N932FR

Part: BATTERY — FAULTY (CABIN) · airframe 33,076 hrs · 16,283 cycles

HEAVY CHECK FOUND EPSU BATTERY FAULT 13WL. R & R EPSU BATTERY 13WL IAW AMM 33-51-38-000-002 & AMM 33-51-38-400-002, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 33,076 hrs · 16,283 cycles

HEAVY CHECK FOUND EPSU BATTERY FAULT 12WL. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002 & AMM 33-51-38-400-002, OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,898 hrs · 16,193 cycles

DURING OVERNIGHT INSPECTION THE LT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY WAS FOUND DEAD. R & R LT OVERWING EPSU BATTERY IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,300 hrs · 15,327 cycles

AIRCRAFT OUT OF SERVICE FOR C6 CHECK. CORROSION ON FLOORBEAM AT L2 DOOR, FR67, Y1292. FOUND TO BE OVER 50 PERCENT MATERIAL LOSS, OUT OF LIMITS. REMOVED BEAM, LOCATED AND DRILLED NEW BEAM, REF SRM 51-44-11. INSTALLED NEW BEAM REF SRM 51-42-11, PAR 5.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,301 hrs · 15,327 cycles

ACFT OUT OF SERVICE DUE TO C6 CHECK. AFT GALLEY FLOORBEAM AT R2 DOOR ENTRY -Y1292, FRAME 68 HAS LIGHT CORROSION UPPER SURFACE. BLENDED IAW SRM 53-00-14, PB101, PARA 4.B AND SRM 51-75-12, PARA 3.C.(6)(7). FOUND TO BE WITHIN LIMITS.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,301 hrs · 15,327 cycles

AIRCRAFT OUT OF SERVICE DUE TO C6 CHECK. DISCREPANCY: AFT GALLEY FLOORBEAM AT L2 DOOR ENTRY Y1292, FRAME 68 HAS CORROSION. CORRECTIVE ACTION: BLENDED PER SRM 53-00-14, PB101, PARAGRAPH 4.B. AND SRM 51-75-12, PARAGRAPH 3.C.(6)(7). FOUND TO BE WITHIN LIMITS.

Part: BATTERY PACK — DISCHARGED (POWER SUPPLY) · airframe 30,747 hrs · 15,043 cycles

EMERGENCY LIGHT TEST FAILS FORWARD EPSU BATTERY. REPLACED FORWARD EPSU BATTERY REF AMM 33-51-38-400-002-A. OP'S CHECK NORMAL.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 23,858 hrs · 11,586 cycles

PRIOR PUSH BACK, RT FWD DOOR WOULD NOT ARM BTB. ADJUSTED R-1 DOOR SLIDE GIRTBAR ATTACH, OPS CHECK GOOD, SLIDE ARMS AS REQUIRED. REF AMM 25-62.00, PB 501. OK TO CONTINUE FLIGHT.

Part: WIRE — LOOSE (CABIN) · airframe 21,676 hrs · 10,564 cycles

LEFT AFT EMERGENCY SIGN LIGHT INOPERATIVE. FOUND WIRE 3351-1306 NOT LOCKED INTO TERMINAL BLOCK 7222VT. RE-LOCKED POWER WIRE INTO TERMINAL BLOCK REFERENCE A319 AMM 33-51-03. OPERATIONAL CHECK NORMAL REFERENCE A319 AMM 33-51-00-710-007.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0894. FLOOR PANEL 231KF HAS TWO EACH PUNCTURES. REPAIRED FLOOR PANEL 231KF IAW A319 SRM 53-02-00 SOLUTION A.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0848. L-2 DOOR SILL CORRODED AT GIRT BAR FITTING MOUNT HOLES. REMOVED AND REPLACED L-2 DOOR SILL IAW A319 SRM 51-42-11 AND 51-72-11 PARAGRAPHS 5A AND 6A.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

