N823NK

Part: SLIDE — DISLODGED (L2 DOOR)

ACY - DURING MAINTENANCE THE CLEANERS OPENED L2 DOOR AND DROPPED SLIDE PACK ON RAMP. REMOVED AND REPLACED L-2 SLIDE. (M)

Part: GIRT BAR — DIRTY (L1 SLIDE PACK)

ORD - FLT 1525A - L1 SLIDE PACK SLIPS OUT OF PLACE WHEN SLIDE IS DISARMED. DETERMINED GIRT BAR FALLING OUT OF LOCKS. CLEANED AND LUBED GIRT BAR LOCKS, OPS CHECK NORMAL. ALSO, ADJ GIRT BAR DISENGAGE HOLDER. (M)

Part: FRAME — DAMAGED (FUSELAGE)

FTW - FOUND NOSE GEAR RIGHT SIDE AFT DOOR JAMB HAS DENTED/DAMAGED STATION 110. REMOVED DAMAGED FRAME. INSTALLED FRAME. (M)

Part: WARNING LIGHT — ILLUMINATED (SLAT SYSTEM)

A/C 823 HAS AUTO SLAT FAIL LIGHT ON TAXI OUT. UNSCHEDULED CHANGE A/C EN ROUTE. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

ON STABILZED APPROACH WITH FLAPS UP THE STALL INDICATION FAILURE LIGHT ILLUMINATED FOR ONE MINUTE THEN LIGHT REMAINED ON FOR REST OF THE APPROACH, ALSO HEADING LIGHT ON BOTH FMA'S WAS ILLUMINATED, HEADINGS WERE SPLIT 6-7 DEGREES BOTH LIGTHS ON STEADY. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)

Part: GENERATOR — FAILED (LEFT)

SELECTED EMERGENCY POWER AFTER LEFT GEN FAIL. CAPTAINS ATTITUDE FLAGS IN VIEW AND UNPOWERED EMER AC AND EMG DC ANNUNCIATOR LIGHTS REMAINED OUT AND ALL INDICATIONS WERE BUSSES POURED FOR EMERGENCY AC AND DC. PERFORMED OPS CHECKS ON EMERGENCY POWER SYSTEM, NO DEFECTS NOTED. (M)

Part: BULB — BURNED OUT (MLG INDICATOR)

NOSE WHEEL NLG INDICATOR NOT OUT WHEN GEAR DOWN. LANDING GEAR NOSE LIGHT OUT. LUBRICATED NOSE GEAR VISUAL IND LEVER INDICATOR PRITRUDES .375 INCHES ABOVE TOP SURFACE OF PEDESTAL COVER PLACT WITH HYDRAULIC PRESSURE APPLIED. RELAMPED NOSE GEAR GREEN DOWN AND LOCKED LIGHTS AND OPS NORMAL. (M)

Part: WIRE — UNSECURE (EMERGENCY LIGHT)

L1 DOOR EXIT IDENTIFIER, INOPERATIVE. T/S AND FOUND POWER WIRE NOT SECURED. SECURED POWER WIRE.

Part: FRAME — CORRODED (FUSELAGE)

FOUND CORRODED FRAME IN AFT LEFT LAVATORY AT FS 1338 LEFT SIDE APPROX 6 INCHES ABOVE CUSP LINE. FABRICATED 3 ANGLE AND 5 SPLICE ANGLE. INSTALLED 3 ANGLE AND 5 SPLICE REPAIR. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

FORWARD LAV ENTRY STA 256 FLOOR PANEL DELAMINATED. REMOVED FLOOR PANEL. FABBED FLOOR PANEL. INSTALLED NEW FLOOR PANEL.

Part: FLOORBOARD — CRACKED (CABIN)

FLOORBOARD MAIN CABIN STA 826-927 LT, CRACKED. STOP DRILLED CRACK. FABBED REPAIR DOUBLER. INSTALLED REPAIR PARTS.

Part: FLOORBOARD — DELAMINATED (CABIN)

FORWARD ENTRY STA 200 FLOOR PANEL DELAMINATED. REMOVED FLOOR PANEL. FABRICATED NEW FLOORBOARD. INSTALLED NEW FLOORBOARD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN STA 203, RBL 5, LBL 19 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED FLOOR SUPPORT.

