# Cessna 210L

- Type: Aircraft model (FAA registry)
- Registry code: 2073448
- Manufacturer (registry): CESSNA
- Model: 210L
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 6
- Weight class: Up to 12,499 lb
- Cruise speed: 87 mph
- Certification: Type certificated
- Data sheet: [TCDS 3A21](https://openairdocs.org/tcds/3A21) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 234
- Page: https://openairdocs.org/model/cessna-210l

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [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). Effective Mar 21, 2022
- [AD 2020-03-16](https://openairdocs.org/ad/2020-03-16): Fuselage Main, Structure · Textron 210G, 210H, 210J and 9 more. Effective Mar 9, 2020
- [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 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 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 2005-25-08](https://openairdocs.org/ad/2005-25-08): Electronic Flight Information System (EFIS) · B-N Group BN-2A, 172, 180 and 22 more. Effective Jan 23, 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 98-25-02](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 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 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 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 91-22-01](https://openairdocs.org/ad/91-22-01): Electrical Wires · Cessna 210, 210-5 (205), 210-5A (205A) and 14 more. Effective Nov 4, 1991
- [AD 84-10-01 R1](https://openairdocs.org/ad/84-10-01-R1): Bladder Fuel Cells · Cessna 180, 180A, 180B and 103 more. Effective Jul 5, 1988
- [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 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 85-10-02](https://openairdocs.org/ad/85-10-02): Engine Induction Airbox · Cessna 206, 207, 207A and 24 more. Effective Jun 20, 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 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 80-21-03](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 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979
- [AD 77-16-05](https://openairdocs.org/ad/77-16-05): Fuel Selector Valve · Cessna 206, 206H, 207 and 55 more. Effective Aug 11, 1977
- [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 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 72-07-09](https://openairdocs.org/ad/72-07-09): Cracks And Loose Bolts In Fin & Rudder · Cessna 182, 182A, 182B and 74 more. Effective Oct 17, 1974
- [AD 74-13-06](https://openairdocs.org/ad/74-13-06): Main Wheel Assemblies · Cessna 180J, 210L, A185F and 4 more. Effective Jun 24, 1974
- [AD 74-08-01](https://openairdocs.org/ad/74-08-01): Autopilot Servo Actuators · Aircraft Radio Autopilot Servo Actuators, 172L, 172M and 29 more. Effective Apr 9, 1974
- [AD 69-08-11](https://openairdocs.org/ad/69-08-11): Fuel Boost Pump · Cessna 206, 206H, 210 and 38 more. Effective Apr 22, 1969

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

## Information bulletins (advisory) (12)

- [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 AIR-20-10](https://openairdocs.org/saib/AIR-20-10): AD 2020-03-16 Alternative Methods of Compliance and FAQ. Issued May 29, 2020
- [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-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-09-42](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 CE-05-27R1](https://openairdocs.org/saib/CE-05-27R1): Stabilizers. Issued Sep 6, 2007
- [SAIB CE-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007

