N925FR

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,347 hrs · 16,385 cycles

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

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 31,671 hrs · 15,495 cycles

AFT GALLEY FRAME 68 - FRAME 69, STRINGER 23 RT - STRINGER 24 RT, SHEAR PLATE TRAY CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51-42-11 PARA 6 AND 13.

Part: TUBE — BROKEN (HYD SYSTEM) · airframe 27,814 hrs · 13,526 cycles

ECAM IN FLIGHT. HYD Y R5VR LO AIR PT, Y RSVR LO LVL, Y ELEC PUMP LO PR. FOUND TUBE BROKEN. R & R TUBE ASSY, OPS AND LEAK CHECK NORMAL. SERVICED YELLOW SYS HYD, REF AMM 29·13-49 PB401.

Part: FITTING — OUT OF RIG (GIRTBAR) · airframe 20,447 hrs · 9,988 cycles

PILOT REPORTS AN INTERMITTENT WARNING FOR THE R2 CABIN DOOR SLIDE ON THE ELECTRONIC CENTRALIZED ACFT MONITORING SYS. MX FOUND THE R2 GIRT BAR FITTING OUT OF RIG. MX RIGGED THE GIRT BAR FITTINGS IAW AMM 52-13-22-820-056 AND INSTALLED SLIDE ASSEMBLY IAW AMM 25-62-44-400-006.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,438 hrs · 9,984 cycles

DURING C4 C-CHECK, INSP NOTED THE LT PROFILE AT FRAME 56 TO FRAME 58 HAS CORROSION AROUND THE FASTENER HOLES. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 PARAGRAPH 7.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,438 hrs · 9,984 cycles

DURING C4 C-CHECK, INSP NOTED THAT THE PROFILE AT FRAME 59 AND STR 38R TO 38L HAD CORROSION AROUND THE FASTENER HOLES. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-73-11 AND 51-42-11 PARAGRAPH 7.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,438 hrs · 9,984 cycles

DURING C4 C-CHECK, INSP NOTED PROFILE ON FRAME 56 FROM STR 41 RT TO 38 LT IN AFT PIT FOR THE FLOORBOARD PANEL SHOWS SIGNS OF CORROSION AROUND FASTENER HOLES. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11 AND SRM 51-72-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,438 hrs · 9,984 cycles

DURING C4 C-CHECK, INSP NOTED THE PROFILE ON FRAME 58 FROM STR 41 RT TO 38 LT IN AFT PIT FOR THE FLOORBOARD PANEL SHOWS SIGNS OF CORROSION AROUND FASTNER HOLES. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11, SRM 51-44-11, SRM 51-46-11 AND SRM 51-72-11.

Part: FRAME — CORRODED (ZONE 100) · airframe 20,438 hrs · 9,984 cycles

DURING C4 C-CHECK, INSP NOTED AFT PIT FRAME 52 CTR TIE DOWN POINT HAS EVIDENCE OF CORROSION AT FASTENER HOLES. MX REMOVED AND REPLACED PLATE IAW SRM 51-42-11, SRM 53-41-14, SRM 51-31-00 AND SRM 51-72-11.

Part: HINGE FITTING — WORN (LT MLG DOOR) · airframe 22,804 hrs · 10,925 cycles

DURING C5 C CHECK INSPECTION NOTED THE LEFT HAND FORWARD MAIN LANDING GEAR DOOR HINGE FITTING HAS OBLONG HOLES IN FITTING ATTACHED TO DOOR. MAINTENANCE INSTALLED A NEW FITTING ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30327 AND AMM 20-21-11 PAGE BREAK 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: COMPUTER — FALSE INDICATION (ZONE 200) · airframe 15,431 hrs · 7,423 cycles

AFTER TAKEOFF, THE FLIGHT CREW RECEIVED AN ECAM WARNING "LAND ASAP" AND RECALL FUNCTION DISPLAYED AVIONICS SMOKE. IAW TSM 26-15-00-810-803 AND TFU 26.15.15.001 FOUND FAULT WAS LATCHED IN FLIGHT WARNING COMPUTERS. MAINT RESET FLIGHT WARNING COMPUTERS IAW THE REQUIREMENTS TSM 26-15-00-810 OPERATION CHECK NORMAL AND THE AC WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (CABIN) · airframe 22,804 hrs · 10,925 cycles

