N715SY

Part: BALLAST — SHORTED (LAV MIRROR LIGHT) · airframe 44,125 hrs · 22,171 cycles

FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR 2L AFT LAV, RAN QRH AND DIVERTED. SHORT FOUND IN MIRROR LIGHT IN THE L2 LAVATORY, COLLARED THE CIRCUIT BREAKER. REMOVED AND REPLACED THE BALLAST. CHECKED GOOD. OK FOR SERVICE.

Part: INSERT — CORRODED (AFT FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 43,576 hrs · 21,957 cycles

FOUND THE FLOOR SUPPORT AT BS 344-328 TO BE CRACKED IN UPPER FWD RADIUS. DRILLED AND INSTALLED A NEW FLOOR SUPPORT.

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 43,576 hrs · 21,957 cycles

COCKPIT R1 WINDOW FRAME DAMAGED AT UPPER OUTBOARD CORNER AFT SURFACE. REPAIRED THE WINDOW FRAME.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAD SEVERAL CORRODED INSERTS. REPAIRED THE INSERTS.

Part: FLOOR SUPPORT — CORRODED (BS 967-986) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 967 TO 986, RBL 16 FLOOR SUPPORT IS CORRODED. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT.

Part: ANGLE — CORRODED (BS 986) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA CREASE BEAM INNER ANGLE CORRODED AROUND SEVERAL FASTENER HOLES COMMON TO BS 986. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED & REPLACED THE CREASE BEAM INNER ANGLE.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 221DF TOP PLY IS DISBONDED. REPAIRED THE FLOOR PANEL UPPER SURFACE.

Part: CREASE BEAM — CORRODED (BS 336) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA, R1 CREASE BEAM HAS AREA OF CORROSION AT BS 336. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED THE CREASE BEAM. LOCATED AND DRILLED A NEW CREASE BEAM AND INSTALLED.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 221BF HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS.

Part: SUPPORT — CORRODED (BS 990-1016) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 990 TO 1016, RBL 32 GALLEY SUPPORT ANGLE HAS CORROSION. BLENDED THE CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE GALLEY SUPPORT ANGLE.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 222BF HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS AND FLOATING INSERTS.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAD SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: INSERT — CORRODED (AFT CABIN) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THROUGH INSERTS,

Part: INSERT — CORRODED (AFT FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 986 FLOORBEAM BL 0 TO LBL 44 HAS CORROSION. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 947.5 TO 967, RBL 16 FLOOR SUPPORT IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED & REPLACED THE FLOOR SUPPORT.

Part: FILLER — MISSING (LT WING SLAT) · airframe 43,576 hrs · 21,957 cycles

LEFT WING, NR 1 SLAT, LOWER TRAILING EDGE SKIN MISSING THE RUB PAD, OR REPAIR PART. CLEANED OUT MISSING FILLER AREA, FABRICATED A NEW FILLER AND BONDED IN PLACE. APPLIED FILLET SEAL AND TOP COATED.

Part: FLOOR SUPPORT — GOUGED (BS 927-947) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 927 TO 947.5, RBL 16, FLOOR SUPPORT IS GOUGED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE FLOOR SUPPORT.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 43,576 hrs · 21,957 cycles

CABIN, FLOOR PANEL 241AF UPPER SURFACE HAD THE PLIES PEELED OFF. FABRICATED A NEW FLOOR PANEL AND REPLACED.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAD SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBEAM — CORRODED (BS 947.5) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 947.5, LBL 6 FLOORBEAM HAS CORROSION AROUND FASTENER HOLE. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF UPPER FLANGE FROM BL 0 - LBL 58 AND REPAIRED.

Part: FLOOR SUPPORT — CORRODED (BS 294-312) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA BETWEEN BS 294.5 AND 312, LBL 12 FLOOR SUPPORT HAS CORROSION. REMOVED AND INSTALLED A NEW FLOOR SUPPORT.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 221DF HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: INSERT — CORRODED (AFT FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: CREASE BEAM — CORRODED (BS 986) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA CREASE BEAM INNER ANGLE CORRODED AROUND SEVERAL FASTENER HOLES COMMON TO BS 986. BLENDED THE CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CREASE BEAM, DRILLED AND INSTALLED NEW CREASE BEAM. PRIMED AND APPLIED CIC.

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA BETWEEN BS 312 AND 328, LBL 12, FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOORBEAM BS 328, RBL 12 TO RBL 52 HAS AREAS OF CORROSION AND SCRATCHES. REMOVED CORROSION AND FOUNDTO BE OUT OF LIMITS. REMOVED DAMAGED UPPER FLANGE FROM BL 0 - RBL 58 AND ACCOMPLISHED REPAIR.

