N260AE

Part: EEC — FAULTED (NR 1 ENGINE) · airframe 33,421 hrs · 38,026 cycles

DURING CRUISE FLIGHT, CLEAR ATMOSPHERIC CONDITIONS NR 1 ENGINE FLAMEOUT, RESTART WAS SUCCESSFUL (DECLARED EMERGENCY) REMOVED AND INSTALLED NR1 ENG EEC IAW ATR JIC 73-23-61, RAI 10000-026 ALSO REMOVED AND INSTALLED NR 1 T2 SENSOR & NR 2 T2 SENSOR IAW MM 72-01-60. ALSO REPLACED AFU NR 1 ENG IAW MM 72-01-10 REF NRWC NR 327579 & 327568 FOR WORK ACCOMPLISHED.

Part: LIGHT — DAMAGED (EMERGENCY LIGHTS) · airframe 33,353 hrs · 37,957 cycles

FLOOR PATH EMERGENCY LIGHT STRIP BY ROWS 10&11 MISSING COVER AND DAMAGED. R & R FLOOR PATH LIGHT STRIP. OPS CHECK OK IAW MM JIC 33-50-00-OPT-10000.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,353 hrs · 37,957 cycles

SEVERAL LIGHTS OUT ON FLOOR PATH EMERGENCY LIGHTING. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW MM JIC 33-51-21-RAI-10000. OPS CHECK OK IAW 33-50-00-OPT-10000 (61WL).

Part: SOCKET — BURNED (GALLEY LIGHT) · airframe 33,349 hrs · 37,951 cycles

ELECTRICAL BURNING SMELL NOTICED BY F/A AND GROUND CREW WHEN A/C PARKED ON GROUND MORE MID CABIN TO GALLEY. FOUND AFT LIGHT SOCKET ABOVE 17-AB BURNED ITEM DEFERRED IAW MEL NR 33-2 AUTH, NR 070229-C. CAT "C" WAITING FOR COMPLETION OF MEL FOR FURTHER DETAILS. R & R LIGHT UPPER SOCKET IAW WIRING MANUAL, STANDARD PRACTICE 20-45-10 MEL RESTORED.

Part: SOCKET — BURNED (CABIN LIGHT) · airframe 33,007 hrs · 37,562 cycles

STRONG BURNING SMELL INSIDE COCKPIT AREA AFTER T/O. RETURN TO MIA FOR PRECAUTIONARY LANDING. FOUND FLUORESCENT TUBE SOCKET AT 290LG BURNED AND MELTING. R & R SOCKET AND TESTED IAW ATR 72 JIC 33-21-23. ALL TEST OK. ACFT OK FOR RETURN TO SERVICE.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 32,802 hrs · 37,302 cycles

EMERGENCY FLOOR PATH LIGHTING INOP AT PAX SEAT 10B. RELAMPED EMERGENCY FLOOR PATH LIGHT BULB IAW JIC NR 33-50-00.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 NACELLE) · airframe 32,560 hrs · 37,016 cycles

ENG NR 2 FIRE WARNING INDICATION DURING TAXI. BOTTLE NR 1 DISCHARGED. MODERATE TAILWIND DURING TAXI. R & R RT ENG FIRE EXTINGUISHING BOTTLE AND SQUIB IAW W/C EX-262171-RAI-10000-RT. NO SIGNS OF FIRE NOTED. PERFORMED ENG GROUND PERFORMANCE CHECK AND FOUND WORKING PROPERLY, NO LEAKS WERE FOUND IAW W/C EX-055007-CS-20000-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,730 hrs · 36,001 cycles

FRAME 36 FLOORBEAM HAS CORROSION. REMOVED AND REPLACED FLOORBEAM AT FR36 IAW EO NR E2-53EP-204.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,730 hrs · 36,001 cycles

FRAME 39 FLOORBEAM HAS CORROSION. REMOVED AND REPLACED FLOORBEAM AT FR39 IAW EO E2-5300-030.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,564 hrs · 35,816 cycles

ELECTRICAL BURNING ODOR IN COCKPIT. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,565 hrs · 35,816 cycles

SHORTLY AFTER LEAVING THE GATE THE ODOR OF ELECTRICAL WIRING BURNING IN THE COCKPIT WAS DETECTED. PAX IN 17A ALSO DETECTED SAME ODOR. FOUND LT ENGINE OVERSERVICED WITH OIL. DE-SERVICED TO CORRECT LEVEL IAW JIC NR 12-13-79-CHK-10000. PERFORMED ENGINE RUNS IAW JIC NR 72-00-00-ERU-10000. OPS CHECK GOOD. NO ELECTRICAL SMELL DETECTED.

