N948FR

Part: SEAT TRACK — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAMES 16-20, -Y1292, SEAT TRACK HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAME 68, Y1162, CORROSION AROUND FASTNERS. EVALUATED DAMAGE ON FLOORBEAM AND FOUND TO BE OUT OF REPAIRABLE LIMITS. REMOVED THE DAMAGED FLOORBEAM AND INSTALLED A NEW FLOORBEAM IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FLOORBEAM AT FRAME 66, Y1292, CORRODED. EVALUATED THE DAMAGE AND FOUND TO BE OUT OF REPAIRABLE LIMITS. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAME 16, Y254 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-11-911-001.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAME 66, R2 DOOR SILL SPLICE HAS AREAS OF CORROSION. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001, 53-41-14-283-002, AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAME 68, -Y1162 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 68 - 69 IAW SRM 53-00-14, AND 51-72-11-911-001.

Part: WEB — CORRODED (FRAME 16) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

WEB AT THE L1 DOOR, FRAME 16, Y1584 HAS AREA OF CORROSION. REMOVED AND REPLACED THE WEB IAW SRM 51-72-11-911-002.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FLOORBEAM AT FRAME 66, Y919 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAMES 16 - 20, -Y254 SEAT TRACK HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11, AND 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAMES 64 - 66, Y512 FLOOR SUPPORT HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: SUPPORT BEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAME 16, Y-81, GALLEY SUPPORT BEAM CORRODED. EVALUATED THE DAMAGED AND FOUND TO BE OUT OF REPAIRABLE LIMITS. REMOVED AND REPLACED THE BEAM IAW 51-72-11-911-001.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FR66 Y765 CORROSION AT TOOLING MARK AND CORROSION AT SPLICE. CORROSION REMOVAL OUT OF LIMITS ORIGINAL THICKNESS 0.100" MATERIAL LOSS .04" REMAINING .06" IAW SRM 53-00-14. REMOVED AND REPLACED BEAM IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FRAMES 66-68 -Y1292 FLOOR SUPPORT HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FLOOR SUPPORT AT FRAMES 66 - 68, Y1292 CORRODED AROUND FASTNER HOLES AT FRAME 68 AND AREA OF CORROSION AT FRAME 66. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: DOOR SILL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 42,530 hrs · 18,129 cycles

FORWARD CARGO DOOR SILL WEB HAS AREA OF CORROSION. EVALUATED THE DOOR SILL WEB AND FOUND IT TO BE OUT OF LIMITS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-44-11, AND 51-72-11-911-001.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 42,238 hrs · 17,996 cycles

EPSU 12WL BATTERY FAILED TEST. REMOVED & REPLACED EMERGENCY POWER BATTERY IAW AMM 33-51-38, PB 401. EPSU TESTED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 37,231 hrs · 15,903 cycles

REFERENCE LOG PAGE 989145. DURING INSPECTION IT WAS NOTED THAT EMER EXIT LIGHTS & SIGNS IN ARMED POSITION EPSU WOULD NOT TEST. R & R SWITCH EPSU IAW AMM 33-51-38 PB 401 OPERATIONAL CHECKED GOOD.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 36,873 hrs · 15,751 cycles

LOG PAGE 981218, AFTER TAKEOFF THE FLIGHT CREW NOTED SMOKE IN THE AFT CABIN. THE FLIGHT DECLARED AN EMER & RETURNED TO THE FIELD. FOUND THE NR 2 PACK INOPERATIVE. APPLIED MEL 21-52-01E CONTROL NR 1120060. R & R NR 2 ACM IAW AMM 21-52-21 PAGE BREAK 401. OPERATIONAL CHECKED GOOD. REMOVED MEL 21-52-01E.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,791 hrs · 13,959 cycles

EMERGENCY PATH LIGHT AT SEAT 4, FWD BULB INOPERATIVE. R & R THE BULB. OPERATIONS CHECK IS GOOD IAW AMM 33-51-18 PB 401 LP 885113-1.

Part: TUBE — LEAKING (HYDRAULIC SYS) · airframe 32,388 hrs · 13,795 cycles

LOG PAGE 864172 ITEM 1. HYD GREEN SYS LOW LEVEL & PRESS. FOUND NR 1 ENG HYD SWITCH TUBE LEAKING. R & R IAW AMM 29-11-49-000-005A & 29-11-49-400-005A. RAN NR 1 ENG WITH NO LEAKS NOTED. PUT LG BACK TO NORMAL MODE IAW AMM 32-00-00-860-003A.

