# N319AM: 2005 Aviat A-1B

- Status: Valid registration
- Airframe: [Aviat A-1B](https://openairdocs.org/model/aviat-a-1b) (registry code 2210406, 2 seats)
- Engine: [Lycoming O-360-A1P](https://openairdocs.org/engine/lycoming-o-360-a1p) (registry code 42259)
- Data sheets: [TCDS A22NM](https://openairdocs.org/tcds/A22NM) (Aviat Aircraft Inc.), [TCDS E-286](https://openairdocs.org/tcds/E-286) (Lycoming Engines) (OpenAirDocs)
- Serial number: 2319
- Year built: 2005
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: October 7, 2005
- Certificate issued: April 17, 2023
- Expires: April 30, 2030
- Mode S code: A3684C
- Registered owner: [Jones Arthur L](https://openairdocs.org/faa-owner/JONES%20ARTHUR%20L)
- Location: [Bend, OR](https://openairdocs.org/faa-place/OR/Bend)
- Owner type: Individual
- Owner's area on the map: 43.9828° N, 121.2097° W: Placed by OpenAirDocs at the center of ZIP code 97702, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=319AM
- Page: https://openairdocs.org/aircraft/N319AM

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): 22 in force

### Matched by airframe (Aviat A-1B)

- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2020-16-06](https://openairdocs.org/ad/2020-16-06): Horizontal Stabilizer Structure · Aviat A-1, A-1A, A-1B and 2 more. Effective Sep 1, 2020

### Matched by engine (Lycoming O-360-A1P)

- [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 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 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 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012
- [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 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 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 98-02-08](https://openairdocs.org/ad/98-02-08): Crankshaft · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 216 more. Effective Mar 30, 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 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 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 89-04-02](https://openairdocs.org/ad/89-04-02): Carburetors · Continental Motors O-470-11, O-470-11-CI, O-470-11B and 175 more. Effective Mar 8, 1989
- [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980
- [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 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969
- [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967
- [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 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 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 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 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) (6 in force)

- [SAIB CE-17-18](https://openairdocs.org/saib/CE-17-18): Engine Exhaust System, Muffler Cracking. Issued Jun 20, 2017
- [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-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008

## NTSB investigations (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 SEA07CA261](https://openairdocs.org/ntsb/SEA07CA261), Sep 13, 2007: Aviat A-1B (N319AM), Grangeville, ID, substantial damage. Probable cause: The pilot's failure to maintain directional control during the landing roll. Factors include a ditch located between the runway and the taxiway.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20200923022309I](https://openairdocs.org/incident/20200923022309I), Sep 23, 2020: Aviat Aircraft Inc A-1B (N319AM), Afton, WY, Minor damage. Just prior to touchdown on runway 34 at kafo, a gust of wind lifted left wing and caused right tire to to contact pavement. Pilot applied left stick and right…
- [Incident 20070913020749I](https://openairdocs.org/incident/20070913020749I), Sep 13, 2007: Aviat A1B (N319AM), Grangeville, ID, Minor damage. (-23) The pilot was landing on runway 07 at Grangeville 'S80' id. Upon roll out the pilot lost control of the aircraft. The aircraft exited the runway on 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 N319AM not matched to an aircraft (66, newest 50)

