N130NK

Part: COMBUST CHAMBER — WORN (ENGINE)

BOROSCOPE RECORD, FOUND IGNITER GUIDE NR 4 COMBUSTION CHAMBER WORN AND OUT OF CHAMBER RESTING IN OUTER COMBUSTION CASE IGNITER PORT NR 4. BURNER CANS HAVE BEEN REPACED DURING SHOP VISIT.

Part: ISOLATOR — DEFECTIVE (NR 1 ENGINE)

DTW - FOUND LOWER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE LOWER ISOLATOR, CLOSED 10/10/02. (M)

Part: ISOLATOR — DEFECTIVE (NR 1 ENGINE)

DTW - FOUND UPPER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE UPPER ISOLATOR, CLOSED 10/10/02. (M)

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

AEX - AUTOPILOT TURNS A/C RIGHT WITH TURN KNOB CENTERED AUTOPILOT OVER TRIMS AIRCRAFT DURING TURNS RESULTING IN LARGE OUT OF TRIM CORRECTIONS. (M)

Part: CONTROL UNIT — INOPERATIVE (AUTOPILOT SYS)

FLL - FLT 41 - AUTOPILOT PITCH CONTROL IS INOPERATIVE. TRANSFERRED TO CMI NR 0019690-3. CAT C MEL 22-10. PLACARD INSTALLED. (M)

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS)

FLL - FLT 139 - WITH A/P ENGAGED AL PORPOISES ABRUPTLY WITH A/P ELEV SERVO OFF PROBLEM CEASES. DMI NR 1669-1 ASSIGNED PER MEL 22-3-0 CAT C DUE DATE D4-24-01 AMEND NR 1 1730Z HR PLACARDED ELEV SERVO SWITCH. (M)

Part: AUTOPILOT SYS — FLUTTER (COCKPIT)

MLB - FLT 72 - WHEN AUTOPILOT IS ENGAGED THERE IS A RAPID OSCILLATION (FLUTTER) IN PITCH, SERVO OFF NO OSCILLATION. TRANFERRED TO MEL 22-16-0 DMI NR 0001663-1 CAT C DUE 4-22-01 AMEND NR 1 1115Z HK. (M)

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT)

FLT 72 - FLL - AUTO PILOT WILL NOT ENGAGE AT ALL. CHECKED THE AUTO PILOT OPERATIONS. FUNCTIONS NORMAL. TALKED TO THE CAPTAIN, HE STATED AUTO PILOT IS NORMAL BOTH ON GROUND AND IN FLIGHT. NO FAULT FOUND. THIS CLEARS DMI NR 0001619-1. PLACARDS REMOVED IAW DC-9 MM 22-10-00. (M)

Part: AUTOPILOT SYS — VIBRATION (COOCKPIT)

WITH AUTO PILOT ON, THERE IS A LOW FREQUENCY VIBRATION IN PATCH AXIS, PITCH SERVO OFF, NO VIBRATION. NORMAL OPERATION. OPS CHECK GOOD ON GROUND IAW DC-9 MM 22-10-00. THIS CLEARS DMI NR 000165-1. PLACARDS REMOVED. (M)

Part: TAIL CONE — DISLODGED (FUSELAGE)

MYR - FLT 303 - TAILCONE CAME OFF ON LANDING. TAILCONE RELEASE SYSTEM EVACUATED AND REPAIRED BY BOEING. REPLACED EXTERIOR CABLE FITTING AND RIGHT LOWER LOCKING PIN. TAILCONE WAS FIT FOR CLEARANCES AND DROP CHECK PERFORMED AS PER DC-9 MM 53-50-3. (M)

Part: TAIL CONE — SEPARATED (AFT)

DCA - FLT 72 - TAILCONE FELL OFF DURING LANDING. REMOVED AND REPLACED TAILCONE IAW MM 53-50-3, OPS CHECK NORMAL. (M)

Part: WIRE — BROKEN (CABIN)

DTW - EMERGENCY FLOOR TRACK LIGHTING FORWARD SECTION INOPERATIVE. REPAIRED BROKEN WIRE OPS CHECKS GOOD IAW DC9 MM 33-53-00. (M)

Part: LENS — MISSING (CABIN)

DTW - EMERGENCY RACK LIGHTING DOES NOT HAVE RED LENSES IN AFT OF FUSELAGE. (STRIP LIGHTING) (FAA). INSTALLED RED STRIP IN AFT TRACK LIGHTING IAW DC-9 MM 33-50-0. OPS CHECKS GOOD. (X)

