N927FR

Part: UNKNOWN — ODOR (COCKPIT) · airframe 49,839 hrs · 24,570 cycles

MUSKY DIRTY SOCK SMELL ON DECENT BETWEEN 15000 AND 10000 FEET. ONLY IN COCKPIT FA'S DID NOT SMELL IT. PERFORMED TSM 05-50-00-810-813-A PROBABLE CAUSE OF ODOR, NR 1 ENGINE PACK NR 1. INSPECTED PACK DUCTS, COMPRESSOR, OZONE FILTERS PER TSM 21-00-00-615A NO OIL CONTAMINATION NOTED. PERFORMED BORE-SCOPE INSPECTION OF NR 1 ENGINE IAW TSM 71-00-00-810-802-A AND AMM 72-31-00-293-002 NO WETTING PRESENT PERFORMED BURN OF BLEED AIR DUCTS IAW TSM 21-00-615-004-A OPERATED PACKS FULL HOT IAW TSM 71-00-00-710-003 NO ODOR PRESENT REPLACED OZONE AND RECIRCULATION FILTERS.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,752 hrs · 24,520 cycles

FLIGHT ATTENDANTS REPORTED ODORS IN TH ECABIN DURING DESCENT. EACH FA REPORTED A DIFFERENT ODOR. THE AIRCRAFT LANDED. RAN THE NR 1 & 2 ENGINES WITH BOTH PACKS SELECTED, FOUND NO ODORS. ISOLATED 1 AND 2 BLEEDS, NO ODORS AT THIS TIME. PERFORMED BORESCOPE OF THE NR 1 ENGINE HP STAGE NR 1 AND 2 BLADES, S1 AND S2. NO OIL WETTING NOTED. PERFORMED A BORESCOPE OF THE NR 2 ENGINE HP STAGE, NR 1 AND 2 BLADES, S1 AND S2. NO OIL WETTING NOTED.

Part: ENGINE — LEAKING (NR 1) · airframe 49,049 hrs · 24,179 cycles

ODOR OF OIL FUMES AT TOP OF CLIMB WITH POWER CHANGE. REMOVED AND REPLACED THE NR 1 ENGINE IAW CARDS MP71042-01 AND MP71042-02. ENGINE OPS CHECKED NORMAL. NO LEAKS, NO ODORS OR FUMES IN THE CABIN OR FLIGHT DECK.

Part: ENGINE — LEAKING (RIGHT) · airframe 48,790 hrs · 24,059 cycles

FUMES DURING CLIMBOUT AT 320 FULL POWER, BOTH PACKS ON. REMOVED AND REPLACED THE RT ENGINE.

Part: SEAL — LEAKING (APU OIL CAP) · airframe 48,512 hrs · 23,921 cycles

STRONG ODOR DURING DESCENT IN COCKPIT ONLY. FOUND APU OIL FILL CAP SEAL LEAKING. REPLACED THE CAP AND SEAL, LEAK AND OPS CHECKED IAW AMM 49-00-81-710-197-A. NO ODORS DETECTED.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 46,635 hrs · 23,021 cycles

LEFT EPSU BATTERY FAULT. REMOVED AND REPLACED THE EPSU BATTERY 11WL ON LEFT SIDE EMERGENCY EXIT. OPS CHECKED GOOD IAW AMM 33-51-38-000-002-A, AND AMM 33-51-38-400-002-A.

Part: CONNECTOR — DIRTY (NLG) · airframe 37,240 hrs · 18,523 cycles

DEFECTIVE ECAM IN FLIGHT LG DOORS NOT CLOSED, FOLLOWED BY LG SYS DISAGREE WITH RED NOSE GEAR LIGHT ON. CHECKED NLG PROX SENSOR IAW AMM 32-31-73-200-002-A, PERFORMED BITE OF LGCIU 1 & 2 IAW AMM 32-69-00-740-001-A. FOUND FAULTY NLG PROX SENSOR 19GA. INSPECTED & CLEANED ELEC CONNECTOR IAW AMM ESPM 20-55-00. PERFORMED BITE OF LGCIU 1 & 2, NO FAULTS PRESENT AT THIS TIME. ACFT OK FOR SERVICE.

