N417AT

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 34,349 hrs · 33,610 cycles

DURING POST FLIGHT, THE CREW FOUND THE SERVICE DOOR EXIT SIGN (LOWER) LIGHT VERY DIM. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED WIRE AT SERVICE DOOR EXIT SIGN IAW MM 20-27-13. OPS TEST SATISFACTORY IAW MM 33-50-00, OPT 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 34,240 hrs · 33,464 cycles

DURING MX INSP FOUND EMERGENCY BATTERY CHARGE LOW. THE ACFT WAS REMOVED FROM SERVICE. EMERGENCY BATTERY REPLACED IAW MC WC EX-243185-RAI-10020-002. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,136 hrs · 33,334 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY LIGHTING POWER SUPPLY AT FR 23 INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHTING POWER SUPPLY AT FR 23 IAW JIC 33-51-21, RAI 10000. THE OPS CHECKED WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: ROD — FAILED (ELEVATOR TRIM) · airframe 34,136 hrs · 33,334 cycles

DURING MX INSPECTION, FOUND THE RT ELEVATOR TRIM TAB CONTROL ROD FAILED SPECIAL DETAILED INSPECTION. FOUND FLAKED INTERNAL PROTECTIVE FINISH AND TRACES OF CORROSION. R & R THE RT ELEVATOR TRIM TAB CONTROL ROD IAW JIC 27-31-41.

Part: SKIN — SEPARATED (LT SPOILER) · airframe 34,136 hrs · 33,334 cycles

DURING MX INSPECTION FOUND THE LT SPOILER PANEL HAS SEPARATION AND CORROSION ON THE UPPER T/E. ACFT REMOVED FROM SERVICE. INSTALLED SPOILER ASSY IAW JIC 57-71-00. ACFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,136 hrs · 33,334 cycles

THE CREW REPORTED THE MAIN DOOR CABIN STAIRS EMERGENCY LIGHT IS INOPERABLE. R & R BULB IAW JIC 33-51-24. OPS CHECKED GOOD.

Part: CONTROL ROD — FAILED (RUDDER) · airframe 34,136 hrs · 33,334 cycles

DURING MX INSPECTION, FOUND THE RUDDER SPRING TAB CONTROL ROD FAILED SPECIAL DETAILED INSPECTION. FOUND TRACES OF CORROSION INSIDE ROD. THE ACFT WAS REMOVED FROM SERVICE. DURING MX INSP FOUND THE RUDDER SPRING TAB CONTROL ROD FAILED SPECIAL DETAILED INSPECTION. FOUND TRACES OF CORROSION INSIDE ROD. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED ROD IAW JIC 27-21-42 RAI 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: ROD — FAILED (LT ELEVATOR TRIM) · airframe 34,136 hrs · 33,334 cycles

DURING MX INSPECTION, FOUND THE LT ELEVATOR TRIM TAB CONTROL ROD FAILED, SPECIAL DETAILED INSPECTION. FOUND FLAKED INTERNAL PROTECTIVE FINISH AND TRACES OF CORROSION. R & R LT TRIM TAB CONTROL ROD ASSY IAW JIC 27-31-41.

Part: BATTERY — DISCHARGED (MASTER) · airframe 33,920 hrs · 33,074 cycles

DURING MX INSPECTION, FOUND THE MAIN BATTERY HAD A LOW VOLTAGE. ACFT REMOVED FROM SERVICE. R & R MAIN BATTERY & EMERGENCY BATTERY IAW W/C EX-243185-RAI-100010-006. ACFT RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 33,907 hrs · 33,055 cycles

THE CREW REPORTED AFTER TAKEOFF THEY WERE UNABLE TO MOVE LANDING GEAR HANDLE OUT OF DOWN POSITION. LANIDNG GEAR WOULD NOT RETRACT. REMOVED AND INSTALLED LT MLG FWD PROXIMITY SWITCH AND HARNESS IAW JIC 32-61-00 RAI 10000 AND AMM 20-21-00. OPS CHECKED GOOD.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,855 hrs · 32,991 cycles

DURING B INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT STRIP END CAPS AT GALLEY COMPARTMENT AND ROW 1AB MISSING. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED FLOOR EMERGENCY LIGHT STRIP END CAPS AT GALLEY COMPARTMENT AND ROW 1AB IAW CMM 33-52-10. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,493 hrs · 32,561 cycles

THE CREW REPORTED THE EMERGENCY FLOOD LIGHT AT THE SERVICE DOOR INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED OPS TEST OF EMERGENCY FLOOD LIGHT IAW JIC 33-50-00 OPT-10000. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,493 hrs · 32,561 cycles

THE CREW REPORTED THE EMERGENCY LIGHT AT THE BOTTOM OF THE STEPS IS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY LIGHT ASSY IAW JIC 33-51-24. THE OPS CHECK WAS GOOD. THE ACT WAS RETURNED TO SERVICE.