Part: STRUCTURE — CORRODED (SUBFLOOR)

CABIN STA 218, LBL 43, SUBFLOOR CORRODED. CUT OUT DAMAGE. DRILL AND LOCATE DOUBLER. INSTALLED DOUBLER.

Part: FLOORBOARD — CRACKED (FUSELAGE)

PAX CABIN FLOORBOARD CRACKED/BROKEN AT FS 218-294 LEFT BETWEEN SEAT TRACKS 1 AND 2. REMOVED FLOORBOARD, DRILL AND LOCATE AND INSTALLED FLOORBOARD.

Part: SKIN — DAMAGED (FUSELAGE)

FORWARD ENTRY DOOR HOLD OPEN PIN CUTOUT SKIN DAMAGED, REPAIRS. UPON FURTHER INSPECTION THE PAN COMMON TO THE ENTRY DOOR HOLD PIN ASSY WAS FOUND TO BE CRACKED. FABBED -13, -11 DOUBLERS, -3 PLATE. LOCATED AND DRILLED NEW PAN. INSTALLED FORWARD ENTRY DOOR HOLD OPEN PIN ASSY AND REPAIR PARTS NOTED IN STEP NR 1.

Part: FLOOR PANEL — BROKEN (FUSELAGE)

CABIN FLOOR PANEL AT FS 200-237 CENTER IS BROKEN IN CENTER. FABRICATED NEW FLOOR PANEL.

Part: FIRESEAL — CRACKED (NR 2 ENGINE)

NR 2 ENGINE APRON UPPER 4TH FROM FORWARD FIRESEAL CRACKED. REMOVED CRACKED FIRESEAL. FABRICATED NEW FIRESEAL. INSTALLED NEW FIRESEAL.

Part: FIRE SEAL — CRACKED (NR 2 ENGINE)

NR ENGINE APRON UPPER 6TH FROM FORWARD FIRE SEAL CRACKED. REMOVED CRACKED FIRE SEAL. FABRICATED NEW FIRE SEAL. INSTALL NEW FIRE SEAL.

Part: FRAME — CORRODED (FUSELAGE)

AFT PIT CORRODED AT FRAME, STATION 1079 - 1309. REMOVED CORROSION ON FRAME STATION 1231-1271 AND 1309. FOUND OUT OF LIMITS. CUTOUT DAMAGE IF FRAME FROM STATION 1231. INSTALLED NEW SECTION OF FRAME. SPLICE REPAIR STATION 1231. CUTOUT DAMAGE AREA OF FRAME STATION 1271. LOCATED AND DRILLED NEW SECTION OF FRAME. FABRICATED 4 REPAIR SPLICES AND 4 PLATES. INSTALLED SECTION OF FRAME AND SPLICES REPAIR ON FRAME STATION 1271. LOCATED AND DRILLED NEW FRAME. FOUR ANGLES REPAIRS 5, 9 FOR SPLICE REPAIR. FABRICATED FOUR PLATES. INSTALLED NEW SECTION OF FRAME STATION 1309 L28R AND L28L. INSTALLED FRAME SPLICES. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFT PIT STA 1155 FORWARD DOOR FRAME CORRODED. REMOVED DAMAGED AREA. FORMED REPAIR. INSTALLED 2 REPAIR PIECES.

Part: FITTING — CORRODED (FUSELAGE)

AFT PIT LT FITTING SUPPORT LOWER DOOR JAMB, 2 EA CORRODED STA 1155, STA 1211. REMOVED 2EA LT FITTINGS. LOCATED AND DRILLED NEW FITTINGS. INSTALLED NEW FITTING.

Part: BRACKET — CORRODED (CARGO TRACK)

AFT PIT STA 1155 TO STA 1117. 4 EA BRACKETS SUPPORT RIGHT CARGO TRACK CORRODED (ATTACH TO THE BEAM). FABRICATED 4 EA ANGLES.

Part: SKIN — CORRODED (FUSELAGE)

FOUND AFT PIT STATION 1174 CORRODED AT SKIN WITH INNER/OUTER DOUBLER, LOWER DOOR JAMB. INNER SKIN FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLERS. INSTALLED 2 DOUBLERS. (M)

Part: FITTING — CRACKED (FUSELAGE)

AFT PIT STA 1007 1 FITTING SUPPORT END CARGO TRACK ATTACH TO INTERCOASTAL RIGHT SIDE IS CRACKED. REMOVED CRACKED FITTING. HOLES LOCATED AND DRILLED ON NEW FITTING. INSTALLED NEW FITTING.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

MID CARGO FS 695, INTERCOASTAL CORRODED AND TOOL MARKS STR 29L. FABRICATED NEW INTERCOSTAL. PRIOR TO STEP 5, REMOVED DAMAGED INTERCOSTAL. INSTALLED INTERCOSTAL.

