N76153

Part: CONNECTOR — UNSECURE (CABIN) · airframe 46,380 hrs · 6,877 cycles

SEAT 29LK PSU OXYGEN DOOR OPERATION CHECK FAILED. SEAT 29 OK PSU OXYGEN DOOR ELECTRICAL CONNECTOR RE-SECURED AND OPERATION CHECKED NORMAL MM-35-21-00.

Part: STIFFENER — CRACKED (NR 1 PYLON) · airframe 46,380 hrs · 6,877 cycles

NR 1 PYLON STA 285 FOUND O/B STIFFENER CRACKED NR1 PYLON STA 285 O/B CRACKED STIFFENER. REPLACED AS PER SRM 51-10-02 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ITEM 1-2 ACCOMPLISHED.

Part: SKIN — DEFORMED (MAIN EQUIP DOOR) · airframe 46,380 hrs · 6,877 cycles

MAIN EQUIPMENT CENTER DOOR RT FWD CORNER BEYOND SKIN CLEARANCE LIMIT. MAIN EQUIPMENT CENTER DOOR EXTERIOR SKIN REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 (NEW SKIN FABRICATED DETAIL REF NRC 100-0260 (6611379)) ATT MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 8 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,380 hrs · 6,877 cycles

CABIN BS 325 RBL 75 FLOORBEAM CORRODED. CABIN BS 325 RBL 75 FLOORBEAM UPPER CHORD CORROSION REMOVED OUT OF SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMIT & CORRODED UPPER CHORD REPAIRED AS PER ECRA#5310-05376 REV- AND FORM 44.0008 ATTACHED ITEM 1-9 ACCOMPLISHED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,380 hrs · 6,877 cycles

CABIN RT STA 742-764 RBL 35 FLOOR SUPPORT ANGLE FOUND CRACKED. CABIN RT STA 742-764 RBL 35 CRACKED FLOOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND NEW SUPPORT ANGLE INSTALLED AS PER SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,380 hrs · 6,877 cycles

CABIN RT STA 1241-1263 RBL 35 FLOOR SUPPORT ANGLE FOUND CRACKED. CABIN RT STA 1241-1263 RBL 35 CRACKED FLOOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT ANGLE INSTALLED AS PER SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,380 hrs · 6,877 cycles

CABIN LT STSA 1241-1263 LBL35 FLOOR SUPPORT ANGLE FOUND CRACKED. CABIN LT STA 1241-1263 LBL 35 CRACKED FLOOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT ANGLE INSTALLED AS PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,380 hrs · 6,877 cycles

CABIN BS 1485 LBL 55 SEAT TRACK FLANGE CORRODED. CABIN BS 1361 TO BS 1485 LBL 55 SEAT TRACK FLANGE CORROSION REMOVED OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CORRODED SEAT TRACK REPLACED AS PER SRM51-10-02 & NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02 AT STA 1361 TO STA 1486 LBL 55.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,961 hrs · 6,566 cycles

CABIN STA 325 LBL 40 FLOORBEAM FOUND CORROSION. CABIN FLOORBEAM UPPER CHORD CORROSION AREA REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AT STA 325 LBL 40 AND FORM 44.0008 ATTACHED ITEM 1-25 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,961 hrs · 6,566 cycles

CABIN STA 303 LBL 30-40 FLOORBEAM FOUND CORROSION. CABIN CORRODED FLOORBEAM UPPER CHORD REPLACED AS PER SRM 53-00-51 REPAIR FIG 201 AT STA 303 LBL 30-40 AND FORM 44.0008 ATTACHED ITEM 1-15 ACCOMPLISHED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 42,770 hrs · 6,408 cycles

COCKPIT OVER DOOR EMERGENCY EXIT LIGHT SIGN INOP. REMOVED AND REPLACED EXIT SIGN LIGHT ASSY PER 33-51-01, OPS CKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT 1387287 SN OFF 00574 LIGHT, EMERGENCY OFF 64-3351-9-9001 0574 ON 64-3351-9-9001 0686.

Part: REGULATOR — FAILED (EVAC SLIDE) · airframe 42,270 hrs · 6,344 cycles

LEFT OVERWING SLIDE DID NOT DEPLOY AS PER W/C 62-2560-1-7800 STEP C.8.H. OVERWING SLIDE DID NOT INFLATE. FOUND CONFIRMED FAILURE ON LT O/W SLIDE INFLATION CYLINDER PRES SURE REGULATOR. FINDING CONFIRMED BY ENGINEER. INFLATION CYLINDER / REGULATOR AND SLIDE REPLACED AND SYSTEM RESTORED TO NORMAL PER SCHEDULED WORKCARD 62-2560-1-7800. PARTS CHANGE ACCOMPLISHED ON SEPARATE NON-ROUTINES. ENGINEER WAS ONSITE AND HAS PHOTOS OF THIS EVENT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,822 hrs · 5,740 cycles

L-4 DOOR SLIDE LIGHT DID NOT COME ON WHEN TESTED. RELAMPED L-4 SIDE LIGHT, OPERATION CHECKS GOOD PER AMM 33-51-06.

