N619DL

Part: SPAR — DAMAGED (TE FLAP) · airframe 73,763 hrs · 36,304 cycles

DURING SHOP VISIT, GROUND DAMAGE WAS FOUND TO THE OUTBOARD MAIN FLAP FRONT SPAR. THE WEB AND UPPER CHORD WERE DAMAGED. REPAIRED PER ERA 467854-14.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 71,484 hrs · 35,192 cycles

LEFT HYD FAILURE AFTER T/O STT, AA MTC FOUND THE RT RETRACT ACT PRESSURE LINE LEAKING. AA MTC REPLACED SAME LEAK CHECKED GOOD. AA MTC ALSO CHECKED THE CASE DRAIN FILTERS AND DIFFERENTIAL PRESSURE POP OUTS ALL OK.

Part: SKIN — PUNCTURED (BS 620 S16L) · airframe 71,443 hrs · 35,175 cycles

FUSELAGE SKIN PUNCTURED AFT OF STA 620 ABOVE STER 16L. ADJACENT SKIN REPAIR REMOVED AND BOTH CUTOUTS REPAIR WITH A DOUBLER.

Part: LIGHT — SMOKE (LT FWD OVERWING) · airframe 70,448 hrs · 34,719 cycles

DURING PUSHBACK PAX REPORTED SMOKE FROM LEFT FORWARD OVERWING EXIT VERTICAL EMERGENCY EXIT SIGN. F/A USED HALON FIRE EXTINGUISHER. REPLACED LIGHT ASSY CABIN HALON BOTTLE AND PBE. EMERGENCY LIGHTS CK GOOD. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 61,740 hrs · 31,295 cycles

EMERGENCY TRACK LIGHTING INOP AT ROW 30D, 36D, 45D. REPAIRED WIRING AT 3 LOCATIONS.

Part: SHUTOFF VALVE — FAILED (NR 1 ENGINE) · airframe 58,243 hrs · 29,952 cycles

ON TAKEOFF GOT LT ENG BLEED ALERT ON EICAS, AND OFF LIGHT ON OVERHEAD BLEED PANEL. REPLACED LEFT PRSOV.

Part: VALVE — FAILED (RT MLG WW) · airframe 55,436 hrs · 28,777 cycles

ON TAXI OUT, PARKING BRAKE LIGHT AND ANTISKID LIGHTS ILLUMINATED SIMULTANEOUSLY AND WOULD NOT RECYCLE. REPLACED PARKING BRAKE VALVE V41 PER M/M.

Part: COWLING — LEAKING (NR 1 ENGINE) · airframe 55,027 hrs · 28,565 cycles

PANEL UNDER LT ENG FWD COWL OPENED EN ROUTE LGA. FOUND AIR LEAK INSIDE INLET COWL. REPLACED LT ENG NOSE COWL PER MM PERFORMED ENG ANTI-ICE CKS OK.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 50,613 hrs · 26,486 cycles

AT FLT LVL 330 - 40 MILES OUT OF BNA, TOOK 1 BREATH OF FRESH AIR, THE NEXT BREATH WAS FOUL AND TOXIC, SMELL WAS THROUGHOUT CABIN AND COCKPIT. ON GROUND 30 SECONDS SMELL GOT WORSE. EVACUATED A/C. REPLACED PWR WIRE AND L-1 WINDOW ASSY DUE TO HEAT DAMAGE.

Part: COMPUTER — OVERHEATED (AUTO FLIGHT) · airframe 50,252 hrs · 26,316 cycles

CENTER AUTOPILOT DISCONNECTED APPROXIMATELY 1.5 HRS IN CRUISE FLIGHT. THIS WAS FOLLOWED BY NO-LAND 3 AND ELECTRICALINSULATION ACIDIC SMELL IN COCKPIT THEN THROUGHOUT CABIN WITH NO EVIDENCE OF SMOKE. THE SMELL DISSIPATED AFTER 15 MINUTES. THE RIGHT AUTOPILOT WAS ENGAGED WITH NO PROBLEM. FOUND THE CENTER FCC INOP WITH BURNING SMELL. REPLACED SAME. NO OTHER DEFECTS WERE FOUND. RAN MCDP TEST ON NEW FCC. ALL CHECKS WERE NORMAL OK FOR SERVICE

Part: WIRE — BROKEN (ROW 42) · airframe 46,726 hrs · 24,651 cycles

ROW 43, 44, 45 AND AFT LAV E PATH LIGHTS INOP. REPLACED SEAT QUICK DISCONNECT CONNECTOR PER BOEING CH 20 AT ROW 42.

