N447AM

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT)

FWD RT EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY 43WL.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

RIGHT FORWARD EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REPLACED BULB.

Part: SWITCH — MISSING (AUDIO) · airframe 29,731 hrs · 33,329 cycles

THE CREW REPORTED THE EMERGENCY AUDIO CANCEL SWITCH IS MISSING TOGGLE SWITCH; IS STILL SAFETY WIRED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY AUDIO CANCEL SWITCH 12WW IAW STANDARD PRACTICES MM CAP 20-27-13 . THE OPS TEST IAW JIC 31-50-00-10000 WAS OK. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 29,716 hrs · 33,305 cycles

DURING MX INSPECTION, FOUND HALF THE LIGHTS OF FOWARD AISLE EVACUATION PATH LIGHTS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FWD EMERGENCY LIGHT POWER SUPPLY 43WL AND CLEANED FLOOR PROXIMITY ESCAPE PATH STRIP LIGHT CONNECTOR 55WL(B) IAW JIC 33-51-21, RAI 10000 AND ASM 33-51-00. THE OPS TEST WAS SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,550 hrs · 33,074 cycles

THE CREW REPORTED THE NR 2 F/A FLASHLIGHT WAS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 2 F/A FLASHLIGHT IAW MM 25-60-00. THE OPS CHECKED WAS GOOD. THE ACFT WAS RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 29,499 hrs · 33,015 cycles

FLIGHT 4888, CREW REPORTED THAT THE LANDING GEAR HANDLE WAS STUCK ON THE DOWN POSITION, WOULD NOT MOVE. THE CREW ELECTED TO RETURN TO DEPARTURE. ACFT REMOVED FROM SERVICE. CHECKED AND FOUND ON LT MAIN GEAR PROXIMITY SWITCH 50 GB WITH BROKEN ELECTRICAL PIN. REPLACED PROXIMITY SWITCH 50 GB IAW JIC 32-61-00 -RAI-10000. CHECKED OK IAW JIC 32-31-81.OPT-00100 & REMOVED AND INSTALLED OF LANDING GEAR CONTROL LEVEL- TEST JIC32-31-81. ACFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,311 hrs · 32,789 cycles

DURING PS-1 INSPECTION CHECK, FOUND EMERGENCY FLOOD LIGHT IN FRONT OF GALLEY INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT BULB IAW JIC 33-51-24. OPS CHECKED SATISFACTORY. ACFT RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE · airframe 29,209 hrs · 32,645 cycles

DURING MX INSPECTION FOUND THE EMERGENCY BATTERY WITH LOW VOLTAGE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY BATTERY IAW WORK CARD EX-243185-RAI-10020-002. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (RT WING) · airframe 28,926 hrs · 32,265 cycles

DURING MX INSPECTION, FOUND CORROSION AT BLENDED AREAS OF RT WING, LOWER SKIN EXT SURFACE OF FUEL PUMP CUT-OUT. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO E2-5700-487. THE ACFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 28,926 hrs · 4,815 cycles

DURING MX INSPECTION, FOUND THE LT WING BETWEEN RIBS 4 AND 5 WATER DRAIN VALVE CUTOUT WITH CORROSION. PERFORM PERMANENT REPAIR IAW PART B OF EO E2-5700-488 AT PRIOR TO THE NEXT SCHEDULE C CHECK. TEMPORARY DISPOSITION FOR CORROSION DAMAGE TO THE LOWER LT WING BETWEEN RIB 4 & 5 WATER DRAIN CUTOUT E2-5700-488. THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (RT WING) · airframe 28,926 hrs · 32,265 cycles

DURING MX INSPECTION, FOUND THE RT WING FUEL FEEDER TANK WATER DRAIN HAS MATERIAL REMOVED DURING CORROSION REMOVAL. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED BLEND OUT AND REPAIR AT RT WING LOWER SKIN AT WATER DRAIN BTW RIB 4-5 IAW EO E2-5700-489. THE ACFT WAS RETUNRED TO SERVICE.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 28,926 hrs · 32,265 cycles

DURING MX INSP FOUND THE LT WING LOWER SKIN RIB NR 5 FUEL DRAIN VALVE SURROUNDING AREA WITH CORROSION. THE ACFT WAS REMOVED FROM SERVICE. FOLLOWING TURNOVER PERFORMED ALL REMAINING STEPS EO E2-5700-488. C/W E2-5700-488 LOWER WING BETWEEN RIB 4 & 5 BLEND OUT. THE ACFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (RT WING) · airframe 28,926 hrs · 4,815 cycles

