N931FR

Part: STRUCTURE — CONTAMINATED (RT ELEVATOR) · airframe 30,870 hrs · 15,068 cycles

RT ELEVATOR, THERMOGRAPHY INSPECTION SHOWS FOUR INDICATIONS OF WATER INGRESS, LOCATED ON UPPER SKIN PANEL. INDICATIONS ARE IRREGULAR IN SHAPE AND BLACK IN COLOR. SEE NDT REPORT FOR SPECIFIC LOCATIONS. REMOVED SKIN AT AREAS OF LIQUID INGRESS. COMBINED AREAS 1 & 2 DUE TO PROXIMITY. PREPARED SURFACE FOR REPAIR DRIED REPAIR AREAS WITH HOT BONDER, APPLIED EC3524 TO CORE, APPLIED REPAIR PLYS WITH EA9396 A/B RESIN, AND APPLIED VACUUM. SANDED REPAIRS SMOOTH, APPLIED PORE FILLER EPIBOND 156 A/B, APPLIED PRIMER AND TOP COAT IAW SRM 55-20-00, PB 101, DIA2, PB201, PAR2A(1)(A,B), 2A(2)(A-J), 2B(2)(A)1-10 AND SRM 55-21-11, PB201, FIG205, PAR 5E(2)(F)1-6 AND 5E(2)(G).

Part: STRUCTURE — CONTAMINATED (LT ELEVATOR) · airframe 30,870 hrs · 15,068 cycles

LT ELEVATOR, THERMOGRAPHY INSPECTION SHOWS ONE INDICATIONS OF WATER INGRESS, LOCATED ON UPPER SKIN PANEL, INDICATION IS IRREGULAR IN SHAPE AND BLACK IN COLOR. SEE NDT REPORT FOR SPECIFIC LOCATION. REMOVED SKIN AT AREA OF LIQUID INGRESS, PREPARED SURFACE FOR REPIAR. DRIED REPAIR AREAS WITH HOT BONDER, APPLIED EC3524 TO CORE, APPLIED REPAIR PLYS EITH EA9396 A/B RESIN, AND APPLIED VACUUM. SANDED REPAIRS SMOOTH, APPLIED PORE FILLER EPIBOND 156 A/B, APPLIED PRIMER AND TOP COAT IAW SRM 55-20-00, PB201, PAR2A(1-2)(B),2A(2)(A-J), 2B(2)(A)1-10 AND SRN 55-21-11, PB201, FIG204, PAR 5D(2)(E) AND PB101, DIA2.

Part: SIGN — INOPERATIVE (CABIN) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0773. RT FWD LOWER EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. R & R IDENTIFIER IAW AMM 33-51-13-000-001.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0771. EMERGENCY EXIT SIGN OVER LT AFT ENTRY DOOR DOES NOT ILLUMINATE. FOUND CONNECTOR IMPROPERLY SEATED. PROPERLY SEATED CONNECTOR IAW AWM 33-51-04 P005 FIG 3.

Part: EPSU — INOPERATIVE (CABIN) · airframe 21,093 hrs · 10,254 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0772. EMERGENCY EXIT MARKER INOPERATIVE LOWER FWD AT L-1 DOOR. R & R EPSU 10WL IAW AMM 33-51-38-000-001 AND 33-51-38-400-001.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0757. LT ROW 7 EMERGENCY ESCAPE PATH LIGHTING HARNESS HAS 1 EACH WIRE PULLED LOOSE. R & R WIRING HARNESS IAW ASM 33-51-00 SCH 04 P106.

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0733. FWD CARGO FLOOR PANEL 131AF DISBONDED AT CORNERS. REPAIRED IAW SRM 53-02-00, PAGE 208, FIG 203.

Part: FLOOR PANEL — DEBONDED (CARGO BAY) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0601. AFT CARGO FLOOR PANEL 152UG DISBONDED. FABRICATED NEW PANEL IAW MCG IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (CARGO BAY) · airframe 21,093 hrs · 10,254 cycles

REFERENCE HEAVY MX NON ROUTINE N0639. AFT CARGO PANEL 151UG DISBONDED. FABRICATED NEW PANEL IAW NCG IRM 9701 REV G.

