N906FR

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 39,882 hrs · 19,385 cycles

LIGHT BATTERY 10WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY ASSY 10WL.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 39,882 hrs · 19,385 cycles

LIGHT BATTERY 12WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY ASSY 12WL.

Part: TRAY — CRACKED (ZONE 200) · airframe 37,916 hrs · 18,319 cycles

AFT WET AREA LT SHEAR PLATE TRAY CRACKED. R & R LT SHEAR PLATE TRAY IAW SRM 51-42-11, PARA 6 AND 7.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,916 hrs · 18,319 cycles

AFT CABIN FLOORBEAM AT L2 ENTRY AREA HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.

Part: PLATE — CRACKED (ZONE 200) · airframe 37,916 hrs · 18,319 cycles

LT LATERAL SHEAR PLATE CRACKED AFT OF FR69. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6 AND 10.

Part: PLATE — CRACKED (ZONE 200) · airframe 37,916 hrs · 18,319 cycles

RT LATERAL SHEAR PLATE CRACKED AFT OF FR 69. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6 AND 10.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,916 hrs · 18,319 cycles

MAIN CABIN SEAT TRACK Y-1292 HAS CORROSION BETWEEN FR17 - 18. R & R BEAM IAW SRM 51-42-11, PARA 5 AND 7.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,191 hrs · 17,934 cycles

DURING HEAVY CHECK FOUND SEAT 17 ABC EMERGENCY LIGHT INOPERATIVE. R & R SEAT 17 ABC EMERGENCY LIGHT IAW AMM 33-51 -19 PB 401. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,191 hrs · 17,934 cycles

DURING HEAVY CHECK FOUND SEAT 22 ABC EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51 -19, PB 401. OPS CHECKED GOOD.

Part: SOCKET — SMOKE (EMERGENCY LIGHT) · airframe 35,752 hrs · 17,190 cycles

A/C LP 686501; EMERGENCY EXIT LIGHT PATH 17C ILLUMINATED AND PRODUCED SMOKE AFTER POWER TRANSFER. NOTE; PASSENGER SMASHED LIGHT UNTIL IT QUIT SMOKING. R & R LIGHT ASSY, OPS CHECKED GOOD REF AMM 33-51-19 PB401. INSPECTED SEAT WIRING, NO FURTHER DAMAGED NOTED.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 32,956 hrs · 15,759 cycles

C-CHECK: NON ROUTINE NR 22652; NR 2 ENGINE HAS LIGHTNING STRIKE AT THE 4 O'CLOCK POSITION. REPAIRED NR 2 ENGINE OTBD THRUST REVERSER AT THE 4 O'CLOCK POSITION IAW CMM 54-30-00, REPAIR NR 13.

Part: CONNECTOR — COCKED (EMERGENCY LIGHTS) · airframe 29,306 hrs · 13,974 cycles

REF HEAVY MX NON ROUTINE N0674. OPS TEST OF EMERGENCY LIGHTS FAILS. FOUND CONNECTOR FOR EPSU 10WL COCKED. RESEATED CONNECTOR. PERFORMED OPS CHECK IAW AMM 33-51-00-710-050. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,306 hrs · 13,974 cycles

REF HEAVY MX NON-ROUTINE N0480. AFT CABIN RT FLOORBEAM -Y1292 FROM FRAME 66 TO FRAME 68 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 29,306 hrs · 13,974 cycles

REF HEAVY MX NON-ROUTINE N0476. AFT CABIN LT FLOORBEAM Y1292 FROM FRAME 66 TO FRAME 68 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,306 hrs · 13,974 cycles

REF HEAVY MX NON ROUTINE N0478. AFT CABIN RT FLOORBEAM -Y765 FROM FRAME 67 TO FRAME 70 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,306 hrs · 13,974 cycles

REF HEAVY MX NON ROUTINE N0477. AFT CABIN LT FLOORBEAM Y1292 FROM FRAME 68 TO FRAME 69 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 29,306 hrs · 13,974 cycles

REF HEAVY MX NON ROUTINE N0479. AFT CABIN RIGHT HAND FLOORBEAM -Y1293 FROM FRAME 68 TO FRAME 69 TOP SURFACE HAS CORROSION. R & R FLOORBEAM REF A319 AMM 51-72-11.

