N828NK

Part: ENGINE — OVERHEATED (NR 1)

SJU - LEFT ENGINE OIL GREATER THAN 170 ON CLIMB-OUT. SHUT ENGINE DOWN PER QRH AND RETURNED TO SJU. REMOVED AND REPLACED NR 1 ENGINE IAW MM 71-00-00 AND W/C 00191. (M)

Part: PROXIMITY SENSOR — DEFECTIVE (LT L/E SLAT) · airframe 34,328 hrs · 20,289 cycles

UPON RETRACTION OF SLATS AND FLAPS, SLAT DISAGREE LIGHT CAME ON AND REMAINED ON UNTIL SLATS RE-SELECTED. AFTER LANDING LIGHT CAME BACK ON WHEN SLAT/ FLAP SELECTED TO UP/RETRACT, AIR RETURN. INSPECTED PROXIMITY SWITCHES AND FOUND SWITCH ON NR 1 SLAT (C) SENSOR, CLEANED AND LUBED NR 1 SLAT PROXIMITY SENSOR AND PERFORMED OPS CHECK- GOOD. T/S FOUND LT WING SENSOR (CT) TARGET BAD, REMOVED AND REPLACED SENSOR AND PERFORMED TEST OF PROX BOX, NORMAL. (K)

Part: COALESCER BAG — DIRTY (A/C BAY)

PBI - FLT 330 - GATE RETURN FOR SMOKE HAZE IN THE CABIN. REMOVED AND REPLACED COALESCER BAG. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 207, RBL 11 INCH FLOOR SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT AT STATION 207, RBL 11, FABRICATED NEW FLOOR SUPPORT, TREATED, PRIMED, TOPCOATED AND INSTALLED FLOOR SUPPORT. (M)

Part: SKIN — CRACKED (FUSELAGE)

FTW - FOUND FUSELAGE SKIN CUTOUT FOR L1 DOOR HOLD OPEN HOOK CRACKED AND GOUGED OUT. BLENDED GOUGE AND REMOVED CRACKED EDGE AT L1 DOOR CUTOUT, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOOR SEAT TRACK CORRODED AT STATION 200-237, RBL 22. REMOVED CORROSION AND SECTION OF TRACK AT STATION 200-237, FABRICATED SECTION OF SEAT TRACK, TREATED, PRIMED AND TOPCOATED, OK TO INSTALL. (M)

Part: ACCESS PANEL — DAMAGED (LT WING)

FTW - FOUND LEFT WING INBOARD BUTTE DOOR INBOARD EDGE, BOTTOM SIDE IS DAMAGED. BLENDED OUT DAMAGE MATERIAL LOSS OUT OF LIMITS, FABRICATED NEW DOUBLER, DRILLED AND LOCATED HOLES. OK TO TREAT, PRIME AND INSTALLED DOUBLER. (M)

Part: SLIDE — FAILED (L1 DOOR)

FTW - FOUND L1 DOOR SLIDE FAILED TO DEPLOY. REPLACED L1 DOOR SLIDE. (M)

Part: WEDGE — DENTED (TE FLAPS)

FTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD WEDGE BOTTOM SIDE HAS DENT WITH FILLER COMPOUND. STRIPPED FILLER COMPOUND DENT OUT OF LIMITS, CUT OUT DAMAGE 1.5 INCH BY 2.5 INCH, FABRICATED FILLER AND DOUBLER, DRILLED HOLES. OK TO TREAT AND PRIME AND INSTALLED REPAIR. (M)

Part: SKIN — DAMAGED (FUSELAGE)

FTW - FOUND FORWARD CARGO DOOR HAS DENT ON LOWER EDGE OF SKIN APPROX .098 INCH DEEP 1.0 INCH DIAMETER. CUT OUT DAMAGED, DENTED SKIN. FABRICATED REPAIR DOUBLER AND FILLER, TREATED AND PRIMED FABRICATED PARTS AND INSTALLED REPAIR. (M)

Part: GIRT BAR — LOOSE (ESCAPE SLIDE)