Part: FLOOR PANEL — DEBONDED (CARGO BAY) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0654 AFT CARGO FLOOR PANEL 151FE DISBONDED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.

Part: STRUT — CORRODED (RT MLG) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0538. RT MLG INNER BARREL (CYL) HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW EA 3 AC-32R-31779.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,093 hrs · 10,254 cycles

REFERENCE HEAVY MX NON ROUTINE N0432. AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL HAS 6 AREAS OF CORROSION TOTALING 10 SQ INCHES. REPAIRED DOOR SEAL IAW EA A9-53R-31778.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 21,093 hrs · 10,254 cycles

REFERENCE HEAVY MAINTENANCE NON ROUTINE N0366. COCKPIT FLOOR PANEL 211GF IS DELAMINATED. REPAIRED PANEL IAW SRM 5302-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0281. FLOORBEAM AT FRAME 68 BEAM +4765 CORRODED. CUT OUT DAMAGED AREA.FABRICATED REPAIR SECTION AND INSTALLED IAW SRM 53-00-14 FIG 204.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON ROUTINE N0295. LT AFT DOOR SILL AREA FWD OF FRAME 66 ATTACH SUPPORT HAS (6) SQUARE INCHES OF CORROSION ON UPPER SURFACE. R & R DOOR SILL IAW SRM 51-42-11, PAGE 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,093 hrs · 10,254 cycles

HEAVY MX NON-ROUTINE N0283. REAR FUSELAGE FLOORBEAM AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. REPAIRED AREA IAW SRM 53-41-14, PAGE 201, FIGURE 201 PRINCIPLE NR 6.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 21,093 hrs · 10,254 cycles

REF HEAVY MX NON-ROUTINE N0280. AFTER FINDING MINOR CORROSION ON SHEAR PLATE FOUND PART TO BE WRONG CONFIGURATION. R & R SHEAR PLATE IAW EO- A0-53EO-31434.

Part: STRUT — DISCHARGED (ZONE 200) · airframe 19,990 hrs · 9,747 cycles

DURING CLIMB OUT THE FLIGHT CREW RECEIVED A WARNING THAT THE NLG WOULD NOT FULLY RETRACT. MX COMPLIED WITH BORESCOPE INSP OF THE ANTI ROTATION LUG IAW AMM 32-21-00-200-008 AND NO DAMAGE WAS NOTED. MX REPLACED CHARGING VALVE, SERVICED NLG STRUT AND PERFORMED GEAR SWING IAW AMM 32-31-13-420-052, AMM 12-14-32-614-004 AND AMM 32-31-00-720-005.

Part: SELECTOR VALVE — UNSERVICEABLE (MLG) · airframe 19,638 hrs · 9,577 cycles

THE FLIGHT CREW MADE AN AIR RETURN TO DEPARTURE DUE TO AN ELECTRONIC CENTRALIZED ACFT MONITORING MESSAGE FOR NLG DOORS NOT CLOSED AND LANDING GEAR SYS DISAGREE. MX REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AT POSITION 41GA AND PERFORMED A FUNCTIONAL TEST OF LANDING GEAR DOORS WITH NORMAL RESULTS. THE ACFT WAS RETURNED TO SERVICE.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED FLOOR PANEL AND INSTALLED SERVICEABLE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 262EF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED SEVERAL PUNCTURES AND EDGE DELAMINATION TO AFT CARGO TRANSITION PANEL 151AE. MAINTENANCE REMOVED AND REPLACED CARGO PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-14-400-001.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261DF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 212.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FIRE PANEL DISCHARGE LIGHT FOR THE NR 1 FIRE BOTTLE OF THE NR 2 ENGINE FAILS TO ILLUMINATE DURING THE OPERATIONAL CHECK OF THE BOTTLE LOW PRESSURE INDICATING CIRCUIT TEST. MAINTENANCE REMOVED AND REPLACED FIRE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 26-12-12-00-001, 26-12-00-710-001 AND 26-21-00-720-005.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES, HOLES OUT OF LIMITS PER SRM 53-00-14. MAINTENANCE REMOVED CORRODED FLOORBEAM AND UPPER COUPLER AND INSTALLED SERVICEABLE FLOORBEAM AND UPPER COUPLER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11 PARAGRAPH 5B(1) - 6A(2), DRAWINGS D53472816 AND D53472780.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 15,458 hrs · 7,451 cycles

