N908FR

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,153 hrs · 21,021 cycles

EPSU EMER LIGHT BATTERY 10WL, FWD LT, FAILED CAPACITY TEST AT A CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-36-000-002A & 33-51-36-400-002A.

Part: RIB — CRACKED (LT WING) · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. WHILE CLEANING AREA TECHNICIAN FOUND INBD LE RIB, AT SLAT TRACK 12, CRACKED BETWEEN TWO FASTENER HOLES. R & R SLAT TRACK 12, INBD LE RIB IAW A319 SRM 51-42-11, PAR 6 A, 7 B & 13.D & PRODUCTION DRAWING D57443551.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. RT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED 9 EACH INDICATIONS, BETWEEN UPPER & LOWER PANELS, THAT ARE IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED RT ELEVATOR 9 EACH AREAS OF LIQUID INGRESS RU1 - RU8 & RL1 WITH HOT BONDER IAW A319 SRM 55-20-00, PB201, PAR 2 A, PAR 2 B & SRM 55-21-11, PB201, CL, PAR 5 D & FIG 204, SH1. WEIGHED ELEVATOR IAW A319 CMM 55-21-15, PAR 3, FOUND WITHIN LIMITS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT OUT OF SERVICE FOR C8 S2 CHECK. AFT CABIN FLOOR BEAM, FWD OF L2 DOOR AT FR 67, HAS CORROSION. DETERMINED CORROSION TO BE OUT OF LIMITS. R & R AFT CABIN FLOOR BEAM AT L2 DOOR, FR 67, IAW A319 SRM 51-42-11, PAR 5 A.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. RT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED 1 EACH INDICATION RU9 ON UPPER PANEL THAT IS IRREGULAR IN SHAPE & BLACK IN COLOR. LIGHTNING STRIP REMOVAL, REQUIRED DUE TO INDICATION BEING PARTIALLY OCCLUDED BY LIGHTNING PROTECTION PLATE. REPAIRED RT ELEVATOR 1 EACH AREAS OF LIQUID INGRESS RU9 UNDER LIGHTNING PROTECTION STRIP, WITH HOT BONDER & REINSTALLED LIGHTNING STRIP IAW A319 SRM 55-20-00, PB201, PAR 2 A, PAR 2 B & SRM 55-21-11, PB201, C1, PARA 2, 5 N & FIG 214, SH L & 2. WEIGHED ELEVATOR IAW A319 CMM 55-21-15, PAR3, FOUND WITHIN LIMITS.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. LT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED 12 INDICATIONS ON UPPER PANEL THAT ARE IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR 12 EACH AREAS OF LIQUID INGRESS WITH HOT BONDER IAW A319 SRM 55-20-00, PB201, PAR 2 A & SRM 55-21-11, PB201, C1, PAR 5 D & FIG 204, SH 1. WEIGHED ELEVATOR IAW A319 CMM 55-21-15, PAR 3, FOUND WITHIN LIMITS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN RT AFT LAVATORY ATTACHMENT POINT HAS MINOR CORROSION ON FLOOR BEAM. R & R FLOOR BEAM IAW SRM 51-42-11 PARAGRAPH 6.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN RT LATERAL SHEAR PLATE HAS CORROSION BETWEEN FR 69 - FR 70, STRINGER 23. R & R RT SHEAR PLATE IAW SRM 51-42-11, PARAGRAPH 6, 7 & 13.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE HAS CORROSION BETWEEN FR 69 - FR 70, STRINGER 23. R & R LT SHEAR PLATE IAW SRM 51-42-11, PARAGRAPH 6.B 1 - 8.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. DOT 086, 023 SILL FRAME IN FWD BAG PIT HAS CORROSION, DOOR SILL. REMOVED LIGHT SURFACE CORROSION FROM FWD DOOR SILL. MEASURED WITH DEPTH GAUGE T98225 1 CAL. DUE 5-10-2014, FOUND TO BE WITHIN LIMITS IAW SRM 51-73-00 FIG. 001. ALODINED, PRIMED & TOP COATED IAW SRM 51-21-11 AND 51-75-12.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,492 hrs · 19,071 cycles

AIRCRAFT IS OUT OF SERVICE DUE TO C8 S2 CHECK. FWD CARGO COMPARTMENT THRESHOLD WEB FWD OF FRAME 26 RT HAS SURFACE CORROSION AT NUTPLATE UPPER & LOWER SURFACES. BLENDED WITHIN LIMITS LIGHT SURFACE CORROSION IAW SRM 51-73-00 FIGURE 001, SRM 51-21-11 & SRM 51-75-12.

