N643AS

Part: ANGLE — CRACKED (RT WING BOX) · airframe 28,352 hrs · 32,939 cycles

RIGHT WING BOX FRAME 28A REPAIR ANGLE CRACKED.

Part: PLATE — CRACKED (LT WING) · airframe 28,352 hrs · 32,939 cycles

LEFT WING BOX FR 28, FACE PLATE CRACKED. LT WING BOX FR 28 FACE PLATE REPLACED IAW SRM 51-25-01.

Part: SKIN — CORRODED (FAIRING) · airframe 28,352 hrs · 32,939 cycles

ON MLG SKIN CORRODED AT FR 27 BL 0. CORROSION REMOVED ON MLG SKIN AT FR 27 BL 0 IAW SRM 51-21-42 U/T PERFORMED IAW NTM NOM=0.063" MIN=0.060". REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.063. MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-51-00 FIG 301. SUPPLEMENTAL - SDR CLOSED 11/01/07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

RIGHT MLG INTERCOSTAL AT FR 25 CRACKED. REPLACED AND INSTALL IAW SRM 51-25-01.

Part: LANDING GEAR — CORRODED (RIGHT) · airframe 28,352 hrs · 32,939 cycles

RIGHT MLG LWR FLANGE ON AFT SURFACE AT FR 27 CORRODED. RT MLG LWR FLANGE ON AFT SURFACE AT FR 27, CORROSION REMOVED IAW SRM 51-21-42 FOUND WITHIN LIMITS OF SRM 51-10-10 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 28,352 hrs · 32,939 cycles

RIGHT MLG LWR ANGLE ON FWD SURFACE AT FR 27 BL 0 CORRODED. CORROSION REMOVED IAW SRM 51-21-42 FOUND WITHIN LIMIT OF SRM 51-10-10MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10.

Part: FLANGE — CORRODED (RT MLG) · airframe 28,352 hrs · 32,939 cycles

RIGHT MLG LWR FLANGE ON FWD SURFACE AT FR 27 CORRODED. CORROSION REMOVED IAW SRM 51-21-42 FOUND WITHIN LIMITS OF SRM 51-10-10 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 51-10-10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

RIGHT MLG ANGLE ON AFT SURFACE AT INTERCOSTAL FR 27 CRACKED. RT MLG ANGLE ON AFT SURFACE AT INTERCOSTAL FR 27 INSTALLED IAW SRM 51-25-01 FABRICATION COVER ON W/C 2000-167 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

TOP ANGLE CRACKED ON INTERCOSTAL (LT NLG AREA) AT FR 25.

Part: FRAME — CRACKED (LT WING BOX) · airframe 28,352 hrs · 32,939 cycles

LEFT WING BOX FRAME 28 CRACKED. REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A.

Part: FRAME — CRACKED (LT WING BOX) · airframe 28,352 hrs · 32,939 cycles

LEFT WING BOX FRAME 28A FACE PLATE FOUND CRACKED. REPLACED IAW SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.

Part: CREASE BEAM — NONE (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

RIGHT CREASE BEAM ZEE FLOOR CORRODED AT FLOORBEAM 40. FOUND WITHIN LIMITS.

Part: FLOORBEAM — NONE (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

FLOORBEAM 36 TOP SURFACE CORRODED. CORROSION REMOVED, FOUND WITHIN LIMITS.

Part: FRAME — CRACKED (WING BOX) · airframe 28,352 hrs · 32,939 cycles

RIGHT WING BOX FR 28 CRACKED. REPLACED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.

Part: SKIN — CRACKED (PAX DOOR) · airframe 28,352 hrs · 32,939 cycles

PAX DOOR INNER SKIN CRACKED TWO LOCATIONS AROUND NUT PLATE HOLES FWD TOP AREA.