R-1 DOOR SILL IS CORRODED. REMOVED AND REPLACED DOOR SILL IAW A319 SRM 51-44-11 AND SRM 51-72-11 PAGE 1 STEP 6.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0772. CABIN FLOOR PANEL 231KF HAS DELAMINATION ON TOP LAYER. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0649. AFT CARGO FLOOR PANEL 161EF DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0567. CORROSION ON UPPER SIDE OF FLOORBEAM Y1292 AT FRAME 68. REMOVED AND REPLACED FLOORBEAM Y1292 FROM FRAME 68 TO FRAME 70 IAW A319 SRM 51-42-11 AND 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0531. RIGHT SHEAR PLATE IN CABIN FLOOR STRUCTURE BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11 AND EO A0-53EO-31434.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0612. SUPPORT FRAME CORRODED BETWEEN FRAME 69 AND FRAME 70 RIGHT. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-44-11.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0524. AFT CARGO FLOOR PANEL 151AE DENTED WITH COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0526. AFT CARGO FLOOR PANEL 151BE HAS 30 SQUARE INCHES OF DENTS WITH CRACKS AND COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0613. FRAME SUPPORT FROM FRAME 69L TO FRAME 70L AT STRINGER 23L CORRODED. REMOVED AND REPLACED FRAME SUPPORT IAW A319 SRM 51-42-11 PARAGRAPH 6.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0505. AFT CARGO PIT FLOOR PANEL 151UG IS DENTED CRACKED AND HAS COMPRESSION DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW MCG IRM 9701 REVISION G.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0502. AFT CARGO PIT FLOOR PANEL 152UG DENTED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0473. BULK CARGO FLOOR PANEL 161CF HAS APPROXIMATELY 20 SQUARE INCHES OF DENTS WITH COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL 161CF IAW MCG IRM 9701 REVISION G.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE NO523. AFT CARGO FLOOR PANEL 152TG DENTED WITH COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: FLOOR PANEL — DENTED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0504. AFT CARGO FLOOR PANEL 152XG DENTED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

FORWARD CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED FORWARD CARGO DOOR SILL REFERENCE EA A0-53R-31817 REVISION A PAGES 1 THRU 5.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0648. AFT CARGO FLOOR PANEL 162EF MISSING SKIN AT CORNER. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0006. TEMPORARY FASTENER INSTALLED AT FRAME 13 LEFT AT STRINGER 18 LEFT. INSTALLED PERMANENT REPAIR IAW AIRBUS SRM 53-11-11 PARAGRAPH 5.E. FIGURE 208 AND EA A9-53R-30716.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0003. TEMPORARY REPAIR INSTALLED AT FRAME 12 LEFT AT STRINGER 19 LEFT. INSTALLED PERMANENT REPAIR IAW AIRBUS SRM 53-11-11 PARAGRAPH 5E FIGURE 208 AND EA A9-53R-30716.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 21,676 hrs · 10,564 cycles

REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0005. TEMPORARY REPAIR INSTALLED AT FRAME 16 LEFT AT STRINGER 16 LEFT. INSTALLED PERMANENT REPAIR IAW AIRBUS SRM 53-11-11 PARAGRAPH 5B FIGURE 208 AND EA A9-53R-30716.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON THE LOWER SURFACE. MAINTENANCE REPLACED FLOOR PANEL WITH NEW IN ACCORDANCE WITH A319 AMM 53-42-12-400-002.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED L2 DOOR SILL, AFT OF GIRT BAR FITTING, AFT OUTBOARD NUT PLATE HOLE HAS SIGNS OF CORROSION. MAINTENANCE REMOVED NUT PLATE IN ACCORDANCE WITH A319 SRM 51-42-11, ENLARGED HOLE TO CLEAN CORROSION, PRIMED AND PAINTED IN ACCORDANCE WITH A319 SRM 51-75-12 AND ENGINEERING AUTHORIZATION A9-53R-30723.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON THE LOWER SURFACE. MAINTENANCE REPLACED FLOOR PANEL WITH NEW IN ACCORDANCE WITH A319 AMM 53-42-12-400-002.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED LONGERON Y1292 FORWARD OF FRAME 68 HAS CORROSION ON FORWARD INBOARD NUT CLIP HOLE. MAINTENANCE REMOVED CORROSION IN ACCORDANCE WITH A319 SRM 53-00-14, FIGURE 102. ROTO-PROBED HOLES WITH NO DEFECTS NOTED IN ACCORDANCE WITH NTM 51-10-01. ALL WORK ACCOMPLISHED PER ENGINEERING AUTHORIZATION A9-53R-30725.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED LONGERON Y1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN NUMEROUS NUT CLIP HOLES. MAINTENANCE REWORKED 4 HOLES TO REMOVE ALL CORROSION IN ACCORDANCE WITH A319 SRM 53-00-14 FIGURE 102. ROTO-PROBED HOLES WITH NO DEFECTS NOTED. TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH ENGINEERING AUTHORIZATIONS A9-53R-30730 AND A9-53R-30731.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED R2 DOOR SILL, AFT OF GIRT BAR FITTING, AFT OUTBOARD NUT PLATE HOLE HAS SIGNS OF CORROSION. MAINTENANCE REMOVED NUT PLATE IN ACCORDANCE WITH A319 SRM 51-42-11, ENLARGED HOLE TO CLEAN CORROSION, PRIMED AND PAINTED IN ACCORDANCE WITH A319 SRM 51-75-12 AND ENGINEERING AUTHORIZATION A9-53R-30726.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED LONGERON -Y1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION ON NUMEROUS NUT CLIP HOLES. MAINTENANCE REMOVED DAMAGED BEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PARAGRAPHS 6 AND 7. MAINTENANCE INSTALLED NEW FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PARAGRAPH 5.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 15,760 hrs · 7,666 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE PATH LIGHT PLUG IN FOR ROW 8, SEATS ABC, WAS PULLED OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT WIRING AND PLUG IN ACCORDANCE WITH ASM 33-51-00 SCH 04 P 105, FIGURE 2 AND AMM 33-51-00-710-009. MAINTENANCE PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH AMM 33-51-00-710-009.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 11,793 hrs · 5,730 cycles

