# N742AS: 1975 Cessna 337G

- Status: Valid registration
- Airframe: [Cessna 337G](https://openairdocs.org/model/cessna-337g) (registry code 2075730, 6 seats)
- Engine: [Continental IO-360 series](https://openairdocs.org/engine/continental-io-360-series) (registry code 17025)
- Data sheets: [TCDS A6CE](https://openairdocs.org/tcds/A6CE) (Textron Aviation Inc.), [TCDS E1CE](https://openairdocs.org/tcds/E1CE) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 33701646
- Year built: 1975
- Type: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: May 13, 1975
- Certificate issued: November 4, 2022
- Expires: November 30, 2029
- Mode S code: A9FA09
- Registered owner: [A2g International LLC](https://openairdocs.org/faa-owner/A2G%20INTERNATIONAL%20LLC)
- Location: [San Juan Capo, CA](https://openairdocs.org/faa-place/CA/San%20Juan%20Capo)
- Owner type: LLC
- Owner's area on the map: 33.4998° N, 117.6537° W: Placed by OpenAirDocs at the center of ZIP code 92675, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=742AS
- Page: https://openairdocs.org/aircraft/N742AS

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. The registry lists only the engine series, so ADs for every Continental IO-360 model are included.

## ADs that may apply (OpenAirDocs): 42 in force

### Matched by airframe (Cessna 337G)

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [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 2011-15-11](https://openairdocs.org/ad/2011-15-11): Wings · Nineteen and a half(19.5 U.S.) gallons wing tip fuel tank (Flint Aero STC SA5090NM). Effective Sep 6, 2011
- [AD 2011-10-09](https://openairdocs.org/ad/2011-10-09): Seat Rails and Roller Housing Inspections · Cessna 150A, 150B, 150C and 221 more. Effective Jun 17, 2011
- [AD 2010-21-18](https://openairdocs.org/ad/2010-21-18): Wings · Wing tip extension fuel tanks (Aviation Enterprises STC SA02055AT or 3 others). Effective Nov 3, 2010
- [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009
- [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 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 2000-06-01](https://openairdocs.org/ad/2000-06-01): Fuel Strainer Assembly · Cessna 150F, 150G, 150H and 163 more. Effective May 5, 2000
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988
- [AD 78-09-05](https://openairdocs.org/ad/78-09-05): Wing Spar Caps and Web Doublers · Cessna 336, 337, 337A and 16 more. Effective May 11, 1978
- [AD 77-12-08](https://openairdocs.org/ad/77-12-08): External Electrical Ground Power Receptacle · Cessna 172M, 172N, 177B and 19 more. Effective Jun 27, 1977
- [AD 77-08-05](https://openairdocs.org/ad/77-08-05): Single Engine Takeoffs · Cessna 337, 337A, 337B and 15 more. Effective Apr 28, 1977
- [AD 76-04-03](https://openairdocs.org/ad/76-04-03): ARC PA-500A Actuators · Cessna 172L, 172M, 177B and 43 more. Effective Feb 26, 1976
- [AD 75-09-05](https://openairdocs.org/ad/75-09-05): Pitot System · Drooped ailerons in flaps down mode, recontoured wing leading… (Sierra Industries STC SA1627WE). Effective Apr 22, 1975
- [AD 72-23-03](https://openairdocs.org/ad/72-23-03): Wing Flap Actuator · Cessna 336, 337, 337A and 7 more. Effective Nov 10, 1972
- [AD 71-17-08](https://openairdocs.org/ad/71-17-08): Rear Engine Stoppage On Take Off · Cessna 337, 337A, 337B and 6 more. Effective Aug 24, 1971

