N822NK

Part: SLIDE — DETACHED

FWD ENTRY DOOR SLIDE PACK CAME OFF. REINSTALLED SLIDE PACK. (K)

Part: CONTROL VALVE — WARPED (LT MLG)

BRAKES WERE SPONGY AND SLOW TO STOP AC. REMOVED AND REPLACED LT POWER BRAKE CONTROL VALVE ASSY. (K)

Part: ACTUATOR — LEAKING (RT MLG)

RT MLG ACTUATOR SWIVEL GLAND LEAKING, AC TAIL SWAP WITH N815NK. RESEALED RT MLG ACTUATOR SWIVEL GLAND, NO LEAKS NOTED. (K)

Part: SEAL — LEAKING (ACM DUCT)

TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF, AIR RETURN BACK TO FLL AND AIRCRAFT TAIL SWAP WITH N815NK. REMOVED AND REPLACED SEALS ON LEFT AND RIGHT ACM DUCTS, SECURED TWO LOOSE CLAMPS, RAN ENGINES AT ALL PARAMETERS. OPS AND LEAK CHECKS GOOD. (M)

Part: STUD — STRIPPED (NR 2 GEARBOX)

NR 2 ENGINE USED 4 QUARTS OF OIL DURING FLT NR 931, AIRCRAFT TAIL SWAP WITH 830. FOUND ENGINE OIL FILTER COVER LEAKING. REPLACED 3 HELI-COILS FOR THE PULLED OUT STUDS ON THE GEARBOX, NO LEAKS NOTED ON ENGINE RUN. (M)

Part: GASKET — DAMAGED (A/C PACK)

FLL - FLT 758 - AFTER TAKEOFF AT 800 FEET, THE TAIL COMPARTMENT OVERTEMP LIGHT CAME ON, FOLLOWED QRH PROCEDURES THE LIGHT WENT OUT WHEN THE LEFT THROTTLE WAS PLACED IN IDLE. THE LIGHT CAME BACK ON WHEN THE THROTTLE WAS RETURNED ABOVE 1.5 EPR, THE LIGHT WENT OUT WHEN THROTTLE WAS REDUCED BELOW 1.4 EPR, RETURNED TO FLL ON REDUCED POWER. INSPECTED THE PNEUMATIC DUCTING ON THE LEFT SIDE TAIL COMPARTMENT AND DETERMINED THE PACK INLET HIGH TEMP SENSOR GASKET WAS DAMAGED. REMOVED AND REPLACED SENSOR GASKET, OPS CHECK GOOD. (M)

Part: UPLOCK SENSOR — MALFUNCTIONED (LT MLG)

DTW - FLT 706 - DURING CLIMB, AFTER RETRACTION LEFT GEAR UNSAFE LIGHT. REMOVED AND REPLACED LEFT MLG UP AND LATCH SENSOR P/N 833605, PROX BOX P/N 833703 AND PROX SWITCH. (M)

Part: B-NUT — LEAKING (HYD SYSTEM)

FLT 1153 - VERTY STRONG ODOR OF OIL OR SKYDROL THROUGHOUT THE CABIN AND COCKPIT DURING CRUISE. FOUND HYDRAULIC FLUID LEAKING FROM LINE IN AFT PIT LEFT WALL. FLUID DRAINED ON BOTTOM OF FUSELAGE AND WENT INTO APU INLET AND FUMES FROM FLUID WENT INTO RECIRC FAN IN AFT PIT. TIGHTENED B-NUT ON LINE. LEAK CHECK GOOD. THIS CLEARED ODOR IN CABIN. NO FURTHER DEFECTS NOTED. (M)

Part: CONTACTOR — LOOSE (BATTERY)

DTW - FOUND LEFT AND RIGHT FORWARD PLUG DOOR EMERGENCY LIGHT INOPERATIVE. CLEANED BATTERY CONTACTS. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

RSW - FLT 1504 - SLIDE PACK L-1 DOOR CAME OFF AS THE DOOR WAS OPENED IN ORD. REINSTALLED L-1 DOOR SLIDE PACK AND COVER. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

FLT 223 - ORD - ON TAXI OUT, FOUND L1 SLIDE PACK FELL OUT OF COVER. REINSTALLED SLIDE PACK ADJUSTED LOWER LATCH AND CLIP MECH. (M)