They name N319AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR TRB2004F00005](https://openairdocs.org/sdr/TRB2004F00005), Dec 30, 2003: COMPUTER. FAULTY. DURING TAKEOFF ROLL THE PITCH ASSYMETRIC WARNING CAME ON. REMOVED AND REPLACED THE CREW ALERTING COMPUTER.
- [SDR TRB2004F00001](https://openairdocs.org/sdr/TRB2004F00001), Dec 25, 2003: INDICATOR. ERRATIC. DURING TAKEOFF THE RT ENGINE ITT WENT TO 765 DEGREES. CREW ABORTED THE TAKEOFF AND RETURNED TO BLOCK. REMOVED AND REPLACED THE ITT INDICATOR FOR THE RT ENGINE.
- [SDR SIMA200221203](https://openairdocs.org/sdr/SIMA200221203), Jul 29, 2002: BATTERY. DISCHARGED. MIA - FLT 5069 - FOUND EMERGENCY LIGHTS DON'T WORK WHEN AIRCRAFT IS NOT POWERED UP. LIGHT DON NOT WORK WHEN POWER IS ON IE, OR EXTERNAL POWER RAI ALL 6 BATTERY 
- [SDR SIMA200210030](https://openairdocs.org/sdr/SIMA200210030), Apr 5, 2002: SILL DRAIN. CORRODED. SAW - DURING CPCP2 FOUND SERVICE DOOR SILL DRAIN TRACK CORRODED. REMOVED AND REPLACED SILL PLATE DRAIN TRACK IAW SRM 51-25-01 AND 51-25-03. AIRCRAFT WAS RETURNE
- [SDR SIMA200210028](https://openairdocs.org/sdr/SIMA200210028), Apr 5, 2002: FLOOR SUPPORT. CORRODED. SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 38 TO 39 CORRODED. REMOVED AND REPLACED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR 42 SRM 51-25-02. AIRCRA
- [SDR SIMA200210027](https://openairdocs.org/sdr/SIMA200210027), Apr 5, 2002: FLOOR SUPPORT. CORRODED. SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 36 TO 38 CORRODED. REMOVED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR42 SRM 51-25-01. AIRCRAFT WAS RETURNE
- [SDR SIMA200210026](https://openairdocs.org/sdr/SIMA200210026), Apr 5, 2002: FRAME. CORRODED. SAW - DURING CPCP2 FOUND RIGHT FRAME 37 CORRODED ON AFT SIDE JUST ABOVE SILL PLATE CORRODED. REMOVED AND REPLACED FRAME 37 RIGHT IAW SRM 51-25-02 AND 51-25-04. 
- [SDR SIMA200209432](https://openairdocs.org/sdr/SIMA200209432), Apr 2, 2002: FLAP. CORRODED. SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP MIDDLE FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-006
- [SDR SIMA200209431](https://openairdocs.org/sdr/SIMA200209431), Apr 2, 2002: FLAP. CORRODED. SAW - DURING INSPECTION, FOUND RIGHT OUTBOARD FLAP OUTBOARD FORWARD BEAM ATTACH FITTING CORRODED. REPLACED RIGHT OUTBOARD FLAP ASSY IAW JIC-57-53-00-RAI-10000-0
- [SDR SIMA200209430](https://openairdocs.org/sdr/SIMA200209430), Apr 2, 2002: FLAP. CORRODED. SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP AFT BEAM ATTACH FITTING CORRODED. REPLACED LEFT OUTBOARD FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-006. (M)
- [SDR SIMA200209429](https://openairdocs.org/sdr/SIMA200209429), Apr 2, 2002: FLAP. CORRODED. SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLAP ASSY IAW JIC 57-53-00-RAI-10000-006. (M)
- [SDR SIMA200209428](https://openairdocs.org/sdr/SIMA200209428), Apr 2, 2002: SUPPORT. CORRODED. DURING CPCP4 INSPECTION, FOUND ALL PAX DOOR TREAD SUPPORTS HAVE CORROSION. REPLACED ALL PAX DOOR TREAD SUPPORTS IAW SRM 51-25-02. (M)