Part: TOWERSHAFT — FRACTURED (LT ENGINE) · airframe 30,788 hrs · 34,946 cycles

THE AS RECEIVED EXAMINATION OF THE ENGINE SHOWED METALLIC FLAKES ON THE TURBOMACHINE CHIP COLLECTOR. THE HAND ROTATION OF HIGH PRESSURE (HP) REVEALED A DISCONTINUITY FROM THE ACCESSORY GEARBOX (AGB). THE AGB ANGLE DRIVE COVER WAS REMOVED AND THE TOWERSHAFT WAS FOUND FRACTURED. THE TOWERSHAFT HAD FRACTURED BELOW THE SPLINES AND THE SURFACES SHOWED SMEARING AND CORROSION. THE FRACTURE SURFACE SHOWED A FLAT TOPOGRAPHY INDICATION OF FATIGUE PROPAGATION. THE TOWERSHAFT SPIGOT FITS MATING WITH THE SPIRAL GEAR WEAR FOUND WORN. MAJOR PART AFFECTED (PRIMARY DISTRESS) P/N: 3111968-01 S/N: 50D536 DESCRIPTION: TOWERSHAFT CONDITION: FRACTURED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 29,306 hrs · 33,482 cycles

SERVICE DOOR'S BOTTOM EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULBS AND PERFORMED OP CK IAW JIC NR 33-50-00.

Part: BULB — FAILED (EMERGENCY LIGHTS) · airframe 29,142 hrs · 33,340 cycles

EMERGENCY LIGHT ON ON STAIRS. REPLACED EMERGENCY LIGHT BULB ON STAIRS IAW JIC 25-60-00.

Part: LIGHT — FAILED (PAX DOOR) · airframe 28,833 hrs · 33,037 cycles

PAX DOOR STAIR EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOD LIGHT ASSEMBLY IAW JIC NR 33-51-24. PERFORMED OP CK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

CORROSION FOUND ON EXTERNAL SURFACEOF LT GUTTER BETWEEN GUTTER BETWEEN FRAME 14 TO 17. FORWARD CARGO ENTRY GUTTER REPLACED AS PER SRM 51-25-01.

Part: LATCH — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

CARGO DOOR ENTRY CORROSION FOUND NEAR AFT DOOR LATCH FITTING. CARGO DOOR ENTRY REPAIRED AS PER SRM 53-00-00 FIG 402.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

FOUND FORWARD AND AFT HOLDING ANGLE FOR SIDE PANEL 222 CW AND 222A AW CORRODED. FORWARD AND AFT HOLDING ANGLE FOR SIDE PANEL 222CW AND 222AW REPLACED AS PER 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

FOUND FLOORBEAM AT FRAME 38 IS CORRODED. FLOORBEAM AT FRAME 38 REPLACED AS PER SRM 51-25-01.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

LT SEAT TRACK BETWEEN FRAME 39 AND FRAME 41 IS CORRODED. LT SEAT TRACK BETWEEN FRAME 39 AND FRAME 41 REPLACED AS PER SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

LT SEAT TRACK BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. LT SEAT TRACK BETWEEN FRAME 39 AND FRAME 39 REPLACED AS PER SRM 51-25-04

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

RT SEAT TRACK BETWEEN FRAME 39 AND FRAME 40 IS CORRODED. RT SEAT TRACK BETWEEN FRAME 39 AND FRAME 40 REPLACED AS PER SRM 51-25-04.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

RT THRESHOLD PLATE AT FRAME 36 IS CORRODED. RT THRESHOLD PLATE AT FRAME 36 REPLACED AS PER SRM 51-25-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