Part: ACM — MALFUNCTIONED (NR 1) · airframe 30,478 hrs · 14,934 cycles

AFTER LANDING, CABIN FILLED WITH SMOKE, DUCT TEMPS INCREASED TO OVER 110 DEGREES. MX DETERMINED THE NR 1 PACK TO BE OVERHEATING. RAN NR 1 PACK FOR 45 MINTUES. OPS CHECKED GOOD REF AMM 21-61-00-710-001A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,788 hrs · 14,589 cycles

EMERGENCY LIGHT BATTERY 13WL FAILED TEST ON HEAVY SERVICE CHECK. R & R BATTERY PACK 13WL. REF AMM 33-51-39-000-005-A AND 33-51 -39-400-005A.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 26,570 hrs · 12,976 cycles

EMERGENCY LIGHT AT SEATS ROW 11 ABC INOPERATIVE. R & R LIGHT. OPS CHECKED GOOD. REF AMM 33-51-00-710-001.

Part: ACTUATOR — OUT OF RIG (RUDDER TRIM) · airframe 23,494 hrs · 11,455 cycles

ACFT FLEW AT 5 TO 10 DEGREE LT WING DOWN ON AP, FL CTL SHOWED LT AILERON UP. FUEL BALANCE OK. ACFT WANTED TO FLY IN LT SLIP. FOUND RUDDER TRIM TO BE OUT RIG. REMOVED RUDDER TRIM ACTUATOR, PERFORM ZEROING PROCEDURE ON ACTUATOR. ADJUST ARTIFICIAL FEEL SPRING ROD. REINSTALL RUDDER TRIM ACTUATOR. PERFORM OP'S TEST OF THE RUDDER TRIM ACTUATOR OP'S CHECK GOOD. NO PARTS WERE FOUND TO BE UNSERVICEABLE. RIG ONLY.

Part: TRANSMITTER — ERRATIC (ENGINE OIL) · airframe 22,823 hrs · 11,103 cycles

PILOT REPORT ERMENGENCY DECLARED. AIR TURN BACK, NR 1 ENGINE LOW OIL QUANTITY. PLACED NR 1 ENGINE OIL QUANTITY ON MEL 79-31-01A. R & R NR 1 ENGINE OIL QUANTITY TRANSMITTER. REF 79-31-15 PG BLOCK 401. OPS AND LEAK CHECK NORMAL.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED THE AFT CARGO RIGHT TRANSITION PROFILE HAS CORROSION ON FASTENER HOLE ONE INCH AFT OF FRAME 52. MAINTENANCE REMOVED AND REPLACED RIGHT TRANSITION PROFILE AT FRAME 52 TO FRAME 56 IAW SRM 51-42-11.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED THE FORWARD CARGO FLOOR PROFILE ON FRAME 28 HAS SURFACE CORROSION ON SEVERAL NUT PLATE HOLES AND SEVERAL DEFORMED HOLES. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: PANEL — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED THE FORWARD CARGO LEFT TRANSITION PANEL FROM FORWARD OF FRAME 25 TO FRAME 28 HAS CORROSION ON SEVERAL FASTENERS. MAINTENANCE REMOVED AND REPLACED LEFT PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION, NOTED FRAME 52 TO FRAME 56 LEFT TRANSITION PROFILE HAS CORROSION AND GOUGES ALONG ENTIRE LENGTH. MAINTENANCE INSTALLED NEW TRANSITION PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION ON PROFILE FRAME 61 STRINGER 38 RIGHT TO STRING 28 LEFT. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION, NOTED CORROSION ON FLOOR PROFILE AT FRAME 58 IN AFT PIT. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: FITTING — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION, NOTED CORROSION ON FITTING FORWARD OF FRAME 58. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-42-11 AND SRM 51-44-11.

