# N824MA: 1981 Cessna P210N

- Status: Valid registration
- Airframe: [Cessna P210N](https://openairdocs.org/model/cessna-p210n) (registry code 2073454, 6 seats)
- Engine: [Continental TSIO-520 series](https://openairdocs.org/engine/continental-tsio-520-series) (registry code 17040)
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21) (Textron Aviation Inc.), [TCDS E8CE](https://openairdocs.org/tcds/E8CE) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: P21000763
- Year built: 1981
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: October 30, 1981
- Certificate issued: September 2, 2025
- Expires: September 30, 2032
- Mode S code: AB40CB
- Registered owner: [E D Santos & Associates LLC Trustee](https://openairdocs.org/faa-owner/E%20D%20SANTOS%20%26%20ASSOCIATES%20LLC%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: LLC
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=824MA
- Page: https://openairdocs.org/aircraft/N824MA

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 TSIO-520 model are included.

## ADs that may apply (OpenAirDocs): 87 in force

### Matched by airframe (Cessna P210N)

- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 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 2023-02-17](https://openairdocs.org/ad/2023-02-17): Fuselage Main, Structure · Textron 210N, 210R, P210N and 8 more. Effective Mar 20, 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 2012-10-04](https://openairdocs.org/ad/2012-10-04): Wings · Cessna 210G, 210H, 210J and 15 more. Effective Jun 5, 2012
- [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 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 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 2002-07-01](https://openairdocs.org/ad/2002-07-01): Horizontal Stabilizer Attachment Reinforcement Brackets · Cessna 207, 207A, 210G and 32 more. Effective May 13, 2002
- [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 98-21-21 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 98-05-14 R1](https://openairdocs.org/ad/98-05-14-R1): AFM - Limitations Section - Icing · Cessna P210N, P210R and T210N. Effective Sep 22, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 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 94-12-08](https://openairdocs.org/ad/94-12-08): Flight Manual Revision · Cessna 210G, 210H, 210J and 15 more. Effective Jul 22, 1994
- [AD 88-25-04](https://openairdocs.org/ad/88-25-04): AFM/POH Changes - Magneto · Cessna P210N, T210L, T210M and 2 more. Effective Dec 26, 1988
- [AD 88-22-07](https://openairdocs.org/ad/88-22-07): Hose Assemblies · Cessna P210N, P210R, T207 and 22 more. Effective Nov 24, 1988
- [AD 86-24-07](https://openairdocs.org/ad/86-24-07): Engine Controls Installation · Cessna 150C, 150D, 150E and 142 more. Effective Jan 7, 1987
- [AD 86-19-11](https://openairdocs.org/ad/86-19-11): Contaminated Fuel · Cessna 177, 177A, 177B and 83 more. Effective Oct 4, 1986
- [AD 85-11-07 R1](https://openairdocs.org/ad/85-11-07-R1): Turbocharger Oil Reservoir · Cessna P210N, P210R and T210R. Effective Aug 9, 1985
- [AD 85-02-07](https://openairdocs.org/ad/85-02-07): Fuel Selector · Cessna 206, 207, 207A and 45 more. Effective Mar 6, 1985
- [AD 81-23-03 R2](https://openairdocs.org/ad/81-23-03-R2): Engine Exhaust System · Cessna P210N. Effective Nov 15, 1982
- [AD 82-06-10](https://openairdocs.org/ad/82-06-10): Vacuum-Driven-Attitude Instruments · Cessna 210L, 210M, 210N and 5 more. Effective Apr 15, 1982
- [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981
- [AD 81-15-05](https://openairdocs.org/ad/81-15-05): Engine and Airplane Modifications · Cessna P210N. Effective Jul 27, 1981
- [AD 80-21-03](https://openairdocs.org/ad/80-21-03): Roll Axis Flight Control · King Model KFC-200 two axis flight control system (Honeywell International STC SA1202CE or SA1487CE). Effective Oct 23, 1980
- [AD 79-25-07](https://openairdocs.org/ad/79-25-07): Alternator Ground · Cessna 180, 180A, 180B and 95 more. Effective Dec 13, 1979
- [AD 79-19-06](https://openairdocs.org/ad/79-19-06): Fuel Flow System Per STC SA3835WE · Hoskins Model CFS-1000, -1001, FT-100 or FT-101 fuel flow… (Sandia Aerospace STC SA3835WE). Effective Sep 17, 1979
- [AD 79-15-01](https://openairdocs.org/ad/79-15-01): Fuel Flow Distribution · Cessna 206, 206H, 207 and 57 more. Effective Jul 26, 1979
- [AD 78-26-12](https://openairdocs.org/ad/78-26-12): Fuel Quantity System · Cessna 210G, 210H, 210J and 8 more. Effective Jan 4, 1979
- [AD 78-11-05](https://openairdocs.org/ad/78-11-05): Autopilot Actuator · Cessna 210M, 310R, 340A and 9 more. Effective Jun 5, 1978