Part: AUGMENT VALVE — DAMAGED (LEFT)

MCO - FLT 940 - DURING THE USE OF ENGINE ANTI-ICE ON, PASSENGER COMPLAINED OF A BAKEOLITE OR OTHER SUBSTANCE, BURNING/OVER HEAT ODOR. REMOVED AND REPLACED LEFT AUG VALVE. (M)

Part: FLOOR PANEL — CRACKED

LT FLOORBOARD STA 927-1003 CORNERS CRACKED. FABED NEW FLOOR PANEL.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE)

CABIN CENTER FLOOR SUPPORT STA 845 BROKEN. REMOVED BROKEN FLOOR SUPPORT. FABRICATED LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1155 LBL 22 TO LBL 44. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED SUPPORT. INSTALLED MAIN CABIN FLOOR SUPPORT.

Part: SLIDE — DAMAGED (TAILCONE)

FTW - FOUND TAILCONE EVAC SLIDE UNPACKED AND MISSING O/H DATE. REMOVED TAILCONE EVAC SLIDE. INSTALLED TAILCONE EVAC SLIDE. (M)

Part: WEB — CRACKED (FUSELAGE)

DENT AT FS 204 BETWEEN LONGERONS 15 AND 17L. DENT IS WITHIN ONE INCH FROM STRUCTURE AND MUST BE REPAIRED. FOUND WEB AT STA 200-207 CRACKED. FABRICATED WEB DOUBLER AND REPAIR FILLER. INSTALLED WEB DOUBLER REPAIR.

Part: SEAT TRACK — WORN (FUSELAGE)

CABIN RT MIDDLE SEAT TRACK WORN AND CORRODED STA 200-1307. MATERIAL LOSS ON RT MIDDLE SEAT TRACK STA 937-1033 OUT OF LIMITS. REMOVED RT MIDDLE SEAT TRACK. LOCATED AND DRILLED RT MIDDLE REPLACEMENT SEAT TRACK STA 937-1033 AND SPLICE. INSTALLED RTMIDDLE SEAT TRACK.

Part: SEAT TRACK — WORN (FUSELAGE)

CABIN LT IB SEAT TRACK WORN AND CORRODED STA 200-1307. STA 935 TO 1117 AND STA 1200 OUT OF LIMITS. REMOVED SEAT TRACK AND SPLICES STA 915-1090 AND 1184-1221. INSTALLED SEAT TRACK AND SPLICES STA 1184-1221. INSTALLED SEAT TRACK AND SPLICES STA 915-1090.

Part: SKIN — DAMAGED (RT ELEVATOR)

RT ELEVATOR LOWER SKIN IS CREASED. CUT OUT DAMAGED AREA OF LOWER SKIN AT RT ELEVATOR (9.5 X 18.5) FABRICATED FINGER DOUBLERS AND SKIN FILLER. INSTALLED REPAIR PARTS.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FOUND CENTER AILSE FLOOR PANEL APPEARS TO BE SPONGY BETWEEN SEAT ROW 16 AND 17. REINFORCED FLOOR PANEL. (M)

Part: SLIDE — UNLATCHED (L1 DOOR)

DTW - FLT 709 - SLIDE PACK FELL OFF DOOR WHEN DOOR SHUT FOR PUSH-LATCH CAME UNDONE. FOUND SLIDE PACK STILL INSTALLED, LATCH CAME UNDONE. RELATCHED, NO OTHER DEFECTS NOTED. (M)

Part: SLIDE — OUT OF POSITION (L1 DOOR)

DTW - FLT 417 - L1 SLIDE PACK FELL FROM DOOR. REINSTALLED SAME SLIDE PACK A REQUIRED. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

LAS - FLT 1108 - L1 DOOR SLIDE PACK HAS SLIPPED DOWN OUT OF ITS JACKET. REINSTALLED SLIDE L-1 DOOR. (M)

Part: COVER — OUT OF ADJUST (L1 DOOR)

FLL - FLT 702 - FOUND L1 DOOR SLIDE LOOSE. ADJUSTED L1 DOOR SLIDE COVER. OK FOR SERVICE. (M)