DURING HEAVY SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT ROWS 15 AND 16. RE-SECURED LOOSE CONNECTOR AT SIDE PANEL. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-001 AND CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,365 hrs · 5,532 cycles

DURING HEAVY CHECK, INSPECTION REPORTED EMERGENCY FLOOR PATH WHITE LIGHT AT ROW 5 INOPERATIVE. RELAMPED BOTH LAMPS AT ROW 5 EMERGENCY FLOOR PATH WHITE LIGHT. OPS CHECKED GOOD IAW AMM 33-51-19-400-002.

Part: CONTROL SERVO — FAULTED (NLG STEERING) · airframe 8,047 hrs · 3,885 cycles

FLIGHT CREW REPORTED FOLLOWING ECAM: (WHEEL N/W STRL FAULT), AT CRUISE THROUGH LANDING. PRIOR TO LANDING AT SFO, A FLY-BY WAS PERFORMED TO ENSURE THE NOSE WHEEL WAS ALIGNED CORRECTLY. AN EMERGENCY WAS DECLARED UPON LANDING IN SFO AND AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. FAULT RE-OCCURRED AFTER THE BSCU WAS RESET AT THE GATE, THEN DISAPPEARED AFTER APPROX. 1 MINUTE. IAW AMM 32-51-00-720-004, FOUND CONNECTOR PLUG ON NLG STEERING SOLENOID LOOSE. CLEANED AND RESECURED CONNECTOR PLUG. PERFORMED FUNCTIONAL TEST OF THE N/W STEERING WITH PEDALS. FLIGHT CREW PERFORMED TAXI. TAXI OPS NORMAL, NO DEFECTS NOTED. SUBSEQUENTLY, DURING FIRST ENGINE START, THE FAULT RE

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 6,442 hrs · 3,047 cycles

DURING APPROACH INTO DEN, FLIGHT CREW RECEIVED A TCAS RA, GENERATED FROM PARALLEL TRAFFIC IN THE AREA AND WAS INSTRUCTED TO INITIATE A GO-AROUND AND CLIMB TO 8000 FT. CLEAN UP AND ACCELERATION WAS NORMAL UNTIL A WING TIP BRAKE ECAM WAS TRIGGERED, WITH FLAPS SELECTED IN POSITION 1. FLAPS F-LOCKED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AND WITHOUT INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING PER TASK 27-51-00-810-810, WITH NO DEFECTS NOTED. FLAPS OPS CHECKED GOOD PER AMM 27-54-00-710-001. THERE WAS HIGH TURBULENCE DURING APPROACH.

Part: COMPUTER — MALFUNCTIONED (FLT MANAGEMENT) · airframe 2,694 hrs · 1,257 cycles

AUTOPILOT APPEARED TO ENTER A HARDOVER CONDITION, DISCONNECTED A/P AS ACFT ATTEMPTED TO ROLL RIGHT PAST 30" ADB. PERFORMED AFS TEST, TESTED OK. PERFORMED LAND CAT 3 TEST, TESTED OK. ACCOMPLISHED MEL 02-60-01A. PERFORMED DOWNLOAD OF FLT DATA RECORDER, NO TURBULENCE OR PILOT ERROR. ROLL ANGLE DIFFERENTIAL LIGHT DID NOT INDICATE ANY ANOMALIES. BOTH FMGC'S WERE REPLACED AS PRECAUTIONARY. BOTH UNITS HAVE BEEN QUARANTINED FOR EVALUATION BY AIRBUS. IN DEN, PERFORMED ANOTHER AFS TEST & LAND CAT IIIB TEST, OPS TEST CHECK GOOD. UPGRADED CAT IIIB, REMOVED MEL. 1ST OCCURRENCE ON F9 FLEET, PER AIRBUS, VERY RARE. OEB JANUARY, 2005, INDICATES SOFTWARE ISSUE. PER AIRBUS, NEW SOFTWARE WILL BE DESIGNED THIS SUMMER.