N710SY

Part: FLAP — DAMAGED (RT WING) · airframe 56,245 hrs · 29,601 cycles

BOTTOM OUTBOARD FLAP AT CANOE 7 OUTBOARD SIDE HAS WEAR AND MISSING PAINT FROM CANOE FLAP SURFACE. WEAR WAS FOUND TO BE ON RIGHT OUTBOARD AFT FLAP LOWER SURFACE ON A PREVIOUS REPAIR DOUBLER THAT IS WORN THROUGH DOUBLER IN THE CRITICAL AREA. DAMAGE IS OUT OF LIMITS. REMOVED RIGHT WING OUTBOARD AFT FLAP. 22. AFTER REMOVAL OF AFT FLAP, FOUND OTBD ROLLERCAM FOLLOWER WORN WITH A FLAT SPOT. INSTALLED NEW FLAP. FIT FAIR RIG CHECK GOOD. RII OF RIGHT WING OUTBOARD AFT FLAP INSTALLATION COMPLETE.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 56,127 hrs · 29,560 cycles

WHEN GEAR HANDLE WAS MOVED FROM UP TO OFF POSITION, NOSE GEAR EXTENDED TO DOWN AND LOCKED POSITION. MX NOTIFIED. PERFORMED FIM TASK AND AMM. MULTIPLE GEAR SWINGS WITH NO FAULTS NOTED. OPS CHECKS GOOD.

Part: STIFFENER — BROKEN (LT WING) · airframe 55,304 hrs · 29,246 cycles

DURING REPAIR OF UPPER LT WING SKIN, FOUND A STIFFINER AT THE WING LE TO PYLON RIB WS 204 WAS BROKEN. REMOVED THE DAMAGED STIFFENER. NDT INSPECTION PERFORMED. NO CRACKS NOTED. INSTALLED THE NEW STIFFENER. OK FOR SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 55,304 hrs · 29,246 cycles

LEFT WING UPPER SURFACE L/E. OTBD OF KRAS 206. THE LAST 18 OTBD AFT RIVETS ARE LOOSE AND WORKING. REMOVE 29 FASTNERS. FOUND L/E SKIN DAMAGED IN THE FORM OF OVERSIZED COUNTER SINKS IN THE SKIN. MOST OBRD FASTNER PULLED THROUGH THE SKIN. REMOVED PNEU. DUCT BY THE REPAIR AREA FOR ACCESS. REMOVED PANEL 431CR TO FOM. REAMED HOLES IN SKIN ONLY TO REMOVE DAMAGE AS NECESSARY. HOLES HAVE BEEN INSPECTED WITH HFEC OPEN HOLE INSPECTION IN SPAR TO VERIFY NO CRACKS AT NOMINAL DIAMETER. SKIN HAS BEEN INSPECTED WITH HFEC SURFACE SCAN TO VERIFY NO CRACKS IN SKIN. NDT PERFORMED. NO CRACKS NOTED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER. REAMED ALL HOLES. CUT OUT DAMAGE AREA. NEEDS HFEC FOR TRIM EDGE AND OPEN HOLE INSPECTION. NDT HFEC PERFORMED ON CUTOUT AND FASTENER HOLES. NO CRACKS. FABRICATED NEW DOUBLER OUT 2024-T42 0.071 NEEDS CHAMFER AND COUNTERSINKING. STARTED TO INSTALL HI-LOCKS. CHAMFERED AND COUNTERSANK DOUBLER. INSTALLED DOUBLER AND FILLER.

Part: MOUNT — CORRODED (AFT LAVATORY) · airframe 54,544 hrs · 28,957 cycles

AFT LAVATORY AFT INBD MOUNT HAD CORROSION EVIDENCE. REPAIRED THE MOUNT.

Part: PLATE — CORRODED (AFT CARGO) · airframe 54,544 hrs · 28,957 cycles

AFT CARGO PANEL "HOCKEY STICK" AND A SPLICE PLATE CORRODED, BOTHSIDE OF PLATES. REMOVED AND REPLACED AFT PIT PANEL HOCKEY STICK AND SPLICE PLATE.

