N714SY

Part: RIVET — MISSING (RT WING) · airframe 44,034 hrs · 22,420 cycles

FOUND DURING OTHER MAINTENANCE; 2 MISSING RIVITS AND 2 LOOSE RIVITS ON RT WING FIXED TRAILING EDGE APPROX 31 INCHES FWD OF TRAILING EDGE ONE INCH INBD OF NUMBER 8 FLIGHT SPOILER. REPAIRED.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD P/N DN141A5810-137 HAS CORRODED OR MISSING INSERTS. REMOVED AND REPLACED THROUGH, FLOATING AND GIRT BAR INSERTS AS NEEDED ON FLOOR PANEL P/N 141A5810-137.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 222DF HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED THROUGH, FLOATING AND GIRT BAR INSERTS IN FLOOR PANEL 222DF.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 221EF HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED CORRODED OR MISSING INSERTS.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FORWARD CARGO COMPARTMENT STA 500C TO STA 500D RIGHT SIDE, UPPER FLANGE OF BAFFLE HAS DAMAGED NUT PLATE HOLE. REMOVED DAMAGED INTERCOSTAL AT STA 500C TO STA 500D, RIGHT SIDE, AND INSTALLED NEW INTERCOSTAL 146A7503-6.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FWD CARGO RT Z ANGLE CORRODED IN SEVERAL AREAS FROM STA 500A-500D. REMOVED CORROSION FROM Z-ANGLE, RIGHT SIDE, FROM STA 500A-500D. ORIG 'T' IS .050" WITH A LOSS OF .013" REMAINING 'T' OF .037" IS OUT OF LIMITS. REMOVED EXISTING Z-ANGLE FROM RIGHT SIDE STA 500A--500D. FABRICATED NEW Z-ANGLE. TREATED & PRIMED Z-ANGLE. INSTALLED NEW Z ANGLE ON RIGHT SIDE AT STA 500A-500D.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 147A5810- 17 HAS DELAMINATION AND MISSING OR CORRODED INSERTS. REPAIRED DELAMINATION TO TOP PLY OF FLOOR PANEL 147A5810-17 AND REPLACED INSERTS.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

L-2 CREASE BEAM INNER CHORD HAS SEVERAL AREAS OF CORROSION FROM STA 967-995. REMOVED CORROSION FROM L-2 CREASE BEAM INNER CHORD SURFACE STA 967-945, FOUND ORIG T. 080" WITH .018" REMOVED, .062" REMAINING "OUT OF LIMITS". REMOVED & REPLACED INNER CHORD PNL 147A8540-7.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

F/B 222AF HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED CORRODED OR MISSING INSERTS.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 43,857 hrs · 22,340 cycles

AFT PIT FLOOR PANEL 140BF, CORRODED AROUND FASTENER HOLES. VERIFIED CORROSION ON AFT CARGO FLOOR PANEL 140BF TO BE OUT OF LIMITS. FABRICATED NEW FLOOR PANEL. REPLACED.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 147A5810-344 HAS CORRODED OR MISSING INSERTS. REMOVED AND REPLACED CORRODED OR MISSING INSERTS.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 147A5810-30 HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED MISSING OR CORRODED INSERTS.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD DN 147A5810-23 HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED MISSING OR CORRODED INSERTS.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 221BF HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED THROUGH INSERT, AS NEEDED ON FLOOR BOARD 221BF, REPAIR O/B AFT CORNER OF FLOOR BOARD 221BF.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

R-1 CREASE BEAM INNER CHORD CORRODED AT SEVERAL AREAS STA 290-328. REMOVED "OUT OF LIMITS" R1 CREASE BEAM INNER CHORD AND INSTALLED NEW R1 CREASE BEAM INNER CHORD AS REQ'D.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 222DF HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED THROUGH AND GIRT BAR INSERTS ON FLOOR PANEL 222DF.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

INTERCOSTAL STA 328-312 RBL12 HAS CORROSION AT FLOORBOARD HOLES. REMOVED "OUT OF LIMITS" PANEL BREAK AND INSTALLED NEW PANEL BREAK STA 312-328 RBL 12.