Part: WEB — CORRODED (CARGO BAY)

FORWARD CARGO CEILING AREA WEB CORRODED FS 226, STR 18R. FABRICATED WEB DOUBLER. INSTALLED DOUBLER AND FILLER.

Part: STRINGER — CORRODED (FUSELAGE)

FORWARD CARGO STRINGER 28L CORRODED FS 428. FAB STRAP. INSTALLED STRAP.

Part: SKIN — CORRODED (FUSELAGE)

FOUND MID CARGO FS 690 STATION STRINGER 30-29L SKIN CORRODED. AFTER FURTHER EVALUATION, MORE DAMAGE FOUND ON EXTERNAL SKIN. FABRICATED EXT DOUBLER. FABRICATED INT DOUBLER. INSTALLED REPAIR DOUBLERS. (M)

Part: WEB — CORRODED (FUSELAGE)

AFT PIT STA 1150 TO STA 1220 WEB CORRODED. FAB NEW WEB.

Part: WEB — CORRODED (FUSELAGE)

E AND E BAY FS 162 CEILING AREA WEB CORRODED LBL 51. DRILL AND LOCATED DOUBLER. INSTALLED DOUBLER.

Part: DOOR FRAME — CORRODED (FUSELAGE)

FTW - AFT LOWER CARGO, LOWER DOOR JAMB CUTOUT CORROSION AT DOUBLER REPAIR, ATTACH TO O/B BEAM. REMOVED DOOR JAMB BEAM STATION 1114 TO 1249. LOCATED AND DRILLED NEW JAMB BEAM STATION 1114 TO STATION 1249. INSTALLED NEW JAMB BEAM. (M)

Part: DOOR FRAME — CORRODED (LWR DOOR JAMB)

FORWARD CARGO LOWER DOOR JAMB CUTOUT CORRODED (DOOR PAN). FABRICATED -19, -21 REPAIR SPLICES. DRILLED AND LOCATED NEW PAN. INSTALLED DOOR JAMB PAN. INSTALLED FWD AND AFT REPAIR SPLICE.

Part: BEAM — CORRODED (CARGO DOORWAY)

MID LOWER CARGO, LWR DOOR JAMB OB BEAM CORRODED. REMOVED DOOR JAMB BEAM L28R STA 598 TO 733. DRILLED AND LOCATED HOLES IN NEW BEAM, INSTALLED DOOR JAMB BEAM.

Part: LINER — DELAMINATED (NR 2 ENGINE)

DTW - ACCOUSTIC LINER DELAMINATED IN NR 2 ENGINE FAN DISCHARGE TURBINE EXHAUST SECTION OUTER DUCT. REMOVED AND REPLACED NR 2 ENGINE. (M)

Part: DOOR — OPEN (NLG)

DEN - FLT 980 - UPON ROTATION AND GEAR UP, ENCOUNTERED VIBRATION IN NOSE WHEEL AS IF DOOR STAYED OPEN. ON TAXI, IN RIGHT NOSE GEAR DOOR WAS OPEN. INSPECTED NOSE GEAR DOOR, LINKAGES/STRUT/TORQUE LINKS. NO DEFECTS NOTED. TESTED NOSE GEAR DOOR LOCKS BY PULLING ON IT, THEY REMAINED LOCKED. NO DEFECTS NOTED, OK TO CONTINUE. (M)

Part: WARNING LIGHT — ILLUMINATED (RT MLG)

FLT 787 - RIGHT MAIN GEAR LIGHT REMAINED ON AFTER RETRACTION, PER QRH RECYCLED GEAR/UNSAFE LIGHT WENT OUT. INSPECTED PROX SENSOR AND ASSOCIATED MECH. NO DEFECTS NOTED. ACP PROXIMITY BOX SENSOR CHECK. ALL OPS NORMAL, REF UP AND LATCH SENSOR. (M)

Part: CSD — FAILED (NR 2)