Part: ENGINE — LEAKING (RIGHT) · airframe 36,121 hrs · 17,302 cycles

SMOKE IN THE CABIN, AIR RETURN TO DEPARTURE. BORESCOPED LT AND RT ENGINES, FOUND OIL WETTING IN RT ENGINE. R & R ENGINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,342 hrs · 16,885 cycles

EMERGENCY LIGHT ON SEAT 15 ABC INOPERATIVE. R & R ROW 15 ABC EMERGENCY SEAT LIGHT IAW AMM 33·51·19 PB 401. OPS CHECKED GOOD.

Part: FILTER — CONTAMINATED (A/C PACK) · airframe 34,931 hrs · 1,665 cycles

BLOCK TURN BACK OILY SMELL IN CABIN AFTER TAXI OUT. RAN BOTH ENGINES AND APU WITH AIR CONDITIONING PACKS FULL HOT AND FULL COLD TO VENT AIR CONDITIONING SYS. R & R RECIRCULATION FILTERS AND OPS CHECKS NORMAL IAW AMM 21-21-41, PB 401.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,792 hrs · 16,595 cycles

EMERGENCY LIGHT POWER SUPPLY BATTERY 11WL FAILED TEST AT HEAVY SERVICES CHECK. R & R BATTERY UNIT IAW 33-51-38-000-002A AND 33-51-38-400-002A, UNIT CHECK NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 34,730 hrs · 16,565 cycles

DURING C-CHECK, AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N403; AFT CARGO BAY PANEL FOR LIVETV ON THE FLOOR PANEL 161EF HAS DELAMINATION AND SKIN DAMAGE AT CORNER. FABRICATED REPLACEMENT PANEL 161EF IAW MCG IRM 9701 REV G.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N305; CABIN FLOORBEAM Y1292 BETWEEN FRAMES 66 AND 68 HAS 3 AREAS OF EXFLOTATION. R & R FLOORBEAM Y1292 AT FRAME 66 TO 68 IAW SRM 51-42-11 PARA 5 AND 7.

Part: NUT — LOOSE (L1 DOOR SLIDE) · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0742; PAX DOOR L1 ESCAPE SLIDE WOULD NOT ARM PROPERLY. FOUND SEALING NUT OUT OF FLEXIABLE CONTROL UPPER END. RETORQUED SEALING NUT IAW AMM 12-22-52-640-063 A.3.(F). DOOR ARMS PROPERLY.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0538; MAIN CABIN RT SIDE FROM FRAME 69 TO FRAME 70 SHEAR PLATE HAS 6 SQUARE INCHES OF CORROSION. R & R SHEAR PLATE AT FRAME 69 TO 70 IAW SRM 51-72-11 PAGE 1-3 AND E.O. A0-53EO-31434.

Part: NUT — LOOSE (R1 DOOR SLIDE) · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0743; PAX DOOR R1 ESCAPE SLIDE WOULD NOT ARM PROPERLY. FOUND SEALING NUT OUT OF FLEXIABLE CONTROL UPPER END.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0539; LT SHEAR PLATE BETWEEN FRAMES 69L TO 70L HAS 1 SQUARE INCH CORROSION AND IS THE OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW SRM 51-72-11 PAGE 1-3 AND EO A0-53EO-31434.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0319; FLOORBEAM -Y1292 BETWEEN FRAMES 67.5 AND 68 HAS 2 HOLES WITH CORROSION OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOORBEAM -Y1292 BETWEEN 67.5 AND 68 IAW SRM 51-42-11, PARA 7.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0316; CABIN FLOORBEAM Y1292 AT FRAME 68, 3 INCHES FORWARD OF THE FRAME HAS A 0.5 INCH X 0.5 INCH AREA OF CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PAR 5 AND 7.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,419 hrs · 14,426 cycles

C-CHECK: NON ROUTINE N0707; DURING EMERGENCY LIGHT TEST, SEATS 19, 21, 23 AND AFT OVERHEAD EMERGENCY LIGHTS FLASHED. R & R EPSU 13WL IAW AMM 33-51-38 PB 401. PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS IAW AMM 33-51-38-740-050. OPS CK GOOD.