- [SDR SIMA200209427](https://openairdocs.org/sdr/SIMA200209427), Apr 1, 2002: LINK. CORRODED. MBV - DURING FOUND LEFT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED LEFT AILERON DUAL LOAD PATH LINK IAW JIC 27-11-72-RAI-10000-002. (M)
- [SDR SIMA200209419](https://openairdocs.org/sdr/SIMA200209419), Mar 27, 2002: CLIP. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND CLIPS ON PAX DOOR INTERCOSTAL TO CENTER RIB ABOVE VENT DOOR CORRODED. REPLACED CLIPS ON PASSENGER DOOR INTERCOSTAL IAW SRM 
- [SDR SIMA200209418](https://openairdocs.org/sdr/SIMA200209418), Mar 27, 2002: SILL. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND PASSENGER DOOR SILL PLATE DRAIN TRACK CORRODED. REPLACED PASSENGER DOOR SILL PLATE DRAIN TRACK IAW SRM 51-21-42. (M)
- [SDR SIMA200209417](https://openairdocs.org/sdr/SIMA200209417), Mar 27, 2002: WEB. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND LEFT WEB FROM FRAME 39-40 AT Z-MEMBER CORRODED. REPLACED LEFT WEB FROM FRAMES 39-40 AT Z-MEMBER 39-40 IAW SRM 51-25-02. (M)
- [SDR SIMA200209416](https://openairdocs.org/sdr/SIMA200209416), Mar 27, 2002: ATTACH FITTING. CORRODED. DURING CPCP4 INSPECTION, FOUND RIGHT FORWARD CARGO LOWER PANEL ATTACH FITTINGS CORRODED. REPLACED RIGHT FORWARD LOWER CARGO ATTACH FITTINGS IAW ATR 42 SRM 51-25
- [SDR SIMA200209415](https://openairdocs.org/sdr/SIMA200209415), Mar 27, 2002: ACCESS PANEL. CORRODED. SAW - DURING CPCP4 INSPECTION, FOUND OVERWING ACCESS PANELS CORRODED. REPLACED OVERWING ACCESS PANELS IAW ATR42 JIC 57-00-00OAC10000-012. (M)
- [SDR SIMA200209414](https://openairdocs.org/sdr/SIMA200209414), Mar 27, 2002: CARGO TRACK. CORRODED. SAW - DURING CPCP4 INSPECTION, FOUND AFT CARGO SEAT TRACKS TO BE CORRODED. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M)
- [SDR SIMA200209413](https://openairdocs.org/sdr/SIMA200209413), Mar 27, 2002: FLOOR SUPPORT. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND LEFT FLOOR SUPPORT BETWEEN 39-40 CORRODED. REPLACED FLOOR SUPPORT BETWEEN 39-40 IAW SRM 51-25-02. (M)
- [SDR SIMA200209412](https://openairdocs.org/sdr/SIMA200209412), Mar 27, 2002: ANGLE. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND LEFT Z-MEMBER CORRODED. REPLACED LEFT Z-MEMBER IAW ATR42 SRM 51-25-02. (M)
- [SDR SIMA200209426](https://openairdocs.org/sdr/SIMA200209426), Mar 27, 2002: LINK. CORRODED. SAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK FITTINGS ON WING IS CORRODED. REPLACED WING FITTINGS FOR RIGHT AILERON DUAL LOAD PATH LINK IAW 
- [SDR SIMA200209425](https://openairdocs.org/sdr/SIMA200209425), Mar 27, 2002: FRAME. CORRODED. MBV - FOUND DURING INSPECTION, FRAME 45 CORRODED BETWEEN STRINGER 18L AND 20 R. INSTALLED NEW SHEER TIE ON FRAME 45 BETWEEN STRINGER 18L AND 20R IAW ATR-42 SRM 
- [SDR SIMA200209424](https://openairdocs.org/sdr/SIMA200209424), Mar 27, 2002: LINK. CORRODED. SAW - DURING INSPECTION, FOUND RIGHT AILERON DUAL LOAD PATH LINK CORRODED. REPLACED RIGHT AILERON DUAL LOAD PATH LINK IAW ATR-42 JIC 27-11-72 RAI 10000-002. (M)
- [SDR SIMA200209423](https://openairdocs.org/sdr/SIMA200209423), Mar 27, 2002: FITTING. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND PAX DOOR SILL PLATE FORWARD TEE FITTING CORRODED. REPLACED PAX DOOR FORWARD TEE FITTING IAW SRM 51-25-03. (M)