DURING MX INSPECTION, FOUND THE RT WING BTW RIB 5-6 MAGNETIC FUEL IND. WITH CORROSION. COMPLIED WITH CORROSION BLEND OUT EO E2-5700-486. THE ACFT WAS RETUNRED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,875 hrs · 32,191 cycles

DURING FLIGHT, THE F/A REPORTED STRONG FUEL ODOR ROWS 1 - 4. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF UPPER AND LOWER WING SKINS FOR LEAKS, NO LEAKS FOUND IAW MM 28-11-00 AND 57-11-00, LOWERED OVERHEAD BINS 1CD - 10CD AND 1AB - 4AB IAW MM 25-24-21; INSPECTED AREA, NO ODORS OR LEAKS NOTED. PERFORMED RUN-UP & NO LEAKS FOUND IAW MM 72-00-00 NEITHER FUEL ODOR DETECTED DURING RUN-UP, FUEL SYS WORKING PROPERLY. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 28,758 hrs · 32,034 cycles

DURING MX INSPECTION, FOUND CORROSION AT LT WING LOWER SKIN T/E BETWEEN RIB 7 & 8. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED CORROSION TREATMENT IAW EO E2-5700-482. THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (LT WING LOWER) · airframe 28,747 hrs · 32,020 cycles

DURING INSP, FOUND CORROSION AT LT WING LOWER SKIN T/E BETWEEN RIB 7 AND 8. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED LT WING CORROSION TREATMENT ON RIB 7 STIFFENER 10 IAW EO E2-5700-482. THE ACFT WAS RETURNED TO SERVICE.

Part: BRAKE ASSY — UNKNOWN (MLG) · airframe 28,498 hrs · 31,651 cycles

ON FLIGHT 4819, THE CREW REPORTED THE LT SIDE BRAKES ARE GRABBING WHEN MINIMUM PRESSURE IS APPLIED TO THE BRAKE PEDAL. A STRONG BURNING ODOR BY LT BRAKE ASSEMBLY AND WARM AIR FROM SAME SIDE ASSY WAS REPORTED. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF BRAKES AND PERFORMED OPS CHECK IAW 32-42-00. FOUND SYS WORKING PROPERLY. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,443 hrs · 31,589 cycles

DURING MX BASE VISIT FOUND THE RT AFT FUSELAGE EMERGENCY FLOOD LIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED OPS CHECK ON THE RT AFT FUSELAGE EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: GUARD — DEFORMED (SMOKE DETECTOR) · airframe 28,258 hrs · 31,355 cycles

CREW REPORTED THE METAL GUARD FOR SMOKE DETECTOR IN C2 CARGO COMPARTMENT IS DEFORMED AND MISSING A SCREW. ACFT REMOVED FROM SERVICE. INSTALLED NEW GRILL ON FORWARD CARGO SMOKE DETECTOR IAW JIC 26-15-21 RAI 10000-001. ACFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,220 hrs · 31,308 cycles

EMERGENCY LIGHT, BULB INOPERATIVE, AREA M, ROW 5. DEFERRED IAW MEL 33-29, AUTH 120028D-C.

Part: BATTERY — DISCHARGED · airframe 28,170 hrs · 31,260 cycles

EMERGENCY BATTERY IS LOW. R & R EMERGENCY BATTERY IAW W/C EX 243185, RAI 10020-002.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,099 hrs · 31,174 cycles

MAIN CABIN LT SIDE EMERGENCY LIGHT OUT TOWARD FRONT AND MIDDLE. R & R POWER SUPPLY 43WL IAW 33-51-21 AND USED WC EX335000 OPT 10000-001 AND EX335121 RAI10010-006.

