# N358CA: 1989 Piper PA-28-161 - Status: Valid registration - Airframe: [Piper PA-28-161](https://openairdocs.org/model/piper-pa-28-161) (registry code 7102803, 4 seats) - Engine: [Lycoming O-320-D3G](https://openairdocs.org/engine/lycoming-o-320-d3g) (registry code 42156) - Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13) (Piper Aircraft Inc.), [TCDS E-274](https://openairdocs.org/tcds/E-274) (Lycoming Engines) (OpenAirDocs) - Serial number: 2841283 - Year built: 1989 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, normal, utility - Airworthiness date: January 28, 2011 - Certificate issued: July 13, 2015 - Expires: July 31, 2028 - Mode S code: A402B8 - Registered owner: [Freeman Braxton L](https://openairdocs.org/faa-owner/FREEMAN%20BRAXTON%20L) - Location: [West Lebanon, NH](https://openairdocs.org/faa-place/NH/West%20Lebanon) - Owner type: Individual - Owner's area on the map: 43.6383° N, 72.3065° W: Placed by OpenAirDocs at the center of ZIP code 03784, 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=358CA - Page: https://openairdocs.org/aircraft/N358CA 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): 50 in force ### Matched by airframe (Piper PA-28-161) - [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024 - [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 2020-26-16](https://openairdocs.org/ad/2020-26-16): Wing Spar · Piper PA-28-151, PA-28-161, PA-28-181 and 12 more. Effective Feb 16, 2021 - [AD 2018-07-03](https://openairdocs.org/ad/2018-07-03): Placard and Markings · Piper PA-28-140, PA-28-150, PA-28-151 and 12 more. Effective Apr 20, 2018 - [AD 2017-14-04](https://openairdocs.org/ad/2017-14-04): Engine Oil · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Aug 15, 2017 - [AD 2016-07-21](https://openairdocs.org/ad/2016-07-21): Wing Ribs/Bulkhead · Piper PA-28-161, PA-28-181 and PA-28R-201. Effective Apr 26, 2016 - [AD 2013-02-13](https://openairdocs.org/ad/2013-02-13): Stabilizer Control System · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Mar 11, 2013 - [AD 2010-26-04](https://openairdocs.org/ad/2010-26-04): Engine · Piper PA-28-161 with STC SA03303AT. Effective Feb 1, 2011 - [AD 2010-15-10](https://openairdocs.org/ad/2010-15-10): Control wheel shafts · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Aug 31, 2010 - [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009 - [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 2005-19-20](https://openairdocs.org/ad/2005-19-20): Bushing screw thread expanders · Piper PA-28-160, PA-28-161, PA-28-180 and 1 more. Effective Nov 4, 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 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [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 99-26-05](https://openairdocs.org/ad/99-26-05): Induction Air Filter · Lavia Argentina PA-25, PA-25-235, PA-25-260 and 5 more. Effective Jan 13, 2000 - [AD 96-10-03](https://openairdocs.org/ad/96-10-03): Flap Handle Attach Bolt · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jun 14, 1996 - [AD 87-08-08 R3](https://openairdocs.org/ad/87-08-08-R3): Lower spar cap · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective May 22, 1989 - [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986 - [AD 81-23-05](https://openairdocs.org/ad/81-23-05): Seat Springs and Battery Box · Piper PA-28-151 and PA-28-161. Effective Mar 8, 1982 - [AD 80-14-03](https://openairdocs.org/ad/80-14-03): Bendix, King or Narco