RT FLOOR BETWEEN FRAME 36 THRU 38 IS CORRODED. RT FLOOR SUPPORT BETWEEN FRAME 36 THRU 38 REPLACED AS PER SRM 51-25-01.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

RT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. RT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 REPLACED AS PER SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

FOUND FLOORBEAM AT FRAME 36 IS CORRODED. FLOORBEAM AT 36 REPLACED AS PER SRM 51-25-01 AND 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

FOUND FLOORBEAM AT FRAME 40 IS CORRODED. NEW FLOORBEAM INSTALLED IAW SRM 51-25-01 AND 51-25-04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

LT FLOOR SUPPORT BETWEEN FRAME 39 AND FRAME 40 IS CORRODED. LT FLOOR SUPPORT BETWEEN FRAME 39 AND FRAME 40 REPLACED AS PER SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

RT SEAT TRACK BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. RT SEAT TRACK BETWEEN FRAME 36 AND FRAME 39 REPLACED AS PER SRM 51-25-04.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

LT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 IS CORRODED. LT THRESHOLD BETWEEN FRAME 36 AND FRAME 39 REPLACED AS PER SRM 51-25-01.

Part: BULKHEAD — CORRODED (BS 2962) · corrosion level 2 · airframe 28,147 hrs · 32,325 cycles

CORROSION FOUND ON FORWARD PRESSURE BULKHEAD AT GROUND POINTS (8) LOCATIONS. FORWARD BULKHEAD LT AND RT UPPER AT STA 2962 REPAIRED AS PER SRM 53-11-10 FIG 404.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 28,148 hrs · 32,325 cycles

THREAD SUPPORT NR 1 (BOTTOM) OF PASSENGER DOOR STAIRCASE IS CORRODED UNDER NUT PLATES. THREAD SUPPORT NR 1 FROM BOTTOM REPLACED AS PER SRM 51-25-01.

Part: ENGINE — MALFUNCTIONED (RIGHT)

SHORTLY AFTER TAKEOFF, RT ENGINE. AC DECLARED EMERGENCY AND RETURNED TO DEPARTURE, NO FIRE INDICATION NOTED. REMOVED AND REPLACED RT ENGINE IAW MM 055006-CS20000-00R1. (K)

Part: LIGHT — BROKEN (CABIN)

MIA - FLT 9221 - CREW REPORTED ONE FLOOR PROXIMITY LIGHT AT ROW 15 IS BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT AT ROW 15. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED CRACK INDICATIONS DURING EDDY CURRENT ROTO TEST OF THE LEFT AND RIGHT WING TO FUSELAGE ATTACH POINTS AT FRAME 25 AND STRINGER 7. MAINTENANCE REPAIRED THE HOLES IAW EO E2-53MR-113. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED CRACK INDICATIONS DURING EDDY CURRENT ROTO TEST OF THE LEFT AND RIGHT WING TO FUSELAGE ATTACH POINTS AT FRAME 25 AND STRINGER 7. MAINTENANCE REPAIRED THE HOLES IAW EO E2-53MR-113. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0788. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCKS HOLES AT OUTBOARD SEAT TRACK ATTACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0783. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCK HOLES AT OUTBOARD SEAT TRACK ATTACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0781. (M)

Part: FLOORBEAM — OVERSIZED (FUSELAGE)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCK HOLES AT OUTBOARD SEAT TRACK ATTACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 20 AND 21 HAD MISDRILLED HI-LOCKS HOLES AT OUTBOARD SEAT TRACK ATTACH POINT. MAINTENANCE REPAIRED BOTH SEAT TRACKS IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AND THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AND THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0692. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AND THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0692. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR INNER SKIN CRACKED NEXT TO THE PRESSURE RELIEF DOOR AND THE UPPER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-00 AND 51-25-02, AND REPAIRED THE UPPER PAN IAW SRM 52-11-00 FIGURE 911. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PAN — CORRODED (PAX DOOR)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE PAX DOOR INNER SKIN CRACKED NEXT TO THE PRESSURE RELIEF DOOR AND THE UPPER PAN CORRODED. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 52-11-00 AND 51-25-02, AND REPAIRED THE UPPER PAN IAW SRM 52-11-00 FIGURE 911. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0785. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 39-40 CORRODED, AND THE RIGHT FLOOR SUPPORTS BETWEEN FRAMES 38-39 AND 36-38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0692. (M)

