# N413: 1988 Park STEEN SKYBOLT

- Status: Valid registration
- Airframe: [Park STEEN SKYBOLT](https://openairdocs.org/model/park-steen-skybolt) (registry code 0565555, 2 seats)
- Engine: [Lycoming IO-540 series](https://openairdocs.org/engine/lycoming-io-540-series) (registry code 41530)
- Data sheets: [TCDS 1E4](https://openairdocs.org/tcds/1E4) (Lycoming Engines) (OpenAirDocs)
- Serial number: 32848
- Year built: 1988
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Experimental, amateur built
- Airworthiness date: August 9, 1988
- Certificate issued: December 1, 1993
- Expires: January 31, 2029
- Mode S code: A4DF44
- Registered owners: [Shearer John W](https://openairdocs.org/faa-owner/SHEARER%20JOHN%20W), [Shearer Barbara L](https://openairdocs.org/faa-owner/SHEARER%20BARBARA%20L)
- Location: [The Dalles, OR](https://openairdocs.org/faa-place/OR/The%20Dalles)
- Owner type: Co-owned
- Owner's area on the map: 45.5525° N, 121.1518° W: Placed by OpenAirDocs at the center of ZIP code 97058, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=413
- Page: https://openairdocs.org/aircraft/N413

From the FAA registry file of October 21, 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. The registry lists only the engine series, so ADs for every Lycoming IO-540 model are included.

## ADs that may apply (OpenAirDocs): 47 in force

### Matched by airframe (Park STEEN SKYBOLT)

None in force.