Transmitters · Piper PA-28-161, PA-28-181, PA-28-201T and 16 more. Effective Jul 1, 1980 - [AD 79-26-05](https://openairdocs.org/ad/79-26-05): Oil and Fuel System Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jan 3, 1980 - [AD 79-22-02](https://openairdocs.org/ad/79-22-02): Fuel Leakage · Piper PA-28-161, PA-28-181, PA-28-201T and 6 more. Effective Oct 26, 1979 - [AD 79-13-03](https://openairdocs.org/ad/79-13-03): Fire Hazard Prevention · Piper PA-28-161, PA-28-181, PA-28-201T and 5 more. Effective Jun 8, 1979 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 - [AD 79-02-05](https://openairdocs.org/ad/79-02-05): Fuel Flow · Piper PA-28-161, PA-28R-201 and PA-28R-201T. Effective Jan 29, 1979 - [AD 77-23-03](https://openairdocs.org/ad/77-23-03): Rod End Bearings · Piper PA-28-140, PA-28-151, PA-28-161 and 12 more. Effective Nov 14, 1977 ### Matched by engine (Lycoming O-320-D3G) - [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 2012-03-07](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 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 98-17-11](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 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 98-01-06](https://openairdocs.org/ad/98-01-06): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Feb 13, 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 93-19-04](https://openairdocs.org/ad/93-19-04): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Oct 18, 1993 - [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 90-04-06 R1](https://openairdocs.org/ad/90-04-06-R1): Propeller Governor External Oil Line · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 427 more. Effective May 28, 1991 - [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 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 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 ### Historical (superseded or no longer in force) - [AD 2018-02-05](https://openairdocs.org/ad/2018-02-05) (historical): Placard and Markings · Piper PA-28-140, PA-28-150, PA-28-151 and 12 more. Effective Feb 7, 2018 - [AD 2015-20-13](https://openairdocs.org/ad/2015-20-13) (historical): Wing Ribs/Bulkhead · Piper PA-28-161, PA-28-181 and PA-28R-201. Effective Oct 29, 2015 - [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008 - [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008 - [AD 95-26-13](https://openairdocs.org/ad/95-26-13) (historical): Inspect Oil Cooler Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Feb 5, 1996 - [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) (22 in force) - [SAIB 2022-20](https://openairdocs.org/saib/2022-20): Wing Spar. Issued Oct 19, 2022 - [SAIB AIR-21-10](https://openairdocs.org/saib/AIR-21-10): Wing, Attach Fittings (JASC 5740). Issued Jun 29, 2021 - [SAIB AIR-21-07](https://openairdocs.org/saib/AIR-21-07): WING SPAR, Verification of Correct Washers used with Wing Spar Attach Bolts. Issued Mar 30, 2021 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-11-12R1](https://openairdocs.org/saib/CE-11-12R1): Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Dec 2, 2015 - [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014 - [SAIB CE-11-42](https://openairdocs.org/saib/CE-11-42): Flight Controls: Control Cable/Pulley Inspections. Issued Jun 29, 2011 - [SAIB CE-11-14](https://openairdocs.org/saib/CE-11-14): Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point Corrosion. Issued Jan 5, 2011 - [SAIB