N939FR

Part: DOOR FRAME — CRACKED · airframe 39,921 hrs · 20,025 cycles

RIGHT EMERGENCY OVERWING EXIT FWD AND AFT I/B FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED IAW SRM 51-42-11.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 39,921 hrs · 20,025 cycles

LEFT EMERGENCY OVERWING EXIT AFT INBD DOOR FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED EMERGENCY EXIT AFT DOOR FRAME IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 39,921 hrs · 20,025 cycles

AFT CABIN FRAME 66+10 THROUGH 68+6 Y1292 FLOOR SUPPORT TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,921 hrs · 20,025 cycles

CORROSION ON FLOORBEAM Y1292, FASTENER HOLE BETWEEN FRAME 20 AND FRAME 18. R & R FLOORBEAM AT Y1292, FRAME 12-24 IAW SRM 51-72-11-911 AND SRM 51-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,921 hrs · 20,025 cycles

AFT CABIN FRAME 67-FRAME 68, Y765, FLOORBEAM TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. R & R AFT CABIN FLOORBEAM Y765 AT FRAME 67-FRAME 68 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,921 hrs · 20,025 cycles

CORROSION ON FLOORBEAM Y1292 BETWEEN FRAME 17 AND FRAME 20. R & R FLOORBEAM AT Y1292, FRAME 17 AND FRAME 20 IAW SRM 51-72-11, 51-42-11, 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,921 hrs · 20,025 cycles

AFT CABIN, FRAME 66, Y508 FLOORBEAM CORRODED AT MULTIPLE LOCATIONS. REMOVE CORROSION MAXIMUM DEPTH OF REWORK IS .016, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 001. REMOVED OLD BEAM AT Y508, FR 66 IAW SRM 52-42-11. LOCATED & DRILLED NEW FLOORBEAM, INSTALLED NEW BEAM AT FRAME 66, Y508 IAW SRM 51-42-11.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,479 hrs · 16,335 cycles

C6 CHECK. PAX CABIN FROM FRAME 69 - 70 RT - Y1292 HAS SURFACE CORROSION AT FIVE EACH MULTIPLE FASTENERS HOLES AT SKIN PLATE. R & R SKIN PLATE IAW EO A0-53EO-31434, SRM 51-42-11 PAR 6B 3 A-D PAR 13D 1-4.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,403 hrs · 16,293 cycles

EPSU EMER LIGHTS BATTERY 12WL FAILED CAPACITY TEST ON TASK CARD A332204-02. R & R THE EPSU BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & 33-51-38-400-002A.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 35,551 hrs · 15,260 cycles

DOOR R2 SLIDE PRESS LOW. R & R R2 DOOR ESCAPE SLIDE IAW AMM 25-62-44 PB 401.

Part: BLEED AIR SYS — ODOR (ZONE 600) · airframe 28,616 hrs · 14,180 cycles

ODOR IN CABIN AT LOW ALTITUDES, BOTH TAKEOFF AND APPROACH (AROUND 10,000' AGL) STRONG ODOR AROUND ROW 20-22. RAN APU, ENGINE NR 1 AND ENGINE NR 2 AND COULD NOT DETECT AN ODOR. R & R RECIRCULATION FILTERS REF AMM 21-21-45, PB401. ACFT NEEDS OPS CHECK FLIGHT TO DETERMINE SOURCE OF ODOR. DISCREPANCY NR 2: OPS CHECK FLIGHT UNSATISFACTORY - NR 2 ENGINE BLEED ON, NR 1 ENGINE BLEED OFF - SMOKE SMELL IN CABIN SIMILAR TO OIL OR ENGINE EXHAUST. SMELL DIMINISHES WHEN BLEED NR 2 TURNED OFF AND BLEED NR 1 TURNED ON. SMELL INCREASES WITH INCREASE IN THRUST ON NR 2 ENGINE. R & R NR 2 ENGINE IAW MP71042-02, AMM 71-00-00-710-008, 71-00-00-710-025, 36-11-00-710-003-A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,978 hrs · 13,348 cycles

C-CHECK, EMERGENCY LIGHT SYS TEST FAILED FOR FWD EPSU 10WL. R & R EPSU IAW AMM 33-51-38-020-051-A. SYSTEM OPS GOOD IAW 33-51-38-740-050-B.