Part: BATTERY — DISCHARGED · airframe 28,069 hrs · 31,137 cycles

EMERGENCY BATTERY VOLTAGE LOW, .7 VOLTS. R & R EMERGENCY BATTERY IAW JIC 24-31-85, RAI-10020. WC EX-243185-RAI-10020-001 SATISFACTORILY ACCOMPLISHED.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,925 hrs · 30,987 cycles

DURING CRUISE AT 17,000 FT THERE WAS A STRONG ELECTRICAL ODOR ON THE FLIGHT DECK. CONSULTED WITH THE F/A WHO CONFIRMED THE ODOR. WERE IN VMC CONDITIONS AT THE TIME, HOWERVER HAD LEVEL 2 ICING ON AS WE HAD JUST EXITED ICING CONDITIONS. DURING DESCENT WENT TO LEVEL 1 ICING AND FUMES WENT AWAY. ALSO UPON LANDING THE LIGHT BY THE OBSERVERS MASK ILLUMINATED. OPENED ALL OVERHEAD STOWAGE COMPARTMENTS AND INSPECTED ELECTRICAL CONNECTIONS. NO FAULTS FOUND. OAC IAW JIC 25-24-21. OPENED AVIONICS RACKS ACCESS DOORS AND FWD AVIONICS COMPARTMENT. PERFORMED BOTH ENGINE RUN UP WITH ALL ELECTRICAL SYS OPERATING, ANTI-ICE AND DE-ICE SYS OPERATING FOR 30 MINS AND NO FAULTS AND ELECTRICAL ODOR NOTICED AT THIS MOMENT. RUN-UP IAW JICS 72-00-00, 30-42-00 AND 30-61-00. ATA 30 JICS FOR DE-ICE & ANTI-ICE.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 27,632 hrs · 30,653 cycles

THE F/A REPORTED THE EMERGENCY FLOOD LIGHT ON STAIRS IS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. SECURED WIRE ON CONNECTOR IAW AWM 33-50-00. NO PARTS R & R. THE OPS CHECK WAS OK. THE ACFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

F/A EMERGENCY LIGHT PUSHBUTTOM LAMP INOP. R & R F/A EMERGENCY LIGHT PUSHBUTTOM LAMP IAW AMM/JIC 33-50-00.

Part: LIGHT — OUT OF ALIGNMENT (EMERGENCY EXIT) · airframe 27,417 hrs · 30,395 cycles

EMERGENCY EXIT LIGHT ON MAIN CABIN STAIRS OUT OF ALIGNMENT. R & R EMERGENCY LIGHT FIXTURE IAW JIC 33-51-24, RAI 10000-002.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 27,353 hrs · 30,320 cycles

MAIN PASSANGER DOOR EMERGENCY LIGHT INOP. R & R PAX DOOR EGRESS LIGHT ASSY. (FLOOD LIGHT) OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 27,222 hrs · 30,160 cycles

MAIN CABIN ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. RELAMP MAIN CABIN ENTRY IAW JIC 33-50-00. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (LT MLG WOW) · airframe 26,526 hrs · 29,367 cycles

LT MAIN GEAR WOULD NOT RETRACT AFTER T/O STAYED DOWN AND LOCKED PLUS RED UNLOCK WAS ON, (DECLARED EMERGENCY) PLACED ON MEL 32-03 AUTH NR110015DMC. CLEANED CORRODED CONNECTOR AT LT MLG WOW PROX SWITCHES 50GB & 51GB, RESECURED WIRE BUNDLE TO SELECTOR VALVE 13GA, REF 72AWM SP 29-27-17. PERFORMED LANDING GEAR EXTENSION & RETRACTION IAW JIC 323100-FUT-10000. FUT GOOD, MEL 32-03 RESTORED.

Part: LIGHT — BROKEN (GALLEY) · airframe 26,363 hrs · 29,185 cycles

GALLEY AREA EMERGENCY LIGHT FLOOR STRIP (FWD) BROKEN. RAI GALLEY AREA FWD EMERGENCY LIGHT FLOOR STRIP IAW MM 33-52-10. OPS CHECK GOOD.

Part: FUEL NOZZLE — LEAKING (LT ENGINE) · airframe 52,062 hrs · 27,397 cycles

AFTER TAKEOFF AND ABOUT 600 FT WE START TO LOOSE PWR ON ENG NR1. DURING THE RETURN TO THE AIRPORT, LOST THE DC GEN NR 1 AND ACW GEN NR 1. THEN ON FINAL APPROACH WE LOST ALL OIL PRESSURE WITH A MASTER WARNING, REPETITIVE CHIME, ANALOG INDICATION AT "0" AND THE RED LOCAL LIGHT "ON". AFTER LANDING WE SHUTDOWN THE ENG AS A PRECAUTION IAW AOM VOL 1. DURING POST FLIGHT FOUND THE WING AND THE FUSELAGE COVERED WITH OIL AND FUEL DUE TO A LEAK. REPLACED FUEL NOZZLE KIT AND FUEL FLOW DIVIDER IAW /C EX ATR NR 73-RAI-001 & FCD NR E2-73-003R1. CLEANED ENGINE NR 1 AND PERFORMED RUN UP IAW W/C EX NR 055007-CS-20000-001. NO FUEL OR OIL LEAKS NOTED.