Part: PLACARD — MISSING · airframe 28,352 hrs · 32,939 cycles

EXTERIOR AND INTERIOR PLACARD ON A/C IS MISSING OR DAMAGED. INSTALLED AS PER AMM 11-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

CORROSION FOUND ON LT INBOARD SEAT TRACK BETWEEN FR 13 TO FR 17. SEAT TRACK SPLICES IAW SRM 53-00-00 FIG 434 MATERIAL THICKNESS: 0.394 MATERIAL REMOVED: 0.040 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304.

Part: PLATE — CRACKED (WING BOX) · airframe 28,352 hrs · 32,939 cycles

RIGHT WING BOX FR 28A FACE PLATE CRACKED. REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.

Part: SHEAR TIE — CORRODED (LT WING SKIN) · airframe 28,352 hrs · 32,939 cycles

LEFT WING SKIN FLANGE FOR PANEL 521DT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND IAW SRM 51-25-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

CREASE BEAM CORRODED AT STR 14 BETWEEN FR 13+17. REPAIRED.

Part: BRACKET — CRACKED (WING BOX) · airframe 28,352 hrs · 32,939 cycles

WING BOX FR 24 L-BRACKET CRACKED 291BL.

Part: BRACKET — CRACKED (LT TE FLAP) · airframe 28,352 hrs · 32,939 cycles

LEFT INBOARD FLAP 2 OMEGA BRACKET CRACKED ON FLAP BEAM RIB 5.

Part: HINGE — BROKEN (EMERGENCY EXIT) · airframe 28,352 hrs · 32,939 cycles

FITTING HINGE (AFT) BROKEN ON RT EMERGENCY EXIT (RESOLVED ON W/O: 71093 TASKCARD: N/R-00253 ), FITTING HINGE ON RT EMERGENCY EXIT REPLACED AND INSTALLED IAW SRM 51-25-04. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-04, SUPPLEMENTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,352 hrs · 32,939 cycles

CORROSION FOUND ON RT SEAT TRACK BETWEEN FR 36 - 39.

Part: ANGLE — CRACKED (WING BOX) · airframe 28,352 hrs · 32,939 cycles

RIGHT WING BOX FR 28A ANGLE CRACKED.

Part: SHEAR TIE — CORRODED (LT WING) · airframe 28,352 hrs · 32,939 cycles

LEFT WING SKIN FLANGE FOR PANEL 522CT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND. INSTALLED SRM 51-25-01 FABRICATION COVER ON W/C 2000-206 MATERIAL THICKNESS: 0.753 MATERIAL REMOVED: 0.009 WITHIN LIMITS AS PER SRM: 57-14-12 FIG 301.

Part: WARNING LIGHT — ILLUMINATED · airframe 28,307 hrs · 32,894 cycles

FLAP UNLOCK LIGHT CAME ON DURING APPROACH. EMERGENCY DECLARED.

Part: SIGN — MISSING (CABIN) · airframe 28,082 hrs · 32,665 cycles

EMERGENCY EXIT SIGN MISSING INSIDE AIRCRAFT NEXT TO SERVICE DOOR.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 27,835 hrs · 32,436 cycles

EMERGENCYY EXIT SIGN MISSING THAT GOES TO THE LEFT OF THE SERVICE DOOR IS MISSING.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,021 hrs · 31,587 cycles

ON TAXI OUT, FIRST HALF OF EMERGENCY FLOOR TRACK LIGHTING WILL NOT EXTINGUISH, GATE RETURN. FLT 4582 DEL 180 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,872 hrs · 31,406 cycles

EMERGENCY LIGHT STRIP NEXT TO SEAT 8B FAILS TO OPERATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,872 hrs · 31,406 cycles

ASD EMERGENCY LIGHT INOP.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,682 hrs · 31,174 cycles

HEAVY ELECTRICAL BURNING SMELL IN THE COCKPIT / FWD CARGO AREA WHILE INFLIGHT AT 800. FLTS 4366, 4858 CX.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 26,349 hrs · 30,774 cycles

CABIN DOOR WILL NOT LOCK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,311 hrs · 30,724 cycles

ASD EMERGENCY LIGHT BULB INOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,937 hrs · 30,274 cycles

FLOOR EMERG LIGHT TRACK AFT LIGHT BULB INOP.

