N288AM

Part: DOME — CRACKED (NR 1 ENGINE) · airframe 33,889 hrs · 39,184 cycles

OIL LEAK FROM CRACK AT FRONT BORE OF ACTUATOR DOME, FOUND DURING PERFORMANCE RUNS.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 33,934 hrs · 39,226 cycles

GROUND FLOOR LIGHT NEAR SERVICE DOOR IS INOPERATIVE. F/A FOUND LIGHT INOPERATIVE ON WALK AROUND RESET LIGHT BULB , OPS CHECKED GOOD REF AMM 33-51-24.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 33,933 hrs · 39,225 cycles

MAIN CABIN DOOR VERY HARD TO OPEN. CLEAN ROLLER ON UPPER LT SIDE OF PAX DOOR AND PERFORMED FUNCTIONAL CHECK GOOD IAW 52-11-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,934 hrs · 39,226 cycles

GROUND FLOOR LIGHT ON MAIN CABIN DOOR IS INOPERATIVE. F/O FOUND LIGHT INOPERATIVE ON WALK AROUND RESET LIGHT BULB, OPS CHECKED GOOD REF AMM 33-51-24.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,654 hrs · 38,927 cycles

EMERGENCY LIGHT CABIN DOOR INOPERATIVE. RELAMPED LIGHT ON CABIN DOOR IAW JIC 33-40-00.

Part: WARNING LIGHT — MALFUNCTIONED (FIRE EXTINGUISH) · airframe 33,602 hrs · 38,863 cycles

THE AGENT 2 DISCHARGE LIGHT IS ILUMINATED ON FIRE DETECTION 1 AND AGENT 1 IS ON SYS 2. OPS CHECKED SYS GOOD REF AMM 26-12-00, OPT 10000.

Part: WIRE — DAMAGED (EXTING SYS) · airframe 33,602 hrs · 38,863 cycles

THE AGENT 2 DISCHARGE LIGHT IS ILUMINATED ON FIRE DETECTION SYS 1 AND AGENT 1 IS ON SYS 2. OPS CHECKED SYS GOOD REPAIRED WIRES IAW AMM SPM 20-41-00 AND OPS CHECKED GOOD IAW AMM 26-12-00, OPT 10000.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 33,551 hrs · 38,802 cycles

EMERGENCY LIGHT AT BOTTOM OF PAX DOOR BLINKS INTERMITTENTLY. CLEANED CONTACT ON EMERGENCY LIGHT SOCKET IN ENTRANCE STAIRS. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,289 hrs · 38,515 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT THE BOTTOM OF THE CABIN DOOR TO BE INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. RELAMPED IAW MM 33-50. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 33,108 hrs · 38,297 cycles

EMERGENCY EXIT LIGHT ON STAIRS INOPERATIVE. RESECURED PINS AT TERMINAL CONNECTOR FIN NR 253VC IAW 33-51-11. OPS CHECK OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,536 hrs · 37,591 cycles

EMERGENCY LIGHT (BOTTOM STEP LIGHT ) ON CABIN DOOR, INOP. REPOSITIONED MAIN DOOR EMERG LIGHT BULB AND OPT CK GOOD IAW W/C EX-33-50-00 OPT-001.

Part: LIGHT — NO TEST (CABIN) · airframe 32,531 hrs · 37,585 cycles

CABIN DOOR EMERGENCY LIGHT WON'T TEST. R & R OF EMERGENCY GROUND ILLUMINATION FLOOD LIGHT ASSY 21WL IAW AMM JIC 33-51-24 AND W/C OPT SATISFACTORY IAW EX-335000OPT10000-001.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 32,526 hrs · 37,577 cycles

EMERGENCY LIGHT AT BOTTOM OF STAIRS ON MAIN CABIN DOOR INOP. REPAIRED WIRE BY DOOR UPPER STEP IAW STD PRACTICE, OPT CK GOOD IAW MM 33 50 00.

