# N536MC: 2003 Buckeye DREAM MACHINE

- Status: Valid registration
- Airframe: [Buckeye DREAM MACHINE](https://openairdocs.org/model/buckeye-dream-machine) (registry code 05901BU, 2 seats)
- Engine: [Rotax 582SER](https://openairdocs.org/engine/rotax-582ser) (registry code 55556)
- Serial number: 6217
- Year built: 2003
- Type: Powered parachute
- Engine type: 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
- Registered owner: [Corrigan Michael S](https://openairdocs.org/faa-owner/CORRIGAN%20MICHAEL%20S)
- Location: [Cedar Grove, TN](https://openairdocs.org/faa-place/TN/Cedar%20Grove)
- Owner type: Individual
- Owner's area on the map: 35.8393° N, 88.5293° W: Placed by OpenAirDocs at the center of ZIP code 38321, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=536MC
- Page: https://openairdocs.org/aircraft/N536MC

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Buckeye DREAM MACHINE)

None in force.

### Matched by engine (Rotax 582SER)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N536MC.

## FAA accident and incident reports

None matched to N536MC.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty 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 UIEA200600181](https://openairdocs.org/sdr/UIEA200600181), Jul 20, 2006: SKIN. CRACKED. PYLON 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 5
- [SDR UIEA200600179](https://openairdocs.org/sdr/UIEA200600179), Jul 20, 2006: BRACE. CHAFED. NR 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 R
- [SDR UIEA200600182](https://openairdocs.org/sdr/UIEA200600182), Jul 20, 2006: SKIN. DELAMINATED. LT 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. ACCOMPLISHE
- [SDR UIEA200600180](https://openairdocs.org/sdr/UIEA200600180), Jul 20, 2006: SKIN. CRACKED. PYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA 281.34, PANEL 483AL, HAS A 1.0 INCH LONG CRACK AT LOWER AFT CORNER. ACCOMPLISHED SKIN AND INNER DOUBLER PERMANENT REPAI
- [SDR UIEA200600183](https://openairdocs.org/sdr/UIEA200600183), Jul 20, 2006: STIFFENER. CRACKED. NOSE WHEEL WELL, LT SIDEWALL STIFFENER BETWEEN FUSELAGE STATION 320 LT AND 340 LT, WL 180, WAS FOUND WITH CRACK DURING HFEC INSPECTION. REMOVED AND REPLACED STI
- [SDR UIEA200600119](https://openairdocs.org/sdr/UIEA200600119), May 23, 2006: COMPRESSOR. STALLED. ON TAKEOFF OUT OF DOV NR 2 ENGINE STALLED ABOUT 5 TIMES WITH REDUCTIONS IN N1, EGT AND N2. NO PARAMETERS WERE EXCEEDED. FLIGHT CONTINUED TO JFK WITHOUT SHUTDOWN
- [SDR UIEA200500079](https://openairdocs.org/sdr/UIEA200500079), May 24, 2005: SHEAR TIE. CRACKED. FRAME 440, RT SIDE BETWEEN STRINGERS 10A AND 11 TOP HOLE OF FRAME TO FUSELAGE SKIN ATTACHMENT ANGLE HAS .2500 INCH CRACK GOING UPWARD AND .0625 INCH CRACK GOING
- [SDR UIEA200500070](https://openairdocs.org/sdr/UIEA200500070), Apr 26, 2005: PAN. CRACKED. LT SIDE CANTED BULKHEAD AT BS 1245, LBL 60 CLOSURE PAN FOR AILERON CONTROL CABLE FEED THROUGH TO PRESSURE DECK FOUND WITH (2) CRACKED LINES. CLOSURE PAN REPAIRE
- [SDR UIEA200500069](https://openairdocs.org/sdr/UIEA200500069), Apr 26, 2005: SKIN. CRACKED. NR 1 PYLON LT ACCESS DOOR 452BL CUT OUT LOWER EDGE CRACKED. REPAIRED ACCOMPLISHED IAW MFG MM. (K)
- [SDR UIEA200500068](https://openairdocs.org/sdr/UIEA200500068), Apr 26, 2005: FRAME. CRACKED. NOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K)
- [SDR UIEA200500067](https://openairdocs.org/sdr/UIEA200500067), Apr 26, 2005: PRESSURE PANEL. CORRODED. BS 1408, LBL 78 WHEEL WELL PRESSURE DECK CORRODED AT FASTENERS LOCATIONS. PRESSURE DECK REPAIRED IAW MM. (K)
- [SDR UIEA200500066](https://openairdocs.org/sdr/UIEA200500066), Apr 26, 2005: PRECOOLER. CRACKED. PYLONS NR1, 2, 3, AND 4, PRECOOLER EXHAUST CUT OUT LOWER EDGE CRACKED. REPAIRS ACCOMPLISHED IAW MM. (K)
- [SDR UIEA200500065](https://openairdocs.org/sdr/UIEA200500065), Apr 26, 2005: PYLON. CRACKED. LT WING NR 1 PYLON STRUT DOOR 453BL UPPER CORNER CRACKED. (K)
