N919FR

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 46,477 hrs · 22,703 cycles

DURING ROUTINE HEAVY SERVICE CHECK, R-2 DOOR FAILED EMERGENCY LIGHTING TEST. R & R R-2 DOOR SLIDE REF TC25831-02. TESTED EMERGENCY LIGHT IAW WORK CARD. OPS CHECK GOOD, END.

Part: SLIDE RAFT — FAILED (R1 DOOR) · airframe 46,477 hrs · 22,703 cycles

REF LOG PAGE 1001551: DURING ROUTINE HEAVY SERVICE CHECK, R-1 DOOR FAILED EMERGENCY LIGHTING TEST. R & R R-1 DOOR SLIDE REF TC25831-02. TESTED EMERGENCY LIGHT TEST IAW WORK CARD, OPS CHECK GOOD, END.

Part: LIGHT — NO TEST (L1 DOOR SLIDE) · airframe 46,477 hrs · 22,703 cycles

DURING ROUTINE HEAVY SERVICE CHECK, THE L1 DOOR FAILED THE EMERGENCY LIGHT TEST. REMOVED AND REPLACED L1 DOOR SLIDE IAW TC25831-02. TESTED EMERGENCY LIGHTS IAW WORK CARD, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,761 hrs · 19,989 cycles

EPSU BATTERY AFT LT 13 WL, FAILED BATTERY TEST AT SCHEDULED HEAVY SERVICE CHECK. R & R THE EPSU BATTERY AT 13WL IAW AMM 33-51-38-000-002A & 33-51-38-400-002A.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 26,620 hrs · 21,958 cycles

BULKHEAD WEB CORRODED AT BS 280.

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 38,965 hrs · 19,089 cycles

LEFT ELEVATOR UPPER SURFACE INDICATION IS IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR IAW SRM 55-21-11 PB 201. WORK ACCOMPLISHED ON NR 40656 WORK ORDER 1162 C8 S2 CHECK.

Part: PLATE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 38,965 hrs · 19,089 cycles

AIRCRAFT DUE C8 S2 INSPECTION. FLOOR TO FUSELAGE PLATE TRAY AFT OF FRAME 68 CRACKED LT Y1292. R & R SHEAR PLATE TRAY AFT OF FRAME 68 IAW SRM 51-42-11 PAR 6 1-8 PART 7 B 1 A-D, PAR 13 D 1-4. ACFT DUE OUT OF C CHECK 9/16/2014.

Part: PLATE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 38,965 hrs · 19,089 cycles

AIRCRAFT DUE C8 S2 INSPECTION. FLOOR TO FUSELAGE PLATE TRAY AFT OF FRAME 68 CRACKED RT Y-1292. R & R SHEAR PLATE TRAY AFT OF FRAME 68 IAW SRM 51-42-11 PAR 6 1 -8 PAR 7 B 1 A-D, PAR 13 D 1-4. ACFT DUE OUT OF C CHECK 9/16/2014.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,965 hrs · 19,089 cycles

AIRCRAFT DUE C8 S2 INSPECTION. AFT CABIN FLOORBEAM Y-1292 BETWEEN FRAME 66 TO 68 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-44-11 & 51-42-11. ACFT DUE OUT OF C CHECK 9/16/2014.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,965 hrs · 19,089 cycles

AIRCRAFT DUE C8 S2 CHECK. FWD CABIN FLOORBEAM BETWEEN FRAME 16 - 18 Y1292 CORRODED TO 50% OF MATERIAL THICKNESS, OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-42-11 PAR 5 A-D. ACFT DUE OUT OF C CHECK SEPTEMBER 16, 2014.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,965 hrs · 19,089 cycles

AIRCRAFT DUE C8 S2 INSPECTION. AFT CABIN FLOORBEAM Y1292 BETWEEN FRAME 66 - 68 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS. R & R FLOOR BEAM IAW SRM 51-44-11 & 51-42-11. ACFT DUE OUT OF C CHECK 9/16/2014.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 36,160 hrs · 17,586 cycles

HYD YELLOW LOW PRESSURE. R & R CRACKED HCU LINE FROM TRSOV. NO LEAKAGE NOTED REF AMM 29-13-19-400-049.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,968 hrs · 15,910 cycles

DURING THE HEAVEY SERVICE CHECK, THE BATTERY FAILED THE EMERGECY LIGHT TEST. R & R THE 13WL IAW AMM 33-51-38 PB401.