Part: ENGINE — FAILED (NR 1) · airframe 32,437 hrs · 37,473 cycles

NR 1 ENGINE FAILURE DURING DESCENT WITH IMMEDIATE RELIGHT. PERFORMED SPECIAL REQUEST 288720348, ISPECTED LT ENGINE WIRING, NO DEFECTS NOTED. REMOVED AND REPLACED AFU IAW ATR 72 JIC 77-13-62 OPS CHECK NORMAL. INSPECTED AND CLEANED TORQUE SENSORS CONNECTOR, NO DEFECTS NOTED ATR JIC 72 / 77-13-62. SPECIAL REQUEST 288280349 TDMI OPENED TO PERFORM EO E9-2800-001 R1 IN 250 FLIGHT HOURS TO MAKE SURE THERE IS NO DEBRIS FOUND IN THE LT AND RT FUEL FEEDER TANKS AND ENGINE JET PUMPS. A/C RELEASE FOR FCF PORPOSE ONLY. FCF PASSED SATISFACTORY.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 32,245 hrs · 37,225 cycles

PASSENGER STAIR EMERGENCY LIGHT BURNED OUT. REPAIRED WIRE AT MAIN DOOR CONNECTOR IAW STD PRACTICE ,OPT CK GOOD IAW MM 52 70 00.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 32,210 hrs · 37,181 cycles

DURING SCHEDULED HEAVY CHECK INSP, CORROSION WAS FOUND ON THE FWD PRESSURE IN 1 AREA OF THE BULKHEAD WEB. COMPLIED WITH EO E2-53MR-260 ON FRAME 1 FWD PRESSURE BULKHEAD WEB CORROSION BLEND OUT REPAIR, REF NDT REPORT AMS 100907-27 FOR HFEC & UT VALVES NO DEFECTS NOTED, COMPLIED WITH ATR72SRS DO/TS-4711/10.

Part: SOCKET — BURNED (COCKPIT LIGHT) · airframe 32,210 hrs · 37,181 cycles

AFTER TAKEOFF STRONG ELECTRIC ODOR IN COCKPIT POSSIBLY UNDER PANEL BEHIND F/O SEAT, F/A'S CABIN HAS NO SMELL. IAW JIC 33-21-23, REPLACED FLORESCENT TUBS SOCKET LIGHT ASSY FIN 286LGA. OPS CHECK OK AWM USED 61-22-01 FOR WIRE CONNECTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,712 hrs · 36,500 cycles

EMERGENCY LIGHT MAIN ENTRY STAIRS INOP. ADJUSTED BULB OF MAIN DOOR AND PERFORMED OPT IAW JIC 33-50-00.

Part: O-RING — LEAKING (LT ENGINE) · airframe 31,633 hrs · 36,388 cycles

DURING CLIMB OUT WHEN SELECTING BLEED VALVES ON , IN THE COCKPIT WE GET A NOXIOUS DIRTY SOCK EXHAUST SMELL, SMELL GOES AWAY WHEN DESELECTING NR 1 BLEED VALVE. R& R LT ENG NR 5, 6 AND 7 SCAVENGE TUBE O-RINGS IAW MM 72-01-50, NO SMELL NOTED AT THIS TIME, NO LEAKS NOTED.

Part: O-RING — LEAKING (LT ENGINE) · airframe 31,633 hrs · 36,388 cycles

DURING CLIMB OUT WHEN SELECTING BLEED VALVE ON IN THE COCKPIT WE GET A NOXIOUS DIRTY SOCK EXHAUST SMELL. SMELL GOES AWAY WHEN DESELECTING NR 1 BLEED VALVE. R & R LT ENG NR 5, 6, 7 SCAVENGE TUBES O-RINGS IAW MM 72-01-50. NO SMELL NOTED AT THIS TIME, NO LEAKS.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 31,473 hrs · 36,168 cycles

ON APPROACH RT ENGINE TQ AND NP WENT TO 0 PERCENT, NH AND ITT STILL SHOWED 76 PERCENT AND 400 PERCENT, PLANE YAWED SHARPLY DURING EVENT. PERFORMED ENGINE GROUND OPS CHECK IAW EX-055007-CS-20000-001 AND FOUND WORKING OK, CANNOT DUPLICATE PROBLEM ON GROUND. TAC 36168

Part: UNKNOWN — ODOR (CABIN) · airframe 31,457 hrs · 36,139 cycles

AFTER BLEEDS ON DURING CLIMB, A STRONG ACIDIC ODOR FILLED THE COCKPIT AND THEN SLOWLY GOT BETTER ENROUTE. BOTH COCKPIT CREW EXPERIENCED THE FEELING OF LIGHT HEADEDNESS, TINGLING LIPS & FINGERS BY THE TIME WE STARTED OUR DESCENT, AFTER TOUCHDOWN THE SAME STRONG SMELL RETURNED. AWAITING AML PAGE FOR FURTHER DETAILS