Part: POWER SUPPLY — FAILED (CABIN)

DTW - FLT 570 - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT EXTERIOR EMERGENCY LIGHT POWER SUPPLY IAW 24-21-00. OPS CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

CLE - FLT 541 - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. PLACED EMERGENCY LIGHT ON DMI 539. REF MEL 33-20 CAT 'B'. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE - FLT 541 - LEFT EXTENSION EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (ROW 2/4)

MYR - FLT 257 - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 2 AND 4. REMOVED AND REPLACED BATTERY PACK AT B5-24 IAW MM 33-53-0, OPS CHECK GOOD. (M)

Part: CONNECTOR — DISCONNECTED (WARNING LIGHT)

MYR - FLT 257 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND CANNON PLUG UNATTACHED FROM BATTERY PACK. LOCKED CANNON PLUG ON BATTERY. OPS CHECKED GOOD. (M)

Part: LIGHT — LOOSE (CABIN)

DTW - FLOOR TRACK LIGHTING INOPERATIVE, RED STRIP NEAR FORWARD GALLEY. RECONNECTED FLOOR TRACK LIGHTING NEAR FORWARD GALLEY. SYSTEM OPERATION CHECKS GOOD IAW MM 33-53-00. (M)

Part: JAMB — CRACKED (CARGO DOORWAY)

MHV - LOWER AFT CORNER OF FORWARD CARGO PIT DOOR JAMB HAS A CRACK APPROX 2 INCH LONGERON IN THE TORQUE BOX. REMOVED DAMAGED AREA PER ENGINEERING AVQ-XXX-99-0001RR AND SPLICED IN NEW CARGO DOOR PAN PER DC9 -40 SRM 53-05 FIG 44. (M)

Part: LONGERON — CRACKED (BS 237-323)

MHV - FOUND STATION 237-277 STRINGER 16L AND STATION 237-323 STRINGER 17L LONGERONS CRACKED AT FRAME ATTACH POINTS. REMOVED AND REPLACED STRINGER 16L FROM STATION 237-277 STRINGER 17L FROM 237-323 IAW DC940 SRM 53-02 FIG 18. (M)

Part: SKIN — MISREPAIRED (VERT STABILIZER)

MHV - VERTICAL STABILIZER L/E ASSY AT STATION 2 FS 52.300 THERE IS AN EXISTING REPAIR THAT IS BLENDED AND FILLED WITH EPOXY 4 COUNTER SINKS BONDO HAS FALLEN OUT. CUT OFF BONDED FINGER DOUBLER FABRICATED TITANIUM REPAIR DOUBLER PER ENG G INSTRUCTION (DRAWING) AND INSTALLED FABRICATED REPAIR DOUBLER PER DC9 SRM 51-30-2 ( RIVET INSTALL) AND SRM 51-30-5 (HILOCK INSTALL). (M)

Part: SKIN — SCRAPED (FUSELAGE)

MHV - REF SPIRIT CARRY OVER NR 0097 SKIN SCRAPES APPROX 1 FT AFT OF FORWARD BAGGAGE DOOR. NDT PERFORMED, NO CRACKS NOTED. LIGHTLY BLENDED AREA AS REQUIRED PER SRM 53-04 FIG 38 SHT 2 FUSELAGE SKIN ALODINE AND PRIME IAW DC9 SRM 51-10-3. (M)

Part: SKIN — GOUGED (BS 229-305)

MHV - W/O'S A096-503-F032, F034, F029 SKIN DENTS AND GOUGE STATION 229 TO STATION 305 APPROX TO BE WORKED ON THIS NON-ROUTINE. REMOVED DENTS AND GOUGES AT STATION 229 TO STATION 305 APPROX BETWEEN STRINGER 16L AND 17L AND REPAIRED PER DRAWING NR 53-99294-1. (M)

Part: CLIP — CRACKED (BS 1219-1244)

MHV - FOUND STATION 1219-1244 RT RBL 24 UPPERMOST CLIP UNDER VENT BOX CRACKED COMPLETELY THROUGH AFT ACCESSORY AREA. INSTALLED NEW CLIP AS PER SRM 51-10-1. (M)

Part: FLOORBEAM — DAMAGED (BS 237.5)