Part: OVEN — ODOR (GALLEY) · airframe 26,969 hrs · 12,747 cycles

THE FLIGHT CREW REPORTED A BURNING ODOR COMING FROM THE NR 2 OVEN. THE CIRCUIT BREAKER WAS PULLED AND MX DEFERRED THE NR 2 OVEN IAW NEF 25-99-30AE.

Part: TRANSPONDER — FAILED (ATC) · airframe 24,915 hrs · 11,763 cycles

DURING SCHEDULED MX TASK CARD TC34210-07, ATC TRANSPONDER NR 2 FAILED FUNCTIONAL TEST. MX REMOVED AND REPLACED THE NR 2 ATC TRANSPONDER AND PERFORMED BITE TEST, REF AMM 34-52-33 PB 401.

Part: SERVO CONTROL — FAULTED (ELEVATOR/AILERON) · airframe 24,793 hrs · 11,701 cycles

AIRCRAFT RETURNED TO BLOCK IN DEN DUE TO NR 1 ELAC (ELEVATOR AILERON COMPUTER) FAULT. MAINTENANCE REMOVED AND REPLACED THE RIGHT BLUE SYSTEM ELEVATOR SERVO AND PERFORMED OPERATIONAL AND LEAK CHECK, REFERENCE AMM 27-34-51 PB 401 AND 27-34-00-820-002. MAINTENANCE SUSPECTS INTERNAL BINDING OR HYDRAULIC LOCK IN SERVO.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 24,793 hrs · 11,701 cycles

DURING C5 C-CHECK, INSPECTION NOTED THAT RIGHT OVERWING EXIT ARM LIGHT FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AND PERFORMED OPERATIONAL TEST, REFERENCE AMM 33-51-38-000-002 AND AMM 33-51-38-400-001.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SEAT TRACK FLOORBEAM +Y1292 FROM FR 64 TO 4 INCHES AFT OF FR 66 CORRODED AT NUTPLATE HOLES. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 AND 51-44-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR SILL CORRODED AT NUTPLATE HOLES UNDER FWD L2 GIRT BAR FITTING/PLATE AREA, JUST AFT OF FR66. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 52-42-11.

Part: FAIRING — CRACKED (NR 1 ENGINE) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED NR 1 ENGINE FAN OUTLET FAIRING INSTALLATION HAD CRACKS AT THE 7 O'CLOCK AND 9 O'CLOCK POSITIONS. REMOVED AND REPLACED NR 1 ENGINE FAN OUTLET FAIRING IAW SRM 51-44-11, 51-42-11 AND AMM 51-75-12-300-003.

Part: BOLT — CORRODED (LAVATORY MOUNT) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED ONE BOLT FOR FLOOR HOLD DOWN ON LAVATORY E CORRODED. REMOVED AND REPLACED CORRODED BOLT IAW AMM 25-43-42-100-001.

Part: ATTACH BOLT — CRACKED (RUDDER ATTACH) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RUDDER ATTACH FITTING NR 7 ATTACHMENT BOLT CRACKED AROUND CENTER CIRCUMFERENCE AREA. REMOVED AND REPLACED HARDWARE IAW AMM 27-21-41-420-051.

Part: ATTACH BOLT — CORRODED (AILERON) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT AILERON NR 3 HINGE SUPPORT FRAME ATTACHMENT BOLTS (ATTACHES TO BRACKET ON WING) WORN AND CORRODED. REPLACED RT AILERON NR 3 HINGE SUPPORT BRACKET MOUNTING BOLTS IAW AMM 57-51-31-400-0001.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED TWO CORRODED FASTENERS IN THE R2 AFT GIRT BAR MOUNT PLATE. BLENDED OUT CORROSION ON OTBD MIDDLE FASTENER HOLE, BOTTOM SIDE OF SILL PLATE IAW SRM 51-22-00 - WITHIN LIMITS IAW SRM 53-41-14-PG103/104. INSTALLED AFT GIRT BAR MOUNT PLATE IAW SRM 51-42-11.