Part: COFFEEMAKER — NOT SEATED (GALLEY)

DTW - FLT 1874 - FLIGHT ATTENDANT REPORTED A SPARK FROM AFT COFFEE MAKER CB WHEN PULLED. RESEATED COFFEE MAKERS AND PERFORMED. OPS CHECK, NO DEFECTS NOTED AT THIS TIME. (M)

Part: SLIDE — DISLODGED (L1 DOOR)

MCO - FLT 1913 - L1 SLIDE FELL OUT OF DOOR PANEL. RE-INSTALLED L1 SLIDE PACK AND COVER. (M)

Part: LANYARD — DETACHED (ESCAPE SLIDE)

FLL - FLT 1443 - L1 SLIDE PACK NEEDS TO BE ATTACHED. REINSTALLED L1 SLIDE PACK LANYARD. (M)

Part: LANYARD — DISCONNECTED (L1 SLIDE PACK)

LGA - FLT 381 - L1 DOOR SLIDE PACK LANYARD IS NOT ATTACHED. RE-INSTALLED L1 DOOR SLIDE PACK LANYARD. NO DEFECTS NOTED. (M)

Part: COALESCER BAG — ODOR (AIR CONDITIONING)

CABIN AIR SMELLS LIKE BURNT OIL WHEN MIX VALVES MOVE TOWARD MID RANGE WARM OR HOT. REMOVED AND REPLACED AIR CONTIONING COALESCER BAGS. INSPECTED ACM OIL LEVEL CK GOOD. RAN PACKS, NO ABNORMAL ODORS NOTD, OK FOR SERVICE. (M)

Part: ACOUSTIC LINER — MISSING (ENGINE)

NR 1 ENGINE 14 SD INCHES OF ACOUSTIC LINER MISSING AFT OF NR 4 BEARING STRUT. PLACED ON CARRYOVER NR 0107964-1 AND NR 0120963-3 IS CONTAINED WITHIN 0120964-1. INSPECTED AND FOUND AIRWORTHY FOR FLIGHT. (M)

Part: ACCOUSTIC LINER — DAMAGED (NR 1 ENGINE)

FTW - FOUND THE NR 1 ENGINE HAS APPROX 12 SQUARE INCHES OF ACCOUSTIC LINING MISSING AFT OF THE NR 4 BEARING STRUT AT THE 7 O'CLOCK POSITION. COMPLIED WITH EA 7230-0305. (M)

Part: ACCOUSTIC LINER — DAMAGED (NR 1 NACELLE)

DURING DAILY INSPECTION, FOUND NR 1 ENGINE ACCOUSTIC LINER DAMAGED. REMOVED/REPLACED NR 1 ENGINE NOSE COWL, NO DEFECTS NOTED. (M)

Part: SLIDE — DEPLOYED (TAIL COMPARTMENT)

LGA - FLT 9822 - TAILCONE SLIDE DEPLOYED UPON TRIGGERING OF THE AFT ENTRY DOOR. SLIDE REMOVED AND PLACED ON AC. REMOVED AND REPLACED TAILCONE SLIDE. (M)

Part: LINER — DAMAGED (NR 2 NOSE COWL)

MCO - NR 2 ENGINE NOSE COWL LINER DAMAGED. REMOVED AND REPLACED NR 2 ENGINE NOSE COWL AS REQ. (M)

Part: PIN — DISLODGED (TAIL SLIDE)

LGA - FLT 1865 - FOUND TAIL COMPARTMENT SLIDE COVER PINS OUT ON RIGHT SIDE AND HALF OUT ON LEFT SIDE. REINSTALLED TAIL COMPARTMENT SLIDE COVER PINS LEFT AND RIGHT SIDE. (M)

Part: SLIDE — OUT OF POSITION (L1 DOOR)

FLT 945 - ACY - L1 SLIDE PACK FELL OUT ON TAXI. REINSTALLED L1 DOOR SLIDE PACK IAW MM 25-62-00. (M)

Part: ANGLE — CRACKED (THRUST REVERSER)

FTW - FOUND NR 2 ENGINE THRUST REVERSER INBOARD FAIRING PYLON CLOSEOUT PANEL CRACKED. REMOVED CRACKED ANGLE DOUBLER. FABRICATED NEW ANGLE DOUBLER. INSTALLED NEW DOUBLER. (M)

Part: FLOORBOARD — CORRODED (PAX CABIN)

PAX CABIN STA 200 TO 160 FLOORBOARD CORRODED AT INSERTS/ DELAMINATED. FABRICATED NEW FLOORBOARD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAX CABIN, STA 200 TO 160 SUPPORT FLOOR CORRODED LBL 54. REMOVED FLOOR SUPPORT, LOCATED AND DRILLED NEW FLOOR SUPPORT, INSTALLED NEW FLOOR SUPPORT COMMON TO PAX CABIN, STA 200-160.