Part: PROXIMITY SENSOR — INOPERATIVE (RT OVRWG SLIDE) · airframe 28,684 hrs · 13,675 cycles

REF LOG PAGE NRS 537910 AND 537923. CAPTAIN NOTED RT OVERWING EXIT SLIDE NOT SHOWING ARMED. MX ISSUED MEL 25-60-04C, CONTROL NR 1074315, TO THE RT OVERWING SLIDE, REF LOG PAGE NR 537910. MX R & R PROXIMITY DETECTOR IAW AMM 52-73-11-400-004A. OPS CHECK GOOD, REF LOG PAGE NR 537923.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 28,618 hrs · 13,648 cycles

FLIGHT CREW NOTED GREEN RESERVOIR HYD PUMP LOW PRESSURE ECAM MESSAGE. AN EMERGENCY WAS DECLARED AND FLIGHT DIVERTED. MX AND INSP NOTED THE LT MLG DOOR ACTUATOR HYD LINE LEAKING. MX R & R LT MLG DOOR ACTUATOR HYD LINE IAW AMM 32-31-39, PB 401 AND SERVICED THE HYD SYS IAW AMM 12-12-29-611-00. OPS AND LEAK CHECKS NORMAL IAW AMM 32-31-00-710-002 AND AMM 29-11-00-710-001.

Part: STRUT — CORRODED (MLG) · airframe 26,879 hrs · 12,824 cycles

LINE MX PERFORMED THE LT MLG STRUT REPACK AND FOUND CORROSION ON THE MAIN FITTING BORE WHERE THE LWR BRG IS INSTALLED. MX REMOVED THE CORROSION, PERFORMED NDT OF AREA, FLAP PEENED AREA, CADMIUM PLATED AREA, APPLIED PRIMER TO AREA AND REASSEMBLED STRUT. REF EA A9-32R-31378.

Part: HEAT EXCHANGER — ODOR (ZONE 100) · airframe 23,546 hrs · 11,122 cycles

FLIGHT CREW MADE AN UNSCHEDULED LANDING DUE TO A STRONG ELECTRICAL SMELL THROUGHOUT THE AIRCRAFT CABIN ON CLIMB-OUT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THAT ALL AIRCRAFT BAY HEAT EXCHANGERS WERE REPLACED THE NIGHT BEFORE DURING SCHEDULED OVERNIGHT MAINTENANCE, WITHOUT SUFFICIENT RUN TIME. CABIN FILTERS WERE REMOVED AND REPLACED IN ACCORDANCE WITH ATSM 21-00-00810-802 AND SIL 21-132. APU BLEED AND ENGINE BLEED SYSTEMS RAN UNTIL SMELL DECREASED IN ACCORDANCE WITH AMM 21-21-41-PB401.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,373 hrs · 10,017 cycles

DURING THE CABIN CHECK, THE INSPECTION DISCLOSED EMERGENCY LIGHTS WERE NOT FUNCTIONING ON TWO ROWS (ROWS 8 AND 15). MAINTENANCE REPLACED THE EMERGENCY LIGHTS ON THE TWO MALFUNCTIONING ROWS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-19 PB 401. UPON COOMPLETION OF THE INSTALLATION THE LIGHTS WERE TESTED AND FOUND ACCEPTABLE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 19,831 hrs · 9,278 cycles

INSPECTION REPORTED SEAT ROW 9ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED WIRE HARNESS AT SEAT ROW 9ABC IAW ESPM 20-33-00. PERFORMED OPERATIONAL TEST ON EMERGENCY LIGHTS IAW AMM 33-51-00-710-007. OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FWD LEFT AND AFT LEFT EPSU BATTERIES FAILED CAPACITY CHECK. REPLACED EMERGENCY ESCAPE PATH LIGHT BATTERY PACKS, FWD, AFT, MID L AND MID R. OPS CHECKS NORMAL IAW AMM 33-51-38-00-002 AND 33-51-38-400-002.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SEAT EMERGENCY LIGHT AT ROW 21 INOP. REPINNED WIRE HARNESS ASSY 350WL10 UNDER ROW 21 IAW ASM 33-51-00, SCH 04, P101, SHEET 3. OPS CHECKED GOOD IAW AMM 33-51-00-710-008.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED BULBS INOP IN ROW 4 AND 6 ABC SEAT FLOOR PATH LIGHTING. RELAMPED ROW 4 AND 6 ABC SEAT FLOOR PATH LIGHTS. OPS CHECK NORMAL IAW A319 AMM 33-51-00-710-007.