### Matched by engine (Continental IO-360 series)

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [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 2011-26-07](https://openairdocs.org/ad/2011-26-07): Engine · Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jan 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 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 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 98-19-02](https://openairdocs.org/ad/98-19-02): Piston Pins · Continental Motors IO-360-A, IO-360-AB, IO-360-C and 31 more. Effective Nov 9, 1998
- [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 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998
- [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 92-04-09](https://openairdocs.org/ad/92-04-09): Rocker Shaft Hold Down Stud · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 41 more. Effective Jun 22, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988
- [AD 81-13-10 R1](https://openairdocs.org/ad/81-13-10-R1): Oil Pressure · Continental Motors IO-360-A, IO-360-AB, IO-360-C and 28 more. Effective Nov 20, 1981
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981
- [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 70-14-07](https://openairdocs.org/ad/70-14-07): Fuel Injection Pump · Continental Motors IO-360-A, IO-360-C, IO-360-D and 25 more. Effective Nov 22, 1974
- [AD 74-18-07](https://openairdocs.org/ad/74-18-07): Cylinder · Continental Motors IO-360-A, IO-360-C, IO-360-D and 3 more. Effective Aug 28, 1974
- [AD 72-24-03](https://openairdocs.org/ad/72-24-03): Oil Filter Adapter · Continental Motors IO-360-A, IO-520-B, IO-520-C and 3 more. Effective Nov 15, 1972

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

- [AD 87-20-03 R2](https://openairdocs.org/ad/87-20-03-R2) (historical): Seat Tracks · Cessna 150A, 150B, 150C and 212 more. Effective Sep 24, 1990
- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2022-04-04](https://openairdocs.org/ad/2022-04-04) (historical): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Mar 29, 2022
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [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 2002-13-04](https://openairdocs.org/ad/2002-13-04) (historical): Magneto impulse coupling stop pin · Teledyne Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jul 12, 2002
- [AD 2000-11-51](https://openairdocs.org/ad/2000-11-51) (historical): Magnetos · Teledyne Continental Motors IO-360 Series (all), LTSIO-520-AE, O-300-A and 21 more
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more

## Information bulletins (advisory) (17 in force)

- [SAIB CE-13-27R1](https://openairdocs.org/saib/CE-13-27R1): Flight Controls  Frayed Flap Extend Cables. Issued Jan 5, 2022
- [SAIB AIR-21-16](https://openairdocs.org/saib/AIR-21-16): FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection. Issued Aug 26, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls  Loose Glide Screw. Issued Aug 9, 2012
- [SAIB CE-12-24R1](https://openairdocs.org/saib/CE-12-24R1): Flight Controls  Frayed Flap Extend Cables. Issued May 21, 2012
- [SAIB CE-12-14](https://openairdocs.org/saib/CE-12-14): Three Alternative Methods of Compliance for AD 2011-10-09. Issued Jan 25, 2012
- [SAIB CE-10-40R1](https://openairdocs.org/saib/CE-10-40R1): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 30, 2010
- [SAIB CE-10-20R1](https://openairdocs.org/saib/CE-10-20R1): Wing Structure; Wingtip Extensions. Issued May 12, 2010
- [SAIB CE-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009
- [SAIB CE-09-10](https://openairdocs.org/saib/CE-09-10): Availability of Secondary Seat Stops for Pilot and Copilot Seats. Issued Feb 5, 2009
- [SAIB CE-01-41R2](https://openairdocs.org/saib/CE-01-41R2): Flight Controls. Issued Oct 1, 2007
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009
- [SAIB CE-02-09](https://openairdocs.org/saib/CE-02-09): . Issued Dec 28, 2001
- [SAIB CE-12-24](https://openairdocs.org/saib/CE-12-24) (historical): Flight Controls  Frayed Flap Extend Cables. Issued Apr 6, 2012
- [SAIB CE-10-20](https://openairdocs.org/saib/CE-10-20) (historical): Wing Structure; Wingtip Extensions. Issued Mar 16, 2010
- [SAIB CE-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007

## NTSB investigations

None matched to N742AS.

## FAA accident and incident reports

None matched to N742AS.