Part: WEB — CORRODED (SUB FLOOR)

PAX CABIN STA 1654, LBL 53, CORRODED ON SUB FLOOR WEB. REMOVED DAMAGED SECTION, FABBED FILLER AND REPAIR DOUBLER, INSTALLED REPAIR.

Part: ISOLATOR — MISINSTALLED (RT ENGINE)

RT LOWER FORWARD VIBRATION ISOLATOR MARKS MISALIGNED. REMOVED RT ENGINE LOWER FORWARD VIBRATION ISOLATOR. REPLACED RT ENGINE LOWER FORWARD VIBRATION ISOLATOR.

Part: WEB — CRACKED (FUSELAGE)

FUSELAGE AFT CARGO BAY FS 1290 LONGERON 18R HAS CRACKED CUSP WEB DOUBLER AT NR 2 ENGINE TELFLEX CABLE FLOOR ACCESS. CUT OUT DAMAGED WEB AT CUSP LONGERON 18 RT STA 1278-1309. FABRICATED WEB FOR REPAIR AT CUSP, LONGERON 18 RT STA 1275-1309. INSTALLED WEB REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

AFT CARGO PIT CRACKED FLOORBEAM INTERCOSTAL FS 1271-1287 OBL (IN OVERHEAD). REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL AND INSTALLED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FTW - FOUND MID CARGO FLOOR SUPPORT STATION 619-712 ELONGATED HOLE, TOOL MARKS, BARE METAL, FASTENER SHANKS. UPON FURTHER INSPECTION, PART FOUND TO BE CRACKED. DRILLED AND LOCATED NEW FLOOR SUPPORT. (M)

Part: LONGERON — CRACKED (FUSELAGE)

FTW - AT FS 1429 ON LONGERONS 2L AND 2R CRACKS IN LONGERON TERMINATION (END). CUT OUT DAMAGE AREA FROM FS 1429 ON LONGERON 2R IN LONGERON TERMINATION. CUT OUT DAMAGE AREA FROM FS 1429 ON LONGERON 2L LONGERON TERMINATION. FABRICATED LEFT LONGERON 2L AND RIGHT L2R LONGERONS AND REPAIR SPLICES. INSTALLED LONGERON 2L AND 2R, TWO SPLICES. (M)

Part: SKIN — GOUGED (FUSELAGE)

FTW - FOUND GOUGES AT FS 1190 RIGHT ON WINDOW BELT REQUIRES TO BE BLENDED AND CHECKED FOR LIMITS. FABRICATED -7 DOUBLER. FABRICATED -5 DOUBLER. INSTALLED REPAIR ON WINDOW BELT. (M)

Part: ATTACH FITTING — CRACKED (INTERCOSTAL)

AFT FUSELAGE LT SIDE IS CRACKED AT INTERCOSTAL ATTACH TO 1510 CANT, 1497 CANT. REMOVED DAMAGED INTERCOSTAL. FABRICATED REPAIR PART AND INSTALLED.