Part: LAMP — NO TEST (EMERGENCY LIGHTS) · airframe 23,867 hrs · 25,848 cycles

EMERGENCY LIGHT ON STAIRS INOPERATIVE. REINSTALLED BULB ON EMERGENCY LIGHT AT MAIN ENTRANCE STAIR IAW JIC NR 33-51-24. WORKING PROPERLY.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 22,891 hrs · 24,688 cycles

DURING TAXI A/C LOST BRAKES. AWAITING FOR AML FOR FURTHER DETAILS.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 22,824 hrs · 24,614 cycles

THE EMERGENCY LIGHT ON THE CABIN STAIRS MAIN DOOR IS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK IAW JIC NR 33-50-00-OPT-10000-001.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 22,816 hrs · 24,606 cycles

LOWER LEFT EMERGENCY LIGHT BY THE MAIN PAX DOOR HAS TWO BULBS INOPERATIVE. REMOVED AND REPLACED BULBS AND PERFORMED OPT CK IAW JIC NR 33-50-00.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,011 hrs · 23,690 cycles

F/O WINDSHIELD CRACKED IN FLIGHT AT CRUISE. ORIGINAL FLIGHT SJU-EIS, DIVERTED TO STT. REMOVED AND REPLACED RH WINDSHIELD IAW JIC 53-11-10. PERFORMED OPERATIONAL AND LEAK CHECK AND FOUND SATISFACTORY.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 21,458 hrs · 22,972 cycles

EXIT SIGN OVER THE AFT F/A SEAT DOES NOT COME ON WHEN EMERGENCY LIGHT SWITCH IS TURN INTO THE ON POSITION. MAINTENANCE REPAIRED WIRE AS PER ATR-72-AMM-20-27-17 AT EXIT SIGN LOCATED BY AFT F/A SEAT. PERFORMED OPERATIONAL CHECK AS PER ATR-72-JIC-33-50-00.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

RT "T" SUPPORT BRACKET FOR THRESHOLD AT FR 37 CORRODED. RT "TEE" SUPPORT BRACKET AT FR 37 FABRICATED AS PER SRM 53-67-70 FIG 104 AND INSTALLED AS PER SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON LT SEAT TRACK BETWEEN FRAME 36-39. LEFT SEAT TRACK BETWEEN FRAME REPLACED IAW SRM 51-25-04.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

RT INTERCOSTAL BETWEEN FRAME 38-39 CORRODED. NOW RT INTERCOSTAL BETWEEN FRAME 38-39 INSTALLED IAW SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON LT I/B SEAT TRACK BETWEEN FRAME 34-36. LEFT INBOARD FRAME 33-36 SEAT TRACK REPAIR SPLICING AS PER SRM 53-00-00 FIG 435.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

FOUND STR 21-L BETWEEN FRAME 41-40 CORRODED. STR21 L BETWEEN FRAME 40-41 IS REPAIRED IAW SRM 53-00-00 FIG 428 (SHEET 2).

Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND CHORD ANGLE AT RT STR 14 BETWEEN FRAME 13 AND 17 UPPER AND LOWER SURFACE. CORROSION FOUND CHORD ANGLE AT RT STR 14 BETWEEN FRAME 13 AND 17 UPPER AND LOWER SURFACE REPAIRED AS PER 53-31-50 FIGURE 402.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

RT "Z" FLOOR BETWEEN FRAME 39-41 CORRODED. RIGHT "Z" FLOOR BETWEEN FRAME 39-41, REPLACED IAW SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON LT SEAT TRACK BETWEEN FRAME 39-41. NEW SEAT TRACK INSTALLED LEFT BETWEEN FRAME 39-41 AS PER SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON RT I/B SEAT TRACK BETWEEN FRAME 34-36. RT INBD SEAT TRACK BETWEEN 34-36 REPAIR SPLICING AS PER SRM 53-00-00 FIGURE 434 (SHEET1).