Part: A/C PACK — SMOKE (NR 2) · airframe 26,062 hrs · 12,878 cycles

ECAM MESSAGE NR 2 PACK OVERHEAT, ON DEPARTURE CLIMBING THROUGH 11,000 F/A CALLED WITH INFO ON SMOKE IN CABIN (AFT), ODOR WAS NOTABLE BUT DISSIPATING. EMERGENCY DECLARED AIR TURN BACK ON LANDING ROLL OUT, ECAM MESSAGE APPEARED, ACTIONS COMPLETED.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,384 hrs · 10,746 cycles

C-CHECK: NON ROUTINE NR 1287; CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 48, FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM AT FR 68, RBL 48 IAW SRM 51-24-00, PARA 6.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 21,384 hrs · 10,746 cycles

C-CHECK: NON ROUTINE NR1262; LT AFT LATERAL SHEAR PLATE IS CRACKED, FR69, STR 24. REPLACED LT AFT LATERAL SHEAR PLATE WITH NEW CONFIGURATION IAW EO A0-53EO-31434 AND IAW SRM 51-42-11-1- A, B, C.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,384 hrs · 10,746 cycles

C-CHECK: CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 30. R & R FLOORBEAM AT FR 66-70, RBL 30 IAW SRM 51-74-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 21,384 hrs · 10,746 cycles

C-CHECK: CABIN FLOOR PANEL 241JF HAS DELAMINATION IN SEVERAL AREAS AND FOUND TO BE OUT OF REPAIRABLE LIMITS. R & R FLOOR PANEL 241JF IAW SRM 53-02-00, PB 101.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 21,384 hrs · 10,746 cycles

C- CHECK: NON ROUTINE NR1329: COCKPIT FLOORBOARD, 211GF SURFACE IS DAMAGED. FOUND DAMAGE TO FLOORBOARD 211GF BEYOND REPAIRABLE LIMITS. REPLACED FLOORBOARD IAW SRM 53-12-00, DIAGRAM 101.

Part: COMPUTER — FAULTED (ELAC NR 2) · airframe 18,986 hrs · 9,375 cycles

REF: PILOT REPORT LOG PAGE 549851 ITEM 1. CLIMBING THROUGH FLIGHT LEVEL 380 ELAC NR 2 FAULTED, ACFT WENT INTO ALTERNATE LAW. AIR TURN BACK TO SMF. REPLACED NR 2 ELAC REF AMM 27-93-34 PAGE BLOCK 401, OPS CHECK GOOD. PERFORMED LAND CATAGORY III CAPABILITIES TEST REFERENCE AMM 22-97-00-710-001. CATAGORY IIIA RETAINED. REFERENCE TSM 27-93-00-810-830.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 16,972 hrs · 8,445 cycles

DURING LANDING THE FLIGHT CREW NOTED THE L2 DOOR SLIDING ARMING LEVER DISARMS IN FLIGHT AND APPEARS RELATED TO CABIN PRESSURE DIFFERENTIAL ABOVE 10000 FEET. MX ADJUSTED ESCAPE SLIDE RELEASE MECHANISM AFT GIRT BAR FITTING ADJUSTED TO CORRECT CLEARANCES AND PERFORMED TEST OF THE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM IAW AMM 52-13-22-820-056 AND AMM 52-73-00-710-050.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 16,970 hrs · 8,444 cycles

DURING CRUISE ALTITUDE, THE FLIGHT CREW NOTED THE L2 DOOR ARM LIGHT WAS ON AND INTERMITTENT. MX ADJUSTED THE GIRT BAR FITTING FOR THE L2 DOOR AND PERFORMED A TEST OF THE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM IAW AMM 52-13-22-820-056 AND AMM 52-73-00-710-050.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP NOTED SEAT ROW 10B AND 10C EMERGENCY EXIT LIGHT WIRE WAS BROKEN AT CONNECTOR OTBD SEAT LEG GOING TO FLOOR. MX REMOVED AND REPLACED EMERGENCY EXIT WIRE HARNESS IAW AMM 25-21-41-000-001 STEP 4A(2)(B), AMM 25-21-41-400-001 STEP 4D(1)(C) AND AMM 33-51-00-710-009.