Part: FRAME — DENTED (FUSELAGE)

FTW - FOUND DENT OVER FRAME AT FS 484 BETWEEN LONGERONS 28 AND 29L REQUIRES REPAIR. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: FORMER — CRACKED (VERTICAL STAB)

FTW - FOUND VERTICAL STAB DORSAL FIN CRACKED ON FORMER RIGHT SIDE LOWER ATTACH TO PLATE/STRAP. REMOVED FORMER. LOCATED AND DRILLED NEW FORMER. INSTALLED NEW FORMER, STRAP AND LEFT AND RIGHT PLATES. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

FTW - FOUND STATION 218 STIFFENER NR 4 IS DENTED AND HAS MULTIPLE SPOT OF SURFACE CORROSION. REMOVED DAMAGED PORTION OF NR 4 STIFFENER. FABRICATED REPAIR ANGLE. INSTALLED REPAIR ANGLE. (M)

Part: ATTACH ANGLE — PUNCTURED (FUSELAGE)

FTW - FOUND DORSAL FIN, RIGHT OUTBOARD (TWO) ATTACH ANGLE PUNCTURED. REMOVED TWO RIGHT OUTBOARD ATTACH ANGLE. LOCATED AND DRILLED TWO ATTACH ANGLES, INSTALLED. (M)

Part: SUPPORT — CORRODED (CARGO BAY)

STA 218 FORWARD CARGO BAY, UPPER BLOCK SHELF SUPPORT CORRODED, ENTIRE LENGTH. REMOVED UPPER SUPPORT. FABRICATED UPPER SUPPORT. INSTALLED UPPER SUPPORT.

Part: RIB — CRACKED (LT WING)

FTW - LEFT WING LEADING EDGE RIB CRACKED AT XRS 290. STOP DRILLED CRACK. FORMED REPAIR ANGLES. INSTALLED REPAIR ANGLES. (M)

Part: FRAME — CORRODED (FUSELAGE)

FTW - FOUND AFT CARGO PIT CORRODED FRAME FLANGE FS 1287-L22L 2, CORROSION CLIP ANGLE FS 1287 LONGERON 27L TO 28L.3 AND CORROSION FS 1287 LONGERON 29L ON FRAME. MATERIAL LOSS ON CLIP FS 1287 LONGERON 27L-28L OUT OF LIMITS. REMOVED CLIP. INSTALLED NEW CLIP. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

AFT CARGO BAY HAS A CRACKED FLOORBEAM INTERCOSTAL AT FS 1287-1309 (IN OVERHEAD). REMOVED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. AND INSTALLED.

Part: ANGLE — CRACKED (CARGO BAY)

MID CARGO BAY HAS A CRACKED VERTICAL ANGLE, LT LOWER END OF FS 522 LONGERON 23 LT. REMOVED VERTICAL ANGLE. FABRICATED NEW VERTICAL ANGLE AND INSTALLED.

Part: VANE — DAMAGED (T/E FLAP)

FTW - FOUND RIGHT WING MID FLAP VANE NR 4 HAS HOLE IN LEADING EDGE, SPOT CORROSION AND BARE METAL. REPAIRED FLAP VANE HOLE AND SPOT CORROSION. DOUBLER AND THE FILLERS (2 FILLERS) WERE BONDED TO THE VANE. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND PASSENGER CABIN LEFT INBOARD FLOOR PANEL STATION 465 TO 541 HAS CRACKED METAL, CORE DAMAGE AND FASTENER BROKEN OFF IN PANEL. FABRICATED NEW PANEL. (M)

Part: ACCESS PANEL — CRACKED (LT WING)

FTW - FOUND LEFT WING ACCESS PANEL NR 1163 HAS TOOL MARKS, CORROSION AND BARE METAL. FOUND PANEL TO BE CRACKED. ROUTED OUT CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)

Part: PANEL — CORRODED (WING LE)

LT LEADING EDGE PANEL NR 1168C HAS BARE METAL, CORRODED. MATERIAL LOSS IS OUT OF LIMITS, FABRICATED NEW LT LEADING EDGE PANEL.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 237-863. REMOVED FLOOR PANEL FS 768-826 LBL 22-44 TO REMOVED CORROSION. FOUND THE FLOOR BOARD AT FS 768-826 LBL 22-44 MISSING INSERT AND CRACK EDGE. FABRICATED NEW FLOOR BOARD. INSTALLED FLOOR BOARD. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK WORN AND CORRODED FS 1212-1309. STATION 1227-1250 ON LEFT INBOARD SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. REMOVED LEFT INBOARD SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED LEFT INBOARD SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT MID SEAT TRACK WORN AND CORRODED FS 1212-1309. SEAT TRACK STATION 1227 TO 1309 LEFT MID WAS FOUND TO BE CORRODED OUT OF LIMITS. REMOVED SEAT TRACK. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED LEFT MID SEAT TRACK. (M)