## Registered aircraft (234, first 50)

- [N101JH](https://openairdocs.org/aircraft/N101JH): [Hi-Per Aviation Inc](https://openairdocs.org/faa-owner/HI-PER%20AVIATION%20INC), [Arroyo Grande, CA](https://openairdocs.org/faa-place/CA/Arroyo%20Grande), built 1972, S/N 21059759
- [N10242](https://openairdocs.org/aircraft/N10242): [Alexander Holding Services Inc](https://openairdocs.org/faa-owner/ALEXANDER%20HOLDING%20SERVICES%20INC), [Newark, DE](https://openairdocs.org/faa-place/DE/Newark), built 1972, S/N 21059704
- [N10HG](https://openairdocs.org/aircraft/N10HG): [Gerardy Harlan D](https://openairdocs.org/faa-owner/GERARDY%20HARLAN%20D), [Gruver, TX](https://openairdocs.org/faa-place/TX/Gruver), built 1974, S/N 21060169
- [N10HL](https://openairdocs.org/aircraft/N10HL): [Hoyt Robert H Trustee](https://openairdocs.org/faa-owner/HOYT%20ROBERT%20H%20TRUSTEE), [Canby, OR](https://openairdocs.org/faa-place/OR/Canby), built 1975, S/N 21060646
- [N10Y](https://openairdocs.org/aircraft/N10Y): [Seitz William D](https://openairdocs.org/faa-owner/SEITZ%20WILLIAM%20D), [Gordonville, TX](https://openairdocs.org/faa-place/TX/Gordonville), built 1972, S/N 21059697
- [N110YD](https://openairdocs.org/aircraft/N110YD): [Lloyd Clee](https://openairdocs.org/faa-owner/LLOYD%20CLEE), [Canby, OR](https://openairdocs.org/faa-place/OR/Canby), built 1975, S/N 21060858
- [N1110S](https://openairdocs.org/aircraft/N1110S): [Mob Aviation USA LLC](https://openairdocs.org/faa-owner/MOB%20AVIATION%20USA%20LLC), [Kissimmee, FL](https://openairdocs.org/faa-place/FL/Kissimmee), S/N 21061119
- [N115CW](https://openairdocs.org/aircraft/N115CW): [Whitlock Gary D](https://openairdocs.org/faa-owner/WHITLOCK%20GARY%20D), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne), built 1974, S/N 21060520
- [N1190Q](https://openairdocs.org/aircraft/N1190Q): [Britell Andrew Paul](https://openairdocs.org/faa-owner/BRITELL%20ANDREW%20PAUL), [Sandwich, NH](https://openairdocs.org/faa-place/NH/Sandwich), built 1972, S/N 21059690
- [N121CE](https://openairdocs.org/aircraft/N121CE): [Advanced Flight Instruction LLC](https://openairdocs.org/faa-owner/ADVANCED%20FLIGHT%20INSTRUCTION%20LLC), [Greenwood, DE](https://openairdocs.org/faa-place/DE/Greenwood), built 1974, S/N 21060503
- [N123CE](https://openairdocs.org/aircraft/N123CE): [Bas Part Sales LLC](https://openairdocs.org/faa-owner/BAS%20PART%20SALES%20LLC), [Greeley, CO](https://openairdocs.org/faa-place/CO/Greeley), S/N 21061054
- [N12KF](https://openairdocs.org/aircraft/N12KF): [N12kf LLC](https://openairdocs.org/faa-owner/N12KF%20LLC), [Pass Christian, MS](https://openairdocs.org/faa-place/MS/Pass%20Christian), built 1973, S/N 21059853
- [N12PW](https://openairdocs.org/aircraft/N12PW): [Ohio State University College Of Engineering](https://openairdocs.org/faa-owner/OHIO%20STATE%20UNIVERSITY%20COLLEGE%20OF%20ENGINEERING), [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus), built 1972, S/N 21059796
- [N1574P](https://openairdocs.org/aircraft/N1574P): [Southern Seaplane Inc](https://openairdocs.org/faa-owner/SOUTHERN%20SEAPLANE%20INC), [Belle Chasse, LA](https://openairdocs.org/faa-place/LA/Belle%20Chasse), built 1976, S/N 21061258
- [N1609X](https://openairdocs.org/aircraft/N1609X): [Harvey P J](https://openairdocs.org/faa-owner/HARVEY%20P%20J), [Midland, TX](https://openairdocs.org/faa-place/TX/Midland), built 1975, S/N 21060645
- [N1651X](https://openairdocs.org/aircraft/N1651X): [Peters Mark E](https://openairdocs.org/faa-owner/PETERS%20MARK%20E), [Newport News, VA](https://openairdocs.org/faa-place/VA/Newport%20News), built 1975, S/N 21060686
- [N1656X](https://openairdocs.org/aircraft/N1656X): [Anderson George E](https://openairdocs.org/faa-owner/ANDERSON%20GEORGE%20E), [Newnan, GA](https://openairdocs.org/faa-place/GA/Newnan), built 1975, S/N 21060691
- [N1696X](https://openairdocs.org/aircraft/N1696X): [Centurion LLC](https://openairdocs.org/faa-owner/CENTURION%20LLC), [New Bern, NC](https://openairdocs.org/faa-place/NC/New%20Bern), built 1975, S/N 21060731
- [N1698X](https://openairdocs.org/aircraft/N1698X): [Cmo Blue Sky LLC](https://openairdocs.org/faa-owner/CMO%20BLUE%20SKY%20LLC), [Tomball, TX](https://openairdocs.org/faa-place/TX/Tomball), S/N 21060733
- [N1716X](https://openairdocs.org/aircraft/N1716X): [Bell Brian](https://openairdocs.org/faa-owner/BELL%20BRIAN), [Oakland, CA](https://openairdocs.org/faa-place/CA/Oakland), built 1975, S/N 21060738
- [N1720X](https://openairdocs.org/aircraft/N1720X): [Kregel Brian D](https://openairdocs.org/faa-owner/KREGEL%20BRIAN%20D), [Garnavillo, IA](https://openairdocs.org/faa-place/IA/Garnavillo), built 1975, S/N 21060742
- [N1734X](https://openairdocs.org/aircraft/N1734X): [Right Wing Left Wing Flyers LLC](https://openairdocs.org/faa-owner/RIGHT%20WING%20LEFT%20WING%20FLYERS%20LLC), [Cleveland, GA](https://openairdocs.org/faa-place/GA/Cleveland), built 1975, S/N 21060755
- [N1744X](https://openairdocs.org/aircraft/N1744X): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), built 1975, S/N 21060765
- [N1754X](https://openairdocs.org/aircraft/N1754X): [West Alabama Lime Co Inc](https://openairdocs.org/faa-owner/WEST%20ALABAMA%20LIME%20CO%20INC), [Livingston, AL](https://openairdocs.org/faa-place/AL/Livingston), built 1975, S/N 21060775
- [N1763X](https://openairdocs.org/aircraft/N1763X): [Robins Nest Aviation LLC](https://openairdocs.org/faa-owner/ROBINS%20NEST%20AVIATION%20LLC), [Harrison, OH](https://openairdocs.org/faa-place/OH/Harrison), built 1975, S/N 21060784