FLT 779 - LGA - IN CRUISE AT 35,000 FEET NEAR WILMINGTON NC, LOST ALL ELECTRICAL POWER. SELECTED EMERGENCY POWER DECLARED EMERGENCY, BEGAN DIVERSION TO MYR. PERFORMED QRH PROCEDURES GOT LEFT GENERATOR ON LINE, HAD X-TIE LOCKOUT. LANDED SUCCESSFULLY IN MYR. PRIOR TO LOSS OF ELECTRICAL, HEARD AND FELT LOW RUMBLE AND VIBRATION IN A/C. ALL ENGINE GEN VOLTS AND FREQS NORMAL. ALL ENGINE INDICATIONS NORMAL. NEVER ABLE TO GET RT GENERATOR ON LINE. REMOVED AND REPLACED NR 2 CSD IAW MD 80 MM 24-10-01 SERVICED CSD AND CAVITY OPS AND LEAK CHECK GOOD. (M)

Part: BLADE — DAMAGED (RT ENGINE)

LGA - ON WALK AROUND, FOUND RIGHT ENGINE FOD DAMAGE. NR 2 ENGINE NOSE COWL ACOUSTIC LINER DAMAGED. REMOVED AND REPLACED DAMAGED C-1 BLADES. REMOVED AND REPLACED NR 2 ENGINE NOSE COWL. (M)

Part: ODOR — DETECTED (CABIN)

FLT 1927 - ORD - STRONG ODOR OF BURNING RUBBER OR OIL IN CABIN, JUST FORWARD OF OVERWING EXITS, DURING APPROACH, BEFORE LANDING GEAR WAS LOWERED. INSPECTED CABIN LIGHTING, OPERATED LEFT AND RIGHTS PACKS, NO DEFECTS NOTED. CHECKED C/B'S, NONE TRIPPED. AIRCRAFT OK FOR CONTINUED SERVICE. (M)

Part: SEAL — OUT OF POSITION (L2 DOOR)

DTW - FLT 639 - AT 9,000 FT SOUTH OF DTW, LOST PRIMARY AND SECONDARY PRESSURE CONTROLLER, WENT TO MANUAL CONTROLLER, WENT BACK TO AUTO, WORKED OK AT 29,000 FT IN CRUISE, CABIN STARTED TO CLIMB IN AUTO AND MANUAL FULL FORWARD. DESCENDED TO 25,000 FT. MAINTAINED CABIN AT 8,500 IN AUTO AND MANUAL PER F/A, NOISE FORWARD LEFT EMERGENCY EXIT. QRH PROCEDURES COMPLIED WITH. INTERMITTENT FLOW LIGHT IN CRUISE 1.90 EPR AND LESS. CHECKED CABIN PRESSURE CONTROL SYSTEM. NO DEFECTS NOTED. FOUND LOWER AREA OF L2 DOOR SEAL OUT OF GROOVE. REINSTALLED INTO GROOVE PER M/M 52-42-02. PRESSURIZED A/C. INSPECTED L2 DOOR AND EMERGENCY OVERWING EXIT DOORS FOR LEAKS. NO LEAKS NOTED. OK TO CONTINUE. (M)

Part: DOWNLOCK SENSOR — MALFUNCTIONED (NLG)

UPON INT. DESCENT NOSE WHEEL UNSAFE LIGHT CAME ON STAYED ON AT ALL POWER SETTING. FOLLOWED QRH PROCEDURES. HAD THREE GREEN FOR LANDING. REMOVED AND REPLACED NOSE GEAR DOWN LOCK PROX SENSOR AND OPS CHECK GOOD IAW MM.

Part: DOOR — UNSECURE (NLG)

DIVERTED, VIBRATION NOISE IN NOSE AREA AFTER GEAR RETRACTION AT LGA RECYCLED GEAR, NO HELP, PUT GEAR DOWN. RIGHT NOSE LANDING GEAR DOOR UNSECURE. INSPECTED NOSE LANDING GEAR DOORS/WHEEL WELL SECURED NOSE LANDING GEAR DOORS.