Part: PANEL — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

PANEL BREAK STA294-STA312 RBL 11 CORRODED ON UPPER SURFACE. REMOVED "OUT OF LIMITS" PANEL BREAK AND INSTALLED NEW PANEL BREAK STA 294-312 RBL 11.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 43,857 hrs · 22,340 cycles

CABIN FLOORBOARD 222AF, HAS A FEW SPOTS WHERE FIBERGLASS PLIES HAVE PEELED UP. REPAIRED TOP PLY OF FLOOR BOARD 222AF AS NEEDED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FWD CARGO PIT LT Z ANGLE HAS SEVERAL AREAS OF CORROSION FROM STA 500A-STA 500D. REMOVED CORROSION FROM Z-ANGLE, LEFT SIDE FROM STA 500A-500D. ORIG 'T' IS .050" WITH A LOSS OF .022" AT DEEPEST LOCATION. REMAINING 'T' OF .020" IS OUT OF LIMITS. REMOVED EXISTING Z-ANGLE FROM STA 480+10 TO STA 500D. FABRICATED NEW Z-ANGLE, TREATED, PRIMED & INSTALLED NUT PLATES. INSTALLED NEW Z-ANGLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

INTERCOSTAL STA312-STA328 RBL 31 IS CRACKED AT FASTENER HOLES. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL STA 312-328 RBL.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

NUMBER 1 WINDOW FRAME LEFT SIDE UPPER OUTER CORNER CRACKED. MARKED OUT SIDE AND INTERIOR SIDE WITH BLACK MARKER. REPAIRED LT WINDOW FRAME CRACK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOOR SUPPORT INTERCOSTAL STA 967-986 LBL16 HAS CORROSION AROUND FASTENER HOLES. FOUND CORROSION ON INTERCOSTAL / FLOOR SUPPORT TO BE 100% THROUGH MATERIAL, "OUT OF LIMITS". REMOVED & REPLACED FLOOR SUPPORT.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FWD CARGO R/H Z SHIELD AFT OF DOOR CUTOUT IS CORRODED IN SEVERAL SPOTS FROM STA 490-STA 500A. BLENDED SHIELD, AFT OF CARGO DOOR CUTOUT ON RIGHT SIDE, FROM STA 490-500A. ORIG "T" IS .032" WITH A LOSS OF .006". REMAINING "T" OF .026" IS OUT OF LIMITS. REMOVED EXISTING SHIELD. INSTALLED NEW SHIELD ASSY.

Part: BAFFLE — DAMAGED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FORWARD CARGO COMPARTMENT STA 500A TO STA 500B, UPPER FLANGE OF BAFFLE HAS EXISTING NUT PLATE FASTENER HOLE THAT IS DAMAGED. FABRICATED AND INSTALLED REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

AFT CARGO FRAME STA 767 HAS MULTIPLE DENTS ON FREE FLANGE BETWEEN STR 26L-STR23L. REMOVED DENTS ON FREE FLANGE OF FRAME STA 767 BETWEEN STR 26L-STR 23L AND REPAIRED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,857 hrs · 22,340 cycles

AFT CARGO FLOOR SUPPORT RAIL TRACK CORRODED AROUND SEVERAL FASTENER HOLES FROM STA 795-STA 807 RBL 13. BLENDED CORROSION AND FOUND TO BE 100% MAL. LOSS. AFT CARGO FLOOR SUPPORT RAIL TRACK. REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOOR SUPPORT BETWEEN STA 947-STA 967 LBL 16 HAS CORROSION ON UPPER SURFACE. FOUND CORROSION DAMAGE TO BE 100% THROUGH MATERIAL ON FLOOR SUPPORT STA 947-967 LBL16 "OUT OF LIMITS". REMOVED & REPLACED FLOOR SUPPORT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

INTERCOSTAL STA 277-STA 294 BL0 IS CRACKED AT FASTENER HOLES. REMOVED & REPLACED CRACKED INTERCOSTAL BETWEEN STA 277-294 BL 0.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 147A5810-53 HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED MISSING OR CORRODED INSERTS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

WHILE ACCOMPLISHING FRAME REPAIR AT STA 767 LT NDT FOUND CRACK INDICATIONS IN 2 HOLES IN Z ANGLE COMMON TO STA 767 AND 787. REMOVED Z ANGLE BETWEEN STA 727D-787. LOCATED DRILLED AND INSTALLED NEW Z ANGLE BETWEEN STA 727D 787.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