### Matched by engine (Lycoming IO-540 series)

- [AD 2026-17-10](https://openairdocs.org/ad/2026-17-10): Reciprocating Engine Cylinder Section · Lycoming Engines O-235, O-235-A, O-235-AP and 159 more. Effective Sep 14, 2026
- [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022
- [AD 2017-16-11](https://openairdocs.org/ad/2017-16-11): Reciprocating Engine Power Section · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-360-B1G6 and 93 more. Effective Aug 15, 2017
- [AD 2015-19-07](https://openairdocs.org/ad/2015-19-07): Fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 187 more. Effective Nov 3, 2015
- [AD 2015-02-07](https://openairdocs.org/ad/2015-02-07): Propeller governor shaft set screw · Lycoming Engines AEIO-320-D1B, AEIO-360-A1E, AEIO-360-A1E6 and 10 more. Effective Mar 11, 2015
- [AD 2012-19-01](https://openairdocs.org/ad/2012-19-01): Crankshafts · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 321 more. Effective Oct 24, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2010-07-08](https://openairdocs.org/ad/2010-07-08): Turbochargers · Kelly Aerospace Energy Systems HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 137 more. Effective Apr 19, 2010
- [AD 2009-26-12](https://openairdocs.org/ad/2009-26-12): Cylinder assemblies · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 264 more. Effective Feb 4, 2010
- [AD 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009
- [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2006-10-21](https://openairdocs.org/ad/2006-10-21): ECi connecting rods · Engine Components Reciprocating Engine Connecting Rods, AEIO-360-B1B, AEIO-360-B1D and 171 more. Effective Jun 22, 2006
- [AD 2005-19-11](https://openairdocs.org/ad/2005-19-11): Crankshafts · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 59 more. Effective Oct 21, 2005
- [AD 2005-12-06](https://openairdocs.org/ad/2005-12-06): Riveted-impulse coupling assemblies and snap-ring coupling assemblies · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 154 more. Effective Jul 19, 2005
- [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004
- [AD 2004-05-24](https://openairdocs.org/ad/2004-05-24): Zinc-plated Crankshaft Gear Retaining Bolts · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 161 more. Effective Mar 30, 2004
- [AD 2003-14-03](https://openairdocs.org/ad/2003-14-03): Rotary fuel pumps · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 262 more. Effective Aug 14, 2003
- [AD 2002-19-03](https://openairdocs.org/ad/2002-19-03): Crankshaft · Lycoming Engines IO-540-A1A5, IO-540-AA1A5, IO-540-AA1B5 and 81 more. Effective Sep 20, 2002
- [AD 2002-12-07](https://openairdocs.org/ad/2002-12-07): Oil Filter Converter Plate Gasket or the Converter Plate Kit · Lycoming Engines HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 95 more. Effective Jul 3, 2002
- [AD 99-04-04](https://openairdocs.org/ad/99-04-04): Impulse Coupling Pawl · Lycoming Engines IO-540-K1A5, IO-540-K1B5, IO-540-K1G5 and 6 more. Effective Feb 25, 1999
- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997
- [AD 97-01-04](https://openairdocs.org/ad/97-01-04): Cylinder assemblies · Lycoming Engines IO-540-M1B5D, LTIO-540-F2BD, LTIO-540-J2B and 10 more. Effective Apr 22, 1997
- [AD 96-23-03](https://openairdocs.org/ad/96-23-03): High pressure fuel pumps · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 174 more. Effective Dec 23, 1996
- [AD 96-09-10](https://openairdocs.org/ad/96-09-10): Oil pump · Lycoming Engines AEIO-320-E1A, AEIO-320-E1B, AEIO-320-E2A and 334 more. Effective Jul 15, 1996
- [AD 95-26-02](https://openairdocs.org/ad/95-26-02): Aviation Gasoline · Lycoming Engines IO-320-B1A, IO-320-B1B, IO-320-B1C and 182 more. Effective Jan 24, 1996
- [AD 95-07-01](https://openairdocs.org/ad/95-07-01): Connecting Rod Bolt · Lycoming Engines AEIO-360-A1E, AEIO-360-B1G6, AEIO-360-H1A and 177 more. Effective Apr 12, 1995
- [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992
- [AD 87-10-06 R1](https://openairdocs.org/ad/87-10-06-R1): Rocker Arm Assembly · Lycoming Engines IO-360-B4, IVO-360-A1A, O-340-A1A and 243 more. Effective Sep 1, 1989
- [AD 83-22-04](https://openairdocs.org/ad/83-22-04): Injector Fuel Diaphragm Stem · Lycoming Engines AEIO-540-L1B5D, IO-540-AA1A5, IO-540-G1B5 and 30 more. Effective Nov 4, 1983
- [AD 81-03-05](https://openairdocs.org/ad/81-03-05): Mixture Control Shaft Assembly · Lycoming Engines IGO-540-A1A, IGO-540-B1A, IGO-540-B1C and 9 more. Effective Feb 11, 1981
- [AD 79-04-05](https://openairdocs.org/ad/79-04-05): Regulator Diaphragm Stem Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 215 more. Effective Sep 26, 1979
- [AD 78-23-10](https://openairdocs.org/ad/78-23-10): Center Body Bellows Seal Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 218 more. Effective Nov 7, 1978
- [AD 78-23-08](https://openairdocs.org/ad/78-23-08): Fuel Pump To Fuel Injector Tube Elbow · Lycoming Engines IO-540-G1B5, IO-540-K1F5, IO-540-P1A5 and 1 more. Effective Nov 7, 1978
- [AD 75-08-09](https://openairdocs.org/ad/75-08-09): Oil Pump Drive Shaft · Lycoming Engines AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C and 365 more. Effective Aug 18, 1977
- [AD 73-23-01](https://openairdocs.org/ad/73-23-01): Piston Pin Assembly · Lycoming Engines AIO-360-A1A, AIO-360-A1B, AIO-360-A2A and 215 more. Effective Jan 13, 1977
- [AD 75-09-15](https://openairdocs.org/ad/75-09-15): Fuel Starvation To The Engine · Lycoming Engines AIO-320-A1A, AIO-320-A1B, AIO-320-A2A and 130 more. Effective Apr 30, 1975
- [AD 73-10-02](https://openairdocs.org/ad/73-10-02): Bendix Fuel Injectors · Bendix Fuel Injectors, AIO-320-A1A, AIO-320-A1B and 88 more. Effective May 16, 1973
- [AD 69-08-09](https://openairdocs.org/ad/69-08-09): Lycoming Engines IO-540-G1A5. Effective Apr 23, 1969
- [AD 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969
- [AD 67-22-06](https://openairdocs.org/ad/67-22-06): Fuel Injectors · Lycoming Engines HIO-360-A1A, HIO-360-B1A, HIO-360-B1B and 28 more. Effective Aug 9, 1967
- [AD 66-20-04](https://openairdocs.org/ad/66-20-04): Oil Filter Adapter Gasket · Lycoming Engines IO-320-A1A, IO-320-A2A, IO-320-B1A and 121 more. Effective Aug 27, 1966
- [AD 64-16-05](https://openairdocs.org/ad/64-16-05): AC Pumps · Lycoming Engines HIO-360-B1A, HIO-360-B1B, IO-320-B1A and 86 more. Effective Jul 10, 1964
- [AD 63-14-03](https://openairdocs.org/ad/63-14-03): Oil Pump Drive Shaft · Lycoming Engines IO-540-A1A5, IO-540-B1A5, IO-540-B1B5 and 21 more. Effective Jul 6, 1963