### Matched by engine (Continental TSIO-520 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 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022
- [AD 2020-16-11](https://openairdocs.org/ad/2020-16-11): SUMMARY: Reciprocating Cylinder Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 23 more. Effective Sep 21, 2020
- [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016
- [AD 2014-05-29](https://openairdocs.org/ad/2014-05-29): SAP replacement parts manufacturer approval (PMA) investment cast cylinder assemblies · Continental Motors TSIO-520-A, TSIO-520-AE, TSIO-520-AF and 55 more. Effective Apr 25, 2014
- [AD 2012-10-13](https://openairdocs.org/ad/2012-10-13): Starter adapters · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Jun 8, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2011-13-03](https://openairdocs.org/ad/2011-13-03): Turbocharger Turbine · Lycoming Engines LTO-360-E1A6D, O-540-L3C5D, TIGO-541-E1A and 20 more. Effective Jul 13, 2011
- [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 2010-07-08](https://openairdocs.org/ad/2010-07-08): Turbochargers · Kelly Aerospace Energy Systems HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 137 more. Effective Apr 19, 2010
- [AD 2009-19-07](https://openairdocs.org/ad/2009-19-07): EQ3 cylinders · Continental Motors IO-470-C, IO-470-D, IO-470-E and 72 more. Effective Oct 7, 2009
- [AD 2008-08-17](https://openairdocs.org/ad/2008-08-17): Turbocharger turbine housing flange and the exhaust tube flange · Teledyne Continental Motors TSIOL-550-A 'Liquid-Cooled' engines (RAM Aircraft Limited Partnership STC SA7633SW or SA7633SW-D). Effective May 6, 2008
- [AD 2007-16-10](https://openairdocs.org/ad/2007-16-10): Kelly Aerospace Power Systems turbochargers · Turbonormalizing system (Engine Technologies STC SE10589SC or SA10588SC). Effective Aug 23, 2007
- [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 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004
- [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 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [AD 97-26-17](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 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 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 93-16-15](https://openairdocs.org/ad/93-16-15): Fuel Pump Drive Shaft · Continental Motors IO-520-B, IO-520-BA, IO-520-BB and 27 more. Effective Dec 14, 1993
- [AD 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 1993
- [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 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 89-24-01 R1](https://openairdocs.org/ad/89-24-01-R1): Scavenge Oil Pump Gears · Continental Motors TSIO-520-B, TSIO-520-BB, TSIO-520-D and 11 more. Effective Aug 10, 1990
- [AD 89-24-03](https://openairdocs.org/ad/89-24-03): Turbocharger Inlet Assembly · Continental Motors TSIO-520-UB. Effective Jun 18, 1990
- [AD 89-14-01](https://openairdocs.org/ad/89-14-01): Crankshaft · Continental Motors TSIO-520-BE. Effective Sep 22, 1989
- [AD 88-17-03](https://openairdocs.org/ad/88-17-03): Starter Adapter Shaftgear Assembly · Continental Motors IO-520-BA, IO-520-BB, IO-550-B and 4 more. Effective Aug 10, 1988
- [AD 87-26-08](https://openairdocs.org/ad/87-26-08): Crankshaft and Piston Pins · Continental Motors TSIO-520-BE and TSIO-520-CE. Effective Apr 29, 1988
- [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 86-13-04 R3](https://openairdocs.org/ad/86-13-04-R3): Cylinder Assemblies · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 44 more. Effective Feb 24, 1988
- [AD 87-14-02](https://openairdocs.org/ad/87-14-02): Starter Adapter Shaftgear · Continental Motors IO-520-BA, IO-520-BB, IO-550-B and 4 more. Effective Oct 5, 1987
- [AD 84-25-05](https://openairdocs.org/ad/84-25-05): Turbocharger Oil Scavenge Reservoir · Continental Motors TSIO-520-BE. Effective Mar 4, 1985
- [AD 82-09-01](https://openairdocs.org/ad/82-09-01): Fuel Pressure Regulator Inlet and Outlet · Continental Motors TSIO-520-J, TSIO-520-K, TSIO-520-N and 1 more. Effective Jul 8, 1982
- [AD 81-24-06](https://openairdocs.org/ad/81-24-06): Engine Driven Fuel Pumps · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 51 more. Effective Nov 23, 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 80-22-05](https://openairdocs.org/ad/80-22-05): Crankshaft Front Oil Seal · Continental Motors TSIO-520-M, TSIO-520-P and TSIO-520-R. Effective Oct 24, 1980
- [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 80-01-04](https://openairdocs.org/ad/80-01-04): Cylinder Holddown Flange Assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 44 more. Effective Jan 25, 1980
- [AD 79-05-09](https://openairdocs.org/ad/79-05-09): Oil Pump Assembly Or Oil Pressure Relief Valve Screw And/Or Plunger · Teledyne Continental Motors 6-285-CA, GTSIO-520-C, GTSIO-520-D and 60 more. Effective Mar 12, 1979
- [AD 78-06-01](https://openairdocs.org/ad/78-06-01): Cylinder Intake Tube · Continental Motors TSIO-520-J and TSIO-520-N. Effective Jan 24, 1979
- [AD 77-05-04](https://openairdocs.org/ad/77-05-04): Crankshaft · Continental Motors IO-470-L, IO-520-D, IO-520-F and 6 more. Effective Mar 11, 1977
- [AD 76-13-09](https://openairdocs.org/ad/76-13-09): Left Hand Rear Exhaust Elbow, And Left And Right Hand Flanges · Continental Motors TSIO-520-L. Effective Aug 26, 1976
- [AD 75-09-13](https://openairdocs.org/ad/75-09-13): Turbocharger Oil Inlet Adapter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 9 more. Effective Apr 24, 1975
- [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
- [AD 71-09-03](https://openairdocs.org/ad/71-09-03): Gasket and/or Fuel Leakage · Continental Motors TSIO-360-A, TSIO-520-B, TSIO-520-D and 2 more. Effective Apr 29, 1971
- [AD 70-13-03](https://openairdocs.org/ad/70-13-03): Hydraulic Lock · Continental Motors TSIO-520-C. Effective Jul 2, 1970

