N827NK

Part: BOLT — LOOSE (EVAC SLIDE)

RT FWD HOLD DOWN STRAP CLIP FOR AFT EVAC SLIDE HAS A LOOSE IB MOUNTING BOLT. TIGHTENED MOUNTING BOLT.

Part: HANDLE — DISCONNECTED (L1 SLIDE)

L1 SLIDE INFLATION CABLE NOT CONNECTED TO MANUAL INFLATION HANDLE. CONNECTED L1 SLIDE INFLATION CABLE TO MANUAL INFLATION HANDLE. (M)

Part: ENGINE — FAILED (NR 2)

ENGINE FAILURE AT 29,000 FT WHEN POWER WAS REDUCED TO CRUISE. ALL PARAMETERS NORMAL ENGINE STARTED TO VIBRATE RT ENGINE OIL PRESS WENT TO 0 SHUT DOWN RT ENGINE RT OIL TEMP WENT TO 166 DEGREES AFTER SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. (M)

Part: BUNGEE CYLINDER — DAMAGED (MLG)

ON FINAL APPROACH, 3 GREEN LANDNG GEAR, THEN AT 500 FEET RT MLG FLICKERED RED, THEN WENT STEADY RED ACCOMPANED BY LANDING GEAR WARNING HORN. FOLLOWED QRH PULLED THEN STOWED EMERGENCY LANDING GEAR HANDLE AFTER GETTING 3 GREEN LIGHT, LANDING UNEVENTFUL. LUBED OVER CENTER LINKS AND REMOVED AND REPLACED MLG BUNGEE CYLINDER, OPS AND LEAK CHECK GOOD ON GEAR SWING. (M)

Part: ACTUATOR — MALFUNCTIONED (MLG)

LGA - FLT 706 - AFTER TAKEOFF, RIGHT MAIN GEAR DOOR LIGHT WOULD NOT GO OUT WITH GEAR UP. JACKED AIRCRAFT FOR THE TROUBLE SHOOTING FOUND MLG ACTUATOR SLOW TO RETRACT ON RIGHT SIDE. REMOVED AND REPLACED RT MLG ACTUATOR. PERFORMED GEAR SWING ALL LIGHTS OUT. OPS CHECK NORMAL. (M)

Part: SENSOR — INOPERATIVE (LATCH)

AFTER TAKEOFF WE GOT AN UNSAFE LIGHT (RED). WE RECYCLED AND IT WENT OUT. (RT MAIN). REMOVED AND REPLACED RT UP AND LATCH SENSOR.

Part: SKIN — DAMAGED (FUSELAGE)

LAS - FLT 1103 - FOUND DAMAGE ON RIGHT SIDE OF A/C AT STATION 522-560 LONGERON 20 DUE TO DAMAGE. FUSELAGE EXTERNAL DOUBLER REPAIR INSTALLED AT FS 503-560, L19R-23R PER FLIGHT VEHICLES DRAWING 53-04162-1 EA 5310-0408. (M)

Part: LANYARD — MISINSTALLED (EVAC SLIDE)

DTW - FOUND R1 SLIDE COVER RELEASE LANYARD INSTALLED INCORRECTLY. CORRECTLY INSTALLED R1 SLIDE COVER RELEASE LANYARD. (M)

Part: CONNECTOR — INOPERATIVE (FIRE LOOP)

FLL - FLT 900 - FIRE WARNING LT ENGINE B-LOOP CONNECTOR P1-863 ON THE NR 1 ENGINE. OPS CHECK GOOD ON THE NR 1 ENGINE FIRE LOOP TEST. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

MCO - EMERGENCY EXIT IDENTIFIER LIGHT FOR AFT CABIN DOOR INOPERATIVE. REPAIRED WIRES FOR EMERGENCY EXIT IDENTIFIER AT AFT CABIN DOORS, OPS CHECK OK. (M)

Part: SLIDE — TORN (L2 DOOR)

LGA - L2 DOOR ESCAPE SLIDE HAS RIP ALONG GIRT BAR HOLDER. REMOVED AND REPLACED L2 EVACUATION DOOR SLIDE. (M)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT)

EXIT IDENTIFIER AT RIGHT FORWARD OVERWING EXIT INOPERATIVE. REPAIRED BROKEN WIRE BEHIND LIGHT ASSEMBLY AT THE RIGHT FORWARD OVERWING EXIT. (M)

Part: DOOR — DELAMINATED (THRUST REVERSER)

THRUST REVERSER S/N 1741, UPPER CLAMSHELL DOOR OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED CLAMSHELL DOOR. (M)

Part: SKIN — DELAMINATED (RUDDER)