- [N1764X](https://openairdocs.org/aircraft/N1764X): [Leschber Larry](https://openairdocs.org/faa-owner/LESCHBER%20LARRY), [Hutto, TX](https://openairdocs.org/faa-place/TX/Hutto), built 1975, S/N 21060785
- [N176LL](https://openairdocs.org/aircraft/N176LL): [Clear Above LLC](https://openairdocs.org/faa-owner/CLEAR%20ABOVE%20LLC), [Haymarket, VA](https://openairdocs.org/faa-place/VA/Haymarket), built 1975, S/N 21061135
- [N1770X](https://openairdocs.org/aircraft/N1770X): [Park Avenue Group Inc](https://openairdocs.org/faa-owner/PARK%20AVENUE%20GROUP%20INC), [Stuart, FL](https://openairdocs.org/faa-place/FL/Stuart), built 1975, S/N 21060791
- [N1794X](https://openairdocs.org/aircraft/N1794X): [Gulf Atlantic Airways Inc](https://openairdocs.org/faa-owner/GULF%20ATLANTIC%20AIRWAYS%20INC), [Gainesville, FL](https://openairdocs.org/faa-place/FL/Gainesville), built 1975, S/N 21060814
- [N1797X](https://openairdocs.org/aircraft/N1797X): [N1797x Aero LLC](https://openairdocs.org/faa-owner/N1797X%20AERO%20LLC), [Gulf Breeze, FL](https://openairdocs.org/faa-place/FL/Gulf%20Breeze), built 1975, S/N 21060817
- [N1798X](https://openairdocs.org/aircraft/N1798X): [N1798x LLC](https://openairdocs.org/faa-owner/N1798X%20LLC), [Etna Green, IN](https://openairdocs.org/faa-place/IN/Etna%20Green), built 1975, S/N 21060818
- [N200LD](https://openairdocs.org/aircraft/N200LD): [Fenske Jeffrey D](https://openairdocs.org/faa-owner/FENSKE%20JEFFREY%20D), [Gold Hill, OR](https://openairdocs.org/faa-place/OR/Gold%20Hill), built 1973, S/N 21059895
- [N2029S](https://openairdocs.org/aircraft/N2029S): [Canyon West LLC](https://openairdocs.org/faa-owner/CANYON%20WEST%20LLC), [Amarillo, TX](https://openairdocs.org/faa-place/TX/Amarillo), built 1975, S/N 21060997
- [N2036S](https://openairdocs.org/aircraft/N2036S): [Lissie Flying Service](https://openairdocs.org/faa-owner/LISSIE%20FLYING%20SERVICE), [Lissie, TX](https://openairdocs.org/faa-place/TX/Lissie), built 1975, S/N 21061004
- [N2103S](https://openairdocs.org/aircraft/N2103S): [San Diego Flight Corp](https://openairdocs.org/faa-owner/SAN%20DIEGO%20FLIGHT%20CORP), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego), built 1975, S/N 21061067
- [N2105S](https://openairdocs.org/aircraft/N2105S): [Southport Aviation LLC](https://openairdocs.org/faa-owner/SOUTHPORT%20AVIATION%20LLC), [Cape Coral, FL](https://openairdocs.org/faa-place/FL/Cape%20Coral), built 1976, S/N 21061069
- [N210BJ](https://openairdocs.org/aircraft/N210BJ): [Summers Equipment Leasing Inc](https://openairdocs.org/faa-owner/SUMMERS%20EQUIPMENT%20LEASING%20INC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1974, S/N 21060221
- [N210BN](https://openairdocs.org/aircraft/N210BN): [By Land Air And Sea LLC](https://openairdocs.org/faa-owner/BY%20LAND%20AIR%20AND%20SEA%20LLC), [Alto, MI](https://openairdocs.org/faa-place/MI/Alto), built 1974, S/N 21060526
- [N210BV](https://openairdocs.org/aircraft/N210BV): [Plane Fun Inc Tr Trustee](https://openairdocs.org/faa-owner/PLANE%20FUN%20INC%20TR%20TRUSTEE), [Snellville, GA](https://openairdocs.org/faa-place/GA/Snellville), built 1975, S/N 21061114
- [N210BW](https://openairdocs.org/aircraft/N210BW): [Sc & Dss LLC](https://openairdocs.org/faa-owner/SC%20%26%20DSS%20LLC), [Mckinney, TX](https://openairdocs.org/faa-place/TX/Mckinney), built 1976, S/N 21061483
- [N210BX](https://openairdocs.org/aircraft/N210BX): [Nova Aircraft Holdings Inc](https://openairdocs.org/faa-owner/NOVA%20AIRCRAFT%20HOLDINGS%20INC), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego), built 1972, S/N 21059583
- [N210CH](https://openairdocs.org/aircraft/N210CH): [One Up LLC](https://openairdocs.org/faa-owner/ONE%20UP%20LLC), [Stuttgart, AR](https://openairdocs.org/faa-place/AR/Stuttgart), built 1974, S/N 21060142
- [N210DC](https://openairdocs.org/aircraft/N210DC): [Rrr Land & Cattle Co LLC](https://openairdocs.org/faa-owner/RRR%20LAND%20%26%20CATTLE%20CO%20LLC), [Midland, TX](https://openairdocs.org/faa-place/TX/Midland), built 1973, S/N 21060159
- [N210DD](https://openairdocs.org/aircraft/N210DD): [Dwoskin David F Trustee](https://openairdocs.org/faa-owner/DWOSKIN%20DAVID%20F%20TRUSTEE), [San Pedro, CA](https://openairdocs.org/faa-place/CA/San%20Pedro), built 1976, S/N 21061464
- [N210DG](https://openairdocs.org/aircraft/N210DG): [Washburn Stig K](https://openairdocs.org/faa-owner/WASHBURN%20STIG%20K), [Westminster, MA](https://openairdocs.org/faa-place/MA/Westminster), built 1972, S/N 21059559
- [N210DN](https://openairdocs.org/aircraft/N210DN): [Martin John J](https://openairdocs.org/faa-owner/MARTIN%20JOHN%20J), [Honesdale, PA](https://openairdocs.org/faa-place/PA/Honesdale), S/N 21059676
- [N210FB](https://openairdocs.org/aircraft/N210FB): [Bongard Frederic S](https://openairdocs.org/faa-owner/BONGARD%20FREDERIC%20S), [Torrance, CA](https://openairdocs.org/faa-place/CA/Torrance), built 1974, S/N 21060441
- [N210GA](https://openairdocs.org/aircraft/N210GA): [Twin D LLC](https://openairdocs.org/faa-owner/TWIN%20D%20LLC), [Lake City, FL](https://openairdocs.org/faa-place/FL/Lake%20City), built 1974, S/N 21060480
- [N210GM](https://openairdocs.org/aircraft/N210GM): [Stipe Leslie Wayne](https://openairdocs.org/faa-owner/STIPE%20LESLIE%20WAYNE), [Mcalester, OK](https://openairdocs.org/faa-place/OK/Mcalester), built 1976, S/N 21061393
- [N210GS](https://openairdocs.org/aircraft/N210GS): [Retail Online Solutions Inc](https://openairdocs.org/faa-owner/RETAIL%20ONLINE%20SOLUTIONS%20INC), [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus), built 1976, S/N 21061283