### Historical (superseded or no longer in force)

- [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024
- [AD 2011-26-04](https://openairdocs.org/ad/2011-26-04) (historical): Externally mounted fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 186 more. Effective Jan 25, 2012
- [AD 2011-15-10](https://openairdocs.org/ad/2011-15-10) (historical): Fuel servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 256 more. Effective Aug 16, 2011
- [AD 2008-19-05](https://openairdocs.org/ad/2008-19-05) (historical): Parallel Valve'' reciprocating engines · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 262 more. Effective Oct 20, 2008
- [AD 2008-14-07](https://openairdocs.org/ad/2008-14-07) (historical): Externally mounted fuel injector fuel lines · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 185 more. Effective Aug 14, 2008
- [AD 2008-08-14](https://openairdocs.org/ad/2008-08-14) (historical): Fuel injection servo plugs · Superior Air Parts AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 242 more. Effective Apr 29, 2008
- [AD 2008-06-51](https://openairdocs.org/ad/2008-06-51) (historical): Fuel injection servo plugs · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 235 more
- [AD 2006-20-09](https://openairdocs.org/ad/2006-20-09) (historical): Certain crankshafts replacing · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 82 more. Effective Nov 3, 2006
- [AD 2005-26-10](https://openairdocs.org/ad/2005-26-10) (historical): ECi cylinder assemblies. · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 413 more. Effective Jan 31, 2006
- [AD 2002-26-01](https://openairdocs.org/ad/2002-26-01) (historical): Fuel injector fuel lines · Textron Lycoming, AVCO IGO-480-A1B6, IGO-540-B1A, IGO-540-B1C and 178 more. Effective Jan 31, 2003
- [AD 2002-23-06](https://openairdocs.org/ad/2002-23-06) (historical): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, AEIO-540-D4A5, AEIO-540-D4B5 and 46 more. Effective Nov 19, 2002
- [AD 2002-20-51](https://openairdocs.org/ad/2002-20-51) (historical): Crankshaft gear retaining bolts · Textron Lycoming, AVCO AEIO-540, IO-540 Series (all), LTIO-540-F2BD and 39 more
- [AD 2000-18-53](https://openairdocs.org/ad/2000-18-53) (historical): Oil Filter Converter Plate Gaskets · Textron Lycoming, AVCO AEIO-540, IO-360-A1B6D, IO-360-A1D6D and 73 more
- [AD 98-18-12](https://openairdocs.org/ad/98-18-12) (historical): Fuel Pump · Textron Lycoming, AVCO AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 249 more. Effective Sep 28, 1998
- [AD 81-18-04 R2](https://openairdocs.org/ad/81-18-04-R2) (historical): Engine Oil Pump Driven Impeller and Shaft · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 376 more. Effective Jun 7, 1982