FTW - FOUND RUDDER LEFT SIDE LOWER DELAMINATED ON EDGE AND LEFT SIDE FAIRING PAINT CRACK VISABLE TO MATERIAL. REPAIRED DAMGED AREA. REPLACED FLAME SPRAY. (M)

Part: SKIN — LIGHTNING STRIKE (LT WING SLAT)

LT WING NR 5 SLAT HAS LIGHTNING STRIKE AT INBOARD END ON TOP OF SLAT. AFTER FURTHER EVALUATION LIGHTNING STRIKE WAS FOUND TO BE CORROSION. CUT OUT DAMAGED SKIN. FABRICATED REPAIR SKIN AND DOUBLERS. INSTALLED REPAIR SKIN AND DOUBLERS. (M)

Part: FRAME — CORRODED (FUSELAGE)

FOUND FORWARD PIT FRAME AT FS 465 LONGERON 30 CORRODED OUT OF LIMITS. FABRICATED REPAIR ANGLE, FILLER AND DOUBLER. INSTALLED REPAIR ANGLE, FILLER AND DOUBLER. (M)

Part: FLOORBOARD — PEELING (FUSELAGE)

FOUND CABIN FLOORBOARD CENTER STATION 468-541 HAS EDGE DAMAGE AND FLOORBOARD FACESIDE PEELING. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FOUND CABIN FLOORBOARD RIGHT STATION 541-617 CRACKED. FABRICATED CABIN FLOORBOARD. (M)

Part: ISOLATION MOUNT — LOOSE (NR 2 ENGINE)

FTW - FOUND NR 2 ENGINE AFT VIBRATION ISOLATOR INNER RESILIENT ELEMENT HAS .5 INCH AREA OF LOOSE AND UNRAVELING STRANDS. REMOVED NR 2 ENGINE AFT VIBRATION ISOLATOR. INSTALLED NR 2 ENGINE AFT VIBRATION ISOLATOR. (M)

Part: ATTACH ANGLE — CRACKED (RT NACELLE)

FTW - FOUND RT ENGINE UPPER PYLON ATTACH ANGLE CRACKED AT CANT 1500. CUT OUT DAMAGED CRACK. FABRICATED ANGLE DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER REPAIR. (M)

Part: ISOLATOR — OUT OF ADJUST (NR 1 PYLON)

FLL - NR 1 ENGINE/PYLON, FORWARD LOWER ISOLATOR ALIGNMENT MARKS ARE OFF BY .25 INCH. REMOVED AND REPLACED NR 1 ENGNE LOWER FORWARD ISOLATOR. (M)

Part: ODOR — DETECTED (CABIN)

MCO - FLT 1865 - STRONG OIL/BURN SMELL AFTER ROTATION AT LGA-HEAVY RAIN, APU ON, RIGHT CABIN TEMP HOT. STOPPED AFTER APU SHUTDOWN AND RIGHT TEMP TO AUTO. NO FURTHER PROBLEM OR SMELL DURING FLIGHT. INSPECT APU AND ACM'S OIL LEVELS NORMAL AND CLEAN. RAN BOTH PACKS SYSTEMS OFF APU AIR EXTENSIVELY THROUGHOUT TEMP RANGES AND NO OIL SMELL DETECTED. (M)

Part: WARNING SYSTEM — FALSE ACTIVATION (PAX DOOR)

DTW - FLT 777 - FOUND DOOR LIGHT MASTER CAUTION ON TAKEOFF ROLL REJECTED TAKEOFF AT 70 KTS. SELF-TESTED PROXIMITY UNIT AS REQUIRED OPS CHECK GOOD. NO FAULTS DETECTED. INSPECTED DOORS EXTERIOR DOORS, FOR SECURITY, NO DEFECTS NOTED. (M)

Part: RHEOSTAT — FAILED (COCKPIT)

LAX - FLT 709 - FOUND AUTO PILOT NR 1 AND NR 2 DISCONNECTS DURING RIGHT TURNS. ALSO PULSES IN ROLL. OK STRAIGHT AND LEVEL AND LEFT TURNS. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REMOVED AND REPLACED RHEO STAT AND AILERON SERVO DRIVE PER MD-80 MM 22-11-01. SYSTEM OPS CHECKED GOOD PER MD80 MM 22-11-01 AND RTS PER 22-01-05. (M)

Part: RHEOSTAT — FAILED (AILERON SERVO)

DEN - FLT 980 - IN TURN YOKE VERY JERKY, AUTO PILOT DISENGAGES. OK IN LEVEL FLIGHT, NR 2 AUTO PILOT. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REMOVED AND REPLACED RHEOSTAT AND AILERON SERVO DRIVE PER MD-80 MM 22-11-01. SYSTEM OPS CHECKED GOOD PER MD80 MM 22-11-01 AND RTS PER 22-01-05. (M)