Part: STEP — CORRODED (PAX DOOR) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON ALL PAX DOOR STEPS UNDER NUTPLATES. CORROSION REMOVED ON ALL PAX DOOR STEPS UNDER NUTPLATE BY SRM 51-10-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON RT SEAT TRACK BETWEEN FRAME 39-40. RIGHT SEAT TRACK BETWEEN FRAME 39-40 REPLACED IAW SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

CORROSION FOUND ON RT SEAT TRACK BETWEEN FRAME 36-39. RT SEAT TRACK BETWEEN FRAME 36-39. REPLACED AS PER SRM 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

FLOORBEAM 36 CORRODED. FLOORBEAM 36 REPAIRED IAW SRM 53-00-00 FIG 435.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

FOUND FLOORBEAM 38 CORRODED. FLOORBEAM 38 REPAIRED IAW SRM 53-00-00 FIG 435.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,384 hrs · 22,883 cycles

FLOORBEAM 41 CORRODED. FLOORBEAM 41 IS REPAIRED IAW SRM 53-61-40 FIG 412 SHEET 1.

Part: HINGE — CORRODED (SERVICE DOOR) · airframe 21,384 hrs · 22,883 cycles

SERVICE DOOR UPPER AND LOWER DOOR SIDE HINGE FITTING CORRODED. CORROSION ON SERVICE DOOR UPPER AND LOWER DOOR SIDE HINGE FITTING REMOVED IAW SRM 51-21-42. FOUND WITHIN LIMITS IAW SRM 51-10-10.

Part: FUEL NOZZLE — DEFECTIVE (RT ENGINE)

ON APPROACH RT ENGINE FLAMED OUT. LANDED SUCCESSFULLY. REPLACED RT ENGINE FUEL NOZZLE KIT, AND FUEL FLOW DIVIDER IAW MM 71-01-40. PERFORMED ENGINE RUN-UP AND FOUND SATISFACTORY. (K)

Part: FLOW DIVIDER — DEFECTIVE (RT ENGINE)

ON APPROACH RT ENGINE FLAME OUT, LANDED SUCCESSFULLY. REPLACED RT ENGINE FUEL NOZZLE KIT, AND FUEL FLOW DIVIDER IAW MM 71-01-40. PERFORMED ENGINE RUN-UP AND FOUND SATISFACTORY. (K)

Part: FLOW DIVIDER — LEAKING (RT ENGINE)

WHILE IN CLIMB, NR 2 ENGINE TQ DROPS SLOWLY UP TO 25 PERCENT AND LOST POWER UNTIL THE ENGINE FLAMED OUT BY ITSELF. REPLACED FUEL FLOW DIVIDER IAW MM 72-01-40 AND FUEL NOZZLES 8,9,10,11 AND 12 TRANSFER TUBES AND SEALS IAW 72-01-40. PERFORMED ENGINE RUN UP NO LEAKS FOUND AND WORKING PROPERLY. (K)

Part: FIRE LOOP — DEFECTIVE (RT NACELLE)

JUST AFTER LANDING RT ENGINE FIRE WARNING INDICATION CAME ON. DISCHARGED BOTH FIRE BOTTLES BUT INDICATION STAYED ON. TAXIED A/C TO THE GATE FOR MTX CHECK. REPLACED NR 2 LOOP AT THE LOWER AFT OF THE ENGINE NACELLE AS PER JIC 26-12-61. PERFORMED OP CHECK ON SYSTEM, COULD NOT DUPLICATE INDICATION. (M)

Part: ARM — CRACKED (MLG)

WHILE PERFORMING A NON DESTRUCTIVE TESTING (NDT) INSPECTION OF THE MAIN LANDING GEAR SIDE BRACE, THE LEFT UPPER ARM SHOWED A DEFECT (CRACK). REPLACED LEFT MAIN LANDING GEAR UPPER ARM. (M)

Part: CIRCUIT BOARD — SHORTED (CABIN)

DISCREPANCY: WHILE CRUISING AT 17,000 FT, THE CREW HEARD A RELAY CLICKING SOUND FOLLOWED BY CIRCUIT BREAKERS POPPING OUT FOR SEAT BELT, NO SMOKING, CALL SYSTEM AND RT CABIN READING LIGHTS. FLIGHT ATTENDANT REPORTED ELECTRIC SPARKS AND SMOKE COMING FROM THE PASSENGER SERVICE UNIT (PSU) 8 C/D. AIRCRAFT DIVERTED.

