N641AS

Part: PIN — BROKEN (ASD HANDLE) · airframe 28,533 hrs · 33,094 cycles

REF DEF 086935 ASD HANDLE HAS BROKEN PIN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,435 hrs · 32,988 cycles

FLT 4508 - EMERGENCY LIGHT ON CABIN DOOR NOT WORKING. DEL 225 MINS.

Part: DRAG BRACE — DAMAGED (NLG) · airframe 28,312 hrs · 32,864 cycles

NLG DRAG BRACE TO BE REPLACED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 28,312 hrs · 32,864 cycles

AFT INTERCOSTAL OF ROLLER STOP, PAX DOOR CRACKED. 10-9-07 ROLLER STOP OF PAX DOOR RAI FOM IAW AMM 20-21-12. AFT INTERCOSTAL OF ROLLER STOP REPLACED AS PER SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 51-25-01.

Part: STRUCTURE — CRACKED (SERVICE DOOR) · airframe 28,312 hrs · 32,864 cycles

SERVICE DOOR SURROUND 256DW CRACKED. REPAIRED AS PER CMM 25-00-01 SERVICE DOOR SURROUND 256DW PAINTED AS PER SRM 51-21-28.

Part: BRACKET — BROKEN (T/E FLAP) · airframe 28,312 hrs · 32,864 cycles

ON RIGHT WING O/B FLAP ARM AT RIB 13, 1 OMEGA BRACKET BROKEN OFF TO BE FABRICATED.

Part: BRACKET — BROKEN (LT I/B FLAP) · airframe 28,312 hrs · 32,864 cycles

LT I/B FLAP, O/B FLAP ARM (3) OMEGA BRACKETS BROKEN.

Part: STRUCTURE — CRACKED (SERVICE DOOR) · airframe 28,312 hrs · 32,864 cycles

SERVICE DOOR SURROUND 256EW CRACKED. REPAIRED AS PER CMM 25-00-01 SERVICE DOOR SURROUND 256EW PAINTED AS PER SRM 51-21-28

Part: SKIN — CORRODED (LT WING) · airframe 28,312 hrs · 32,864 cycles

LEFT WING FLANGE OF ACCESS 522CT CORRODED. 10-11-07 LT WING FLANGE 522 CT AREA, CORROSION REMOVED IAW SRM 57-14-12 FIG 401. FLANGE WITHING LIMITS (MATERIAL REMAINING), 0748 IAW SRM 57-14-12. HFEC PERFORMED BY HEATHAIR AMO 46-90 W/O 37536 IAW NTM NO CRACKS FOUND.

Part: INTERCOSTAL — CRACKED (WING BOX) · airframe 28,312 hrs · 32,864 cycles

WING BOX FR 23, JUNCTION WITH INTERCOSTAL, ANGLE CRACKED.

Part: SKIN — CORRODED (WING) · airframe 28,312 hrs · 32,864 cycles

FLANGE (ON WING) OF FWD PANEL 622CT CORRODED. 10-11-07 RT WING FLANGE, 622 CT AREA, CORROSION REMOVED IAW SRM 57-14-12 FIG 401. FLANGE WITHIN LIMITS (MATERIAL REMAINING 0.746") IAW SRM 57-14-12 FIG 301, HFEC PERFORMED IAW NTM, NO CRACKS FOUND. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 57-14-12 FIG 401. MATERIAL THICKNESS: 0.782 MATERIAL REMOVED: 0.036 WITHIN LIMITS AS PER SRM: 57-14-12 FIG 301.

Part: SKIN — CORRODED (LT WING) · airframe 28,312 hrs · 32,864 cycles

LEFT WING FLANGE OF ACCESS 521DT CORRODED. 10-11-07 LT WING FLANGE, 521 DT AREA, CORROSION REMOVED IAW SRM 57-14-12 FIG 401 FLANGE WITHIN LIMITS (MATERIAL REMAINING 0.762") IAW SRM 57-14-12 FIG 302 HFEC PERFORMED IAW NTM. NO CRACKS FOUND, REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 57-14-12 FIG 401. MATERIAL THICKNESS: 0.782 MATERIAL REMOVED: 0.030 WITHIN LIMITS AS PER SRM: 57-14-12 FIG 301.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

ETNRC - LT SEAT TRACK BETWEEN FR 36-38 CORRODED. CORROSION ON LT SEAT TRACK BTW FR 36-38 REMOVED IAW SRM 51-21-42 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: 0.043. MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