DURING C5 C CHECK INSPECTION NOTED ALL FOUR EPSU BATTERY PACKS FAILED EMERGENCY LIGHTS CAPACITY TEST. MAINTENANCE REMOVED AND REPLACED EPSU BATTERIES 10WL, 11WL, 12WL AND 13WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-400-002. UPON COMPLETION OF THE REPAIR THE BATTERIES OPERATIONAL CHECKED GOOD AND WAS INSPECTED AND FOUND ACCEPTABLE.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 15,411 hrs · 7,412 cycles

REFERENCE LOG PAGE 321828. DURING PRE FLIGHT INSP, THE CREW NOTED EMERGENCY EXIT LIGHT OVER L2 DOOR WAS ILLUMINATED. THE CREW WAS UNABLE TO EXTINGUISH WITH EMERGENCY EXIT LIGHT SWITCH IN THE COCKPIT. MAINT SWAPPED WIRES AND TESTED EMERGENCY EXIT LIGHTS IAW THE REQUIREMENTS OF AMM 33-51-00-710-001. MAINT OPERATION CHECKED GOOD AND RETURNED THE AC TO SERVICE.

Part: ATTACH FITTING — DAMAGED (FUSELAGE) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED, THE LEFT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING ON KEEL BEAM FORWARD LUG HAS NICK ON FORWARD EDGE. MAINTENANCE BLENDED AREA ON LEFT MAIN LANDING GEAR ACTUATOR FITTING ON KEEL BEAM DEPTH OF AREA IS .013 INCH AND LENGTH IS .123 INCH AREA FOUND TO BE WITHIN LIMITS. REMOVED LEFT TO FACILITATE OTHER MAINTENANCE, PERFORMED FLAP ROTO PEENING ON BLENDED AREA TO INTENSITY OF .015 MMN AND REINSTALLED LEFT MAIN LANDING GEAR DOOR ACTUATOR. ALL WORK WAS COMPLETED IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30270, SRM 51-73-00, SRM51-29-11 AND AMM 32-31-25-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FITTING — CORRODED (L2 DOOR) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED L2 DOOR AFT LOWER CORNER CAST FITTING IS CORRODED. MAINTENANCE REMOVED AND REPLACED L2 DOOR AFT LOWER CORNER CAST FITTING IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND AMM 53-45-15. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LEFT FLOORBOARD FRAME AT STRINGER 38 LEFT BETWEEN FRAMES 58 AND 59 HAS AREAS OF CORROSION AROUND NUT CLIP HOLES. MAINTENANCE REMOVED AND INSTALLED FLOORBOARD FRAME DOOR SILL PLATE AT STRINGER 38 LEFT BETWEEN FRAMES 58 AND 59 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SUPPORT BRACKET — CRACKED (LT ENGINE) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED CRACK IN LPT COOLING TUBE SUPPORT BRACKET ON LEFT ENGINE RIGHT SIDE APPROXIMATELY FOUR O'CLOCK POSITION. MAINTENANCE REMOVED AND INSTALLED NEW LPT COOLING SUPPORT BRACKET ON LEFT ENGINE RIGHT SIDE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 20-21-11-991-034. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO FLOOR PANEL 151ZG WAS DELAMINATED. MAINTENANCE TRIMMED BACK UPPER SKIN REMOVED CORE AND LOWER SKIN ABRADED BOTTOM SURFACE OF SKIN IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T-10131. MANUFACTURED FILLER PLATE AND DOUBLER PLATE, STEP SANDED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T-10131 AND SRM 53-02-00 AND 51-57-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO RIGHT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 RIGHT BETWEEN FRAMES 52 AND 55 HAS AREAS OF CORROSION AROUND NUTPLATE HOLES. MAINTENANCE REMOVED AND REPLACED RIGHT FLOORBOARD SUPPORT PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUNDS ACCEPTABLE.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO FLOOR PANEL 151DE HAS DAMAGED EDGE AND CORNER. MAINTENANCE CLEANED AND PREPPED AREA, MANUFACTURED DOUBLER AND APPLIED REPAIR TO AREA. MANUFACTURED DOUBLER, APPLIED TREATED AND PRIMED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 AND 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD PROFILE AT FRAME 59 BETWEEN STRINGER 38 LEFT AND 38 RIGHT HAS AREAS OF CORROSION AROUND NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED PROFILE AT FRAME 59 BETWEEN STRINGER 38 LEFT AND 38 RIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED CORROSION ON AND AROUND FASTENERS ON BEAM INBOARD OF R2 DOOR BETWEEN FRAME 68 AND 70. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-42-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED BULK CARGO PANEL 161BF HAS A PUNCTURE. MAINTENANCE CLEANED AREA FOR DAMAGE PREPPED AND REPAIRED, APPLIED PRIMER AND TOP COAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH C AND SRM 51-75-12 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED LEFT AVIONICS COMPARTMENT FRAME C20 LATERAL BRACE IS FRETTING AT FRAME C20 MOUNT HOLE. MAINTENANCE REMOVED DAMAGED CROSSBEAM, DRILLED UP AND INSTALLED NEW CROSSBEAM AT FRAME C20 LEFT AVIONICS BAY IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED UPON REMOVAL OF SHEAR PLATE FOUND FRAME SUPPORT TO BE CORRODED ON UNDER SIDE. MAINTENANCE REMOVED CORRODED FRAME SUPPORT AND REPLACED WITH NEW SERVICEABLE FRAME SUPPORT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: BEARING — SEIZED (DOOR HOOK) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED RIGHT HAND AFT ENTRY DOOR UPPER LATCH HOOK BEARING SEIZED. MAINTENANCE REMOVED AND REPLACED RIGHT AFT ENTRY DOOR UPPER LATCH HOOK BEARING IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-13-00-820-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED NAD FOUND ACCEPTABLE.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD PROFILE AT FRAME 58 BETWEEN STRINGER 38 LEFT AND STRINGER 41 RIGHT HAS AREA OF CORROSION AROUND NUTPLATE HOLES. MAINTENANCE REMOVED AND REPLACED AFT CARGO FLOORBOARD PROFILE AT FRAME STATION 58 BETWEEN STRINGER 38 LEFT AND STRINGER 41 RIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-00 AND SRM 53-41-14. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED FWD CARGO DOOR FLOOR PANEL HAD A PUNCTURE. MAINTENANCE CLEANED AREA, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FITTING — CORRODED (GIRT BAR) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION REPORTED L2 AFT DOOR GIRT BAR FITTING WAS CORRODED. MAINTENANCE REMOVED GIRT BAR FITTING, FABRICATED NEW GUIDES AND NUTPLATE STRIPS FROM 2024T3 .050. INSTALLED NEW FABRICATED PARTS AND REINSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: BATTERY BOX — LOOSE · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED THE FORWARD BATTERY TRAY AFT OUTBOARD MOUNT HAS EXCESSIVE PLAY CAUSING FRETTING. MAINTENANCE REMOVED AND REPLACED AFT OUTBOARD MOUNT FROM FORWARD BATTERY TRAY IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO RIGHT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 RIGHT FROM FRAME 25 TO FORWARD OF FRAME 34 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED RIGHT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 RIGHT FROM FRAME 28 TO FRAME 34 AND INSTALLED FASTENER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: MOUNT — WORN (BATTERY TRAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT BATTERY TRAY FORWARD AND AFT OUTBOARD MOUNTS HAVE EXCESSIVE PLAY CAUSING FRETTING. MAINTENANCE REMOVED AND REPLACED OUTBOARD FORWARD AND AFT MOUNTS ON BATTERY TRAY IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO DOOR) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO MID FLOOR PANEL 152WG HAS DAMAGED END. MAINTENANCE REMOVED DAMAGE AND PREPPED FOR REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. APPLIED REPAIR TREATED AND PRIMED AND APPLIED TOP COAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C, SRM 51-75-12 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO LATERAL FLOORBOARD SUPPORT PROFILE AT FRAME 28 FROM STRINGER 38 LEFT TO 38 RIGHT HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE BLENDED CORROSION AROUND SEVERAL NUT PLATE HOLES ON FLOORBOARD SUPPORT PROFILE AT FRAME 28 FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE REMOVED FLOORBOARD SUPPORT AND REPLACED IT WITH NEW FLOORBOARD SUPPORT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-00, SRM 53-00-14, SRM 53-00-00, SRM 53-74-00, SRM 53-21-14 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED NUMBER ONE SLAT RIGHT WING APPROXIMATELY 36 INCHES FROM OUTBOARD END DENT MEASURES 7 INCHES BY 2 7/8 INCHES BY .252. DENT WITHIN LIMITS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-40-00 PAGE BREAK 201 PARAGRAPH 5D FIGURE 204. MAINTENANCE REMOVED NUMBER ONE RIGHT SLAT, REPAIRED DENT ON RIGHT NUMBER ONE SLAT AND REINSTALLED RIGHT NUMBER ONE SLAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-40-00 AND AMM 27-84-63-000-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED FWD CARGO LEFT SIDE PANEL 131EG PANEL RACK DAMAGED. MAINTENANCE CLEANED AND PREPPED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 8C AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-02. TREATED, PRIMED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED CORROSION ON AND AROUND NUT CLIPS ON FLOORBEAM JUST IN FRONT OF R2 DOOR BETWEEN FRAMES 66 AND 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-00 AND SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