Part: DRAIN — CORRODED (RT WING) · corrosion level 2 · airframe 33,392 hrs · 4,910 cycles

DURING MX INSP FOUND CORRSION AT RT INBD AFT WATER DRAIN. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO E2-5700-490, PART A. THE ACFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,868 hrs · 31,838 cycles

ON FLIGHT 4950 THE CREW REPORTED THE EXIT LIGHT NEXT TO THE PASSENGER DOOR NEEDS TO BE RELAMPED. THE ACFT WAS REMOVED FROM SERVICE. RELAMPED EXIT SIGN AT PASSENGER DOOR REF AMM 33-51-00. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 32,818 hrs · 31,782 cycles

DURING MX INSP FOUND THE EMERGENCY FLOOR LIGHT STRIP IN GALLEY AREA HAS END CAP DAMAGED. THE ACFT WAS REMOVED FROM SERVICE. REPLACED GALLEY EMERGENCY LIGHT STRIP END CAPS IAW CMM 33-52-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 32,710 hrs · 31,658 cycles

AFTER TAKEOFF, THE CREW REPORTED THE WINSCREEN CRACKED. THE CREW ELECTED TO RETURN TO DEPARTURE. THE ACFT WAS REMOVED FROM SERVICE. R & R CAPTAIN'S WINDSHIELD IAW JIC 56-11-00, RAI 10000. THE OPS CHECK AND LEAK CHECK OK. THE ACFT WAS RETURND TO SERVICE.

Part: BATTERY — DISCHARGED · airframe 32,745 hrs · 31,696 cycles

DURING MX BASE VISIT FOUND THE EMERGENCY BATTERY LOW VOLTAGE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY BATTERY IAW JIC 24-31-85.. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 32,576 hrs · 31,488 cycles

EMERGENCY BATTERY DEAD. R & R EMERGENCY BATTERY IAW EX-243185-RAI-10020-002.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,328 hrs · 31,210 cycles

EMERGENCY EXIT LIGHT ON ENTRY STAIRS INOPERATIVE. RELAMPED EMERGENCY EXIT LT IAW JIC 33-51-24. OPS CHECKED GOOD.

Part: BULB — FAILED (READING LIGHT) · airframe 32,328 hrs · 31,210 cycles

UPON LANDING, THE FAS INFORMED ME THAT THE SAW AND SMELLED SMOKE IN THE FORWARD PART OF THE CABIN. R & R READING BULBS AT 1A, B AND 3 C, D IAW STANDARD PRACTICES 20-45-1.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,326 hrs · 31,207 cycles

EMERGENCY LIGHT FRONT NR1 GALLEY CART INOPERATIVE. RELAMPED EMERGENCY LIGHT AND OPS CHECKED GOOD IAW JIC 33-50-00, OPT 10000.

Part: LIGHT — FAILED (SEAT 9A) · airframe 32,321 hrs · 31,200 cycles

ON FINAL APPROACH, F/A CALLED AND ADVISED UD THERE WAS SMOKE IN THE CABIN. TOLD HER TO PREPARE FOR AN EVAC. ONCE WE STOPPED ACFT ON GROUND, SMOKE DISSAPATED. SMOKE COMING FROM SEAT 9A. R & R LIGHT ASSY AT SEAT 9A IAW/JIC 33-25-21 RAI 10000 OPTS CHECK GOOD.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 32,008 hrs · 30,868 cycles

THE CREW REPORTED THE EMERGENCY LIGHT IN THE MAIN PASSENGER ENTRY STEP WAS NOT WORKING. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND RE-SECURED LOOSE BULB AT PASSENGER ENTRY DOOR LOWER STEP, THE OPS CHECKED GOOD IAW AMM 33-50-00. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: CONTROL VALVE — INOPERATIVE (TE FLAPS) · airframe 31,942 hrs · 30,790 cycles

THE CREW REPORTED THAT UPON TAKEOFF THE FLAPS WERE STUCK AT 15 DEGREE POSITION AND WOULD NOT RETRACT TO 0 DEGREES, BUT THEY MOVED TO 30 DEGREES. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE ACFT PERFORMED A 15 DEGREE FLAPS LANDING AT DEPARTURE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE HYD CONTROL FLAP VALVE IAW MM 27-54-71, RAI 10000 AND 27-51-00-OPT 10020. THE OPS CHECK WAS NORMAL. THE ACFT WAS RETURNED TO SERVICE.