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

- [AD 98-05-14](https://openairdocs.org/ad/98-05-14) (historical): Airplane Flight Manual (AFM) - Icing · Cessna P210N, P210R and T210N. Effective Apr 30, 1998
- [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 2011-25-51](https://openairdocs.org/ad/2011-25-51) (historical): Starter Adapter Gear Shaft · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Dec 28, 2011
- [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 2009-16-03](https://openairdocs.org/ad/2009-16-03) (historical): Cylinder assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 55 more. Effective Sep 9, 2009
- [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
- [AD 87-23-08](https://openairdocs.org/ad/87-23-08) (historical): Crankshafts · Teledyne Continental Motors IO-520 Series (all) and TSIO-520 Series (all). Effective Nov 30, 1987
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more

All 99: https://openairdocs.org/aircraft/N824MA/ads.md

## Information bulletins (advisory) (19 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-17-16](https://openairdocs.org/saib/CE-17-16): Main Landing Gear  Actuator Inspection. Issued Jun 9, 2017
- [SAIB CE-13-16](https://openairdocs.org/saib/CE-13-16): Hydraulic Power Pack/Landing Gear System. Issued Feb 8, 2013
- [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls  Loose Glide Screw. Issued Aug 9, 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-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-05-27R1](https://openairdocs.org/saib/CE-05-27R1): Stabilizers. Issued Sep 6, 2007
- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT  Alternator Drive Coupling. Issued Jun 20, 2018
- [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT  Engine damage as a result of kickback. Issued May 10, 2017
- [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-10-07](https://openairdocs.org/saib/NE-10-07): Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.. Issued Nov 2, 2009
- [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009
- [SAIB NE-07-09R1](https://openairdocs.org/saib/NE-07-09R1): Periodic Inspections of ECi Cylinder Assemblies for Cracks in the Aluminum Head. Issued Mar 21, 2007
- [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002

## NTSB investigations

None matched to N824MA.

## FAA accident and incident reports

None matched to N824MA.

## Reports on N824MA not matched to an aircraft (1)

They name N824MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19990210016849I](https://openairdocs.org/incident/19990210016849I), Feb 10, 1999: Dhav DHC8102 (N824MA), Syracuse, NY. (-5)On Wednesday, February 10, 1999, a Dehavilland DHC-8-102, s/n 327, operated by allegheny airlines experienced a warning light in the aft cargo compartment…