Part: SWITCH — FAILED (CENTER PEDESTAL)

DURING LANDING WHEN POWER LEVERS WERE MOVED FROM GROUND IDLE POSITION TO REVERSE, THE ENGINE NH WENT BELOW 71 PERCENT. AIRCRAFT AC POWER WAS LOST THEREFORE, NO HYDRAULIC POWER AVAILABLE. UNABLE TO TAKE OFF POWER CONTROL SYSTEM (ATPCS) SWITCH. THIS IS NOT A TIME CONTROLLED COMPONENT THEREFORE, THERE IS INFO PERTAINING TO THE PART TT NOR THE TSO.

Part: SPACER — CRACKED (LT MLG)

DURING PILOTS PREFLIGHT, FOUND ON LEFT MAIN LANDING GEAR SWINGING LEVER SPACER BROKEN. REMOVED AND REPLACED LEFT MLG SPACER AS PER JIC 32-11-00. PERFORMED EXTENSION AND RETRACTION CHECK AND FOUND SATISFACTORY PER JIC 32-31-00, LEAK CHECKED AND FOUND SATISFACTORY. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AROUND NUT CLIP ON FLOORBEAM 36. INSTALLED SPLICE AND NEW SECTION OF FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT AFT INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — FAILED (CABIN)

HRL - FLT 3665 - F/A REPORTED AN ELECTRICAL SMOKE SMELL IN CABIN. CHECKED A/C. FOUND SAFE FOR FERRY FLIGHT HRL TO DFW. DFW FOUND TRANSFORMER 9AB BURNED MEL'D LIGHTS. REPLACED POWER SUPPLY BOARD FOR SEAT 9AB. PERFORMED OPERATIONAL CHECK SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CIRCUIT BOARD — FAILED (CABIN)

LBB - FLT 3727 - CREW REPORTED BURNING SMELL IN CABIN THAT DISSIPATED WITH READING LIGHT SYSTEM TURNED OFF. ISSUED MEL ON READING LIGHT SYSTEM. RAI'D TRANSFORMER BOARD FOR LIGHT ASSY AT ROW 15CD. PERFORMED OPERATIONAL CHECK SATISFACTORILY. A/C RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3625 - FORWARD EMERGENCY LIGHTS WILL NO GO OUT. EMERGENCY POWER SUPPLY NEED BATTERY PACK. INSTALLED NEW BATTERY PACK. PERFORMED SYSTEM OPS CHECK. NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CLAMP — LOOSE (RIGHT)

DFW - FLT 3597 - SMOKE IN CABIN WITH RT BLEED IN X OVER, RT ENGINE RUNNING, LEFT ENGINE SHUT DOWN. PERFORMED RIGHT ENGINE RUN FOUND AIR LEAKING AROUND GROUND COOLING FAN, TIGHTENED CLAMPS, NO ADDITIONAL LEAKS NOTICED. OPS CHECK GOOD IAW 72-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACM — FAILED (RIGHT)

DFW - FLT 3687 - ABOUT TWO MINUTES AFTER TAKEOFF, NR 1 F/A CALLED AND REPORTED SMELL OF SMOKE. SOON AFTER, COULD SMELL IT IN THE COCKPIT. AIRCRAFT RETURNED TO DFW. REPLACED RIGHT ACM DUE TO SEIZURE. (X)

Part: LIGHT — FAILED (SERVICE DOOR)

ORD - FLT 4132 - RAI LIGHT ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CASE DRAIN — LEAKING (NR 1 ENG)

ORD - FLT NR 4031 - AFTER BOTH ENGINES WERE RUNNING THE ELECTRICAL SMOKE INDICATOR ILLUMINATED. THE CREW SHUT DOWN THE ENGINES AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND A LEAK AT INNER COMPRESSOR CASE DRAIN. RAI'D NR 1 ENGINE DUE TO INTERNAL LEAK. PERFORMED GROUND PERFORMANCE RUN. OPS CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (PITOT HEAT)

DFW - FLT 3831 - DURING TAXI-OUT F/O'S PITOT HEAT FAULT LIGHT CAME ON. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED CURRENT SENSING RELAY 33DA. AIRCRAFT RETURNED TO SERVICE. (W)