All 234: https://openairdocs.org/model/cessna-210l/aircraft.md

## STCs approved for it (366, first 50)

- [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer.. J P Instruments
- [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 SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc
- [STC SA00161BO (1 OF 3)](https://openairdocs.org/stc/SA00161BO%20(1%20OF%203)): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation
- [STC SA00172WI](https://openairdocs.org/stc/SA00172WI): Installation of TKS anti-icing system components, with placard stating 'Flight into known icing conditions is prohibited.'. CAV Ice Protection Inc
- [STC SA00215NY](https://openairdocs.org/stc/SA00215NY): Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.. CAVU Products Limited
- [STC SA00238SE](https://openairdocs.org/stc/SA00238SE): Installation of Aviation Development Corporation's sump mounted chip detector. Aviation Development Corporation
- [STC SA00243BO (2 OF 5)](https://openairdocs.org/stc/SA00243BO%20(2%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.. Avidyne Corporation
- [STC SA00272WI](https://openairdocs.org/stc/SA00272WI): Replacement of hydraulic system pressure switch.. APPH Wichita Inc.
- [STC SA00274AT](https://openairdocs.org/stc/SA00274AT): Installation of a Teledyne Continental model IO-550L engine and a McCauley model D3A34C402/90DFA-10 or a Hartzell model PHC-J3FY-1RF/F7691 propeller with associated spinner.. John Jewell Aircraft Inc
- [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation
- [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number  700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne 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 SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA00353BO](https://openairdocs.org/stc/SA00353BO): Installation of an auto lean system. Flight Enhancements LLC
- [STC SA00367DE](https://openairdocs.org/stc/SA00367DE): Installation of an Oilamatic Preoiler system.. Oilamatic Inc
- [STC SA00368DE](https://openairdocs.org/stc/SA00368DE): Installation of an Aircraft Noise Control System.. Quiet Flight LLC
- [STC SA00393SE](https://openairdocs.org/stc/SA00393SE): Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System.. Protective Technologies Int
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development Corporation
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA00422WI](https://openairdocs.org/stc/SA00422WI): Installation of McCauley Propeller Model D3A34C402/90DFA -8, -10 and associated changes.. Air Plains Services Corporation
- [STC SA00425DE](https://openairdocs.org/stc/SA00425DE): Installation of model FB-02 'Fixed Arm' Pilot Arm Rest on R/H side of pilot seat and optional GPS Support Arm System.. Quality Aircraft Components LC
- [STC SA00426DE](https://openairdocs.org/stc/SA00426DE): Installation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat.. Quality Aircraft Components LC
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments
- [STC SA00455DE](https://openairdocs.org/stc/SA00455DE): Installation of a large vertical left hand side window and/or an optional Del Air One Passenger Observation Rear Seat Assembly.. Del-Air
- [STC SA00553AT](https://openairdocs.org/stc/SA00553AT): Installation of either a Hartzell model PHC-J3YF-1RF/F7691() or PHC-J3YF-1RF/F8468A() -6R propeller and associated spinner assembly in accordance either Bonaire Aviation Company Propeller Installation Instructions in Cessna 201 Series Aircraft (Continental IO-520L Powered)  dated June 1, 1994, or later FAA approved revision; or John Jewell Aircraft, Inc. Cessna 210 Hartzell PHC-J3YF-1RF/F7691 or PHC-J3YF-1RF/F8468A SA00553AT Installation Manual  dated March 1, 2011, or later FAA approved revision.. John Jewell Aircraft Inc
- [STC SA00606NY](https://openairdocs.org/stc/SA00606NY): Installation of O & N Aircraft Modifications low fuel warning device.. Griggs Aircraft Refinishing LLC
- [STC SA00631WI](https://openairdocs.org/stc/SA00631WI): Installation of additional equipment for approval for flight into icing.. CAV Ice Protection Inc.
- [STC SA00669AT](https://openairdocs.org/stc/SA00669AT): Installation of a replacement auxiliary fuel pump.. C J Aviation
- [STC SA00678SE](https://openairdocs.org/stc/SA00678SE): Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments. J P Instruments
- [STC SA00680SE (3 OF 6](https://openairdocs.org/stc/SA00680SE%20(3%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International
- [STC SA00709LA](https://openairdocs.org/stc/SA00709LA): Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.. Trevor Burward-Hoy
- [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 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 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 SA00773AT](https://openairdocs.org/stc/SA00773AT): Installation of a Hartzell PHC-J3YF-1RF/F7691( ) Model Propeller and C-4582-(P) Spinner. Hartzell Propeller Inc
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA00796AT](https://openairdocs.org/stc/SA00796AT): Installation of a dual-isolator forward engine mount system. Summit Aviation Inc.
- [STC SA00812CH](https://openairdocs.org/stc/SA00812CH): Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies.. Vantage Plane Plastic Ltd
- [STC SA00846WI](https://openairdocs.org/stc/SA00846WI): Installation of B&C Specialty products BC 425-1 standby alternator.. B & C Specialty Products Inc
- [STC SA00855SE](https://openairdocs.org/stc/SA00855SE): Installation of BAS, Inc. duel belt shoulder harness with inertia reel in accordance with BAS Report 1002, dated April 1, 2000, or later FAA approved revision.. BAS Inc
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems 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 SA00941SE](https://openairdocs.org/stc/SA00941SE): Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156, Revision IR, dated April 18, 2001, and Installation Manual MA2157, Revision IR, dated July 3, 2001, or later FAA approved revision to either of these documents. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.. Micro AeroDynamics Inc
- [STC SA00954SE (1 OF 2)](https://openairdocs.org/stc/SA00954SE%20(1%20OF%202)): Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.. J P Instruments
- [STC SA01077SE](https://openairdocs.org/stc/SA01077SE): Installation of fluoropolymer film.. Columbia Pacific Airlines