Part: CREASE BEAM — CORRODED (BS 312-344) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA L1 CREASE BEAM HAS AREAS OF CORROSION BETWEEN BS 312 TO 344. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE CREASE BEAM. LOCATED, DRILLED, COUNTER SUNK, APPLIED ALODINE, PRIMED.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 947.5, RBL 6, FLOORBEAM HAS CORROSION AROUND FASTENER HOLES. REMOVED THE CORROSION AND FOUND OUT OF LIMITS. CUT AND REMOVED THE DAMAGED FLOORBEAM TEE FITTING FROM BL 0 - RBL 58. REPAIRED.

Part: INSERT — CORRODED (AFT FLOORBEAM) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA BS 986, RBL 18 TO BL 0 FLOORBEAM HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED THE UPPER FLANGE FROM RBL 58 TO LBL 58 AND REPAIRED.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

AFT WET AREA FLOOR PANEL HAD SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 222CF HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOORBEAM, BS 312, LBL 13 TO LBL 51, HAS AREAS OF CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT AND REMOVED THE FLOORBEAM UPPER FLANGE FROM RBL 22-LBL 58 AND ACCOMPLISHED TEE REPAIR.

Part: FILLER — MISSING (LT WING SLAT) · airframe 43,576 hrs · 21,957 cycles

LEFT WING, NR 4 SLAT, LOWER SURFACE TRAILING EDGE SKIN, MISSING EITHER RUB STRIP OR REPAIR. CLEANED CUT OUT ON LOWER SURFACE AND FOUND IT WAS MISSING A RUB STRIP FILLER. FABRICATED A NEW FILLER, ALODINED AND PRIMED AND BONDED THE FILLER.

Part: FLOOR PANEL — CORRODED (FWD CABIN) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA OB MOST LEFT FLOOR PANEL BS 344 TO 380 (METAL PANEL) HAS AREA OF CORROSION. REMOVED CORROSION BS 344 TO 380, FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOOR PANEL.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 221AF HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOOR PANEL 222AF HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,576 hrs · 21,957 cycles

L1 COCKPIT WINDOW FRAME, UPPER OTBD CORNER OF WINDOW CUTOUT, A .500 INCH CRACK IN FRAME FROM OUTSIDE SURFACE TO INSIDE SURFACE, VERIFIED BY NDT INSPECTION. REPAIRED THE WINDOW FRAME.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,576 hrs · 21,957 cycles

COCKPIT R1 WINDOW FRAME, UPPER OTBD CORNER HAD A .400 INCH CRACK, VERIFIED BY NDT INSPECTION. REPAIRED THE WINDOW FRAME.

Part: FLOORBOARD — DEBONDED (FWD CABIN) · airframe 43,576 hrs · 21,957 cycles

FWD WET AREA FLOORBOARD 221FF TOP PLY IS DISBONDED. REPAIRED THE FLOORBOARD.

Part: SENSOR — FAULTY (TE FLAP) · airframe 41,036 hrs · 20,927 cycles

FLAP ASYMMETRY ON TAKEOFF. FLAPS LOCKED AT 2 DEGREES FLAP POSITION INDICATION SPLIT AT 2 DEGREES. REMOVED AND REPLACED NR 3 FLAP SKEW SENSOR. ACCOMPLISHED FLAP SENSOR FUNCTIONAL CHECK. ALL FLAP SENSOR WITHIN LIMITS. OK FOR SERVICE.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,273 hrs · 19,590 cycles

RIGHT EMERGENCY OVERWING DOOR EXIT LIGHT ON MIDDLE RT OF DOOR DOES NOT WORK. R & R RT EMERGENCY OVERWING DOOR EXIT LIGHT FUSE. OK FOR SERVICE.

Part: TRANSITION PANEL — CORRODED (BS 500-500A) · airframe 37,641 hrs · 19,209 cycles

FORWARD CARGO BAY RT TRANSITION PANEL FROM BS 500 - 500A IS CORRODED. R & R THE TRANSITION PANEL.

Part: STRUCTURE — DENTED (VERTICAL STAB) · airframe 37,641 hrs · 19,209 cycles

VERTICAL STAB L/E LT SIDE APROXIMATELY 4 FEET FROM BOTTOM IS DENTED. REPAIRED VERTICAL STAB L/E LT SIDE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,641 hrs · 19,209 cycles

LEFT OVER WING EMERGENCY EXIT HEADER PANEL LIGHT WILL NOT ILLUMINATE. R & R THE POWER SUPPLY.