MHV - FLOORBEAM REPAIR AT STATION 237.5. MACHINED FLOORBEAM REPAIR PER DWG NR 53-9803-1. (M)

Part: SKIN — CRACKED (BS 1123)

MHV - REF CARRY OVER ITEM NR 0154 AT FS 1123 NON PRESSURIZED SKIN AT LONGERON 10R, THERE IS A 3 INCH CRACK WITH A CLASS III TEMP REPAIR INSTALLED. CUTOUT DAMAGE AREA IAW DC9 SRM 53-01 FIG 4 SHT 2. FABRICATED DOUBLER AND PLATE IAW DC9 SRM 53-01 FIG 4 SHT 3. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED DOUBLER AND PLATE IAW DC9 SRM 51-30-2 PAGE 1. (M)

Part: FLOORBEAM — CRACKED (BS 180)

MHV - E/E BAY STATION 180 UPPER FLOORBEAM AT BL 0 AFT ANGLE CRACKED AND WEB BOW. REMOVED DAMAGED ANGLE FABRICATED NEW ANGLE FROM 7075T6.032 PO NR 84365 ALODINED AND PRIMED ANGLE IAW SRM 51-10-3 AND INSTALLED ANGLE IAW DC9 SRM 51-30-2. (M)

Part: JAMB — DAMAGED (CARGO DOORWAY)

MHV - LOWER CARGO DOOR JAMB PAN REQ 2 EACH -19 AND -21 SPLICE ANGLE REPAIR. FABRICATED ANGLES -19 AND -21 PER DC9 IAW SRM 53-05 PAGE 107 AND 114 FIG 44 SHT 5 SECTION G-G. (M)

Part: BULKHEAD ANGLE — CORRODED (BS 1127)

MHV - T-ANGLE ON BULKHEAD AT FS 1127 RUNNING FROM LONG L6 AND R6 HAS 3 GROUND OUT AREAS AND CORROSION IN EACH AREA. REMOVED AND REPLACED T-ANGLE PER SRM 51-10-1 AND 51-30-5 AND 51-30-2. (M)

Part: LONGERON — CRACKED (BS 200)

MHV - FORWARD FUSELAGE STATION NR 200 AT LONGERON 24 LONGERON CRACKED. REMOVED CRACKED LONGERON FROM STATION 190 TO STATION 228. FABRICATED LOCATED AND DRILLED LONGERON 24 AND SPLICE PER DC9 SRM 53-2. ALODINED AND PRIMED PER DC9 SRM 51-10-3. INSTALLED PARTS PER DC9 SRM 51-30-2. (M)

Part: FLOORBEAM — CRACKED (BS 180)

MHV - E/E BAY STATION 180 LBL 20 FLOORBEAM CRACKED 3 PLACES FORWARD SIDE OF WEB. FABRICATED REPAIR DOUBLER PER SRM 53-05 PAGE 227 AND 247 FIG 17 FROM 7075T6.032 PO NR 84365 ALODINED AND PRIMED PARTS PER SRM 51-10-3 AND INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

MHV - AS MARKED EDDY CURRENT INSPECTION REVEALS A CRACK ON THE FWD PART OF DOUBLER FROM THE FASTENER HOLE TO THE END ON UPPER ANTI-COLLOSION LIGHT. RADIUS OUT CRACK, CRACK REMOVAL BOUGHT OFF BY NDT TRIMMED -17 SHIM AND LAYOUT OF -11 DOUBLER PER SB 53-186 PAGE 41 FIG 5 SHT 5 - 7. COUNTER SANK ALODINED AND PRIMED IAW DC9 SRM 51-10-3 AND INSTALLED -17 SHIM AND -11 DOUBLER IAW SB 53-186 PAGE 43 FIG 5 SHT 5 O 7. (M)

Part: BULKHEAD DOUBLER — CRACKED (BS 1219-1244)

MHV - STATION 1219-1244 FORWARD OF CANTED BULKHEAD DOUBLER WHERE HARNESS GOES THROUGH IS EXFOLIATING AND CRACKED AFT ACCESSORY AREA. FABRICATED NEW DOUBLER AND INSTALLED IAW DC9 SRM 53-01 FIG 4 SHT 3. (M)

Part: BULKHEAD T — CORRODED (BS 1127)