All 366: https://openairdocs.org/model/cessna-210l/stcs.md

## NTSB investigations (222, newest 50)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB GAA25WA220](https://openairdocs.org/ntsb/GAA25WA220), Jul 29, 2025: Cessna 210L (N1110S), Turks and Caicos Islands, United Kingdom, substantial damage
- [NTSB CEN25FA144](https://openairdocs.org/ntsb/CEN25FA144), Apr 3, 2025: Cessna 210L (N1574P), Raceland, LA, destroyed, 2 fatal, investigation ongoing
- [NTSB ERA24LA186](https://openairdocs.org/ntsb/ERA24LA186), Apr 12, 2024: Cessna 210 (N777NT), Concord, NC, substantial damage. Probable cause: Failure of a landing gear extension system hydraulic hose, which resulted in a landing with the landing gear retracted.
- [NTSB ERA21LA085](https://openairdocs.org/ntsb/ERA21LA085), Dec 21, 2020: Cessna 210L (N2246S), Midway, GA, substantial damage, 1 fatal. Probable cause: The pilot's intentional visual flight rules flight into instrument meteorological conditions, which resulted in controlled flight into terrain. Contributing to the accident was the pressure to…
- [NTSB CEN20LA162](https://openairdocs.org/ntsb/CEN20LA162), Apr 28, 2020: Cessna T210 (N210HH), New Braunfels, TX, substantial damage. Probable cause: The pilot's inadequate preflight inspection and fuel planning, which resulted in the loss of engine power due to fuel exhaustion.
- [NTSB WPR20LA101](https://openairdocs.org/ntsb/WPR20LA101), Mar 5, 2020: Cessna 210 (N123CE), Needles, CA, substantial damage. Probable cause: A loss of engine power for undetermined reasons due to a lack of available evidence.
- [NTSB ERA20LA070](https://openairdocs.org/ntsb/ERA20LA070), Dec 24, 2019: Cessna 210 (N30259), Concord, NC, substantial damage. Probable cause: A malfunction of the left main landing gear brake during landing for undetermined reasons. Contributing was the pilot’s failure to attain a proper touchdown point and maintain an appropriate approach…
- [NTSB WPR19FA250](https://openairdocs.org/ntsb/WPR19FA250), Sep 4, 2019: Cessna 210 (N94262), Henefer, UT, substantial damage, 2 fatal. Probable cause: The pilots’ decision to enter a canyon at low altitude, which resulted in controlled flight into terrain while attempting to exit the canyon.
- [NTSB ERA17LA239](https://openairdocs.org/ntsb/ERA17LA239), Jul 11, 2017: Cessna 210L (N732FJ), Wilkes-Barre/Scranton, PA, substantial damage. Probable cause: Failure of the left landing gear door actuator, which resulted in a loss of all hydraulic pressure and subsequent gear collapse on landing.
- [NTSB GAA17CA128](https://openairdocs.org/ntsb/GAA17CA128), Jan 28, 2017: Cessna 210 (N59196), Charleston, WV, substantial damage. Probable cause: The pilot’s improper landing flare in gusting wind conditions, which resulted in a hard landing and runway excursion.
- [NTSB ERA16LA135](https://openairdocs.org/ntsb/ERA16LA135), Mar 19, 2016: Cessna 210L (N59196), Myrtle Beach, SC, substantial damage. Probable cause: A complete loss of electrical power, which resulted from the separation of an alternator wire due to corrosion. Contributing to the accident was the failure of the emergency landing gear extension…
- [NTSB CEN14LA345](https://openairdocs.org/ntsb/CEN14LA345), Jul 3, 2014: Cessna 210L (N1175Q), Las Vegas, NM, substantial damage. Probable cause: The pilot's loss of airplane control during an aborted landing. Contributing to the accident was the pilot's inadequate preflight planning, which resulted in his attempt to land on a runway closed by…
- [NTSB ERA14FA120](https://openairdocs.org/ntsb/ERA14FA120), Feb 15, 2014: Cessna 210L (N732EJ), Clay, AL, destroyed, 2 fatal. Probable cause: The pilot's failure to maintain control of the airplane while being vectored to intercept the localizer during night instrument meteorological conditions (IMC). Contributing to the accident was the…
- [NTSB ERA14LA051](https://openairdocs.org/ntsb/ERA14LA051), Nov 28, 2013: Cessna 210L (N777BK), Montrose, PA, substantial damage. Probable cause: The pilot’s failure to check the fuel tanks for contaminants after fueling, which resulted in a total loss of engine power due to water contamination.
- [NTSB CEN13LA056](https://openairdocs.org/ntsb/CEN13LA056), Nov 9, 2012: Cessna 210L (N732BL), La Grange, TX, substantial damage. Probable cause: The total loss of engine power due to the loss of oil to the engine. Contributing to the accident was maintenance personnel’s improper installation of the engine oil filter adaptor, which resulted in…
- [NTSB WPR11LA378](https://openairdocs.org/ntsb/WPR11LA378), Aug 13, 2011: Cessna 210L (N732FY), Seattle, WA, substantial damage. Probable cause: A loss of electrical power while on final approach due to a depleted battery, which resulted in an intentional gear-up emergency landing.
- [NTSB CEN10LA389](https://openairdocs.org/ntsb/CEN10LA389), Jul 9, 2010: Cessna 210 (N2157S), Houston, TX, substantial damage. Probable cause: The failure of a hydraulic fluid line, which caused a loss of hydraulic pressure to the landing gear extension system and resulted in the partial collapse of the right main landing gear during…
- [NTSB ERA10LA307](https://openairdocs.org/ntsb/ERA10LA307), Jun 9, 2010: Cessna 210L (N2263S), Tampa, FL, substantial damage. Probable cause: The total loss of engine power due to inadequate torgue on the crankcase bolts. Contributing to the accident was the inadequate inspection performed 19.5 hours prior to the accident.
- [NTSB WPR10LA140](https://openairdocs.org/ntsb/WPR10LA140), Feb 18, 2010: Cessna 210L (N777FW), Aurora, OR, substantial damage. Probable cause: The failure of the landing gear to properly function for undetermined reasons, resulting in the right main landing gear collapsing during landing. Contributing to the accident was the pilot's failure…
- [NTSB MIA08LA066](https://openairdocs.org/ntsb/MIA08LA066), Feb 27, 2008: Cessna 210L (N5489V), Tampa, FL, substantial damage. Probable cause: The malfunction of the right main landing gear down-and-locked switch.
- [NTSB SEA08LA028](https://openairdocs.org/ntsb/SEA08LA028), Nov 16, 2007: Cessna 210L (N987M), Santa Barbara, CA, substantial damage. Probable cause: The left main landing gear's down limit switch plunger being bent and stuck in the closed position, which resulted in the collapse of the landing gear during the landing roll. The reason for the down…
- [NTSB SEA07CA239](https://openairdocs.org/ntsb/SEA07CA239), Aug 25, 2007: Cessna 210L (N75032), Cottage Grove, OR, substantial damage. Probable cause: The loss of engine power for an undetermined reason. A contributing factor was the lack of suitable terrain for the forced landing.
- [NTSB DFW06CA016](https://openairdocs.org/ntsb/DFW06CA016), Oct 26, 2005: Cessna 210L (N59051), Baker, LA, substantial damage. Probable cause: The pilot's failure to maintain clearance during takeoff roll.
- [NTSB DFW05CA135](https://openairdocs.org/ntsb/DFW05CA135), May 25, 2005: Cessna 210L (N5120Q), Harvey, LA, substantial damage. Probable cause: The loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.
- [NTSB DFW05CA124](https://openairdocs.org/ntsb/DFW05CA124), May 15, 2005: Cessna 210L (N1766X), Houston, TX, substantial damage. Probable cause: The pilot's failure to maintain directional control during landing roll. A contributing factor was reported partial loss of brake control.
- [NTSB LAX05FA108](https://openairdocs.org/ntsb/LAX05FA108), Mar 8, 2005: Cessna 210L (N2044S), Oxnard, CA, substantial damage. Probable cause: A pinhole leak in the fuel pressure line during the takeoff roll that was ignited by an electrical arc associated with wires adjacent to the fuel line. A contributing factor in the accident was the…