- [SDR SIMA200209422](https://openairdocs.org/sdr/SIMA200209422), Mar 27, 2002: VENTURI. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND LAVATORY VENTURI TUBE CORRODED. REPLACED LAVATORY VENTURI TUBE IAW SRM 51-25-02. (M)
- [SDR SIMA200209421](https://openairdocs.org/sdr/SIMA200209421), Mar 27, 2002: FITTING. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND PAX DOOR SILL PLATE AFT TEE FITTINGS CORRODED. REPLACED AFT TEE FITTINGS ON PAX DOOR SILL PLATE IAW SRM 51-25-04. (M)
- [SDR SIMA200209420](https://openairdocs.org/sdr/SIMA200209420), Mar 27, 2002: DOOR FRAME. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND FRAME ON PAX DOOR ABOVE VENT DOOR CORRODED. REPLACED FRAME ON PASSENGER DOOR IAW SRM 51-25-02 AND 51-25-03. (M)
- [SDR SIMA200209408](https://openairdocs.org/sdr/SIMA200209408), Mar 21, 2002: STRINGER. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND STRINGER 17R TO BE CORRODED. REPLACED STRINGER 17R IAW ATR 42 SRM 51-25-02. (M)
- [SDR SIMA200209407](https://openairdocs.org/sdr/SIMA200209407), Mar 21, 2002: SEAT TRACK. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND LEFT MID INBOARD AND LEFT FORWARD OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACKS IAW EO E1-53MR-271. (M)
- [SDR SIMA200209406](https://openairdocs.org/sdr/SIMA200209406), Mar 21, 2002: FLOORBEAM. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND FLOORBEAM 40 TO BE CORRODED. REPLACED FLOORBEAM 40 IAW ATR 42 SRM 51-25-02. (M)
- [SDR SIMA200209405](https://openairdocs.org/sdr/SIMA200209405), Mar 21, 2002: DOOR. CORRODED. SAW - DURING CPCP8 INSPECTION, AFT AVIONICS COMPARTMENT DOOR HAS CORROSION AROUND CIRCUMFERENCE. REPLACED AFT AVIONICS COMPARTMENT DOOR IAW ATR 42 STANDARD PRAC
- [SDR SIMA200209404](https://openairdocs.org/sdr/SIMA200209404), Mar 21, 2002: ATTACH ANGLE. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND PASSENGER DOOR LOWER ATTACH ANGLE FOR STEP SHELL IS CORRODED BEYOND LIMITS. REPLACED PASSENGER DOOR LOWER ATTACH ANGLE IAW 
- [SDR SIMA200209403](https://openairdocs.org/sdr/SIMA200209403), Mar 21, 2002: SKIN. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND AIRFRAME CUTOUT FOR AFT AVIONICS DOOR IS CORRODED BEYOND LIMITS. REPLACED CUTOUT REINFORCING IAW ATR42 SRM 51-25-02. (M)
- [SDR SIMA200209402](https://openairdocs.org/sdr/SIMA200209402), Mar 21, 2002: FLOORBEAM. CORRODED. SAW - DURING CPCP2 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 TO BE CORRODED BEYOND LIMITS. REPLACED FLOORBEAMS IAW ATR 42 SRM 51-25-02. (M)
- [SDR SIMA200209401](https://openairdocs.org/sdr/SIMA200209401), Mar 21, 2002: SEAT TRACK. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND RIGHT FORWARD OUTBOARD, RIGHT FORWARD INBOARD, LEFT FORWARD INBOARD, RIGHT MID OUTBOARD, RIGHT MID INBOARD, LEFT MID OUTBOA
- [SDR SIMA200209411](https://openairdocs.org/sdr/SIMA200209411), Feb 27, 2002: BULKHEAD. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND GROUNDING POINTS TO RADOME ON FORWARD PRESSURE BULKHEAD HAVE PITTING CORROSION. REPAIRED LOWER RIGHT GROUNDING POINT ON FOR