Part: FIRE DETECTOR — NO TEST (CARGO BAY) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DETECTORS (2) FAILED TEST. REPLACED AFT CARGO COMPARTMENT FIRE DETECTORS (5WH AND 6WH). PERFORMED OPS TEST OF CARGO SMOKE DETECTORS IAW A319 AMM 26-16-15-000-001.

Part: BUSHING — WORN (E/E BAY DOORWAY) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FRETTING ON C-16 CROSSBEAM, DOOR ACCESS 812 (LT AVIONICS DOOR). REMOVED BOLT. FOUND WEAR ON THE BUSHING. CLEANED AREA IAW A319111 SRM 51-42-11, DRAWING D53913231. REASSEMBLED WITH NEW BUSHING IAW A319111 AMM 20-21-11-991-003.

Part: MOUNT — CHAFED (BATTERY RACK) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FRETTING ON BATTERY RACK MOUNTS. REPLACED (4) MOUNT FITTINGS AT FR 10 IAW EA NR A9-53R-10649.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND FASTENER HOLES WHERE FLOORBEAM Y1292 ATTACHES TO FR68. REMOVED AND REPLACED FLOORBEAM ASSY. IAW A319 SRM 51-42-11.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C-4/S-1 CHECK, INSPECTION REPORTED BRACKET FOR ANTENNA CORRODED IN AFT PIT UNDER FLOOR PANEL 151VG, AT APPROX STR 43, BETWEEN FR 58 AND FR 59. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET IAW A319 SRM 51-42-11, PARA 6 D AND FIG 8; 51-31-00, TABLE 4; 51-70-12, PARA 1E, TABLES 3 AND 4; 51-21-11, PARA 1B; 51-75-12, PARA. 4; 51-42-11, PARA. 6; AND AIRBUS DRAWING D53910479.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED WEB PLATE SUPPORT UNDER SHEAR PLATE BETWEEN FR 69 AND FR 70 JUST BEHIND FLOORBEAM -Y1292 SUPPORT FRAME CORRODED. FOUND WEB PLATE SUPPORT TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, FIG 101. REMOVED AND REPLACED SHEAR PLATE AND SUPPORT FRAME BETWEEN FR 69 AND FR 70 BEHIND FLOORBEAM -1292 IAW A319 SRM 51-42-11, FIG 9, 12, 40, 43, TABLE 22 AND 25.

Part: BEAM — BENT (BULKHEAD) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD BULKHEAD BEAM RT OF CENTER BENT. REPLACED BULKHEAD BEAM IAW A319 SRM 51-42-11, PARA. 5, PG 6-7 AND PARA 6, PG 22-23, AND SRM 51-44-21.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT FRAME (SHEAR PLATE) BETWEEN FR69 AND FR70, JUST BEHIND FLOORBEAM -Y1292 CORRODED. FOUND SHEAR PLATE TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED SHEAR PLATE IAW A319 SRM 51-42-11, FIG 8. LOCATED AND DRILLED HOLES INTO THE NEW SHEAR PLATE IAW A319 SRM 51-72-11. INSTALLED NEW SHEAR PLATE AND SUPPORT FRAME BETWEEN FR69 AND FR70 IAW A319 SRM 51-42-11, FIG 9, 12, 40 AND 43, TABLE 22 AND 25.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 68 AND FR 69 AT Y1292. FLOORBEAM FOUND TO BE OUT OF LIMITS PER A319 ARM 51-00-14, FIG 101. REPLACED FLOORBEAM IAW A319 SRM 51-42-11 AND SRM 51-44-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT SUPPORT FRAME CORRODED BETWEEN FR 69 AND FR 70, JUST BEHIND FLOORBEAM -Y1292. FOUND SUPPORT FRAME TO BE OUT OF LIMITS IAW A319 SRM 51-74-00. REMOVED AND REPLACED SUPPORT FRAME IAW A319 SRM 51-72-11, PAGES 1 AND 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLE ON FLOORBEAM BETWEEN FR 66AND FR 68 AT Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW A319 SRM 51-00-14, FIG 8. REPLACED FLOORBEAM IAW A319 SRM 51-44-11 3B AND 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLE AT FR 66 ON FLOORBEAM BETWEEN FR 66 AND FR 64 AT Y1292. REMOVED AND REPLACED FLOORBEAM ASSY IAW A319 SRM 51-42-11.