Part: BULB — OUT OF ADJUST (EMERGENCY LIGHT) · airframe 31,932 hrs · 30,779 cycles

DURING THE PREFLIGHT INSP THE CREW FOUND THE MAIN CABIN ENTRY DOOR EMERGENCY LIGHT OUT. THE ACFT WAS REMOVED FROM SERVICE. ADJUSTED BULB AND CHECKED IAW 33-50-00. NO PARTS REMOVED OR REPLACED. THE ACFT WAS RETURNED TO SERVICE.

Part: MASTER CYLINDER — FAILED (BRAKE SYSTEM) · airframe 31,674 hrs · 30,496 cycles

F/O'S BRAKE FAILED. R & R F/O SIDE MASTER CYINDER IAW JIC 32-42-13. OPS CHECKED GOOD.

Part: FIREWALL — CRACKED (NR 2 NACELLE) · airframe 31,656 hrs · 30,482 cycles

CRACK ON THE NACELLE REAR SECTION AT THE ANGLE BELOW THE FIREWALL ASSY. INSTALLED NR 2 ENGINE FIREWALL FLANGE IAW SRM 51-25-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,357 hrs · 30,133 cycles

EMERGENCY EXIT LIGHT ON MAIN CABIN ENTRY DOOR IS INOP. R & R EMERGENCY EXIT LIGHT BULB ON MAIN CABIN ENTRY DOOR IS IAW AMM 33-50-00. OPT GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,333 hrs · 30,107 cycles

FLOOR PROXIMITY, EMERGENCY ESCAPE PATH MARKING SYS HAS MULTIPLE BULBS LIGHT THAT DO NOT ILLUMINATE. OPS TESTED EMERGENCY ESCAPE PATH LIGHT AT FLOOR IAW JIC 33-50-00 WORKING PROPERLY.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 31,333 hrs · 30,107 cycles

GROUND FLOOD LIGHT ON BOTTOM STEP OF MAIN CABIN ENTRY DOOR IS INOP. OPS CHECKED FLOOD LIGHT EMERGENCY LIGHT AT MAIN CABIN DOOR BOTTOM STEP FOUND WORKING PROPERLY TESTED OK IAW JIC 33-50-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,230 hrs · 28,839 cycles

SMOKE SMELL IN CABIN. EMERGENCY DECLARED. NO HEAT SOURCE OR SMOKE FOUND. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: FAN — FAILED (ZONE 100) · airframe 30,230 hrs · 28,839 cycles

STRONG BURNING ODOR FELT THROUGH OUT THE CABIN AND COCKPIT. NO SIGN OF HEAT SOURCE NOR SMOKE WAS IDENTIFIED. OPENED ALL OVERHEAD BINS AND INSPECTED FOR BURNING ODOR ALL ELECTRICAL COMPONENTS IAW JIC 25-24-21. ALSO OPENED ACCESS DOORS TO ELECTRONIC RACKS AND INSPECTED FOR BURNING IAW JIC 25-14-12. NO BURNING SMELL WAS NOTICED AT THIS MOMENT ON THE ABOVE MENTIONED AREAS. FOUND RECIRCULATING FAN NR 2 MAKING A VERY LOUD NOISE AND WHEN SELECTED ON, A LIGHT BURNING WAS NOTICED. RECIRCULATING FAN PLACED ON MEL 21-3 AUTH NR 050108-C. ALSO PERFORMED ENGINE PUMP IAW JIC 72-00-00. ON 05-15-10 MEL 21-3 WAS CLEARED AT SJU: R & R NR 2 RECIRCULATING FAN IAW JIC 21-22-21-RAI-10000.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 29,772 hrs · 28,376 cycles

LT FUEL ELECTRIC PUMP SURROUNDING SKIN CORRODED. BLENDED CORROSION AND TREATED IAW EO E2-57MR-366.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 29,346 hrs · 27,928 cycles

CORROSION FOUND AROUND RT WING ELECTRICAL FUEL PUMP. BLEND OUT PERFORMED IAW EO NR E2-57MR-358.