Part: BEAM — CORRODED (FUSELAGE)

FTW - FOUND AFT PIT JAM BEAM CORRODED, INSIDE AND OUT. REMOVED LOWER JAMB BEAM. INSTALLED NEW LOWER JAMB BEAM. (M)

Part: BEAM — CORRODED (CARGO DOORWAY)

MID CARGO DOOR, BOTTOM FORWARD AND AFT DOOR STOPS HAVE CORRODED UNDERNEATH. MID CARGO DOOR JAM BEAM HAS CORROSION ON THE REPAIR STRAP INSIDE OF BEAM. REMOVED JAMB BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED DOOR JAMB BEAM.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CARGO COMPARTMENT CORRODED AT INTERCOSTAL STATION 446 TO 427 ATTACH TO LONGERON 29. REMOVED CORRODED INTERCOSTAL. FABRICATED NEW INTERCOSTAL. INSTALLED INTERCOSTAL. (M)

Part: SKIN — CRACKED (L/E SLAT)

FTW - FOUND RIGHT NR 1 SLAT CRACKED AT LOWER SURFACE AT OUTBOARD SEAL AND SEAL FASTENERS NOT INSTALLED PROPERLY. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR. (M)

Part: RIB — CRACKED (LT WING LE)

LT WING LEADING EDGE RIB, CRACKED AT XRS267. FABRICATED 2 REPAIR ANGLES. STOP DRILLED CRACK ON LT WING LEADING EDGE RIB AT XRS 267. INSTALLED REPAIR ANGLES AT XRS 267 LT WING LEADING EDGE.

Part: ISOLATOR — MISALIGNED (ENGINE)

LT LOWER FORWARD VIBRATION ISOLATOR MARKS MISALIGNED. REMOVED LT LOWER FORWARD VIBRATION ISOLATOR. INSTALLED LT LOWER FORWARD VIBRATION ISOLATOR.

Part: ARM — BENT (LANDING GEAR)

FTW - COULD NOT GET GEAR LIGHT TO TURN FROM RED TO GREEN WHEN USING EMERGENCY GEAR EXTENSION BOTH PRESSURIZED AND UNPRESSURIZED HYDRAULICS. REMOVED SHAFT, SPRING, RETAINER BLOCK, SUPPORT AND ARM. UPON FURTHER INSPECTION FOUND ARM BENT, BEARINGS WORN IN SPRING RETAINER BLOCK, BEARING IN SUPPORT WORN AND COVER BROKEN. INSTALLED SHAFT, NEW SUPPORT ASSEMBLY, SPRING ARM AND BLOCK ASSEMBLY AS AN ASSEMBLY. (M)

Part: GENERATOR — FAILED (LEFT)

DTW - FLT 706 - AFTER TAKEOFF OVER MILE AREA, LEFT GEN FAULT FEEDER AND GEN BUS AND X-TIE LIGHT CAME ON, QRH FOLLOWED. FOUND LEFT GENERATOR BAD. ON GENERATOR T5 TO T6 READ .5 OHMS WHICH FAIL GENERATOR. REMOVED AND REPLACED LEFT POWER RELAY FOR PRECAUTIONARY. (M)

Part: GENERATOR — FAILED (LEFT)

FLT 706 - LGA - AFTER TAKEOFF OVER MILE AREA LT GENERATOR FAULT FEEDER AND GEN BUS AND X-TIE LIGHT CAME ON, QRH FOLLOWED. FOUND LEFT GENERATOR BAD. ON GENERATOR T5 TO T6 READ .5 OHMS WHICH FAIL GENERATOR. REMOVED AND REPLACED LEFT POWER RELAY FOR PRECAUTIONARY. REF ITEM 43556-1 FOR LEFT GEN REPLACEMENT IAW MD80 MM 24-20-00. (M)

Part: GCU — MALFUNCTIONED (LT GENERATOR)