ETNRC - RT SEAT TRACK BETWEEN FR 36-38 CORRODED. CORROSION ON RT SEAT TRACK BTW FR 36-38 REMOVED IAW SRM 51-21-42 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: 0.043. MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

ETNRC - RT FLOOR SUPPORT CORRODED BETWEEN FR 39-41. CORROSION ON RT FLOOR SUPPORT REMOVED IAW SRM 51-21-42 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: 0.050. MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

ETNRC - FLOORBEAM 39 CORRODED. CORROSION ON FLOORBEAM 39 REMOVED IAW SRM 51-21-42 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: 0.071 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 305.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

ETNRC - RIGHT SEAT TRACK CORRODED BETWEEN FR 387-40. CORROSION ON RT SEAT TRACK BTW FR 38-40 REMOVED IAW SRM 51-21-425 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: 0.043. MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

RIGHT BELLY AFT SURFACE ON FR 27 NEAR STRINGER 14R FOUND CRACKED. 10-16-07 CRACK ON RT BELLY FR 27 REMOVED IAW DO/TS 4R1/07-9315 E/C PERFORMED ON CUTOUT BY HEATHAIR AMO 46-90 W/O 37536 IAW NTM NO CRACKS FOUND RT BELLY FR 27 REPAIRED IAW DO/TS 4191/07-9315 FABRICATION OF DOUBLER COVER ON W/C 2000-165 REPAIRED FAIRING FR 27 PER TC EO 72-53-0255.

Part: STRINGER CLIP — CORRODED · airframe 28,312 hrs · 32,864 cycles

ETNRC - LEFT STRINGER CLIP AT FR 38 AND STRINGER 21L FOUND CORRODED. CORROSION REMOVED ON LT STR CLIP AT FR 38 AND STR 21L IAW SRM 51-21-42. FABRICATION LT STR CLIP AT FR 38 AND STR 21L COVER W/C 2000-63. LT STR CLIP REPLACED IAW SRM 51-25-01 AND 51-25-03. 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: 0.013 WITHIN LIMITS AS PER SRM: OUT LIMITS AS PER SRM 53-61-00 FIG 301.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,312 hrs · 32,864 cycles

INSPECT & REPAIR OR REPLACE EMERGENCY LIGHTS TRACK IAW CMM AS REQ'D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

ETNRC - FLOORBEAM 38 CORRODED. CORROSION ON FLOORBEAM 38 REMOVED IAW SRM 51-21-42. 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: 0.071 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 305 .

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

FWD PRESSURE BULKHEAD AT LBL 10 LWR AREA, FITTING CORROSION FOUND (0.125 INCH) ON WEB.

Part: TRUSS — CRACKED (RT MLG) · airframe 28,312 hrs · 32,864 cycles

ETNRC - RIGHT MLG TRUSS CRACKED AT FR 26. 10-16-07 HFEC PERFORMED W/O 37536 END OF CRACKS MARKED ON MLG TRUSS. CUTOUT IN RT MLG TRUSS CARRIED OUT IAW DWG 15S535R0199 HFEC PERFORMED AROUND CUT-OUT W/O 37536 NO CRACKS FOUND. REPAIR PERFORMED PER SRM 51-24-04. REPAIRED CRACKS IN RT MLG TRUSS SHEAR MEMBER PER TC EO 72-53-0253 AND SRI DO/TS 4126-07-929.

Part: DOOR FRAME — CRACKED (BS 6250) · airframe 28,312 hrs · 32,864 cycles

CARGO DOOR ACTUATOR AFT FITTING FRAME CRACKED AT FS STA 7065. HFER PERFORMED BY HEATHAIR W/O 37536 CRACK CINFIRMED ON STA, CARGO DOOR FRAME STA 6250, REPAIRED IAW SRM 52-31-00 FIG 402.