Part: TURNBUCKLE — CRACKED (RT WING) · airframe 54,544 hrs · 28,957 cycles

RIGHT WING TRAILING EDGE TURNBUCKLE BRACKET INBD OF DEFLECTION RIB WAS CRACKED. REMOVED AND REPALCED THE TURNBUCKLE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,092 hrs · 28,728 cycles

R2 DOOR EMERGENCY LIGHT SIGN DOES NOT ILLUMINATE. REMOVED AND REPLACED R2 DOOR EMERGENCY LIGHT POWER SUPPLY. OPS CK'D OK. A/C OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,092 hrs · 28,728 cycles

ON RON CHECK FOUND THE FWD EMG FLOOR LIGHT INOP. DEACTIVATED THE FWD LEFT WIND SCREEN PROX LIGHT. PLACED DEACTIVATION OF LT FWD PROX LIGHT ON GMM/MTI FOR TRACKING PURPOSES. R&R FWD LEFT EMERG LIGHT BATT CHARGER. OP CHKS GOOD. OK FOR SVC, THIS CLEARS MTI/GMM.

Part: CONNECTOR — DISCONNECTED (PROX LIGHT) · airframe 52,517 hrs · 27,864 cycles

ON LT FORWARD WINDSCREEN, LOWER PROXIMITY LIGHT IS INOPERATIVE. CONNECTED EXIT LIGHT BATTERY PACK M1675 CONNECTOR D10750P AND CONNECTED D12350 TO FWD LEFT WINDSCREEN PROXIMITY LIGHT RECEPTICLE D92352. OP CHECKED GOOD. ACFT IS OK FOR SERVICE.

Part: ATTACH FITTING — LOOSE (RT WING SKIN) · airframe 52,080 hrs · 27,696 cycles

RIGHT WING UPPER FIXED TRAILING EDGE PANEL ATTACH FITTING LOOSE. REPAIRED.

Part: CONNECTOR — DEFECTIVE (TE FLAP) · airframe 51,610 hrs · 27,499 cycles

FLAP ASYMMETRY OFF OF "UP" AT GATE. REMOVED AND REPLACED SKEW NR 5 CONNECTOR D11822. COMPLETED FLAP SKEW FUNCTIONAL TEST. OPS TEST NORMAL.

Part: COWLING — DENTED (NR 2 ENGINE) · airframe 50,136 hrs · 26,762 cycles

FOUND DENT AT 7 O'CLOCK POSITION ON NR 2 ENG INLET COWL, 11" X 8" BY .5". DENT OUT OF LIMITS. REMOVE AND REPLACED NR 2 ENGINE INLET COWL.

Part: SEAT TRACK — CORRODED (BS 647) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 647, RBL 24 HAS CORROSION. REMOVED THE CORROSION ON THE SEAT TRACK.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 49,689 hrs · 26,525 cycles

FWD CABIN FLOORBOARD 222DF CORNER IS DELAMINATED. REPAIRED THE FLOORBOARD.

Part: SEAT TRACK — CORRODED (BS 836) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 836, RBL 45 HAS CORROSION. REMOVED CORROSION.

Part: SEAT TRACK — CORRODED (BS 807) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 807, LBL 48 HAS CORROSION. REMOVED CORROSION ON THE SEAT TRACK.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 49,689 hrs · 26,525 cycles

FWD WET AREA FLOORBOARD 222AF HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: CHANNEL — CORRODED (BS 992-1016) · airframe 49,689 hrs · 26,525 cycles

ZEE CHANNEL AT RBL 29 FROM BS 992 - 1016 IS CORRODED. FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED A NEW ZEE CHANNEL. REMOVED AND INSTALLED

Part: SEAT TRACK — CORRODED (BS 663) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 663, RBL 45 HAS CORROSION. REMOVED CORROSION.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

RIGHT HORIZONTAL STABILIZER LOWER SIDE NR 1 RIB STIFFINER CRACKED MARKED. VERIFIED CRACK ON RT HORIZONTAL STABILIZER LOWER SIDE NR 1 RIB STIFFINER. REPAIRED CRACKED.

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 49,689 hrs · 26,525 cycles

RIGHT CREASE BEAM IS CORRODED IN SEVERAL AREAS ON UPPEER SURFACE FROM BS 947+9 - 986+7. REMOVED AND REPLACED THE CREASE BEAM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 49,689 hrs · 26,525 cycles

BS 986 UPPER TEE, FORWARD FLANGE, LOWER SURFACE COMMON TO FASTENER HOLE IS CORRODED AT LBL 30. REMOVED CORROSION.

