N429AT

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,054 hrs · 32,209 cycles

THE CREW REPORTED THE PASSENGER MAIN ENTRY DOOR BOTTOM EMERGENCY EXIT LIGHT WAS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-50-00 AND SPM 20-48-51. PERFORMED OPS CHECK IAW JIC 33-50-00-CHK-10000, SYS TESTED NORMAL. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 34,918 hrs · 32,048 cycles

DURING MX INSPECTION, FOUND THE FLOOR EMERGENCY LIGHTING AT 4 AB CONNECTOR PLUG DISCONNECTED AT WIRES. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED WIRES AT 4 AB EMERGENCY LIGHTING CONNECTOR PLUG 20-43-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 34,861 hrs · 31,988 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING END CAP AT SEAT 1B, 10B, 15B AND GALLEY AREA. THE ACFT WAS REMOVED FROM SERVICE. R & R LIGHT STRIP IN GALLERY AREA AND RE-INSTALLED LOOSE END CAPS AT SEAT 1B, 10B, AND 15B IAW CMM 33-52-10. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 34,833 hrs · 31,956 cycles

DURING MX INSPECTION, FOUND THE GALLEY COMPTARTMENT AFT EMERGENCY LIGHT STRIP BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE GALLEY COMPTARTMENT AFT EMERGENCY LIGHT STRIP IAW CMM 33-52-10. THE OPS CHECKED GOOD IAW JIC 33-50-00-OPT-10000. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 34,784 hrs · 31,898 cycles

DURING MX INSPECTION, FOUND THE END CAPS MISSING ON EMERGENCY FLOOR LIGHT STRIP IN GALLEY AREA. ACFT REMOVED FROM SERVICE. REPLACED EMERGENCY FLOOR LIGHT STRIP END CAPS IN GALLEY AREA IAW JIC 25-28-21 RAI 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED · airframe 34,783 hrs · 31,897 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY BATTERY LOST CHARGE. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY BATTERY IAW JIC 24-31-85-RAI-10020-004. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED · airframe 34,784 hrs · 31,898 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY BATTERY CHARGE BELOW LIMITS. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY BATTERY IAW EX-243185-RAI-10020. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHTS) · airframe 34,615 hrs · 31,710 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY LIGHT AT GALLEY FLOOR MISSING END CAP. AIRCRAFT REMOVED FROM SERVICE. INSTALLED MISSING END CAP ON FLOOR EMERGENCY LIGHT IAW CMM 33-52-10. AIRCRAFT RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 34,545 hrs · 31,632 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHT BY THE PASSENGER ENTRY DOOR WAS OUT. THE ACFT WAS REMOVED FROM SERVICE. RELAMPED, BUT DID NOT FIX THE ISSUE. FURTHER TROUBLESHOOTING FOUND A BROKEN WIRE AT THE LIGHT ASSY. REPAIRED THE WIRE IAW SPM 20-40-00. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,507 hrs · 31,588 cycles

DURING MAINTENANCE INSPECTION, FOUND AFT EMERGENCY LIGHT BY GALLEY AREA INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD EMERGENCY POWER SUPPLY IAW JIC 33-51-21. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED · airframe 34,398 hrs · 31,449 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY BATTERY HAS LOW VOLTAGE. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY BATTERY IAW WC EX-243185-RAI-10020-001. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 34,305 hrs · 31,342 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING END CAP AT SEAT 1B. THE ACFT WAS REMOVED FROM SERVICE. FOUND AND REINSTALLED EMERGENCY FLOOR LIGHT STRIP MISSING END CAP AT SEAT 1B IAW JIC 33-51-24 RAI 10000. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 34,208 hrs · 31,226 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP LOOSE AT GALLEY AREA. ACFT REMOVED FROM SERVICE. RESECURED EMERGENCY FLOOR LIGHT STRIP AT GALLEY AREA IAW CMM 33-50-01. RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,149 hrs · 31,154 cycles

DURING MX INSPECTION, FOUND THE AFT FLASHLIGHT BATTERY LOW IAW THE FAA REPORT. ACFT REMOVED FROM SERVICE. REPLACED BATTERY. ACFT RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,984 hrs · 30,956 cycles