## Reports on N742AS not matched to an aircraft (2)

They name N742AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19890811047739I](https://openairdocs.org/incident/19890811047739I), Aug 11, 1989: Boeing 737290C (N742AS), Deadhorse, AK. State truck on right side of runway while landing. Afs unaware of vehicle position. Truck checking for caribou.
- [Incident 19880314041539I](https://openairdocs.org/incident/19880314041539I), Mar 14, 1988: Boeing 737290C (N742AS), Juneau, AK. Unable to raise nose gear after takeoff. Diverted. Failure of a hydraulic line kept pilot from raising gear.

## 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 N742AS not matched to an aircraft (548, newest 50)

They name N742AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ASAA0711531](https://openairdocs.org/sdr/ASAA0711531), Mar 13, 2007: MODULE. INOPERATIVE. L1, R1 AND HATCH COVER EMERGENCY EXIT MARKER LIGHTS OUT. REPLACED MODULE M7331. OPS NORMAL.
- [SDR ASAA0711513](https://openairdocs.org/sdr/ASAA0711513), Mar 12, 2007: MODULE. INOPERATIVE. L1 & R1 AND HATCH COVER EMERGENCY EXIT MARKER LIGHTS OUT. REPLACED MODULE M7331, OPS NORMAL.
- [SDR ASAA0611293](https://openairdocs.org/sdr/ASAA0611293), Dec 1, 2006: BATTERY. DISCHARGED. SMOKE BARRIER NR 8 EMERGENCY EXIT LIGHT BATTERY LOW. REPLACED BATTERY PER AMM.
- [SDR ASAA0610648](https://openairdocs.org/sdr/ASAA0610648), May 30, 2006: LIGHT. INOPERATIVE. L1 EMERGENCY LIGHT INOP. INSTALLED SERVICABLE EXIT LIGHT ABOVE L1 DOOR PER AMM.
- [SDR ASAA0610608](https://openairdocs.org/sdr/ASAA0610608), May 18, 2006: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHT ADJACENT TO AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY PACK AT BS 950 PER AMM.
- [SDR ASAA0610587](https://openairdocs.org/sdr/ASAA0610587), May 12, 2006: BATTERY. DISCHARGED. AFTER RECON SMOKE BARRIER EMERGENCY LIGHT INOP DURING TEST. REPLACED SMOKE BARRIRER EXIT SIGN EMERGENCY LIGHT BATTERY.
- [SDR ASAA0610442](https://openairdocs.org/sdr/ASAA0610442), Apr 11, 2006: REPAIR. NONE. TIME LIMITED SKIN REPAIR. REPAIRED PER ASA EA 5330 02075
- [SDR ASAA0610424](https://openairdocs.org/sdr/ASAA0610424), Apr 11, 2006: REPAIR. NONE. TIME LIMITED REPAIR. REPAIRED PER ASA EA 5330 02075.
- [SDR ASAA0610445](https://openairdocs.org/sdr/ASAA0610445), Apr 11, 2006: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED. REPLACED FLOORBEAM PER EA 5310 02602 AND ERO 5606.
- [SDR ASAA0610444](https://openairdocs.org/sdr/ASAA0610444), Apr 11, 2006: FRAME. CORRODED. FOUND FRAME CORRODED. REPAIRED FRAME PER SRM 53 10 4 FIG 6.
- [SDR ASAA0610443](https://openairdocs.org/sdr/ASAA0610443), Apr 11, 2006: STRINGER. CRACKED. FOUND CRACKED STRINGER. REPLACED STRINGER WITH FABRICATED REPAIR PART PER SRM 51 30 05 AND ASA EA 5310 02583.
- [SDR ASAA0610440](https://openairdocs.org/sdr/ASAA0610440), Apr 11, 2006: FRAME. CORRODED. FOUND FRAME CORRODED UNDER STRINGER LOWER LOBE FUSELAGE. REPAIRED PER SRM 51 40 3 FIG 1.
- [SDR ASAA0610436](https://openairdocs.org/sdr/ASAA0610436), Apr 11, 2006: FRAME. CORRODED. FOUND FRAME CORRODED. REPAIRED FRAME PER SRM 53 10 4 FIG 6.
- [SDR ASAA0610435](https://openairdocs.org/sdr/ASAA0610435), Apr 11, 2006: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED. REPAIRED PER SRM 53 10 1 FIG 1 AND 51 30 7 REF NRC 4926376.