## Information bulletins (advisory) (13 in force)

- [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019
- [SAIB NE-08-32R1](https://openairdocs.org/saib/NE-08-32R1): Propeller Governor  Idler Gear Shaft Set Screw. Issued May 13, 2016
- [SAIB NE-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014
- [SAIB NE-13-06](https://openairdocs.org/saib/NE-13-06): Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series Engines. Issued Nov 21, 2012
- [SAIB NE-08-26R3](https://openairdocs.org/saib/NE-08-26R3): Magneto/Distributor. Issued Mar 31, 2011
- [SAIB NE-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-05-89](https://openairdocs.org/saib/NE-05-89): . Issued Sep 30, 2005
- [SAIB NE-05-40](https://openairdocs.org/saib/NE-05-40): . Issued Mar 18, 2005
- [SAIB NE-03-18](https://openairdocs.org/saib/NE-03-18): . Issued Jan 22, 2003
- [SAIB NE-03-12](https://openairdocs.org/saib/NE-03-12): . Issued Dec 30, 2002
- [SAIB NE-01-37](https://openairdocs.org/saib/NE-01-37): . Issued Aug 16, 2001
- [SAIB NE-01-22](https://openairdocs.org/saib/NE-01-22): . Issued May 11, 2001
- [SAIB NE-08-26R1](https://openairdocs.org/saib/NE-08-26R1) (historical): Dual Magnetos. Issued Jul 8, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008

## NTSB investigations

None matched to N413.

## FAA accident and incident reports

None matched to N413.

## Service difficulty reports (48)

As reported by operators and repair stations. Reports filed since June 6, 1975, when the mark's previous registration was cancelled.