ON FLIGHT 4930, THE CREW REPORTED THE SERVICE DOOR LOWER EMERGENCY EXIT SIGN INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R THE SERVICE DOOR LOWER EXIT SIGN IAW JIC 25-26-27-RAI-10000-005 IAW W/C EX-335000-OPT-10000-001. THE OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — LOOSE (GALLEY) · airframe 33,982 hrs · 30,954 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT LOOSE IN GALLEY AREA. ACFT REMOVED FROM SERVICE. ADJUSTED EMERGENCY FLOOR LIGHT IN THE GALLEY AREA IAW JIC 33-50-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,856 hrs · 30,802 cycles

DURING MX INSPECTION FOUND THE F/A NR 2 FLASHLIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 2 F/A FLASHLIGHT IAW JIC 25-26-25 RAI 10000. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 33,560 hrs · 30,442 cycles

DURING MX VISIT, FOUND FLOOR EMERGENCY LIGHT STRIP MISSING END CAP AT SEAT 12D. ACFT REMOVED FROM SERVICE. REPLACED END CAP IAW CMM 33-20-00. ACFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 3,291 hrs · 29,739 cycles

THE F/A REPORTED THE EMERGENCY EXIT LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. C/A: R & R BULB IAW JUC 33-50-00. THE OPS CHECK WAS GOOD IAW JIC33-10-00. THE ACFT WAS RETURNED TO SERVICE,

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE RT WING ASSY LOWER SKIN SURFACE AT RIB 10 JACK POINT. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT WING ASSY LOWER SKIN SURFACE AT RIB 10 JACK POINT. PERFORMED SRAS DO/TS-1209/05 3141 ISSUE B, NO NEW CORROSION NOTED IN AREA AT THIS TIME.

Part: RIB — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE RT INBD FLAP ASSY RIB. CORROSION WAS FOUND OUT OF LIMITS. CLEANED LIGHT SURFACE CORROSION IAW SRM 51-21-42. TREATED, PRIMED AND TOP COATED AREA IAW SRM 51-21-17 AND 51-21-27.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE LT OTBD FLAP ASSY SUPPORT. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON LT OTBD FLAP ASSY SUPPORT. CLEANED LIGHT SURFACE CORROSION ON LT OTBD FLAP SUPPORT IAW SRM 51-21-42. TREATED, PRIMED AND TOP COATED SUPPORT IAW SRM 51-21-17 AND 51-21-27.

Part: RIB — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE RT OTBD FLAP ASSY RIB. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT OTBD FLAP ASSY RIB. CLEANED LIGHT SURFACE CORROSION ON RT OTBD FLAP SUPPORT ATTACH POINT IAW SRM 51-21-42. TREATED, PRIMED AND TOP COATED AREA IAW SRM 51-21-17 AND 51-21-27.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE LEFT OTBD FLAP ASSY SUPPORT. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON LT OTBD FLAP ASSY SUPPORT. CLEANED LIGHT SURFACE CORROSION ON LT OTBD FLAP SUPPORT IAW SRM 51-21-42. TREATED, PRIMED AND TOP COATED SUPPORT IAW SRM 51-21-17 AND 51-21-27.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE RT WING ASSY LOWER SLAT-STRIP UPPER SUFACE NEAR RIB 12. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT L/E WING ASSY LOWER SLAT-STRIP UPPER SURFACE NEAR RIB 12. PERFORMED SRI DO/TS-3915/11-15634 AND SRAS DO/TS-4162/03-1…2651 ISSUE B.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE LT WING ASSY LOWER SKIN SURFACE AROUND WATER DRAIN AT RIB 5 BETWEEN STIFFNERS 6-7. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON LT WING ASSY LOWER SKIN SURFACE AROUND WATER DRAIN AT RIB 5 BETWEEN STIFFENERS 6-7. PERFORMED SRI DO/TS-3833/11-15655 AND SRAS DO/TS-2187/10…5735 ISSUE C.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE RT WING ASSY LOWER SKIN SURFACE INBD AND OTBD OF RIB 8 FLAP ATTACH FITTING. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON RT T/E WING ASSY LOWER SKIN SURFACE INBD AND OTBD OF RIB 8 FLAP ATTACH FITTING. PERFORMED SRI DO/TS-3678/11-15633 AND SRAS DO/TS3678/11 6557.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE LT OTBD FLAP ASSY SUPPORT. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON LT OTBD FLAP ASSY SUPPORT PN S5751224720000. R & R SUPPORT BRACKET ASSY IAW MM 51-25-02.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 32,922 hrs · 29,713 cycles

