# N575D: 2002 Callahan Robert R PROG AERODN SEAREY

- Status: Valid registration
- Airframe: [Callahan Robert R PROG AERODN SEAREY](https://openairdocs.org/model/callahan-robert-r-prog-aerodn-searey) (registry code 05614M1, 2 seats)
- Engine: [Bombardier ROTAX (ALL)](https://openairdocs.org/engine/bombardier-rotax-all) (registry code 09050)
- Serial number: 1MK270C
- Year built: 2002
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Kit: Progressive Aerodyne Inc SEAREY
- Airworthiness: Experimental, amateur built
- Airworthiness date: September 6, 2002
- Certificate issued: August 15, 2017
- Expires: August 31, 2027
- Mode S code: A76147
- Registered owners: [Singdahlsen Krynn](https://openairdocs.org/faa-owner/SINGDAHLSEN%20KRYNN), [Mitchell Bruce](https://openairdocs.org/faa-owner/MITCHELL%20BRUCE)
- Location: [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks)
- Owner type: Co-owned
- Owner's area on the map: 64.8378° N, 147.7164° W: Placed by OpenAirDocs: center of Fairbanks, AK, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=575D
- Page: https://openairdocs.org/aircraft/N575D

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 (Callahan Robert R PROG AERODN SEAREY)

None in force.

### Matched by engine (Bombardier ROTAX (ALL))

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N575D.

## NTSB investigations on N575D not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC01FA011](https://openairdocs.org/ntsb/ANC01FA011), Oct 22, 2000: Beech 1900D (N575D), Bethel, AK, substantial damage. Probable cause: The flight crew's failure to maintain directional control during the landing roll. A factor associated with the accident was the crew's failure to follow appropriate procedures.

## FAA accident and incident reports

None matched to N575D.

## Reports on N575D not matched to an aircraft (3)

They name N575D, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20020202000999I](https://openairdocs.org/incident/20020202000999I), Feb 2, 2002: Beech 1900D (N575D), Talkeetna, AK, Minor damage. (-23) Aircraft was in normal cruise flight at FL210 in VMC when pilot windshield suddenly cracked. Entire windshield was covered with numerous fracture lines…
- [Incident 20010411007659I](https://openairdocs.org/incident/20010411007659I), Apr 11, 2001: Beech 1900D (N575D), Anchorage, AK. (-23)Right top engine cowl departed aircraft during flight. Aircraft landed without incident. Actual number of pax on board is unknown, however there were no…
- [Accident 20001022027949A](https://openairdocs.org/incident/20001022027949A), Oct 22, 2000: Beech 1900D (N575D), Bethel, AK, No damage. (-23)The PIC of frontier flight 522 on the landing roll out, instructed the first officer to engage the power steering in preparation to taxi clear of the…

## 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 N575D not matched to an aircraft (7)

They name N575D, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR FFS2003F00009](https://openairdocs.org/sdr/FFS2003F00009), Jan 13, 2003: BOLT. UNDERTORQUED. WHILE PERFORMING AN INSPECTION OF THE TAIL SECTION, THE UPPER FOUR ATTACH BOLTS FOR THE VERTICAL STABILIZER FORWARD SPAR WERE SMOKING AND THE WASHERS WERE LOOSE
- [SDR FFS2003F00007](https://openairdocs.org/sdr/FFS2003F00007), Jan 11, 2003: TUBE. CRACKED. WHILE INVESTIGATING A RT BLEED AIR FAIL ANNUNCIATOR. DISCOVERED THE WELD FOR THE PRESSURE SWITCH CRACKED ON THE RT WING DEICE TUBE, INBOARD OF THE RT INSTRUMENT
- [SDR FFS2003F00005](https://openairdocs.org/sdr/FFS2003F00005), Dec 14, 2002: STIFFENER. CHAFED. EXTERNAL POWER ANNUNCIATOR WOULD NOT EXTINGUISH. FOUND AFT STIFFENER IN LEFT NACELLE AFT SKIN HAD CHAFED THROUGH INSULATION ON ELECTRICAL LEADS THAT GO FROM THE
- [SDR FFS2002F00009](https://openairdocs.org/sdr/FFS2002F00009), Dec 14, 2002: LEAD. CHAFED. EXTERNAL POWER ANNUNCIATOR WOULD NOT EXTINGUISH. FOUND AFT STIFFENER IN LT NACELLE AFT SKIN, HAD CHAFED THRU INSULATION ON ELECTRICAL LEADS THAT GO FROM THE EXT
- [SDR FFS2002F00003](https://openairdocs.org/sdr/FFS2002F00003), Feb 4, 2002: WINDSHIELD. CRACKED. PILOTS WINDSHIELD, FAILED IN CRUISE.
- [SDR FFS2001F00000](https://openairdocs.org/sdr/FFS2001F00000), Jul 11, 2001: SERVO VALVE. FAILED. POWER STEERING INOPERATIVE. FAILURE CODE C: ACTUATOR SERVO VALVE FAILURE: COMPUTER DETECTS A DECREASE IN SERVO CURRENT.
- [SDR FFSAFL92048](https://openairdocs.org/sdr/FFSAFL92048), Jul 11, 2001: SERVO VALVE. FAILED. POWER STEERING INOPERATIVE. FAILURE CODE C. ACTUATOR SERVO VALVE FAILURE. COMPUTER DETECTS A DECREASE IN SERVO CURRENT. SERVO VALVE MAY BE DAMAGED.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Callahan Robert R PROG AERODN SEAREY aircraft: https://openairdocs.org/model/callahan-robert-r-prog-aerodn-searey/aircraft.md
- The Bombardier ROTAX (ALL) engine: https://openairdocs.org/engine/bombardier-rotax-all.md

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