Part: STRUCTURE — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CONNECTING SECTION ASSY (BROWN PIECE THAT GOES UNDER THE FLOOR PANEL AND UP THE SIDE OF THE FLOOR PANEL) CORRODED AT FR66. INSTALLED REPLACEMENT SECTION ASSY IAW SRM 51-42-11, PARA 5.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR SILL, FWD SPLICE JUST FWD OF FR66. REMOVED SPLICES AND RE-MEASURED AREA. SUBMITTED EAR FOR APPROVAL OF MATERIAL LOSS. ROTOPROBED HOLES AND REINSTALLED SPLICES AND NEW COUPLING IAW EA A9-53R-12290.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FRAME SUPPORT CORRODED AT FR 69-70, -Y1732. REMOVED AND INSTALLED REPLACEMENT FRAME SUPPORT IAW SRM 51-42-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SILL AT AFT INBD END AT NUT PLATE HOLES, APPROX 1-4 INCHES FWD OF FR 68. DETERMINED DAMAGE TO BE OUT OF LIMITS IAW SRM 53-41-14. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 52-42-11.

Part: STRAP — CORRODED · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C-4/S1 CHECK, INSPECTION REPORTED PANEL 262EF TIE-DOWN STRAP CORRODED. REPLACED AFT TIE-DOWN STRAP ON PANEL 262EF IAW AMM 53-32-12-400-002.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED MAIN CABIN FLOORBEAM AT FR16, +Y254, CORRODED. DETERMINED CORROSION TO BE OUT OF LIMITS IAW SRM 53-11-14. CUT OUT CORRODED AREAS, AND FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-11-14 AND 51-75-12.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR SILL CORRODED IN TWO AREAS AFT OF INBD AFT NUTPLATE HOLE LOCATED 1.5 INCHES AND 2.5 INCHES AFT. REPAIRED CORRODED AREAS IAW SRM 53-41-14, FIG 101, PAGES 103/104.

Part: BLANKING PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R2 GIRT BAR CORRODED. REMOVED AND REPLACED R2 DOOR BLANKING PLATE IAW AMM 52-11-31-400-005.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE AT FR 69-70, -Y1732, CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, PARA 6,7,14, AND EA A9-53R-12267.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBOARD 261FF CORRODED. REMOVED AND REPLACED FLOORBOARD 261FF IAW AMM 53-32-12-400-002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED NUTPLATE HOLES CORRODED ON FLOORBEAM +Y1292 (LT), 4 INCHES FWD OF FR68. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 7.

Part: BLANKING PLATE — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR FWD GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACED R2 DOOR GIRT BAR BLANKING PLATE IAW AMM 52-11-31-400-005.

Part: BLANKING PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R2 DOOR AFT GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACED R2 DOOR AFT BLANKING PLATE IAW AMM 52-11-31-400-005.

Part: FITTING — CRACKED (NLG) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CRACK IN HOLE H4 ON THE NLG FITTING MOD (EO NR A0-53EO-20373, REV. B). UPSIZED HOLE FROM .277 TO .309 AND RE-INSPECTED HOLE. NO DEFECTS NOTED. INSTALLED NEW FASTENER IAW EA NR A9-53R-12284 AND SRM 51-49-00, TABLE 18.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED MAIN CABIN FLOOR DUMMY RAIL AT +Y503.2 BETWEEN FR 12 AND 16 CORRODED. REMOVED AND INSTALLED CORRODED DUMMY RAIL IAW SRM 51-42-11, 51-44-11 AND DWG D531 12825.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT SHEAR PLATE CORRODED AT FR 69-70 AT BEAM +1732 (APPROX). REMOVED AND INSTALLED LT AFT SHEAR PLATE IAW SRM'S 51-72-11 AND 51-42-11.

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND L2 DOOR FWD GIRT BAR ATTACH BRACKET MOUNTING HOLES. REMOVED AND REPLACED GIRT BAR BLANKING PLATE IAW AMM 52-11-31-000-005 AND 52-11-31-400-005.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AMM 53-12-12-PB401, AMM 53-12-12-400-001, AND FRONTIER WORK CARD CP753-12.