## 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 N824MA not matched to an aircraft (33)

They name N824MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MALA976108](https://openairdocs.org/sdr/MALA976108), Apr 26, 1998: INVERTER. FAILED. DURING FLIGHT, THE PRIMARY INVERTER CIRCUIT BREAKER POPPED. CREW RAN QRH ITEMS, RESET CIRCUIT BREAKER PER MAINTENANCE CONTROL, CIRCUIT BREAKER IMMEDIATELY POPPE
- [SDR MALA976073](https://openairdocs.org/sdr/MALA976073), Mar 29, 1998: BATTERY PACK. DISCHARGED. DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHTING IS INOP. MAINTENANCE REPLACED 6 EMERGENCY LIGHT BATTERY PACKS, OPS CHECK GOOD.
- [SDR MALA975841](https://openairdocs.org/sdr/MALA975841), Dec 29, 1997: SIGN. FAILED. DURING INSPECTION, EXIT LIGHT AT ROW 4 INOP. MAINTENANCE REPLACED EXIT SIGN, ALL CHECKS GOOD.
- [SDR MALA975822](https://openairdocs.org/sdr/MALA975822), Dec 20, 1997: BULB. FAILED. DURING INSPECTION, FLOOR TRACK LIGHT, SEAT 4 INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT. ALL CHECKS GOOD.
- [SDR MALA975817](https://openairdocs.org/sdr/MALA975817), Dec 18, 1997: LIGHT. INOPERATIVE. DURING INSPECTION, ONE FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT. ALL CHECKS GOOD.
- [SDR MALA975809](https://openairdocs.org/sdr/MALA975809), Dec 14, 1997: BULB. FAILED. DURING INSPECTION, ONE FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT. ALL CHECKS GOOD.
- [SDR MALA975693](https://openairdocs.org/sdr/MALA975693), Oct 10, 1997: LIGHT. INOPERATIVE. DURING INSPECTION, ONE FORWARD RED EMERGENCY LIGHT INOP. MAINTENANCE REPLACED LAMP MODULE. ALL CHECKS GOOD. (M)
- [SDR MALA975679](https://openairdocs.org/sdr/MALA975679), Sep 30, 1997: LIGHT. INOPERATIVE. DURING INSPECTION, TWO EMERGENCY LIGHTS OUT, ONE FLOOR TRACK, P/N 7239410-802, AND ONE EXIT, P/N 3071BPEGPL. MAINTENANCE RELAMPED BOTH EMERGENCY LIGHTS. ALL CHE
- [SDR 97ZZZM1076](https://openairdocs.org/sdr/97ZZZM1076), Sep 30, 1997: LIGHT. INOPERATIVE. DURING INSPECTION, TWO EMERGENCY LIGHTS OUT, ONE FLOOR TRACK, P/N 7239410-802, AND ONE EXIT, P/N 3071BPEGPL. MAINTENANCE RELAMPED BOTH EMERGENCY LIGHTS. ALL CHE
- [SDR MALA975573](https://openairdocs.org/sdr/MALA975573), Jul 31, 1997: BULB. FAILED. DURING INSPECTION ONE FLOOR PATH LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)
- [SDR MALA975551](https://openairdocs.org/sdr/MALA975551), Jul 23, 1997: BULBS. FAILED. ON INSPECTION, FOUND TWO EMERGENCY FLOOR TRACK LIGHT BULBS INOP. MAINTENANCE REPLACED BULBS. OPS CHECK GOOD. (M)
- [SDR MALA975526](https://openairdocs.org/sdr/MALA975526), Jul 15, 1997: BULB. FAILED. DURING INSPECTION, EXIT SIGN INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)
