N630AS

Part: VALVE — FAILED (BLEED SYS) · airframe 3,665 hrs · 3,115 cycles

MULTIPLE BLEED 1 FAIL CAS MESSAGES APPEARED IN FLIGHT.

Part: VALVE — FAILED (CABIN AIR) · airframe 3,512 hrs · 2,958 cycles

BLEED 2 FAIL CAS IN FLIGHT.

Part: VALVE — LEAKING (PARKING BRAKE) · airframe 3,239 hrs · 2,689 cycles

AFTER BRAKE RELEASE. PARK BRAKE LIGHT STAYS ON OR IS INTERMITTENT COMING ON. DURING BRAKE SET. PUMP IS CYCLING EXCESSIVELY.

Part: SCREW — LOOSE (WINDSHIELD) · airframe 2,020 hrs · 1,661 cycles

FOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 50% OF SCREWS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,204,804 hrs · 35,991 cycles

ASD EMERGENCY LIGHT INOP. REPLACED BULB IN ASD EMERGENCY LIGHT IAW AMM 33-51-24. OPS CK GOOD. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,801 hrs · 35,741 cycles

F/A REPORTS EMERGENCY LIGHT ON MAIN CABIN DOOR IS INOP.

Part: ANGLE — CRACKED (WHEEL WELL) · airframe 31,544 hrs · 35,470 cycles

FWD WHEEL WELL, ANGLE CRACKED AT FR 7 STR LEFT 20.

Part: ANGLE — CRACKED (LT WING) · airframe 31,544 hrs · 35,470 cycles

LEFT ON TOP WING BOX AT FR 23D AND RIB 2 ANGLE OF FR FOUND CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,544 hrs · 35,470 cycles

ANGLE CRACKED AT FR 26 STRINGER 4R (INTERNAL FUSELAGE). REMOVED AS PER SRM 51-25-01. RT SHEAR WEB BTW FR 25 & 27 REMOVED IAW AMM 20-21-12. ANGLE AT FR 26 STR 4 RT INSTALLED AS PER SRM 51-25-01. RT SHEAR WEB RE-INSTALLED IAW TECH INSTRUCTION 57-01-91.

Part: STRUCTURE — CRACKED (WING) · airframe 31,544 hrs · 35,470 cycles

ON TOP WING BOX AT RT SIDE BETWEEN FR 25 23D SUPPORT TUBULAR FOUND CRACKED.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 31,544 hrs · 35,470 cycles

LEFT ON TOP WING BOX AT FR 23D AND RIB 1, ANGLE OF INTERCOSTAL FOUND CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,544 hrs · 35,470 cycles

ANGLE CRACKED AT FR 26 STRINGER 4L (INTERNAL FUSELAGE). ANGLE AT FR 26 STR 4 LT REMOVED AS PER SRM 51-25-01. LT SHEAR WEB BTW FR 25 & 27 REMOVED IAW AMM 20-21-12. ANGLE AT FR 26 STR 4 LT INSTALLED AS PER SRM 51-25-01. LT SHEAR WEB RE-INSTALLED IAW TECH INSTRUCTION 57-01-91.

Part: ANGLE — CRACKED (RT WING) · airframe 31,544 hrs · 35,470 cycles

RIGHT ON TOP WINGBOX FWD FR 23D AND RIB 3 ANGLE FOUND CRACKED.

Part: LIGHT — BROKEN (CABIN) · airframe 31,379 hrs · 35,303 cycles

F/A REPORTS TRACK LIGHTING AT 8AB BROKEN.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 31,354 hrs · 35,276 cycles

FLAP UNLOCK ON APPROACH. EMERGENCY DECLARED. FLTS 4415, 4821 CX.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,868 hrs · 34,785 cycles

EMERGENCY EXIT SIGN BY PAX DOOR IS INOP.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,761 hrs · 34,675 cycles

AFT LOWER EMERGENCY EXIT SIGN BY PAX DOOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,656 hrs · 34,574 cycles

SEVERAL CABIN EMERGENCY LIGHTS INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,205 hrs · 34,089 cycles

AFT F/A'S FLASHLIGHT IS INOP.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,903 hrs · 33,729 cycles

EMERGENCY FLOOR LIGHTS WILL NOT EXTINGUISH.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 29,397 hrs · 33,127 cycles

ETNRC 2000-91, CARGO FLOOR DOUBLER (PANEL) CRACKED 261GF.