Part: BRACKET — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SPRING ATTACH BRACKETS BETWEEN FRAMES 39 AND 40 LEFT CORRODED. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKETS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE CLEARED TDMI NR 260MQ5301D5, DENT IN RIGHT SIDE OF FUSELAGE AT FRAME 40 STRINGER 17. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BRACKET — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SPRING ATTACH BRACKETS BETWEEN FRAMES 39 AND 40 LEFT CORRODED. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKETS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0694. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AND RIGHT FLOOR ZEE MEMBER BETWEEN FRAMES 39 ND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBERS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107301. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AND RIGHT FLOOR ZEE MEMBER BETWEEN FRAMES 39 ND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBERS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0693. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - FOUND DURING CPCP-2 INSPECTION MAINTENANCE, REPORTED THE PAX DOOR SILL PLATE BETWEEN FRAME 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107301. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: FRAME — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FRAMES 29 AND 38 CORRODED AT STRINGERS 20 AND 21. MAINTENANCE REMOVED AND REPLACED THE LOWER FRAME SEGMENTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FRAMES 29 AND 38 CORRODED AT STRINGERS 20 AND 21. MAINTENANCE REMOVED AND REPLACED THE LOWER FRAME SEGMENTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107302. (M)

Part: TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND SERVICE DOOR DRAIN TRACK BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA0691 (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD,LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, LAV, LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT MIDDLE OUTBAORD, RIGHT MIDDLE INBOARD AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200107303. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

MIA - FLT 5392 - UNABLE TO TURN OFF EMERGENCY EXIT LIGHTS IN THE FORWARD CABIN. REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY ABOVE THE NR 1 OVERHEAD BIN. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5226 - EMERGENCY FLOOR PROXIMITY LIGHT INOPERATIVE, PUT ON MEL. MAINTENANCE SOLDERED LOOSE SLEEVE BACK ON WIRE IAW ATR AWM 20-42-21. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,150 hrs · 19,382 cycles

MIA - FLT 5349 - EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT 68WL. OPS CHECKED GOOD. (X)

Part: CONTACTOR — FAILED (STARTER/GEN)

MCO - EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH IN THE ARM POSITION. REMOVED AND REPLACED NR 1 ENGINE START/GEN CONTACTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE RT MIDDLE OUTBOARD, THE LEFT AFT OUTBOARD AND THE RIGHT AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. OPER CNTRL NR SIMA991822 AND 99ZZZX2816.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE RT MIDDLE OUTBOARD, THE LEFT AFT OUTBOARD AND THE RIGHT AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. OPER CNTRL NR 99ZZZX2815 AND 99ZZZX2816. (X)

Part: FLOORBEAM — OVERSIZED HOLE (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND FLOORBEAM 36 WITH A HILOCK HOLE THAT WAS OVERSIZED BEYOND LIMITS. REPAIRED THE FLOORBEAM IAW SRM 53-00-00 PAGE 498. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE RT MIDDLE OUTBOARD, THE LEFT AFT OUTBOARD AND THE RIGHT AFT INBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. OPER CNTRL NR SIMA991822 AND 99ZZZX2815.

Part: RGB — DAMAGED (NR 1 ENGINE)

HRL - FLT 3724 - AFTER TAKEOFF FROM HRL THE FLT CREW SELECTED 'CLIMB' ON THE POWER MANAGEMENT PANEL AND BEGAN TO BRING THE CONDITION LEVERS BACK TO ACHIEVE 86 PERCENT NP WHEN THE NR 1 ENGINE BEGAN TO SURGE AND THEN THE TQ WENT TO ZERO. THE NP STABILIZED AT 30 PERCENT AND THE NH AT 45 PERCENT. THE ENGINE WAS SHUT DOWN AS A PRECAUTION MEASURE. A/C RETURNED TO HRL SAFELY. CFR WAS CALLED AND FOLLOWED THE AIRCRAFT TO THE GATE. PAX DEPLANED NORMALLY. MX INSPECTED ENG AND FOUND EVIDENCE OF DAMGE TO RGB COMPONENTS. PERFORMED SYSTEM AND ENGINE CHANGE CHECKS SATISFACTORILY. A/C WAS RETURNED TO SERVICE. (M)

