N322AC

Part: LIGHT — UNKNOWN (CABIN)

EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. OPS CHECKED GOOD.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 34,019 hrs · 38,877 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHTS REMAINED ON WITH THE SWITCH ON THE ARM POSITION (FIRST HALF REMAINED ON). THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK 43WL. PERFORMED OPS TEST IAW JIC 33-51-21-RAI-10000 AND JIC 33-51-21-RAI-10010 AND FOUND SYS OK. THE ACFT WAS RETURNED TO SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 33,964 hrs · 38,802 cycles

THE CREW REPORTED THE EMERGENCY LIGHT COVER IN FRONT OF THE GALLEY IS MISSING. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED THE EMERGENCY LIGHT COVER IN FRONT OF THE GALLEY IAW MM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,879 hrs · 38,693 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN STAIRS INOPERATIVE. ACFT REMOVED FROM SERVICE. REPOSITIONED PASSENGER/CREW DOOR EMERGENCY LIGHT AND PERFORMED OPS CHECKED IAW JIC 33-50-00. ACFT RETURNED TO SERVICE.

Part: GUIDE — CORRODED (LT WING TE FLAP) · airframe 33,819 hrs · 38,626 cycles

DURING B INSPECTION, FOUND THE LT WING HAS 4 INTERNAL FLAP CAM GUIDES WITH CORROSION OUT OF LIMITS. THE ACFT WAS REMOVED FROM SERVICE. LT WING 4 INTERNAL FLAP CAM GUIDES REMOVAL AND REPLACEMENT COMPLETED IAW MM 57-53-12. THE ACFT WAS RETURNED TO SERVICE.

Part: GUIDE — CORRODED (RT WING TE FLAP) · airframe 33,819 hrs · 38,626 cycles

DURING B INSPECTION, FOUND THE RT WING HAS 2 EXTERNAL FLAP CAM GUIDES WITH CORROSION OUT OF LIMITS. THE ACFT WAS REMOVED FROM SERVICE. REMOVAL AND INSTALLATION OF RT WING 2 EXTERNAL FLAP CAM GUIDES COMPLETED IAW MM 57-53-12. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED · airframe 33,765 hrs · 38,568 cycles

THE CREW REPORTED THE EMERGENCY LIGHTS ON WITH THE SWITCH ON THE ARM POSITION. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND FOUND WORKING PROPERLY IAW JIC 33-50-00AND W/C EX-335000-OPT-10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — FAILED (BACK UP) · airframe 33,739 hrs · 38,533 cycles

DURING MAINTENANCE INSPECTION, FOUND AN EMERGENCY BATTERY FAULT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY BATTERY IAW EX-243185-RAI-10020-002. THE OPS CHECK OF THE SYS WAS OK. THE ACFT WAS RETURNED TO SERVICE.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 33,709 hrs · 38,502 cycles

CREW REPORTED SERVICE DOOR EMERGENCY LIGHT COVER BROKEN. ACFT REMOVED FROM SERVICE. R & R THE SERVICE DOOR EMERGENCY LIGHT COVER, AS PER 33-50-00. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (SPOILER) · airframe 33,516 hrs · 38,294 cycles

DURING MX INSPECTION, FOUND THE LT SPOILER UPPER SUFACE METAL STRIP CORRODED AND DEBONDED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT SPOILER IAW JIC 57-71-00. THE OPS CHECK PERFORMED, FOUND THE SYS WORKING PROPERLY. THE ACFT WAS RETURNED TO SERVICE.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 33,174 hrs · 37,911 cycles

THE CREW REPORTED THE FORWARD EXIT EMERGENCY EXIT LIGHT ON LT SIDE OF ACFT IS INTERMITTENT. THE ACFT WAS REMOVED FROM SERIVCE. SECURED LIGHT BULB IAW AMM 33-50-00. NO PARTS R & R. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,079 hrs · 37,801 cycles

DURING B INSPECTION, FOUND EMERGENCY LIGHT MISSING END CAP AT SEAT 17B. ACFT REMOVED FROM SERVICE. RESECURED EMERGENCY LIGHT END CAP IAW CMM 25-25-03. ACFT RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,016 hrs · 37,726 cycles

DURING B-INSPECTION, FOUND THE GALLEY AFT EMERGENCY LIGHT MISSING END CAP. ACFT REMOVED FROM SERVICE. RE INSTALLED END CAP IAW CMM 33-51-01. ACFT RETURNED TO SERVICE.