Part: SILL — CORRODED (ZONE 200) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP, NOTED THE L2 DOOR SILL CORRODED AT FWD SPLICE IN AND AROUND THE FLOORBOARD ATTACH HOLE. MX REPAIRED DOOR SILL IAW SRM 53-41-14 AND EA A9-53R-31579.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP NOTED A HOLE IN FLOORBEAM Y1292 JUST AFT OF LAVATORY D FROM FRAME 64 TO FRAME 66 AND WAS ALSO CORRODED. MX REMOVED AND REPLACED FLOORBEAM Y1292 IAW SRM 51-42-11 AND SRM 51-44-11.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP, NOTED MAIN CABIN FLOOR PANEL 261FF HAS CORROSION. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE FROM FRAME 69 TO FRAME 70 WAS CORRODED. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-21-00.

Part: THRESHOLD — CORRODED (ZONE 200) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP, NOTED THRESHOLD STRIP FOR L2 DOOR THRESHOLD IS CORRODED. MX REMOVED AND REPLACED THRESHOLD STRIP IAW AMM 53-42-12-400-001.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT Y1292 FRAME 66 TO FRAME 69. MX REMOVED AND REPLACED FLOOR SUPPORT Y1292 AT FRAME 66 TO FRAME 69 RT SIDE IAW SRM 51-42-11, SRM 51-21-00 AND EA A9-53T-30392.

Part: PLATE — CORRODED (ZONE 200) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP NOTED THE ARMED PLATE FOR THE R2 DOOR WAS CORRODED. MX REMOVED AND REPLACED ARM PLATE IAW AMM 53-42-12-420-051.

Part: STRIP — CORRODED (ZONE 100) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSPECTION, NOTED THE THRESHOLD STRIP FOR PANEL 262EF IS CORRODED. MX REMOVED AND REPLACED STRIP IAW AMM 53-42-12-400-002.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT FLOOR SUPPORT Y1292 FROM FRAME 66 TO FRAME 69. MX REPLACED FLOOR SUPPORT Y1292 AT FRAME 66 TO FRAME 69 LT SIDE IAW SRM 51-42-11 AND SRM 51-44-11.

Part: PLATE — CORRODED (ZONE 200) · airframe 16,966 hrs · 8,441 cycles

DURING C3 C-CHECK INSPECTION, NOTED ARMED PLATE FOR L2 DOOR IS CORRODED. MX REMOVED AND REPLACED ARMED PLATE ON L2 DOOR THRESHOLD IAW AMM 20-21-11, PB 201.

Part: HMU — FAILED (NR 2 ENGINE) · airframe 14,000 hrs · 6,944 cycles

PILOT REPORTED THAT THE NR 2 ENGINE FAILED ON DESCENT FROM FL 350, THE ENGINE RECOVERED AND FURTHER DESCENT, APPROACH AND LANDING WERE UNEVENTFUL ON TWO ENGINES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRO MECHANICAL UNIT AND PERFORMED SATISFACTORY OPERATIONAL AND LEAK CHECKS IN ACCORDANCE WITH AMM 73-21-10 PB 401.