Part: SHEAR TIE — SHEARED · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE SHEARED BETWEEN FR 68 AND FR 69, JUST OTBD OF FLOORBEAM -Y1292. REMOVED AND INSTALLED SHEAR PLATE IAW A319 SRM 53-41-14, FIG 18, 51-42-11, 51-20-00, PARA 3, AND 51-23-11.

Part: SILL — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED NUT CLIP AREA CORRODED ON FLOORBEAM -Y1732 AT FR 66, FWD OF R-2 DOOR FRAME. REMOVED AND REPLACED R-2 DOOR SILL IAW A319 SRM 51-42-11; 51-42-11, FIG 8; 51-42-11, PARA. 6; 51-21-11; 51-75-12; 51-12-11; 51-45-11, FIG 8; AND 51-42-11, 7B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 67 AND FR 68 AT-Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS PER A319 SRM 51-00-14, FIG 101. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT SHEAR PLATE CORRODED BETWEEN FR 69 AND FR 70, JUST BEHIND FLOORBEAM Y1292. REMOVED AND REPLACED SHEAR PLATE SUPPORT FRAME AND SHEAR PLATE IAW A319 SRM 51-42-11, FIG. 8; 51-44-11, TABLE 3; 51-72-11, PARA. 5.A.; 51-42-00, PARA. 6,7,10; AND AIRBUS DRAWING D53474180, ISSUE G.

Part: BUSHING — BROKEN (SEAT TRACK) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RT SIDE FLOOR EXPANSION JOINT AT FRAME 35 HAD BROKEN BUSHING ON BOTH SEAT TRACK BEAMS. REMOVED AND REPLACED PLASTIC BUSHINGS ON BOTH RT SEAT TRACKS EXPANSION JOINTS AT FS 35 IAW A319 SRM 51-42-11, PARA 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LIGHT CORROSION AROUND NUT PLATE HOLE ON SEAT TRACK AT -Y1292, FR65. REMOVED AND INSTALLED FLOORBEAM IAW A319 SRM 51-42-11; 51-42-11, FIG 8; 51-42-11, PARA 7; AND 51-42-11, STEP 7 B.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED NUT CLIP AREA CORRODED ON FLOORBEAM Y1732 AT FR 66, FWD OF L-2 DOOR FRAME. REMOVED FASTENERS FROM L-2 DOOR SILL IAW A319 SRM 51-42-11, PARA. 5. REPLACED L2 DOOR SILL IAW A319 SRM 51-42-11, SRM 51-75-12, SRM 51-44-11, AND AMM 51-78-00-615-005.

Part: ATTACH FITTING — CORRODED (NLG) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED INTERNAL CASTING AND THROUGH PIN BUSHING ON NLG UPPER TORSION LINK LUG CORRODED. REMOVED CORROSION AT UPPER TORSION LINK. TREATED, CAD PLATED AND REINSTALLED BUSHINGS IAW EA A9-32R-11842.

Part: BUSHING — BROKEN (SEAT TRACK) · airframe 17,895 hrs · 8,332 cycles

DURING C-4/S1 CHECK, INSPECTION REPORTED LT SIDE FLOOR EXPANSION JOINT AT FRAME 35 HAD BROKEN BUSHING ON BOTH SEAT TRACK BEAMS. REPLACED BOLTS AND BUSHINGS IN THE EXPANSION JOINTS AT FS 35 ON THE LT SIDE SEAT TRACKS IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR68 AND FR69 AT -Y1162. FOUND TO BE OUT LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED AND INSTALLED FLOORBEAM ASSY IAW A319 SRM 51-42-11.

Part: SHEAR TIE — SHEARED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE WAS SHEARED BETWEEN FR 68 AND FR 69 JUST OTBD OF FLOORBEAM Y1292. FABRICATED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11, FIG 7 AND 8; 53-41-14, FIG 18; 51-42-11; AND 51-20-00, PARA. 3; 51-23-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L2 SILL PLATE UPPER SPLICE ANGLE FWD OF FR 66 AT Y1732, INBD SIDE, CORRODED. INSTALLED REPLACEMENT SPLICE ANGLE IAW A319 SRM 51-42-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT LAV D FWD WALL CORRODED AT OTBD ANCHOR POINT. REMOVED AND CLEANED FITTING AND REINSTALLED WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 305, 618 AND 740.