DURING THE MX BASE CHECK FOUND CORROSION ON THE LT OTBD FLAP ASSY SUPPORT. THE ACFT WAS REMOVED FROM SERVICE. CORROSION WAS FOUND OUT OF LIMITS ON LT OTBD FLAP ASSY SUPPORT. R & R SUPPORT BRACKET ASSY IAW MM 51-25-02.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 32,870 hrs · 29,659 cycles

DURING THE PREFLIGHT INSP, FOUND THE EMERGENCY GROUND FLOOD LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY GROUND FLOOD LIGHT BULB IAW JIC 33 50 00. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BURNED (AUDIO PANEL) · airframe 32,365 hrs · 29,104 cycles

AT CRUISE 14000FT SMOKE COMING FROM BEHIND CAPTAIN LEFT SHOULDER FOR ABOUT 1 MIN. COULD SEE AND SMELL THE SMOKE WHICH WAS COMING CLOSE TO THE HEADSET JACK. FOUND BURNED ELECTRICAL CABLES BEHIND CAPTAIN SEAT AT PANEL 80 VU. REPAIRED CABLES TO CONNECTOR 54 VC PINS -E,-H,-A AND H AND TO CONNECTOR 232 VC PIN E AS PER MM 20-27-13 AND 20-27-17. PERFORMED OPERATIONAL TEST OF ALL AFFECTED SYSTEMS. GPS AS PER ETN E2-34-018, ACARS SYSTEM AS PER 23-24-00 AND OXYGEN SYSTEM AS PER 35-12-00 AND 35-23-00. FOUND IT SATISFACTORY.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 32,061 hrs · 28,703 cycles

EMERGENCY LIGHT IN CABIN STAIR NOT WORKING. REPAIRED WIRE A ON PAX DOOR CONNECTOR PLUG IAW AMM 20-27-17, OPS CHECK OK.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 31,448 hrs · 27,974 cycles

EXCESSIVE FUEL BURN OUT OF RT FUEL TANK - NO FUEL BURN OUT OF LT TANK. "EMERGENCY DECLARED". R & R CROSSFEED FUEL VALVE AND ACTUATOR IAW 28-23-72. RAI 10000 AND 28-23-71 RAI 10000. OPS TEST GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,352 hrs · 27,853 cycles

EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. R & R THE POWER SUPPLY AND BATTERIES AT LOCATION 73WL AND OPS CHECK OK IAW AMM JIC 33-51-21-RAI-10000, 33-51-21-RAI-10010, 33-50-00-OPT-10000 AND WORK CARD EX-335000-OPT-10000.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 30,994 hrs · 27,410 cycles

CORROSION ON LT WING LOWER SKIN AT FUEL MAG STICK. OTBD OF RIB 5 BTW STIFFENERS 5-6. PERFORMED TEMPORARY REPAIR LT WING LOWER SKIN AT FUEL MAG STICK OTBD OF RIB 5 BTW STIFFENERS 5-6. ATR HAS ADVISED THAT DAMAGE CAN REMAIN AS IS UNTIL THE NEXT SCHEDULED C-CHECK WHEN A PERMANENT REPAIR WILL BE APPLIED IAW SRI DO/TS-2187/10-13660 ISSUE B AND EO E2-57MR-382.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 30,994 hrs · 27,410 cycles

CORROSION ON LT WING LOWER SKIN AT RIB 10 JACK POINT. PERFORMED TEMPORARY REPAIR LT WING LOWER SKIN AT RIB 10 JACK POINT FOLLOWING SRI INSTRUCTIONS UNTIL NEXT SCHEDULED C-CHECK WHEN A PERMANENT REPAIR WILL BE APPLIED IAW SRI DO/TS-2187/10-13360 ISSUE B AND EO NR E2-57MR-381.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 29,979 hrs · 26,195 cycles

MAIN PAX DOOR STAIR EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY FLOOD LIGHT AT MAIN PAX DOOR STAIR IAW JIC NR 33-50-00. OPS CK GOOD IAW JIC NR 33-50-10.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 26,424 hrs · 22,555 cycles

EMERGENCY EXIT LIGHT UNDER SERVICE DOOR INOP. REPAIRED BROKEN WIRE AT EMERGENCY LIGHT ASSY, AS PER STANDARDS PRACTICES 20-20-00, OP CHECK FOUND OK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