Part: GEARBOX — DAMAGED (NR 1 ENGINE)

HRL - FLT 3724 - AFTER TAKEOFF, CREW SELECTED 'CLIMB' ON POWER MGMNT PANEL AND BEGAN TO BRING CONDITION LEVERS BACK TO 86 PERCENT NP WHEN THE NR 1 ENGINE BEGAN TO SURGE, THEN TORQUE WENT TO ZERO. NP STABILIZED AT 30 PERCENT AND NH AT 45 PERCENT. SHUT DOWN THE ENGINE AS PRECAUTIONARY MEASURE. A/C RETURNED TO FIELD. PAX DEPLANED NORMALLY. REMOVED AND REPLACED NR 1 ENGINE ASSY. EXTENSIVE DAMAGE TO VARIOUS RGB COMPONENTS. THIS MIGHT HAVE BEEN CAUSED BY AC GENERATOR FAILURE, WHEREBY THE DRIVESHAFT DID NOT SHEAR AND IT CAUSED SUDDEN RGB STOPPAGE AND SUBSEQUENT COMPONENT DAMAGE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDLE OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRACKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2396 THROUGH 98ZZZX2399.

Part: SILL — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL PLATE CORRODED. REMOVED AND REPLACED SILL PLATE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDLE OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRACKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR 98ZZZX2396 THROUGH 98ZZZX2399. (X)

Part: SILL — CORRODED (PAX DOORWAY)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE JOINT PLATE FOR THE LEFT AFT OUTBOARD SEAT TRACK TO PASSENGER DOOR SILL PLATE AT FRAME 36 CORRODED. REMOVED AND REPLACED THE JOINT PLATE. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X)

Part: SILL — CORRODED (PAX DOORWAY)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL PLATE GULLEY CORRODED. REMOVED AND REPLACED THE GULLEY. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X)

Part: STIFFENER — CORRODED (FUSELAGE)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT AND RIGHT STIFFENER BETWEEN FRAMES 36 AND 39 CORRODED. REMOVED AND REPLACED BOTH STIFFENERS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. REF: OPERATOR CONTROL NR 98ZZZX2395. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDLE OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRACKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2397 THROUGH 98ZZZX2399.

Part: STIFFENER — CORRODED (FUSELAGE)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT AND RIGHT STIFFENER BETWEEN FRAMES 36 AND 39 CORRODED. REMOVED AND REPLACED BOTH STIFFENERS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. REF: OPERATOR CONTROL NR SIMA981682.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDLE OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRACKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2396 THROUGH 98ZZZX2399.

Part: SUPPORT — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNEL SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR 98ZZZX2400 THROUGH 98ZZZX2402. (X)

Part: SUPPORT — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNEL SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR SIMA98168-1, AND, 98ZZZX2400 THROUGH 98ZZZX2401.

Part: SUPPORT — CORRODED (CARGO DOOR)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE CARGO DOOR DRAIN CHANNEL SUPPORT PLATE BETWEEN FRAMES 13 AND 17 CORRODED. REMOVED AND REPLACED THE SUPPORT PLATE. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. (X)

Part: SUPPORT — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNEL SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR SIMA98168-1, AND, 98ZZZX2400 THROUGH 98ZZZX2402.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDLE OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRACKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2396 THROUGH 98ZZZX2399.

Part: SILL — CORRODED (SERVICE DOORWAY)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR SILL PLATE WEB CORRODED. REMOVED AND REPLACED THE WEB. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X)

Part: SUPPORT — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNEL SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR SIMA98168-1, AND, 98ZZZX2401 THROUGH 98ZZZX2402.