Part: BLEED VALVE — INOPERATIVE (LEFT ENG) · airframe 31,457 hrs · 36,169 cycles

AFTER BLEEDS ON DURING CLIMB, A STRONG ACIDIC ODOR FILLED THE COCKPIT AND THEN SLOWLY GOT BETTER ENROUTE. BOTH COCKPIT CREW EXPERIENCED FEELING OF LIGHTHEADEDNESS, TINGLING LIPS & FINGERS, BY THE TIME WE STARTED OUR DESCENT, AFTER TOUCHDOM THE SAME STRONG SMELL RETURNED. PERFORMED LT ENG BLEED SYS BLANKING CAPS INSTALLATION TO BLEED DUCTS. BLEED SYS NR 10 M MEL 36-02 AUTH NR 030131DM-C LT BLEED VALVE SYS INOP IAW MEL 36-02 BLEED VALVE SECURED CLOSED BLANKING CAPS INSTALLED PERFORMED ENG'S RUN-UP IAW 72-00-00 NO SMELL NOTED. NRWC 282722 ASSIGNED TO CLEAR MEL 36-02 AUTH NR 030131DM-C (SEET TURNOVER.) FLUSHED AND CLEANED LT HEAT EXCHANGER (REMOVED AND RE-INSTALLED IAW JIC 21-51-51). PERFORMED AIR BLEED SYS OPT AND FOUND OK IAW JIC 36-11-00. ALSO PERFORMED AIR CONDITIONING OPT AND FOUND OK NO ODOR NOTED AT THIS TIME IAW JIC 21-10-00. MEL CLEANED. AML 288969 ACFT RELEASE FOR FCF PURPOSE, WHY, TO VERIFY OIL ODOR IN COCKPIT AFTER BLEEDS ON DURING TAKEOFF. FCF PASSED NO ODOR DETECTED.

Part: UNKNOWN — ODOR (A/C PACK) · airframe 31,449 hrs · 36,128 cycles

STRONG ODOR COMING FROM BOTH PACKS ON CLIMB AFTER BLEEDS SELECTED ON. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: VALVE — ODOR (CABIN AIR) · airframe 31,449 hrs · 36,128 cycles

STRONG ODOR COMING FROM BOTH PACKS ON CLIMB AFTER BLEEDS SELECTED ON. (SEE TURNOVER). ADDED SPACERS ON AIR SWITCHING VALVE, LT ENGINE MFG TROUBLESHOOT MANUAL 72-00-01. FAULT ISOLATION FIG 108, OPS CHECK FOUND WORKING PROPERLY FOR MORE INFO NRWC 245019, TAC 36128.

Part: SEAL — LEAKING (ENGINE) · airframe 31,430 hrs · 36,102 cycles

LT PACK INOP, UNABLE TO BRING DUCT TEMP BELOW 40 DEGREES C, DURING T-OFF & CLIMB, STRONG BURNED OIL SPELL ACCOMPANIED BY TOO WARM TEMP. RETURNED TO DEPARTURE. R & R LT AIR CYCLE MACHINE CLAMP IAW MM 21-11-51 AND PERFORMED OPS CHECK AND FOUND WORKING PROPERLY AT THIS TIME. ON 3/4/10 PERFORMED ENGINES GROUND RUN-UP IAW JIC 72-00-00 AT VARIOUS POWER SETTINGS IAW 72-00-10 FIG 108 FAULT ISOLATION PG SYS NORMAL. ON 3/4/10 R & R NP SENSOR SEAL AND CLEANED BRG 6 AND 7 BREATH TUBE AND PERFORMED OPS CHECK AND FOUND WORKING PROPERLY AT THIS TIME IAW MM 72-01-60, TAC 36108 AT THIS TIME CLEARED THIS ITEM OR ITEM 1 IAW MM 72-01-60

Part: CLAMP — FAILED (ACM) · airframe 31,430 hrs · 36,102 cycles

LT PACK INOP, UNABLE TO BRING DUCT TEMP BELOW 40 DEGREES C, DURING T-OFF & CLIMB, STRONG BURNED OIL ODOR ACCOMPANIED BY TOO WARM TEMP. RETURNED TO DEPARTURE. R & R LT AIR CYCLE MACHINE CLAMP IAW MM 21-11-51 AND PERFORMED OPS CHECK AND FOUND WORKING PROPERLY AT THIS TIME.