- [SDR ASAA0610434](https://openairdocs.org/sdr/ASAA0610434), Apr 11, 2006: FRAME. CRACKED. FOUND FRAME TO SKIN WEB CRACKED REPAIRED PER SRM 53 10 4 FIG 10.
- [SDR ASAA0610433](https://openairdocs.org/sdr/ASAA0610433), Apr 11, 2006: SPLICE. CORRODED. FOUND FRAME SPLICE CORRODED. REPLACED FRAME SPLICE PER SRM 53 10 1 FIG 1.
- [SDR ASAA0610431](https://openairdocs.org/sdr/ASAA0610431), Apr 11, 2006: TIE CLIP. CRACKED. FOUND PASSENGER CABIN TIE CLIP CRACKED. REPLACED PER SRM 51 30 02 AND 53 10 01 FIG 1.
- [SDR ASAA0610430](https://openairdocs.org/sdr/ASAA0610430), Apr 11, 2006: FRAME. CRACKED. FOUND MAIN CARGO DOOR INTERIOR FRAME TO SKIN WEB CRACKED. REPAIRED PER SRM 53 10 4 FIG 10.
- [SDR ASAA0610429](https://openairdocs.org/sdr/ASAA0610429), Apr 11, 2006: FRAME. CORRODED. FOUND MAIN CARGO DOOR FRAME TO SILL WEB IS CORRODED. REPAIRED PER SRM 51 40 3 FIG 1.
- [SDR ASAA0610428](https://openairdocs.org/sdr/ASAA0610428), Apr 11, 2006: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED. REPAIRED FLOORBEAM PER SRM 51 30 02 AND ASA EA 5310 02601
- [SDR ASAA0610426](https://openairdocs.org/sdr/ASAA0610426), Apr 11, 2006: STRINGER. CRACKED. FOUND STRINGER CRACKED. REPAIRED CRACKED STRINGER PER SRM 53 10 3 FIG 1.
- [SDR ASAA0610422](https://openairdocs.org/sdr/ASAA0610422), Apr 11, 2006: DOOR FRAME. CRACKED. FOUND MAIN CARGO DOOR CRACKED 6" BELOW HINGE AT FRAME LIGHTING HOLE TO INBD EDGE. REPAIRED PER ERO 5682 AND EA 5310 02608.
- [SDR ASAA0610421](https://openairdocs.org/sdr/ASAA0610421), Apr 11, 2006: CLIP. CRACKED. FOUND PASSENGER CABIN INTERIOR TIE CLIP CRACKED. REPLACED TIE CLIP PER 51 30 02 AND 53 10 1 FIG 1.
- [SDR ASAA0610420](https://openairdocs.org/sdr/ASAA0610420), Apr 11, 2006: FLOORBEAM. CORRODED. FOUND FLOORBEAM IS CORRODED. REPLACED UPPER FLOORBEAM PER EA 5310 02602.
- [SDR ASAA0610419](https://openairdocs.org/sdr/ASAA0610419), Apr 11, 2006: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK BEAM. REPLACED SEAT TRACK BEAM PER EA 5310 02604.
- [SDR ASAA0610418](https://openairdocs.org/sdr/ASAA0610418), Apr 11, 2006: STRINGER. CORRODED. FOUND STRINGER CORRODED. REPAIRED PER SRM 53-10-03.
- [SDR ASAA0610417](https://openairdocs.org/sdr/ASAA0610417), Apr 11, 2006: FLOOR SUPPORT. CORRODED. FOUND MAIN DECK FLOOR ACROSS I BEAM FOUND CORRODED. REPAIRED IAW SRM 53 10 01.
- [SDR ASAA0610441](https://openairdocs.org/sdr/ASAA0610441), Apr 11, 2006: FLOORBEAM. CRACKED. FOUND FLOORBEAM CORRODED. REPLACED FLOORBEAM IAW EA 5310 02602 AND ERO 5606.
- [SDR ASAA0610439](https://openairdocs.org/sdr/ASAA0610439), Apr 11, 2006: STRINGER. CRACKED. FOUND STRINGER CRACKED AT GND FASTENER HOLES. REPAIRED PER ERO 5373 AND EA 5310 02599.
- [SDR ASAA0610438](https://openairdocs.org/sdr/ASAA0610438), Apr 11, 2006: TIE CLIP. CORRODED. FOUND TIE CLIP CORRODED. REPLACED TIE CLIP PER SRM 51 30 02 AND 51 30 05.
- [SDR ASAA0610437](https://openairdocs.org/sdr/ASAA0610437), Apr 11, 2006: TIE CLIP. CRACKED. TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51 30 02.
- [SDR ASAA0610432](https://openairdocs.org/sdr/ASAA0610432), Apr 11, 2006: TIE CLIP. CRACKED. FOUND TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51 30 02 FIG 11.