- [SDR A6WA2016072144126](https://openairdocs.org/sdr/A6WA2016072144126), Jul 19, 2016: LANDING GEAR. MALFUNCTIONED. FLT NR 4047. AFTER TAKEOFF, SELECTED GEAR UP AND RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSG. (MC-NLG WAS DOWN AT THE TIME) WITHIN 6 SECONDS OF GEAR U
- [SDR A6WA201304024894](https://openairdocs.org/sdr/A6WA201304024894), Mar 29, 2013: SKIN. DAMAGED. RIGHT ELEVATOR LIGHTNING STRIKE ON TRAILING EDGE. REPAIR OF SKINS & REPLACEMENT OF T/E EXTRUSION P/N 601R24042-1 IAW REO 601R-55-21-382 REV C.
- [SDR A6WA201304014865](https://openairdocs.org/sdr/A6WA201304014865), Mar 29, 2013: MOUNT. CRACKED. NR 2 HYD SYSTEM O/B CASE DRAIN FILTER MOUNT IS CRACKED. REMOVED UNSERVICEABLE NR 2 HYD SYSTEM O/B CASE DRAIN FILTER MOUNT AND REPLACED WITH SERVICEABLE MOUNT IA
- [SDR A6WA201304024893](https://openairdocs.org/sdr/A6WA201304024893), Mar 28, 2013: SKIN. DAMAGED. C/W AWAC CARD 4DMI16663 REPAIR LEFT STAB LWR SKIN. REMOVED AND RE-INSTALLED NEW SERVICEABLE RIVET IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA201304024892](https://openairdocs.org/sdr/A6WA201304024892), Mar 28, 2013: POST. CRACKED. FS 409 VERT POST AT LBL & RBL 27 I/B RADIUS CRACKED FROM BOTTOM OF POST APPROX HALFWAY BETWEEN FIRST & SECOND RIVET. REPAIRED LT & RT LBL 27 POSTS I/B IAW GREO 
- [SDR A6WA201304024891](https://openairdocs.org/sdr/A6WA201304024891), Mar 28, 2013: FAIRING. DAMAGED. LEFT FLAP STAB FAIRING CHAFED AND GOUGED NEW SERVICEABLE STUB FAIRING FABRICATED & INSTALLED NEW SERVICEABLE SEAL RETAINERS. REMOVED UNSERVICEABLE LEFT STUB FAI
- [SDR A6WA201304014868](https://openairdocs.org/sdr/A6WA201304014868), Mar 28, 2013: SCREW. LOOSE. APU EXHAUST HEAT SHIELD HAS 4 EACH LOOSE SCREWS. REPAIRED HEAT SHIELD SCREW HOLES 4 EA IAW REO 601R-49-81-167.
- [SDR A6WA201304024884](https://openairdocs.org/sdr/A6WA201304024884), Mar 27, 2013: PANEL. DAMAGED. LEFT ELEVATOR HINGE UNDER PANEL 334AB HAS TOOLING MARKS. REPAIRED DAMAGE IAW REO 601R-55-11-456.
- [SDR A6WA201304014882](https://openairdocs.org/sdr/A6WA201304014882), Mar 27, 2013: DOOR. OUT OF LIMITS. LEFT MLG DOOR IS OUT OF LIMITS PER AMM 32-12-01-502 ZONE E. REMOVED AND REPLACED UNSERVICEABLE LEFT MLG DOOR WITH UNSERVICEABLE LEFT MLG DOOR P/N 601R31178-169,
- [SDR A6WA201304014877](https://openairdocs.org/sdr/A6WA201304014877), Mar 27, 2013: DOOR. CHAFED. RIGHT MLG DOOR AFT EDGE IS CHAFED. REPAIRED CHAFING ON AFT EDGE OF RIGHT MLG DOOR IAW BOMBARDIER REO 601R-32-82-366.
- [SDR A6WA201304014855](https://openairdocs.org/sdr/A6WA201304014855), Mar 27, 2013: STRUCTURE. SCRATCHED. NICKS AND SCRATCHES FOUND ON CARGO DOOR CUTOUT FWD LIP. BLENDED & RESTORED FINISH IAW REO 601R-53-61-4839. BLENDED & RESTORED FINISH IAW REO 601R-53-61-4839.
- [SDR A6WA201304014854](https://openairdocs.org/sdr/A6WA201304014854), Mar 27, 2013: STRUCTURE. SCRATCHED. NICKS AND SCRATCHES FOUND ON CARGO DOOR CUTOUT UPPER LIP. BLEND RESTORE FINISH IAW REO 601R-53-61-4839.
- [SDR A6WA201304014869](https://openairdocs.org/sdr/A6WA201304014869), Mar 26, 2013: COWLING. DELAMINATED. RIGHT UPPER CORE COWL HAS DELAMINATION ON I/B SIDE & L/E (FIRE SHIELD). REPAIRED IAW REO 601R-71-12-458.