- [SDR MALA975464](https://openairdocs.org/sdr/MALA975464), Jun 13, 1997: GCU. FAILED. FLT 3003 - DURING FLIGHT, THE RIGHT AC GENERATOR FELL OFF LINE AND WILL NOT RESET. AIRCRAFT RETURNED TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 GCU. OPS CHEC
- [SDR MALA975442](https://openairdocs.org/sdr/MALA975442), Jun 1, 1997: LIGHT ASSEMBLY. INOPERATIVE. DURING INSPECTION, THREE FLOOR EMERGENCY LIGHTS WERE FOUND INOP. MAINTENANCE RELAMPED. FUNCTION CHECK GOOD. (M)
- [SDR MALA975351](https://openairdocs.org/sdr/MALA975351), Mar 14, 1997: TEMP CONTROL. MALFUNCTIONED. FLIGHT 3389 - AFTER DEPARTING DTW, CREW COULD NOT COOL THE DUCT TEMPERATURE BELOW 45 DEGREES USING AUTO OR MANUAL MODE. AIRCRAFT RETURNED TO DTW. MAINTENANCE OP
- [SDR MALA975339](https://openairdocs.org/sdr/MALA975339), Mar 1, 1997: ENGINE. FAILED. FLT 3432 - DURING CLIMB-OUT FROM DTW, RIGHT ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 50 PSI. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK, REDUCED POWER TO F
- [SDR MALA975337](https://openairdocs.org/sdr/MALA975337), Feb 27, 1997: CHECK VALVE. FAILED. FLT 2926 - ON APPROACH INTO DTW, THE LAVATORY SMOKE DETECTOR ACTIVATED AFTER FUMES ENTERED THE CABIN AT REDUCED POWER SETTING, SELECTED BLEEDS OFF, DETECTOR STO
- [SDR MALA975334](https://openairdocs.org/sdr/MALA975334), Feb 26, 1997: CONNECTOR. FAILED. FLT 3098 - OUTBOUND OF DTW, CREW REPORTED RIGHT ELEVATOR HORN HEAT LIGHT ILLUMINATED. RETURNED TO DTW. MAINTENANCE REPAIRED WIRES AND REPLACED CANNON PLUG ON EL
- [SDR MALA975331](https://openairdocs.org/sdr/MALA975331), Feb 24, 1997: ACM. FAILED. FLIGHT 3125 - DURING SHORT FINAL, THE LAVATORY SMOKE DETECTOR WENT OFF. UPON LANDING AND SHUTDOWN, CREW NOTICED A LIGHT MIST IN CABIN. MAINTENANCE REPLACED AIR 
- [SDR MALA975293](https://openairdocs.org/sdr/MALA975293), Jan 18, 1997: GCU. FAILED. FLT 3453 - FOLLOWING LIFTOFF, DC BUS LIGHT ON ANNUNCIATOR PANEL ILLUMINATED. CREW FOLLOWED QUICK REFERENCE PROCEDURES AND RETURNED TO DTW. MAINTENANCE REMOVED A
- [SDR MALA965254](https://openairdocs.org/sdr/MALA965254), Dec 19, 1996: PSEU. FAILED. FLT 3319 - ON CLIMB-OUT FROM DTW, THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE PS
- [SDR MALA965224](https://openairdocs.org/sdr/MALA965224), Nov 29, 1996: HYD LINE. FAILED. FLT NR 3421 - ON CLIMB-OUT, WHEN GEAR WAS SELECTED UP, THE MASTER CAUTION LIGHT, NR 2 ENGINE HYDRAULIC PUMP, OUTBOARD ROLL SPOILER, RUD PRESS NR 2 AND RUD FULL 