Part: FLOOR SUPPORT — CRACKED (BS 295-312) · airframe 49,689 hrs · 26,525 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 295.5 - 312, RBL 15. REMOVED & REPLACED THE DAMAGED FLOOR SUPPORT.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 49,689 hrs · 26,525 cycles

FWD CABIN FLOORBOARD 222BF HAS 1 MISSING INSERT AND SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: HINGE FITTING — CRACKED (LT MLG DOOR) · airframe 49,689 hrs · 26,525 cycles

LEFT MLG INBD HINGED DOOR, AFT HINGE FITTING ON INBD DOOR, CRACK IN FITTING AT AFT OTBD ATTACH BOLT HOLE, END OF CRACK MARKED IN BLACK, VERIFIED BY NDT INSP. ACCOMPLISH TASK CARD FOR REPAIRS. R & R -1 & -2 HINGES.

Part: SEAT TRACK — CORRODED (BS 679) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 679 LBL 24 HAS CORROSION. REMOVED THE CORROSION FROM THE SEAT TRACK.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

LT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 142 LOWER CORD HAS ELONGATED FASTENER HOLE. REPAIRED LT HORIZONTAL STABILIZER L/E LOWER SKIN AT STA 142, LOWER CHORD.

Part: FLOORBOARD — DAMAGED (FWD CABIN) · airframe 49,689 hrs · 26,525 cycles

FWD CABIN FLOORBOARD 221GF HAS DAMAGE WHERE INSERT WAS PULLED. REPAIRED THE FLOORBOARD.

Part: SUPPORT BRACKET — BROKEN (FUSELAGE) · airframe 49,689 hrs · 26,525 cycles

LOWER CENTER PANEL SUPPORT BRACKET BROKEN ON RIGHT SIDE. MARKED WITH A DOT. KEELBEAM BETWEEN A/C ACCESS PANELS. REMOVED AND REPLACED LOWER CENTER PANEL SUPPORT BRACKET A/C ACCESS PANEL.

Part: MOUNT — CORRODED (CABIN) · airframe 49,689 hrs · 26,525 cycles

G4 GALLEY CENTER DIVIDER FLOOR MOUNT CORRODED. REPLACED G4 GALLEY CENTER DIVIDER FLOOR MOUNT THAT WAS CORRODED.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA CABIN FLOORBOARD, PN147A5810-288 HAS 3 CORRODED INSERTS. INSTALLED 3 INSERTS.

Part: INSERT — CORRODED (CABIN FLOORBOARD) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA CABIN FLOORBOARD HAS CORRODED INSERTS AND ONE MISSING INSERT. REMOVED & REPLACED THE INSERTS.

Part: CREASE BEAM — CORRODED (BS 967-986) · airframe 49,689 hrs · 26,525 cycles

LEFT CREASE BEAM IS CORRODED IN SEVERAL AREAS ON UPPER SURFACE FROM BS 967+10 - 986+6. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED THE CREASE BEAM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,689 hrs · 26,525 cycles

DURING DVI AND NDT INSPECTION OF LT NR 1 FLIGHT DECK WINDOW FRAME, FOUND FRAME CRACKED AT UPPER OTBD CORNER. VERIFIED WITH HFEC AND MARKED CRACK END IN BLACK. INSTALLED REPAIR. GAINED AND RESTORED ACCESS TO THE LT NR 1 FLIGHT DECK WINDOW FRAME BY REMOVING AND REINSTALLING THE LT NR 4 AND NR 5 WINDOW PLUGS. REMOVED AND REINSTALLED THE L-1 SILL PLATE. PAINTED WINDOW FRAME REPAIR. PERFORMED LT NR 1 WINDOW FRAME CRACK PERMANENT REPAIR. NO PRESSURIZATION LEAKS NOTED.

Part: SEAT TRACK — CORRODED (BS 804) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 804, RBL 45 HAS CORROSION. REMOVED CORROSION.

Part: RIB — DAMAGED (RT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

RIGHT HORIZONTAL STABILIZER LOWER NR 5 RIB HAS BAD HOLE MARKED. CUTOUT DAMAGE HOLE ON RT HORIZONTAL STABILIZER NR 5 RIB. FABRICATED AND INSTALLED REPAIR.