Part: DOOR FRAME — CRACKED (BS 7141) · airframe 28,312 hrs · 32,864 cycles

CARGO DOOR FRAME AT STA 7141 CRACKED. 10-16-07 HFEC PERFORMED AND CRACK CONFIRMED. CARGO DOOR FRAME REPAIRED WITH DOUBLE IAW SRAS DO/TS-4166/07. REPAIRED INTERCOSTAL ON CARGO DOOR PER EC EO 72-52-0107.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 28,312 hrs · 32,864 cycles

CORROSION FOUND ON FWD PRESSURE WEB, LBL 10 TOP AREA. 10-9-07 CORROSION REMOVED IAW SRM 51-21-42 WEB OUT OF LIMITS IAW SRM 53-11-00 FIG 301. REPAIR CARRIED OUT IAW SRM 53-11-10 FIG 403 FABRICATION COVER ON W/C 2000-9 MATERIAL THICKNESS: 0.053 MATERIAL REMOVED: 0.018 OUT OF LIMITS AS PER SRM: 53-11-00 FIG 301.

Part: ANGLE — CRACKED (RT WING) · airframe 28,312 hrs · 32,864 cycles

RIGHT WING PRESSURE DECK ANGLE FR 27 CRACK FOUND IN Y AXIS. 10-16-07 HFEC PERFORMED W/O 37536. CRACK CONFIRM, DOES NOT EXTEND BEYOND FASTENER. PRC 870 APPLIED IAW SRI DO/TS-4165/07-9309 INSPECTED PRESSURE DECK ANGLE AND EXISTING CRACK PER TC EO 72-53-0254.

Part: DOOR FRAME — CRACKED (BS 6695) · airframe 28,312 hrs · 32,864 cycles

CARGO DOOR FRAME AT STA 6695.5 CRACKED. 10-16-07 HFEC PERFORMED BY HEATHAIR W/O 37536 CRACK CONFIRMED CARGO DOOR FRAME STA 6695.5 REPAIRED WITH DOUBLER IAW SRAS DO/TS-4166/07. REPAIRED INSTERCOSTAL ON CARGO DOOR PER EC EO 72-52-0107.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 28,312 hrs · 32,864 cycles

CARGO DOOR FRAME REPAIR CRACKED AT STA 6619.5. CRACK CONFIRMED, REPAIRED WITH DOUBLE. REPAIRED INTERCOSTAL ON CARGO DOOR PER EC EO 72-52-0107.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,709 hrs · 32,283 cycles

CAPTAIN'S FLASHLIGHT IS INOP.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 27,533 hrs · 32,083 cycles

EMERG LIGHTS COMING ON DURING FLIGHT INTERMITTENT WHEN LEFT IN ARMED POSITION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,426 hrs · 31,961 cycles

COPILOT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES IN COPILOT FLASHLIGHT AS REQUIRED. OPS CHECK GOOD AT THIS TIME.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 27,118 hrs · 31,599 cycles

DURING APPROACH AFTER SELECTING FLAPS 30 DEG RECEIVED FLAP UNLOCK WENT AROUND RAN QRH. EN ROUTE TO PEN A/C DIVERTED TO MGM. EMERGENCY DECLARED. FLT 4450 CX.

Part: HANDLE — BROKEN (SERVICE DOOR) · airframe 26,827 hrs · 31,247 cycles

RAMP REPORTS SERVICE DOOR T-HANDLE BROKEN. FLT 4193 DEL 236 MINS. SERVICE DOOR HOLD OPEN DEVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,903 hrs · 30,148 cycles

EMERGENCY LIGHT - LEFT SIDE FORWARD OUT. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,709 hrs · 29,873 cycles

ASD STEP LIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

DURING A GROUND INSPECTION, THE FIRST OFFICER’S FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SIGN — BROKEN (EMERGENCY EXIT)

DURING A GROUND INSPECTION, THE RT FORWARD EMERGENCY EXIT SIGN WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ENGINE — MALFUNCTIONED (RIGHT)

FLT 4086 - DURING DESCENT INTO ATL FROM AGS, AT APPROX 9,000 FEET THE CREW NOTICED THE RIGHT ENGINE TORQUE AT APPROX 20 PERCENT AND THE NP AT APPROX 35 PERCENT WITH ALL OTHER INDICATIONS SHOWING NORMAL WHICH WAS FOLLOWED BY A LARGE YAW TO THE RIGHT AND VIBRATIONS OCCURRED DURING THE OBSERVATION. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MCN, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE ELECTRONIC ENGINE CONTROL, HYDRO-MECHANICAL UNIT AND THE FUEL PUMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CORRODED (FS 48)

