# N301SW: Piper PA-23-250

- Status: Valid registration
- Airframe: Piper PA-23-250 (registry code 7102308, TCDS 1A10 (OpenAirDocs match))
- Serial number: 27-195
- Type: Fixed wing multi engine
- Certificate issued: September 7, 2026
- Expires: September 30, 2033
- Mode S code: A324AE
- Registered owner: Fly Rite Aviation LLC
- Location: Fort Myers, FL
- Owner's area on the map: 26.5815° N, 81.8350° W: Placed by OpenAirDocs at the center of ZIP code 33966, within about 2 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N301SW

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 matched by airframe (Piper PA-23-250) (OpenAirDocs)

- [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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI). Effective Mar 21, 2022
- [AD 2021-25-11](https://openairdocs.org/ad/2021-25-11): Horizontal Stabilizer Structure · Piper PA-23-250. Effective Jan 25, 2022
- [AD 2017-15-05](https://openairdocs.org/ad/2017-15-05): Air Conditioning · Piper PA-23, PA-23-160, PA-23-235 and 3 more. Effective Aug 28, 2017
- [AD 2015-24-05](https://openairdocs.org/ad/2015-24-05): PLACARDS AND MARKINGS; Interior Placards · Piper PA-23-250, PA-24-250, PA-24-260 and 7 more. Effective Jan 12, 2016
- [AD 2009-13-06 R1](https://openairdocs.org/ad/2009-13-06-R1): Doors · Piper PA-23, PA-23-160, PA-23-235 and 16 more. Effective Nov 3, 2011
- [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 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2005-01-10](https://openairdocs.org/ad/2005-01-10): Turbocharger Oil Reservoir · Piper PA-23-235, PA-23-250, PA-23-250 (Navy UO-1) and 1 more. Effective Feb 22, 2005
- [AD 2003-09-13](https://openairdocs.org/ad/2003-09-13): Flap control torque tube assembly · Piper PA-23, PA-23-160, PA-23-235 and 2 more. Effective Jun 23, 2003
- [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000
- [AD 99-14-01](https://openairdocs.org/ad/99-14-01): AFM - Limitations Section - Icing · Piper PA-23, PA-23-160, PA-23-235 and 21 more. Effective Aug 17, 1999
- [AD 99-05-09](https://openairdocs.org/ad/99-05-09): Induction Air Filter · Piper PA-23-235, PA-23-250, PA-23-250 (Navy UO-1) and 20 more. Effective Mar 19, 1999
- [AD 83-22-01 R1](https://openairdocs.org/ad/83-22-01-R1): Fuel Weight Limitations · Piper PA-23-235, PA-23-250, PA-23-250 (Navy UO-1) and 1 more. Effective Nov 25, 1998
- [AD 85-02-05 R1](https://openairdocs.org/ad/85-02-05-R1): Piper P/N s 81090-02, 683-107 Placard Installation · Lavia Argentina PA-25, PA-25-235, PA-25-260 and 32 more. Effective Nov 21, 1997
- [AD 96-21-04](https://openairdocs.org/ad/96-21-04): Hydraulic Hose Inspection · Piper PA-23, PA-23-160, PA-23-235 and 13 more. Effective Dec 10, 1996
- [AD 93-06-02](https://openairdocs.org/ad/93-06-02): Fuel Hose · Integral 24 gallon auxiliary fuel tank in each wing tip (Met-Co Aire STC SA1480WE). Effective May 12, 1993
- [AD 88-21-07 R1](https://openairdocs.org/ad/88-21-07-R1): Fuel Filler Compartment · Piper PA-23, PA-23-160, PA-23-235 and 3 more. Effective Aug 22, 1989
- [AD 81-04-05 R1](https://openairdocs.org/ad/81-04-05-R1): Flap-Spar Hinge Attachment · Piper PA-23, PA-23-235, PA-23-250 and 1 more. Effective Feb 11, 1982
- [AD 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981
- [AD 80-26-04 R1](https://openairdocs.org/ad/80-26-04-R1): Rudder Pulley at Cabin Step · Piper PA-23, PA-23-160, PA-23-235 and 2 more. Effective Aug 28, 1981
- [AD 80-18-10](https://openairdocs.org/ad/80-18-10): Fuel Selector Valves · Piper PA-23, PA-23-160, PA-23-235 and 8 more. Effective Sep 8, 1980