MHV - T-EXTRUSION AT FS 1127 BULKHEAD IS CORRODED BEYOND USE. MACHINED T-EXTRUSION PER DC9 SRM 51-10 AND EXAMPLE ISSUED TO FLOOR IN BLANK CONDITION LOCATED AND DRILL REF A096S03L053. (M)

Part: FLOORBEAM — CRACKED (BS 180)

MHV - E/E BAY STATION 180 LBL 22 FLOORBEAM WEB CRACKED FORWARD SIDE AND ANGLE ON AFT SIDE CRACKED. FABRICATED DOUBLER IW DC9 SRM 53-05 PAGE 227. TREATED AND PRIMED DOUBLER IAW DC9 SRM 51-10-3. INSTALLED DOUBLER IAW DC9 SRM 53-05 PAGE 227. (M)

Part: ANGLE — CRACKED (BS 1041)

MHV - FOUND STATION 1041 LEFT SIDE A/C AFT SIDE OF FRAME ANGLE (FRAME TO LONGERON) AT LONGERON NR 17 CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-01 PAGE 1 APPLIED SEALANT IAW SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IAW SRM 51-01 PAGE 1 APPLIED SEALANT IAW SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IAW SRM 51-30-2 PAGE 6 FIG 5 REF FO54 FOR FABRICATED ANGLE. (M)

Part: LONGERON — CRACKED (BS 1041)

MHV - FOUND STATION 1041, STATION 1051 LONGERON NR 17 CRACKED BOTH MARKED IN RED. REMOVED AND REPLACED LONGERON NR 17 STATION 1041 AND 1051 AND SHOVEL CUPS PER SRM 51-10-1 AND 51-30-2 LONGERON INSTALLED USING EXISTING SPLICES. (M)

Part: FLOORBEAM — CRACKED (BS 237)

MHV - FORWARD CARGO CABIN FLOORBEAM STATION 237 LEFT 10 INCH CRACK IN FLOORBEAM AT SERVO FULLY BRACKET EXISTING REPAIR NEEDS FURTHER EVALUATION. COMPLETED REPAIR IAW DC9 SRM 53-05 AND RESEMBLE CARGO PANELS. (M)

Part: ANGLE — CRACKED (BS 710)

MHV - RIGHT WING ROOT AREA .5 INCH CRACK INDICATION ON ANGLE 5910465-340 TO CENTER WING BOX APPROX BODY STATION 710. NDT VERIFY CRACK IN ANGLE. REMOVED AND REPLACED ANGLE AIW DC9 SRM 51-10-2, 51-10-4 AND 51-30-5. REINSTALLED FAIRINGS 3 PANELS OPENED FOR ACCESS IAW DC9 SRM 51-30-1. (M)

Part: BATTERY PACK — DISCHARGED (COCKPIT)

MHV - FLT 951A - COCKPIT OVERHEAD EMERGENCY LIGHT OUT. TROUBLESHOT SYSTEM, FOUND EMERGENCY BATTERY PACK WITH DEAD BATTERIES. REPLACED BATTERIES ON JOB CARD. LIGHTS WORK CARD. (X)

Part: SKIN — DENTED (BS 313)

MHV - FORWARD FUSELAGE SKIN AT STATION 313 NEAR BOTTOM OF FUSELAGE HAS A 1.5 INCH BY 1 INCH DENT. CUT OUT DAMAGE IAW DC9 SRM 53-04 FIG 38 VIEW 1. FABRICATED DOUBLER AND FILLER INSTALLED REPAIR COMPLETE IAW SRM 53-04 FIG 38 AND DC9 SRM 51-30-2. (M)

Part: CLIP — CRACKED (BS 1041)

MHV - STATION 1041 LEFT SIDE A/C FORWARD SIDE OF FRAME SHEER CLIP BETWEEN LONGERON 16 AND 17 CRACKED. REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-01 PAGE 1 APPLIED SEALANT IAW DC9 SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IAW SRM DC9 51-30-2 PAGE 6 FIG 5. (M)

Part: LIGHT — INOPERABLE (CABIN)

ACY - FLT 168 - FORWARD FLOOR EMERGENCY TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP. OPERATIONAL CHECKS GOOD IAW MM 33-51-1. (X)

Part: WIRE — BROKEN (CABIN)

ACY - FLT 19 - EMERGENCY AISLE LIGHTS INOPERATIVE. FOUND BROKEN WIRE ON FORWARD SECTION OF AISLE LIGHTS REPAIRED SAME, OPERATIONAL CHECK NORMAL IAW 33-53-0. (M)