Part: LIGHT — FAILED (ZONE 800) · airframe 28,887 hrs · 27,422 cycles

MAIN PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REMOVED AND REPLACED PAX DOOR EMERGENCY STAIR LIGHT ASSY IAW JIC 33-51-24-RAI-10000.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,472 hrs · 26,924 cycles

LT SEAT TRACK FROM FRAME 37 TO FRAME 39 HAS CORROSION. REPLACED SEAT TRACK IAW SRM NR 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,472 hrs · 26,924 cycles

FLOORBEAM AT FRAME 37 HAS CORROSION. REPLACED SECTION OF FLOORBEAM IAW ATR SRM NR 53-00-00 AND NR 51-25-04.

Part: EEC — FAILED (RT ENGINE) · airframe 28,217 hrs · 26,659 cycles

NR 2 ENGINE SHUT DOWN DUE TO A LOW PITCH CONDITION. ACCOMPLISHED DFDR DOWNLOAD IAW ETN NR E2-31-031R1. REPLACED RT EEC IAW JIC NR 73-23-61. ALSO REPLACED RT ENG IBV IAW JIC NR 75-31-61 AND RT ENG SERVO VALVE IAW PW MM NR 72-01-30. FCF PASSED.

Part: WIRE — BURNED (COCKPIT) · airframe 26,425 hrs · 24,881 cycles

EMERGENCY BATTERY FAULT IN FLIGHT AND ELECTRICAL BURNED ODOR IN COCKPIT. AFTER A RESET IT CAME BACK ON. ALSO A FAULT ON THE AVIONICS VENT CAME ON SHORTLY AFTER. REPAIRED VARIOUS WIRES OF THE EMERGENCY BATTERY CHARGE SYSTEM IAW JIC 20-27-17 AND PERFORMED OPT CK IAW JIC 24-31-85. PERFORMED OPT CK OF AVIONICS VENT VALVE IAW JIC 21-23-00.

Part: ENGINE — DAMAGED (LEFT) · airframe 26,407 hrs · 24,867 cycles

LT ENG ITT ROSE TO 800C DURING CLIMB, SMOKE IN THE COCKPIT AND PAX CABIN, CAPT SHUTDOWN ENGINE AS A PRECAUTIONARY PROCEDURE. REMOVED AND REPLACED LT ENGINE AS PER WC 0500-CS-20000-001 R1.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,013 hrs · 24,515 cycles

PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPAIRED LAMP IAW JIC NR 33-50-00. OP CK OK.

Part: ANTI-SKID SYS — MALFUNCTIONED (MLG) · airframe 25,521 hrs · 24,002 cycles

NUMBER 2 MAIN TIRE LOCK-UP DURING LANDING. TIRE NEEDS TO BE CHANGED. MAINTENANCE REPLACED NUMBER 2 MAIN WHEEL ASSY IAW ATR 72-JIC-12-37-32-RAI-10000-001. PERFORMED ANTI-SKID OPERATIONAL TEST IAW ATR-72-AMM32-42-00-FUT-10000-001.

Part: BATTERY PACK — BURNED (EMERGENCY LIGHT)

WHILE IN TAXI, FLIGHT ATTENDANT REPORTED STRONG ODOR FOLLOWED BY SMOKE IN CABIN. A/C RETURNED TO GATE. REPLACED BURNED 62WLA BATTERY PACK AND POWER SUPPLY EMERGENCY FLOOR LIGHT IAW JIC 33-51-01, OPS CHECK GOOD. NO EMERGENCY. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CRUISE, F/O WINDSHIELD CRACKED. AIRCRAFT DIVERTED. REPLACED WINDSHIELD IAW MM. (K)

Part: PROXIMITY SWITCH — INTERMITTENT (LT MLG)

WHILE IN CLIMB, LANDING GEAR DID NOT RETRACT. GEAR HANDLE DID NOT MOVE. AC RETURNED TO DEPARTURE. REPLACED PROXIMITY SWITCH NR 53GB. (K)

Part: SELECTOR — STUCK (MLG)