Part: SWITCH — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 32,731 hrs · 37,388 cycles

ON FLIGHT 4930, THE CREW REPORTED THE EMERGENCY LIGHTS CAME ON DURING ENGINE START AND STAYED ON. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY TOGGLE SWITCH IAW SPM 20-45-11. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,479 hrs · 37,086 cycles

EXIT LIGHT OVER FORWARD CABIN DOOR DOES NOT ILLUMINATE. R & R LIGHT IAW AWM 33-51-00. OPS CHECKED GOOD.

Part: CONTACT — CORRODED (EMERGENCY LIGHT) · airframe 32,468 hrs · 37,074 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHT BELOW LT FWD EMERGENCY EXIT DOOR IS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. CLEANED CORROSION FROM LIGHT CONTACT. NO PARTS R OR R. OPS CHECKED GOOD IAW JIC 33-50-00 OPT 10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,452 hrs · 37,056 cycles

THE CREW REPORTED THE NR 2 EMERGENCY FLOOR LIGHTING BY THE GALLEY IS INOPERATIVE. ACFT REMOVED FROM SERVICE. LIGHT INSTALLED AND WORKING PROPERLY IAW JIC 33-50-00. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,453 hrs · 37,056 cycles

2 EMERGENCY FLOOR LIGHTING BY THE GALLEY IS INOPERATIVE. LIGHT INSTALLED AND WORKING PROPERLY IAW JIC 33-50-00, OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 32,269 hrs · 36,856 cycles

AFTER ENG START, EMERGENCY LIGHTS WERE ON. CYCLED SWITCH LIGHTS AND THEN WORKED PROPERLY. RESECURED CONNECTOR PLUG AT EMERGENCY LIGHT POWER SUPPLY. OPS CK GOOD IAW MM 33-50-00.

Part: LIGHT — LOOSE (CABIN) · airframe 32,147 hrs · 36,728 cycles

CABIN ENTRANCE DOOR STAIR FLOOD LIGHT APPEARS TO BE LOOSE DURING POSTFLIGHT. ADJUSTED CABIN DOOR EMERGENCY LIGHT BULB HOLDER IAW CMM 33-51-25. OPS CHECKED OK IAW W/C EX-335000-OPT-10000-001.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,147 hrs · 36,728 cycles

ALL EMERGENCY LIGHTS REMAIN ON AFTER ENGINE START. 1 RESET IS ALWAYS REQUIRED. ALL CIRCUIT BREAKERS CHECKED OK. SEVERAL ENGINE STARTS ACCOMPLISHED WITH EMERGENCY LIGHTS IN "ARM" POSITION AND FOUND TURNING OFF AUTOMATIC AFTER ENG START. OPS CHECKED OK IAW W/C EX-335000-OPT-10000-001.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,146 hrs · 36,726 cycles

CABIN ENTRANCE DOOR STAIR FLOOD LIGHT INOPERATIVE. REPLACED CABIN ENTRANCE STAIRS FLOOD LIGHT IAW MM 33-51-24. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR PATH LIGHT AT THE FWD CABIN AND AFT CABIN DO NOT ILLUMINATE. ONLY MIDDLE ROW OF LIGHTS WORK. AT THIS TIME EMERGENCY FLOOR LIGHT OPERATIONAL CK. FOUND SATISFACTORY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,167 hrs · 35,663 cycles

LOWER EXIT SIGN ON SERVICE DOOR NEEDS RELAMPED. RELAMPED LOWER EXIT SIGN IAW MM33-00-00. OPS CHECK GOOD. ACFT RETURN TO SERVICE

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,789 hrs · 34,116 cycles

EMERGENCY EXIT LIGHT (BOTTOM ON SERVICE DOOR) INOPERATIVE. FOUND BROKEN WIRE AT PIN NR 1 OF EMER EXIT LT 68WL. RESECURED PIN IAW ASM 33-51-00 OPS CHK GOOD NO FURTHER DEFECTS NOTED.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 29,506 hrs · 33,770 cycles

EMER EXIT LIGHT AT BOTTOM OF STAIRS IS INOP. RELAMP DOOR LIGHT AND OPT CHECK IAW AMM 33-50-00.

Part: FITTING — CORRODED (LT WING AILERON) · corrosion level 2 · airframe 28,836 hrs · 32,929 cycles

LT WING RIB 31 AILERON FITTING HAS CORROSION. REMOVED CORRODED LT WING RIB 31 AILERON FITTING. LOCATED, DRILLED & INSTALLLED NEW FITTING IAW SRM 51-24-08, 57-25-30, 51-25-01, 51-25-02 & 51-25-04.