Part: PANEL — CRACKED (FUSELAGE) · airframe 29,397 hrs · 33,127 cycles

CRACK FOUND ON CROWN PANEL TAB AT FRAME 28.

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,397 hrs · 33,127 cycles

ETNRC 100-26//CORROSION FOUND ON FR 39 RT NEAR STR GR 14.

Part: BRACKET — BROKEN (LT WING) · airframe 29,397 hrs · 33,127 cycles

FOUND OMEGA BRACKET BROKEN ON LT WING FLAP BEAM AT RIB 8. OMEGA BRACKET ON RIB 8 RT WING FABRICATED AS PER SRM 57-52-20 AND REPLACED IAW SRM 51-25-01 . REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SF 663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW WITH SRM 57-52-20. (CLOSED)

Part: ANGLE — CRACKED (WING) · airframe 29,397 hrs · 33,127 cycles

RIGHT BENT ANGLE AT WING RIB 4 FR 28 UPPER FUSELAGE CRACKED. RT BENT ANGLE AT WING RIB 4 FRM 28 REPLACED IAW SRM 51-25-01. REPAIRE DETERMONED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A REPAIRE ACCOMPLISHED IAW SRM 51-25-01. (CLOSED 10/31/06)

Part: BRACKET — BROKEN (LT WING) · airframe 29,397 hrs · 33,127 cycles

LT WING RIB 13 OMEGA BRACKET BROKEN AT LOWER PART I/B AND 1 AT UPPER PART O/B.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,397 hrs · 33,127 cycles

CORROSION FOUND ON ANGLE ON FS 37 AT S14R.

Part: ANGLE — CRACKED (WING) · airframe 29,397 hrs · 33,127 cycles

LEFT BENT ANGLES AT WING RIB 4 FR 28 UPPER FUSELAGE CRACKED (2 PIECES). LT BENT ANGLE AT WING RIB 4 FR 28 UPPER FUSELAGE FABRICATED IAW SRM 53-91-42 AND INSTALLED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A REPAIR ACCOMPLISHED IAW SRM 51-25-01 (CLOSED 10/31/06)

Part: FRAME — CORRODED (FUSELAGE) · airframe 29,397 hrs · 33,127 cycles

ETNRC 100-21// DOUBLER OF FRAME 39 RT SIDE BETWEEN STRG 12 AND 16, CORRODED. CORROSION REMOVED ON DOUBLER OF FRM 39 RH IAW SRM 51-21-42. NEW FRAME DOUBLER INSTALLED IAW SRM 51-25-01 MATERIAL THICKNIESS0.090 MATERIAL REMOVED 0.030 OUT OF LIMITS AS PER SRM 53-61-00 . REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SF 663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW WITH SRM 51-25-01. CLOSED

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,397 hrs · 33,127 cycles

FOUND CORROSION ON DOUBLER ON STRINGER 4 RT AFT OF PRESS BULKHEAD (FS 44) IN AFT AV COMPARTMENT. CORROSION ON OUBLER OF STRG 4 RH AFT OF PRESS BULKHEAD REMOVED AS PER SRM 51-21-42 AND FOUND WITHIN LIMITS IAW SRM 53-81-00. MATERIAL THICKNIESS0.040 MATERIAL REMOVED 0.003 WITHIN LIMITS AS PER SRM 53-81-00 . REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SF 663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW WITH SRM 51-21-42. (CLOSED)

Part: DOOR — STIFF (EMERGENCY EXIT) · airframe 29,397 hrs · 33,127 cycles

FOUND LT EMERGENCY EXIT HARD TO OPEN.

Part: DOOR — CORRODED (E/E BAY) · airframe 29,397 hrs · 33,127 cycles

AFT AVIONICS COMPARTMENT DOOR CORRODED. CORROSION ON AFT AVIONICS COMPARTMENT DOOR REMOVED AS PER SRM 51-21-42 AND FOUND WITH IN LIMITS IAW SRM 52-81-00. MATERIAL THICKNIESS0.063 MATERIAL REMOVED0.004 WITHIN LIMITS AS PER SRM 52-81-00 . REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SF 663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW WITH SRM 51-21-42 (CLOSED 11/02/06)

Part: COVER — DAMAGED (CABIN) · airframe 29,181 hrs · 32,865 cycles

EMERGENCY LIGHTING COVER DAMAGED AT 8A/B (EXIT LIGHT).