Part: WIRE — DISCONNECTED (CONNECTOR) · airframe 30,904 hrs · 35,412 cycles

ACFT DURING TAKEOFF FROM EIS AT ABOUT 1000 TO 1500 FT, HAD AN UNANNOUNCED PITCH DISCONNECT. NO INDICATION ON THE CAP. EMERGENCY DECLARED. LANDED REPAIRED WIRE AT CONNECTOR FIN NR 171WWA IAW ASM NR31-53-00 SCH 06 P111 FIG 1. ALSO RECONNECT PITCH MECHANISM AND FOUND SATISFACTORY IAW JIC NR 27-31-42.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 29,875 hrs · 34,052 cycles

MAIN PAX DOOR STAIR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP AND PERFORMED OPERATIONAL CHECK IAW JIC NR 33-51-00.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 29,875 hrs · 34,052 cycles

RIGHT REAR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP AND PERFORMED OPERATIONAL CHECK IAW JIC NR 33-51-00.

Part: ENGINE — FAILED (RIGHT) · airframe 29,795 hrs · 33,950 cycles

ENGINE OIL ALERT RECEIVED FOR ENGINE 32. BOTH CAP ALERT AND WARNING LIGHT ON INDICATOR. OIL PRESSURE FOR NR 2 ENGINE ZERO. RETURNED TO MIA WITH 32 ENGINE SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE IAW W/C 055006-CS-20000-001 AND 72 JIC NR 72-00-00-RAI-10000.

Part: ENGINE — FAILED (NR 2) · airframe 29,795 hrs · 33,950 cycles

ENGINE OIL ALERT RECEIVED FOR ENGINE NR 2. BOTH CAP ALERT AND WARNING LIGHT ON INDICATOR. OIL PRESSURE FOR NR 2 ENGINE ZERO. RETURNED TO MIA WITH NR 2 ENGINE SHUT DOWN. REMOVAL OF NR 2 ENGINE IN PROGRESS. AWAITING AML FOR FURTHER DETAILS.

Part: LEVER — FAILED (LANDING GEAR) · airframe 29,596 hrs · 33,719 cycles

LANDING GEAR HANDLE WILL NOT MOVE TO RETRACT GEAR POSITION (AT SDQ). DEFERRED LANDING GEAR RETRACTION SYSTEM AS PER MEL 332-03 AUTH NR 020233DM-C. MEL CLEARED ON 02-26-09 AT SJU, REPLACED LANDING GEAR CONTROL LEVER AS PER JIC NR 32-31-81.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 29,330 hrs · 33,376 cycles

PAX DOOR EMERGENCY LIGHT INOPERATIVE. REPOSITIONED LAMP ON PAX DOOR EMERGENCY LIGHT ASSY AND PERFORMED OPT CK IAW MM NR31-51-24.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 29,330 hrs · 33,376 cycles

EMERGENCY LIGHT NEXT TO SERVICE DOOR INOPERATIVE. REPOSITIONED LAMP AT EMERGENCY LIGHT NEXT TO SERVICE DOOR AND PERFORMED OPS CHECK IAW MM NR 35-51-24.

Part: LIGHT — BURNED OUT (CABIN) · airframe 27,770 hrs · 31,354 cycles

PASSENGER ENTRY STAIRS EMERGENCY LIGHT OUT. REMOVED AND REPLACED PAX/CREW DOOR EMERGENCY LIGHT IAW JIC 33-51-25. PERFORMED OPT CHK FOUND WORKING PROPERLY AT THIS TIME.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 27,655 hrs · 31,217 cycles

ONE OF THE EMERGENCY EXIT LIGHTS IN THE STAIRS IS BURNED OUT. REPAIRED BROKEN WIRE AT PASSENGER CREW DOOR IAW SRM 20-24-17. PERFORMED OPT CHK IAW JIC 33-50-00 AND FOUND WORKING PROPERLY AT THIS TIME.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,514 hrs · 31,051 cycles

EMERGENCY EXIT LIGHT ROW 6 INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY LIGHT ROW 6. PERFORMED OPERATIONAL CHECK AND FOUND WORKING PROPERLY PER MM 33-50-00.