Part: PLATE — CRACKED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION, NOTED FRAME 56 TRANSITION PANEL SUPPORT PLATE BETWEEN STRINGER 35 AND STRINGER 38 IS CRACKED OUT AT NUT PLATE HOLE. MAINTENANCE REMOVED AND REPLACED SUPPORT PLATE IAW SRM 51-42-11, SRM 51-44-11, SRM 51-46-11, SRM 51-23-11 AND AIRBUS DRAWING D53974846.

Part: SILL — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION ON FRAME 66 NEXT TO L2 DOOR FRAME. MAINTENANCE REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11, SRM 53-41-14, SRM 51-72-11 AND NTM 51-10-04-270-801-A-01.

Part: PROFILE — GOUGED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C-CHECK INSP NOTED AFT CARGO LT TRANSITION PROFILE FROM C59 TO C63 HAS A GOUGE 4 INCHED FWD OF FRAME C61 AND RIVET DISHED AND PULLING BETWEEN FRAME C62 AND FRAME C63. MX R & R PROFILE IAW SRM 51-42-11 PARAGRAPH 6B.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION ON CARGO NET TIE DOWN POINT. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSP NOTED FRAME 58 AND FRAME 59 CTR FLOORBEAM IN AFT CARGO PIT HAS CORROSION ON FWD MOST SCREW NUTPLATE HOLE. MX REMOVED FLOOR SUPPORT BEAM, FABRICATED NEW AND INSTALLED IAW DWG D53476573 AND SRM 51-42-11.

Part: FRAME — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSP NOTED THE FWD CARGO LT HAND TRANSITION PANEL FRAME 28 TO AFT BULKHEAD HAS CORROSION AT FASTNER HOLE 3 INCHES AFT OF FRAME 30. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO FRAME 56 TO FRAME 58 LEFT TRANSITION PROFILE HAS CORROSION IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11 AND SRM 51-75-12.

Part: SILL — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION WAS FOUND AT FRAME 66 NEXT TO R2 DOOR FRAME. MAINTENANCE REPAIRED IAW SRM 51-23-11, SRM 51-42-11, SRM 53-41-14, SRM 51-75-12, NTM 51-10-08-250-803-A-1, AIRBUS DRWAING D53472189 AND ENGINEERING AUTHORIZATION A9-53R-31671.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED CORROSION ON FLOOR PROFILE AT FRAME 57 IN AFT PIT. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11 AND AMM 25-55-41-400-001.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION, NOTED CORROSION ON FLOOR PROFILE AT FRAME 56 IN AFT PIT. MAINTENANCE REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.

Part: FITTING — CORRODED (GIRT BAR) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSP, NOTED L1 DOOR AFT GIRT BAR FITTING FASTENER HOLDER CORRODED AT FASTENER HOLES. MX REMOVED, FABRICATED NEW AND INSTALLED PLATE IAW DWG B2D53112534 AND SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (RIGHT) · airframe 208,884 hrs · 10,214 cycles

DURING C4/S1 C CHECK INSP NOTED THE RT AFT SHEAR PLATE FRAME 69 TO FRAME 70 CORRODED. MX REMOVED SHEAR PLATE, DRILLED UP NEW SHEAR PLATE, ASSEMBLED NEW SHEAR PLATE ON TO FRAME SUPPORT IAW SRM 51-42-11 AND SRM 51-44-11. SHEAR PLATE WILL BE INSTALLED IAW NON ROUTINE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C-CHECK INSP NOTED FRAME SUPPORT AT FRAME 69 TO FRAME 70 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED FRAME SUPPORT IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSP NOTED SEAT TRACK Y765 HAS CORROSION ON UPPER SURFACE LOCATED IN THE AREA OF FRAME 19. MX R & R FLOORBEAM IAW SRM 53-11-14, SRM 51-42-11 AND SRM 51-44-11

Part: SHEAR PLATE — CORRODED (LEFT) · airframe 20,884 hrs · 10,214 cycles

DURING C4/S1 C CHECK INSP NOTED THE LT AFT SHEAR PLATE FRAME 69 TO FRAME 70 CORRODED. MX R & R SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11, SRM 53-41-14, SRM 51-75-12, NTM 51-40-00-011-E AND EO A0-53EO-31434, STEP 7.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSPECTION NOTED FORWARD PIT FLOOR PANEL 131CG HAS CORROSION AND TWO BAD INSERTS. MAINTENANCE REMOVED AND REPLACED PANEL IAW AMM 53-22-14-400-001.