Part: LIGHT — INOPERATIVE (AIRSTAIRS) · airframe 25,916 hrs · 30,247 cycles

ASD LIGHT INOP

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,732 hrs · 30,006 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF, FLT 4088 DEL 66 MINS.

Part: LIGHT — NONE · airframe 25,433 hrs · 29,611 cycles

SOME EMERGENCY LIGHTS (FOWARD EXIT LIGHTS ABOVE FA STATION AND FLOOR LEVEL LIGHTING FROM FRONT TO ABOUT ROW7) ILLUMINATED WHEN EMERGENCY LIGHT SWITCH IS IN ARMED POSITION. FA INFORMED CREW THAT LIGHTS COME ON WHENEVER NR 2 ENGINE IS SPUN COMING OUT OF HOTEL MODE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT, NEAR THE REAR SERVICE DOOR WAS, FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE REAR SERVICE DOOR. OPERATIONAL CHECKS GOOD GOOD. AIRCRAFT OK FOR SERVICE

Part: LAMP — BURNED OUT (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY LIGHT, NEAR THE FLIGHT ATTENDANTS SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, NEAR THE FLIGHT ATTENDANTS SEAT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE ANGLE AT FS 39, BETWEEN STRINGER 21R-21L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE ANGLE AT FS 39, BETWEEN STRINGER 21R-21L, IAW SRM 51-21-42 AND REPLACED THE ANGLE AT FS 39, BETWEEN STRINGER 21R-21 IAW SRM 51-25-04. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SIDE `Z` FLOOR SUPPORTS, BETWEEN FS 39-40, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE `Z` FLOOR SUPPORT, BETWEEN FS 39-40, IAW ASA EO 72-53-0200, AND REMOVED AND REPLACED THE RIGHT SIDE `Z` FLOOR SUPPORT, BETWEEN FS 39-40, IAW ASA EO 72-53-0201. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE RIGHT SIDE CREASE BEAM, BETWEEN FS 39-40, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE CREASE BEAM, BETWEEN FS 39-40, IAW ASA EO 72-53-0195. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, FLOORBEAM 41, AT BL 0, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FLOORBEAM 41, AT BL 0, IAW ASA EO 72-53-0174. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE RIGHT SIDE DOUBLER, ON FRAME 39, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE DOUBLER, ON FRAME 39, IAW ASA EO 72-53-0194. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LEFT SIDE FLOOR SUPPORT, BETWEEN FS 36-38, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE LEFT SIDE FLOOR SUPPORT, BETWEEN FS 36-38, IAW SRM 51-25-01, AND REPLACED THE LEFT SIDE FLOOR SUPPORT, BETWEEN FS 36-38, IAW ASA EO 72-53-0187. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, FRAME FRAME 23A, AT STRINGER 21R AND STRINGER 21L, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE CORROSION ON FRAME FS 23A, AT STRINGER 21R AND STRINGER 21, IAW SRM 51-21-42. REPAIRED FRAME FS 23A, AT STRINGER 21R AND STRINGER 21L IAW ASA EO 72-53-0199. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C--CHECK IN YUL, THE FLOORBEAM AT FS 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 36, IAW ASA EO 72-53-0170. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE FLOORBEAM, AT FS 39, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED THE FLOORBEAM, AT FS 39, IAW SRM 51-25-01 AND REPLACED THE FLOORBEAM, AT FS 39, IAW ASA EO 72-53-0172.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 38, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM, AT FS 38, IAW ASA EO 72-53-0171. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM, AT FS 40, IAW ASA EO 72-53-0173. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FASTENER — MISSING (PASSENGER DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE REINSTALLED 2 FASTENERS (SCREWS) FOUND MISSING FROM THE PASSENGER DOOR COVER IN THE UPPER AFT CORNER. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SIGN — OUT OF POSITION (CABIN)