Part: SPAR — DAMAGED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

WHILE ACCOMPLISHING LT HORIZONTAL STABILIZER LOWER SKIN MODIFICATION, FASTENER HOLE IN THE FRONT LOWER SPAR WAS ELONGATED AT STA 142. FASTENER HOLE WAS CLEANED TO A .277" DIA, NDT ACCOMPLISHED WITH NO DEFECTS.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 49,689 hrs · 26,525 cycles

FWD WET AREA FLOORBOARD 221CF HAS CORNER DELAMINATED AND ONE INSERT MISSING. REPAIRED THE FLOORBOARD.

Part: SEAT TRACK — CORRODED (BS 647) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT LBL 45, BS 647 HAS CORROSION. REMOVED CORROSION ON THE SEAT TRACK.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,689 hrs · 26,525 cycles

DURING DVI AND NDT INSPECTION OF RT NR 1 FLIGHT DECK WINDOW FRAME, FOUND FRAME CRACKED AT UPPER OTBD CORNER. VERIFIED WITH HFEC AND MARKED CRACK END IN BLACK. INSTALLED REPAIR. REPAIRED NR 1 RT FLIGHT DECK WINDOW AT UPPER OTBD CORNER. REMOVED AND REINSTALLED THE RT NR 1 FLIGHT DECK WINDOW PLUGS. CABIN PRESSURE LEAK CHECK GOOD.

Part: RIB — DAMAGED (RT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

ELONGATED HOLE ON RIB 120.3 OUTBOARD LOWER FLANGE RT. REPAIRED ELONGATED FASTNER HOLE ON RT HORIZONTAL STAB AT RIB STA 120.3.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 49,689 hrs · 26,525 cycles

BS 986 FLOORBEAM UPPER TEE PREVIOUS REPAIR IS CORRODED AT SEVERAL AREAS ON UPPER AND LOWER SURFACES FROM LBL 14 TO RBL 45. REPAIRED.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA FLOORBOARD, PN 147A5810-171 HAS 4 CORRODED INSERTS. R & R 4 EA DAMAGED INSERT IN PANEL 3-147A5810-171.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

WHILE ACCOMPLISHING LT HORIZONTAL STAB LOWER SKIN MODIFICATION, CRACK FOUND AT FASTENER HOLE ON RIB, STA 138.7, 12" FROM AFT SPAR ON THE OTBD HORZ FLANGE. DAMAGE HAS BEEN REMOVED AND 4 FASTENERS ON EITHER SIDE OF THE CUTOUT HAS BEEN NDT FOR CRACKS WITH NO DEFECTS. REPAIR COMPLETED.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 49,689 hrs · 26,525 cycles

FWD WET AREA FLOORBOARD 221BF RT CORNER IS DELAMINATED. REPAIRED THE FLOORBOARD.

Part: FLOORBOARD — DELAMINATED (CABIN) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA CABIN FLOORBOARD HAS MINOR DELAMINATION ON TOP. REPAIRED THE FLOORBOARD.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA FLOORBOARD, PN147A58140-76 DELAMINATED AND FIBERS SHOWING. REPAIRED AFT WET AREA FLOORBOARD, PN 147A58140-76.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

LEFT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 138.7 28" AFT LOWER RIB FLANGE OTBD FASTENER HOLE CRACKED. REPAIRED LT HORIZONTAL STABILIZER L/E LOWER SKIN STA 138.7, 28" AFT LOWER RIB FLANGE OTBD FASTENER.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

LEFT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 138.7 AFT 4" LOWER RIB FLANGE HAS ELONGATED OTBD HOLE. REPAIRED LT HORIZONTAL STABILIZER L/E LOWER SKIN AT STA 138.7, AFT 4" LOWER RIB FLANGE ELONGATED FASTENER HOLE.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA FLOORBOARD HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS.

Part: SEAT TRACK — CORRODED (BS 648) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 648, RBL 45 HAS CORROSION. REMOVED CORROSION.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

LEFT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 138.7, 18" AFT LOWER RIB FLANGE INBD ROW FASTENER HOLE ELONGATED. REAMED HOLE TO FINAL SIZE OF .193 HOLE CLEAN AND ROUND. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,689 hrs · 26,525 cycles

EMERGENCY LIGHT BATTERY PACKS INOPERATIVE. BASE CHARGER FOR BATTER PACK REMOVED AND REPLACED. OPS CHECK ACCOMPLISHED. OPS CHECKED GOOD. REPLACED THE BATERY PACK. TESTED GOOD.