DTW - FLT 874 - AT CRUISE, RECEIVED THE AC CROSSTIE LOCKOUT LIGHT, LT FLIGHT FAULT AND LT GEN OFF LIGHT ON AFTER REINSTALLING POWER TO THE LT AC SYSTEM WITH THE APU PER OUR QRH. UNABLE TO RESTORE LEFT GENERATOR POWER. REMOVED AND REPLACED GENERATOR CONTROL UNIT. TIGHTEN ALL FIREWALL GEN CONTROL AND POWER CONNECTORS. OPS CHECK NORMAL ENGINE. (M)

Part: COWLING — PEELING (NR 2 ENGINE)

DTW - NR 2 ENGINE NOSE COWL, INLET LINER, METAL MESH PEELING AT 12 O'CLOCK POSITION. REPAIRED WIRE MESH ON NR 2 ENGINE, INLET COWL IAW MD80 SRM 54-04. (M)

Part: WIRE — CHAFED (TAIL CONE)

DTW - FOUND WIRES CHAFED IN AFT ACC COMPARTMENT AT TAILCONE JETTISON HANDLE LIGHT ASSEMBLY. SECURED CHAFING WIRES AFT ACC COMPARTMENT IAW MD80 MM 20-50-02 AND REPLACED CHAFFED WIRES. OPS CHECK GOOD. (M)

Part: CONNECTOR — LOOSE (NR 1 ENGINE)

FLL - FLT 1440 - AT 30,000 ON CLIMB-OUT, LT ENGINE GENERATOR DROPPED OFFLINE, CROSSTIE LOCKOUT LIGHT ON LT GEN FEEDER FAULT LIGHT ON LT GEN OFF LIGHT ON LOSS OF CONT LT AC BUS POWER OCCURRED. FOLLOWED QRH, DESCENDED TO 24,000, THE APU FINALLY STARTED. QRH CREW PLACED LT APU BUS SWITCH ON AND CONT. RECOVERED LT AC BUS. CROSSTIE LOCKOUT AND LT GEN FEEDER FAULT REMAINED RETURNED TO FLL FOR A MX RTB. ACCOMPLISHED ENGINE RUN AND PERFORMED AC GENERATOR PREFERENTIAL AND LOAD CHECK. OPENED NR 1 ENGINE COWLING AND INSPECTION GENERATOR FEEDER CABLES FROM AC GENERATOR FROM AC GENERATOR TO THE AFT PRESSURE BULKHEAD. NO DEFECTS NOTED, FOUND GENERATOR FEEDER CONNECTOR LOOSE AT ENGINE FIREWALL, SECURED CONNECTOR. (M)

Part: HEADSET — OVERHEATED (COCKPIT)

DEN - FLT 970 - MIC ON CAPTAIN HEADSET OVERHEATED AND IS INOPERATIVE. SMELLS BURNED AT SWIVEL ATTACHMENT. REMOVED AND REPLACED MIC-HEAD SET. OPS CHECKS NORMAL. (M)

Part: LIMITER — LACK OF LUBE (RUDDER)

FLT 198 - ACY - RUDDER TRAVEL UNRESTRICTED LIGHT DID NOT COME ON DURING FINAL APPROACH UNTIL SLOWING TO BELOW 150 KIAS. CLEANED RUDDER PITOT DRAIN SUMP AND LUBRICATED RUDDER LIMITER SYSTEM IAW MD80 27-20-00. NO DEFECTS NOTED. CLEANED PROXIMITY SENSOR IAW 27-20-06. (M)

Part: LINKAGE — LACK OF LUBE (RUDDER)

RSW - FLT 1525A - FOUND RUDDER TRAVEL UNRESTRICTED LIGHT DID NOT COME ON UNTIL AIRCRAFT TOUCHED DOWN. SPEED ON FINAL WAS 104 K. LUBRICATED BEARINGS IN CONTROL LINKAGES AND ADJUSTED RIGGING ON RUDDER THROW LIMITER SYSTEM. ALL WORK IAW MD80 MM 27-20-00. (M)

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION)

FLT 1570 - MYR - DURING TAKEOFF AT APPROX 70 KTS, SMOKE DETECTOR LOOP ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED RIGHT ENGINE LOOP B LIGHT ON. RETURN TO MAINTENANCE. PERFORMED LEAK CHECK OF ALL RIGHT ENGINE BLEED DUCTS, ALSO PERFORMED VISUAL INSPECTION OF RIGHT ENGINE FIRE DETECTOR LOOP AND CONNECTORS. FOUND NO LEAKS OR DEFECTS. REMOVED AND REPLACED RIGHT ENGINE FIRE DETECTOR AMP CONTROL UNIT IAW MD80 MM 26-10-03. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (M)