Part: LATCH — SEIZED (EMERGENCY EXIT) · airframe 37,822 hrs · 5,740 cycles

LEFT OVERWING ESCAPE COMPARTMENT DOOR LATCH WOULD NOT RELEASE, DOOR WOULD NOT OPEN. FOUND DOOR LATCH SEIZED, REMOVED AND REPLACED DOOR LATCH PER AMM 25-65-09, OPERATION CHECKS GOOD.

Part: TRANSMITTER — INOPERATIVE (TE FLAP) · airframe 37,699 hrs · 5,723 cycles

TRAILING EDGE FLAP LIGHT ON AT FLAPS 5 DURING APPROACH. RAN CHECKLIST LANDED AT FLAPS 5, TROUBLESHOT PER FIM 27-51-00, FIG 104, FOUND MESSAGE NUMBER 27-51080. REMOVED AND REPLACED NR 5 TRAILING EDGE FLAP SKEW TRANSMITTER IAW AMM 27-51-45. OPERATIONAL CHECKS GOOD. ROTABLE PARTS CHANGED TRACKING TAG 1354507, FLAP DRIVE POSITION TRANSMITTER, M& E PART NUMBER 62-2751-9-0008, S/N OFF 1283, S/N ON 1282.

Part: WEB — CRACKED (THRUST REVERSER) · airframe 33,238 hrs · 5,147 cycles

NUMBER 2 ENGINE RIGHTHAND C-DUCT FORWARD TORQUE BOX ATTACH WEB FOUND CRACKED AT 1 O`CLOCK POSITION. NUMBER 2 ENGINE RIGHTHAND C-DUCT FORWARD TORQUE BOX WEB REPAIRED PER MRAS CMM 78-32-02 REPAIR 024.

Part: WEB — CRACKED (THRUST REVERSER) · airframe 33,238 hrs · 5,147 cycles

NUMBER 1 ENGINE INBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB CRACKED AT 1 O`CLOCK POSITION. NUMBER 1 ENGINE INBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB AT 1 O`CLOCK POSITION REPAIRED PER MRAS CMM 78-32-02, REPAIR 024 AND HFEC NO CRACK FOUND.

Part: WEB — CRACKED (THRUST REVERSER) · airframe 33,238 hrs · 5,147 cycles

NUMBER 1 ENGINE OUTBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB CRACKED AT 11 O`CLOCK POSITION. NUMBER 1 ENGINE OUTBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB REPAIRED PER MRAS CMM 78-32-02 REPAIR 024.

Part: CHANNEL — CRACKED (NR 2 PYLON) · airframe 33,238 hrs · 5,147 cycles

NR 2 PYLON AFT FAIRING AFT BULKHEAD ATTACH CHANNEL FOUND CRACKED. NR 2 PYLON AFT FAIRING AFT BULKHEAD ATTACH CHANNEL REPLACED PER SRM 51-10-02 AND INSTALLED PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,238 hrs · 5,147 cycles

CABIN - BS 303 LBL 32 - 55 FLOOR SUPPORT FOUND CORRODED. BS 303 LBL 9 - 65 FLOORBEAM UPPER FLANGE REPAIRED PER SRM 53-00-51, REPAIR FIG 201.

Part: SKIN — DAMAGED (BS 142-157) · airframe 30,710 hrs · 4,803 cycles

THE AIRCRAFT SUSTAINED LIGHTNING STRIKE FUSELAGE SKIN DAMAGE AT STA 157, WL 235 AND AT STA 142, WL 226. THE DAMAGE AT STA 142 WAS REPAIRED IAW ECRA 5330-03743. THE DAMAGE AT STA 157 WAS REPAIRED IAW ECRA 5330-03739.

Part: SKIN — DAMAGED (BS 1132) · airframe 30,710 hrs · 4,803 cycles

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 1132, S8R. THE SKIN WAS REPAIRED IAW ECRA 5330-03744.

Part: SKIN — DAMAGED (BS 256.25) · airframe 30,710 hrs · 4,803 cycles

INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO THE RIGHT FUSELAGE SKIN AT STA 256.25, STRINGER 13R. THE DAMAGE WAS REPAIRED IAW ECRA 5330-03742.

Part: FITTING — OUT OF ADJUST (EVAC SLIDE) · airframe 26,154 hrs · 4,136 cycles

SLIDE FAILED TO DEPLOY UPON TEST. INFLATION ROD END FITTING AND CROSS PIN IMPROPERLY ADJUSTED. ADJUSTED ROD END IAW AMM 25-65-00, 25-65-01, 25-65-02, 25-65-04, 25-65-19.

Part: STIFFENER — CRACKED (LT NACELLE) · airframe 22,603 hrs · 3,609 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285 AREA I/B STIFFENER AFTER FRAME CHORD REMOVAL. THE STIFFENER WAS REPLACED IAW ECRA 5420-01445.

Part: FRAME — CRACKED (LT NACELLE) · airframe 22,603 hrs · 3,609 cycles

INSPECTION FOUND A 1 INCH CRACK IN LT PYLON NAC STA 285.4 AREA I/B FRAME CHORD. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01445.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 22,587 hrs · 3,606 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 28 TO LBL 60. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 303-325) · airframe 22,587 hrs · 3,606 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303 - 325, LBL 32. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 22,587 hrs · 3,606 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 19 TO LBL 32. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.