Part: SEAT TRACK — CORRODED (BS 682) · airframe 49,689 hrs · 26,525 cycles

SEAT TRACK AT BS 682, LBL 45 CORRODED. REMOVED CORROSION ON THE SEAT TRACK.

Part: STRAP — CORRODED (BS 1016) · airframe 49,689 hrs · 26,525 cycles

AFT WET AREA FLOOR STRAP AT RBL 18 IS CORRODED AT AFT AT BS 1016 FLOORBEAM. REMOVED COCRROSION, NDT VERIFIED ORIG. THICKNESS .071" REMAINING = .056" LOSS OF .015", FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED AND DRILLED NEW STRAP.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 49,689 hrs · 26,525 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 277 - 294.5 AT BL 0. REMOVED AND REPLACED THE FLOOR SUPPORT.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 49,689 hrs · 26,525 cycles

KEELBEAM FORWARD AREA LT SIDE EYE BOLT CORRODED. R & R KEELBEAM FORWARD AREA LT SIDE EYE BOLT WITH NEW.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 49,689 hrs · 26,525 cycles

LEFT HORIZON STABILIZER L/E LOWER SKIN, STA 157, 7"AFT INBD FASTENER ROW HAS ELONGATED HOLE. REMOVED HOLE TO FINAL SIZE OF .193. HOLE CLEAN AND ROUND. NO DEFECTS NOTED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,373 hrs · 26,001 cycles

R 1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER. OK FOR SERVICE.

Part: SKIN — DAMAGED (NR 7 SLAT) · airframe 47,996 hrs · 25,836 cycles

FOUND HOLE ON BOTTOM FLEX SKIN ON NR 7 SLAT. DAMAGE IS LOCATED APPROXIMATELY 58" INBD OF OUT EDGE OF SLAT. RT BEHIND PANEL 624DB. REMOVED DAMAGED AREA AND STOPPED DRILLED 1 CRACK.

Part: UNKNOWN — CRACKED (BS 727B) · airframe 47,514 hrs · 25,648 cycles

CRACKED INBD AND OTBD FLANGE FS 727B, RBL 45.5. CUTOUT DAMAGE, HFECD FLAP PEENED, FABRICATED PARTS AND INSTALLED.

Part: LINK — CRACKED (RAM AIR DOOR) · airframe 47,514 hrs · 25,648 cycles

INBD CONNECTING LINK FOR LT RAM AIR DOOR FOUND TO BE CRACKED. R & R LT RAM AIR AFT DOOR LINK.

Part: SKIN — CRACKED (BS 540) · airframe 47,514 hrs · 25,648 cycles

A CRACK WAS NOTED AT THE 2ND HOLE FROM THE TOP, AFT ROW, AND IN THE SKIN ONLY. REAMED HOLE IAW EA FS 540, LT STR 22L.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 46,634 hrs · 25,246 cycles

FIRST 5 FLOOR TRACK EMERGENCY LIGHTS ARE NOT WORKING DURING TEST. FOUND 1 LOOSE WIRE AT RECEPTACLE. RESECURED WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,102 hrs · 24,602 cycles

BS 360 EMERGENCY LIGHTS INOPERATIVE. R & R THE LIGHT ASSY.

Part: LIGHT — DAMAGED (SEAT 24C) · airframe 44,986 hrs · 24,506 cycles

EMERGENCY TRACK LIGHT AT SEAT 24C DAMAGED. INSTALLED NEW LIGHT ASSY & LENS. REPAIRED BROKEN WIRING.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,190 hrs · 24,210 cycles

FLOOR LIGHTING AT ROW 22 NOT WORKING. REPLACED THE LAMP.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 43,901 hrs · 24,102 cycles

LEFT OVERWING EMERGENCY EXIT COVER MISSING. REPLACED LIGHT ASSY.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 43,564 hrs · 23,960 cycles

FLOOR EMERGENCY LIGHT AT ROW 24 IS MISSING COVER. ATTACHED EMERGENCY LIGHT COVER.

Part: BULB — INOPERATIVE (SLIDE LIGHT) · airframe 41,396 hrs · 23,020 cycles

FORWARD LEFT EMERGENCY SLIDE LIGHT DEFECTIVE. R & R BULB.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 40,633 hrs · 22,657 cycles

EMERGENCY LIGHT CONNECTOR DISCONNECTED. CONNECTED CONNECTOR, OPS CHECKED GOOD.