Part: CONTROL PANEL — FAULTY (COCKPIT)

DTW - FLT 114 - FIVE MINUTES AFTER TAKEOFF ATTEMPTED TO ENGAGE AUTO PILOT NR 2 WOULD NOT ENGAGE. TRIED NR 1 IT WOULD NOT ENGAGE. COMPASSES AND ATTITUDE INDICATOR WERE CLOSELY MATCHED. AFTER SEVERAL ATTEMPTS TO ENGAGE AUTO PILOT NR 1 AND NR 2 AUTO PILOT NR 1 ENGAGED AND OPS NORMAL. AUTOPILOT NR 1 USED DTW TO PBI. FOUND CAPTAINS AUTO PILOT DISCOUNTED SWITCH BAND AND FLIGHT GUIDANCE CONTROL PANEL BAD. REMOVED AND REPLACED CAPTAINS AUTO PILOT DISCOUNT SWITCH AND FLIGHT GUIDANCE CONTROL PANEL. SYSTEM OPS CHECK GOOD IAW MD80 MM 22-01-05 AND 22-01-04. (M)

Part: ACTUATOR — FAULTY (SPOILER)

FLL - FLT 779 - FLIGHT SPOILERS WILL NOT STAY IN ANY DETENT. REMOVED AND REPLACED SPOILER AUTOMATIC ACTUATOR, OPS CHECKED NORMAL IAW MM 27-62-05. (M)

Part: SKIN — DENTED (CARGO DOOR)

DTW - INSPECT DENT ON AFT CARGO DOOR FOR LIMITS. DENT PLACED ON C/O 0016919-3 WITHIN LIMITS IAW MD-80 SRM 53-04. (M)

Part: MEGAPHONE — INOPERATIVE (CABIN)

FLT 1525 - RSW - MEGAPHONE INOPERATIVE, FORWARD RIGHT. REMOVED AND REPLACED FORWARD RIGHT MEGAPHONE. NEXT INSPECTION DUE TO 6/02. (M)

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

DTW - FLT 476 - DESCENDING INTO DTW, ALTITUDE ARMED, ALTITUDE DISARMED ITSELF WITHOUT PILOT INTO SHOWING TO 210 KTS AT 12,000 FT. AUTOPILOT WOULD NOT MAINTAIN ALTITUDE DFGC NR 1. CHECKED STP, NO FLIGHT FAULTS LOGGED, PERFORMED A RETURN TO SERVICE BIT CHECK OF BOTH DFGC''S SYSTEM. OPS CHECK GOOD IAW MD-80 MM 27-01-05. (M)

Part: AUTOTHRUST SYS — MALFUNCTIONED (COCKPIT)

ORD - FLT 784 - AUTOTHROTTLE SYSTEM WILL NOT STAY ENGAGED WHEN USING AUTOPILOT NR 1 SYSTEM. WORKS NORMALLY IN AUTOPILOT NR 2 POSITION. ALSO ATS WILL NOT ENGAGE AT ALL ON TAKEOFF ROLL WITH A/P IN NR 1 POSITION. GROUND OPS CHECK GOOD IAW 78-03-00 MD-80 MM. (M)

Part: AUTOTHRUST SYS — MALFUNCTIONED (COCKPIT)

AUTOTHROTTLE DISCONNECTED IN DESCENT AND WOULD NOT RECONNECT. REVIEW STP FOR APPLICABLE FAULTS. PERFORMED A/T MAINTENANCE CHECK IAW MD-80 MM CH 22-31-00. NO DEFECTS NOTED. THIS CLEARS DMI NR 0001940. PLACARDS REMOVED. (M)

Part: AUTOTHRUST SYS — MALFUNCTIONED (AUTOPILOT SYS)

ACY - FLT 1210 - AUTOTHROTTLES FREQUENTLY DISCONNECT AND WON''T RE-ENGAGE. AS SPIRIT MEL 22-15-2 CAT C TRANSFERRED TO DMI NR 0001928-1 PLACARDED. (M)