Part: TIRE — FAILED (RT MLG)

CREW REPORTED DURING T/O, POSSIBLE BLOWN TIRE. FOUND UPON ARRIVAL NR 7 TIRE CAP BLOWN AND RT I/B TRAILING EDGE FLAP HAD A 6 INCH CRACK. ALSO, FOUND NR 7 BRAKE WEAR PIN DAMAGED. REPLACED NR 7, 8 TIRE AND NR 7 BRAKE. REPAIRED TRAILING EDGE FLAP PER ERA 367723-14.

Part: LIGHT — INOPERATIVE (ROW 3C & 5C)

ON LAYOVER, FOUND EMERGENCY LIGHTS AT SEATS 3C AND 5C INOP. FOUND LIGHT SOCKETS PULLED OUT OF LENS COVERS. REINSTALLED LIGHT SOCKETS IN LENS COVERS AND SECURED, OPERATIONAL CHECKS GOOD.

Part: PUMP — FAILED (RT HYD SYSTEM)

RT ELECTRIC HYD PUMP EICAS OVERHEAT MSG IN ROUTE. REPLACED RT SYSTEM AC HYD PUMP, PRESSURE AND CASE DRAIN FILTERS. LEAK CHECK AND OPERATIONAL CK OK.

Part: WIRE — BROKEN (CABIN)

FLOOR EMERG TRACK LIGHTING BETWEEN SEAT COLUMN 20C THROUGH 25C INOP. REPAIRED BROKEN WIRE.

Part: EXTINGUISH LINE — BROKEN (CARGO COMPT)

WHILE WORKING EO 6-71146-12AD, FOUND FIRE PROTECTION LINE BROKEN IN HALF FROM RUBBING ON APU DUCT. REPLACED LINE AND LEAK CHECKED LINE (P/N 453N2602-75) IPC REF 26-23-51-02, ITEM 120.

Part: SKIN — CRACKED (NR 2 STRUT)

DFW - FOUND THE NR 2 ENGINE NACELLE STRUT SKIN CRACKED BEYOND THE SECOND STOP DRILL. THE CRACK IS LOCATED AT THE FWD UPPER CORNER ON THE INBD SIDE. THE FIRST STOP DRILL WAS ACCOMP IN 4/1/95 PER ER/A 301481-14. THE SECOND STOP DRILL WAS PERFORMED PER DAL SRM 54-51-01-2-204. THE CRACK NOW EXTENDS BEYOND THE SECOND STOP DRILL AND IS A TOTAL LENGTH OF 2.10 LONG EXCEEDING THE SRM. REPAIR PER DAL SRM 54-51-01-2-203.

Part: OXY MASK — FAILED (LT COCKPIT)

CAPTAINS O2 MASK HEAD STRAP WILL NOT INFLATE. FAILED ON TEST.

Part: TE WEDGE — DELAMINATED (RT LE FLAP)

T/E WEDGE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02.

Part: FOOD CARRIER — DIRTY (GALLEY)

RETURNED AFTER TAKEOFF WITH SMOKE SMELL IN CABIN. FOUND PROBLEM TO BE MASKING TAPE LEFT ON FOOD CARRIER BY CATERER. TAPE GAVE OFF ODOR WHEN MEALS HEATED. NO MAINTENANCE ACTION NECESSARY.

Part: COFFEE MAKER — FAILED (AFT NBR 1)

AFT GALLEY NR 1 COPILOTS SIDE COFFEE MAKER MAKES POPPING SOUND WITH SPARKS FLYING WHEN TURNED ON. CIRCUIT BREAKER DID NOT POP. REPLACED COFFEE MAKER.

Part: MECHANISM — OUT OF ADJUST (R 4 DOOR)

ON DEPARTURE, R-4 DOOR SLIDE WOULD NOT ARM AND FERRIED TO ATL. ADJUSTED DOOR RIGGING PER MM 52-11-0 AND OPERATION NORMAL.

Part: TE WEDGE — BROKEN (NR 6 LE FLAP)

DURING CRUISE, HAD VIBRATION IN CABIN AT ROWS 23 TO 28. FOUND NR 6 L/E SLAT PANEL TRAILING EDGE WEDGE BROKEN OUT AND VIBRATING. ALSO, A SECTION APPROX 10 BY 20 WITH SURROUNDING HONEY COMB DAMAGED. REPLACED SLAT ASSEMBLY FOR RETURN TO SERVICE.

Part: TE WEDGE — DAMAGED (RT LE FLAP)

UPON ROUTINE INSPECTION, T/E WEDGE WAS FOUND DENTED. REPLACED WEDGE AS PER 57-43-02. ALSO, PERFORMED TERMINATING ACTION OF AD 90-23-06 BY INSTALLING T/E WEDGE 114N3003-34.