WHILE IN CLIMB, LANDING GEAR HANDLE STUCK. UNABLE TO SELECT UP POSITION. AIRCRAFT RETURNED. REPLACED LANDING GEAR SELECTOR HANDLE. (M)

Part: SELECTOR VALVE — BROKEN (MLG)

DURING CLIMB, UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE UP POSITION. REPLACED LANDING GEAR SELECTOR DUE TO BROKEN HANDLE. (M)

Part: ADC — FAILED (NR 1)

DURING TAKEOFF ROLL, CAPTAIN SIDE AIRSPEED FAIL FLAP CAME OUT, THE TRUE AIRSPEED SHOWED ONLY DASHES AND THE STANDBY ALTIMETER STUCK MOMENTARILY. TAKEOFF ABORTED. REPLACED NR 1 AIR DATA COMPUTER. (M)

Part: INDICATOR — FAILED (CAPT. AIRSPEED)

DURING TAKEOFF ROLL, CAPTAIN AIRSPEED INDICATOR FAILED AT 100 KTS, FLUCTUATED BETWEEN 80 KTS AND 120 KTS WITH RED FLAP. REPLACED AIRSPEED INDICATOR. (M)

Part: SMOKE — DETECTED (COCKPIT)

DURING TAXI, ELECTRICAL SMOKE IN CABIN. INSPECTED CABIN LIGHTING SYSTEM, INCLUDING LATERAL LIGHTS SOCKETS AND READING LIGHTS CIRCUIT BOARDS AND FOUND NO EVIDENCE OF DAMAGE THAT COULD CAUSE THE SMOKE IN THE CABIN. (M)

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT)

DFW - FLT 3769 - FLASH LIGHT IN FORWARD END OF CABIN DOES NOT SHOW A FLASHING RED LIGHT. DEFERRED PER MEL 25-33. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY PACK AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - FLT 3576 - LEFT FORWARD EXTERNAL AND PASSENGER DOOR EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE CLEANED PASSENGER DOOR SOCKET AND FOUND NO DEFECT WITH THE LEFT FORWARD LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3633 - LEFT EMERGENCY EXIT OUTSIDE LIGHTS INOPERATIVE. FOUND BAD SOCKET. REMOVED AND REPLACED PAX DOOR EMERGENCY FLOOD LIGHT PER ATR AMM JIC 33-51-21. NO DEFECTS NOTED, LEFT AFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — INOPERATIVE (FUSELAGE)

DFW - FLT 3633 - RIGHT AFT EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED BULB FOR THE RIGHT AFT EMERGENCY LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,874 hrs · 14,054 cycles

JAN - FLT 3262 - LOWER EMERGENCY EXIT LIGHT AT SERVICE DOOR INOPERATIVE. MAINTENANCE TIGHTENED BULB CONNECTION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FLOORBEAM — CORRODED (FRAME 38)

FLOORBEAM NR 38, CORROSION AROUND NUTPLATES. REMOVED AND BLENDED OUT CORROSION IAW ATR-72 SRM 51-21-58. REMOVED AND REPLACED FLOORBEAM NR 38 IAW ATR-72 SRM 51-25-01, 51-25-03 AND 51-25-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

LEFT AFT OUTBOARD SEAT TRACK HAS CORROSION IN TRACK (.025 INCH) TO T-5 AREA. BLENDED OUT CORROSION FOUND TO BE BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M)

Part: SEAT TRACK — CORRODED (BS 24-29)

LEFT MID INBOARD SEAT TRACK HAS CORROSION FROM FRAME 24 TO 29 BLENDED OUT CORROSION FOUND TO BE BEYOND LIMIT .028 INCH. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M)

Part: FLOORBEAM — CORRODED (BS 39-40)

FLOOR SUPPORT BETWEEN FLOORBEAMS 30 TO 40 CORRODED.. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 5125-25-58. REMOVED AND REPLACED SUPPORT IAW SRM 51-25-02 AND 51-25-03. (M)

Part: SEAT TRACK — CORRODED (BS 36-39)

RIGHT AFT FLIGHT ATTENDANT SEAT TRACK IS CORRODED AROUND THE NUTPLATES. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW EO NR E9-5300-013 R4. (M)

Part: SEAT TRACK — CORRODED (BS 24-29)