- [AD 79-26-01](https://openairdocs.org/ad/79-26-01): Stabilator Skins and Frame · Piper PA-23-250 and PA-23-250 (Navy UO-1). Effective Dec 24, 1979
- [AD 79-11-06](https://openairdocs.org/ad/79-11-06): Landing Gear Selector Lever · Piper PA-23, PA-23-160, PA-23-235 and 3 more. Effective Aug 29, 1979
- [AD 78-25-03](https://openairdocs.org/ad/78-25-03): Hose Assemblies · Piper PA-23-250, PA-28R-180, PA-28R-200 and 11 more. Effective Jan 15, 1979
- [AD 77-23-09](https://openairdocs.org/ad/77-23-09): Fuel Flow · Piper PA-23-250, PA-23-250 (Navy UO-1) and PA-E23-250. Effective Dec 19, 1978
- [AD 77-09-10](https://openairdocs.org/ad/77-09-10): Electric Trim Switch · Piper PA-23-250, PA-23-250 (Navy UO-1), PA-24-260 and 6 more. Effective May 12, 1977
- [AD 77-01-05](https://openairdocs.org/ad/77-01-05): Strobe NAV Light Wire · Piper PA-23-250 and PA-23-250 (Navy UO-1). Effective Jan 13, 1977
- [AD 76-11-07](https://openairdocs.org/ad/76-11-07): Magnetic Compass Deviations · Piper PA-23-250 and PA-23-250 (Navy UO-1). Effective Jun 4, 1976
- [AD 74-13-03](https://openairdocs.org/ad/74-13-03): Stabilator Attach Bolts · Piper PA-23-235, PA-23-250 (Navy UO-1), PA-24 and 5 more. Effective Apr 30, 1976
- [AD 72-21-07](https://openairdocs.org/ad/72-21-07): Longitudinal Stability · Piper PA-23-250 (Navy UO-1). Effective Apr 29, 1976
- [AD 74-10-01](https://openairdocs.org/ad/74-10-01): Outboard Flap Hinge · Piper PA-23-250 (Navy UO-1). Effective Dec 31, 1975
- [AD 75-11-05](https://openairdocs.org/ad/75-11-05): Glare Shield Panel · Piper PA-23-250 and PA-23-250 (Navy UO-1). Effective May 20, 1975
- [AD 74-22-05](https://openairdocs.org/ad/74-22-05): Full Valve Stem and Cap Nut · Piper PA-23, PA-23-160, PA-23-235 and 2 more. Effective Oct 23, 1974
- [AD 72-14-05](https://openairdocs.org/ad/72-14-05): Engine Exhaust System Stacks · Piper PA-23-250, PA-23-250 (Navy UO-1) and PA-E23-250. Effective Sep 3, 1974
- [AD 72-11-01](https://openairdocs.org/ad/72-11-01): Possible Fire From Fuel Vapor · Piper PA-23-235, PA-23-250 (Navy UO-1) and PA-E23-250 with STC SA179CE or SA867SW. Effective May 19, 1972
- [AD 68-07-04](https://openairdocs.org/ad/68-07-04): Engine Mount · Piper PA-23-250 (Navy UO-1). Effective Apr 11, 1972
- [AD 70-22-05](https://openairdocs.org/ad/70-22-05): Electrical System Modifications · Piper PA-23-250 (Navy UO-1), PA-30, PA-31 and 1 more. Effective Nov 30, 1971
- [AD 71-21-06](https://openairdocs.org/ad/71-21-06): Engine Firewall Flex Duct · Piper PA-23-250 (Navy UO-1). Effective Oct 12, 1971
- [AD 71-18-03](https://openairdocs.org/ad/71-18-03): Left Nose Wheel Door Hinge · Wheel well doors (Apache Modification STC SA598SW). Effective Sep 2, 1971
- [AD 71-12-05](https://openairdocs.org/ad/71-12-05): Electric Trim Switch Modification · Piper PA-23-250 (Navy UO-1), PA-24-260, PA-30 and 5 more. Effective Jun 16, 1971
- [AD 71-12-01](https://openairdocs.org/ad/71-12-01): Engine Control Support Bracket · Piper PA-23, PA-23-160 and PA-23-250 (Navy UO-1). Effective Jun 8, 1971
- [AD 68-21-03](https://openairdocs.org/ad/68-21-03): Exhaust Tailpipe Assemblies · Piper PA-23-250 (Navy UO-1) and PA-E23-250 with STC SA909WE or SA978WE. Effective Oct 28, 1968
- [AD 66-18-03](https://openairdocs.org/ad/66-18-03): Induction System Icing · Piper PA-23-250 (Navy UO-1) and PA-E23-250. Effective Aug 2, 1966
- [AD 64-21-05](https://openairdocs.org/ad/64-21-05): Hartzell Propeller Governor · Piper PA-23-250 (Navy UO-1) and PA-30. Effective Sep 16, 1964