Part: SLIDE RAFT — OUT OF RIG (L1 DOOR) · airframe 32,146 hrs · 13,692 cycles

DOOR L1 INTERMITTENT ARMED INDICATION ON STATUS PAGE. REMOVED & INSTALLED SERVICEABLE ESCAPE SLIDE RAFT PACK ASSEMBLY AT L1 DOOR IAW AMM 25-62-44 PAGE BLOCK 401. NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE. TORQUE WRENCH F9TAB1100C CALIBRATION DUE 10/20/2015.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,664 hrs · 13,473 cycles

EPSU BATTERY 10WL FAILED CAPACITY TEST. REFERENCE TASK CARD A332204-02. R & R BATTERY ASSEMBLY 10WL IAW AMM 33-1-39-000-005A & 33-51-39-400-005A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,664 hrs · 13,473 cycles

EPSU BATTERY 12WL FAILED CAPACITY TEST. REFERENCE TASK CARD A332204-02. R & R BATTERY ASSEMBLY 12WL IAW AMM 33-1-39-000·005A & 33-51-39-400·005A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,664 hrs · 13,473 cycles

EPSU BATTERY 11 WL FAILED CAPACITY TEST. REFERENCE TASK CARD A332204-02. R & R BATTERY ASSEMBLY 11 WL IAW AMM 33-1-39-000-005A & 33-51-39-400-005A.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 25,932 hrs · 10,909 cycles

ENG 1 N1 VIB 9.9, ATB AT 1845'Z, BIRD STRIKE ENG 1. R & R NR 1 ENG REF CARDS MP71042-01 & MP71042-02. OPS AND LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,030 hrs · 10,041 cycles

ERMENGENCY SEAT LIGHT AT 20ABC IS INOPERATIVE. REMOVED AND REPLACED SEAT 20ABC EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19 PB 401. OPS CHECKS GOOD.

Part: WARNING LIGHT — ILLUMINATED · airframe 23,583 hrs · 9,857 cycles

ECAM "F. USED / FOB DISAGREE" -ATB APPROXIMATELY 01308 - EMERGENCY DECLARED WITH AIR TURN BACK. TROUBLESHOT IAW REF TSM 28-LL-00-81O-805A. PERFORMED TEST 3B.

Part: SUPPORT — CRACKED (ZONE 100) · corrosion level 2 · airframe 22,769 hrs · 9,541 cycles

C-CHECK: RT LATERAL SHEAR PLATE AT FR 69-70 HAS A 2.2 INCH LONG CRACK THROUGHT AFT FASTENER. R & R AFT RT SHEAR PLATE BETWEEN FR 68-70. REF. EP A)-53EO-31434, SRM 51-44-11, SRM 51-42-11, PARA 6 & 7.

Part: SUPPORT — CRACKED (ZONE 100) · corrosion level 2 · airframe 22,769 hrs · 9,541 cycles

C-CHECK; RT LATERAL SHEAR PLATE AT FR 69-70 IS CRACKED. EO A0-53EO-31434 DATED 11-20-20-09. REQUIRES LT SHEAR PLATE TO BE REPLACED ALSO, WITH KIT, PN 53120D01R01. R & R AFT LT SHEAR PLATE BETWEEN FR 68-70. REF EO A0-53EO-31434, SRM 51-41-11, SRM 51-42-11 PARA 6 & 7.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,008 hrs · 7,965 cycles

C-CHECK: LT AT FRAME 66L AFT HAS 6 INCHES TO 6 INCHES OF FWD OF FRAME 68 FLOORBEAM, Y1292 HAS 8 SQ INCHES OF CORROSION ON UPPER AND LOWER SURFACE. CORROSION IS OUT OF LIMITS. REPLACED FLOORBEAM, Y1292 AT FRAME 66L IAW SRM 51-72-11, PARA 6.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 17,145 hrs · 7,321 cycles

C-CHECK: NON ROUTINE N0530; AFT CARGO FLOOR PANEL 151UG HAS 7 SQUARED INCHES OF COMPOSITE DAMAGE. FABRICATED REPLACEMENT PANEL IAW IRM 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · corrosion level 2 · airframe 17,145 hrs · 7,321 cycles