- [NTSB MIA04CA040](https://openairdocs.org/ntsb/MIA04CA040), Jan 14, 2004: Cessna 210L (N453MC), Fort Meade, FL, substantial damage. Probable cause: The failure of the pilot to abort the takeoff after encountering fog during the preflight and engine run-up, and also his failure to maintain proper alignment with the runway during the takeoff roll…
- [NTSB ATL04LA015](https://openairdocs.org/ntsb/ATL04LA015), Oct 13, 2003: Cessna 210L (N732AG), Hickory, NC, substantial damage. Probable cause: The pilot's failure to maintain airspeed which resulted in a stall.
- [NTSB ATL04TA012](https://openairdocs.org/ntsb/ATL04TA012), Oct 7, 2003: Cessna 210L (N59063), Tallahassee, FL, substantial damage. Probable cause: Loss of engine power due to crankshaft counterweight failure.
- [NTSB NYC03LA128](https://openairdocs.org/ntsb/NYC03LA128), Jun 12, 2003: Cessna 210L (N1198Q), Crisfield, MD, substantial damage. Probable cause: The pilot's inadequate recovery from a bounced landing and his improper flare which resulted in a hard landing. Contributing factors were the windshear and the crosswind.
- [NTSB FTW03LA094](https://openairdocs.org/ntsb/FTW03LA094), Feb 4, 2003: Cessna 210L (N22432), Morrilton, AR, substantial damage. Probable cause: The failure of the main landing gear to extend and lock, as a result of a hydraulic fluid leak caused by a chaffed and ruptured flex line.
- [NTSB FTW03FA057](https://openairdocs.org/ntsb/FTW03FA057), Dec 4, 2002: Cessna 210L (N210CT), Harrison, AR, destroyed, 1 fatal. Probable cause: The pilot's failure to maintain control of the aircraft and the exceedance of the manufactured limits, which resulted in an in flight break-up. Contributing factors were the dark night conditions and…
- [NTSB FTW03FA044](https://openairdocs.org/ntsb/FTW03FA044), Nov 20, 2002: Cessna 210L (N93770), Kentwood, LA, destroyed, 1 fatal. Probable cause: The failure of the #1 and #2 connecting rods during climb to cruise due to overheating, resulting from oil starvation. A contributing factor was the low cloud conditions limiting the pilot's…
- [NTSB NYC03FA020](https://openairdocs.org/ntsb/NYC03FA020), Nov 14, 2002: Cessna 210L (N2444S), Rochester, NY, destroyed, 1 fatal. Probable cause: A loss of engine power for undetermined reasons. A factor in this accident was the night light condition which precluded the pilot's ability to adequately view suitable forced landing areas.
- [NTSB ATL02LA163](https://openairdocs.org/ntsb/ATL02LA163), Aug 30, 2002: Cessna 210L (N32W), Georgetown, SC, substantial damage. Probable cause: The failure of the landing gear to lock in the down position.
- [NTSB CHI02LA251](https://openairdocs.org/ntsb/CHI02LA251), Aug 10, 2002: Cessna 210L (N3UF), Lacon, IL, substantial damage. Probable cause: The pilot's improper in-flight decision to perform an intentional gear-up precautionary landing instead of continuing to the next available airport. A factor to the accident was the corn crop.
- [NTSB SEA02LA141](https://openairdocs.org/ntsb/SEA02LA141), Jul 30, 2002: Cessna 210L (N732EK), Cascade, ID, substantial damage. Probable cause: The pilot's failure to maintain the proper rate of descent on short final resulting in a touchdown short of the runway threshold. Contributing factors were the variable winds and swampy terrain at…
- [NTSB NYC02LA144](https://openairdocs.org/ntsb/NYC02LA144), Jul 22, 2002: Cessna 210L (N732AK), Zelienople, PA, substantial damage. Probable cause: The pilot failure to follow the published aborted landing procedures, with the retraction of the flaps to 10 degrees prior to reaching a safe altitude and airspeed, which resulted in an uncontrolled…
- [NTSB ATL02IA112](https://openairdocs.org/ntsb/ATL02IA112), May 30, 2002: Cessna 210L (N7PJ), Sarasota, FL, incident, minor damage. Probable cause: The pilot's failure to follow the before landing checklist and confirm that the landing gear was extended.
- [NTSB ATL02LA056](https://openairdocs.org/ntsb/ATL02LA056), Feb 27, 2002: Cessna 210L (N115CW), Atlanta, GA, substantial damage. Probable cause: The pilot's failure to obtain the proper touchdown point and excessive airspeed on landing resulting in the airplane going off the end of the runway, on-ground collision with an embankment, and…
- [NTSB SEA02LA025](https://openairdocs.org/ntsb/SEA02LA025), Jan 9, 2002: Cessna 210L (N1713X), Great Falls, MT, substantial damage. Probable cause: The pilot's intentional continuation of a visual flight rules (VFR) flight into instrument meteorological conditions (IMC), and his failure to maintain clearance from the terrain. Factors include low…
- [NTSB NYC01IA211](https://openairdocs.org/ntsb/NYC01IA211), Aug 13, 2001: Cessna 210L (N732JT), Bluefield, WV, incident, minor damage. Probable cause: Improper maintenance which resulted in the installation of an unserviceable piston assembly, and the subsequent catastrophic engine failure. Factors in this accident were the improper inspection by…
- [NTSB FTW01LA180](https://openairdocs.org/ntsb/FTW01LA180), Aug 12, 2001: Cessna 210 (N8137L), Fort Smith, AR, substantial damage. Probable cause: the overload fracture of the left main landing gear actuator which resulted in the loss of all hydraulic fluid and led to a wheels up landing.
- [NTSB CHI01FA128](https://openairdocs.org/ntsb/CHI01FA128), Apr 24, 2001: Cessna 210L (N5060V), Farmington, MO, substantial damage, 2 fatal. Probable cause: The fracture of the crankshaft due to fatigue, the propeller separating from the airplane while in-flight, which resulted in the propeller striking the empennage structure and flight controls,…
- [NTSB NYC00LA164](https://openairdocs.org/ntsb/NYC00LA164), Jun 16, 2000: Cessna 210 (N485CA), Louisville, KY, substantial damage. Probable cause: The pilot's improper operation of the fuel selector.
- [NTSB FTW00FA144](https://openairdocs.org/ntsb/FTW00FA144), May 8, 2000: Cessna 210L (N732ER), Mack, CO, substantial damage, 2 fatal. Probable cause: The pilot's continued VFR flight into instrument meteorological conditions. Factors were the mountain obscuration and the rising terrain.
- [NTSB LAX00FA176](https://openairdocs.org/ntsb/LAX00FA176), Apr 28, 2000: Cessna T210L (N2193S), North Las Vegas, NV, destroyed, 2 fatal. Probable cause: The pilot's failure to maintain control of the airplane during a go-around in a crosswind condition.
- [NTSB NYC00LA046](https://openairdocs.org/ntsb/NYC00LA046), Dec 4, 1999: Cessna 210L (N1773X), Columbus, OH, substantial damage. Probable cause: The pilot's failure to verify landing gear extension. Factors were the unreliable retraction/extension assembly, and the flying club's continued operation of the airplane with known deficiencies in…
- [NTSB NYC00FA020](https://openairdocs.org/ntsb/NYC00FA020), Oct 27, 1999: Cessna 210L (N76N), Medina, OH, destroyed, 2 fatal. Probable cause: The pilot's failure to maintain proper altitude during the final approach segment of the visual approach. A factor was the diminishing light conditions of a deepening dusk.
- [NTSB FTW00LA002](https://openairdocs.org/ntsb/FTW00LA002), Oct 1, 1999: Cessna 210L (N2157S), Fayetteville, AR, substantial damage. Probable cause: The cause of the right main gear collapse was undetermined. A factor was the failure of the gear 'down & locked' switch resulting in a false 'down & locked' indication in the cockpit.