DTW - FOUND L2 DOOR SLIDE GIRT BAR HOLDING LATCH ON COWL IS LOOSE. INSTALLED OVERSIZE FASTENERS ON L2 DOOR SLIDE GIRT BAR HOLDING LATCH. INSTALLED SLIDE PACK. (M)

Part: COALESCER BAG — CONTAMINATED (CABIN AIR)

LAX - FLT 874 - AFTER TAKEOFF, SMOKE STARTED COMING OT OF THE LEFT AFT LAV, DECLARED AN EMERGENCY AND LANDED ALL ELSE WAS NORMAL. FOUND OIL RESIDUE AT BOTH OF COALESCER BAGS. REMOVED AND REPLACED COALESCER BAGS. OPS AND LEAK CHECK NORMAL. RAN BOTH ENGINES AND RAN BOTH PACKS AT HIGH ENGINE POWER SETTINGS AND NO FAULTS NOTED. OK TO CONTINUE. (M)

Part: RELEASE CABLE — MISINSTALLED (SLIDE PACK)

DTW - FOUND TAIL SLIDE COVER RELEASE CABLES NOT INSTALLED CORRECTLY. INSTALLED TAIL SLIDE COVER RELEASE CABLES PROPERLY. (M)

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,536 hrs · 19,120 cycles

G-4 GALLEY AREA L-2 EXIT SAF-T-GLO SIGN FOUND IN AISLE WAY. INSTALLED NEW EXIT SIGN ASSY. INSTALLED NEW EXIT SIGN ASSY.

Part: CABLE — OUT OF POSITION (TAILCONE)

DTW - FOUND VERIFY TAILCONE SLIDE INSTALLATION. REPOSITIONED KEVLAR CABLE AND TAILCONE COVER STRAP CLIPS. (M)

Part: WIRE — BROKEN (FLAP TO ELEVATOR)

FLL - FLT 262 - AFTER TAKEOFF RETRACTED SLATS, GOT DISAGREE LIGHT. CONFIRMED SLATS DEPLOYED AT 280 KTS OVERSPEED WARNING. ALSO AT LANDING, INDICATIONS WERE 40/40 AND TAKEOFF, GPWS WENT OFF. FOUND FLAP BUSS TO ELEVATOR SERVO FORCE LIMITER CABLE BROKEN. REMOVED AND REPLACED CABLE RUN 208B. (M)

Part: SIGN — BROKEN (CABIN)

FLL - FLT 367 - DURING CABIN INSPECTION, FOUND L-2 DOOR AFT SAF-T-GLO EXIT SIGN DIRTY AND BROKEN. REMOVED AND REPLACED SAF-T-GLO EXIT SIGN AND END CAPS. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MCO - ONE EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT ON PANEL AT LEFT SIDE OF WALKWAY. RELAMPED AND SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT ON PANEL. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MCO - EMERGENCY LIGHTS ABOVE L-2 DOOR AND ON OVERHEAD AT MID F/A STATION INOPERATIVE. SECURED LOOSE CONNECTION O BATTERY PACK FOR EMERGENCY LIGHTS. (M)

Part: OIL SYSTEM — OVERSERVICED (APU)

DIVERTED TO MYR, CRUISE FLIGHT, APU OIL TEMP HIGH ILLUMINATED. FOLLOWED QRH PROCEDURES AND CONSULTED WITH DISPATCH/ DIVERTED TO MYR. FOUND APU OIL OVERSERVICED, DRAINED OIL FROM TANK TO FULL MARK. STARTED APU AND NO FURTHER DEFECTS NOTED. LOADED APU WITH ELECTRICAL AND AIR.

Part: SIGN — DAMAGED (CABIN)

GLO-PATH EXIT SIGNS ARE UNREADABLE AT ALL FOUR OVERWING EXITS AND L2 DOOR. REMOVED AND REPLACED EXIT SIGNS AT ALL FOUR OVERWING EXITS AND L2 DOOR FOR GLO-PATH LIGHTING, AFE-T-GLO. (M)