Part: BUSHING — OUT OF POSITION (L1 DOOR) · airframe 13,002 hrs · 6,433 cycles

REFERENCE LOG PAGE 420725. PILOT REPORTED THE FORWARD ENTRY DOOR L1 GUST LOCK WILL NOT ENGAGE. MAINTENANCE REINSTALLED BUSHING IN THE FORWARD ENTRY DOOR GUST LOCK MECHANISM IN ACCORDANCE WITH A319 AMM 52-11-11-730-050.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED AFT CARGO PIT FWD FLOORBOARD PANEL 151PE HAS A HOLE AT THE AFT LT EDGE. MAINT REMOVED DAMAGED AREA AND FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED AFT CARGO PIT FWD LT HAND LOWER TRANSITION PANEL 151AE HAS A HOLE AT FWD LOWER END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 151AE IAW SRM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT LT HAND TRANSITION PANEL 161BF HAS A HOLE AT AFT TOP END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 161BF IAW SRM 53-42-44-400-001. COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (CARGO BAY) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG HAS A HOLE AT AFT CENTER SECTION. MAINT REPAIRED TRANSITION PANEL 152WG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (CARGO BAY) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151FE HAS A HOLE AT FWD TOP CORNER. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT FORWARD RT LOWER TRANSITION PANEL 152TG HAS A HOLE AT BOTTOM AFT OF CENTER TIE DOWN CUT OUT. MAINT REPAIRED TRANSITION PANEL 152TG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (CARGO BAY) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD RT UPPER TRANSITION PANEL 152XG HAS SEVERAL HOLES. MAINT REPAIRED TRANSITION PANEL 152XG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT LOWER TRANSITION PANEL 151TG HAS A HOLE AT THE AFT CENTER SECTION. MAINT REPAIRED TRANSITION PANEL IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT HAND UPPER TRANSITION PANEL 151UG HAS SEVERAL HOLES. MAINT REPAIRED FLOOR PANEL IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT UPPER TRANSITION PANEL 162CF HAS SEVERAL HOLES AT AFT END. MAINT REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSPECTION NOTED TWO CRACKS FOUND ON FLOORBOARD 161NF DURING REMOVAL. MAINT REPAIRED FLOOR PANEL 161NF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF HAS A HOLE AT AFT CENTER SECTION. MAINT REPAIRED TRANSITION PANEL 162BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF HAS HOLES IN SEVERAL PLACED. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED FWD PIT TRANSITION PANEL 132EG HAS A PUNCTURE. MAINT REPAIRED TRANSITION PANEL 132EG IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 132BF HAS SEVERAL PUNCTURES. MAINT REPAIRED TRANSITION PANEL 132BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131AF HAS SEVERAL PUNCTURES. MAINT REPAIRED FLOOR PANEL 131AF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 132CF HAS SEVERAL PUNCTURES. MAINT REPAIRED TRANSITION PANEL 132CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED FORWARD PIT TRANSITION PANEL 132DG HAS A PUNCTURE. MAINT REPAIRED TRANSITION PANEL 132DG IAW SRM 53-02-00, FIG 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: HOOK — INOPERATIVE (L2 DOOR) · airframe 11,700 hrs · 5,735 cycles

DURING C-CHECK INSP NOTED L2 DOOR LATCH HANDLE CAN BE OPERATED WHILE DOOR IS OPEN. MAINT REMOVED AND REPLACED L2 DOOR INNER HANDLE LOCK HOOK IAW AMM 52-13-21-420-052 STEP 17. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 9,682 hrs · 4,791 cycles

FLIGHT CREW REPORTED EMERGENCY EXIT SIGN OVER R2 DOOR WOULD NOT ILLUMINATE. RESEATED CONNECTOR ON 32WL AND OPS CHECKED NORMAL IAW AMM 33-51-00-PB501.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,675 hrs · 4,788 cycles

FLIGHT CREW REPORTED AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY UNIT AFT 13WL IAW AMM 33-51-38-PB401. PERFORMED OPS CHECK. CHECKED GOOD.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,675 hrs · 4,788 cycles

FLIGHT CREW REPORTED AFT OVERHEAD EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE WITH GEAR EXTENSION. REPLACED EPSU 13WL IAW AMM 33-51-38-PB401. OPS TEST GOOD IAW AMM 33-51-38-740-040 AND CIDS EPSU TEST IAW 23-73-00-710-010.

Part: STARTER — SEIZED (APU) · airframe 8,852 hrs · 4,402 cycles

MAINTENANCE REPORTED ELECTRICAL SMOKE ODOR IN APU COMPARTMENT AFTER APU AUTO SHUTDOWN. INSPECTED APU COMPARTMENT IAW TSM 24-00-00-810-823 AND IDENTIFIED ODOR WAS FROM STARTER. FOUND APU SENSE WIRE HEAT DAMAGED AND HEAT SHRINK ON POSITIVE WIRE DAMAGED. STARTER WAS SEIZED. REMOVED AND REPLACED APU STARTER IAW AMM 49-42-51-000-004 AND AMM 49-42-51-400-004. WIRE DAMAGED FROM HEAT NEEDS TO BE REPAIRED/REPLACED PER ESPM. APU SYSTEM WAS DEACTIVATED IAW MEL 49-10-01A, CONTROL NUMBER 1029980, AND TRANSFERRED TO SUPPLEMENTAL SHEET.