Part: HINGE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 28,836 hrs · 32,929 cycles

LWR GROUND WIRE ATTACH POINT CORRODED RT FLAP HINGE FITTING RIB 13. REMOVED & REPLACED 2 EA FITTINGS RT WING INBD FLAP OTBD HINGE FITTING IAW SRM 51-21-52 & 51-25-02. LOCATED & DRILLED NEW BRACKETS IAW SRM 51-24-08. TREATED & PRIMED IAW SRM 51-21-17 & 51-21-27.

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 28,380 hrs · 32,381 cycles

EMERGENCY LIGHT ON PAX/ENTRY DOOR INOPERATIVE. REPOSITIONED EMERGENCY LIGHT BULB ON PAX/ENTRY DOOR, PERFORMED OPT IAW JIC NR 33-50-000 AND FOUND SYSTEM WORKING PROPERLY.

Part: BRAKE ASSY — FAILED (ZONE 700) · airframe 28,360 hrs · 32,363 cycles

F/O SIDE LEFT SIDE BRAKE PEDAL NO BRAKE WHEN CYCLE. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY IAW JIC NR 32-42-55. OPT CK GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 27,790 hrs · 31,660 cycles

RT AFT EXTERIOR EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW JIC NR 33-50-00.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 27,790 hrs · 31,660 cycles

LEFT FORWARD EXTERIOR EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW JIC NR 33-50-00.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 27,687 hrs · 31,532 cycles

LT ENGINE TORQUE WENT TO 95 PERCENT UNCOMMANDED. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 25,752 hrs · 29,599 cycles

EMERGENCY LIGHT OUT LEFT EXTERIOR FORWARD OF EMERGENCY EXIT. REMOVED AND REPLACED EMERGENCY EXIT POWER SUPPLY AS PER MM 33-51-21.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 25,655 hrs · 29,512 cycles

CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY 62WL AND PERFORMED OP CK IAW JIC NR 33-50-00.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 25,639 hrs · 29,499 cycles

RT THRESHOLD BTW FRAME 36-39 GUTTER CORRODED. RT THRESHOLD BTW FRAME 36-39 GUTTER REPLACED IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,639 hrs · 29,499 cycles

FLOORBEAM 39 CORRODED ON UPPER AND LOWER SURFACE. CORROSION OF FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIGURE 450 AT 2 LOCATIONS.

Part: SUPPORT BRACKET — CORRODED (FOLDING STEP) · airframe 25,639 hrs · 29,499 cycles

FWD "T" BRACKET OF FOLDING STEP CORRODED. FWD "T" BRACKET OF FOLD ONG STEP REPLACED IAW SRM 51-25-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,340 hrs · 29,124 cycles

F/A REPORTED EMERGENCY EXIT FORWARD TOP LIGHT INOPERATIVE WHEN ACTIVATED THE SYSTEM AND BATTERY POWER WAS OFF. MAINTENANCE RE-LAMPED LIGHT AND PERFORMED OPERATIONAL CHECK AS PER ATR 72- AMM-33-50-00.

Part: LIGHT — INOPERATIVE (CABIN)

PERFORMING POST FLIGHT CREW NOTED LT FWD EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED FWD FLOOD LIGHT BULB IAW JIC 33-50-00. (K)

Part: TORQUE SENSOR — INOPERATIVE (RT ENGINE)

AFTER TAKEOFF AND DURING CLIMBING, THE RT ENGINE STARTED TO FLUCTUATE ABOUT 10 PERCENT. REPLACED NR 2 TORQUE SENSOR. (K)

Part: ENGINE — FIRE (LEFT)

DURING TAXI, LEFT ENGINE FIRE INDICATOR ILLUMINATED, FIRE EXTINGUISHER DISCHARGED. REPLACED ENGINE. WAITING FOR TEARDOWN REPORT. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

MIA - FLT 4975 - CREW REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

MIA - FLT 5420 - ON TAKEOFF, ITT ON NR 2 DURING ROLL WAS 765 DEGREES AND CLIMBING. PULLED NR 2 POWER LEVER BACK 6 DEGREES TORQUE BEFORE IT STOPPED CLIMBING AT 769. APPLIED POWER MANAGEMENT AT 700 FT AND ITT STARTED DOWN. DIVERTED TO MIA. PERFORMED ENGINE T6 IND SYSTEM INSPECTION AND CHECK IAW 72-01-60. NO DEFECTS NOTED. PERFORMED ENGINE PERFORMANCE RECOVERY WASH IAW JIC 72-00-00. GROUND RUNS CHECKED AND WITH LIMIT IAW 72-00-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5409 - EMERGENCY FLOOR LAMP AFT OF GALLEY INOPERATIVE, MEL PER 33-30. REMOVED AND REPLACED BULB IAW AMM. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5409 - FOUND EMERGENCY FLOOR LAMP AFT OF GALLEY INOPERATIVE, MEL PER 33-30. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