Part: HOOK — INOPERATIVE (L2 DOOR) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSP NOTED L2 DOOR OPEN/CLOSE INTERNAL HANDLE MOVES TO CLOSED POSITION BEFORE THE DOOR IS IN THE HOLE. MX R & R HOOK IAW AMM 52-11-21-400-001.

Part: HOOK — INOPERATIVE (L1 DOOR) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C-CHECK INSP NOTED L1 DOOR OPEN/CLOSE INTERNAL HANDLE MOVES TO THE CLOSED POSITION BEFORE THE DOOR IS IN THE HOLE. MX ADJUSTED THE UPLOCK HOOK ON THE L1 DOOR IAW AMM 52-11-21-400-001.

Part: HOOK — INOPERATIVE (R2 DOOR) · airframe 20,884 hrs · 10,214 cycles

DURING C4 S1 C CHECK INSP NOTED R2 DOOR OPEN/CLOSE INTERNAL HANDLE MOVES TO CLOSED POSITION BEFORE THE DOOR IS IN THE HOLE. MX ADJUSTED THE UPLOCK HOOK IAW AMM 52-11-21-400-001.

Part: PRESSURE VALVE — FAILED (NR 2 ENGINE) · airframe 16,659 hrs · 8,100 cycles

PILOT MADE AN AIR TURN BACK TO DEN DUE TO ENGINE NR 2 AIR BLEED FAULT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE PRESSURE REGULATOR VALVE ASSEMBLY IN ACCORDANCE WITH A319 AMM 36-11-52-400-042.