All 222: https://openairdocs.org/model/cessna-210l/ntsb.md

## FAA accident and incident reports (518, newest 50)

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

- [Incident 20260603005419I](https://openairdocs.org/incident/20260603005419I), Jun 3, 2026: Cessna 210L (N1190Q), Gilford, NH, Minor damage. On June 3, 2026, at approximately 2056Z, the pilot indaicated that he performed a stable approach to runway 08 at klci. Flaps were at 30 and gear was down PIC…
- [Accident 20250402003709A](https://openairdocs.org/incident/20250402003709A), Apr 2, 2025: Cessna 210L (N1574P), Bayou Blue, LA, Destroyed, 2 fatal. 04/02/2025 20:10 CDT: the aircraft departed the base of operation crewed by an instrument rated commercial pilot and a flight instructor holding an ATP…
- [Incident 20250117000459I](https://openairdocs.org/incident/20250117000459I), Jan 17, 2025: Cessna 210L (N94077), Fresno, CA, Minor damage. On January 17, 2025, during landing, the PIC inadvertently cycled the landing gear switch to the up position immediately after touchdown, causing the left main…
- [Incident 20241004013419I](https://openairdocs.org/incident/20241004013419I), Oct 4, 2024: Cessna 210L (N210DC), Midland, TX, Minor damage. On October 4, 2024 at approximately 1400 local time, a Cessna 210L aircraft received minor damage during a landing on runway 07 at the Midland Airpark Airport…
- [Accident 20240412003959A](https://openairdocs.org/incident/20240412003959A), Apr 12, 2024: Cessna 210L (N777NT), Concord, NC, Substantial damage. Pilot placed the landing gear down during the approach. The main landing gear did not extend. The pilot performed the manual extension procedure with no…
- [Incident 20231102018179I](https://openairdocs.org/incident/20231102018179I), Nov 2, 2023: Cessna 210L (N4621Q), Cambridge, MN, Minor damage. Aircraft landed with the gear up after a short flight to calibrate the newly installed angle of attack (AOA) system. No injuries. PIC stated he forgot to put…
- [Incident 20230801022039I](https://openairdocs.org/incident/20230801022039I), Aug 1, 2023: Cessna 210L (N121CE), Ridgely, MD, Minor damage. Aircraft landed on runway 12 and the aircraft began to shake forcing it to veer off the runway which caused the right main gear to collapse.
- [Incident 20220414005409I](https://openairdocs.org/incident/20220414005409I), Apr 14, 2022: Cessna 210L (N10HL), Wickenburg, AZ, Minor damage. On April 14, 2022 at approximately 1500 mountain standard time (MST), a Cessna 210L airplane (N10HL) departed Wickenburg Municipal Airport (E25) on the first…
- [Accident 20201220020629A](https://openairdocs.org/incident/20201220020629A), Dec 20, 2020: Cessna 210L (N2246S), Midway, GA, Substantial damage, 1 fatal. On the evening of December 20, 2020 a private pilot departed out of Swainsboro, GA (ksbo) at approx. 19:40 headed southeast for Eagle Neck Airport (1GAO)…
- [Accident 20200428006519A](https://openairdocs.org/incident/20200428006519A), Apr 28, 2020: Cessna 210L (N210HH), Canyon Lake, TX, Substantial damage. On April 28, 2020, aircraft, lost engine power while in flight and attempted an emergency landing on Canyon Lake. The pilot and one passenger swam to shore…
- [Accident 20200304008689A](https://openairdocs.org/incident/20200304008689A), Mar 4, 2020: Cessna 210L (N123CE), Needles, CA, Substantial damage. N123CE was tracked by los angeles center (zla) due to a request by homeland security. N123CE was lost on radar at 0430Z near the Needles VOR R-245, 27 DME.…
- [Incident 20200127009809I](https://openairdocs.org/incident/20200127009809I), Jan 27, 2020: Cessna 210L (N732GP), Johnstown, PA, Minor damage. 01/27/20 Incident summary ? N732GP I departed W29 at around 7:00 am. The initial part of the flight was VMC but the majority was IMC. On approach to lbe I…
- [Accident 20191224022439A](https://openairdocs.org/incident/20191224022439A), Dec 24, 2019: Cessna 210L (N30259), Concord, NC, Substantial damage. Pilot was attempting to land on a wet grass rwy at NC35 with 3 passengers on board. After touching down near midpoint of the 2,180' grass strip, pilot…
- [Accident 20190904012479A](https://openairdocs.org/incident/20190904012479A), Sep 4, 2019: Cessna 210L (N94262), Henefer, UT, Destroyed, 2 fatal. Aircraft was flying pipeline observation when it appears that the aircraft flew into a box canyon. The aircraft impacted the ground at a high velocity just…
- [Incident 20190426003449I](https://openairdocs.org/incident/20190426003449I), Apr 26, 2019: Cessna 210L (N2160S), Palm Beach, FL, Minor damage. After clearing customs at Palm Beach intl., N2160S made a wrong turn and entered a service road. The right wing tip hit a cyclone fence. Ground controller…
- [Incident 20190301005819I](https://openairdocs.org/incident/20190301005819I), Mar 1, 2019: Cessna 210L (N5400V), Elkhart, IN, Minor damage. On March 01, 2019 at 1700 eastern daylight time, a Cessna CE-210L aircraft, N5400V, registered to and operated by a student pilot, received minor damage when…
- [Incident 20170826017549I](https://openairdocs.org/incident/20170826017549I), Aug 26, 2017: Cessna 210L (N29209), Madison, IN, Minor damage. On August 26, 2017, at approximately 12:15PM eastern daylight time (EDT), a Cessna 210L, N29209, sustained minor damage following a gear-up landing at the…
- [Accident 20170711011539A](https://openairdocs.org/incident/20170711011539A), Jul 11, 2017: Cessna 210L (N732FJ), Substantial damage. Main landing gear failed to extend.
- [Incident 20170708012179I](https://openairdocs.org/incident/20170708012179I), Jul 8, 2017: Cessna 210L (N2246S), Ossabaw Island, GA, No damage. Departed 1GAO flying VFR to khxd. Upon receiving flight following from ATC at 2500', engine began to shake violently followed by excessive smoke in the cabin.…
- [Accident 20170128016129A](https://openairdocs.org/incident/20170128016129A), Jan 28, 2017: Cessna 210L (N59196), Charleston, WV, Substantial damage. During the touchdown phase of flight the aircraft, due to mismanaging contols, began to oscillate causing loss of control. The pilot was unable to regain…
- [Incident 20160724011529I](https://openairdocs.org/incident/20160724011529I), Jul 24, 2016: Cessna 210L (N176LL), Bismarck, ND, Minor damage. Aircraft departed kbis. Flew 100 miles outbound and alternator failed. Hydraulic power pack failed to shut off due to internal mechanical failure and drained…
- [Incident 20160715011989I](https://openairdocs.org/incident/20160715011989I), Jul 15, 2016: Cessna 210L (N93260), Brownsville, TX, Minor damage. PIC reported that the nose gear would not extend when attempting to land at kssf and decided to return to kbro . Upon arrval nose gear would not extend and PIC…
- [Incident 20160613012159I](https://openairdocs.org/incident/20160613012159I), Jun 13, 2016: Cessna C210L (N1574P), Belle Chasse, LA, Minor damage. Pilot failed to extend the landing gear on visual pattern into airport. Aircraft touched down on belly and skidded to a stop on paved runway at private airport…
- [Accident 20160319002009A](https://openairdocs.org/incident/20160319002009A), Mar 19, 2016: Cessna 210L (N59196), Myrtle Beach, SC, Substantial damage. On March 19, 2016, at 1020 eastern daylight time, a Cessna 210L, N59196, sustained substantial damage when the main landing gear collapsed during a…
- [Incident 20150520010959I](https://openairdocs.org/incident/20150520010959I), May 20, 2015: Cessna 210L (N732JZ), Apple Valley, CA, Minor damage. N732JZ was at cruise altitude, when aircraft experienced loss of power, pilot moved engine to idle cutoff and fuel selector to off position, declared an…
