N12505

Part: FUSE — BLOWN (CABIN)

DTW - TAIL CONE CATWALK EMERGENCY TRACK LIGHTING INOPERATIVE. INSTALLED FUSE IN BATTERY PACK, OPERATIONAL CHECK GOOD. (X)

Part: POWER SUPPLY — FAILED (CABIN)

AFT STAIRWAY EMERGENCY TRACK LIGHTING INOP. FOUND BURNED OUT POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY IAW MM 33-50-00, OPERATIONAL CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

ACY - FLT 119 - CABIN FLOOR LIGHTING REAR EMERGENCY EXIT ROW NEEDS FIXING. REPAIRED WIRING AT SEAT TRACK SEAT 11 IAW W/D 33-51-03. GROUND OPS CHECK OK. (M)

Part: BULB — FAILED (CABIN)

DTW - ONE RED FLOOR PATH LIGHT INOPERATIVE AT FORWARD EMERGENCY EXIT ROW 14. REPLACED ONE FLOOR PATH BULB ASSEMBLY. OPS CHECK GOOD IAW MM 33-50. (M)

Part: BRAKE BLEEDER — LOOSE (RT MLG)

MSP - FLT 900 - ON LANDING AT MSP, TOWR REPORTED SMOKE FROM RIGHT GEAR AREA. INSPECTED RIGHT MLG FOUND NR 4 BRAKE LEAKING FROM BLEEDER. PARTS TIGHTENED SECURELY AND SAFETIED. OPS CHECK GOOD, NO LEAKS NOTED. (M)

Part: CONTROL CABLE — BROKEN (LT TE FLAP VANE)

DTW - FLT 420 - LEFT INBD FLAP MOVEABLE VAN CABLE 168A, FOUND BROKEN. REMOVED AND REPLACED LEFT INBOARD FLAP MOVEABLE VANE CABLE IAW MM 37-51-2. RIGGED/ADJUST TEST ALSO IAW MM 27-51-2. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MYR - FLT 1601 - EMERGENCY EXIT LIGHTS OVER WING 1/2 EACH INOPERABLE. (EXIT ROW 15). REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK WITH SERVICEABLE BATTERIES IAW DC-9 MM 33-50. OPERATIONAL CHECK GOOD AT OVER THE WING EMERGENCY EXIT ROW 15. (X)

Part: POWER SUPPLY — INOPERABLE (CABIN)

MYR - FLT 1601 - EMERGENCY EXIT LIGHTS OVER WING 1/2 EACH INOPERABLE. (EXIT ROW 15.) REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK WITH SERVICEABLE BATTERIES IAW DC-9 MM 33-50. OPERATIONAL CHECK GOOD. (X)

Part: ADI — FAILED (RT COCKPIT)

DTW - FLT 177 - AFTER PUSHBACK AND ENGINE START, FO ADI PROCESSED 30 DEGREES TO THE RIGHT, AND ROLL ANNUNCIATOR ON COMPARATOR PANEL ILLUMINATED. REMOVED AND REPLACED F/O'S ADI. OPS CHECK GOOD IAW DC-9 MM 34-22-0. (M)

Part: LENS — BROKEN (CABIN)

MYR - FLT 111A - EMERGENCY FLOOR TRACK LIGHT SOCKET AND LENS BROKEN AT ROW 14 D, E, F. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT SOCKET AND LENS (RED) AND ROW 14 D, E, F AND RE-LAMPED SOCKET IAW DC-9 MM 33-50. OPS CHECK GOOD. REFERENCE GTIA9700339.

Part: SOCKET — BROKEN (CABIN)

MYR - FLT 111A - EMERGENCY FLOOR TRACK LIGHT SOCKET AND LENS BROKEN AT ROW 14 D, E, F AND RE-LAMPED SOCKET IAW DC-9 MM 33-50. OPS CHECK GOOD. (M)

Part: WIRE — FAILED (ELEVATOR POWER)

ACY - FLT 186 - DURING TAXI OUT, NO ELEVATOR POWER ON TEST. RETURNED TO GATE. TRANSFERRED TO DMI NR 000659 PER MEL 27-14, CAT 'C'. PLACARDS INSTALLED. REPAIRED WIRES AT PRESSURE SWITCH. OPS CHECK NORMAL IAW MM 27-30-12. THIS CLEARS DMI NR 00659. PLACARDS REMOVED. (X)