DURING A C-CHECK IN YUL, THE UPPER AND LOWER STATIC BASE DOUBLERS, AT FS 48 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE UPPER AND LOWER STATIC BASE DOUBLERS AT FS 48, IAW AMM 20-21-12. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE ANGLE BETWEEN THE TAIL BUMPER BOX AND FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE BETWEEN THE TAIL BUMPER BOX AND FS 39 IAW SRM 51-25-01. (M)

Part: RETAINER — CORRODED (SEAL)

DURING A C-CHECK IN YUL, THE SEAL RETAINERS, AT FS 45 AND FS 46, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAL RETAINERS, AT FS 45 AND FS 48, IAW SRM 51-21-42 AND AMM 20-21-12. (M)

Part: STANCHION — CRACKED (FUSELAGE)

DURING A C-CHECK IN YUL, THE LEFT STANCHION, AT FLOORBEAM 39, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT STANCHION, AT FS 39, IAW SRM 51-25-01. (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: FLOORBEAM — CORRODED (FUSELAGE)

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

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: FRAME — CORRODED (FS 39)

DURING A C-CHECK IN YUL, THE FS 39, AND STRINGER 14R, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 39, AT STRINGER 14R, IAW ASA EO 72-53-0185.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, FLOORBEAM AT FS 41, BETWEEN BL 0 TO RBL 26, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 41, BETWEEN BL 0 TO RBL 26, IAW ASA EO 72-53-0184. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE SEAT TRACK, BETWEEN FS 41-42, RBL 18 OUTBOARD, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED IAW ASA EO 72-53-0193. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 36, BETWEEN LBL 30 TO RBL 30, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 36, BETWEEN LBL 30 TO RBL 36 IAW ASA EO 72-53-0170. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE SEAT TRACKS, BETWEEN FRAME 36-40, AT RBL 8, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS, BETWEEN FS 36-39, IAW ASA EO 72-53-0190, AND REPLACED THE SEAT TRACKS BETWEEN FS 36-39 IAW ASA EO 72-53-0192. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE SEAT TRACKS, BETWEEN FRAME 36-41, AT LBL 4, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, BETWEEN FRAME 36-39 IAW ASA EO 72-53-0186 AND REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FS 39-41 IAW ASA EO 72-53-0191. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING A C-CHECK IN YUL, THE INTERCOSTAL BETWEEN FS 36-38, LBL 35 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL, BETWEEN FS 36-38 LBL 35, IAW ASA EO 72-53-0187. (M)

Part: COVER — BROKEN (EMERGENCY LIGHT)

FLT 4121 - DURING HANGAR MAINTENANCE IN ATL, THE LEFT EXIT LIGHT COVER WAS FOUND TO BE BROKEN. MAINTENANCE REPLACED THE LEFT EXIT LIGHT COVER. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACE — DAMAGED (LT MLG)

FLT 4089 - DURING APPROACH INTO ATL FROM AGS, UPON SELECTING GEAR DOWN, THE LEFT MAIN LANDING GEAR INDICATED UNSAFE ON BOTH LANDING GEAR PANELS. THE AIRCRAFT PERFORMED A GO AROUND TO COMPLY WITH THE QRH. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED. THE AIRCRAFT LANDED SAFELY IN AT. MAINTENANCE REMOVED AND REPLACED THE UPPER ARM ASSEMBLY ON THE SECONDARY BRACE OF THE LEFT MLG IAW ASA EO 72-32-0020A, PART C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BALLAST — DEFECTIVE (CABIN)

DURING A GROUND INSPECTION IN MGM, THE OVERHEAD EMERGENCY LIGHT AT ROWS 7 AND 11 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BALLAST AT STATION 61WL IAW ATR72 AMM 33-51-00. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HYDROMECH UNIT — MALFUNCTIONED (LT ENGINE)

DURING CRUISE, THE CREW NOTICED THE LT ENGINE ITT RISE IN EXCESS OF 800 DEGREES ITT AND REDUCED THE POWER ON THE ENGINE TO BRING IT WITHIN ITT LIMITS AT WHICH TIME THE ENGINE BEGAN TO SURGE. AN EMERGENCY WAS DECLARED AND JUST PRIOR TO THE CREW SHUTTING DOWN THE LT ENGINE, IT RETURNED TO NORMAL AND STOPPED SURGING. THE DECISION WAS MADE TO LEAVE THE LT ENGINE RUNNING AND CONTINUED. THE AIRCRAFT LANDED SAFELY. MAINT REMOVED AND REPLACED THE HYDROMECHANICAL UNIT AND THE FUEL PUMP ON THE LT ENGINE. OPS AND LEAK CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: ENGINE — MALFUNCTIONED (LEFT)