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 40,631 hrs · 22,656 cycles

FLIGHT DECK LT WINDOW FRAME NR 3 CRACKED AND OUT OF LIMITS AND REQUIRES REPLACEMENT. R & R FLIGHT DECK LT NR 3 WINDOW FRAME.

Part: SEAT TRACK — CHAFED (BS 727-727B) · airframe 40,631 hrs · 22,656 cycles

RIGHT OTBD SEAT TRACK HAS SEVERAL CHAFE MARKS BETWEEN FS 727 TO FS 727B IN CABIN. REMOVED CHAFE FROM RT OTBD SEAT TRACK. R & R SEAT TRACK AT RBL 45.50 FROM STA 727B-887.

Part: FLOORBEAM — CORRODED (BS 947.5) · airframe 40,631 hrs · 22,656 cycles

TRANSVERSE FLOORBEAM AT STA 947.5 UPPER SURFACE CORRODED BETWEEN LBL 24.75 AND RBL 24.75. REPAIRED FLOOR UPPER CORD AT STA 947.50.

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · airframe 40,631 hrs · 22,656 cycles

AFT CARGO BAY CORROSION AT DOOR THRESHOLD WEB. R & R WEB.

Part: FLOOR SUPPORT — CORRODED (BS 887) · airframe 40,631 hrs · 22,656 cycles

FLOOR SUPPORT AT BS 887 IN AFT CARGO BAY CORRODED. R & R FLOOR SUPPORT.

Part: ANGLE — CORRODED (BS 989) · airframe 40,631 hrs · 22,656 cycles

CANTILEVER FLOOR OTBD RT SHEAR WEB UPPER LONGITUDINAL ZEE ANGLE CORRODED AT STA 989, OTBD OF RBL 27.95. FABRICATED NEW ZEE ANGLE. ZEE ANGLE REMOVED AND INSTALLED.

Part: SUPPORT — CORRODED (BS 727C-767C) · airframe 40,631 hrs · 22,656 cycles

FLOOR TO SIDEWALL SUPPORT HAS SURFACE CORROSION IN AFT PIT FROM FS STA 767C TO FS 727C. R & R FLOORBOARD TO SIDEWALL SUPPORT IN AFT PIT FROM STA 767C TO FS 727C.

Part: INTERCOSTAL — CORRODED · airframe 40,631 hrs · 22,656 cycles

FOUND CORROSION AROUND NUTPLATE HOLES ON INTERCOSTAL BS 747 TO 767, RBL 23. R & R INTERCOSTAL.

Part: SHEAR WEB — CORRODED (BS 986) · airframe 40,631 hrs · 22,656 cycles

CANTILEVER FLOOR OTBD RT SHEAR WEB CORRODED AT STA 986.5. ORDERED NEW WEB AND DRILLED UP WEB. REMOVED AND INSTALLED.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 40,631 hrs · 22,656 cycles

AFT CARGO NR 1 FLOOR PANEL HAS BARE METAL ON LOWER ATTACH AREAS AND LIGHT CORROSION ON UPPER SURFACE ATTACH AREAS. FABRICATED NEW FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL CTR BS 887-947 HAS PEELING FIBERS AND CORRODED INSERTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL RT OTBD BS 887-946 HAS DAMAGED AND CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL LT BS 986-1016 HAS CORRODED INSERTS. DAMAGED INSERTS, POTTED INSERTS NOT FLUSH WITH TO OF PANEL, AND EDGE DAMAGE NEAR GALLEY MOUNT CUTOUTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL RT BS 1016 TO AFT PRESSURE BULKHEAD HAS PEELING FIBERS AND TOOL DAMAGE. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL LT BS 1016 TO AFT PRESSURE BULKHEAD HAS PEELING FIBERS AND CORROSIVE RESIDUE ON BOTTOM SIDE OF PANEL. REPAIRED FLOOR PANEL .