FLT 4709 - DURING A GROUND INSPECTION IN CSG, THE EMERGENCY EXIT SIGN BY THE SERVICE DOOR WAS FOUND MISSING. THE CREW FOUND THE EMERGENCY EXIT SIGN COVER UNDER THE SERVICE CART AND MAINTENANCE REINSTALLED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 22,651 hrs

DURING A GROUND INSPECTION, THE COCKPIT EMERGENCY LIGHT SWITCH FAILED. WHEN SELECTED TO THE ARM POSITION THE LIGHTS ARE ON AND WHEN SELECTED TO THE ON POSITION, THE SWITCH SPRINGS BACK TO THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IAW ATR 72-JIC 33-51-07. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: ACTUATOR — LEAKING (LT WING TE FLAP)

FLT 4145 - DURING CLIMB-OUT FROM VPS-ATL, AT APPROXIMATELY 6,000 TO 7,000 FEET THE CREW RECEIVED A LOW LEVEL MESSAGE ON THE BLUE HYDRAULIC SYSTEM. THE CREW FOLLOWED THE QRH AND SHUTOFF THE BLUE PUMPS. APPROXIMATELY FORTY MILES FROM ATL, A LOW LEVEL MESSAGE ON THE GREEN HYDRAULIC SYSTEM WAS RECEIVED. THE CREW FOLLOWED THE QUH AND SHUT OFF THE GREEN PUMP EXPERIENCING A TOTAL HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FLAP ACTUATOR. MAINTENANCE ALSO CYCLED THE FLAPS FIFTEEN TIMES WITHOUT ANY DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACTUATOR — LEAKING (LT WING TE FLAP)

DURING CLIMB-OUT, AT APPROXIMATELY 6,000 TO 7,000 FEET, THE CREW RECEIVED A LOW LEVEL MESSAGE ON THE BLUE HYDRAULIC SYSTEM. THE CREW FOLLOWED THE QRH AND SHUTOFF THE BLUE PUMPS. APPROXIMATELY FORTY MILES FROM AIRPORT, A LOW LEVEL MESSAGE ON THE GREEN HYDRAULIC SYSTEM WAS RECEIVED. THE CREW FOLLOWED THE QRH AND SHUT OFF THE GREEN PUMP EXPERIENCING A TOTAL HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND AC LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED LT IB FLAP ACTUATOR. ALSO, CYCLED THE FLAPS FIFTEEN TIMES WITHOUT ANY DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN VPS, THE AFT EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: NUT — INOPERATIVE (EMERGENCY LIGHT)

FLT 4197 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT BUTTON ON THE FLIGHT ATTENDANTS PANEL WAS FOUND STUCK IN THE ON POSITION. MAINTENANCE REINSTALLED THE LOCK NUT ON THE EMEGENCY LIGHT BUTTON SWITCH AT THE FLIGHT ATTENDANTS PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURNG AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CEHCKS GOOD. AIRCARFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (GALLEY)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — INOPERATIVE (EMERGENCY SIGN)

FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE AFT EMERGENCY EXIT SIGN AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES ON THE BACK OF THE AFT EMERGENCY EXIT SIGN ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (ROW 5)

DURING A HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT STRIP AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AND WIRING (P/N M22759/41-24-9) AT ROW FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE RIGHT FLOOR SUPPORT ZEE CHANNEL BETWEEN FRAME 39 TO 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SUPPORT ZEE CHANNEL BETWEEN FRAME 39 TO 41 IAW SRM 51-25-01. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, FLOOR SUPPORT TEE ANGLE AT THE SERVICE DOOR THRESHOLD BETWEEN FRAME 36 TO FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT TEE ANGLE AT THE SERVICE DOOR THRESHOLD BETWEEN FRAME 36 TO FRAME 38 IAW SRM 51-25-01. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE SERVICE DOOR THRESHOLD DOUBLER FORWARD OF FR 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR THRESHOLD DOUBLER FORWARD OF FRME 36 IAW SRM 51-25-02 AND 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FRAME 36 TO FRAME 39 AND THE RIGHT SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 36 TO FRAME 39 AND THE RIGHT SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 IAW SRM 51-25-04 AND 51-25-01. (M)