- [SDR MALA965210](https://openairdocs.org/sdr/MALA965210), Nov 23, 1996: BRUSH BLOCK. WORN. FLT 3121 - ON CLIMB-OUT FROM MSP, THE RIGHT ELEVATOR HORN HEAT BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT BRUSH BLOCK, P/N
- [SDR 96ZZZX6039](https://openairdocs.org/sdr/96ZZZX6039), Nov 23, 1996: LIMITERS. FAILED. FLT 3121 - ON CLIMB-OUT FROM MSP, THE RIGHT ELEVATOR HORN HEAT BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT BRUSH BLOCK, P/N
- [SDR MALA965203](https://openairdocs.org/sdr/MALA965203), Nov 15, 1996: CONTROLS. FROZEN. FLT 3250 - ON CLIMB-OUT FROM MSP, THE CREW REPORTED THAT THE RUDDER PEDALS WERE FROZEN AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO MSP. AFTER GEAR EXTENSION
- [SDR MALA965202](https://openairdocs.org/sdr/MALA965202), Nov 14, 1996: GCU. MALFUNCTIONED. FLT 3370 - EN ROUTE, THE NR 1 AC GEN LIGHT ILLUNMINATED. THE CREW RESET THE GENERATOR AND THEN THE NR 2 AC BUS, RT HORN, AND RT STALL LIGHTS ILLUMINATED. A FEW 
- [SDR MALA954657](https://openairdocs.org/sdr/MALA954657), Oct 7, 1995: WIRE. LOOSE. FLT R 3157 - DURING THE POST FLIGHT INSPECTION IN DTW, THE CREW NOTED THAT THE AFT CEILING LIGHT AND THE RIGHT FORWARD EXIT LIGHT WERE INOPERATIVE. MAINTENANCE 
- [SDR MALA954580](https://openairdocs.org/sdr/MALA954580), Aug 11, 1995: SKIN. DENTED. BNA - DURING C-CHECK INSPECTION, MAINTENANCE NOTED A DENT IN THE FUSELAGE BETWEEN STR 32R AND STR 31R, STA X167 AND STA X182. REPAIRS WERE COMPLETED BY INSTALLI
- [SDR MALA954536](https://openairdocs.org/sdr/MALA954536), Jul 12, 1995: CONTROL UNIT. FAILED. FLT 3409 - ON APPROACH TO DTW, THE INTRANSIT LIGHT ON THE GEAR HANDLE DID NOT ILLUMINATE UPON GEAR EXTENSION. MAINTENANCE REPLACED THE ADVISORY CONTROL UNIT. SY
- [SDR MALA954456](https://openairdocs.org/sdr/MALA954456), May 15, 1995: SEAL. OUT OF POSITION. DURING A PREFLIGHT WALKAROUND, THE CREW NOTED THAT THE RIGHT GEAR DOORS, CENTER AND AFT, RELEASE INTERMITTENTLY. MAINTENANCE REPOSITIONED THE AFT DOOR SEAL AND 
- [SDR MALA954444](https://openairdocs.org/sdr/MALA954444), May 1, 1995: EEL. FAILED. FLT NR 3320 - DURING THE PREFLIGHT INSPECTION IN DTW, THE CREW REPORTED THAT THE COCKPIT HAND HELD EMERGENCY LAMP ASSEMBLY HAD A LOW CHARGE. MAINTENANCE REPLACE
- [SDR MALA954370](https://openairdocs.org/sdr/MALA954370), Mar 12, 1995: PRESS SWITCH. FAILED. FLT 3130 - ON CLIMB-OUT FROM DTW, THE RUD FULL PRESS LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RUDDE
- [SDR MALA954319](https://openairdocs.org/sdr/MALA954319), Feb 14, 1995: UPLOCK ACT. FAILED. CMX - FLT 3125 - ON APPROACH, LT GEAR DID NOT EXTEND UPON GEAR EXTENSION. THE CREW PERFORMED AN ALTERNATE GEAR EXTENSION AND THE GEAR EXTENDED NORMALLY. THE AIR