Historical (superseded or no longer in force): AD 2009-13-06, AD 78-02-03, AD 74-06-01, AD 69-13-03

## Information bulletins (advisory)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
- [SAIB CE-17-08](https://openairdocs.org/saib/CE-17-08): Main Landing Gear  Drag Link Bolt
- [SAIB CE-12-44](https://openairdocs.org/saib/CE-12-44): Exhaust systems
- [SAIB CE-08-11](https://openairdocs.org/saib/CE-08-11): Landing Gear
- [SAIB CE-04-88](https://openairdocs.org/saib/CE-04-88): 

## Earlier aircraft with N301SW

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N301SW before.

- [Cancelled 2009-08-04](https://openairdocs.org/deregistered/N301SW-2009-08-04): Boeing 737-3H4, S/N 22941, built 1984. Triennial form not returned. Owner: Southwest Airlines Co, Dallas, TX

## Service difficulty reports (252)

- [SDR SWAA083914](https://openairdocs.org/sdr/SWAA083914), Jul 15, 2008: SLIDE. R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY.  INSTALLED EVAC SLIDE PER MM.
- [SDR SWAA081717](https://openairdocs.org/sdr/SWAA081717), Mar 27, 2008: SLIDE. L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST.  ADJUSTED EVAC SLIDE PER MM.
- [SDR SWAA081535](https://openairdocs.org/sdr/SWAA081535), Mar 21, 2008: SKIN. DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 523, STR 13R.  REPAIRED SKIN PER SWA EA.
- [SDR SWAA081567](https://openairdocs.org/sdr/SWAA081567), Mar 20, 2008: SKIN. DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT UPPER AFT CORNER.  REPAIRED SKIN PER SRM.
- [SDR SWAA081568](https://openairdocs.org/sdr/SWAA081568), Mar 20, 2008: SLIDE. DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST.  ADJUSTED EVAC SLIDE PER MM.
- [SDR SWAA081569](https://openairdocs.org/sdr/SWAA081569), Mar 20, 2008: SLAT. DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT OUTBOARD T/E.  REPAIRED SLAT PER SRM.
- [SDR SWAA080992](https://openairdocs.org/sdr/SWAA080992), Feb 23, 2008: SKIN. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 17L.  REPAIRED SKIN PER SRM.
- [SDR SWAA080482](https://openairdocs.org/sdr/SWAA080482), Jan 28, 2008: SKIN. DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 17R.  REPAIRED SKIN PER SRM.
- [SDR SWAA076070](https://openairdocs.org/sdr/SWAA076070), Dec 9, 2007: SKIN. DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 742C, STR 14R.  REPAIRED SKIN PER SWA EA.
- [SDR SWAA074217](https://openairdocs.org/sdr/SWAA074217), Aug 27, 2007: SKIN. DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21L.  REPAIRED SKIN PER SWA EA.

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.