REFERENCE NON ROUTINE 31546. DURING C3 S1 C CHECK INSPECTION NOTED THE FORWARD CARGO LEFT FLOOR SUPPORT PROFILE AT STRINGER 38 LEFT FROM FRAME 24A TO 28 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE REMOVED CORRODED PROFILE AND REPLACED WITH NEW FABRICATED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED BULK CARGO PANEL 161CF HAS A PUNCTURE. MAINTENANCE CLEANED AREA FOR DAMAGE AND PREPPED, REPAIRED AND APPLIED PRIMER AND TOP COAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-75-12 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED CORROSION ON PLATE RIGHT SIDE OF AIRCRAFT MOST OUTBOARD BETWEEN FRAMES 69 AND 70. MAINTENANCE REMOVED DOUBLER STANDOFF BRACKET AND WIRE HARNESS, REMOVED AND REPLACED CORRODED SHEAR PLATE AND REINSTALLED DOUBLER AND STANDOFF BRACKET AND REINSTALLED WIRE HARNESS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11, SRM 51-42-11 AND AMM 20-33-42. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED FWD CARGO FLOOR PANEL 132DG HAS A PUNCTURE. MAINTENANCE CLEANED AREA AND PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: BOTTLE — LOW (DOOR ASSIST) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED R1 DOOR ASSIST BOTTLE NEEDS RECHARGING. MAINTENANCE RECHARGED R1 DOOR ASSIST BOTTLE AT 66 DEGREES TO 1700 PSI IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-10-00-614-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED CABIN FLOOR PANEL 241CF HAD A PUNCTURE. MAINTENANCE CLEANED AND PREPPED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED CABIN FLOOR PANEL 252HF HAS A PUNCTURE IN THE TOP SURFACE. MAINTENANCE CLEANED AREA, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8A AND SRM 53-20-00 PARAGRAPH 8A. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT BETWEEN FRAMES 56 AND 58 HAS AREAS OF CORROSION AROUND NUT PLATE HOLES. MAINTENANCE REMOVED CORRODED PROFILE AT STRINGER 38 LEFT FROM FRAME 56 AND 58 LEFT AFT CARGO AND REPLACED WITH NEW PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 CHECK INSPECTION NOTED CORROSION ON AND AROUND NUT CLIPS ON FLOORBEAM JUST INSIDE OF THE L2 DOOR BETWEEN FRAMES 66 AND 68. MAINTENANCE REMOVED AND REPLACED BEAM JUST INSIDE OF L2 DOOR BETWEEN FRAMES 66 AND 68 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 CHECK INSPECTION NOTED FORWARD CARGO LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT FROM FRAME 28 TO FORWARD FRAME 34 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT FROM FRAME 28 TO FRAME 34 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-00 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOORBOARD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD PROFILE AT FRAME 56 BETWEEN STRINGER 38 LEFT AND 41 RIGHT HAS AREA OF CORROSION AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED AFT CARGO FLOORBOARD PROFILE AT FRAME STATION 56 IN ACCORDANCE WITH THE REQUIRMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO FLOOR PANEL 152TG HAS DAMAGED EDGE. MAINTENANCE REPLACED AFT CARGO MID FLOOR PANEL 152TG WITH NEW PANEL. PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF NON ROUTINE 9623. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED HEAVY CORROSION FOUND ON FLOOR SUPPORT JUST FORWARD OF SEAT TRACK AT FRAME 20 RIGHT SIDE. MAINTENANCE REMOVED SEAT TRACK LOCATED AND DRILLED HOLES, INSTALLED BRACKETS, TREATED, PRIMED AND INSTALLED NEW SEAT TRACK IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, SRM 51-21-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT BETWEEN FRAMES 52 AND 56 HAS AREAS OF CORROSION AROUND NUT PLATE HOLES. MAINTENANCE REMOVED PROFILE SUPPORT AT STRINGER 38 LEFT BETWEEN FRAMES 52 AND 56, DRILLED AND PREPPED NEW PROFILE FOR THE INSTALLATION, TREATED, PRIMED AND INSTALLED NEW PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14, SRM 51-42-00 AND SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO AFT FLOORBOARD PARTITION AND PARTITION WALL SUPPORT ANGLE PROFILE JUST FORWARD OF FRAME 34 FROM STRINGER 38 LEFT TO STRINGER 38 RIGHT HAS CORROSION AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AFT FLOORBOARD PARTITION WALL SUPPORT ANGLE PROFILE FORWARD OF HOLES FRAME 34 FROM STRINGER 38 LEFT TO STRINGER 38 RIGHT AND LOCATED AND LAYOUT AND INSTALLED NEW SUPPORT ANGLE PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-44-11, SRM 51-61-11, SRM 53-21-14, SRM 51-72-11 AND SRM 51-40-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: BEARING — SEIZED (LT PAX DOOR) · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED LEFT AFT ENTRY DOOR UPPER LATCH HOOK BEARING WAS SEIZED. MAINTENANCE LUBED AND CLEANED, ROLLER MOVED FREELY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 12-22-52. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,382 hrs · 7,397 cycles

DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD FRAMES AT FRAME 59 BETWEEN STRINGERS 38 LEFT AND 38 RIGHT HAS CORROSION AROUND NUT CLIP HOLES. MAINTENANCE REMOVED CORROSION ON CONNECTING ANGLES, FABRICATED NEW CONNECTING ANGLE. TREATED, PRIMED, TOP COATED AND INSTALLED NEW CONNECTING ANGLE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, SRM 51-74-00, SRM 51-21-11 AND SRM 51-75-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SEAL — WORN (NR 2 PACK) · airframe 11,967 hrs · 5,765 cycles

WHILE PARKED AT GATE, FLIGHT CREW REPORTED BURNED ELECTRIC ODOR IN COCKPIT. PERFORMED TSM TASKS 26-15-00-810-804 AND 26-17-00-810-804. ODOR FOUND TO BE COMING FROM NR 2 PACK, WHICH HAD WORN SEALS. REPLACED SEALS ON NR 2 PACK IAW AMM 21-52-23, PB 401 AND REPLACED ACM GASKET IAW AMM 21-52-21-000-002/400-002. PERFORMED OPS TEST, NO LEAKS OR ODOR NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,972 hrs · 2,976 cycles

BLOCK TURN BACK, FLIGHT CREW REPORTED APU AUTO SHUTDOWN, EMERGENCY SHUTDOWN DUE TO BURNING SMELL. MAINTENANCE PERFORMED AN INSPECTION AND OPERATIONAL CHECKS OF THE APU PER AMM 49-00-81-810-803. NO INDICATION OF BURNING SMELL WAS FOUND. RII INSPECTION PER GMM 85.07. RAN APU AND PACKS IAW 12-33-21-618-001. NO BURNING SMELL DETECTED.

Part: CIRCUIT BREAKER — MELTED (LOCATION Q35) · airframe 8,676 hrs · 4,113 cycles

CIRCUIT BREAKER (LGCIU NR 2) ARCED AND MELTED. REPLACED CIRCUIT BREAKER PER ASM32-31-00, SCH 06, PG 10 AND AMN 32-69-00-740-001.