM 51-42-11.

Part: BEARING — CORRODED (RT PYLON) · corrosion level 2 · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED RT PYLON PANEL 483BL, BOTH SPHERICAL BEARINGS HAD CORROSION. REPLACED BEARINGS IAW AMM 20-21-11-991-003.

Part: GUIDE VANE — CRACKED (ENGINE) · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED NR 1 ENG OUTLET GUIDE VANE AT 8 O'CLOCK POSITION HAD CRACK AT T/E. REPLACED OUTLET GUIDE VANE IAW AMM 72-23-00-400-008 AND 72-23-00-400-026.

Part: BEARING — CORRODED (LT PYLON) · airframe 9,777 hrs · 4,687 cycles

DURING C-2 CHECK, INSPECTION REPORTED LT PYLON PANEL 473BL, ONE SPHERICAL BEARING CORRODED. REPLACED SPHERICAL BEARING PER AMM 51-42-11.

Part: PITOT TUBE — CONTAMINATED (PITOT/STATIC SYS) · airframe 3,590 hrs · 1,655 cycles

ABORTED TAKEOFF AT APPROX 100 KTS, FLIGHT CREW REPORTED DISCREPANCY BETWEEN NR 1 AND NR 2 AIRSPEED INDICATORS. TROUBLESHOT PER TSM 34-13-00-810-998 AND FOUND WATER IN CAPT AND F/O LINES TO PITOT TUBES. REMOVED WATER AND PERFORMED LEAK CHECK PER AMM 34-13-00-790-002. PERFORMED FUNCTIONAL TEST PER AMM 34-11-00-720-001 AND CHECKED OKAY. PERFORMED BRAKE OVERHEAT INSP PER AMM 05-51-16/601. SYSTEMS OPERATED NORMAL.