Part: LIGHT — BROKEN (GALLEY FLOOR) · airframe 27,218 hrs · 30,709 cycles

GALLEY AFT FLOOR ESCAPE EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED LIGHTING STRIP ASSEMBLY IAW JIC NR 33-51-24. OP CK OK.

Part: LINE — BROKEN (HYD SYSTEM) · airframe 26,966 hrs · 30,384 cycles

GREEN HYDRAULIC SYSTEM LO LEVEL INDICATION. REPLACED UNION ON LINE FROM BRAKE DUAL VALVE LINE TO BLUE ACCUMULATOR, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (PAX ENTRY)

DURING PRE-FLIGHT, CAPTAIN FOUND THE STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED AND TESTED ENTRY STAIR EMERGENCY LIGHT ASSY IAW MM 33-51-00, FOUND SYSTEM WORKING PROPERLY. (K)

Part: UPLOCK — INOPERATIVE (NLG)

ON TAKEOFF UPON GEAR RETRACTION, RECEIVED A RED UNSAFE INDICATION ON UPPER AND LOWER PANELS. CYCLED GEAR AND GOT GOOD INDICATION ON BOTH PANELS. AIRCRAFT RETURNED TO THE SJU AIRPORT. REPLACED NLG UPLOCK BOX AS PER JIC 32-31-00. OPERATIONAL CHECK FOUND OK. (M)

Part: CONTROL VALVE — INOPERATIVE (LT MLG)

DURING APPROACH, WHEN LANDING GEAR HANDLE SELECTED DOWN, NO GEAR EXTENSION. REF UNLOCK LIGHTS ON BOTH FORWARD AND OVERHEAD PANEL, PER AOM GRAVITY EXTENSION PERFORMED SUCCESSFULLY. AIRCRAFT LANDED SAFELY AT PUNTA CANA, DOMINICAN REPUBLIC. DEFERRED LANDING GEAR RETRACTION SYSTEM AS PER MEL 32-03, LANDING GEAR PIN AS PER MEL. UPON ARRIVAL TO SAN JUAN, PR, REMOVED AND REPLACED LANDING GEAR CONTROL VALVE AS PER JIC 32-31-51. PERFORMED OPS CHECK, FOUND SYSTEM WORKING PROPERLY AT THIS TIME. (M)

Part: TURBINE BLADES — DAMAGED (ENGINE)

DURING CLIMBOUT A LOUD BANG NOISE WAS HEARD FOLLOWED BY RT ENGINE LOST OF POWER. BEFORE ENGINE SHUTDOWN, A FIRE INDICATION WAS NOTED AND SMOKE AND FUMES IN THE CABIN. EMERGENCY DECLARED. AIRCRAFT RETURNED TO THE AIRPORT. VISUAL INSPECTION REVEALED ENGINE POWER TURBINE BLADES DAMAGED. REMOVED ENGINE FOR INVESTIGATION. (K)

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CRUISE, THE RIGHT WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO ST KITTS. ORIGINAL DESTINATION WAS ST LUCIA. REPLACED F/O WINDSHIELD ASSEMBLY. (M)

Part: SWITCH — FAULTY (CENTER PEDESTAL)

ON TAKEOFF ROLL, THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM DID NOT ARM. TAKEOFF ABORTED. REMOVED AND REPLACED MICROSWITCH. (M)

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT)

FLOOR EMERGENCY LIGHTS REMAIN ON. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: BALLAST — FAILED (CABIN)

SGF - FLT 3858 - FOUND CABIN OVERHEAD EMERGENCY LIGHT BY GALLEY INOPERATIVE. REMOVED AND REPLACED FUSELAGE AT EMERGENCY LIGHT BALLAST IAW AMM. OPS CHECK GOOD. (M)

Part: RADAR — INOPERATIVE (WEATHER RADAR)