Part: WIRE — BROKEN (CABIN)

ACY - FLT 19 - EMERGENCY AISLE LIGHTS INOPERATIVE. FOUND BROKEN WIRE ON FORWARD SECTION OF AISLE LIGHTS. REPAIRED SAME OPERATIONAL CHECKS NORMAL IAW 33-53-0. (M)

Part: BATTERY — DISCHARGED (CABIN)

ACY - FLT 348 - ON PREFLIGHT, FIVE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED NICAD BATTERIES AND BULBS WHERE NEEDED IAW MM 33-40 AND OPERATIONAL CHECKS OK. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MCO - FLT 127 - CABIN EMERGENCY FLOOR PATH LIGHTING HAS AN AREA OF LIGHT BULBS THAT DO NOT ILLUMINATE. REPAIRED AND REPLACED WIRING POWER FEED STRIP CONNECTION FOR CENTER SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FORWARD SECTION OF EMERGENCY FLOOR LIGHTING (EXIT) INOPERATIVE. REMOVED AND REPLACED FORWARD SECTION OF FLOOR LIGHT IAW MM 33-50-00, PERFORMED OPERATIONAL CHECK ON SYSTEM, NO DEFECTS NOTED. (M)

Part: BATTERY PACK — DISCHARGED (LT NACELLE)

DTW - LEFT EXTERIOR EMERGENCY NACELLE SCANNING LIGHT INOP. REMOVED AND REPLACED REAR POSITION EMERGENCY BATTERY PACK AT REAR CARGO COMPARTMENT LOCATION IAW DC-9 MM 33-53-0, PAGE 406. OPS CHECK GOOD. (M)

Part: CIRCUIT BREAKER — TRIPPED (PROX SW CNTRL)

ACY - FLT 185 - ON LANDING, ALL THREE GEAR UNSAFE LIGHTS CAME ON AND WARNING HORN SOUNDED. FOUND CIRCUIT BREAKER FOR PROXIMITY SWITCH CONTROL TRIPPED (Z-21). RE-SET CIRCUIT BREAKER. ALL LIGHTS CHECK NORMAL. (X)

Part: PROX SENSOR — FAILED (RT MLG)

DTW - FLT 621 - RIGHT MAIN GEAR RED LIGHT ON RETRACTION. AFTER EXTENDING GEAR, GREEN LIGHT FLASHING ON AND OFF WHILE RED FLASHED OFF AND ON. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK WARNING PROXIMITY SENSOR IAW MM 32-60-1. JACKED AND PERFORMED GEAR SWING. OPS CHECK GOOD. NO DEFECTS NOTED. (M)

Part: PROX SENSOR — FAILED (LT MLG)

ACY - FLT 112 - LEFT RED GEAR UNSAFE LIGHT STAYED ON FOR ENTIRE FLIGHT. PERFORMED APPROPRIATE CHECK LISTS AND CONTINUED FLIGHT PER RESTRICTIONS IN FCOM. INSPECTED AND CLEANED ALL ASSOCIATED PROX SENSORS AND TARGETS ON LEFT MAIN LANDING GEAR. RELEASED FOR TEST FLIGHT ONLY TO CHECK GEAR LIGHT INDICATOR. TEST FLIGHT FAILED. LEFT RED GEAR UNSAFE LIGHT STAYS ON. REMOVED AND REPLACED PROXIMITY SENSOR IN THE LEFT LANDING GEAR DOWNLOCK POSITION IAW DC-9 MM 32-60-1, CODED 15. SYSTEM CHECKS NORMAL AS OUTLINED IN 32-60-1, CODE 15. OK FOR SERVICE. (X)

Part: ANTI SKID SYSTEM — MALFUNCTIONED (LANDING GEAR)

MYR - DURING TAXI OUT, THE LT AND RT INBD ANTI-SKID ANNUNCIATOR ILLUMINATED. RETURNED TO GATE. TRANSFERRED TO DMI NR 00552 PER MEL 32-4. PLACARD INSTALLED, DISPATCH NOTIFIED. PERFORMED ANTI-SKID SYSTEM TEST IAW DC-9 MM 32-43-0. OPS CHECK GOOD. DISPATCH NOTIFIED BY MAINTENANCE CONTROL. THIS CLEARS DMI NR 00552. (X)

Part: AUTOPILOT — MALFUNCTIONED (E/E COMPT)

