N69154

Part: STIFFENER — CRACKED (BS 246) · airframe 35,075 hrs · 5,363 cycles

BS 246 FLOORBEAM FWD SIDE 1 STIFFENER FOUND CRACK AT LBL 40, MES - BS 246 FLOOR BEAM FWD SIDE LBL 40 STIFFENER REPAIRED IAW ECRA 5310-04828 PART 1 AND MX WORKSHEET FORM 44.0008 ITEM 1 TO ITEM 6 ACCOMPLISHED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,466 hrs · 7,531 cycles

LT OVERWING EMERGENCY EXIT LIGHT (AFT OF FLAP T/E) INOP. RELAMPED LT AFT OVERWING EMERGENCY EXIT LIGHT, CKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,466 hrs · 7,531 cycles

CEILING EMERGENCY EXIT LIGHT ABOVE SEAT 1K INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT ABOVE SEAT 1K, CHECKED GOOD.

Part: SKIN — CORRODED (STA 852-857) · airframe 46,117 hrs · 6,845 cycles

BS 852-857 RBL 83-88 WING CENTER SECTION UPPER FACE BULGE UP. CABIN BS 852-857 RBL 83"-88" WING CENTER SECTION UPPER FACE CORROSION REMOVED OUT OF SRM 57-10-01 ALLOWABLE DAMAGED FIG 101 LIMIT AND CORRODED SKIN AREA REPAIRED AS PER ECRA 5730-02662 REV- AND FORM 44.0008 ATTACHED ITEM 1-14 ACCOMPLISHED.

Part: FLOORBEAM — WORN (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

BS 246 FLOORBEAM LOWER WEB FOUND (1EA) HOLE ELONGATE AT RBL 1.5 INCH. BS 246 FLOORBEAM LOWER WEB ONE HOLE ELONGATE REPAIRED AS PER ECRA 5310-05364 REV AND FORM 44.0008 ATTACHED ITEM 1-9 ACCOMPLISHED (AT BL 0).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

BS 340 LBL 90 FLOOR SUPPORT FOUND CORROSION. L1 DOOR AFT GIRT BAR FITTING FLOOR ATTACHED PLATE ASSY WAS REPLACED AS PER AMM 25-66-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

CABIN BS 347 RBL 45 FLOORBEAM CORRODED. CABIN BS 347 RBL 45 FLOORBEAM UPPER CHORD CORROSION REMOVED OUT OFF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND CHORD UPPER CHORD REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

FS 412 LBL 20 FLOOR SUPPORT FOUND CRACKED CABIN CRACKED SEAT TRACK. REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02 AT BS 340-423 LBL 20 AND FORM 44.0008 ATTACHED ITEM 1-8 ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

BS 340 RBL 90 FLOOR SUPPORT FOUND CORROSION. R1 DOOR AFT GIRT BAR FITTING ATTACHED PLATE ASSY WAS REPLACED AS PER AMM 25-66-05 AND ATTACHED FORM 44.0008 ITEM 1 TO ITEM 2 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

FWD CABIN BS 325 LBL 35-40 FLOORBEAM SURFACE CORROSION REVEALED. FWD CABIN BS 325 LBL 35-40 FLOORBEAM UPPER CHORD CORROSION REMOVED OUT OF SRM 53-00-01 ALLOWABLE DAMAGED FIG 101 LIMIT & CORRODED UPPER CHORD REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR AT BS 325 LBL 9 -71 AND FORM 44.0008 ATTACHED ITEM 1-14 ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

BS 297 RBL 89 FLOOR SUPPORT FOUND CORROSION. R1 DOOR FWD GIRT BAR FITTING ATTACHED PLATE ASSY WAS REPLACED AS PER AMM 25-66-05. ATTACH FORM 44.0008 ITEM 1 TO ITEM 2 ACCOMPLISHED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

AFT CABIN BS 1395-1417 RBL 48 FLOOR SUPPORT FASTENER HOLE CRACKED. AS MARKED AFT CABIN BS 1395 - 1417 RBL 48 CRACKED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ATTACHED ITEM 1 ACCOMPLISHED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

AFT CABIN BS 1395-1417 RBL 38 FLOOR SUPPORT FASTENER HOLE CRACKED. AS MARKED AFT CABIN BS 1395-1417 RBL 38 CRACKED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

AFT CABIN BS 1395-1417 RBL 34 FLOOR SUPPORT FASTENER HOLE CRACKED. AS MARKED AFT CABIN BS 1395-1417 RBL 34 CRACKED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ATTACHED ITEM 1 ACCOMPLISHED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 46,117 hrs · 6,845 cycles

AFT CABIN BS 1395-1417 RBL 40 FLOOR SUPPORT FASTENER HOLE CRACKED. AS MARKED AFT CABIN BS 1395-1417 RBL 40 CRACKED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ATTACHED ITEM 1 ACCOMPLISHED.