TAIL BUMPER AFT BTM ANGLE CORRODED. TAIL BUMPER AFT BTM ANGLE CORROSION REMOVED AS PER SRM 51-21-42 FOUND OUT OF LIMITS 51-10-10 TAIL BUMPER ANGLE REPLACED AS PER SRM 51-25-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

LT "Z" FLOOR BETWEEN FRAME 39-40 CORRODED ON LOWER SURFACE. LT "Z" FLOOR BETWEEN FRAME 39-40 REPLACED AS PER SRM 51-25-02.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

RT THRESHOLD BETWEEN FRAME 36-39 BRACKET ON FRAME 37 CORRODED. RT THRESHOLD BETWEEN FRAME 36-39 BRACKET ON FRAME 37 FABRICATED (W/C 172780) AND INSTALLED IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

FOUND FLOORBEAM AT FRAME 40 CORRODED. FLOORBEAM AT FRAME 40 REPAIRED AS PER SRM 53-00-00 FIG 435.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

STR 21R , BETWEEN FRAME 39-38 NEXT TO TAIL BUMPER BOX FOUND CORRODED. STRINGER 21R BETWEEN FRAME 38-39 REPAIRED AS PER SRM 53-00-00 FIG 428.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

FOUND FLOORBEAM 39 CORRODED. FLOORBEAM 39 REPAIRED AS PER SRM 53-00-00 FIG 435.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,125 hrs · 22,279 cycles

RT CHORD ANGLE BTWEEN FRAME 13-17 CORRODED. RT CHORD ANGLE REPAIRED AS PER SRM 53-31-50.

Part: BLEED VALVE — INOPERATIVE (NR 1 ENGINE)

ON TAKEOFF ROLL, LEFT ENGINE REACHED 787 DEGREES, ABORTED TAKEOFF. REPLACED LT ENGINE INTERCOMPRESSOR BLEED VALVE AS EPR JIC 75-31-61, TRIM RESISTOR HARNESS AND BUS BAR HARNESS AS PER MM 72-01-60. PERFORMED ENGINE RUNUP, PARAMETERS FOUND WORKING PROPERLY AS PER MM 72-00-00. (M)

Part: SOCKET — BURNED (CABIN LIGHTS)

BURNED ODOR IN MID SECTION OF THE CABIN. NO FIRE OR SMOKE EVIDENCE NOTED HOWEVER, FOUND A LIGHT SOCKET BURNED OUT. REPLACED LIGHT SOCKET. (K)

Part: AUTOFEATHER SYS — INOPERATIVE (RT ENGINE)

DURING TAKEOFF THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) DIS NOT ARM. CREW ABORTED THE TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE AUTO FEATHER UNIT.

Part: EEC — FAULTY (RT ENGINE)

NO TORQUE INDICATION DURING TAKEOFF ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ELECTRONIC ENGINE CONTROL (EEC).

Part: AUTOFEATHER SYS — MALFUNCTIONED (NR 2)

AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) SYSTEM DID NOT ARM DURING TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 AUTOFEATHERING UNIT.

Part: SPACER — CRACKED (MLG)

SJU - ON BOTH MAIN LANDING GEARS, THE SPACER ABOVE THE SWINGING LEVER IS CRACKED. DISCREPANCY FOUND DURING PERFORMANCE OF FCD E2-32-004, VISUAL INSPECTION OF LANDING GEAR SWINGING LEVER SPACER. (M)

Part: FLOORBEAM — CORRODED (FRAME 36)

FLOORBEAM NR 36 HAS CORROSION AROUND SEVERAL HOLES UPPER AND LOWER SURFACE AT FLANGE. BLENDED CORRODED AREAS IAW ATR-72 SRM 51-21-58, REMAINING THICKNESS .054. REMOVED AND INSTALLED NEW FLOORBEAM NR 36 IAW ATR SRM 51-25-01. (M)

Part: SUPPORT — CORRODED (FRAME 36-38)

RIGHT CHANNEL, FLOOR SUPPORT, BETWEEN FRAMES 36 AND 38 CORRODED. BLENDED OUT OT BEYOND MANUAL LIMITS. INSTALLED NEW FLOOR SUPPORT BETWEEN FRAME 36 AND 38, IAW ATR 72 SRM 51-25-02. (M)

Part: ZEE — CORRODED (FRAME 39-41)

FOUND CORROSION ON LEFT Z-MEMBER IN LAV BLENDED OUT CORROSION IAW SRM 51-21-58. FOUND TO BE BEYOND LIMITS. REMOVED AND INSTALLED MEMBER IAW ATR SRM 51-25-03. (M)