DURING CRUISE, THE CREW NOTICED LT ENGINE ITT RISE IN EXCESS OF 800 DEGREES ITT AND REDUCED THE POWER ON THE ENGINE TO BRING IT WITHIN ITT LIMITS AT WHICH TIME THE ENGINE BEGAN TO SURGE. AN EMERGENCY WAS DECLARED AND JUST PRIOR TO THE CREW SHUTTING DOWN THE LT ENGINE, IT RETURNED TO NORMAL AND STOPPED SURGING. THE DECISION WAS MADE TO LEAVE THE LT ENGINE RUNNING AND CONTINUED, AC LANDED SAFELY. MAINT PERFORMED ENGINE RUNS AT ALL POWER SETTINGS IAW MM. NO DEFECTS WERE NOTED. AC OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (PAX DOOR)

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

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS)

FLT 4724 - DURING APPROACH FROM ATL-MGM, THE CREW RECEIVED A FLIGHT CONTROL MASTER CAUTION MESSAGE ACCOMPANIED BY A FLAPS ASYMMETRY INDICATION. THE FLAPS WERE OBSERVED STUCK BETWEEN FIFTEEN TO THIRTY DEGREES ON THE FLAP INDICTOR THE CRW WAS UNABLE TO RAISE OR LOWER THE FLAPS AND COULD NOT DETERMINE IF THERE WAS ANY ASYMMETRY BY AIRCRAFT HANDLING OR USUAL MEANS. QRH PROCEDURES WERE COMPLIED AND AN EMERGENCY WAS DECLARED. THE CREW PERFORMED A FIFTEEN DEGREE LANDING PROCEDURE AND THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER AND THE FLAP CONTROL SWITCH UNIT (P/N 7048-1). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SWITCH — SHORTED (EMERGENCY LIGHT)

DURING FLIGHT FROM AGS-ATL, THE EMERGENCY EXIT LIGHTS ILLUMINATED IN THE ARMED POSITION AND EXTINGUISHED WHEN THE DISARMED POSITION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE LEFT AND RIGHT OUTBOARD SEAT TRACKS AND THE RIGHT INBOARD SEAT TRACK, BETWEEN FS 23-29 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SEAT TRACKS AND THE RIGHT INBOARD SEAT TRACK, BETWEEN FS 23-29 IAW SRM 51-25-01, 51-25-04 AND 53-00-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE RIGHT OUTBOARD SEAT TRACK SECTION BETWEEN FS 13-23 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK SECTION BETWEEN FS 13-23 IAW SRM 51-25-01 AND 51-25-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE LEFT AND RIGHT OUTBOARD SEAT TRACKS BETWEEN FS 29-36 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT OUTBOARD SEAT TRACKS BETWEEN FS 29-36 IAW SRM 51-25-01 AND 53-00-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FS 36-39 NEAR FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FS 36-39 IAW SRM 51-25-02. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE RIGHT SIDE WALL SILL PLATE BETWEEN FS 39-41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE WALL SILL PLATE BETWEEN FS 39-41 IAW SRM 51-25-02. (M)

Part: ANGLE — CORRODED (FUSELAGE)

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

Part: CROSSBEAM — CORRODED (FS 36)

DURING A C-CHECK IN BNA, THE CROSSBEAM AT FS 36 BETWEEN THE LEFT AND RIGHT SIDE WALLS WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CROSSBEAM AT FS 36 BETWEEN THE LEFT AND RIGHT SIDE WALLS IAW SRM 51-24-00 AND 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE RIGHT SEAT TRACKS BETWEEN FS 38-39 AND FS 39-40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT SEAT TRACKS BETWEEN FS 38-39 AND FS 39-40 IAW SRM 51-25-02. (M)

Part: SUPPORT BRACKET — CRACKED (MLG)

DURING HANGAR MAINTENANCE IN MCN, THE RIGHT MAIN LANDING GEAR UPSTOP UPPER SUPPORT BRACKET ON THE TOP SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPSTOP UPPER SUPPORT BRACKET IAW SRM 51-00. (M)

Part: ENGINE — MALFUNCTIONED (RIGHT)