- [SDR A6WA201304014867](https://openairdocs.org/sdr/A6WA201304014867), Mar 26, 2013: SKIN. DAMAGED. FUSELAGE SKIN JUST AFT OF APU EXHAUST HAS SCREW MARKS. BLEND REPAIR IAW REO 601R-53-61-4841.
- [SDR A6WA201304014864](https://openairdocs.org/sdr/A6WA201304014864), Mar 26, 2013: ANGLE. CRACKED. AFT SIDE OF 621 BULKHEAD AT STR 14L ANGLE IS CRACKED. REMOVED AND REPLACED P/N 601-35012-51 IAW CRJ 200 SRM 51-40-11, 51-42-31.
- [SDR A6WA201304014863](https://openairdocs.org/sdr/A6WA201304014863), Mar 26, 2013: STIFFENER. CHAFED. CENTER VERTICAL STIFFENER ON AFT SIDE OF 621 BULKHEAD CHAFED BY BLEED AIR VALVE. BLEND REPAIR IAW REO 601R-53-61-4842.
- [SDR A6WA201304014857](https://openairdocs.org/sdr/A6WA201304014857), Mar 25, 2013: FITTING. CORRODED. FITTING AT FS 310.0 STR 17 CORRODED. REMOVED AND REPLACED FITTING P/N 601R38335-1S IAW CRJ 200 SRM 51-40-11 & 51-42-21.
- [SDR A6WA201304024887](https://openairdocs.org/sdr/A6WA201304024887), Mar 24, 2013: STOP FITTING. CHAFED. RIGHT EMERGENCY EXIT STOP FITTING CHAFED 6EA. BLENDED 6EA STOP FITTINGS ON RIGHT EMERGENCY EXIT.
- [SDR A6WA201304014866](https://openairdocs.org/sdr/A6WA201304014866), Mar 24, 2013: MOUNT. CRACKED. NR 2 HYD SYSTEM RETURN FILTER MOUNT IS CRACKED. REMOVED UNSERVICEABLE NR 2 HYD SYSTEM RETURN FILTER MOUNT AND REPLACED WITH SERVICEABLE MOUNT IAW BOMBARDIER REO
- [SDR A6WA201304014848](https://openairdocs.org/sdr/A6WA201304014848), Mar 24, 2013: MOUNT BRACKET. CRACKED. HYD ACCUMULATOR FWD O/B MOUNTING BRACKET IS CRACKED IN THE NOSE HYD COMPARTMENT. REMOVE AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-21.
- [SDR A6WA201304024886](https://openairdocs.org/sdr/A6WA201304024886), Mar 23, 2013: STOP FITTING. CRACKED. MAIN AVIONICS DOOR STOP FITTING BACK UP STUCK ON FWD SIDE IS CORRODED. REMOVED AND REPLACED PART.
- [SDR A6WA201304014872](https://openairdocs.org/sdr/A6WA201304014872), Mar 23, 2013: BRACKET. CRACKED. BRACKET CRACKED ON RIGHT ENGINE NOSE INLET FWD OF T/R FLEX DRIVE SHAFT BETWEEN 4 & 5 O` CLOCK POSITION. REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-13.
- [SDR A6WA201304024883](https://openairdocs.org/sdr/A6WA201304024883), Mar 22, 2013: SKIN. CHAFED. LEFT MLG DOOR INNER SKIN CHAFED. REMOVED & REPLACED CHAFED UPPER INNER SKIN FOUND CHAFE ON LOWER INNER SKIN FOUND WITHIN LIMITS WITH MAT LOSS OF .004, MAX ALLOW
- [SDR A6WA201304014871](https://openairdocs.org/sdr/A6WA201304014871), Mar 22, 2013: BRACKET. BROKEN. RIGHT ENGINE INLET BROKEN BRACKET FWD OF FAN INLET TEMP. REMOVED AND REPLACED BRACKET.
- [SDR A6WA201304024889](https://openairdocs.org/sdr/A6WA201304024889), Mar 21, 2013: STRUCTURE. DAMAGED. 2 FASTENER HOLES ON ACCESS HOLE 132AL ARE DAMAGED 12 O`C LOCK AND 3 O` CLOCK POSITION. REPAIRED PER BOMBARDIER REO 601R-53-11-162 REV B.
- [SDR A6WA201304024888](https://openairdocs.org/sdr/A6WA201304024888), Mar 20, 2013: MOUNT BRACKET. CRACKED. EXTERNAL A/C POWER PLUG MOUNT IS CRACKED. REMOVED AND REPLACED MOUNT BRACKET.