DFW - FLT 3717 - CREW REPORTED THE WEATHER RADAR TO BE INOPERATIVE. AIRCRAFT WAS RETURNED TO DFW TO WEATHER IN HRL. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR R/T UNIT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA09110. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED DOUBLER ON FRAME 36 LEFT SIDE AT FLOOR LEVEL CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUIDE — CORRODED (RT FLAP)

SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED THE RIGHT INBOARD FLAP NR 4, NR 3, NR 2, NR 1 CAM GUIDES CORRODED, P/NS S5751204920500, S5751211020400. THE LEFT OUTBOARD FLAP NR 3, NR 2, NR 1 AND LEFT INBOARD FLAP NR 5, NR 4, NR 3, NR 2, NR 1 CAM GUIDES CORRODED. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW JIC 57-53-12-RAI-1000-001. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR UPPER INNER SKIN CRACKED AND CORRODED AND THE LOWER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-10 FIGURE 411 AND REPAIRED THE LOWER PAN IAW SRM 52-11-00 FIGURE 411. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA09110. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA09110. (M)

Part: PAN — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR UPPER INNER SKIN CRACKED AND CORRODED AND THE LOWER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-10 FIGURE 411 AND REPAIRED THE LOWER PAN IAW SRM 52-11-00 FIGURE 411. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0917 (M)

Part: STEP — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE FORTH AND TOP STEP ON PASSENGER DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED THE STEPS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STEP — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE FORTH AND TOP STEP ON PASSENGER DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED THE STEPS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0918 (M)

Part: SILL DRAIN — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0919. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT, LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD, AND LEFT AFT OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9 5300-02-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36 AND 38 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PLATE — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PLATE ON TOP OF THE CREASE BEAM JUST FORWARD OF FLOORBEAM 36 LEFT CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PLATE IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36 AND 38 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MODULE — MALFUNCTIONED (HYDRALIC SYSTEM)

MIA - FLT 5305 - AFTER TAKEOFF, CREW REPORTED LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED HYDRAULIC MODULE IAW AMM. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,917 hrs · 19,888 cycles

MIA - FLT 9751 - PASSENGER DOOR EXTERIOR LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (PAX DOOR)

MIA - FLT 5432 - MAIN CABIN DOOR EMERGENCY FLOOR LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND LIGHT ASSEMBLY. OPERATIONAL WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: IGNITER — MISSING (NR 2 ENGINE)

DFW - FLT 3701 - ABORTED TAKEOFF, DUE TO INDICATION OF FIRE ON NR 2 ENGINE. FOUND OUTBOARD INGNITER NOT INSTALLED ON RIGHT ENGINE. INSTALLED NEW IGNITER IAW PRATT WHITNEY MM 72-01-30. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — MISSING (CABIN)

MIA - ALL EMERGENCY LIGHTS INOPERATIVE. FOUND BATTERIES NOT INSTALLED IN POWER SUPPLIES. INSTALLED SAME, OPS CHECKED IAW 33-51-21. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: CAM GUIDE — CORRODED (LT TE FLAP)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT INBOARD FLAP INBOARD DEFLECTOR WITH THREE CAM GUIDES CORRODED, THE LEFT OUTBOARD FLAP INBOARD DEFLECTOR WITH TWO CAM GUIDES CORRODED, AND THE LEFT INBOARD FLAP OUTBOARD DEFLECTOR OUTBOARD CAM GUIDE CORRODED. REMOVED AND REPLACED ALL CAM GUIDES IAW SRM 51-25-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CAM GUIDE — CORRODED (LT TE FLAP)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT INBOARD FLAP INBOARD DEFLECTOR WITH THREE CAM GUIDES CORRODED, THE LEFT OUTBOARD FLAP INBOARD DEFLECTOR WITH TWO CAM GUIDES CORRODED, AND THE LEFT INBOARD FLAP OUTBOARD DEFLECTOR OUTBOARD CAM GUIDE CORRODED. REMOVED AND REPLACED ALL CAM GUIDES IAW SRM 51-25-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZZX3058.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZZX3058.

Part: FLOORBEAM — MISDRILLED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, FOUND FLOORBEAM 29 WITH AN OVERSIZED HI-LOCK HOLE AT THE LEFT INBOARD SEAT TRACK CENTER ATTACH POINT. REPAIRED THE FLOORBEAM IAW SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZZX3058.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3054 THROUGH 99ZZZX3057.