Part: PLACARD — CORRODED (R2 DOOR) · corrosion level 2 · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED R2 DOOR THRESHOLD SLIDE "ARMED" PLATE IS CORRODED ON THE BOTTOM. MAINTENANCE REMOVED AND REPLACED R2 DOOR THRESHOLD SLIDE "ARMED" PLATE IAW THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED LIGHT CORROSION AT NUT PLATE LOCATIONS ON LT TRANSITION PROFILE AT FRAME 26. MAINTENANCE BLENDED CORROSION AND UPSIZED HOLE TO .3400, WITH MAXIMUM MATERIAL REMOVED OF .012, IAW THE REQUIREMENTS OF A319 SRM 51-73-00. MAINTENANCE FABRICATED REPAIR DOUBLER (2024-T3 .040), TREATED, PRIMED AND PAINTED, AND INSTALLED DOUBLER IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A9-53R-30529. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL, 162CF, WAS PUNCTURED IN SEVERAL PLACES. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 162CF IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204. MAINT PREPARED AND PAINTED THE FLOOR PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT TRANSITION PANEL, 152AE, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152AE IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL, 152WG, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152WG IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — SCRATCHED (CARGO BAY) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT LOWER TRANSITION PANEL 131BF HAS DEEP SCRATCHES ALONG BOTTOM EDGE. MAINTENANCE REMOVED DAMAGED AREA AND CLEANED IAW THE REQUIREMENTS OF SRM 53-02-00 PAGE 214. MAINTENANCE FILLED DAMAGED AREA IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204 AND PAINTED TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED CORROSION AROUND THE NUT PLATE HOLE ON FLOORBEAM Y1292 AT FRAME 67, AND TOOLING MARK BETWEEN FRAME 67 AND 68 APPROXIMATELY 8 INCHES LONG. MAINTENANCE REMOVED AND REPLACED FLOORBEAM Y1292 BETWEEN FRAME 67 AND FRAME 68, IAW THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP NOTED THE AFT PIT FLOOR PANEL, 151VG, WAS DAMAGED. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 151VG IAW SRM 53-02-00 FIGURE 204. MAINT PAINTED THE FLOOR PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL, 152XG, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152XG IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSP NOTED 5 NUT CLIP HOLES CORRODED ON FLOORBEAM Y1292 (L-2) BETWEEN FRAME 66 AND FRAME 68. MAINT REMOVED ALL FASTENERS FROM THE FLOORBEAM, REMOVED DAMAGED FLOORBEAM, AND INSTALLED NEW FLOORBEAM AND FASTENERS IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL, 161CF WAS PUNCTURED. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 161CF IAW SRM 53-02-00 FIGURE 204. MAINT PREPARED AND PAINTED THE FLOOR PANEL 161CF IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: PROFILE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE TRANSITION PROFILE, LT SIDE BETWEEN FRAMES 28 AND 29 HAD CORROSION AT THE NUT PLATE LOCATIONS. MAINTENANCE REMOVED AND REPLACED TRANSITION PROFILE IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: PLATE — CORRODED (GIRT BAR) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED THE L2 FORWARD GIRT BAR BLANKING PLATE HAD CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED L2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE IAW THE REQUIREMENTS OF AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: BLANKING PLATE — CORRODED (GIRT BAR) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP NOTED THE L2 AFT GIRT BAR BLANKING PLATE HAD CORROSION. MAINT REMOVED AND REPLACED CORRODED L2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP, NOTED THE FLOOR PANEL 251LF NEEDED TOP LAYER OF COMPOSITE REPAIRED IN SEVERAL PLACES. MAINT REPAIRED FLOOR PANEL 251LF IAW SRM 53-02-00 PARAGRAPH 8.A FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: BLANKING PLATE — CORRODED (GIRT BAR) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP NOTED THE R2 FWD GIRT BAR BLANKING PLATE HAD CORROSION. MAINT REMOVED AND REPLACED CORRODED R2 DOOR FWD GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: BLANKING PLATE — CORRODED (GIRT BAR) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP NOTED THE R2 AFT GIRT BAR BLANKING PLATE HAD CORROSION. MAINT REMOVED AND REPLACED CORRODED R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,492 hrs · 7,491 cycles

DURING C-CHECK, INSP NOTED THE FLOOR PANEL 251FF NEEDED TOP LAYER OF COMPOSITE REPAIRED IN SEVERAL PLACES. MAINT REPAIRED FLOOR PANEL 251FF IAW SRM 53-02-00 FIGURE 212. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 15,492 hrs · 7,491 cycles

DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 242FF WAS DAMAGED IN SEVERAL PLACES. MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, PARAGRAPH 3, SOLUTION B, PAGE 245.

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 14,537 hrs · 7,020 cycles

DURING CLIMB-OUT, FLIGHT CREW REPORTED ECAM MESSAGE INDICATING RIGHT OVERWING EMERGENCY EXIT DOOR OPEN. FLIGHT CREW PERFORMED AIR TURNBACK AND EXECUTED UNEVENTFUL LANDING. MAINTENANCE TROUBLE SHOT SYSTEM AND FOUND DOOR PROXIMITY SWITCH OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED SWITCH IN ACCORDANCE WITH REQUIREMENTS OF AMM 52-71-13-820-050. UPON COMPLETION OF ADJUSTMENT, SYSTEM WAS OPERATIONS TESTED AND FOUND OKAY.