- [SDR UIEA200500064](https://openairdocs.org/sdr/UIEA200500064), Apr 26, 2005: PYLON. CRACKED. NR 4 PYLON OB SKIN FOUND (2) CRACKS ON ACCESS DOOR 482AR CUTOUT CRACK 1INCH TO 1.5 INCH ON BOTH SKIN AND DOUBLER. (K)
- [SDR UIEA200500063](https://openairdocs.org/sdr/UIEA200500063), Apr 26, 2005: BULKHEAD. CRACKED. BS 400 BULKHEAD WEB CUT OUT FOR NOSE GEAR RETRACT ACTUATOR PAN FOUND BOTH LOWER CORNERS CRACKED. (K)
- [SDR UIEA200400205](https://openairdocs.org/sdr/UIEA200400205), Dec 27, 2004: FAIRING. MISSING. ON WALK AROUND CHECK, FOUND LT AFT TIP FAIRING OF HORIZONTAL STABILIZER MISSING. EO ISSUED TO ACCOMPLISH TIME-LIMITED REPAIR WORK TO BE DONE PRIOR TO FURTHER FL
- [SDR UIEA200400203](https://openairdocs.org/sdr/UIEA200400203), Dec 21, 2004: CONNECTOR. LOOSE. NR 4 LEADING EDGE FLAP WOULD NOT RETRACT OR EXTEND NORMALLY OR ELECTRICALLY. JETTISONED 60.0 K FUEL. FOUND FORWARD CONNECTOR LOOSE ON L/E DRIVE UNIT. RESECURED 
- [SDR UIEA200400150](https://openairdocs.org/sdr/UIEA200400150), Aug 24, 2004: SEAL. WORN. MXP-BOM - WITH NR 1 PACK ONLY ON OPERATION AT FL280 AND 310, CABIN ALTITUDE WILL CONTINUE TO CLIMB AT 10 TO 20 FPM. IN CRUISE WITH BOTH OUTFLOW VALVES FULL CLOS
- [SDR UIEA200400143](https://openairdocs.org/sdr/UIEA200400143), Aug 7, 2004: VALVE. MALFUNCTIONED. MXP-ALA - AT 1741Z ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS EXPERIENCED THE NR 4 ENGINE FIRE INDICATION. N1 SET AT 106.0. PERFORMED A REJECTED IAW THE FHB. ON
- [SDR UIEA200400122](https://openairdocs.org/sdr/UIEA200400122), Jul 12, 2004: VALVE. ERRATIC. NR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGING. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE D
- [SDR UIEA200400090](https://openairdocs.org/sdr/UIEA200400090), May 4, 2004: BLEED VALVE. MALFUNCTIONED. DURING CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. NR 2 ENGINE SUSTAINED 6 OR MORE HARD COMPRESSOR STALLS WHILE CLIMBING THROUGH 18,000 FT TO 24,000 FT. INSPECTE
- [SDR UIEA200400089](https://openairdocs.org/sdr/UIEA200400089), May 4, 2004: ENGINE. MALFUNCTIONED. PRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SET, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KN
- [SDR UIEA200400068](https://openairdocs.org/sdr/UIEA200400068), Apr 22, 2004: VALVE. INOPERATIVE. AZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BACK TO IDLE LIGHT WILL EXTINGUISH. BUT LI
- [SDR UIEA200400004](https://openairdocs.org/sdr/UIEA200400004), Jan 11, 2004: CLAMP. BROKEN. LEFT WING OVERHEATED TWICE ON CLIMB-OUT AND THEN IN CRUISE. COMPLETED CHECKLIST TO ISOLATE LEFT WING WITH ONLY NR 2 ENGINE PYLON VALVES OFF, AND ISOLATION VALVE
- [SDR UIEA200300072](https://openairdocs.org/sdr/UIEA200300072), Dec 29, 2003: CONTROL CABLE. ICED. NR 3 ENGINE THROTTLE UNABLE TO SELECT IDLE DURING DESCENT. THROTTLE STUCK AT 4 DEGREE THROTTLE ANGLE AND 80 PERCENT N1. ENGINE SHUTDOWN USING ENGINE FAILURE/SHU
- [SDR UIEA200300015](https://openairdocs.org/sdr/UIEA200300015), Mar 26, 2003: CLAMP. LOOSE. NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED & FIRE BELL ACTIVATED DURING CLIMB THROUGH 3000 FT. NR 1 ENGINE NACELLE TEMP INDICATES 'F' FOR BOTH 'A' AND 'B' LOOPS
- [SDR UIEA9921](https://openairdocs.org/sdr/UIEA9921), Apr 14, 1999: FIRE WARNING. ACTIVATED. FLT GT020 - FIRE WARNING BELL AND LIGHT SOUNDED ON FORWARD COCKPIT LIGHT FOR CARGO AREA, BUT WENT OUT TOO FAST TO CHECK F/E PANEL. CHECK CARGO AREA FIRE TEST AN
- [SDR UIEA9916](https://openairdocs.org/sdr/UIEA9916), Apr 5, 1999: FRAME. CORRODED. INSPECTION OF STA 1319 FRAME REVEALED CORROSION ABOVE THE LEFT HAND LONGERON BEAM. THE AREA WAS REPAIRED IAW ATLAS AIR EO 4753A085. (X)

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Buckeye DREAM MACHINE aircraft: https://openairdocs.org/model/buckeye-dream-machine/aircraft.md
- The Rotax 582SER engine: https://openairdocs.org/engine/rotax-582ser.md

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