Part: LIGHT — INOPERATIVE (AIR STAIR DOOR) · airframe 28,753 hrs · 32,351 cycles

ASD EMERGENCY LIGHT INOP. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,718 hrs · 32,301 cycles

CAPT'S FLASHLIGHT INOP.

Part: LAMP — INOPERATIVE (CABIN)

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

Part: FLASHLIGHT — INOPERATIVE (CABIN)

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

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4223 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY FLOOR TRACK LIGHT, NEAR SEAT 4B, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLOOR TRACK LIGHT, NEAR SEAT 4B, AND RECONNECTED THE CANNON PLUG. (M)

Part: CARBON SEAL — WORN (NR 2 ENGINE)

DURING CRUISE, A FUEL SMELL WAS REPORTED AROUND ROWS 2-5, AND REMAINED THE ENTIRE FLIGHT. THE AIRCRAFT LANDED SAFELY. MAINT REMOVED AND REPLACED THE NR 2 ENGINE STARTER GEAR BOX CARBON SEAL. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHT STRIP JUST FORWARD OF SEAT 14D WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLOOR LIGHT STRIP JUST FORWARD OF SEAT 14D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COVER — WORN (EMERGENCY LIGHT)

FLT 4094 - DURING A GROUND INSPECTION IN ATL, THE EXIT SIGN BY THE RIGHT FRONT EMERGENCY DOOR COULD NOT BE READ. MAINTENANCE REMOVED AND REPLACED THE COVER ON THE EXIT SIGN BY THE RIGHT FRONT EMERGENCY DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4239 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE EMERGENCY EXIT LIGHT OVER THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING AN A-CHECK IN MCN, THE EMERGENCY FLOOR LIGHT TRACK AT ROW 15B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 15B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, THE ANGLE AT FS 28 WING TO FUSELAGE ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE AT FS 28 WING TO FUSELAGE ON THE RT SIDE IAW SRM 51-25-01.

Part: BRACKET — CRACKED (T/E FLAP) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, THE OMEGA BRACKET ON THE RT IB FLAP, OB ARM WAS FOUND TO BE CRACKED BEYOND LIMITS.

Part: BRACKET — CRACKED (T/E FLAP) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, THE BRACKET AT THE LEFT FLAP BEAM ACTUATOR (IB FLAP) WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT THE LT FLAP BEAM ACTUATOR (IB FLAP) IAW SRM 51-25-02 AND 51-25-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE ZEE FLOOR SUPPORT BETWEEN FRAMES 39R AND 40R AT STRINGER 16R. MAINTENANCE REMOVED AND REPLACED THE CORRODED Z-ANGLE IAW SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, ON THE RT SEAT TRACK BETWEEN FRAMES 38 AND 39 CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON FLOORBEAM 39 IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, THE TOP FLANGES OF FLOORBEAMS 38 AND 40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM TOP FLANGES IAW 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, THE LT IB SEAT TRACK, CROWN AND FLANGE, BETWEEN FRAMES 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-25-04 AND 51-21-42.

Part: DOUBLER — CORRODED (HANDRAIL FITTING)

DURING C-CHECK INSPECTION, THE UPPER DOUBLER OF THE HANDRAIL FITTING ON THE LT THRESHOLD BETWEEN FS 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED DOUBLER IAW WITH SRM 51-21-42 AND 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING A C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON A FLOORBEAM 36. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01.

Part: DOUBLER — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON PL DOUBLER (GUSSET) BETWEEN LT HAND STRINGER 20 AND 21 AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE CORRODED DOUBLER (SUSSET) IAW SRM 51-21-42 AND 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, THE UPPER FLANGE OF FLOORBEAM 41 BETWEEN STRINGERS 17R AND 21R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORODED FLOORBEAM IAW SRM 51-25-01.

