- Registered owner
- Corrigan Michael S
- Location
- Cedar Grove, TN
- Owner type
- Individual
- Serial number
- 6217
- Year built
- 2003
- Type
- Powered parachute
- Engine
- 2 cycle
- Airworthiness
- Experimental, registered before 01/31/08
- Airworthiness date
- December 22, 2007
- Certificate issued
- December 7, 2007
- Expires
- February 28, 2029
- Mode S code
- A6C7CD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N536MCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Buckeye DREAM MACHINE aircraft
FAA incident reports
No FAA accident or incident reports matched to N536MCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Buckeye DREAM MACHINE aircraft
Service difficulty reports
No reports matched to N536MCGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Buckeye DREAM MACHINE aircraft
Reports on N536MC not matched to an aircraft · 28
They name N536MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR UIEA200600181Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA. 273.09, PANEL 483AL, HAS A 0.750 INCH LONG CRACK AT UPPER FORWARD CORNER. ACCOMPLISHED SKIN PERMANENT REPAIR IAW SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.SDR UIEA200600179Brace · chafedNR 1 PYLON DIAGONAL BRACE HAS A CHAFED AREA ON OB SIDE ZONE 3A. ACCOMPLISHED BLENDOUT REPAIR AND FOUND WITHIN LIMITS IAW SRM 54-41-01 FIG. 3. PERFORMED FPI OF REWORKED AREA, NO DEFECTS FOUND IAW ASTM 1417-05. SHOT PEENED REWORKED AREA IAW SOPM 20-10-03. TREASDR UIEA200600182Skin · delaminatedLT WING UPPER SURFACE LEADING EDGE PANEL AT OLES STA. 1336.0 AND 1495.0 HAS 2 EACH SMALL AREAS OF DELAMINATION. AREAS ARE BOTH 2.0 INCH BY 2.0 INCH. ACCOMPLISHED PREPREG 250 DEGREE PERMANENT HOT BOND REPAIR SRM 51-40-12 AND SRM 51-40-09 FIG. 18. ALSO, REFEREN
See all 28 unmatched reportsSTCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.