CE-11-13](https://openairdocs.org/saib/CE-11-13): Wings - Piper PA-28, PA-32, PA-34 Forward Spar Corrosion. Issued Jan 5, 2011 - [SAIB CE-11-11](https://openairdocs.org/saib/CE-11-11): Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting Corrosion. Issued Jan 5, 2011 - [SAIB CE-11-10](https://openairdocs.org/saib/CE-11-10): Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and Ribs. Issued Jan 5, 2011 - [SAIB CE-11-01](https://openairdocs.org/saib/CE-11-01): Stabilizers -Horizontal Stabilator Turnbuckle. Issued Oct 4, 2010 - [SAIB CE-09-23](https://openairdocs.org/saib/CE-09-23): Fuel: Piper PA-28, PA-32, PA-34. Issued Apr 7, 2009 - [SAIB CE-09-17](https://openairdocs.org/saib/CE-09-17): Fuel: Piper PA-28 Series Aircraft Fuel Vent and Supply Hose Condition. Issued Mar 10, 2009 - [SAIB CE-08-13](https://openairdocs.org/saib/CE-08-13): Electrical Power. Issued Feb 27, 2008 - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006 - [SAIB CE-01-30](https://openairdocs.org/saib/CE-01-30): . Issued Jul 11, 2001 - [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 CE-11-12](https://openairdocs.org/saib/CE-11-12) (historical): PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Jan 5, 2011 - [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 N358CA. ## FAA accident and incident reports (1) 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 20110611011309I](https://openairdocs.org/incident/20110611011309I), Jun 11, 2011: Piper PA-28-161 (N358CA), Merritt Island, FL, Minor damage. [privacy data omitted] (A student pilot-med cert # [privacy data omitted]) was on a solo flight performing full stop landings and takeoffs on runway 11 at 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 N358CA not matched to an aircraft (44) They name N358CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR PLGA990204](https://openairdocs.org/sdr/PLGA990204), Feb 4, 1999: CTOT. FAILED. ALB - FLT 6262 - DURING TAKEOFF, CTOT FAILED TO ARM AND TAKEOFF WAS ABORTED. MAINTENANCE COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR PLGA980330A](https://openairdocs.org/sdr/PLGA980330A), Mar 30, 1998: CONTROL VALVE. FAILED. BOS - FLT 4414 - CREW RECEIVED THE RIGHT DUCT OVERTEMP WARNING WHILE IN FLIGHT. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT BLEED AIR. WARNING LIGHT REMAIN - [SDR COMA9730015](https://openairdocs.org/sdr/COMA9730015), Mar 19, 1997: CONTACTS. DIRTY. AUTO COARSEN SYSTEM DID NOT ARM DURING TAKEOFF. COULD NOT DUPLICATE. CLEANED CONTAMINATION FROM P3 ARMING SWITCH CONNECTIONS, SYSTEM TEST NORMAL. - [SDR COMA9730011](https://openairdocs.org/sdr/COMA9730011), Feb 3, 1997: CONTROL CABLE. WORN. NOSE WHEEL STEERING FAILED. REPLACED WORN STEERING CABLE ASSY. - [SDR COMA9730008](https://openairdocs.org/sdr/COMA9730008), Jan 27, 1997: ADC. FAILED. PILOT'S AIR SPEED INDICATION FAILED. REPLACED THE AIR DATA COMPUTER. PART TOTAL CYCLES, 18,369. - [SDR COMA9730002](https://openairdocs.org/sdr/COMA9730002), Jan 11, 1997: P3 SWITCH. INOPERATIVE. AUTO COARSEN LIGHT DID NOT ILLUMINATE ON TAKEOFF OR SUBSEQUENT GROUND RUN-UP. REPLACED BOTH LEFT AND RIGHT P3 SWITCHES, OPERATIONAL CHECK GOOD. - [SDR COMA9630159](https://openairdocs.org/sdr/COMA9630159), Nov 12, 1996: B NUT. LOOSE. AUTO COARSEN WOULD NOT ARM ON TAKEOFF. ABORTED TAKEOFF. FOUND LOOSE B-NUT ON LT ENG. P3 SWITCH, TIGHTEN B-NUT. OPS CHECK GOOD. - [SDR COMA9630157](https://openairdocs.org/sdr/COMA9630157), Nov 6, 1996: PCU. MALFUNCTIONED. LEFT PROPELLER RPM INDICATES 1380 DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. 