REFERENCE NON-ROUTINE C052153. DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261EF HAS A CUT ON THE SURFACE. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 66, FORWARD HOLE HAS CORROSION. MAINTENANCE BLENDED CORROSION, OVERSIZED HOLE, ROTO-PROBED, TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-00-14, NONDESTRUCTIVE TESTING MANUAL 51-10-01 PART 6, 51-10-08 PART 6 AND ENGINEERING AUTHORIZATION A9-53R-30664.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES, HOLES OUT OF LIMITS PER SRM 53-00-14. MAINTENANCE REMOVED CORRODED FLOORBEAM AND UPPER COUPLER AND INSTALLED SERVICEABLE FLOORBEAM AND UPPER COUPLER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11 PARAGRAPH 5B(1) - 6A(2), DRAWINGS D53472816 AND D53472780.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 68, FORWARD AND AFT HOLES HAVE CORROSION. MAINTENANCE BLENDED CORROSION AND OVERSIZED HOLES IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-00-14, FIGURE 102. MAINTENANCE PERFORMED ROTO-PROBE INSPECTION (NO DAMAGE REMAINS, TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A9-53R-30663.

Part: PLATE — CORRODED (CABIN) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED L-2 GIRT BAR FITTINGS ATTACH PLATE HOLES HAVE CORROSION. MAINTENANCE FABRICATED REPAIR DOUBLER AND FILLER, TREATED, PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A9-53R-30662.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,458 hrs · 7,451 cycles

REFERENCE NON ROUTINE C051883. DURING C3 C CHECK INSPECTION NOTED THE RED EMERGENCY FLOOR PATH INDICATOR ON ROW 11ABC IS NOT ILLUMINATING. MX R&R LIGHT ASSEMBLY IAW THE REQUIREMENTS OF A319 AWM 33-51-07, PAGE 003. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

REFERENCE NON ROUTINE C051966. DURING C3 C CHECK, INSPECTION NOTED FLOOR BEAM Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN SEVERAL HOLES. MX R&R FLOOR BEAM IAW THE REQUIREMENTS OF A319 SRM 51-42-11 AND DRAWING D53472780. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 15,458 hrs · 7,451 cycles

REFERENCE NON ROUTINE CO51711. DURING C3 C-CHECK, INSPECTION NOTED AFT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED CAPACITY CHECK. MX R&R BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-000-001 AND 33-51-38-400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: PLATE — CORRODED (CABIN) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE L-2 FORWARD GIRT BAR FITTING BLANKING PLATE HAS CORROSION ON CORNER. MAINTENANCE REMOVED AND REPLACED L-2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-13-31-400-007.

Part: BLANKING PLATE — CORRODED (ZONE 800) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED GIRT BAR BLANKING PLATE AND INSTALLED NEW, REFERENCE WORK CARD C534103-01.

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 15,458 hrs · 7,451 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE R2 FORWARD DOOR GIRT BAR FITTING BLANKING PLATE IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED CORRODED GIRT BAR BLANKING PLATE AND INSTALLED NEW, REFERNCE WORK CARD C534103-01.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,838 hrs · 6,628 cycles

DURING HEAVY SERVICE CHECK INSPECTION REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-420-052. FOLLOWING INSTALLATION THE SYSTEM WAS TESTED AND CHECKED OKAY.

Part: STOWAGE BOX — NO TEST (CREW OXYGEN) · airframe 9,747 hrs · 4,677 cycles

DURING C-2 CHECK, INSPECTION REPORTED 3RD CREW O2 STOWAGE BOX DID NOT FUNCTION DURING PUSH-TO-TEST. REPLACED 3RD CREW O2 STOWAGE BOX IAW 35-12-41, PB 401. OPS AND LEAK CHECK GOOD.

Part: LATCH — STUCK (GIRT BAR) · airframe 9,747 hrs · 4,677 cycles

DURING C-2 CHECK INSPECTION, REPORTED GIRT BAR LATCH STUCK IN THE DOWN POSITION - L1 DOOR AFT LATCH. CLEANED GIRT BAR FITTING IAW AMM 12-21-12-100-006.