Part: ELEVATOR — MALFUNCTIONED (HORIZONTAL STAB)

FLL - FLT 1754 - DISCONTINUED TAKEOFF AT 90 KNOTS. AIRCRAFT SEEMED TO BE TAIL HEAVY AND ABNORMAL FORWARD YOKE PRESSURE WAS REQUIRED TO MAINTAIN WEIGHT ON THE NOSE TIRE. INSPECTED HORIZONTAL STAB AND ELEVATORS FOR PROPER OPERATION. MD80 MM 27-31-0 AND 27-41-0. COMPLIED WITH HIGHT ENERGY STOP INSPECTION PER MD80 MM 05-57-00. AIRCRAFT FOUND TO BE MECHANICALLY SOUND. (M)

Part: STRUT — DISCHARGED (NLG)

MYR - FLT 1572 - NOSE WHEEL WOULD NOT RETRACT AFTER TAKEOFF, FOLLOWED QRH PROCEDURES RETURNED TO KMYR FOR MX. SERVICED NOSE STRUT TO PROPER LEVEL IAW MD80 MM 32-21-02 AND PERFORMED GEAR SWING IAW MD80 MM 32-30-00. NO DEFECTS NOTED, NOSE GEAR RETRACTION. OPS CHECKS GOOD. (M)

Part: LATCH — OUT OF RIG (RT MLG DOOR)

ORD - AFTER GEAR RETRACTION RIGHT MAIN GEAR RED LIGHT REMAINED ON. DID PROCEDURES ACCORDING TO QRH, GEAR DOOR LIGHT CAME ON. LIGHT WENT OUT WITH RIGHT HYD PUMP ON HIGH RESTRICTED TO .70 M FOR REMAINDER OF FLIGHT. FOUND DOOR LATCH MECH OUT OF RIG. RIGGED RIGHT MAIN GEAR DOOR LATCH MECH AND MAIN GEAR UP SENSOR. SYSTEM OPS CHECK GOOD PER 32-31-04. AIRCRAFT OK FOR SERVICE. (M)

Part: VALVE — FAILED (CABIN PRESSURE)

FL310, CABIN CLIMB GAUGE READS PLUS 500 SHORTLY AFTER FLOW LIGHT. CABIN PRESS READS 5.500 FT. NORMAL CABIN STARTING A SLOW CLIMB THAT COULD NOT BE STOPPED, EVEN WITH CONTROLLER MANUAL/FULL CLOSED. AT ABOUT 8800 FT CABIN ALT STOPPED EMERGENCY DESCENT. COMPLIED WITH ALL QRH ITEMS. DIVERTED TO ACY. CABIN NEVER RECOVERED. CABIN ALT NEVER ABOVE 15K. ALL MASKS DROPPED AS REQ 39329-2 DECAY CHECK REQUIRED REF TO TIME 39329-3, 39329-3. FOUND AFT SAFETY VALVE TO BE OPENING AT 7.6 PSI VALVE CHECKED BAD .39330-2 POST MAINTENANCE TEST FLIGHT DUE FOR PRESSURIZATION. AFT CABIN SAFETY VALVE WAS FOUND BAD AND CHANGED AND CABIN DECAY CHECKED ALSO PERFORMED AUTO PRESSURIZATION CHECK. (M)

Part: DOOR — CRACKED (THRUST REVERSER)

DTW - FOUND CRACK IN THE NR 2 UPPER T/R DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER. (M)

Part: B-NUT — LOOSE (NR 1 ENGINE)

DTW - FLT 902 - NR 1 ENGINE 1.23 EPR MAX-ENGINE HEAT ON LOW SPEED ABORT RETURN TO GATE. REMOVED AND REPLACED LEFT EPR XMITTER NO HELP, FOUND LOOSE 'B' NUT ON PIT FLEX LINE ON PYLON, TIGHTEN SAME SYSTEM OPS CHECK OK PER 77-11-02. AIRCRAFT OK FOR SERVICE. (M)

Part: ACCELEROMETER — MALFUNCTIONED (AUTOPILOT SYS)

DTW - WHILE LEVEL AT CRUISE THE 'YAW DAMP OFF' LIGHT ILLUMINATED FOR APPROX 5 MINUTES AND BOTH FMA'S SHOWED VERTICAL SPEED AND NO AUTOLAND (PREV SHOWED ALT HOLD) THIS WAS ON DFGC NR 1, SWITCHED TO DFGC NR 2 AND PROBLEM REMAINED, AFTER SEVERAL MINUTES SWITCHED BACK TO DFGC NR 1 LIGHT STAYED ON UNTIL NOSE (YAW) TRIM WAS ADJUSTED SLIGHTLY LEFT AND RIGHT THIS ALL OCCURRED WHETHER AUTOPILOT WAS ON OR OFF NO ADVERSE YAW OF AIRCRAFT WAS EVER FELT QRH REF. REMOVED AND REPLACED DUAL LATERAL ACCELEROMETER PER MD80 MM 22-19-02. SYSTEM OPS CHECK (RTS) PER MD80 MM 22-01-05. OPS CHECK GOOD. (M)