Part: FITTING — CORRODED (GALLEY) · airframe 46,117 hrs · 6,845 cycles

AFT GALLEY AREAS BS 1614, LBL 45 GALLEY ATTACHED TIE DOWN FITTING HEAVY CORROSION REVEALED. AFT GALLEY AREA BS 1614 LBL 45 GALLEY ATTACHED TIE DOWN FITTING REPLACED AS PER AMM 20-11-00 PAGE 201.

Part: SKIN — CORRODED (CENTER TANK) · airframe 44,599 hrs · 6,648 cycles

SUPPORT TASK - CABIN LT STA 951 LBL 87 BELOW FLOOR (241SF) CTR / FUEL TANK UPPER SURFACE FOUND CORROSION AS MARKED DURING FLIGHT. CONTROL CABLE INSPECTION FORM 44.0008 ATTACHED. CABIN LT STA 951 LBL 87 BELOW CTR FUEL TANK UPPER SURFACE. CORROSION REMOVED OUT OF SRM 57-10-01 ALLOWABLE DAMAGE 1 FIG 101. LIMIT AND CORROSION REMOVED AREA REPAIRED AS PER ECRA5730-02637. REV- AND FORM 44.0008 ITEM1-24 ACCOMPLISHED.

Part: SEAL — DIRTY (SLIDING WINDOW) · airframe 36,922 hrs · 5,616 cycles

EXCRUCIATINGLY LOUD, VERY HIGH PITCHED, SQUEAL BEGAN WHILE CLIMBING THROUGH 25000 FT TO 37000 FT LEVEL-OFF. TRIED SEVERAL FIXES NOTHING WORKED. ON RETURN TO AIRPORT, NOISE SLOWLY DIMINISHED BELOW 10000 FT AND STOPPED AT 8600 FT. THOROUGHLY CLEANED R1 WINDOW SEAL AND FRAME, REMOVED DC 4 FROM WINDOW FRAME AND PERFORMED INSIDE AND OUTSIDE PRESSURE LEAK CHECKS IAW AMM 05-51-24. ALL TESTS PASSED. NO CABIN PRESSURE LEAKAGE NOTED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,074 hrs · 5,363 cycles

BS 246 FLOORBEAM FWD SIDE ONE STIFFENER FOUND CRACKED AT RBL 8 BS 246 FLOORBEAM FWD SIDE RBL 8 STIFFENER REPLACED PER SRM 51-10-02 AND FASTENERS INSTALLED PER SRM 51-40-02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,074 hrs · 5,363 cycles

FWD CARGO M/D SEAT TRACK CRACKED AT BS 412 LBL 20. FWD CARGO M/D SEAT TRACK BS 412 LBL 20 REPAIRED PER ECRA 5320-01905.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,074 hrs · 5,363 cycles

CABIN STATION 325 LBL 15 TO LBL 64 FLOOR SUPPORT FOUND CORROSION. CABIN STATION 325 LBL 13 TO LBL 64 FLOORBEAM REPAIRED PER SRM 53-00-01 REPAIR 1 FIGURE 201.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,074 hrs · 5,363 cycles

CABIN STATION 246 FLOORBEAM LBL 40 AFT UPPER MID CHORD FOUND CRACKED. CABIN STATION 246 FLOORBEAM LBL 40 AFT UPPER MID CHORD REPAIRED PER SRM 53-10-51 REPAIR FIG 201 REF ECRA 5310-04838.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,074 hrs · 5,363 cycles

CABIN STATION 303 LBL 15 TO LBL 55 FLOOR SUPPORT FOUND CORROSION. CABIN STATION 303 LBL 38 TO LBL 55 CORROSION REMOVED TREATMENT PER SRM 51-10-02 AND PROTECTED PER SRM 51-20-01 WITHIN SRM 53-00-51 ALLOWABLE DMG 1 LIMIT AND LBL 8 TO LBL 38" FLOORBEAM REPAIRED PER SRM 53-00-01 REPAIR 1 FIG 201.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,074 hrs · 5,363 cycles

BS 246 FLOORBEAM FWD SIDE ONE STIFFENER FOUND CRACKED AT LBL 25. FLOORBEAM LBL 25" FWD SIDE STIFFENER REPLACED PER SRM 51-10-02 AND FASTENER INSTALLED PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 23,439 hrs · 3,726 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 21-36. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 23,439 hrs · 3,726 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 35-55. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIGURE 201.

Part: CABLE — DEFECTIVE (EVAC SLIDE) · airframe 17,753 hrs · 2,876 cycles

THE LT OVERWING SLIDE WAS PARTIALLY DEPLOYED WHILE PERFORMING MAINTENANCE. THE DOOR OPENED BUT, THE SLIDE DID NOT INFLATE. INVESTIGATION FOUND THAT THE LT INFLATION CABLE WAS NOT OPERATING PROPERLY AND IT WOULD NOT ACTIVATE THE INFLATION BOTTLE FOR SLIDE DEPLOYMENT. THE LT OVERWING SLIDE AND INFLATION CABLE WERE REMOVED AND REPLACED IAW MM 25-65-01 AND 25-65-04.