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURING A GROUND INSPECTION IN ATL, THE EMEGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COWLING — CRACKED (RT ENGINE)

DURING AN A-CHECK IN MCN, THE RIGHT ENGINE AFT OUTBOARD COWL BOTTOM CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ENGINE AFT OUTBOARD COWL BOTTOM CORNER IAW SRM 54-30-00. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN MCN, THE SECOND AND THIRD PASSENGER DOOR STEPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE SECOND AND THIRD PASSENGER DOOR STEPS IAW SRM 51-12-00. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4164 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

FLT 4295 - DURING GROUND INSPECTION IN ATL, THE AFT EMERGENCY LIGHT CAME ON INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: OIL CAP — MISSING (LT ENGINE)

DURING DECENT, THE LT ENGINE INDICATED A WARNING FOR LOW OIL PRESSURE. THE WARNING SHOWED LOW OIL PRESSURE ON THE CAP AND LOCAL ALERT, WITH AN OIL PRESSURE FLUCTUATION IN THE CAUTION AND WARNING AREAS. THE PILOT SHUT THE ENGINE DOWN IAW THE QRH CHECK LIST REQUIREMENTS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE ENGINE OIL CAP OFF AND THE ENGINE COVERED IN OIL. ENGINE WAS SERVICED WITH ELEVEN QUARTS OF OIL AND RAN AT 60 PERCENT TORQUE FOR FIVE MINUTES AND 35 PERCENT TORQUE FOR FIVE MINUTES. LEAK AND OPERATIONS CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING HANGAR MAINTENANCE IN MCN, A SECTION OF EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AT THE 61WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

FLT 4285 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE AT SEVERAL ROWS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLY AT POSITION 61WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — MAKING METAL (RIGHT)

FLT 4171 - DURING FLIGHT FROM ATL-GNV - PILOT RECEIVED AN INTERMITTENT OIL PRESSURE LIGHT . PILOT DECLARED AN EMERGENCY AND DIVERTED THE AIRCRAFT TO AYS. AIRCRAFT LANDED IN AYS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. THE NR 2 SCAVENGE OIL FILTER WAS FULL OF METAL. THE TEAR DOWN REPORT DID NOT REVEAL THE SOURCE OF THE METAL CONTAMINATION. THE DAMAGE TO THE NR 14 BEARING AND PROPELLER BRAKE COUPLING APPEARS TO BE SECONDARY MECHANICAL DAMAGE AND INDICATE THAT THE METAL FOUND ON THE CHIP DETECTOR MOST LIKELY ENTERED THE REDUCTION GEAR BOX AT THIS POINT WHERE THE MAJORITY OF MECHANICAL DAMAGE WAS FOUND. (M)

Part: ENGINE — FAILED (NR 2)

FLT 4171 - DURING FLIGHT FROM ATL-GNV, PILOT RECEIVED AN INTERMITTENT OIL PRESSURE LIGHT. PILOT DECLARED AN EMERGENCY AND DIVERTED THE AIRCRAFT TO AYS. AIRCRAFT LANDED IN AYS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. THE NR 2 SCAVENGE OIL FILTER WAS FULL OF METAL. THE CAUSE CANNOT BE DETERMINED UNTIL THE ENGINE IS TORN DOWN. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, MAINTENANCE FOUND EMERGENCY LIGHT ON PAX DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTING ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (AIR STAIR DOOR)

ON GROUND INSPECTION, CAPTAIN REPORTED AIR STAIR DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COMPUTER — INOPERATIVE (COCKPIT)

FLT 4031 - DURING FLIGHT FROM ATL TO PFN, THE MFC 1A SPOILER CIRCUIT BREAKER TRIPS AND THE FLAGS UNLOCK LIGHT CAME ON. CREW NOTICED SMOKE SMELL COMING FROM THE MFC. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE MFC AND RIGHT SIDE CAUTION SWITCH. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROP BRAKE — INOPERATIVE (NR 2 ENGINE)