## STCs that may be installed (OpenAirDocs) (418, 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 P210N)

- [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 SA2528NM](https://openairdocs.org/stc/SA2528NM): Installation of an air to air intercooler in the engine induction system downstream of the turbocharger. (P210N S/N P21000001 THRU P21000834). Western Skyways Aircraft Modifications 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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [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 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 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 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 SA00925WI](https://openairdocs.org/stc/SA00925WI): Installation of MT-Propeller model MTV-14-D/195-30a hydraulic 4-blade constant speed propeller. MT- Propeller Entwicklung GmbH
- [STC SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly. Radiorax Aviation Systems LLC
- [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 SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC
- [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 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 SA00631WI](https://openairdocs.org/stc/SA00631WI): Installation of additional equipment for approval for flight into icing. CAV Ice Protection 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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Aero-Mach Wilco LLC
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA966CE](https://openairdocs.org/stc/SA966CE): Installation of leading edge cuffs, droop tips, and stall fences. Curry Aviation LLC
- [STC SA01827WI](https://openairdocs.org/stc/SA01827WI): Installation of LED Position Lights. Aero-Mach Wilco LLC
- [STC SA2558CE](https://openairdocs.org/stc/SA2558CE): Replace the lead acid battery with a Concorde RG 24-11M lead acid battery. Aero-Mach Wilco LLC
- [STC SA2749CE](https://openairdocs.org/stc/SA2749CE): Installation of wing mounted convex mirror, for inspection of nose and main landing gear position. Aero-Mach Wilco LLC
- [STC SA52GL](https://openairdocs.org/stc/SA52GL): On all models listed above, except P210N, install Cleveland Wheel & Brake Conversion Kit P/N 199-60. KAMAN Corporation Aircraft Wheel and Brake LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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
- [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 SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA02415CH](https://openairdocs.org/stc/SA02415CH): Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. Flight Boss Ltd
- [STC ST02307CH](https://openairdocs.org/stc/ST02307CH): Installation of Rudder Pedal Extensions. Flight Boss Ltd
- [STC SA2226NM](https://openairdocs.org/stc/SA2226NM): Installation of inflatable door seal. TALCO Aviation Corp
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [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 SA1487CE](https://openairdocs.org/stc/SA1487CE): Installation of King KFC200 Automatic Flight Control System, two axis, with or without flight director. Honeywell International Inc
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc

All 418: https://openairdocs.org/aircraft/N824MA/stcs.md

## Earlier aircraft with N824MA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N824MA before.

- [Cancelled 2010-11-05](https://openairdocs.org/deregistered/N824MA-2010-11-05): Robinson Helicopter R44, S/N 1186, built 2002. Exported to France. Owner: [Aircraft Guaranty Corp Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20GUARANTY%20CORP%20TRUSTEE), [Onalaska, TX](https://openairdocs.org/faa-place/TX/Onalaska)

## Related

- Other Cessna P210N aircraft: https://openairdocs.org/model/cessna-p210n/aircraft.md
- The Continental TSIO-520 series engine: https://openairdocs.org/engine/continental-tsio-520-series.md

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