- [SDR A6WA201304014873](https://openairdocs.org/sdr/A6WA201304014873), Mar 20, 2013: RIB. CHAFED. CHAFE DAMAGE LEFT I/B FLAP ON I/B END OF FLAP L/E AND SURROUNDING RIVER HEADS. REMOVED AND REPLACED DAMAGED RIB & FASTENERS IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA201304024885](https://openairdocs.org/sdr/A6WA201304024885), Mar 19, 2013: HANDLE. CRACKED. MAIN AVIONICS COMPARTMENT DOOR HANDLE CRACKED. REMOVED AND REPLACED HANDLE ASSY.
- [SDR A6WA201304014874](https://openairdocs.org/sdr/A6WA201304014874), Mar 17, 2013: FITTING. DAMAGED. WHILE PERFORMING COLD WORKING ON RIGHT LOWER FLANGE OF MLG TRUNNION FITTING FOUND 1EA OVERSIZED FASTENERS. REPAIRED HOLE PER REO 601R-57-21-1886.
- [SDR A6WA201304014876](https://openairdocs.org/sdr/A6WA201304014876), Mar 16, 2013: HINGE. GOUGED. RIGHT OUTBD FLAP OUTBD HINGE ARM & HINGE BOX HAVE GOUGING AND FOD DAMAGE AT FLAP HINGE POINT. REPAIR IAW REO 'S 601R-57-53-971 & 601R-57-21-1888.
- [SDR A6WA201304014875](https://openairdocs.org/sdr/A6WA201304014875), Mar 16, 2013: SKIN. CHAFED. BUTE DOOR 694PB HAS CHAFE SPOTS ON UPPER SIDE. REMOVE & REPLACE BUTE DOOR SKIN AIW CRJ 200 SRM 51-42-06.
- [SDR A6WA201304014880](https://openairdocs.org/sdr/A6WA201304014880), Mar 14, 2013: RIB. CRACKED. LEFT MLG BATT RIB CRACKED. REMOVED UNSERVICEABLE REPAIR DOUBLER WITH A SERVICEABLE REPAIR DOUBLER AND INSTALLED.
- [SDR A6WA201304024890](https://openairdocs.org/sdr/A6WA201304024890), Mar 13, 2013: SILL. CORRODED. RIGHT FLOOR SILL IN CARGO COMPARTMENT HAS CORROSION FROM FS 559+80 TO 621. REPAIRED IAW REO 601R-53-00-515.
- [SDR A6WA201304014878](https://openairdocs.org/sdr/A6WA201304014878), Mar 13, 2013: RIB. CRACKED. RIGHT MLG BATT RIB IS CRACKED. REPAIRED PER REO 601R-57-51-046 REPAIR 2.
- [SDR A6WA201304014881](https://openairdocs.org/sdr/A6WA201304014881), Mar 12, 2013: MOUNT BRACKET. CRACKED. LEFT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED. REMOVED AND REPLACED UNSERVICEABLE LEFT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET W
- [SDR A6WA201304014879](https://openairdocs.org/sdr/A6WA201304014879), Mar 12, 2013: BRACKET. CRACKED. RIGHT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED. REMOVED AND REPLACED UNSERVICEABLE RIGHT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET
- [SDR A6WA201304014860](https://openairdocs.org/sdr/A6WA201304014860), Mar 12, 2013: RIVET. POPPED. FS 280 FLOOR SUPPORT STRUCTURE LBL 9 FWD TB ANGLE ABOVE HAS POPPED RIVET HEAD AND ON UNDER DRIVEN RIVET NEXT TO IT HEAD IS NOT SEATED ON ANGLE.
- [SDR A6WA201304014859](https://openairdocs.org/sdr/A6WA201304014859), Mar 12, 2013: FITTING. CRACKED. PAX FS 280 CLIPS ARE CRACKED UPPER O/B LBL 9 & RBL 9. FABRICATED & INSTALLED SERVICEABLE O/B LBL 9 & RBL 9 CLIPS.
- [SDR A6WA201304014850](https://openairdocs.org/sdr/A6WA201304014850), Mar 12, 2013: FLOORBEAM. CORRODED. TOP OF FS 280 FLOORBEAM CAP IS CORRODED. REPLACED FS 280 FLOORBEAM CAP.
- [SDR A6WA201304014849](https://openairdocs.org/sdr/A6WA201304014849), Mar 12, 2013: FITTING. CRACKED. 280 I/B RBL 9 & LBL 9 CLIPS ARE CRACKED. FABRICATED & INSTALLED SERVICEABLE RBL 9 & LBL 9 I/B CLIPS.