- [SDR ASAA0610427](https://openairdocs.org/sdr/ASAA0610427), Apr 11, 2006: STRINGER. CRACKED. FOUND STRINGER CRACKED. REPLACED CRACKED STRINGER IAW SRM 53 10 3 ERO 5735 AND EA5360 01056.
- [SDR ASAA0610425](https://openairdocs.org/sdr/ASAA0610425), Apr 11, 2006: SUPPORT BRACKET. CORRODED. FOUND L2 DOOR SILL ANGLE CORRODED. REPLACED SILL CHORD ANGLE SUPPORT BRACKET PER SRM 51 30 2.
- [SDR ASAA0610423](https://openairdocs.org/sdr/ASAA0610423), Apr 11, 2006: TIE CLIP. CRACKED. FOUND PASSENGER CABIN INTERIOR TIE CLIP CRACKED. REPLACED CRACKED TIE CLIP PER SRM 51 30 05 FIG 4 AND 51 30 2 PARA 7D.
- [SDR ASAA0610406](https://openairdocs.org/sdr/ASAA0610406), Apr 7, 2006: SKIN. DENTED. FOUND FUSELAGE SKIN DENTED. REPAIRED PER SRM 53 30 3 FIG 23.
- [SDR ASAA0610405](https://openairdocs.org/sdr/ASAA0610405), Apr 7, 2006: STRINGER. CORRODED. FOUND STRINGER CORRODED. STRINGER REPAIRED PER EA 5310 02574.
- [SDR ASAA0610404](https://openairdocs.org/sdr/ASAA0610404), Apr 7, 2006: FRAME. CORRODED. FOUND FRAME CORRODED UNDER STRINGER. REPAIRED PER SRM 51 40 3 FIG 1.
- [SDR ASAA0610403](https://openairdocs.org/sdr/ASAA0610403), Apr 7, 2006: STRINGER. CRACKED. FOUND STRINGER CRACKED AT FASTENER HOLE. REPAIRED STRINGER PER EA 5310 02599 AND ERO 5373.
- [SDR ASAA0610402](https://openairdocs.org/sdr/ASAA0610402), Apr 7, 2006: FRAME. CORRODED. FOUND FRAME CORRODED. REPAIRED FRAME PER SRM 53 10 4 FIG 6.
- [SDR ASAA0610401](https://openairdocs.org/sdr/ASAA0610401), Apr 7, 2006: FLOOR SUPPORT. CORRODED. FOUND FLOOR SUPPORT CORRODED. REPLACED PER SRM 53 10 01 FIG 1 AND 51 30 7 REF NRC #4926376.
- [SDR ASAA0610399](https://openairdocs.org/sdr/ASAA0610399), Apr 7, 2006: FRAME. CORRODED. FOUND FRAME SPLICE CORRODED. REPLACED SPLICE PER SRM 53 10 1 FIG 1.
- [SDR ASAA0610398](https://openairdocs.org/sdr/ASAA0610398), Apr 7, 2006: STRINGER CLIP. CRACKED. FOUND TIE CLIP CRACKED. REPLACED PER SRM 51 30 02 FIG 11.
- [SDR ASAA0610397](https://openairdocs.org/sdr/ASAA0610397), Apr 7, 2006: STRINGER CLIP. CRACKED. FOUND TIE CLIP CRACKED. REPLACED PER SRM 51 30 02 ANS 53 10 01 FIG 1.
- [SDR ASAA0610392](https://openairdocs.org/sdr/ASAA0610392), Apr 5, 2006: SKIN. GOUGED. FOUND MAIN CARGO DOOR SKIN AT NR 5 HINGE GOUGED. BLENDED OUT GOUGE PER ERO 5327 AND EA 5230 01310.
- [SDR ASAA0610391](https://openairdocs.org/sdr/ASAA0610391), Apr 5, 2006: SKIN. GOUGED. FOUND MAIN CARGO DOOR SKIN AT NR 6 HINGE ATTACH AREA GOUGED. REPAIRED PER ERO 5327 AND EA 5230 01310.
- [SDR ASAA0610394](https://openairdocs.org/sdr/ASAA0610394), Apr 5, 2006: SKIN. GOUGED. FOUND MAIN CARGO DOOR SKIN AT NR 4 HINGE ATTACH AREA GOUGED. BLENDED OUT GOUGE PER ERO 5327 AND EA 5230 01310.
- [SDR ASAA0610382](https://openairdocs.org/sdr/ASAA0610382), Apr 4, 2006: ATTACH FITTING. NICKED. LT STAB CTR SECTION AFT SPAR UPPER FWD ATTACH LUG FACE NICKED. BLENDED LUG IAW ERO 5334 PARTS 1 16 AND EA 5510 01235.
- [SDR ASAA0610383](https://openairdocs.org/sdr/ASAA0610383), Apr 4, 2006: STRINGER. GOUGED. FOUND STRINGER GOUGED. REPAIRED IAW SRM 53 10 3 AND EA 5360 01054.
- [SDR ASAA0610379](https://openairdocs.org/sdr/ASAA0610379), Apr 4, 2006: STRINGER. GOUGED. FOUND STRINGER GOUGED REPAIRED PER SRM 53 10 3 FIG 1.