Part: LIGHT — MISSING (CABIN)

MYR - FLT 243 - EMERGENCY FLOOD TRACK LIGHT SYSTEM MISSING RED EXIT LENS COVER AND LIGHT BULB AT ROW 15 D, E, F. RELAMPED EMERGENCY FLOOR TRACK LIGHT BULB AT ROW 15, D, E, F AND INSTALLED RED LENS COVER ON FLOOD TRACK. OPS CHECK GOOD. (M)

Part: SLIDE PACK — FELL OFF (PAX DOOR)

DTW - FLT 174 - MAIN DOOR SLIDE PACK FELL OFF. INSTALLED L1 EMERGENCY ESCAPE SLIDE IAW DC9 MM 25-61-0. (M)

Part: DOOR — NOT LATCHED (PAX COMPT)

MYR - FLT 243 - 'AFT CABIN DOOR' CAUTION LIGHT ILLUMINATED DURING DESCENT AND REMAINED ON. NO OTHER INDICATIONS. INSPECTED AND FOUND DOOR HANDLE TO BE PARTIALLY OPEN, CYCLED DOOR HANDLE CLOSED, LIGHT OUT. LIGHT AND DOOR CHECKS NORMAL. OK TO CONTINUE. (M)

Part: LOGO LIGHT — MISSING (RIGHT)

MYR - FLT 1701 - RIGHT LOGO LIGHT DISCOVERED MISSING ON POST FLT INSPECTION. TRANSFERRED TO DMI NR 00292 PER MEL 33-23. CAT 'C'. BOS, INSTALLED LAMP, LOUVER AND CLIPS ON RT LOGO IAW DC-9 MM CHAPTER 33. OPS CHECK GOOD. CLEARS DMI NR 00292. (M)

Part: WHEELS — LOOSE (NOSE LAND GEAR)

FLT 301 - ACY - NOSE GEAR VIBRATES BADLY ON TAKEOFF, FEELS OUT OF BALANCE. SNUBBER DOES NOT SEEM TO STOP IT ON GEAR UP. RE-TORQUED BOTH NOSE TIRES IAW MM CHAPTER 32-40-2. NO TIRE DEFECTS NOTED. (M)

Part: BREAKER — TRIPPED (LEFT)

FLT 195 - BOS - AT BOSTON AFTER ENGINE STARTS, LEFT ENGINE GENERATOR DROPPED OFF LINE. CAPTAIN RESET IT ON AND CROSS TIE LOCK OUT CAME ON. WENT BACK TO GATE AND RESET CROSS TIE. RESET LOCK OUT TIE BREAKER. OPS CHECK OK IAW 24-50. (M)

Part: SLIDE — MALFUNCTIONED (CABIN DOOR)

CIT - FLT 851 - FORWARD CABIN DOOR SLIDE FELL OFF AND INFLATED WHEN DOOR WAS OPENED. REMOVED AND REPLACED FORWARD ENTRY DOOR SLIDE IAW MM 25-62. OK FOR SERVICE. INSPECTED INSTALLATION OF FORWARD ENTRY DOOR SLIDE PER MM 25-62-0. (M)

Part: ENGINE — FAILED (NR 2)

DTW - FLT 626 - IN CRUISE CONFIGURATION, NR 2 THROTTLE SPLIT 3.50 INCHES WITH NR 1 THROTTLE. NR 2 EGT AND FUEL FLOW HIGH, DURING ENGINE ACCELERATION COMPRESSOR STALLS WERE EXPERIENCED ON NR 2 ENGINE. CORRECTIVE ACTION: MAINTENANCE INSPECTED NR 2 ENGINE AND DECLARED AN ENGINE CHANGE. ENGINE REMOVED AND REPLACED WITH A SERVICEABLE ENGINE. MRR TO REMAIN OPEN UNTIL A TEAR DOWN REPORT IS RECEIVED FROM ENGINE REPAIR FACILITY. PART TOTAL CYCLES, 36,637. (X)

Part: OIL CAP — LOOSE (NR 1 ENGINE)

