N500AS
Registered owner: PASTURE PILOT AGRO WORKS LLC, MO (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
20 reports on file, 1999-01-18 – 2002-03-14.
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, STRINGER 19 RIGHT WAS FOUND CORRODED BETWEEN FRAMES 13 AND 17. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-00 AND 51-40-02. (M)
Part: BUTT STRAP — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 21 AND 26. THE LEFT BUTT STRAP WAS ALSO FOUND WITH CORROSION BETWEEN FRAMES 21 AND 26 WITH IT ONLY BEING OUT OF LIMITS FROM FRAME 21 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE CORRODED RIGHT AND LEFT BUTT STRAPS IAW SRM'S 51-25-00, 51-14-02, AND 51-40-02. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION ON STRINGER 20 RIGHT BETWEEN FRAME 13 AND STATION 6653.1. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-22-00 AND 51-40-02. (M)
Part: CROSSBEAM — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, BOTH THE LEFT INBOARD AND RIGHT INBOARD CROSS FRAMES WERE FOUND CORRODED AT FRAME 16. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT AND LEFT CORRODED CROSS BEAMS IAW SRM 51-40-02. (M)
Part: STRINGER — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, STRINGER 18 LEFT WAS CORRODED BETWEEN FRAMES 13A AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE CABIN FLOOR CENTER OMEGA BEAM HAD CORROSION THAT WAS BLENDED OUT OF LIMITS AT FRAME 16. MAINTENANCE REPAIRED THE FLOOR CENTER OMEGA BEAM IAW ASA EO 120-53-0175. THIS EO REFERENCES EAC FAX GST-0894/02, DATED 18 MARCH 2002 AND SRM CHAPTER 51. AIRCRAFT OK FOR SERVICE. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, A SHEAR TIE WAS FOUND CORRODED AT FRAME 21 BETWEEN STRINGERS 19 AND 20 RIGHT AND ALSO BETWEEN STRINGERS 20 AND 21 RIGHT. MAINTENANCE REMOVED AND REPLACED THE CORRODED SHEAR TIE IAW SRM'S 51-25-00, 51-40-02, AND 51-40-05. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, BOTH THE LEFT INBOARD AND OUTBOARD SEAT TRACKS WERE FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 32. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM'S 51-20-01 AND 51-40-02 AND ALSO REFERENCING ASA EO120-25-0007C. (M)
Part: SILL — CORRODED (FUSELAGE)
DURNG C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT FLOOR SILL BETWEEN FRAMES 15 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED LEFT FLOOR SILL IAW SRM'S 51-25-00 AND 51-40-02. (M)
Part: BUTT STRAP — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 13 AND 16 AND ALSO BETWEEN FRAMES 18 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF THE CENTER BUTT STRAP IAW SRM'S 51-21-02, 51-25-00 AND 51-40-02. (M)
Part: CROSSBEAM — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION WAS FOUND ON THE RIGHT OUTBOARD CROSSBEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM'S 51-20-05, 51-40-04, AND 51-40-02. (M)
Part: SILL — CORRODED (FUSELAGE)
DURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SILL WAS CORRODED BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SILL IAW SRM'S 51-20-00 AND 51-40-02. (M)
Part: SEQUENCE VALVE — OUT OF ADJUST (LT MLG WW)