DURING FINAL APPROACH FROM MGM-ATL, WHEN THE CREW PULLED THE POWER LEVERS BACK TO IDEL, THE FLIGHT ATTENDANTS NOTICED A STRONG SMOKE ODOR AND HAZE IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: VALVE — INOPERATIVE (ENGINE)

DURING DESCENT INTO ATL FROM VPS, SMOKE OCCURRED IN THE CABIN DURING OPERATION OF THE RT PACK. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE P2.5 TO P3 SWITCHING VALVE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

FLT 4308 - DURING FINAL APPROACH FROM ATL-PFN, THE FLIGHT ATTENDANT SMELLED AND OBSERVED SMOKE IN THE AFT CABIN SECTION. THE AIRCRAFT LANDED SAFELY IN PFN. MAINTENANCE GROUND RAN THE ENGINES OPERATING ALL RELATED SYSTEMS, BUT COULD NOT DUPLICATE THE SMOKE OR SMELL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CRACKED (PAX DOOR STEP)

DURING HANGAR MAINTENANCE IN MCN, THE FORWARD PASSENGER/CREW DOOR FIRST STEP SUPPORT DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE FORWARD PASSENGER/CREW DOOR FIRST STEP SUPPORT DOUBLER IAW ASA EO 72-52-0070. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PRESSURE SWITCH — INOPERATIVE (FAN)

DURING FINAL APPROACH FROM AVL-ATL, THE FLIGHT ATTENDANT NOTICED A MIST AND UNUSUAL SMELL IN THE CABIN. THE CREW ALSO NOTICED A FAINT OIL ODOR IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RT PACK TURBO FAN PRESSURE AND HEAR EXCHANGER OVERTEMP SWITCHES. OPERATIONAL CHECKS GOOD AND AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN MGM, THE CEILING EMERGENCY LIGHT AT ROW 14 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT LAMP AT ROW 14. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A HANGAR INSPECTION IN MCN, THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY LIGHT ABOVE HER SEAT FLICKERS INTERMITTENTLY DURING FLIGHT. THE PASSENGER DOOR EMERGENCY LIGHT WAS ALSO REPORTED INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLICKERING BULB FROM THE CEILING EMERGENCY LIGHT ASSEMBLY. MAINTENANCE ALSO REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE 62 WL POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON THE ENTIRE LENGTH OF THE TOP FLANGE, FROM LEFT TO RIGHT, UPPER AND LOWER SURFACES AT FRAMES 36, 38, 39, AND 40. MAINTENANCE REPAIRED THE CORROSION IAW ASA EO 72-53-0128. S/D THIS EO REF FAA FROM 8110-3, REPORT NR 02-019, WHICH INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, A CRACK WAS FOUND ON FRAME 26 AT THE BASE LINE. MAINTENANCE REPAIRED THE CRACK IAW ASA EO 72-53-0127. THIS EO REF SERVICE BULLETIN 72-53-1078 AND SRM CHAPTER 51. THIS EO ALSO INCLUDES REPAIR SPECIFICATIONS FOR FRAME 26 CRACK REPAIR FOR A/C. (M)

Part: ENGINE — FAILED (RIGHT)

FLT 4037 - AFTER TAKEOFF FROM ATL, THE RIGHT ENGINE QUIT PRODUCING POWER. THE TORQUE DROPPED SUDDENLY TO APPROXIMATELY 15-20 PERCENT AND FLUCTUATED BETWEEN 15-20 PERCENT. THE FLIGHT ATTENDANT REPORTED SEEING FRAMES. THE CAPTAIN SECURED THE ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. (M)

Part: BEARING — FAILED (RT ENGINE)

FLT 4037 - AFTER TAKEOFF FROM ATL, THE RIGHT ENGINE QUIT PRODUCING POWER. THE TORQUE DROPPED SUDDENLY TO APPROXIMATELY 15-20 PERCENT AND FLUCTUATED BETWEEN 15-20 PERCENT. THE FLIGHT ATTENDANT REPORTED SEEING FLAMES. THE CAPTAIN SECURED THE ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. TEAR DOWN REPORT REVEALED THE PRIMARY CAUSE OF THE DISCREPANCY WAS THE FAILURE OF THE NR 5 BEARING. (M)

Part: PUMP — LEAKING (EQUIPT BAY)

FLT 4288 - DURING FLIGHT FROM CHA TO ATL, THE BLUE HYDRAULIC SYSTEM FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLUE AC HYDRAULIC PUMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