L-1 CREASE BEAM INNER CHORD CORRODED STA 328-344. REMOVED CORROSION ON L-1 CREASE BEAM INNER CHORD AT STA 328 - 344. VERIFIED MATERIAL LOSS IS .050", ORIGINAL "T" .090, REMAINING "T" .040". "OUT OF LIMITS". REMOVED L-1 CREASE BEAM INNER CHORD. LOCATED AND DRILLED NEW CREASE BEAM. INSTALLED NEW L-1 CREASE BEAM INNER CHORD.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD DN147A-5810-136 HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED MISSING OR CORRODED INSERTS.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

AFT CARGO R/H Z ANGLE HAS EXTRA HOLES AND CORROSION STA 727C. BLENDED CORROSION AND FOUND ORIGIN "T" .050 REMAINING .035". LOSS OF .015" FOUND TO BE OUT OF LIMITS. REMOVED Z ANGLE. FABRICATED AND INSTALLED NEW Z ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOORBEAM STA 328 UPPER SURFACE CORRODED RBL31-RBL50. ACCOMPLISHED FLOORBEAM REPAIR ON UPPER CHORD AT STA 328 RBL. 2.0 TO 58 AS REQ'D.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 147A5810-18 HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED THROUGH INSERTS AS NEEDED. REPAIRED TOP PLY FRAY.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 221CF HAS CORRODED OR MISSING INSERTS. REMOVED AND REPLACED THROUGH INSERTS ON FLOOR BOARD 221CF AS NEEDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOORBEAM STA 967 RBL 16 UPPER FLANGE SURFACE CORROSION. REMOVED CORROSION ON STA 967 FLOORBEAM UPPER FLANGE AT RBL16 ORIG T .125" WITH .023" REMOVED .102" REMAINING "OUT OF LIMITS". REPAIRED UPPER FLANGE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FWD CARGO DOOR CUTOUT LOWER CLOSEOUT SILL WEB IS CORRODED AROUND SEVERAL FASTENER HOLES. REMOVED CORROSION FROM FWD CARGO DOOR CUTOUT LWR CLOSE OUT SILL WEB ORIG"T" 0.045 REMOVED 0.022 REMAINING "T" 0.023 OUT OF LIMITS. REMOVED AND REPLACED SILL WEB.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOORBOARD 221CF UPPER PLY IS DAMAGED. REPAIRED TOP PLY OF FLOORBOARD 221CF.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

STA 986 FLOORBEAM UPPER FLANGE SURFACE HAS CORROSION IN SEVERAL AREAS FROM RBL 44-LBL 44. FOUND CORROSION ON STA 986 FLOORBEAM UPPER FLANGE TO BE "OUT OF LIMITS" 10090 MATERIAL LOSS IN SEVERAL AREAS FROM RBL 44-LBL44. CUT OUT UPPER FLANGE AND REPAIRED.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

AFT CARGO PIT RT Z SHIELD STA 767-795 HAS MULTIPLE SPOTS OF CORROSION. FOUND CORROSION TO BE 100% THROUGH MATERIAL ON RT "Z" SHIELD STA 767-795. REMOVED & REPLACED SHIELD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOORBEAM STA 294 CORRODED ON UPPER SURFACE RBL45. REMOVED CORROSION ON STA 294 FLAP RBL 45 UPPER SURFACE ORIG T .094" WITH .040" LOSS .054" REMAINING OUT OF LIMITS. REPAIRED T-CAP.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD DN 147A5810-28 HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED THROUGH INSERTS AS NEEDED ON FLOOR BOARD PN 147A5810-28. REPAIRED TOP PLY OF FLOOR BOARD PN 147A5810-28.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FWD CARGO AFT BULKHEAD LOWER CENTER FLOOR SUPPORT STA 500D HAS SEVERAL AREAS OF CORROSION FROM LBL15-RBL10. REMOVED LWR CENTER FLOOR SUPPORT AT STA 500D, DUE TO 100% MATERIAL LOSS. INSTALLED NEW FLOOR SUPPORT ANGLE.