4 RPM IS TOO MINUTE TO PERCEIVE ON THE ANALOG TYPE RPM INDICATOR. THE PROPELL - [SDR COMA9630144](https://openairdocs.org/sdr/COMA9630144), Sep 17, 1996: ACTUATOR. MALFUNCTIONED. THE STANDBY PITCH TRIM OPERATES WHEN ONLY HALF OF THE TRIM SWITCH IS ACTIVATED. REPLACED THE PITCH TRIM ACTUATOR. - [SDR COMA9630142](https://openairdocs.org/sdr/COMA9630142), Aug 25, 1996: WEU. MALFUNCTIONED. CONFIGURATION WARNING ACTIVATED WHEN POWER ADVANCED FOR TAKEOFF. REPLACED THE WARNING ELECTRONIC UNIT. - [SDR COMA9630113](https://openairdocs.org/sdr/COMA9630113), May 21, 1996: PWR DISTR UNIT. FAILED. RT MAIN ELECTRIC BUS OFF LINE, GENERATOR WOULD NOT RESET. REPLACED THE LT POWER DISTRIBUTION UNIT. - [SDR COMA9630105](https://openairdocs.org/sdr/COMA9630105), Apr 25, 1996: ENGINE. MALFUNCTIONED. LEFT ENGINE OVER TEMP WARNING DURING TAKEOFF ROLL. REPLACED THE LEFT ENGINE. - [SDR COMA9630102](https://openairdocs.org/sdr/COMA9630102), Apr 13, 1996: ITT INDICATOR. DEFECTIVE. RT ENGINE ITT INDICATED 947 DEGREE DURING TAKEOFF. REPLACED THE RT ITT INDICATOR. - [SDR COMA9630100](https://openairdocs.org/sdr/COMA9630100), Apr 8, 1996: BUSHING. FAILED. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE AND BUSHING HAD SPUN. - [SDR COMA9630054](https://openairdocs.org/sdr/COMA9630054), Mar 6, 1996: OVERHEAT LIGHT. ILLUMINATED. LEFT ENGINE TAIL PIPE HOT WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. FOUND NO DEFECTS WITH AIRCRAFT OR TAIL PIPE HOT WARNING SYSTEM. SUBMITTER STATED CAUS - [SDR COMA9630045](https://openairdocs.org/sdr/COMA9630045), Feb 28, 1996: BEARING. SEIZED. AILERON CONTROL MOVEMENT IS EXTREMELY STIFF ON GROUND AND IN FLIGHT. FOUND THE RT INBD AILERON BELL CRANK TO HAVE FROZEN BEARINGS. REPLACED THE CRANK ASSY. - [SDR COMA9630037](https://openairdocs.org/sdr/COMA9630037), Feb 11, 1996: FUSE. FAILED. RT BATTERY BUS IS INOP. REPLACED 200 AMP FUSE AT RT POWER DISTRIBUTION UNIT. - [SDR COMA9630034](https://openairdocs.org/sdr/COMA9630034), Feb 9, 1996: DNLOCK ROLLER. SEIZED. WHEN LANDING GEAR SELECTED DOWN, THE NLG INTRANSIT LIGHT REMAINED ON. REPLACED SEIZED DOWN LOCK ROLLER ON NLG. - [SDR COMA9630033](https://openairdocs.org/sdr/COMA9630033), Feb 7, 1996: WEU. DEFECTIVE. LEFT ENGINE INTAKE HEAT FAIL LIGHT CAME ON DURING FLIGHT. REPLACED DEFECTIVE WARNING ELECTRONIC UNIT. - [SDR COMA9630026](https://openairdocs.org/sdr/COMA9630026), Jan 29, 1996: TQ INDICATION. MALFUNCTIONED. THE RT ENGINE TORQUE INDICATOR WENT FULL DEFLECTION DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY DURING MAINTENANCE RUNS AND ACFT RETURNED TO SERVICE. - [SDR COMA9630021](https://openairdocs.org/sdr/COMA9630021), Jan 21, 1996: WINDSHIELD. NOT SEALED. COPILOTS WINDSHIELD SQUEALS DURING FLIGHT. REPLACED COPILOTS WINDSHIELD. - [SDR COMA9630018](https://openairdocs.org/sdr/COMA9630018), Jan 17, 1996: WEU. MALFUNCTIONED. DURING TAKEOFF, LEFT ENGINE TAIL PIPE HOT WARNING CAME ON. REPLACED THE WARNING ELECTRONIC UNIT. - [SDR COMA9630016](https://openairdocs.org/sdr/COMA9630016), Jan 16, 1996: INLET HEAT. FAILED. LEFT ENGINE INLET HEAT FAIL LIGHT ILLUMINATED. RED GLOW SEEN IN INTAKE. REPLACED THE LEFT LOWER INLET DUCT. - [SDR COMA9630002](https://openairdocs.org/sdr/COMA9630002), Jan 1, 1996: FIRE DETECTOR. DIRTY. LEFT ENGINE TAIL PIPE HOT WARNING SHORTLY AFTER TAKEOFF. CLEANED TAIL PIPE FIRE DETECTORS AND FOUND NO DEFECTS. ACFT RETURNED TO SERVICE. - [SDR