FLT 4052 - DURING FLIGHT FROM CHA-ATL, TWO MINUTE LIGHT STAYS ON THE WHOLE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT IN ATL. MAINTENANCE INSPECTED BUT COULD NOT DUPLICATE THE DISCREPANCY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DEFECTIVE (CABIN)

CREW REPORTED THAT THE AFT EMERGENCY FLOOR TRACK LIGHTING REMAINS ON, AND ALSO WHEN THE EMERGENCY EXIT LIGHT IS ARMED. THE LIGHTS REMAIN ON WITH AIRCRAFT POWER ON. ATL MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING POWER SUPPLIES AT 62WL AND 73WL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED LEFT AFT F/A'S SEAT TRACK CORRODED. REPLACED LEFT AFT F/A SEAT TRACK IAW ASA EO 72-53-0030. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ZEE — CORRODED (CARGO BAY)

SAW - DURING 2C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT 'Z' MEMBER CORRODED. REPLACED 'Z' MEMBER IAW ATR72 SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED FLOORBEAM 39 HAS A HOLE AND CORROSION. REPAIRED FLOORBEAM 39 IAW ATR 72 SRM 53-00-00 FIG 429 AND ASA EO 72-53-0031. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AIRCRAFT OUTBOARD SEAT TRACK CORRODED. REPLACED RIGHT AFT OUTBOARD SEAT TRACK IAW ASA EO 72-53-0034. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (BS 38-39)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. FLOOR SUPPORT WAS REPLACED IAW SRM 512501. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FLOORBEAM 39 HAD HOLE AND CORROSION. BLENDED EDGE DAMAGE IAW SRM 51-10-00 AND HOLE IAW EO 72-53-003 SRM 53-00-00 FIG 429. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT SIDE OF FUSELAGE DENTED BETWEEN FRAMES 18 AND 19 AT STRINGER 16R. REPAIRED SKIN IAW SRM 53-31-24 AND EO 72-53-0033. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (BS 37)

SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FRAME 37 RIGHT TO BE CORRODED. FRAME 37 WAS REPAIRED IAW ATR 72 SRM 53-67-70 AND EO 72-53-0032. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CARGO BAY)

SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AFT CARGO SEAT TRACK CORRODED. RAI'D RIGHT AFT CARGO SEAT TRACK IAW ASA EO 72-53-0034. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED FORWARD LEFT OUTBOARD SEAT TRACK CORRODED. RAI'D SEAT TRACK IAW ATR72 SRM 51-25-04 AND ASA EO 72-53-0034. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AFT F/A'S SEAT TRACK CORRODED. REPLACED RIGHT AFT F/A SEAT TRACK IAW ASA EO 72-53-0030. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FAN — MALFUNCTIONED (COCKPIT)

ON DESCENT THROUGH 11,000 FEET ATL-MYR, THE CREW SMELLED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN. SHORTLY AFTER, THE LEFT RECIRCULATION FAN FAULTED AND WAS SELECTED OFF, WHICH CLEARED THE PROBLEM. FLIGHT LANDED SAFEY AT MYR WITH EMERGENCY EQUIPMENT STANDING BY. LOCAL MTC INSPECTED RECIRCULATION FAN AND AIRCRAFT AND FOUND NO ABNORMALITIES. FOUND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)

Part: DRAIN HOSE — CLOGGED (LT ENG)

FLT NR 8641 - ON APPROACH MCN-ATL, THE LEFT ENGINE FIRE WARNING ILLUMINATED AND THE LEFT ENGINE WAS IMMEDIATELY SHUT DOWN, FIRE HANDLE PULLED, AND AGENT 1 WAS DISCHARGED. THE FIRE WAS EXTINGUISHED AFTER APPROX 25 SECONDS. AN EMERGENCY WAS DECLARED AND FIRE EQUIPMENT REQUESTED. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT, EMERGENCY PERSONNEL CONFIRMED THAT THE FIRE WAS EXTINGUISHED. FOUND LEFT ENGINE FUEL DRAIN HOSE CLOGGED. REMOVED LINE, CLEANED AND REPLACED. AS AN ADDITIONAL PREVENTIVE MEASURE, CLEANED ALL DRAINS LINES ON BOTH ENGINES. REPLACED DAMGED COWLING. (M)