Part: PANEL — CORRODED (CARGO BAY) · airframe 43,857 hrs · 22,340 cycles

AFT PIT PANEL 140CF CORRODED AROUND FASTENER HOLES. VERIFIED MATERIAL FOR NEW AFT PIT PANEL 140CF, FABRICATED LOCATED AND DRILLED, COUNTERSINK. APPLIED ALODINE, PRIMER AND CIC TO BOTTOM OF PNL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOOR SUPPORT BETWEEN STA 947-STA 967 RBL 25 HAS CORROSION ON UPPER SURFACE. VERIFIED CORROSION WAS 100% THROUGH MATERIAL AND PART WAS OUT OF LIMITS. REMOVED FLOOR SUPPORT STA 947 - STA 967, RBL 25. VERIFIED NEW PART (P/N 147A5660-3 A-TAG # PP2979. LOCATED AND DRILLED NEW PART. COUNTER SUNK HOLES. INSTALLED NUT PLATES. INSTALLED NEW FLOOR SUPPORT.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 43,857 hrs · 22,340 cycles

AFT PIT FLOOR PANEL 140DF, CORRODED AROUND FASTENER HOLES. FABRICATED NEW AFT PIT FLOOR PNL 140DF, APPLIED ALODINE, PRIMER AND CIC REPLACED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOORBEAM STA 294 HAS CORROSION ON UPPER SURFACE RBL 4-RBL14. REMOVED CORROSION ON STA 294 T-CAP UPPER SURFACE RBL 4-RBL14. ORIG T.094" WITH .040" LOSS .054" REMAINING OUT OF LIMITS. REPAIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

FLOORBEAM STA 947 HAS CORROSION ON UPPER FLANGE SURFACE AT RBL16. REMOVED CORROSION ON STA 947 FLOORBEAM UPPER FLANGE ORIG T. 180" WITH .038" LOSS .142" REMAINING TO BE OUT OF LIMITS. REPAIRED FLOORBEAM UPPER FLANGE.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

AFT CARGO PIT STA 787 RT FRAME SPLICE CORRODED. REMOVED & REPLACED AFT CARGO STA 787 RT FRAME SPLICE P/N 146A1300-3.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 222CF HAS MISSING OR CORRODED INSERTS. REPAIRED FLOOR PANEL 222CF.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 43,857 hrs · 22,340 cycles

FLOOR BOARD 221 DF HAS MISSING OR CORRODED INSERTS. REMOVED AND REPLACED CORRODED INSERTS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

AFT CARGO DOOR CUTOUT LOWER SILL CLOSEOUT WEB IS CORRODED IN SEVERAL AREAS. REMOVED CORROSION FROM AFT CARGO DOOR CUT OUT LWR SILL CLOSEOUT WEB ORIG "T" .050 REMOVED 0.025 REMAINING "T" 0.025 OUT OF LIMITS. REMOVED AND REPLACED WEB.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,857 hrs · 22,340 cycles

STA 992 LBL33-LBL45 "Z" SUPPORT FOR GALLEY WALL IS CORRODED IN SEVERAL AREAS. FOUND CORROSION ON "Z" SUPPORT STA 992 LBL33-LBL45 TO BE 100% THROUGH MATERIAL "OUT OF LIMITS". REMOVED & REPLACED SUPPORT.

Part: REGULATOR — FAILED (NR 1 BLEED SYS) · airframe 38,829 hrs · 19,925 cycles

AT FLIGHT LEVEL 410 NR 1 BLEED TRIP. RAN QRH AND THE TRIP RESET SUCCESSFULLY. 30 SECONDS LATER, THE NR 1 BLEED TRIP OFF LIGHT REILLUMINATED. WE CONTINUED TO RUN THE QRH WITH THE BLEED TRIP OFF LIGHT NOT RESTTING. 30 SECONDS LATER, THE NR 2 BLEED TRIPPED. WE DID AN EMERGENCY DECENT. O2 MASKS DEPLOYED. PERFORMED A BLEED AIR SYS HEALTH OF NR 1 ENGINE IAW AMM 36-11-00-700-801. THE HIGH STAGE REG FAILED THE REVERSE FLOW DIAPHRAM. R & R NR 1 HIGH STAGE REG IAW AMM 36-11-07, R & R THE NR 1 ENGINE 450 AND 390 THERMOSTAT SENSOR IAW 36-11-05. PERFORMED A BLEED AIR SYS HEALTH CHECK OF NR 2 ENGINE IAW AMM 36-11-00-700-801. THE PRECOOLER CONTROL VALVE, PC PRESSURE WAS OUT OF RANGE. R & R THE NR 2 ENGINE PRECOOLER CONTROL VALVE IAW AMM 36-12-02. R & R OXYGEN GENERATORS.