Part: STANCHION — CORRODED (FRAME 38)

FLOORBEAM NR 38 LEFT STANCHION HAS CORROSION AROUND SEVERAL HOLES. BLENDED CORRODED AREAS IAW ATR-72 SRM 51-2158, REMAINING THICKNESS .053 INCH. REMOVED AND INSTALLED NEW FLOORBEAM NR 38 IAW ATR SRM 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FRAME 36)

RIGHT AFT INBOARD SEAT TRACK HAS CORROSION AROUND HI-LOK HOLES AT FLOORBEAM NR 36. BLENDED CORROSION IAW ATR-72 SRM 51-21-42. COMPLIED WITH EO NR E9-5300-013 R4, PART 'B' WAS SATISFACTORILY ACCOMPLISHED. (M)

Part: SEAT TRACK — CORRODED (FRAME 34-36)

LEFT AFT INBOARD SEAT TRACK HAS CORROSION AREAS FROM FLOORBEAM 34 TO 36. BLENDED CORROSION IAW ATR-72 SRM 51-21-42. COMPLIED WITH EO NR E9-5300-013 R4, PART 'B' WAS SATISFACTORY ACCOMPLISHED. (M)

Part: FLOORBEAM — CORRODED (FRAME 39)

FLOORBEAM NR 39 HAS CORROSION AROUND SEVERAL HOLES, UPPER AND LOWER SURFACE AT FLANGE. BLENDED CORRODED AREAS IAW SRM 51-21-58. REMAINING THICKNESS .053 INCH. REMOVED AND INSTALLED NEW FLOORBEAM NR 39 IAW ATR SRM 51-25-01. (M)

Part: ZEE — CORRODED (FRAME 39-41)

FOUND CORROSION ON RIGHT Z-MEMBER IN AFT CARGO. BLENDED OUT CORROSION IAW SRM 51-21-58. REMOVED AND INSTALLED MEMBER IAW ATR SRM 51-25-03. (M)

Part: STANCHION — CORRODED (FRAME 36)

FLOORBEAM NR 36 LEFT STANCHION HAS CORROSION AROUND GROUND SCREW HOLE. BLENDED CORRODED AREAS IAW SRM 51-21-58. REMOVED AND INSTALLED STANCHION IAW ATR SRM 51-25-01. (M)

Part: BRACKET — CORRODED (FRAME 36-38)

PASSENGER DOOR, TOP TWO FAIRING BRACKETS CORRODED. REMOVED CORROSION IAW ATR-72 SRM 51-25-42. MFG P/N S53689609016 AND S5389609014. REMOVED CORROSION, CLEANED AND TREATED PANEL AND PAINTED IAW SRM 51-25-42. (M)

Part: SEAT TRACK — CORRODED (FRAME 39-40)

CORROSION AROUND SCREW HOLES TO SEAT TRACK. BLENDED OUT CORROSION TO SEAT TRACK IAW ATR72 SRM 51-21-42. EO NR E9-5300-015 R7 PART 'B' WAS SATISFACTORILY ACCOMPLISHED. (M)

Part: SEAT TRACK — CORRODED (FRAME 34-36)

LEFT AFT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FLOORBEAMS 34 TO 36. BLENDED CORRODED AREAS IAW ATR-72 SRM 51-21-42. REMOVED AND INSTALLED NEW LEFT OUTBOARD SEAT TRACK IAW ATR-72 SRM 51-25-04. (M)

Part: BLADE SHEATH — MISSING (LT PROPELLER)

DURING CRUISE, CREW REPORTED SEVERE VIBRATION FROM THE LEFT PROPELLER ALONG WITH TORQUE FLUCTUATIONS. DURING INSPECTION OF LEFT PROPELLER, FOUND ONE BLADE WITH ITS LEADING EDGE NICKEL SHEATH MISSING. BLADE WAS REMOVED AND REPLACED WITH SATISFACTORY RESULTS AFTER RUN-UP.

Part: TQ SENSOR — MALFUNCTIONED (NR 2 ENGINE)

DFW - FLT 3805 - AIR TURN BACK, NR 2 ENGINE TORQUE SURGED WHILE LEVEL AT 4000 FEET ON DEPARTURE. REMOVED AND INSPECTED NR 2 ENGINE TORQUE SENSOR AND INTERTURBINE BLEED VALVE. COMPLIED WITH OVER TORQUE INSPECTION. GROUND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)