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL RT BS 986-1016 HAS CORRODED INSERTS. DAMAGED INSERTS. POTTED INSERTS NOT FLUSH WITH OTP OF FLOOR PANEL, AND EDGE DAMAGE TO FLOOR PANEL NEAR GALLEY MOUNT CUTOUTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL RT INBD STA 887-946 HAS CORRODED, DAMAGED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL CTR BS 946-986 HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 40,631 hrs · 22,656 cycles

AFT WET AREA FLOOR PANEL LT BS 917-946 UNDER LAV HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "D" HAS PEELING FIBERS AND CORRODED INSERTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "K" HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "A" HAS CORRODED INSERTS, SURFACE DAMAGE TO LOWER SIDE, AND EDGE DAMAGE. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FORWARD WET AREA, FLOOR PANEL "C" HAS EDGE DAMAGE AND CORRODED INSERTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "I" HAS CORRODED INSERTS AND PEELING FIBERS AND DIRTY POTTED INSERTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "J" HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "G" HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "B" HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "H" HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "F" HAS CORRODED INSERTS, PEELING FIBERS, AND BAD POTTED INSERTS. REPAIRED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 40,631 hrs · 22,656 cycles

FWD WET AREA FLOOR PANEL "E" HAS CORRODED INSERTS AND PEELING FIBERS. REPAIRED FLOOR PANEL.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 40,631 hrs · 22,656 cycles

VERTICAL STAB L/E PANEL 322B ASSY HAS THREE INTERNAL RIBS CRACKED, RIBS 6, 7, 8 FROM TOP DOWN. REPAIRED AND INSTALLED NR 6 VERT STAB INTERNAL RIB. INSTALLED NR 7, NR 8 VERT STAB INTERNAL RIBS.

Part: ANGLE — CORRODED (BS 992) · airframe 40,631 hrs · 22,656 cycles

CANTILEVER FLOOR OTBD LT SHEAR WEB UPPER TRANSVERSE ZEE ANGLE CORRODED AT STA 992.8, OTBD OF LBL 27.95. R & R SECTION 47 CANTILEVER FLOOR OTBD LT SHEAR WEB UPPER TRANSVERSE ZEE ANGLE.

Part: SKIN — CHAFED (NR 5 SLAT) · airframe 40,631 hrs · 22,656 cycles

RT WING SLATS NR 5 ARE CHAFED ON AFT LOWER SURFACE. REPAIRED SLAT NR 5 AFT LOWER SURFACE AREAS.

Part: SKIN — CHAFED (NR 7 SLAT) · airframe 40,631 hrs · 22,656 cycles

RT WING SLAT NR 7 CHAFED ON AFT LOWER SURFACE. REPAIRED SLAT.

Part: SKIN — CHAFED (NR 8 SLAT) · airframe 40,631 hrs · 22,656 cycles

RT WING NR 8 SLAT CHAFED ON AFT LOWER SURFACE. REPAIRED RT NR 8 SLAT CHAFE ON LOWER SURFACE.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 37,204 hrs · 23,752 cycles

AFT CARGO NR 3 FLOOR PANEL HAS LIGHT CORROSION ON BOTTOM & TOP ATTACH AREAS. FABRICATED FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 37,204 hrs · 23,752 cycles

AFT CARGO NR 2 FLOOR PANEL HAS LIGHT CORROSION ON LOWER SURFACE ATTACH AREAS. FABRICATED AND TREATED FLOOR PANEL.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 40,405 hrs · 22,554 cycles

EXIT ROW 13 PLASTIC EXIT SIGN OFF THE WALL. INSTALLED ROW 13 EXIT SIGN COVER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,587 hrs · 21,005 cycles

FOUND SEVERAL SPOTS OF HEAVY CORROSION IN AFT PIT ZEE CHANNEL SIDEPLATE, LEFT SIDE, FROM FACTOR SPLICE AT STA 727B+10 TO FACTORY SPLICE AT STA 817.

Part: LIGHT — BROKEN (ROW 8) · airframe 29,828 hrs · 18,488 cycles

EMERGENCY ESCAPE PATH LIGHT ASSY. BROKEN ROW 8. R & R LIGHT ASSY IAW AMM 33-51-12-96-802. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,326 hrs · 17,568 cycles

EXTERIOR EMERGENCY LIGHT INOP LEFT SIDE, AFT OF WING. RELAMPED LIGHT, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,117 hrs · 17,131 cycles

DURING A FUNCTIONAL CHECK MAINTENANCE DISCOVERED THE AFT PASSENGER DOOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LAMP AND THE OPERATIONAL CHECK IS NORMAL.