LEFT MID OUTBOARD SEAT TRACK HAS CORROSION AT FRAME 28D BLENDED OUT CORROSION FOUND TO BE BEYOND LIMITS AT ATTACHMENT POINT. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M)

Part: SEAT TRACK — CORRODED (BS 24-29)

RIGHT MID INBOARD SEAT TRACK HAS CORROSION FROM FRAME 24 TO 29, (.27 INCH ON T-5 AREA). BLENDED OUT CORROSION FOUND TO BE BEYOND LIMIT OF .033 INCH. REMOVED AND REPLACED SEAT TRACK IAW EO NR E9-5300-013 R4. (M)

Part: FLOORBEAM — CORRODED (FRAME 36)

FLOORBEAM NR 36, CORROSION AROUND NUTPLATES. REMOVED AND BLENDED OUT CORROSION IAW ATR-72 SRM 51-21-58. REMOVED AND REPLACED FLOORBEAM NR 36 IAW ATR-72 SRM 51-25-05. (M)

Part: DRAIN TRACK — CORRODED (FRAME 36-39)

PAX DOOR SILL DRAIN TRACK CORRODED. BLENDED OUT CORROSION ON SILL DRAIN TRACK, AND FOUND TO BE OUT OF LIMITS IAW ATR 72 SRM 51-21-42. INSTALLED PAX DOOR SILL DRAIN TRACK IAW ATR 72 SRM 51-25-01 AND 51-25-03. (M)

Part: SILL PLATE — CORRODED (FRAME 36-39)

PAX DOOR SILL CORRODED TOP AND BOTTOM. BLENDED OUT CORROSION ON SILL PLATE, (NOMINAL .071, REMAINING .061) IAW ATR 72 SRM 51-21-42. INSTALLED NEW DOOR SILL (WEB) IAW ATR 72 SRM 51-25-03. (M)

Part: ZEE — CORRODED (FRAME 39-41)

AFT CARGO BAY, RIGHT 'Z' MEMBER IS CORRODED. BLENDED OUT CORROSION IAW ATR 72 SRM. REMOVED AND REPLACED RIGHT 'Z' MEMBER IN AFT CARGO BAY IAW ATR 72 SRM 51-25-02. (M)

Part: FLOOR PAN — CORRODED (CABIN)

NUMEROUS AREAS OF PASSENGER DOOR PAN HAVE SURFACE CORROSION. BLENDED OUT CORROSION IAW ATR-72 SRM 51-21-58. REMOVED AND REPLACED DAMAGED SECTION OF PAX DOOR UPPER PANE IAW ATR-72 SRM 52-11-00. (M)

Part: FLOORBEAM — CORRODED (FRAME 39)

FLOORBEAM NR 39, CORROSION AROUND NUTPLATES. BLENDED OUT CORROSION IAW ATR 72 SRM 51-21-58. INSTALLED NEW FLOORBEAM NR 39 IAW ATR 72 SRM 51-25-02. (M)

Part: SEAT TRACK — CORRODED (FRAME 29/36)

LEFT AFT INBOARD SEAT TRACK HAS CORROSION. BLENDED OUT AND FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED LEFT AFT INBOARD SEAT TRACK IAW EO NR E9-5300-013 R4. (M)

Part: CHANNEL — CORRODED (FRAME 36-39)

PAX DOOR SILL SUPPORT IS CORRODED (AFT). BLENDED OUT TO BEYOND MANUAL LIMITS (IAW ATR-72 SRM 51-21-42). INSTALLED NEW FLOOR SUPPORT BETWEEN FRAME 36 AND 39 IAW ATR 72-SRM 51-25-01. (M)

Part: ZEE — CORRODED (FRAME 39-40)

LEFT Z-MEMBER IS CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW ATR 72 SRM 53-61-00. REMOVED AND INSTALLED Z-MEMBER IAW SRM 51-25-03. (M)

Part: CONNECTOR — LOOSE (BATTERY PACK)

HOU - 3627 - SOME OF THE AFT EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. RESEATED THE CONNECTOR ON THE AFT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: SEAT TRACK — CORRODED (CABIN)

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

Part: PLATE — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT OUTBOARD SEAT TRACK JUNCTION PLATE BETWEEN FRAME 35 AND 36 TO BE CORRODED. REMOVED AND REPLACED THE JUNCTION PLATE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SPLICE — CRACKED (FUSELAGE)