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 DOOR AFT GIRT BAR BRACKET CORRODED AROUND ATTACH POINTS. REMOVED AND REPLACED GIRT BAR BLANKING PLATE IAW AMM 52-11-31-000-005 AND 52-11-31-400-005.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR SILL, INBD AFT TWO NUTPLATE HOLES AND NUTPLATE HOLE LOCATED OTBD AND AFT OF FWD GIRT BAR FITTING ON SILL. REPAIRED CORRODED AREAS IAW SRM 53-41-14, PRINCIPAL 5 REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM NUTPLATE HOLES AT +Y1292 (LT), 4 INCHES FWD OF FR68-69. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM'S 51-74-00, 51-42-11, 53-00-14, 51-44-11, 51-75-12 AND EA A9-53R-12267 (STEPS 1 AND 2).

Part: PLATE — LOOSE (FUSELAGE) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SILL PLATE AT FRAME 68, AFT AND OTBD OF +Y1292 BEAM. REMOVED SHEARED RIVETS THAT CONNECT PLATE TO FLOOR BEAM IAW SRM 51-42-11. REPLACED THE FOUR SHEARED BLIND RIVETS THAT ATTACH THE SHEAR PLATES TO THE LONGITUDINAL BEAMS WITH HL11VF6 LOCK FASTENERS. REPLACED THE SHEARED SOLID RIVETS THAT ATTACH THE JOINT SHEETS TO THE LONGITUDINAL BEAMS WITH HL11VF6 LOCK FASTENERS. ABOVE WORK ACCOMPLISHED IAW EA A9-53R-12267.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED BOTTOM OF FLOORBOARD 261FF CORRODED. REMOVED AND REPLACED FLOOR 261FF IAW AMM 53-32-12-400-002.

Part: SPLICE — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221LF SPLICE PLATE CORRODED, AFT END. REPLACED AFT SPLICE PLATE ON FLOOR PANEL 221LF IAW AMM 53-12-12-PB401 AND WORK CARD CP753-12.

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED BOTTOM OF FLOORBOARD 221FF CORRODED. REMOVED AND REPLACED FLOOR PANEL 221FF IAW MM 53-12-12-401 AND 53-12-12-400-001.

Part: FLOORBOARD — CORRODED (CABIN) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED BOTTOM OF FLOORBOARD 222FF CORRODED. REMOVED AND REPLACED FLOOR PANEL 222FF IAW MM 53-12-12-PB401 AND 53-12-12-400-001.

Part: PLATE — LOOSE (FUSELAGE) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SILL PLATE AT FRAME 69, -Y1292 FLOORBEAM. REMOVED SHEARED RIVETS ON WEB PLATE AFT OF FR68 FLOORBEAM AT -Y1292 IAW SRM 51-42-11, PARA. 6. INSTALLED LOCK FASTENER THROUGH WEB PLATE AFT OF FR68 THAT ATTACHES TO -Y1292 BEAM IAW EA A9-53R-12267.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATE HOLES OF FLOORBEAM -Y1292 BETWEEN FR 66 AND 70. REMOVED AND REPLACED FLOORBEAM -Y1292 IAW SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR FITTING UNDER CABINET SECTION OF AFT GALLEY CORRODED. REMOVED AND REPLACED CORRODED FITTING IAW AMM 25-33-41-400-002.

Part: FASTENER — CORRODED (WINDOW) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SCREWS RUSTY AROUND THE OUTSIDE OF THE FIRST OFFICER'S RT AFT FIXED COCKPIT WINDOW. REMOVED FIXED WINDOW IAW AMM 56-11-12-000-001. INSTALLED FIXED WINDOW IAW AMM 56-11-12-000-002. PERFORMED OPS TEST OF WINDOW HEAT SYSTEM IAW 30-42-00-710-001. OPS CHECKED NORMAL.