Part: WARNING LIGHT — FALSE ACTIVATION (L2 DOOR) · airframe 32,013 hrs · 15,399 cycles

DOOR L2 DISARMED DURING FLIGHT CONFIRMED DOOR DISARMED ON EWD DOOR PAGE FLASHING RED LIGHT ON F/A PANEL, INSPECTED AND OPERATED DOOR AND SLIDE ARMED & DISARMED, NO FAULTS NOTED. INTERROGATED CIDS 1 AND 2, NO FAULTS. PERFORMED GROUND SCAN CIDS 1 AND 2, NO FAULTS. PERFORMED OPS CHECK OF DOOR WARNING SYS IAW AMM 52-30-00-860-001. NO FAULTS NOTED. OK FOR SERVICE.

Part: BULB — BURNED OUT (SLIDE INDICATOR) · airframe 30,506 hrs · 14,635 cycles

C-CHECK: L2 DOOR FAILED TASK CARD C522101-02 PARA 4 A, STEP 2. SLIDE ARMED INDICATOR LIGHT ON DOOR DID NOT ILLUMINATE. RELAMPED INDICATOR. OPS CHECKED GOOD LAW AMM 52-73-00-710-001.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 29,742 hrs · 14,247 cycles

DURING TEST EPSU BATTERY FORWARD LT FAILED. REPLACED LT FORWARD EMERGENCY EPSU BATTERY PACK IAW AMM 33-51-38-400-002, CHECKS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 21,127 hrs · 10,081 cycles

DURING HEAVY CHECK, INSPECTION NOTED THE EMERGENCY ESCAPE PATH LIGHT WAS BROKEN AND INOPERATIVE AT SEAT ROW 13ABC. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AND PERFORMED OPERATIONAL TEST, REFERENCE AMM 33-51-19-400-002 AND 33-51-19-000-002.

Part: LIGHT — BROKEN (CABIN) · airframe 21,127 hrs · 10,081 cycles

DURING HEAVY CHECK, INSPECTION NOTED THE EMERGENCY ESCAPE PATH LIGHT WAS BROKEN AND INOPERATIVE AT SEAT ROW 12ABC. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AND PERFORMED OPERATIONAL TEST, REFERENCE AMM 33-51-19-400-002 AND 33-51-19-000-002.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

REFERENCE NON ROUTINE 2008-196522. DURING C4/S1 C CHECK, INSPECTION NOTED FLOOR PANEL 151VG HAD PERFORATION DAMAGE. MX REPAIRED FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

REFERENCE NON ROUTINE 2008-196216. DURING C4/S1 C CHECK, INSPECTION NOTED DENT ON FUSELAGE SKIN AT FRAME 63 + 9 INCHES AND LT STRINGER 43 + 1 INCH. MX REPAIRED DENT ON EXTERNAL SKIN AT FRAME 63 + 9 INCHES BETWEEN LT STRINGER 41 AND RT STRINGER 43, IAW THE REQUIREMENTS OF A319 SRM 53-00-11, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SKIN — DENTED (L/E SLAT) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED DENT ON TOP SKIN OF LT SLAT NR 3 BETWEEN RIB 3 AND 4. MX REPAIRED THE DENT IAW THE REQUIREMENTS OF A319 SRM 57-40-00, FIGURE 224. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 222FF, FWD GALLEY AREA. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-12-12-000-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 221FF, FWD GALLEY AREA. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-12-12-000-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON SHEAR PLATE LOCATED AT FRAME 69 TO FRAME 70 ON THE RIGHT SIDE OF THE PASSENGER CABIN. MX REMOVED AND REPLACED THE SHEAR PLATE IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED DELAMINATION ON FLOOR PANEL 162EF IN THE AFT CARGO COMPARTMENT. MX REMOVED AND REPLACED THE FLOO PANLE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, TABLE 105. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1732 AT FRAME 66. MX REPAIRED FLOORBEAM Y1732 AT FRAME 66 IAW THE REQUIREMENTS OF A319 SRM 53-41-14, FIGURE 201. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED DELAMINATION ON FLOOR PANEL 151DE. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y765 AT FRAME 67+10 INCHES. MX REMOVED AND REPLACED FLOORBEAM AT FRAME 67 IAW THE REQUIREMENTS OF A319 SRM 51-72-11, PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131CG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 151TG WAS DAMAGED. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED DELAMINATION ON FLOOR PANEL 151TG. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1292 AT FRAME 68. MX REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 68 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y765 AT FRAME 66+3 INCHES. MX REMOVED AND REPLACED FLOORBEAM Y765 FROM FRAME 64 TO FRAME 66+6 IAW THE REQUIREMENTS OF A319 SRM 51-72-11, PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y765 AT FRAME 68. MX REMOVED AND REPLACED FLOORBEAM AT FRAME 66 TO FRAME 70 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1292 AT FRAME 68 TO FRAME 69. MX REMOVED AND REPLACED FLOORBEAM AT FRAME 68 TO FRAME 69 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN LOWER SILL LOCATED AT LT FRAME 67+17 INCHES AND FRAME 68. MX PERFORMED STRUCTURAL REPAIR IAW THE REQUIREMENTS OF A319 SRM 53-41-14, FIGURE 201. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1292 AT FRAME 66. MX REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 64 TO FRAME 66 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 132EG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131DG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 132DG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED PERFORATION ON FLOOR PANEL 151VG IN THE AFT CARGO COMPARTMENT. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 151AE WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SKIN — BURNED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