- [SDR SIMA200209410](https://openairdocs.org/sdr/SIMA200209410), Feb 27, 2002: ATTACH FITTING. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND FORWARD CARGO DRAIN TRACK ATTACH PLATE CORRODED. REPLACED FORWARD CARGO DRAIN TRACK ATTACHED PLATE IAW SRM 51-25-02. (M)
- [SDR SIMA200209409](https://openairdocs.org/sdr/SIMA200209409), Feb 27, 2002: TRACK. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND FORWARD CARGO DRAIN TRACK CORRODED. REPLACED FORWARD CARGO DRAIN TRACK IAW SRM 51-25-02. (M)
- [SDR SIMA200210025](https://openairdocs.org/sdr/SIMA200210025), Feb 27, 2002: ANGLE. CORRODED. SAW - DURING CPCP8 INSPECTION, FOUND RIGHT WING REAR SPAR UPPER SPAR ANGLE TO BE CORRODED JUST OUTBOARD OF INBOARD AILERON HINGE. REPAIRED IAW ATR FAX DO/TE/S56
- [SDR SIMA200127705](https://openairdocs.org/sdr/SIMA200127705), Oct 2, 2001: LIGHT. INOPERATIVE. MIA - FLT 5037 - FOUND CABIN DOOR STEP EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY IAW ATR 42 AMM. (M)
- [SDR SIMA200121501](https://openairdocs.org/sdr/SIMA200121501), Aug 3, 2001: MODULE. FAULTY. FLL - FLT 5419 - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED THE SMELL OF SMOKE FOLLOWED BY VISIBLE SMOKE IN CABIN. CREW COMPLIED WITH AIR CONDITION SMOKE PROCE
- [SDR SIMA200120203](https://openairdocs.org/sdr/SIMA200120203), Jul 21, 2001: BATTERY PACK. DISCHARGED. MIA - FLT 5247 - CREW REPORTED THE PASSENGER DOOR EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN POWER SUPPLY UNIT 15W
- [SDR SIMA200118501](https://openairdocs.org/sdr/SIMA200118501), Jul 4, 2001: LIGHT. INOPERATIVE. MIA - MAINTENANCE REPORTED THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPERATIONAL CHE
- [SDR SIMA2892](https://openairdocs.org/sdr/SIMA2892), Oct 15, 2000: SOCKET. DIRTY. NAS - EXTERNAL EMERGENCY LIGHT IN PASSENGER DOOR IS INOPERATIVE. MAINTENANCE CLEANED LIGHT SOCKET. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR SIMA1662](https://openairdocs.org/sdr/SIMA1662), Jun 14, 2000: BATTERY. INOPERATIVE. SAW - DURING PS-2 CHECK, FOUND EMERGENCY LIGHTS BATTERY PACK AT 18WL INOPERATIVE. REMOVED AND REPLACED BATTERY IAW JIC 335121-RAI-10000. OPS CHECK GOOD. (M)
- [SDR SIMA1535](https://openairdocs.org/sdr/SIMA1535), Jun 1, 2000: SEAT TRACK. CORRODED. SAW - DURING MBV-1 INSPECTION, FOUND RIGHT AFT INBOARD AND RIGHT AFT OUTBOARD SEAT TRACKS (P/N S53678001202, S53678001201) CORRODED BEYOND LIMITS. REMOVED AND R
- [SDR SIMA1534](https://openairdocs.org/sdr/SIMA1534), Jun 1, 2000: PLATE. CORRODED. SAW - DURING MBV-1 INSPECTION, FOUND LOWER KEEL BEAM PLATE BETWEEN FRAMES 25A AND 27A CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED KEEL BEAM PLATE IAW 
- [SDR SIMA1533](https://openairdocs.org/sdr/SIMA1533), Jun 1, 2000: GUIDE. CORRODED. SAW - DURING MBV-1 INSPECTION, FOUND RIGHT OUTBOARD FLAP INBOARD DEFLECTOR ALL THREE CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED CAM GUIDES
- [SDR SIMA1532](https://openairdocs.org/sdr/SIMA1532), Jun 1, 2000: ANGLE. CORRODED. SAW - DURING MBV-1 INSPECTION, FOUND RIGHT AFT CARGO ZEE MEMBER CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ZEE MEMBER IAW SRM 51-25-03. (X)