C-CHECK: AFT CARGO FLOOR PANEL 151CE IS DELAMINATED, 1 SQR FOOT. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G

Part: SPLICE PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,145 hrs · 7,321 cycles

C-CHECK: NON ROUTINE N0330; MAIN CABIN RT SIDE FWD OF FRAME 68 ON FLOORBEAM Y1292 SPLICE PLATE HAS 1 SQUARE INCH OF CORROSION. R & R UPPER SPLICE AT RT SIDE FWD OF FRAME 68, FLOORBEAM T1292 IAW SRM 51-42-11 PARA 7.

Part: SPLICE PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,145 hrs · 7,321 cycles

C-CHECK: NON ROUTINE N0378; MAIN CABIN LT SIDE FWD OF FRAME 68 ON FLOORBEAM Y11292 INBD UPPER SPLICE PLATE HAS 2 SQUARE INCHES OF CORROSION AROUND THE SCREW HOLES. R & R UPPER SPLICE AT LT SIDE FWD OF FRAME 68 FLOORBEAM Y1292 IAW SRM 51-42-11, PARA 7.

Part: CENTERING ROD — DEFECTIVE (ZONE 300) · airframe 17,145 hrs · 7,321 cycles

C-CHECK: NON ROUTINE N0344; CENTERING ROD SPRING IS LOOSE ON VERTICAL STABILIZER T/E. R & R CENTERING SPRING ROD IAW AMM 27-21-48-050AND AMM 27-21-48-420-050, OPS CHECK GOOD IAW AMM 27-24-00-710-050.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · corrosion level 2 · airframe 17,145 hrs · 7,321 cycles

C-CHECK: NON ROUTINE N0362; AFT CARGO FLOOR PANEL, 151PE HAS DELAMINATION AND COMPOSITE DAMAGE APPROX 200 SQUARE INCHES. FABRICATED REPLACEMENT PANEL IAW IRM 9701 REV G.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 28. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 26. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES.

Part: SKIN — DAMAGED (FUSLEAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 31. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE ON PRODUCTION SEAM FRAME 24, 3.5 INCHES BELOW STRINGER 7L. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 29. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 27. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,908 hrs · 3,553 cycles

MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, BETWEEN FRAME 27 AND FRAME 28, 1.5 INCHES. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 6,539 hrs · 2,914 cycles

DURING PREDEPARTURE CABIN CHECK THE FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 11 ABC WAS INOPERATIVE. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND WIRE 3351-1021 OPEN AT CONNECTOR AT 11WLA PIN F TO TERMINAL BLOCK 7725VT BLOCK 3. MAINTENANCE REPAIRED THE WIRE IN ACCORDANCE WITH ESPM 20-51-21. FOLLOWING COMPLETION OF THE REPAIR THE SYSTEM OPERATIONALLY CHECKED OKAY.

Part: SLIDE — DAMAGED (L2 DOOR) · airframe 5,804 hrs · 2,616 cycles

DURING C1 C CHECK, INSPECTION REPORTED THE L2 DOOR ESCAPE SLIDE HAD A WORN AREA ON THE GIRT PANEL. MAINTENANCE REMOVED THE GIRT BAR FROM THE DAMAGED PANEL AND INSTALLED THE GIRT BAR IN A NEW ESCAPE SLIDE ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-44-991-031. FOLLOWING INSTALLATION OF THE NEW ESCAPE SLIDE ASSEMBLY, THE INSTALLATION WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SLIDE — DAMAGED (R2 DOOR) · airframe 5,804 hrs · 2,616 cycles

DURING C1 C CHECK, INSPECTION REPORTED THE R2 DOOR EMERGENCY ESCAPE SLIDE HAD A WORN AREA ON THE GIRT PANEL. MAINTENANCE REMOVED THE GIRT BAR FROM THE DAMAGED PANEL AND INSTALLED THE GIRT BAR IN THE NEW ESCAPE SLIDE ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-44-991-031. FOLLOWING INSTALLATION OF THE NEW ESCAPE SLIDE ASSEMBLY, THE INSTALLATION WAS INSPECTED AND FOUND ACCEPTABLE.