FLT 503 - MCO - AUTO-PILOT WILL NOT HOLD ALTITUDE IN CRUISE, AT FL 290 OR 310. AIRCRAFT CLIMBS AT A STABLE 300 FPM WITH THE VERTICAL SPEED WHEEL IN THE DETENT. ASSIGNED TO DMI. DMI NR 00294 IAW MEL 22-16-6 NOTIFIED. MAINTENANCE CONTROL AND PLACARDED CONTROLLER AS REQUIRED. RAN TESTS ON PITCH COMPUTER IAW DC-9 MM 22-10-00. CHECKS GOOD. SYSTEM GROUND CHECKS GOOD, CLEARS DMI NR 00294. (M)

Part: AIR DATA COMP — FAILED (NR 2)

DTW - FLT 566 - CO-PILOT'S ALTIMETER NEEDLE OSCILLATES CONSTANTLY AT ALL ALTITUDES. FOUND NR 2 AIR DATA COMPUTER SERVO OUTPUTS BAD. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD IAW DC-9 MM CH 34-12-0. (M)

Part: AIR DATA COMP — MALFUNCTIONED (NR 2)

DTW - FLT 566 - WITH AUTO-PILOT ENGAGED, YOKE FLUTTERS BACK AND FORTH. FOUND NR 2 AIR DATA COMPUTER OUTPUTS BAD. REFERENCE MRR GTIA9700255 FOR REMOVAL AND REPLACEMENT OF NR 2 AIR DATA COMPUTER. SYSTEM OPS CHECK GOOD IAW DC-9 MM CHAPTER 22-10-0. (M)

Part: CONNECTOR — DIRTY (RT ADC)

DTW - FLT 566 - AT 8000 FEET AUTO-PILOT PULSED AS F/O ALTIMETER OSCILLATED PLUS/MINUS 20. THIS CONTINUED UNTIL AUTOPILOT WAS DISENGAGED, YOKE ALSO PULSED. REMOVED AIR DATA COMPUTER, CLEANED CONNECTORS, REINSTALLED SAME, PERFORMED AIR DATA INSTRUMENT AND ALTIMETER PITOT STATIC IAW MM 34-10-0 AND 34-10-6. AUTO-PILOT OPS CHECK SATISFACTORY IAW MM 22-10-5. (M)

Part: CONNECTOR — LOOSE (RT ALTIMETER)

DTW - FLT 640 - F/O'S BARO-ALTIMETER BOUNCES PLUS/MINUS 20 FEET WHICH IN TURN CAUSED AUTO-PILOT TO CYCLE RAPIDLY IN PITCH (NOT BIG VARIATIONS, BUT CONSTANT). FOUND BAD CONNECTION AT F/O'S ALTIMETER, SECURED AND RECONNECTED F/O'S ALTIMETER. OPS CHECK NORMAL IAW DC-9 MM 34-16. (M)

Part: WINDOW — STUCK (RIGHT COCKPIT)

DTW - FLT 640 - RIGHT SIDE COCKPIT WINDOW WILL NOT OPEN. FOUND GUIDE PIN AT UPPER LINKAGE ROD OUT OF TRACK. RE-INSTALLED GUIDE PIN AND CHECKED WINDOW OPERATION REPEATEDLY IAW MM 56-10-3. OPS CHECK GOOD. (X)

Part: CONNECTOR — DIRTY (RT WING)

DTW - FLT 640 - RIGHT ICE PROTECT TEMP LOW LIGHT DID NOT ILLUMINATE WHEN AIRFOIL ANTI-ICE SELECTED ON. LIGHT DID TEST, BUT DID NOT ILLUMINATE WITH THE RIGHT ICE PROTECT TEMP LOW LIGHT, WAS ABLE TO DUPLICATE DISCREPANCY. CLEANED ELEC CONNECTOR AT RIGHT AIRFOIL. ANTI-ICE LOW TEMP SENSOR SYSTEM OPS CHECK GOOD IAW 30-10-0. (M)

Part: PRESSURE SWITCH — FAILED (AIRFOIL DE-ICE)