FLT 4165 - CREW REPORTED AFTER NR 2 ENGINE START (IN HOTEL MODE), THE PROPELLER BRAKE SLIPPED. AFTER ATTEMPTING TO RE-ENGAGE BRAKE, ENGINE FIRE WARNING CAME ON WITH SMOKE INDICATIONS. CREW BLEW FIRE BOTTLES. RAMPER REPORTED VISIBLE FIRE FROM ENGINE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE PROPELLER BRAKE ASSY. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (FUSELAGE)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT OUTER CHORD AT STRINGER 17, BETWEEN FRAMES 35-40 CORRODED. RAI CHORD IAW ATR SRM 512502. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LEFT F/A'S SEAT TRACK CORRODED. RAI LEFT F/A'S SEAT TRACK IAW EO 72-53-0027. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT F/A'S SEAT TRACK CORRODED. RAI RT F/A'S SEAT TRACK IAW SRM 512504. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (CARGO BAY)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED AIRCRAFT CARGO 'Z' MEMBER CORRODED. INSTALLED NEW 'Z' MEMBER IAW ATR SRM 512503. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING SCHEDULED MAINTENANCE, FOUND SEAT TRACKS RIGHT CENTER AND RIGHT OUTER BETWEEN FRAMES 29 TO 36 UNSERVICEABLE DUE TO CORROSION. REMOVED AND REPLACED SEAT TRACKS IAW EO72-53-0029 AND SRMS 53-53-00, 51-21-17, 27, 31, 51-22-02 AND 51-25-01, 02 (M)

Part: STRINGER — CORRODED (FUSELAGE)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED AIRCRAFT RIGHT LOWER FUSELAGE STRINGER 18R IS CORRODED BETWEEN FRAME 34-35. REPAIRED STRINGER IAW ATR 72 SRM 530000 FIG 428. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BRACKET — CORRODED (DOOR SILL)

DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR SILL PLATE ANGLE ATTACH BRACKETS CORRODED AT FRAME 39. MANUFACTURED AND INSTALLED NEW FRAME CLEAT IAW ATR SRM 512401. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING SCHEDULED MAINTENANCE, FOUND SEAT TRACKS RIGHT CENTER AND RIGHT OUTER BETWEEN FRAMES 29 TO 36 UNSERVICEABLE DUE TO CORROSION. REMOVED AND REPLACED SEAT TRACKS IAW EO72-53-0029 AND SRMS 53-53-00, 51-21-17, 27, 31, 51-22-02 AND 51-25-01, 02 (M)

Part: PANEL — CORRODED (LT WING)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LEFT WING FEEDER TANK PANEL 522CT TO BE CORRODED. REPLACED PANEL 522CT IAW SRM 57000. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PANEL — CORRODED (RT WING)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT WING FEEDER TANK PANEL 622CT CORRODED. REPLACED PANEL 622CT AS REQUIRED IAW SRM 570000. AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER — CORRODED (BS 29/30)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED STRINGER 20 RT BETWEEN FRAMES 29 AND 30 AS CORRODED. REPAIRED STRINGER IAW SRM 530000 ATR 72. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AIRCRAFT OUTBOARD SEAT TRACK AT FLOORBEAM 36R AND FRAME 33 CORRODED. REPLACED SEAT TRACK BETWEEN FLOORBEAM AND FRAME 33 IAW ATR72 SRM 530027 AND EO 72-53-0029. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING SCHEDULED MAINTENANCE, FOUND CRACKED FLOORBEAM AT FRAME 26. INSPECTED FLOORBEAM IAW AI (R) FAX QS/ET603.4275/97, DS/ET603.4237/97 AND EO72-53-0026, SPECIFICATIONS FOR INSPECTION AT C-CHECK AND REINSPECTION EVERY 750 FLIGHTS. (M)