Part: HOUSING — CORRODED (RT WING) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE FLANGE HOUSING AT 522CT. MAINTENANCE REPAIRED THE CORRODED FLANGE HOUSING ON THE RT WING IAW SRM 57-14-12.

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, SEVERAL PLACES ON THE LT SEAT TRACK BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF SEAT TRACK IAW SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, THE RT SEAT TRACK BETWEEN FRAMES 39 AND 40 WERE FOUND TO BE CORRODED BEYOND LIMITS IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT IAW SRM 51-25-04.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE RT INTERCOSTAL BETWEEN FRAMES 36 AND 38 AT STRINGER 16R AND ALSO ON THE LT INTERCOSTAL BETWEEN FRAMES 38 AND 39 AT STRINGER 16L. MAINTENANCE REMOVED AND REPLACED THE CORRODED INTERCOSTALS IAW SRM 51-25-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 25,745 hrs

DURING C-CHECK INSPECTION, THE LT END OF THE FAIL SAFE ANGLE ON FR 36 WAS FOUND TO BE CORRODED AND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT OF THE FAIL SAFE ANGLE ON FR 36 IAW SRM 53-00-00, FIG 417.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION, THE T-FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 WAS FOUND TO BE CORRODED BEYOND LIMITS AT THE LT STR 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED T-FLOOR SUPPORT IAW SRM 51-25-01.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING A GROUNG INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND ILLUMINATING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE TO THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING PRE-FLIGHT CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. UPON COMPLETION OF THE PRE-FLIGHT CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR ILLUMINATED. MAINT INSPECTED THE EMERGENCY LIGHTS SYSTEM INCLUDING THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT AT ROW 16 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 16. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE FLOOR EMERGENCY EXIT FLOOD LIGHT LENS AT THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY EXIT FLOOD LIGHT LENS AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LENS — MISSING (CABIN CEILING)

FLT 4268 - DURING A GROUND INSPECTION IN ATL, THE EXTERIOR EXIT LIGHT AT THE REAR SERVICE DOOR WAS MISSING THE COVER. MAINTENANCE REPLACED THE MISSING EXIT LIGHT COVER. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

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

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4183 - 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: LAMP — BURNED OUT (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: STRINGER — CRACKED (FUSELAGE)

DURING A GROUND INSPECTION IN AVL, THE FORWARD CARGO DOOR HINGE POINT STRINGER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD CARGO DOOR HINGE POINT STRINGER IAW SRM 52-31-00 AND 51-25-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE AFT RIGHT SEAT TRACK FROM FS 36-39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT SEAT TRACK FROM FS 36-39 IAW SRM 51-25-04. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE RIGHT AFT SILL WEB FROM FS 39-41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT SILL WEB FROM FS 39-41 IAW SRM 51-25-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN BNA, THE AFT CENTER SEAT TRACK FROM FS 39-41 IAW SRM 51-25-04. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, PASSENGER DOOR STEP SUPPORT FRAME AT THE CENTER OUTBOARD NUT PLATE ON THE FIRST AND FOURTH STEPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR STEP SUPPORT FRAME AT THE CENTER OUTBOARD NUT PLATE ON THE FIRST AND FOURTH STEPS IAW SRM 51-25-01. (M)

Part: NUT PLATE — CORRODED (DOOR STAIR)

DURING A C-CHECK IN BNA, THE PASSENGER DOOR OUTBOARD CENTER AND FORWARD NUTPLATE ON THE FIRST AND FOURTH STEPS, THE OUTBOARD CENTER AND INBOARD AFT NUT PLATE ON THE SECOND AND THIRD STEPS, AND THE OUTBOARD AFT NUT PLATE ON THE FOURTH STEP WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR OUTBOARD CENTER AND FORWARD NUT PLATE ON THE FIRST AND FOURTH STEPS, THE OUTBOARD CENTER AND INBOARD AFT NUT PLATE ON THE SECOND AND THIRD STEPS, AND THE OUTBOARD AFT NUT PLATE ON THE FOURTH STEP IAW ASA EO 72-52-0030. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: FIREWALL — CRACKED (LT NACELLE)

DURING HANGER MAINTENANCE IN MCN, THE LEFT NACELLE UPPER FIREWALL WAS FOUND TO BE CRACKED WITH MATERIAL FALLING OUT. MAINTENANCE REPAIRED THE CRACKED NACELLE FIREWALL BY INSTALLING A DOUBLER IAW SRM.