Part: FITTING — CORRODED · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED LT AFT LAV D, AFT WALL INBD ANCHOR POINT CORRODED. REMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740.

Part: FITTING — CORRODED (LAVATORY) · airframe 17,895 hrs · 8,332 cycles

DURING C-4/S-1, INSPECTION REPORTED LT AFT LAV D AFT WALL CORRODED AT OTBD POINT. REMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740.

Part: FLOORBOARD — CORRODED (CABIN) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED RUST BUILD-UP IN AFT OB MOUNTING HOLE IN FLOORBOARD, AFT LT LAVATORY. INSTALLED NEW BUSHING AND PACKING IN FLOORBOARD UNDER LAV D AFT OB MOUNT IAW A319 AMM 25-43-41-400-001.

Part: FITTING — CORRODED (LAVATORY) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT LT LAVATORY, AFT OTBD MOUNTING HOLES IN LAV WALL WORN AND CORRODED. REMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740.

Part: FITTING — CORRODED (FUSELAGE) · airframe 17,895 hrs · 8,332 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED AFT LT LAV, AFT INBD MOUNTING HOLES IN LAV WALL WORN, ELONGATED AND CORRODED. REMOVED AND CLEANED FITTING. REINSTALLED FITTING WITH NEW HARDWARE IAW CMM 25-43-51, PAGES 303, 618 AND 740.

Part: RELAY — FAILED (CABIN) · airframe 15,825 hrs · 7,314 cycles

RE-ISSUED. FLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED IN-FLIGHT FOR UNKNOWN REASON. TROUBLESHOT SYSTEM PER TSM 335100810819. REPLACED RELAY 8WL/108VU CTL PWR SUPPLY. PERFORMED EMERGENCY LIGHTING OPS TEST PER AMM 33-51-00-710-001. TESTED NORMAL.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 13,187 hrs · 6,012 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR PANEL 261FF. REMOVED SURFACE CORROSION FROM FLOOR PANEL 261FF. REPAIRED FLOOR PANEL PER SRM 53-02-00 FIG 202.

Part: ADC — INOPERATIVE · airframe 8,468 hrs · 3,744 cycles

ABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FIRST OFFICER'S AIRSPEED WAS 110 KIAS. BRAKE TEMP ACHIEVED 550 DEG. TROUBLESHOT LACK OF AIRSPEED INDICATION. PERFORMED EFCS GND SCAN IAW AMM 27-96-00-740-001 AND IRU-1 GND SCAN IAW 34-13-00-740-003, INCLUDING BITE TESTS/DYNAMIC SLEW OF ADIRU-1. REPLACED ADC 19FP1 IAW AMM 34-11-17, PAGE 401. ADM LEAK CHECK GOOD. INSPECTED BRAKES IAW AMM 05-51-16-PB601. NO DEFECTS NOTED.

Part: PROBE — INOPERATIVE (PITOT SYSTEM) · airframe 8,468 hrs · 3,744 cycles

ABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FO'S AIRSPEED WAS 80 KTS. FOUND CAPTAIN'S PITOT PROBE 9DA1 BAD. REPLACED PITOT PROBE IAW AMM 34-11-15-400-001. PERFORMED OPS AND LEAK CHECK AND AIRSPEED INDICATION TESTED NORMAL.

Part: ODOR — DETECTED (CABIN) · airframe 8,253 hrs · 3,646 cycles

BLOCK TURN BACK. FLIGHT CREW REPORTED ODOR OF SMOKE IN THE CABIN NEAR ROW 20. INVESTIGATED CABIN FOR SMOKE ODOR, OPERATED BOTH ENGINES AND AIR CONDITIONING SYSTEM. INSPECTED ALL LAVATORIES AND CARGO BAYS. NO SMOKE ODOR NOTED, NO FAULTS NOTED. INSPECTED AVIONICS BAYS, NO SMOKE ODOR NOTED. INTERVIEWED SEVERAL PASSENGERS AT ROW 20. PASSENGERS STATED THEY DID NOT ODOR SMOKE. COMPLETED TASK 26-15-00-810-804. RELEASED AIRCRAFT FOR SERVICE.