Part: SERVO — NOISY (AILERON DRIVE)

ACY - RIGHT TURN WHEN AUTO PILOT ENGAGED AILERON SERVO MAKES GROUND NOISE FROM 0-25. REMOVED AND REPLACED AILERON SERVO DRIVE IAW MM 22-10-01. OPS CHECK NORMAL RTS CHECK PERFORMED IAW MM 22-01-05, OPS CHECK NORMAL. (M)

Part: DRIVE UNIT — CHATTERING (AILERON SERVO)

FLT 594 - MCO - WITH AUTO PILOT ENGAGED, THE YOLK CHATTERS IN RIGHT TURNS. REMOVED AND REPLACED AILERON SERVO DRIVE. PERFORMED SYSTEM CHECK SYSTEM GROUND CHECKED GOOD. ALL IAW MD80 MM SECTIONS 22-11-01 AND 22-01-05. (M)

Part: SENSOR — LOOSE (CARGO DOOR)

LGA - FLT 1865 - IMMEDIATELY INTO TAKEOFF ROLL, AFT CARGO DOOR LIGHT ILLUMINATED IT WENT OUT, THEN FLICKERED WHILE TAXIING. TRANSFERRED TO DIM, AFT CARGO DOOR INDICATION INOP. DOOR FOUND CLOSED AND LOCKED, CREW STATED AIRCRAFT WAS ROLLING AT 40 KNOTS NORMAL BRAKING APPLIED. FOUND HARDWARE LOOSE ON STRIKER TIGHTENED AND ADJUSTED IAW MM CH 52-31-00. (M)

Part: COMPUTER — MALFUNCTIONED (COCKPIT)

FLL - FLT 258 - AUTOPILOT DISCONNECTS IN RIGHT TURNS DFGS NR 2 POSITION. REMOVED AND REPLACED NR 2 DFGC IAW MD80 MM 22-01-01, OPS CHECK GOOD. (M)

Part: SLIDE — DISLODGED (CABIN)

FLL - FLT 258 - SLIDE PACK SEPARATED FROM HOUSING. INSTALLED SLIDE PACK IAW MD80 MM 25-62-00. NO DEFECTS NOTED AT THIS TIME. (M)

Part: SLIDE — OUT OF POSITION (L2 DOOR)

DTW - FOUND L2 DOOR SLIDE PACK FELL OFF DOOR AND GOT DAMAGED. REMOVED AND REPLACED L2 DOOR SLIDE PACK IAW MD80 MM 25-62-00. (M)

Part: SENSOR — MALFUNCTIONED (HORIZ STAB)

DTW - FLT 237 - HORIZONTAL STABILIZER AUDIO SIGNAL IS NOT SOUNDED AND NO VOCAL WARNING IN AUTO PILOT MODE, AND MANUAL IN FLIGHT AND GROUND OPS. REMOVED AND REPLACED HORIZONTAL MOTION SENSOR AND OPS NORMAL AS PER MM 27-40-11. (M)

Part: SERVO — FAULTY (AUTOPILOT SYS)

DTW - ERRATIC AUTO PILOT IN TURN'S WITH DFGS NR 2 AUTO PILOT DISCONNECTED IN TURNS. REMOVED AND REPLACED AILERON SERVO IAW MM 22-10-00, OPS CHECKS GOOD. (M)

Part: SENSOR — FAILED (COCKPIT)

DTW - FLT 237 - FOUND HORIZONTAL STABILIZER AUDIO SIGNAL IS NOT SOUNDED AND NO VOCAL WARNING IN AUTO PILOT MODE, AND MANUAL IN FLIGHT AND GROUND OPS. REMOVED AND REPLACED HORIZONTAL MOTION SENSOR (U10-120) AND OPS NORMAL AS PER MM 27-40-11. (M)

Part: LINE — LEAKING (LT ENGINE)

DIVERT TO CVG AND ENGINE IN FLIGHT SHUT DOWN, LEFT OIL STRAINER CLOG LIGHT CAME ON, LOST OIL QUANTITY AND THEN OIL PRESSURE. OIL QTY WAS ZERO AND OIL PRESSURE WAS 29 PSI AT SHUTDOWN. PERFORMED QRH PROCEDURES. NO OIL PRESSURE AND QUANTITY FOR AT LEAST 10 MINUTES LESS THAN 20 MINUTES. REPLACED OIL LINE FROM GEAR BOX TO OIL PRESSURE TRANSMITTER IPC 79-30-00. PERFORMED ENGINE WINDMILL INSPECTION. PERFORMED ENGINE GROUND UP CYCLE. OIL LINE AND FILTER LEAK CHECK OK. (M)