Part: DOOR FRAME — CORRODED (LAVATORY) · airframe 37,641 hrs · 19,209 cycles

RIGHT AFT LAVATORY FWD DOOR POST HEAVILY CORRODED UNDER LAVATORY DOORWAY THRESHOLD. REPAIRED RT AFT LAV FWD DOOR POST UNDER DOORWAY THRESHOLD.

Part: DOOR FRAME — CORRODED (LAVATORY) · airframe 37,641 hrs · 19,209 cycles

LEFT AFT LAVATORY AFT DOOR POST HEAVILY CORRODED UNDER LAVATORY DOORWAY THRESHOLD. REPAIRED LT AFT LAV AFT DOOR POST UNDER LAV DOORWAY THRESHOLD.

Part: SUPPORT ANGLE — CORRODED (BS 767-787) · airframe 37,641 hrs · 19,209 cycles

ANGLE UNDER THE RT TRANSITION PANEL IN THE AFT CARGO BETWEEN BS 767 AND 787 HAS SEVERAL AREAS OF CORROSION. R & R THE ANGLE.

Part: FRAME — DAMAGED (BS 727D) · airframe 37,641 hrs · 19,209 cycles

LEFT FRAME IN THE AFT CARGO AT BS 727D HAS DAMAGED FASTENER HOLE. REPAIRED THE FRAME.

Part: STRINGER — CHAFED (BS 1008-1016) · airframe 37,641 hrs · 19,209 cycles

STRINGER 16R BS 1008-1016 HAS CHAFED EDGE ON AFT TOP FLANGE AND BENT AFT BOTTOM FLANGE. CONTOURED BOTTOM FLANGE AND BLENDED CHAFE.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 37,641 hrs · 19,209 cycles

FLOOR SUPPORT IN THE AFT CARGO AT BS 887 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION. R & R NEW FLOOR SUPPORT.

Part: FRAME — CRACKED (BS 540 BULKHEAD) · airframe 37,641 hrs · 19,209 cycles

WHILE PERFORMING INSPECTION OF RT FUSELAGE SKIN LOWER BULKHEAD FRAMES AT BS 540, A CRACK WAS NOTED AT THE AFT ROW SECOND HOLE FROM THE TOP. ACCOMPLISHED REPAIR TO CRACKED HOLE.

Part: TRANSITION PANEL — CORRODED (BS 767-787) · airframe 37,641 hrs · 19,209 cycles

RT TRANSITION PANEL IN THE AFT CARGO BETWEEN BS 767 AND 787 HAS SEVERAL AREAS OF CORROSION. R & R TRANSITION PANEL.

Part: TRANSITION PANEL — CORRODED (BS 727A-767) · airframe 37,641 hrs · 19,209 cycles

RIGHT TRANSITION PANEL IN THE AFT CARGO BETWEEN BS 727A AND 767 HAS SEVERAL AREAS OF CORROSION. R & R RT TRANSITION PANEL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,822 hrs · 18,802 cycles

EMERGENCY LIGHT AT DOOR R2 IS OUT. REPLACED THE LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,142 hrs · 18,461 cycles

EMERGENCY EXTERIOR LIGHT AT DOOR R2 BURNED OUT. R & R LAMP.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 34,823 hrs · 17,817 cycles

FOUND CRACK ON LT HORIZONTAL STABILIZER LOWER SKIN AT L/E STA 138 AT AFT SPAR. REPAIRED THE SKIN.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 33,092 hrs · 16,951 cycles

FOUND EMERGENCY LIGHT ON COAT CLOSET LENS CRACKED. REPLACED FORWARD COAT CLOSET EMERGENCY LIGHT.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 30,732 hrs · 16,041 cycles

EMERGENCY LIGHT LENS ON OUTSIDE OF LAVATORY D BROKEN. REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED NORMAL.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 30,720 hrs · 16,037 cycles

EXIT LIGHT AT DOOR 2L CAME OFF. REPLACED EXIT SIGN. OK FOR SERVICE.

Part: FUEL/OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 30,541 hrs · 15,978 cycles

AFTER ROTATION, LEFT OIL QTY INDICATED ZERO. WHITE ALERT BOX DISPLAYED ON CLIMBOUT. AMBER OIL PRESS ILLUMINATED. OIL TEMP REMAINED NORMAL. REMOVED AND REPLACED FUEL OIL HEAT EXCHANGER ON NR 1 ENGINE. PERFORMED IDLE RUN. LEAK AND OPS CHECKS GOOD.