Part: SKIN — DAMAGED (RT WING) · airframe 37,878 hrs · 19,525 cycles

RT WING FIXED L/E JUST INBD OF THE NR 2 PYLON HAS MULTIPLE LOOSE AND SMOKING FASTENERS. R & R FASTENERS ON RT WING L/E INBD OF NR 2 PYLON.

Part: SHIM — MIGRATED (RT WING) · airframe 37,878 hrs · 19,525 cycles

RIGHT WING FIXED L/E WIRING GROMMET SHIM IS MIGRATING OTBD OF FRONT SPAR BS 491. LOOSENED GROMMET AND REPOSITIONED SHIM WASHER THEN RESECURED GROMMET.

Part: BULKHEAD — CRACKED (BS 540) · airframe 37,878 hrs · 19,525 cycles

LOWER BULKHEAD BS 540 JUST BELOW STRINGER 22L, SHOWS A CRACK INDICATION. REPAIRED THE BULKHEAD.

Part: SKIN — DAMAGED (LT WING) · airframe 37,878 hrs · 19,525 cycles

LEFT WING FIXED L/E JUST INBD OF THE NR 1 PYLON HAS MULTIPLE LOOSE AND SMOKING FASTENERS. R & R FASTENERS.

Part: RETAINER — CHAFED (LT MLG WW) · airframe 37,878 hrs · 19,525 cycles

LEFT MLG WHEEL WELL WING DOOR CUTOUT AFT SEAL RETAINER IS CHAFED. R & R MLG LWR T/E SHELF PANEL SEAL AND SEAL RETAINER.

Part: DOOR — GOUGED (APU BAY) · airframe 37,878 hrs · 19,525 cycles

APU COWL DOOR IS GOUGED ON FWD FRAME. R & R FWD FRAME ON APU COWL DOOR.

Part: CHANNEL — DAMAGED (BS 727D) · airframe 37,878 hrs · 19,525 cycles

AFT CARGO BAY NUTPLATE CHANNEL AT BS 727D BETWEEN STR 20R-21R HAS DAMAGE AROUND FASTENER HOLES IN 3 EA LOCATIONS. REMOVED NUT PLATE CHANNEL, RECONTURED 3 EA FASTENER HOLES & REINSTALLED NUT PLATE CHANNEL.

Part: FRAME — GOUGED (BS 747) · airframe 37,878 hrs · 19,525 cycles

AFT CARGO BAY: RT FRAME BS 747 AT STR 25R HAS A GOUGE ON FRAME. REMOVED GOUGE.

Part: INTERCOSTAL — CRACKED (APU DOOR FRAME) · airframe 37,878 hrs · 19,525 cycles

UPON REMOVAL OF THE APU DOOR FRAME, FOUND 1ST INTERCOSTAL RT OF CENTER CRACKED WITH BLOWN OUT HOLE. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, INSTALLED NEW INTERCOSTAL.

Part: STAND OFF — BROKEN (BS 500D) · airframe 37,878 hrs · 19,525 cycles

FWD CARGO BAY AFT SIDE OF VERTICAL LT BULKHEAD SUPPORT BS 500D APPROXIMATELY 4" ABOVE FLOOR HAS BROKEN STANDOFF. R & R BROKEN STAND OFF AT FWD CARGO AFT BULKHEAD LT SUPPORT.

Part: SHIM — MIGRATED (HORIZONTAL STAB) · airframe 37,878 hrs · 19,525 cycles

LEFT HORIZONTAL STABILIZER REAR SPAR SHIMS MIGRATING AT LOWER INBD CORNER. R & R SHIM ON LT HORIZONTAL STABILIZER REAR SPAR.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,878 hrs · 19,525 cycles

FWD LT CLOSET: FWD INBD EMERGENCY LIGHT ASSY DAMAGED. R & R FWD LT CLOSET, FWD INBD EMERGENCY LIGHT ASSY.

Part: RETAINER — CHAFED (RT MLG WW) · airframe 37,878 hrs · 19,525 cycles

RIGHT MLG WHEEL WELL WING DOOR CUTOUT AFT SEAL RETAINER IS CHAFED. REMOVED AND REPLACED RMLG LWR T/E SHELF PANEL FWD SEAL AND RETAINER.