Part: WEB — CORRODED (FRAMES 36-38)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT WEB BETWEEN FRAMES 36 AND 38 CORRODED. REMOVED AND REPLACED THE WEB IAW 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL SIMA992096, AND, 99ZZZX3055 THROUGH 99ZZZX3058.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT, THE LEFT AFT INBOARD AND OUTBOARD, THE RIGHT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL 99ZZZX3054 THROUGH 99ZZZX3058. (X)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAMS 36 AND 38 WITH CORROSION AROUND THE NUTPLATE HOLES. REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435, AND REMOVED AND REPLACED FLOORBEAM 38 IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX3053. (X)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAMS 36 AND 38 WITH CORROSION AROUND THE NUTPLATE HOLES. REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435, AND REMOVED AND REPLACED FLOORBEAM 38 IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA992094.

Part: ZEE MEMBER — CORRODED (FRAMES 39-41)

SAW - DURING CPCP-8 INSPECTION, FOUND THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (X)

Part: ZEE — CORRODED (PASSENGER DOOR)

SAW - DURING HMBV-1 INSPECTION, FOUND THE LEFT AFT PASSENGER DOOR ZEE MEMBER CORRODED BETWEEN FRAMES 39 AND 40. REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 52-11-30. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FRAME — CRACKED (CARGO DOOR)

SAW - DURING MBV-2 INSPECTION, FOUND THE THREE FORWARD UPPER FRAMES ON THE CARGO DOOR CRACKED. MAINTENANCE REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA992021 AND 99ZZZX2964.

Part: FRAME — CRACKED (CARGO DOOR)

SAW - DURING MBV-2 INSPECTION, FOUND THE THREE FORWARD UPPER FRAMES ON THE CARGO DOOR CRACKED. MAINTENANCE REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR 99ZZZX2964 AND 99ZZZX2965. (X)

Part: FRAME — CRACKED (CARGO DOOR)

SAW - DURING MBV-2 INSPECTION, FOUND THE THREE FORWARD UPPER FRAMES ON THE CARGO DOOR CRACKED. MAINTENANCE REPAIRED THE FRAMES IAW SRM 52-31-00 FIGURE 402. AIRCRAFT RETURNED TO SERVICE. REF: OPER CNTRL NR SIMA992021 AND 99ZZZX2965.

Part: ENGINE — POWER LOSS (LEFT)

MIA - FLT 5714 - DURING CLIMB-OUT, APPROX 2-3 MINUTES AFTER TAKEOFF, THE LEFT ENGINE TORQUE DROPPED TWENTY PERCENT AS IF IT HAD FLAMED OUT. THE ITT DROPPED ABOUT 100 DEGREES AND THEN THE TORQUE SLOWLY ROSE BACK UP TO CLIMB SETTING. THIS OCCURENCE LASTED ABOUT 15 SECONDS. AIRCRAFT RETURNED TO MIAMI WITH NO FURTHER PROBLEMS. (M)

Part: STRINGER — DAMAGED (BS 46/47)

ABI - DAMAG TO THE LOWER AFT FUSELAGE SKIN AND STRINGERS BETWEEN FRAMES 46 AND 47. REMOVED DAMAGED SKIN AND STRINGERS 17 LEFT AND 17 RIGHT AND CUT TO LENGTH NEW STRINGERS EXTRUSION AND FABRICATED CONNECTING SECTION. FABRICATED REPAIR SKIN .032 THICK AND SPLICES .050 THICK, LAP JOINT 11 BY 7.5 INCH AND FILLER PIECE 12.5 BY 7.5 INCH. INSTALLED ALL ITEMS ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (BS 46/47)

ABI - DAMAG TO THE LOWER AFT FUSELAGE SKIN AND STRINGERS BETWEEN FRAMES 46 AND 47. REMOVED DAMAGED SKIN AND STRINGERS 17 LEFT AND 17 RIGHT AND CUT TO LENGTH NEW STRINGERS EXTRUSION AND FABRICATED CONNECTING SECTION. FABRICATED REPAIR SKIN .032 THICK AND SPLICES .050 THICK, LAP JOINT 11 BY 7.5 INCH AND FILLER PIECE 12.5 BY 7.5 INCH. INSTALLED ALL ITEMS ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LINE — FAILED (HYD SYSTEM)