DTW - FLT 6337 - CREW RETURNED TO DTW AFTER INDICATION OF A POSSIBLE ANTI-ICING DUCT LEAK IN THE WING ANTI-ICE SYSTEM. AIR FOIL ICE PROTECTION PRESSURE ABNORMAL. ANNUNCIATOR REMAINED ON WHEN AIR FOIL ICE PROTECTION WAS UTILIZED (NORMAL DUCT PSI OF PLUS OR MINUS 40). ANNUNCIATOR WENT OUT WHEN TAIL DE-ICE WAS SELECTED BUT THEN RE-ILLUMINATED WHEN SYSTEM SWITCHED AUTOMATICALLY BACK TO WING ANTI-ICE. REMOVED AND REPLACED WING ICE PROTECTION PRESSURE SWITCH IAW MM CHAPTER 30-10-10, PAGE 201. (M)

Part: LIGHTS — INOPERATIVE (CABIN)

DTW - FLT 1130 - COCKPIT EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHTS BATTERIES. OPS CHECK GOOD. (M)

Part: LIGHTS — INOPERATIVE (CABIN)

DTW - FLT 1130 - COCKPIT EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHTS BATTERIES. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FLT 626 - FORWARD EMERGNCY FLOOR LIGHTING UNDER FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. MAINTENANCE REPLACED LIGHTING STRIP UNDER FORWARD FLIGHT ATTENDANT SEAT. OPERATIONAL CHECK SATISFACTORY IAW MM 33-50. (M)

Part: CLAMP — LOOSE (PNEU DUCT)

REF MRR NR 96NK213. LOG/ITEM NR 027691/M293. IN-FLIGHT, BOTH SMOKE DETECTORS WENT OFF. FINDINGS: AFTER INSP, TESTS, AND INVESTIGATION OF CAUSE, FOUND PNEUMATIC DUCTING CLAMP CAME LOOSE AND CAUSED INSTALLATION TO SEPARATE AND AIRBORNE DUST ENTERED THE AIR CYCLE MACHINE, AND PARTICLES FORMED IN CABIN AREA, AND TAIL CONE AREA SETTING OFF SMOKE DETECTORS. FCD GENERATED TO CHECK FLEET FOR SIMILAR PROBLEM. PNEU DUCT CLAMP FAILURE. (X)

Part: PACK — SMOKING (RIGHT)

LOG PAGE NR 028018. ITEM NR P287. AT 18,000 FEET IN DESCENT, BOTH SMOKE DETECTORS WENT OFF. COULD SMELL ELECTRICAL SMOKE (STINKY AND HAZY IN BACK). INSPECTION THE SUSPECT LOCATION OF THE SMOKE-RUNNING RIGHT PACK, BLEW SMOKE FROM PACK. ITEM DEFERRED BY WANER AVIATION (FLL). ACTUAL LOG SHEET PENDING - WILL SEND MRR FOLLOW-UP REPORT ASAP. (X)

Part: WIRE — BROKEN (CABIN)

LOG PAGE 028953. EMERGENCY FLOOR TRACK LIGHTING BY F/A FORWARD JUMP SEAT PARTIALLY NOT ILLUMINATED. REPAIRED BROKEN WIRE TO FLOOR TRACK LIGHTING. OPS CHECK GOOD. (X)

Part: SMOKE DETECTOR — INOPERATIVE (RT AFT LAV)

LOG PAGE 27064. RIGHT LAVATORY SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED RIGHT LAVATORY SMOKE DETECTOR IAW DC-9 MM CHAPTER 26. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DIRTY (CABIN)

LOG PAGE 05466. COCKPIT EMERGENCY LIGHTS WILL NOT TEST WITH EMERGENCY LIGHT SWITCH. CLENAED CONNECTORS ON BATTERY PACK. SYSTEM OPS CHS GOOD. (X)

Part: FUEL CONTROL — OUT OF TRIM (NR 1 ENGINE)

LOG PAGE 07467. ABORTED TAKEOFF. NR 1 ENGINE WOULD NOT PRODUCE TAKEOFF POWER MAX EPR 1.93 MAX N1 94.1 PERCENT, N2 100.1 PERCENT. CHECKED PT2 LINES FOR LEAKS, BLEW OUT (CLEANED). PERFORMED ENGINE TRIM RUN PER MM 71-00. ALL INDCATIONS CHECK NORMAL. LOCAL TEMPERATURE DROPPED 12 DEGREES. (X)

Part: BATTERY — DISCHARGED (CABIN)

MIDDLE SECTION OF EMERGENCY LIGHT TRACK DOES NOT ILLUMINATE. REMOVED AND REPLACED NICAD BATTERIES IAW DC-9-MM 33-50. (X)