SAT - DURING EVALUATION AND MAJOR REPAIR TO KEEL BEAM CHORD AND MLG TRUSS ASSY, MAINTENANCE FOUND FRAME 26 LEFT FLOORBEAM AT BL '0' SPLICE HAD A .6 INCH CRACK ON BOTTOM RADIUS AND A CRACK ON PRESSURE PLATE FORWARD OF BL '0' SPLICE FITTING, .16 INCH LONG. CRACKS WERE INSPECTED PER S/B ATR 72-53-1026 AND REPETITIVE INSPECTION WAS INDICATED AS PER SRAS REF NR DS/ET 603, 22198, 1088. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TRUSS — CRACKED (RT MLG)

DFW - DURING ROUTINE 'A' CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR TRUSS ASSEMBLY WAS FOUND TO HAVE A CRACK AT FIRST RIVET HOLE TO ATTACH BRACKET SUPPORT FOR MLG PANEL 194 CR. AIRCRAFT WAS FERRIED TO SAT FOR EVALUATION. PERFORMED NDT INSPECTION AND VERIFIED CRACK WAS 1.2 INCHES LONG. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PER ATR SRM AND DWG 15S53540150. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: KEEL BEAM — CRACKED (MAIN GEAR WELL)

DFW - DURING ROUTINE 'A' CHECK INSPECTION, THE KEEL BEAM CHORD WAS FOUND CRACKED IN MAIN GEAR WELL. AIRCRAFT WAS FERRIED TO SAT FOR EVALUATION. CONFIRMED CRACK, R/I'D CHORD ASSY IAW SRM CLOSED UP ARGA AND RETURNED A/C TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

ORD - FLT 4310 - A COUPLE LIGHTS INOP ON FLOOR EMERGENCY LIGHTING. REPLACED LIGHTS AS REQUIRED. PERFORMED OPS CHECK AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: BLEED VALVE — FAILED (LT ENGINE)

OKC - FLT 3601 - ON CLIMB-OUT AFTER TAKEOFF, CREW REPORTED STRONG ELECTRIC SMELL IN CABIN, FOLLOWED BY LT PACK FAULT INDICATION. AIRCRAFT RETURNED TO OKC LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE INSPECTED AIRCRAFT BUT NO OBVIOUS DAMAGE WAS NOTED. ITEM WAS DEFERRED UNDER MEL AND AIRCRAFT CONTINUED SERVICE. LATER TROUBLESHOOTING FOUND THE NR 1 HP BLEED VAL AND OVERTEMP SWITCH TO BE THE CAUSE OF PACK FAULT. ITEMS WERE REPLACED AND OPS CHECK WAS SATISFACTORY. AIRCRAFT REMAINS IN SERVICE. (M)

Part: OVER TEMP SW — FAILED (LT ENGINE)

OKC - FLT 3601 - ON CLIMB-OUT AFTER TAKEOFF, CREW REPORTED STRONG ELECTRIC SMELL IN CABIN, FOLLOWED BY LT PACK FAULT INDICATION. AIRCRAFT RETURNED TO OKC LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE INSPECTED AIRCRAFT BUT NO OBVIOUS DAMAGE WAS NOTED. ITEM WAS DEFERRED UNDER MEL AND AIRCRAFT CONTINUED SERVICE. LATER TROUBLESHOOTING FOUND THE NR 1 HP BLEED VAL AND OVERTEMP SWITCH TO BE THE CAUSE OF PACK FAULT. ITEMS WERE REPLACED AND OPS CHECK WAS SATISFACTORY. AIRCRAFT REMAINS IN SERVICE. REF SIMA9700551.

Part: BATTERY — DISCHARGED (CABIN EEL)

DFW - DURING ROUTINE MAINTENANCE CHECK, NUMEROUS EMERGENCY LIGHTS OUT IN AFT SECTION OF AIRCRAFT. RAI'D EMERGENCY P/N 301-2001, LOCATION 62WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

ORD - FLT 4275 - EMERGENCY LIGHT ROW 10 FOUND INOPERABLE. REPLACED EMERGENCY LIGHT POWER SUPPLY 61WL, OPS CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. (X)

Part: DUCT — LOOSE (RT ACM)

ORD - FLT NR 4152 - DURING TAXI NR 2 BLEED LEAK WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RECONNECTED BLOWN DUCTING AT AIR CYCLE MACHINE INLET. (M)