- [SDR A6WA201304014862](https://openairdocs.org/sdr/A6WA201304014862), Mar 11, 2013: RIVET. SHEARED. CARGO BAY NET TIE DOWN SUPPORT ANGLE AS IT ATTACHES TO 621 BULKHEAD HAS SHEARED OFF RIVETS (2EA). REPLACED RIVETS IAW CRJ 200 SRM.
- [SDR A6WA201304014858](https://openairdocs.org/sdr/A6WA201304014858), Mar 11, 2013: FITTING. CRACKED. CLIP UNDER CARGO DOOR SILL BENEATH AFT CARGO DOOR STOP AT FS 605 IS CRACKED. REMOVED & REPLACED CLIP IAW CRJ 200 SRM.
- [SDR A6WA201304014856](https://openairdocs.org/sdr/A6WA201304014856), Mar 9, 2013: STRUCTURE. GOUGED. RIGHT AFT SIDE FS 280 AT RBL 9 APPROX 12 INCHES UP FROM FLOOR GOUGED 2 LOCATIONS FROM FWD GALLEY DOOR. REPAIRED RIGHT AFT SIDE FS 280 AFT RBL 9 IAW REO 601R-53-
- [SDR A6WA201304014853](https://openairdocs.org/sdr/A6WA201304014853), Mar 9, 2013: CARGO TRACK. CORRODED. SEAT TRACK IN CARGO COMPARTMENT AT RBL 9 FROM 559+86 TO 559+96 (APPROX) IS CORRODED. REMOVE AND REPLACE CORRODED SEAT TRACK FROM FS 559 +96 TO 559 +96 (APPROX).
- [SDR A6WA201304014852](https://openairdocs.org/sdr/A6WA201304014852), Mar 9, 2013: ANGLE. CRACKED. PAX PRESSURE FLOOR FS 484.0 CLIP ANGLE IS CRACKED UPPER I/B RBL 27. REMOVED AND REPLACED FS 484.0 CLIP ANGLE.
- [SDR A6WA201304014851](https://openairdocs.org/sdr/A6WA201304014851), Mar 9, 2013: ANGLE. CRACKED. PAX PRESSURE FLOOR FS 484.0 CLIP ANGLES CRACKED UPPER I/B LBL 27 AND UPPER O/B LBL 36. REMOVED AND REPLACED 484.0 CLIP ANGLES ON UPPER I/B LBL 27 & UPPER O/B LB
- [SDR A6WA201304014861](https://openairdocs.org/sdr/A6WA201304014861), Mar 8, 2013: SEAT TRACK. CORRODED. CORROSION FOUND ON RIGHT PAX SEAT RAIL AT FS 364.00 FOUND TO BE OUT OF LIMITS DEPTH OF DAMAGE 024" MAX ALLOWED 020". REMOVED AND REPLACED PAX SEAT RAIL BETWEEN 
- [SDR A6WA201304014870](https://openairdocs.org/sdr/A6WA201304014870), Mar 7, 2013: COWLING. DENTED. TWO DENTS & 1 HOLE FOUND ON RIGHT LWR CORE COWL BETWEEN 2ND & 3RD BEAMS ON I/B SIDE. PERFORM REPAIR IAW CRJ 200 CMM 71-12-01 REPAIR SRS 021.

## Earlier aircraft with N413

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N413 before.

- [Cancelled 1975-06-06](https://openairdocs.org/deregistered/N413-1975-06-06): Park B-8M, S/N 32848. Exported to Canada. Owner: [Park Stephen D](https://openairdocs.org/faa-owner/PARK%20STEPHEN%20D), [Rochester, IL](https://openairdocs.org/faa-place/IL/Rochester)
- [Cancelled 1929-05-21](https://openairdocs.org/deregistered/N413-1929-05-21): Mohawk PINTO MSW, S/N 118. Owner: [First National Productions Corp](https://openairdocs.org/faa-owner/FIRST%20NATIONAL%20PRODUCTIONS%20CORP), [Burbank, CA](https://openairdocs.org/faa-place/CA/Burbank)

## Related

- Other Park STEEN SKYBOLT aircraft: https://openairdocs.org/model/park-steen-skybolt/aircraft.md
- STCs for the Park STEEN SKYBOLT: https://openairdocs.org/model/park-steen-skybolt/stcs.md
- The Lycoming IO-540 series engine: https://openairdocs.org/engine/lycoming-io-540-series.md

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