DFW - FLT 3690 - GREEN SYSTEM HYDRAULIC LOW LEVEL WARNING LIGHT CAME ON. PULLED EMERGENCY GEAR EXTENSION HANDLE. REMOVED AND REPLACED BROKEN PIPE FROM THE GREEN ACCUMULATOR TO THE BRAKE MANIFOLD. RESERVICED HYDRAULIC SYSTEM AND PERFORMED LEAK CHECK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (BS 8-10)

ABI - DAMAGE ON RIGHT LOWER FUSELAGE BETWEEN FRAMES 8 AND 10, AND BETWEEN STRINGER 20 AND BL 0. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSPECTION. FABRICATED AND INSTALLED EXTERNAL DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE SUPPORT AND DRAIN TRACK CORRODED AT FRAME 37. REMOVED AND REPLACED THE SILL PLATE SUPPORT AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DRAIN — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE SUPPORT AND DRAIN TRACK CORRODED AT FRAME 37. REMOVED AND REPLACED THE SILL PLATE SUPPORT AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DRAIN — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE PAX DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE SILL PLATE AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE PAX DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE SILL PLATE AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER MODULE — FAILED (CABIN)

CRP - FLT 3829 - PASSENGERS REPORTED A BURNT SMELL AND SMOKE NEAR ROW 9. FLT CREW PULLED C/B MAINTENANCE FOUND TRANSFORMER ON 11 AB BURNED. DISCONNECTED TX FROM POWER SOURCE. ISSUED MEL 25-19 AND RETURNED A/C TO SERVICE. R/I'D READING LIGHT POWER MODULE AT ROW 11 AB. PERFORMED OPERATIONAL CHECK SATISFACTORILY. REMOVED MEL AND RETURNED A/C TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

GALLEY EMERGENCY PROXIMITY LIGHTING INOPERABLE. CHECKED LIGHT AND ISSUED MEL 33-22 AND RETURNED AIRCRAFT TO SERVICE. REPLACED LIGHTING STRIP. OPS CHECK SYSTEM AND REMOVED MEL. RETURNED AIRCRAFT TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

DFW - FLT 3604 - FLOOR PROXIMITY LIGH TNR 2 FORWARD OF PAX DOOR AREA IS INOP. MEL'D LIGHT PER 33-22, AND RETURNED AIRCRAFT TO SERVICE. REPAIRED WIRING, PERFORMED OPS CHECK AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: VALVE — FAILED (LT ENGINE)

DFW - FLT 3655 - PILOT SQUAWKED ELECTRICAL SMOKE INDICATION AFTER ENGINE START. MX REMOVED AND REPLACED P2.5 SWITCHING VALVE. GROUND RUN CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND FLOOR PROXIMITY LIGHTS INOP. RAI'D POWER SUPPLY 62WL. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (AC DISTR SYS)

ORD - FLT 4383 - NR 2 ACW BUS OFF INTERMITTENT IN FLIGHT AND ON GROUND AFTER LANDING. NO EQUIPMENT FAILURES NOTED WITH BUS OFF INDICATION. RAI'D RELAY 6XN IN 94VU. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: MULT FUNC COMP — MALFUNCTIONED (RIGHT)

DFW - FLT NR 3596 - SMOKE IN COCKPIT AND CABIN, AIRCRAFT EMERGENCY EVACUATION. 1B MULTI FUNCTION COMPUTER FAULTED AND WOULD NOT RESET. GROUND RAN AIRCRAFT FOR 10 MINUTES, FOUND NO SMOKE IN COCKPIT OR CABIN, 1B MULTI FUNCTION COMPUTER DID NOT FAULT. AFTER RESET NO DEFECTS NOTED, AFTER FURTHER TROUBLESHOOTING RAI P2.5/P3 SWITCHING VALVE INNER HOUSING AND PISTON RING. GROUND RAN AIRCRAFT AND WITH NO DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: EEL CONTROLLER — FAILED (CABIN)

DFW - FLT NR 3722 - UPON LANDING AT DFW THE REAR HALF OF THE INTERIOR EMERGENCY LIGHTS ILLUMINATED. BATTERY PACK CONTROLLER ASSY AND BATTERY WERE REPLACED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)