All 548: https://openairdocs.org/aircraft/N742AS/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (230, 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 (Cessna 337G)

- [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 SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists 337 Series
- [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 SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [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 SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Aero-Mach Wilco LLC
- [STC SA2821CE](https://openairdocs.org/stc/SA2821CE): Installation of wing tips. Curry Aviation LLC
- [STC SA937CE](https://openairdocs.org/stc/SA937CE): Installation of leading edge cuffs, stall fences, droop wing tips, and vortex generators on rear engine lower cowling. Curry Aviation LLC
- [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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA09120AC-D](https://openairdocs.org/stc/SA09120AC-D): Installation of S-TEC System 55/55X Two Axis automatic flight guidance system, Model ST-603. S-TEC Corporation
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC ST02307CH](https://openairdocs.org/stc/ST02307CH): Installation of Rudder Pedal Extensions. Flight Boss Ltd
- [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA2858SO](https://openairdocs.org/stc/SA2858SO): Installation of a FLIR airborne surveilance system. Air USA Inc
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc
- [STC SA1205CE](https://openairdocs.org/stc/SA1205CE): Installation of King KFC-200 2-axis(3 optional) flight control system with a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller. Honeywell International Inc
- [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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA32RM](https://openairdocs.org/stc/SA32RM): Installation of electrically driven freon air-conditioning system. Air Comm Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments

All 230: https://openairdocs.org/aircraft/N742AS/stcs.md

## Related

- Other Cessna 337G aircraft: https://openairdocs.org/model/cessna-337g/aircraft.md
- The Continental IO-360 series engine: https://openairdocs.org/engine/continental-io-360-series.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.