Part: BRAKE — INOPERATIVE (MLG) · airframe 11,903 hrs · 5,770 cycles

BLOCK TURN BACK, FLIGHT CREW REPORTED RT AFT BRAKE INOPERATIVE. SERVICED ALTERNATE BRAKE CONTROL RESERVOIR IAW AMM 32-43-00-011-051. SYSTEM CHECKED NORMAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 9,954 hrs · 4,825 cycles

AIR TURN BACK, BOTH FWD WINDSHIELDS CRACKED AT 20:00Z. ANTI-ICE LT AND RH WINDHIELDS. NO IMPACT ON WINDSHIELDS. OCCURRED ON CLIMB-OUT AT 7000 MSL. REPLACED BOTH NR 1 AND NR 2 WINDSHIELDS IAW AMM 56-11-11, PB401. PART NUMBERS AND SERIAL NUMBERS ARE AS FOLLOWS: NR 1 WINDSHIELD - P/N STA320-1-7-1A (MFG SULLY), S/N 56343; NR 2 WINDSHIELD, P/N NP165311-8 (MFG - PPG IND.), S/N 05028H8440.

Part: BLOWER — DAMAGED (AIR DISTRIBUTION) · airframe 9,932 hrs · 4,811 cycles

ON SHORT FINAL, FLIGHT CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE COCKPIT AND LOUD SOUND OF FAN POWERING DOWN ALONG WITH A VENT BLOWER FAULT LIGHT. PER TSM 24-00-00-810-823, IDENTIFIED AVIONICS BLOWER FAN AS SOURCE OF SMELL. REPLACED AVIONICS BLOWER FAN REF MM 21-26-51, PG 401. OPS CHECKED GOOD, VENT BLOWER FAULT CLEARED.

Part: SLIDE — NO TEST (R1 DOOR) · airframe 9,638 hrs · 4,670 cycles

DURING C-2 CHECK, INSPECTION REPORTED R1 DOOR SLIDE FAILED BITE TEST. REPLACED R1 DOOR SLIDE PER AMM 25-62-44-560-050 AND TASK CARD C528001-8.

Part: STARTER — BURNED (APU) · airframe 9,638 hrs · 4,670 cycles

DURING C-2 CHECK, INSPECTION REPORTED THE APU STARTER TERMINAL BLOCK AND RUBBER FOOT BURNED AND MELTED. WIRES GOING TO APU STARTER MOTOR BURNED AT TERMINAL LUGS. REPLACED APU STARTER PER SMM 49-42-51-000-004 AND 49-42-51-400-004. RE-TERMINATED POSITIVE WIRE WITH NEW TERMINAL PER AMM 20-48-11. TERMINATED SENSE WIRE TO APU STARTER PER AMM 49-42-01, PAGE 001, SHEET 1. CONNECTED WIRES AND INSTALLED NEW BOOT PER AMM 49-42-51-991-006, STEPS 4A (9)(10). PERFORMED FUNCTION CHECK OF THE STARTER MOTOR CLUTCH PER AMM 49-42-51-400-004, STEP 4B. PERFORMED OPS CHECK OF APU STARTER PER AMM 49-00-00-860-008.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 9,406 hrs · 4,553 cycles

DURING FLIGHT, THE GREEN HYDRAULIC SYSTEM STARTED LOOSING HYDRAULIC FLUID. UPON ARRIVAL IN DEN, MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING AND REPLACED THE PUMP. NO EMERGENCY ACTION WAS NEEDED BY THE FLIGHT CREW.

Part: LINE — CRACKED (APU) · airframe 8,350 hrs · 4,010 cycles

DURING START IN DCA, APU EXPERIENCED AN AUTO SHUTDOWN WITH SUBSEQUENT FIRE BOTTLE DISCHARGE. INSPECTED TAILCONE, APU AND ACCY COMPARTMENT IAW AMM 05-23-10-200-003. FOUND A CRACKED APU TURBINE BEARING RETURN LINE AND EVIDENCE OF FIRE IN THE APU ASSY. (APU IS A (RIVETED) TURBINE WHEEL). NO DAMAGE NOTED TO AIRCRAFT STRUCTURE. PLACARDED APU IAW MEL 49-10-01A. PLACARDED APU FIRE DET. EXT. SYSTEM IAW MEL 26-22-00A. PERFORMED RII INSPECTION AND AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT IS SCHEDULED FOR APU REPLACEMENT ON 8/31/06.