REFERENCE NON ROUTINE 2008-196727. DURING C4/S1 C-CHECK, INSPECTION NOTED LIGHTNING STRIKE DAMAGE ON EXTERNAL SKIN LOCATED AT FRAME 1 + 8 INCHES, RT HAND SIDE UPPER FUSELAGE AT VERTICAL REFERENCE AXIS Z O. MX PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-11-11, FIGURE 209. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PERFORATED (FUSELAGE) · airframe 19,348 hrs · 9,194 cycles

DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131EG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00,PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: DEU — INOPERATIVE (CABIN LIGHTS) · airframe 18,753 hrs · 8,875 cycles

DURING FLIGHT MANY CABIN LIGHTS WERE COMING ON AND OFF ON AC RT. THE F/A NOTICED A BURNING SMELL OVER ROWS 16,17 AND 18 ON AC RT. MAINT FOUND DEU-A 200RH12 INOPERATIVE AND HAD A SMELL TO IT. MAINT REMOVED AND REPLACED DEU-A 200RH12 IAW AMM 23-73-46 AND OPS CHECKED NORMAL AND THE AC WAS RETURNED TO SERVICE. (B)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,571 hrs · 8,773 cycles

DURING WALK AROUND MAINT, NOTED LT FUSELAGE GOUGED AND DAMAGED FRAME 57 TO FRAME 58 AND STRINGER 30 LT TO STRINGER 31 LT. MAINT PERFORMED A PERMANENT REPAIR IAW SRM 53-00-11 FIGURE 203 AND E.A. A9-53R-30409. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: DEU — ODOR (CABIN LIGHTS) · airframe 18,450 hrs · 8,712 cycles

DURING FLIGHT, THE FLIGHT CREW NOTICED MANY CABIN LIGHTS ON THE RT SIDE OF THE AC COMING ON AND OFF. THE F/A ALSO NOTICED A BURNING ODOR OVER SEAT ROWS 16 TO 18 ON AC RT. MAINT REMOVED AND REPLACED 200RH 12 DEU-A IAW AMM 23-73-46 PAGE BREAK 401 AND OPERATIONAL CHECKED GOOD. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 13,591 hrs · 6,400 cycles

DURING C-3 CHECK, INSPECTION REPORTED FWD CARGO PIT FLOOR COVER SHEET CORRODED AROUND SEVERAL HOLES, AFT COVER SHEET NR 131CG. FOUND CORROSION IN FWD PIT AT Y692 TRANSITION SUPPORT PLATE RUNNING FROM FR 28 TO FR 34 AT THE FASTENER HOLES. FABRICATED AND INSTALLED TRANSITION PLATE AND COVER SHEET IAW A319 SRM 51-42-11.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,591 hrs · 6,400 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION FOUND UNDER NUT CLIPS LT BEAM Y1292 BETWEEN CROSSBEAMS FR67 AND FR68 PROFILE 195. REPLACED BEAM IAW SRM 51-42-11 AND SRM 53-41-14.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,591 hrs · 6,400 cycles

DURING C-3 CHECK, INSPECTION REPORTED CORROSION FOUND UNDER NUT CLIPS LT BEAM Y1292 BETWEEN CROSS BEAMS FR 58 AND FR 69 PROFILE 80. BURNISHED SURFACE CORROSION AND OVERSIZED HOLES TO REMOVE CORROSION IAW SRM 51-22-00, PAGE 11, AND EA A9-53R-11805.