COMA9531221](https://openairdocs.org/sdr/COMA9531221), Dec 19, 1995: ITT TRIMMER. DEFECTIVE. LEFT ENGINE ITT INDICATION FLUCTUATES, RETURNED TO CVG FOR REPAIR. REPLACED THE ITT TRIMMER. - [SDR COMA9531210](https://openairdocs.org/sdr/COMA9531210), Dec 16, 1995: BEARINGS. SEIZED. WITH FLAPS AT 35 DEGREES, THE ELEVATORS REQUIRE EXCESSIVE CONTROL TO FORCE BOTH NOSE DOWN AND NOSE UP DURING FLARE. REPLACED SEIZED BEARINGS ON LEFT ELEVATOR TR - [SDR COMA9531211](https://openairdocs.org/sdr/COMA9531211), Dec 14, 1995: OVERHEAT IND. ACTIVATED. LEFT TAIL PIPE HOT WARNING AFTER TAKEOFF. ENGINE SECURED AND ACFT RETURNED TO FIELD. COULD NOT DUPLICATE DISCREPANCY. GROUND RUN AT 100 PERCENT POWER FOR 10 MIN - [SDR COMA9531190](https://openairdocs.org/sdr/COMA9531190), Nov 11, 1995: COMPRESSOR. DAMAGED. LEFT ENGINE IS MAKING A HIGH PITCHED WHINE DURING TAKEOFF. FOUND COMPRESSOR TO HAVE FOD DAMAGE, REPLACED ENGINE. - [SDR COMA9531189](https://openairdocs.org/sdr/COMA9531189), Nov 7, 1995: AOA VANE. DEFECTIVE. THE LEFT ALPHA LIGHT ILLUMINATED DURING FLIGHT. REPLACED THE LEFT AOA VANE. - [SDR COMA9531160](https://openairdocs.org/sdr/COMA9531160), Sep 20, 1995: STARTER GEN. FAILED. DURING START SEQUENCE, THE LEFT ENGINE DOES NOT ROTATE. REPLACED THE LT ENGINE STARTER/GENERATOR. - [SDR COMA9531154](https://openairdocs.org/sdr/COMA9531154), Sep 16, 1995: WINDSHIELD. BIRD STRIKE. BIRD STRIKE ON RT WINDSHIELD AREA. PERFORMED BIRD STRIKE INSPECTION IAW INSPECTION PROGRAM, NO DEFECTS FOUND AND AIRCRAFT RETURNED TO SERVICE. - [SDR COM31142](https://openairdocs.org/sdr/COM31142), Aug 25, 1995: CONTROL SYSTEM. OUT OF ADJUST. FLAP WARNING ON CWP ACTIVATED. RIGGED THE FLAP CONTROL SYSTEM IAW M/M SPECIFICATIONS AND AIRCRAFT TO SERVICE. - [SDR COM31126](https://openairdocs.org/sdr/COM31126), Jul 28, 1995: AIR DATA COMP. DEFECTIVE. INFLIGHT LOST FLIGHT DIRECTOR BARS, RECEIVED RED FLIGHT DIRECTOR WARNING. REPLACED THE AIR DATA COMPUTER. - [SDR COM31116](https://openairdocs.org/sdr/COM31116), Jul 12, 1995: RELAY. FAILED. HYDRAULIC PUMP FAILED. REPLACED RELAY 7LM. - [SDR COM31113](https://openairdocs.org/sdr/COM31113), Jul 5, 1995: DUCT ASSY. CRACKED. LEFT BLEED LEAK WARNING ACTIVATED. REPLACED CRACKED BLEED AIR DUCT AT LEFT WING ROOT. - [SDR COM31102](https://openairdocs.org/sdr/COM31102), Jun 8, 1995: WIRE. BROKEN. LEFT ENGINE WILL NOT START, NO ROTATION. REPAIRED BROKEN WIRE AT RELAY 83PC AND ENGINE STARTS NORMAL. - [SDR COM31082](https://openairdocs.org/sdr/COM31082), May 17, 1995: INNER RACE. SPUN. MECHANIC REMOVED WHEEL FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR R - [SDR COM31071](https://openairdocs.org/sdr/COM31071), May 1, 1995: INNER RACE. SPUN. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION, FOUND INNER RACE HAD SPUN. WHEEL SUBASSY HAS BEEN REMOVED AND SENT TO - [SDR COM31048](https://openairdocs.org/sdr/COM31048), Mar 14, 1995: TRUNNION BEARING. DIRTY. LOUD SQUEAL FROM NLG DURING EXTENSION OR RETRACTION. CLEANED NLG TRUNNION BEARINGS AND SQUEALING NOISE STOPPED. - [SDR COM31043](https://openairdocs.org/sdr/COM31043), Mar 12, 1995: PRESS SWITCH. DEFECTIVE. RECEIVED AUTO COARSEN WARNING DURING TAKEOFF. REPLACED THE P3 PRESSURE SWITCHES. - [SDR COM31039](https://openairdocs.org/sdr/COM31039), Mar 1, 1995: PA CRADLE ASSY. ODOR. TOXIC SMELL IN COCKPIT. REPLACED THE CABIN PA SYSTEM CRADLE ASSY. - [SDR COM31035](https://openairdocs.org/sdr/COM31035), Feb 14, 1995: EEL POWER SUPPLY. DISCHARGED. EMERGENCY