Part: SMOKE — DETECTED (COCKPIT)

FLT 4121 - DURING CLIMB-OUT FROM ATL-CSG, AT APPROXIMATELY 3,000 FT, THE CREW SMELLED SMOKE WITH NO VISIBLE SIGNS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MX REMOVED, INSPECTED AND RE-INSTALLED THE SMOKE DETECTOR IN THE ELECTRONICS RACK, INCLUDING INSPECTION OF THE DUCTS AND RELAY SHELVES WITH NO DEFECTS NOTED. MAINTENANCE ALSO PERFORMED TWO THIRTY MINUTE ENGINE RUNS WITH NO ELECTRICAL SMOKE MESSAGES OCCURRING ON THE CREW ALERT PANEL. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (PAX DOOR)

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

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING GROUND INSPECTION IN ATL, THE FIRST FEW EMERGENCY LIGHTS STAYED ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY AT THE 43WL POSITION. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND AT FRAMES 36, 38, 39, 40, AND 41. CORROSION WAS ALSO FOUND ON THE FORWARD RADAR ALTIMETER CUTOUT BETWEEN FRAMES 15 AND 16. MAINTENANCE REPAIRED CORROSION TO THE FUSELAGE IAW ASA EO 72-53-0114. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR AIRCRAFT CORROSION. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND AT FRAMES 36, 38, 39, 40 AND 41. CORROSION WAS ALSO FOUND ON THE FORWARD RADAR ALTIMETER CUT OUT BETWEEN FRAMES 15 AND 16. THIS AIRCRAFT IS STILL IN C-CHECK. ASA ENGINEERING IS CURRENTLY WRITING AN EO. (M)

Part: VALVE — INOPERATIVE (RT ENGINE)

FLT 4100 - ON THE GROUND WHILE IN HOTEL MODE FOR A FLIGHT FROM ATL TO TRI, CREW EXPERIENCED SMOKE IN THE CABIN. MAINTENANCE FOUND THE RIGHT ENGINE EMITTING OIL OUT OF THE CASE VENT DRAIN. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE 2.5 SWITCHING VALVE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: RECEPTACLE — SHORTED (GROUND POWER)

FLT 4100 - CREW REPORTED THAT WHEN THE GROUND POWER UNIT WAS CONNECTED TO THE AIRCRAFT THAT SPARKS SHOT OUT FROM AROUND THE PLUG AND THE COCKPIT FILLED UP WITH SMOKE. SMOKE CLEARED AFTER GPU WAS DISCONNECTED. MAINTENANCE FOUND THE BACK SIDE OF THE GROUND POWER BOX DAMAGED. MAINTNANCE REPAIRED THE GROUND POWER BOX USING SRM 53-11-28. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER PACK — DEFECTIVE (CABIN)

CREW REPORTED THAT SOME EMERGENCY LIGHTS STAYED ON WHEN SYSTEM WAS SELECTED OFF. LOCAL MECHANIC INSPECTED AIRCRAFT AND FOUND SAFE FOR A FERRY FLIGHT TO ATL. ATL MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHTING POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)

Part: DOOR — DAMAGED (NLG)

FLT 7138 - DURING TAKEOFF VPS-ATL, THERE WAS A LOUD NOISE HEARD CONCURRENT WITH A ONE-TIMER SHUDDER. CAPTAIN LEFT THE GEAR DOWN AND FLEW BY THE TOWER, WHICH REPORTED NO APPARENT DAMAGE. CREW ELECTED TO CONTINUE TO ATL AND DECLARED AND PRECAUTIONARY EMERGENCY. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. INSPECTED ALL LANDING GEAR AND GEAR DOORS. NOTED DAMAGE TO THE LEFT NOSE GEAR DOOR. DOOR WAS REMOVED, SENT TO MCN FOR REPAIR AND REINSTALLED AFTER REPAIR. A TEST FLIGHT WAS PERFORMED (INCLUDED THREE GEAR CYCLES) AND AIRCRAFT WAS FOUND TO BE SATISFACTORY FOR CONTINUED SERVICE. (M)