Part: MOUNT — CORRODED (LAVATORY) · airframe 37,878 hrs · 19,525 cycles

FWD LAVATORY HAS THREE MOUNT BLOCKS HEAVILY CORRODED: FWD OTBD, AFT OTBD, AND AFT INBD. R & R THE MOUNT BLOCK ON FWD LAVATORY FWD OTBD, AFT OTBD, AFT INBD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,878 hrs · 19,525 cycles

UPON OPS CHECKS OF FWD ENTRY EMERGENCY LIGHTS: FOUND BATTERY PACK TO BE DEAD AT LOCATION, FWD ENTRY CEILING PANEL LT PACK. R & R BATTERY PACK AT LT FWD ENTRY CEILING PANEL.

Part: SHIM — MIGRATED (LT WING) · airframe 37,878 hrs · 19,525 cycles

LEFT WING FIXED L/E WIRING GROMET HAS A MIGRATING SHIM OTBD OF FRONT SPAR BS 385. LOOSENED GROMMET AND REPOSITIONED SHIM WASHER, THEN RESECURED GROMMET.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,878 hrs · 19,525 cycles

NUMEROUS EMERGENCY LIGHTING STRIPS CRACKED, STAINED, BROKEN. R & R ALL FLOOR PATH LIGHTING STRIPS ON PANEL RACK.

Part: NUT PLATE — BROKEN (BS 500) · airframe 37,878 hrs · 19,525 cycles

FORWARD CARGO COMPARTMENT CEILING SUPPORT HAS A NUT PLATE BROKEN LOOSE AT BS 500 LBL 54. R & R NUT PLATE IAW 51-40-02-0G-0, PARA 4.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 37,878 hrs · 19,525 cycles

AFT CARGO COMPARTMENT, LINER SUPPORT BRACKET IS CRACKED AT BS 727 BULKHEAD RBL 3. R & R SUPPORT BRACKET.

Part: SUPPORT — DAMAGED (BS 500G) · airframe 37,878 hrs · 19,525 cycles

FORWARD CARGO COMPARTMENT ANGLED CEILING SUPPORT HAS A BROKEN NUT PLATE AT BS 500G, +3 RBL 24. R & R NUTPLATE IAW 51-40-02-0G-0, PARA 4.

Part: MOUNT — CORRODED (LAVATORY) · airframe 37,878 hrs · 19,525 cycles

RIGHT AFT LAVATORY HAS ONE MOUNT BLOCKS HEAVILY CORRODED, AFT OTBD AND AFT INBD FWD INBD. REPLACED RT AFT LAV BLOCKS IAW SPM 25-46-99, PGS 128-154.

Part: SKIN — DAMAGED (BS 440) · airframe 37,878 hrs · 19,525 cycles

INCOMING LIGHTNING STRIKE, BLIND FASTENER REQUIRES SKIN REPAIR AFTER UPSIZING HOLE AT BS 440 BETWEEN STRINGERS 8L-9L. REPAIRED SKIN IAW SRM 53-00-01-2R-6.

Part: SKIN — DAMAGED (BS 470) · airframe 37,878 hrs · 19,525 cycles

INCOMING LIGHTNING STRIKE, BLIND FASTENER REQUIRES SKIN REPAIR AFTER UPSIZING HOLE AT BS 470 BETWEEN STRINGERS 7L-8L. REPAIRED SKIN IAW SRM 53-00-01-2R-6.

Part: SWITCH — MALFUNCTIONED (ANTI ICE SYS) · airframe 33,259 hrs · 17,223 cycles

NR 1 ENGINE BLEED TRIP OFF ILLUMINATED FOLLOWED BY NR 2 ENGINE BLEED TRIP OFF. FOLLOWED BLEED TRIP PROCEDURE. FOUND WING ANTI-ICE SWITCH FAILED TO TRIP OFF DURING TAKE-OFF. SYSTEM RESTORED TO NORMAL. CLEANED AND EXERCISED ANTI ICE SWITCH AND TAI SWITCHES. PERFORMED WING ANTI-ICING OPERATIONAL CHECK. SYSTEM OPS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 32,703 hrs · 17,002 cycles

EMERGENCY LIGHTS MOUNTED JUST FORWARD & AFT OF CABIN/FIRST CLASS COAT CLOSET, LENS & BULB ARE BROKEN. R & R COAT CLOSET MOUNTED EMERGENCY LIGHTS. OPS CHECK GOOD.