LIGHTING ABOVE FWD RT EMERGENCY EXIT IS INOP. REPLACED BATTERY PACK. - [SDR COM31030](https://openairdocs.org/sdr/COM31030), Feb 6, 1995: CABLE ASSY. BINDING. POWER LEVERS ARE DIFFICULT TO MOVE. REPLACED DEFECTIVE SECTIONS OF LT AND RT POWER CONTROL CABLES. LT P/N: C82180-3; RT P/N: C82224-7; RT P/N: C82146-3. - [SDR COM31018](https://openairdocs.org/sdr/COM31018), Jan 18, 1995: COMPUTER. DEFECTIVE. NR 1 AHRS HEADING WAS OFF BY 25 DEGREES. REPLACED THE NR 1 AHC-85. ## STCs that may be installed (OpenAirDocs) (385, 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 (Piper PA-28-161) - [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 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 SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [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 SA02661LA](https://openairdocs.org/stc/SA02661LA): Installation to enlarge the existing main landing gear over-wing access hole in the upper wing skin. M2 Aviation Soultions LLC - [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc - [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc - [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC - [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists PA-28 Series - [STC SA316SO](https://openairdocs.org/stc/SA316SO): Carburetor ice detector. LegacySTC.com. Lists PA-28 Series - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA00037WI](https://openairdocs.org/stc/SA00037WI): Installation of B & C Specialty Products BC100-1 battery. B & C Specialty Products Inc - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels 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 SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument 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 SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC - [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA00060AT](https://openairdocs.org/stc/SA00060AT): Installation of flap gap seals. Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA01038AT](https://openairdocs.org/stc/SA01038AT): Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28, -28R, -32, -32R, -34 series MODELS WITH CONSTANT-CHORD WINGS). Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp - [STC SA2156CE](https://openairdocs.org/stc/SA2156CE): Installation of flap and aileron gap seals. Curry Aviation LLC - [STC SA2230CE](https://openairdocs.org/stc/SA2230CE): Installation of replacement stabilator tips. Curry Aviation LLC - [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes. Aero-Mach Wilco LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA01982AT](https://openairdocs.org/stc/SA01982AT): Installation of new composite wingtip with recognition light. Whelen Aerospace Technologies - [STC SA00028AT](https://openairdocs.org/stc/SA00028AT): Installation of 'speed splitter' flap bracket fairings. Whelen Aerospace Technologies. Lists PA-28 Series - [STC SA04231CH](https://openairdocs.org/stc/SA04231CH): Installation and activation of a TruTrak Vizion autopilot system. Honeywell International Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems 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 All 385: https://openairdocs.org/aircraft/N358CA/stcs.md ## Related - Other Piper PA-28-161 aircraft: https://openairdocs.org/model/piper-pa-28-161/aircraft.md - The Lycoming O-320-D3G engine: https://openairdocs.org/engine/lycoming-o-320-d3g.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.