DTW - FLT 423 - IN CLIMB CONFIGURATION, FLIGHT CREW OBSERVED NR 1 ENGINE OIL QUANTITY DECREASE FROM 16 QUARTS TO 6 QUARTS. RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE OIL TANK SERVICE CAP NOT SECURED. SERVICED ENGINE WITH OIL, SECURED OIL CAP. ENGINE RUN-UP CHECKED NORMAL IAW DC 9 MM, CHAPTER 79-11-0. ACCOMPLISHED AN OVERWEIGHT LANDING INSPECTION IAW DC 9 MM 5-51-0 AND NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FUSE — BLOWN (CABIN)

AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED BLOWN FUSE IN BATTERY PACK, OPERATIONAL CHECK GOOD IAW DC-9 MM CH 33-53-01. (M)

Part: PRESSURE SYSTEM — FAILED (CABIN)

AIRCRAFT LOG PAGE NR 028813, ITEM NR P744 - PRESSURIZATION FAILED ON TAKEOFF OUT OF ACY. RETURNED ON TAKEOFF, OUT OF ACY. RETURNED FOR MAINTENANCE INSPECTION. DEFERRED PRESSURIZATION IAW MEL 21-24, DMI NR 2595. (M)

Part: SEAT BELT — CUT (CABIN)

FORWARD LIGHT ATTENDANT JUMPSEAT OUTBOARD SEAT BELT INBOARD HARNESS STRAP CUT AND FRAYED. REPLACED SEAT BELT HARNESS STRAP. (M)

Part: FLOOR SUPPORT — EXFOLIATED (BS 160-200)

DURING C-CHECK, FOUND FORWARD ENTRY DOOR WAY FLOOR SUPPORT MEMBER AT FS 160-200 EXFOLIATED. FABRICATED, TREATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-1, 51-30-0, 51-10-3. (M)

Part: RIB CAP — CORRODED (BS 930)

DURING C-CHECK, FOUND CORRODED RIB CAP IN AFT CARGO COMPARTMENT STATION 930 LEFT. FABRICATED, TREATED AND INSTALLED NEW RIB CAP IAW SRM 51-10-3, 51-10-1 AND 51-10-4. (M)

Part: MEMBRANE — CORRODED (BS 180)

DURING C-CHECK, FOUND LEVEL 2 CORROSION IN GALLEY DOOR ENTRY WAY AT FS 180 AND APPROX 40 INCHES RIGHT OF CENTERLINE. ALSO, MEMBRANE HAS CORROSION UNDER THE SEAM AREA. REMOVED CORROSION AND REPLACED MEMBRANE, TREATED AREA IAW 53-10, 51-10-3 AND 51-30-0. (M)

Part: FLOOR SUPPORT — CORROSION (BS 160-200)

DURING C-CHECK, FOUND UNDER FLOOR MEMBRANE CORRODED ALONG FLOOR SUPPORT MEMBER BETWEEN FS 160-200, 36 INCHES LEFT OF CENTER. FABRICATED, TREATED AND INSTALLED NEW MEMBRANE IAW SRM 53-01, 51-10-03, AND 51-30-0. (M)

Part: STRAP — CORRODED (BS 327)

DURING C-CHECK, FOUND FORWARD CARGO BAY STATION 327 TO 370, RIGHT SIDE RBL 17 FLOOR BOARD SUPPORT STRAP CORRODED. FABRICATED SUPPORT STRAP AND TREATED CORROSION IAW SRM 53-03, 51-10-3. (M)

Part: FLOOR SUPPORT — CORROSION (BS 160-200)

DURING C-CHECK, FOUND FLOOR SUPPORT MEMBER IS GALLEY SERVICE DOOR ENTRYWAY, 36 INCHES RIGHT OF CENTER CORRODED ALONG TOP OF FLANGE. FABRICATED, TREATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-1, 51-30-0 AND 51-10-3. (M)

Part: FLOOR BOARD — CORRODED (COCKPIT)

DURING C-CHECK, FOUND CENTER COCKPIT FLOOR BOARD CORRODED. FABRICATED, TREATED AND INSTALLED REPLACEMENT FLOOR BOARD IAW 51-10-2, 51-10-3, 51-30-0 AND 51-20-0. (M)