Part: STRUCTURE — CRACKED (RT PYLON) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CRACK EMANATING FROM RT PYLON (OTBD UPPER, ABOVE TR) SCREW HOLE. CUT OUT DAMAGED AREA, FABRICATED REPAIR FILLER AND SPLICE, AND INSTALLED REPAIR IAW SRM 54-52-11, REPAIR E, STEP 2C; 54-52-12, FIG. 205; AND EA A9-54R-12271.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BATTERY FROM POWER SUPPLY UNIT 12WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001. OPS TEST NORMAL.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FWD LT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BATTERY FROM POWER SUPPLY UNIT 10WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001. OPS TEST NORMAL.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BATTERY FROM POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-001. OPS TEST NORMAL.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 19,058 hrs · 8,878 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. REMOVED EMERGENCY BATTERY FROM POWER SUPPLY UNIT 11WL IAW AMM 33-51-38-000-002. INSTALLED SERVICEABLE BATTERY IAW AMM 33-51-38-400-002. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-001. OPS CHECK NORMAL.

Part: CONTROL UNIT — INOPERATIVE (MLG) · airframe 16,723 hrs · 7,709 cycles

FLIGHT CREW REPORTED ECAM L/G LGCIU2 FAULT ON APPROACH. PERFORMED GO-AROUND AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) IAW 32-31-71-400-001 AND TESTED GOOD.

Part: STOWAGE BOX — NO TEST (OXYGEN MASK) · airframe 13,360 hrs · 6,018 cycles

DURING C-3 CHECK, CAPTAINS O2 MASK FAILED PRESS-TO-TEST. REPLACED CAPTAINS O2 BOX ASSY PER AMM 35-12-41-000-001, 35-12-41-406-001 AND 35-12-41-710-001. OPS CHECKED GOOD.

Part: FRAME — MISDRILLED (FR 54) · airframe 13,360 hrs · 6,018 cycles

DURING C-3 CHECK, INSPECTION REPORTED RIVET HOLE AT FRAME FS 54, STR 4L, FOUND MISDRILLED. REPAIRED PER EA A9-53R-11345.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,360 hrs · 6,018 cycles

DURING C-3 CHECK, INSPECTION REPORTED RIVET HOLE AT FRAME FS 54, STR 4L, FOUND MISDRILLED. REPAIRED PER EA A9-53R-11345.

Part: FLOORBEAM — CORRODED (FR 66 - 68) · corrosion level 2 · airframe 13,360 hrs · 6,018 cycles

DURING C3 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOORBEAM AFT OF FRAME 66 AND FORWARD OF FRAME 68 (10" INBD OF L2 DOOR CUTOUT) AT OR NEAR CLIPNUTS AT FS 66. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 AND EA A9-53R-11343.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 13,360 hrs · 6,018 cycles

DURING C3 CHECK, INSPECTION REPORTED SURFACE CORROSION ON FLOORBEAM AFT OF FRAME 66 AND FORWARD OF FRAME 68 (10" INBD OF L2 DOOR CUTOUT) AT OR NEAR CLIPNUTS AT FS 66. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 AND EA A9-53R-11343.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 13,360 hrs · 6,018 cycles

DURING C-3 CHECK, INSPECTION REPORTED RT WING OTBD FLAP L/E BETWEEN NR 3 AND 4 FAIRINGS DAMAGED. CUT OUT DAMAGED SKIN PER SRM 57-53-00, PAGE 213. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-53-00 AND EA A9-57R-11353.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 13,360 hrs · 6,018 cycles

DURING C-3 CHECK, INSPECTION REPORTED STR 4L DAMAGED AT FRAME 54. CUT OUT DAMAGED STRINGER SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 53-00-13, PAGE 201.

Part: CHECK VALVE — BROKEN (RT A/C PACK) · airframe 10,778 hrs · 4,803 cycles

FLIGHT CREW REPORTED STRONG, SMOKY/BURNING ELECTRICAL FUMES ON DESCENT AND WAS STRONGER IN AFT CABIN. REPLACED RT PACK CHECK VALVE (19HM) PER AMM 21-63-42, PB 401. NO LEAKS OR ODOR NOTED.

Part: COVER — OUT OF ADJUST (EMERGENCY EXIT) · airframe 46 hrs · 22 cycles

ABORTED TAKEOFF. FLIGHT CREW REPORTED LT OVERWING EMERGENCY EXIT OPEN INDICATION AT 100 KTS. ADJUSTED LT OVERWING EXIT DOOR HANDLE COVER FLAP. TESTED PER MM 25-23-47-401, TASK 25-23-47-991-017, FIG 402, AND CHECKED OKAY.