UPON TAKEOFF FROM TXK, THE CAPTAIN SELECTED THE LANDING GEAR HANDLE UP. THE RED A/B LIGHTS ON THE LEFT MAIN AND THE RED B LIGHT ON THE RIGHT MAIN GEAR WERE ILLUMINATED AND FAILED TO EXTINGUISH. THE TXK TOWER INFORMED THE CAPTAIN THAT THE LEFT MLG HAD FAILED TO RETRACT. THE CAPTAIN THEN ATTEMPTED TO RETRACT THE GEAR AGAIN BUT RECEIVED THE SAME RESULTS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO TXK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND ADJUSTED THE SEQUENCE VALVES ON THE LEFT MLG DOORS. MX ALSO INSPECTED THE LEFT AND RIGHT GEAR UPLOCK PROXIMITY SWITCHES AND FOUND THE RIGHT GEAR B UPLOCK PROXIMITY SWITCH OUT OF ADJUSTMENT. THE RIGHT GEAR B UPLOCK PROXIMITY SWITCH TARGET WERE ADJU
Earlier reports · 1999–2001 · 7 reports
2001
Part: ODOR — DETECTED (COCKPIT)
FLT 4751 - DURING FLIGHT FROM ROA TO ATL, CAPTAIN REPORTED WHEN WINDSHIELD HEAT IS TURNED ON IT CAUSES AN ELECTRICAL SMELL IN THE COCKPIT. WHEN WINDSHIELD HEAT IS TURNED OFF SMELL DISSIPATES. AIRCRAFT LANDED IN ATL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED WIRES AND CONTACTORS. SYSTEMS OPERATIONAL CHECKS GOOD. MAINTENANCE RAN BOTH THE CAPTAIN AND FIRST OFFICERS WINDSHIELD HEATING SYSTEMS FOR 25 MINUTES. OPERATIONAL CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ODOR — DETECTED (COCKPIT)
FLT 4388 - CRUISE FLIGHT FROM ROA TO ATL, AFTER TURNING ON WINDSHIELD HEAT, REPORTED AN ELECTRICAL SMELL IN THE COCKPIT. THE SMELL SEEMED TO GO AWAY WHEN THE WINDSHIELD HEAT WAS TURNED OFF. THE CAPTAIN AGAIN TURNED THE WINDSHIELD HEAT ON. A DEFINITE SMELL OF ELECTRIC SMOKE WAS COMING FROM THE OVERHEAD PANEL. THE CAPTAIN THEN TURNED OFF THE WINDSHIELD HEAT AND LEFT IT OFF. NO FURTHER SMELLS WERE NOTICED. A/C LANDED SAFELY IN ATL. MAINT DROPPED THE OVERHEAD PANEL AND INSPECTED THE WIRES AND SWITCHES. NO DEFECTS NOTED. MAINT RAN THE WINDSHIELD HEAT FOR APPROXIMATELY 10-15 MINUTES AND RECEIVED NO INDICATIONS OF SMOKE OR ELECTRICAL SMELLS. THE PANEL WAS RESECURED. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BRAKE — FAILED (RT MLG)
FLT 4066 - CREW REPORTED THE RIGHT MAIN LEFT INBOARD BRAKE LOCKED UP DURING TAXI OUT OF ATL. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LEFT INBOARD BRAKE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BULB — BURNED OUT (CABIN)
FLT 4817 - DURING GROUND INSPECTION IN DFW, ONE LIGHT BURNED OUT ON EMERGENCY EVACUATION LIGHTS. MAINTNANCE REMOVED AND REPLACED THE BURNED OUT BULB IN FRONT OF GALLEY AREA. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
2000
Part: STRINGER — CORRODED (FUSELAGE)
DURING INSPECTION, FOUND CORROSION IN FRAME 21 ON STRINGER 18. MAINTENANCE IS REPAIRING CORROSION FOLLOWING EO 120-53-0142 WHICH OUTLINES PROCEDURES FOR CORROSION REPAIR. (M)
Part: FITTING — BROKEN (LT MLG)
LEFT MAIN LANDING GEAR AFT OUTBOARD DOOR, AFT HINGE FITTING WAS FOUND BROKEN DURING C-CHECK INSPECTION. POSSIBLE CAUSE, FATIGUE. (X)
1999
Part: FAN — FAILED (RT PACK)
ON TAXI OUT, CREW ADVISED THAT THE RIGHT PACK FAILED AND REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE GATE AND DEBOARDED. ATL, MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK GROUND COOLING FAN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)