Part: SPOILER — MALFUNCTIONED (WING)

FLL - FLT 765 - ON TOUCHDOWN, SPOILER HANDLE MOVED AFT THEN FORWARD WAS UNABLE TO MANUALLY EXTEND SPOILERS THEREAFTER W/O HOLDING THE HANDLE BACK. PERFORMED SYSTEM CHECK OUT IAW MD80 MM 27-60-00. RESET SYSTEM, CHECK OK. AUTOSPOILER DO NOT USE LIGHT OUT. (M)

Part: ACCELEROMETER — FAILED (NR 2)

DTW - FLT 678 - AT 33,000 FT, LOST NR 2 DFGC. SWITCHED TO NR 1. OK FOR 10 SECONDS THEN LOST IT. NO FMA'S, NO FD, NO AUTO PILOT, NO AUTO THROTTLE. COMPLIED WITH ORH, NO SUCCESS. EVERYTHING CAME BACK ALL BY ITSELF AT 12,000. CHECKED STP, FOUND MANY ACCELEROMETER FAULTS. REMOVED AND REPLACED DUAL LATERAL ACCELEROMETER PER MD 80 MM 22-19-02. SYSTEM OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

FLL - EMERGENCY CEILING LIGHTS BETWEEN STATION 800 AND 925 INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY (B5-107) IAW MM 33-53-00, OPS CHECK OK REF WDM 33-51-01. (M)

Part: COMPUTER — FAILED (NR 1)

ACY - AUTO PILOT INOPERATIVE IN CMP NR 1. REMOVED AND REPLACED NR 1 DFGC, OPS CHECK NORMAL. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

FLL - THE EXTERIOR EMERGENCY LIGHTS ASSEMBLIES ILLUMINATED WHEN EMERGENCY LIGHT SWITCH IS PLACED FROM ARM TO OFF. REMOVED AND REPLACED BATTERY POWER SUPPLY ASSEMBLY. OPS CHECKED IAW MD 80 MM 33-53-00 NORMAL. (M)

Part: ENGINE — LEAKING (NR 2)

DTW - FLT 1691 - F/A'S REPORTED SMOKE IN CABIN, FOLLOWED QRH, LANDED AT 128,000 NR TURNED OFF L PACK. SMOKE PERSISTED. TURNED LEFT AND RETURNED OFF LATER TURNED OFF NI SMOKE. FOUND OIL IN 13TH STAGE DUCT REPLACED NR 2 ENGINE. (M)

Part: TERMINAL — LOOSE (COCKPIT)

DTW - WHILE CHECK TAKEOFF WARNING SYSTEM. UNABLE TO GET A FLAP WARNING. ALL OTHER WARNINGS OK. FOUND LOOSE TERMINAL ON FLAP SWITCH IN PEDESTAL, RESECURED IAW MM 20-00-00. NO DEFECTS NOTED. (M)

Part: ACM — LEAKING (RIGHT)

DTW - FLT 941 - ON INITIAL CLIMB THROUGH APPROX 4000 'A' FLIGHT ATTENDANT REPORTED THICK OILY SMOKE IN AFT CABIN COMPLIED WITH QRH PROCEDURE RETURNED TO DTW BOTH AC PACKS OFF SMOKE DISIPATED. FOUND ACM (RT) SHAFT LEAKING OIL INTO AIR CONDITIONING SYSTEM. REMOVED AND REPLACED RIGHT ACM IAW MD 80 MM 21-51-01 LEAK AND FUNCTIONAL CHECK GOOD. NO SMOKE NOTED IN CABIN. (M)

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY)

FLL - RIGHT AFT LAV SMOKE ALARM OPERATES INTERMITTENTLY. MUST GO TO L2 DOOR (CEILING) TO CANCEL HORN AND LIGHT. REMOVED AND REPLACED RIGHT AFT SMOKE DETECTOR IAW 25-31-08. (M)