N36MW

CIRRUS DESIGN CORP SR22T · 2024 · Valid Registration

Registered owner: M & A AIRCRAFT LLC, MT (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

O · 2016-06-28 Matched by certificate designator
ATA 4950

DURING MAINTENANCE INVESTIGATION OF REPORTED LOW APU BLEED AIR PRESSURE DURING ENGINE START CYCLE, A DISCREPANCY BETWEEN AFM REV 49 DATED 10 DEC 2012 AND AMM REV 26 DATED SEPT 2015 FOR APU BLEED AIR PRESSURES REQUIRED FOR ENGINE START WAS DISCOVERED. AMM ENGINE OPS TEST 71-00-00 REQUIRES 20 PSI MINIMUM FOR ENGINE START. AFM STARTING ENGINES PROCEDURES REQUIRE 25 PSI MINIMUM FOR ENGINE START. THIS DIFFERENCE CAUSES CONFLICT BETWEEN AIRCRAFT CREW AND MAINTENANCE FOR AIRCRAFT RETURN TO SERVICE. ASC 465C-APU, INSTALLATION OF 36-150G, HAS BEEN ACCOMPLISHED FOR ENHANCED PERFORMANCE OF APU AND BLEED AIR SYSTEM.

Source: SDR ZLWA20160926001 · FAA SDRS
K · 2011-06-05 Matched by certificate designator
ATA 2810

LEFT WING STARTED VENTING FUEL IN CLIMBOUT. AFTER TROUBLESHOOTING TECHNICIANS FOUND LEFT WING OUTBOARD AFT VENT FLOAT/ NON RELIEVING VALVE TO BE INOP. REPLACED VALVE WITH A NEW VALVE, P/N 16F123 AND SEAL, P/N GA215-160 IAW GULFSTREAM G-IV MAINTENANCE MANUAL 28-02-00 AND IPC 28-10-00. PERFORMED AIRCRAFT FUELING PROCEDURES IAW GULFSTREAM G-IV MAINTENANCE MANUAL 28-04-00. PERFORMED LEAK CHECK ON REMOVED WING ACCESS PANELS 21-FT16 AND 21-FT-17 WITH NO DISCREPANCIES. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR ZLWA20110608003 · FAA SDRS
N · 2003-09-23 Unresolved
ATA 3411

AC WAS ON TAKEOFF ROLL WHEN THE FLIGHT CREW NOTED A SUBSTANTIAL SPLIT BETWEEN AIRSPEED INDICATORS. AC WAS TAXIED BACK FOR TROUBLESHOOTING. PITOT/STATIC CHECKS WERE ACCOMPLISHED AND DISCREPANCY DUPLICATED. ALL PITOT AND STATIC LINES WERE DISCONNECTED AND NITROGEN WAS BLOWN INTO THE LINES. SEVERAL BUGS WERE REMOVED FROM THE LINES. ALL LINES WERE RECONNECTED AND PITOT/STATIC CHECKS RE ACCOMPLISHED AND ALL CHECKS NORMAL IAW MFG MM. (SW15200402394) (K)

Source: SDR ZLW2004F00000 · FAA SDRS
O · 2002-10-11 Matched by certificate designator
ATA 3040

WINDSHIELD HEAT CONTROLLER, INTERNAL FAILIURE.

Source: SDR ZLW2002F00000 · FAA SDRS
O · 2002-10-11 Matched by certificate designator
ATA 3040

CRACKED WINDSHIELD ON COPILOT SIDE. AFTER THE NEW WINDSHIELD WAS INSTALLED A FUNCTIONAL CHECK WAS PERFORMED AND IT WAS NOTED THAT THE WINDSHIELD STAYED FULL HOT. THE WINDSHIELD HEAT CONTROLLER WERE SWAPPED AND THE WINDSHIELD HEATED NORMALLY.

Source: SDR ZLW2002F00001 · FAA SDRS