MIA - FLT 5236 - PASSENGER DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PUMP — FAILED (HYD BAY)

MIA - FLT 5339 - CREW REPORTED AFTER TAKEOFF, THE LANDING GEAR WOULD NOT FULLY RETRACT. CREW ALSO REPORTED A THUMPING NOISE AND RECEIVED A LEFT MLG UNLOCK LIGHT. CREW RETURNED TO MIA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE GREEN SYSTEM HYDRAULIC PUMP IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT SIDE OF FLOORBEAM 34 HAD A CRACK IN A HI-LOCK HOLE. MAINTENANCE REPAIRED FLOORBEAM 34 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-25-01. AIRCRAFT WAS RETUREND TO SERVICE. (M)

Part: TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURNIG CPCP-8 INSPECTION, MAINTENANCE REPORTED THE FLOOR BOARD SUPPORT PLATE AT FRAME 13 RIGHT CORRODED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATE IAW SRM 51-25-02. AIRCRAFT WAS RETURNED SERVICE. (M)

Part: SILL — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SILL PLATE CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL ROD — CORRODED (ELEVATOR)

SAW - DURING HMBV-1 INSPECTION REPORTED, THE LEFT AND RIGHT ELEVATOR TRIM TAB CONTROL RODS CORRODED INTERNALLY. MAINTENANCE REMOVED AND REPLACED THE CONTROL RODS IAW JIC 27-31-41 RAI-1000. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0111. (M)

Part: CONTROL ROD — CORRODED (ELEVATOR)

SAW - DURING HMBV-1 INSPECTION REPORTED, THE LEFT AND RIGHT ELEVATOR TRIM TAB CONTROL RODS CORRODED INTERNALLY. MAINTENANCE REMOVED AND REPLACED THE CONTROL RODS IAW JIC 27-31-41 RAI-1000. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

SAW - DURNG CPCP-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 42 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TRACK — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUIDE — CORRODED (RT FLAP)

SAW - DURING MBV-2 INSPECTION MAINTENANCE REPORTED, THE NR 1, 2, 3, AND NR 4 CAM GUIDES CORRODED ON THE RIGHT INBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-52-11. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLAP — CORRODED (LT WING)

SAW - DURNIG MBV-2 INSPECTION, MAINTENANCE REPORTED ALL SIX CAM GUIDES, NR 2 AND NR 6 CAM GUIDE ATTACH BRACKETS, OUTBOARD BEAM ATTACH BRACKETS, AND THE MIDDLE BEAM ATTACH BRACKET CORRODED ON THE LEFT OUTBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-004. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUIDE — CORRODED (LT FLAP)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE NR 1, NR 2 AND NR 3 CAM GUIDES CORRODED ON THE LEFT INBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BRACKET — BROKEN (NLG)

SAV - FLT 5342 - AFTER TAKEOFF, CREW TRIED TO SELECT GEAR UP AND FOUND THE HANDLE WOULD NOT MOVE. MAINTENANCE FOUND A NOSE LANDING GEAR PROXIMITY SWITCH TARGET BRACKET BROKEN. BRACKET WAS REPLACED IAW CMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 5276 - FORWARD CABIN DOOR EXIT AND CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT 61WL POWER SUPPLY. OPS CHECK GOOD. (M)

Part: FUSE — INOPERATIVE (POWER SUPPLY)

MIA - EMERGENCY LIGHT IN PASSENGER STAIRS INOPERATIVE. REPLACED FUSE IN 62WL POWER SUPPLY. OPS CHECKED GOOD IAW JIC 33-50-00-OPT-10000-004. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

MIA - FLT 5322 - PASSENGER DOOR EMERGENCY LIGHT ON THE STAIRS IS INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD. (M)

Part: GUIDE — CORRODED (RT FLAP)

SAW - DURING MBV-2 INSPECTION MAINTENANCE, REPORTED THE NR 3, NR 4 AND NR 5 CAME GUIDES CORRODED ON THE RIGHT OUTBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION, FOUND LEFT FORWARD INBOARD AND OUTBOARD, LEFT MIDDLE INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FLIGHT ATTENDANT, RIGHT FORWARD AND RIGHT MIDDLE OUTBOARD, AND THE RIGHT AFT AND RIGHT MIDDLE INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — ELONGATION (FUSELAGE)

SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAM 18 HAD AN ELONGATED HI-LOCK HOLE. REPAIRED FLOORBEAM 18 IAW SRM 53-00-00 FIGURE 429. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — CANNING (FUSELAGE)

SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED OIL CANNING OF LEFT FUSELAGE SKIN BETWEEN FRAME 9 AND 10 AND STRINGER 14 AND 18. MAINTENANCE INSTALLED A SKIN PATCH AND THREE STIFFENERS IAW ATR DRAWING NR 11S531R016 AND SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (M)

Part: MFC — FAILED (E/E BAY)

MIA - FLT 5782 - LEFT MAIN LANDING GEAR UNLOCK LIGHT ON OVERHEAD PANEL IS ILLUMINATED. REMOVED AND REPLACED NR 2 MULTIFUNCTION COMPUTER (MFC). GEAR EXTENSION/RETRACTION CHECKS GOOD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981192.

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1968. (X)

Part: SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. THE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981191, 98ZZZX1969, AND 98ZZZX1971.

Part: SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. THE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981191, 98ZZZX1970, AND 98ZZZX1971.

Part: WEB — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. THE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1969, 98ZZZX1970, AND 98ZZZX1971. (X)

Part: SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. THE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981191, 98ZZZX1969, AND 98ZZZX1970.

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPAIRED DENT ON RIGHT SIDE OF FUSELAGE ABOVE NLG WELL AT FRAME 3 WL 2327.5. MAINTENANCE REPAIRED DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTING INOPERATIVE, 66WL POWER SUPPLY CONTROLS THEM. REPLACED BATTERY PACK AT 66WL POWER SUPPLY IAW JIC 33-51-21 SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X)

Part: BATTERY — DISCHARGED (CABIN)

LBB - EMERGENCY BATTERY PACK AT 61WL HAS EVIDENCE OF POSSIBLE HEAT DAMAGE. REPLACED BATTERY PACK AT 61WL. OPS CHECK GOOD IAW JIC 33-51-21 SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X)

Part: READING LIGHT — BURNED (CABIN)

ORD - FLT 4280 - ON APPROACH FOR LANDING IN SBN, FLIGHT ATTENDANT NOTED SMOKE IN THE AREA OF THE READING LIGHTS AT SEATS 1DC. FLIGHT ATTENDANT SELECTED BOTH READING LIGHTS OFF AND SMOKE STOPPED IMMEDIATELY. MX INSPECTED AND NOTED THE READING LIGHT TRANSFORMER AT SEATS 11DC WAS BURNED. READING LIGHTS WERE DEFERRED FOR THE RETURN TRIP TO ORD, PER MEL 25-19. FOLLOWING ARRIVAL IN ORD, MX REPLACED THE READING LIGHT POWER MODULE UNIT. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - FLT 3651 - F/A REPORTS EMERGENCY EXIT LIGHTS (FWD/AFT CABIN) CAME ON DURING TAXI. RAI'D POWER SUPPLY AT 73WL FOR EMERGENCY LIGHT SYSTEM. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING ROUTINE A-CHECK, FOUND FORWARD PAX COMPARTMENT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. RAI'D EMERGENCY LIGHT PACK AT 61 WL IAW ATR 72 JIC 33-51-21. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4321 - EMERGENCY EXIT LIGHT OVER NR 2 FLIGHT ATTENDANTS SEAT INOP. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FAN — FAILED (RIGHT)

FLT 3677 - FLIGHT DIVERTED TO BGS WITH SMELL AND VISIBLE SMOKE IN COCKPIT AND CABIN. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. AT DFW, TROUBLESHOOTING AND INSPECTION, INCLUDING GROUND RUNS, COULD NOT DUPLICATE PROBLEM, HOWEVER UPON TAXI TO GATE FOR FCF FLIGHT, THE RIGHT RECIRC FAN FAILED FILLING THE COCKPIT WITH SMOKE. MAINTENANCE RETURNED AIRCRAFT TO HANGAR AND RAI'D THE RECIRC FAN. OPS CHECK GOOD AND RUNS GOOD. NO FCF REQUIRED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GARLOCK SEAL — TORN (NR 2 ENGINE)

DFW - FLT 3620 - NR 2 ENGINE LOST OIL PRESSURE WITH ALL WARNINGS. CREW SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. REMOVED AND INSTALLED AC WILD GENERATOR GARLOCK SEAL IAW P AND W MM 72-10-00. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES 4,692. (X)