All 66: https://openairdocs.org/aircraft/N319AM/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (168, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Aviat A-1B)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA11177SC](https://openairdocs.org/stc/SA11177SC): Installation of a Hartzell Propeller Inc. model HC-C2YR-IN/NG8301-3 propeller. Hartzell Propeller LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA02396AK](https://openairdocs.org/stc/SA02396AK): Replacement of Sky International Inc. landing gear strut assemblies with Floats Alaska, LLC. +3 extended gear, part numbers 45017-501HD-3X and 45017-502HD-3X. Seaplanes North LLC
- [STC SA02589AK](https://openairdocs.org/stc/SA02589AK): Installation of the Hartzell Model 3C1-R430A1/80C01 Propeller. Momentum Aeronautics Holdings LLC
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02765SE](https://openairdocs.org/stc/SA02765SE): Installation of Acme Stinger tailwheel landing gear shock absorber. Acme Suspensions LLC
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA01416SE](https://openairdocs.org/stc/SA01416SE): Installation of a butterfly valve in the oil cooler inlet duct. Westview Aviation LLC
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA01606CH](https://openairdocs.org/stc/SA01606CH): Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA02838CH](https://openairdocs.org/stc/SA02838CH): Installation of Wipaire Skis Main Wheel Skis Model C2200. F.Atlee Dodge Aircraft Services
- [STC SA3-423](https://openairdocs.org/stc/SA3-423): Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. F.Atlee Dodge Aircraft Services
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA02023CH](https://openairdocs.org/stc/SA02023CH): Installation of an MT-Propeller model MTV-15-B/210-58 and spinner assembly P-277-B. McFarlane Aviation LLC
- [STC SA02870CH](https://openairdocs.org/stc/SA02870CH): Installation of MT Propeller, model MTV-9-B/(198-200) -52, MTV-9-B-C-R-M/CR 198-200-52, MTV-15-B-C-R-M/CR 210-58, MTV-15-B/(205-210)-58, MTV-15-B/203-52 and MTV-15-B-C-R-M/CR-203-52, with matching spinner. McFarlane Aviation LLC
- [STC SA02568AK](https://openairdocs.org/stc/SA02568AK): Installation of Airframes Alaska Aluminum Lift Struts. Airframes Alaska LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA01721CH](https://openairdocs.org/stc/SA01721CH): Installation of Baumann Model BF2150A floats per Baumann Drawing List BF-2150A-01, Rev B, dtd 9/19/02 or later FAA approved revisions. Baumann Floats LLC
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA02288AK](https://openairdocs.org/stc/SA02288AK): Installation of Alpha Omega Suspension System (AOSS) in place of original bungees. Burl's Aircraft LLC
- [STC SA02153AK](https://openairdocs.org/stc/SA02153AK): Installation of Burl's Aircraft Rebuild Magnum I tail wheel Penetration ski. Burl's Aircraft Rebuild LLC
- [STC SA03819NY](https://openairdocs.org/stc/SA03819NY): Installation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH
- [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies

All 168: https://openairdocs.org/aircraft/N319AM/stcs.md

## Related

- Other Aviat A-1B aircraft: https://openairdocs.org/model/aviat-a-1b/aircraft.md
- The Lycoming O-360-A1P engine: https://openairdocs.org/engine/lycoming-o-360-a1p.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.