Part: SILL — CORRODED (PAX DOORWAY)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR THROAT AND SILL PLATE CORRODED. REMOVED AND REPLACED THE THROAT PLATE. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAM 33 AND 39 WS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 33 AND 39 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FLOORBEAM 36 AND 38 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAM 36 AND 38 IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (BS 38)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT FAIL/SAFE BETWEEN STRINGER 20 AND 21 AT FRAME 38 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE FAIL/SAFE ANGLE IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAM 33 AND 39 WS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 33 AND 39 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FLOORBEAM 36 AND 38 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAM 36 AND 38 IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3825 - EMERGENCY LIGHTS AT FORWARD EMERGENCY EXITS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD IAW ATR 72 JUC 24-30-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - FLT 3540 - AFT CABIN EMERGENCY LIGHTS STAY ON. RAI EMERGENCY POWER SUPPLY AND BATTERY PACK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MAF - FLT 3570 - DURING TEST, THE FORWARD CABIN EMERGENCY LIGHT WOULD NOT OPERATE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

LBB - FLT 3853 - PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTORS — DIRTY (NR 2 FIRELOOP)

DFW - FLT 3892 - ON LANDING, NR 2 ENG FIRE ILLUMINATED CAP ALONG WITH MASTER WARN, HOWEVER, NR 2 ENG FIRE HANDLE DID NOT ILLUMINATE. RED FUEL SHUT OFF LIGHT IN THE RT CONDITION LEVER DID NOT ILLUMINATE. ALL ENG INSTRUMENT IND NORM. F/A'S OBSERVED NO SMOKE OR FLAMES FROM RT ENG. AFTER 5 SECS THE NR 2 ENG FIRE LIGHT ON THE CAP WENT OUT. TESTED CAP LIGHT AND TEST NORMAL. PERFORMED ENG FIRE TEST AND SYSTEM TESTED NORM WITH ALL LIGHTS TESTING NORM. VISUAL INSPECTION OF RT ENG FIRE DETECTION IAW 26-12-61 PERFORMED OPS TEST OF RT FIRE DETECTION IAW 26-12-00 AND NO FAULTS WERE NOTED. PERFORMED GROUND RUNS AND COULD NOT DUP AND CLEANED FIRE LOOP CONNECTORS AS PRECAUTIONARY. A/C WAS RETURNED TO SERV. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - FLT 3530 - ONE LIGHT IN FLOOR PATH LIGHTING IN OPERATIVE. REPLACED POWER SUPPLY 43WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: UPLOCK BOX — FAILED (RT MLG)

CRP - FLT 3822 - GEAR UNSAFE RIGHT MAIN ON UPPER PANEL ON CLIMB. MAINTENANCE CONFIRMED DISCREPANCY. REPLACED RT UPLOCK BOX IAW WITH ATR 72 AMM JIC 32-31-00. PERFORMED GEAR SWING, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

ICT - FLT 3746 - PAX DOOR EMERGENCY LIGHT INOP. REPAIRED BROKEN GROUND WIRE TO LIGHT. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GCU — FAILED (LEFT)

HRL - FLT 3724 - FLIGHT CRWE NOTICED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO GATE, FLIGHT CREW CALLED CFR. NO FIRE WAS FOUND AND PASSENGERS DEPLANED NORMALLY. RAI'D AC GEN BPCU AND GCU. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GEAR SELECTOR — FAILED (COCKPIT)

HOU - FLT 3548 - UPON DEPARTURE, THE AIRCRAFT GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO HOUSTON SAFELY, MEL 32-3 ISSUED. AIRCRAFT WAS FLOWN TO DFW, REPLACED LANDING GEAR SELECTOR HANDLE THERE. PERFORMED OPERATIONAL CHECK IAW AMM 32-30. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

GRR - EMERGENCY LIGHTS IN AFT CABIN FOUND INOPERATIVE IN MAINTENANCE CHECK. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

SBN - FLT 4127 - FLAP EXTENSION FLAG STUCK WHEN FLAPS WERE SELECTED TO 30 DEGREES WITH A FLAP UNSTUCK WARNING. FLAPS WORKED OK AT 15 DEGREE SETTING. RESET NR 1 AND NR 2 MFC'S AND PERFORMED OPERATIONAL CHECK OF THE FLAP SYSTEM. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT COMPLETED SATISFACTORY TEST FLIGHT. AIRCRAFT WAS RETURNED TO SERVICE. (X)