- [Incident 20141209021419I](https://openairdocs.org/incident/20141209021419I), Dec 9, 2014: Cessna 210L (N4697Q), Amarillo, TX, Minor damage. On December 9, 2014, at 1416 local time, a Cessna CE-210-L aircraft, bearing registration number n 4697Q, registered to a private owner, hit a runway light…
- [Incident 20141110019969I](https://openairdocs.org/incident/20141110019969I), Nov 10, 2014: Cessna 210 (N1574P), Ama, LA, Minor damage. After takeoff gear handle was raised gear seemed to come up but there was no indication of up and locked. Gear pump motor remained on. After leveling off tried…
- [Accident 20140702012579A](https://openairdocs.org/incident/20140702012579A), Jul 2, 2014: Cessna 210L (N1175Q), Las Vegas, NM, Substantial damage. Pilot attempted to land on closed runway 32 at lvs. After seeing men and equipment on the runway, PIC attempted a go-around. Aircraft unable to go-around and…
- [Incident 20140405006439I](https://openairdocs.org/incident/20140405006439I), Apr 5, 2014: Cessna 210L (N444PJ), Phillipsburg, OH, Minor damage. After landing on roll out the aircraft cought a sudden gust of cross wind. The nosewheel of the aircraft went off the runway and dug into the mud. The right…
- [Accident 20140214001949A](https://openairdocs.org/incident/20140214001949A), Feb 14, 2014: Cessna 210L (N732EJ), Clay, AL, Destroyed, 2 fatal. Aircraft crashed in a heavily wooded area near Clay, Alabama. The commercial pilot and one passenger were fatally injured. The airplane was destroyed.…
- [Accident 20131128024629A](https://openairdocs.org/incident/20131128024629A), Nov 28, 2013: Cessna 210L (N777BK), Bridgewater Twp, PA, Substantial damage. Usc 146 a 1974 Cessna 210L registration number N777BK was enroute teterboro, NJ (teb) to buffalo, NY (buf) at cruise at an altitude of 8,500 feet. Pilot…
- [Incident 20131026020869I](https://openairdocs.org/incident/20131026020869I), Oct 26, 2013: Cessna 210L (N30549), Springfield, OH, Minor damage. Aircraft landed with landing gear in the up position at the Springfield-Beckley airport (sgh) on runway 24. The aircraft skidded on its belly approximately…
- [Incident 20130608010429I](https://openairdocs.org/incident/20130608010429I), Jun 8, 2013: Cessna 210L (N59090), Monroeville, PA, Minor damage. The pilot stated he landed long and with too much speed resulting in an overrun on runway 05 at Monroeville (4G0) airport near Pittsburgh Pennsylvania.
- [Incident 20121228028579I](https://openairdocs.org/incident/20121228028579I), Dec 28, 2012: Cessna 210L (N2013S), Pahokee, FL, No damage. 12/28/2012: Aircraft was on a 14CFR135 flight from ktpa-kopf when the pilot noted an alternator failure and smelt smoke. Pilot declared and emergency and…
- [Accident 20121109028179A](https://openairdocs.org/incident/20121109028179A), Nov 9, 2012: Cessna 210L (N732BL), La Grange, TX, Substantial damage. On November 9th, 2012 at approximately 07:00AM aircraft N732BL Cessna 210 enroute from san marcus, Texas (khyi) to baytown, Texas (khpy) experienced a loss…
- [Incident 20121031024709I](https://openairdocs.org/incident/20121031024709I), Oct 31, 2012: Cessna 210L (N4699Q), San Juan, PR, Minor damage. On November 1 at 11:30 am I was directed by the front line manager to investigate an incident that took place at isla grande airport where a Cessna 210 landed…
- [Incident 20120723015249I](https://openairdocs.org/incident/20120723015249I), Jul 23, 2012: Cessna 210L (N59141), Omaha, NE, No damage. Pilot noticed an unsafe gear indication. Requested low pass by tower to verifiy gear down and locked. Aircraft landed without incident.
- [Incident 20120704013459I](https://openairdocs.org/incident/20120704013459I), Jul 4, 2012: Cessna 210L (N210BX), Tacoma, WA, No damage. On July 4, 2012, at approximately 0950 PDTN210BX, a Cessna 210 took-off from (S50) auburn airport flown by [privacy data omitted] along with 3 passengers…
- [Incident 20120510010329I](https://openairdocs.org/incident/20120510010329I), May 10, 2012: Cessna 210L (N59090), Mansfield, OH, Minor damage. Pilot was attempting a landing at the Mansfield Ohio airport. While selecting the landing gear to the down position, the landing gear did not indicate a down…
- [Incident 20111218028859I](https://openairdocs.org/incident/20111218028859I), Dec 18, 2011: Cessna 210L (N210BR), Hilton Head, SC, Minor damage. Pilot was landing this aircraft at Hilton Head Island Airport, in south carolina. He attempted to put the landing gear down. The landing gear would not go…
- [Incident 20110906022319I](https://openairdocs.org/incident/20110906022319I), Sep 6, 2011: Cessna 210L (N94005), Sheldon, SC, Minor damage. Pilot landed gear up on his private grass strip. Prop struck the ground and minor damage under the fuselauge.
- [Accident 20110813018819A](https://openairdocs.org/incident/20110813018819A), Aug 13, 2011: Cessna 210L (N732FY), Seattle, WA, Substantial damage. At approximately 1400 PST August 13,2011 pilot [privacy data omitted] was operating Cessna 210 under the provisions of 14 CFR part 91 from Friday harbor,…
- [Incident 20110731020429I](https://openairdocs.org/incident/20110731020429I), Jul 31, 2011: Cessna 210L (N2550S), Lodi, CA, No damage. Aircraft amp meter indicated discharge. Pilot shutdown electrical system to conserve battery power for gear extension. Aircraft landed with no further incident.
- [Incident 20110508009579I](https://openairdocs.org/incident/20110508009579I), May 8, 2011: Cessna 210L (N2390S), Jackson, MI, Minor damage. Aircraft landed RWY24 gear up
- [Incident 20110118002199I](https://openairdocs.org/incident/20110118002199I), Jan 18, 2011: Cessna 210L (N5489V), Lakeland, FL, Minor damage. On January 18, 2011, at approximately 12:14 pm, while taxing in dense fog, aircraft N5489V veered off the taxiway pavement into the grass the rotating…
- [Accident 20100708037619A](https://openairdocs.org/incident/20100708037619A), Jul 8, 2010: Cessna 210L (N2157S), Houston, TX, Substantial damage. Aircraft departed castroville municipal airport, TX (cvb) enroute to Ellington Field, TX (efd). Upon approach to efd there was no safe gear indication. Pilot…
- [Accident 20100609045039A](https://openairdocs.org/incident/20100609045039A), Jun 9, 2010: Cessna 210L (N2263S), Tampa, FL, Substantial damage. On departure from Tampa international airport N2263S had to accomplish an off airport landing due to an engine failure. Upon inspection of the engine the…
- [Incident 20100508033999I](https://openairdocs.org/incident/20100508033999I), May 8, 2010: Cessna 210L (N210BX), Blythe, CA, No damage. Aircraft ran out of fuel. Pilot induced.
- [Incident 20100312042269I](https://openairdocs.org/incident/20100312042269I), Mar 12, 2010: Cessna 210L (N777BK), Owensville, MO, Minor damage. In cruise flight, pilot reported loss of propeller control followed by engine vibration and engine stoppage. Off airport landing was made. No airframe damage…
- [Incident 20100304042509I](https://openairdocs.org/incident/20100304042509I), Mar 4, 2010: Cessna 210L (N9JP), Cumberland Isla, GA, Minor damage. Engine failure at approximately 1000 ft off Cumberland island beach. Pilot unable to restart engine and landed gear up on beach. Engine propeller sustained…

All 518: https://openairdocs.org/model/cessna-210l/incidents.md

## Service difficulty reports (184, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2020FA0000281](https://openairdocs.org/sdr/2020FA0000281), Jun 4, 2020: WIRE. BROKEN. WIRE BROKE IN-BETWEEN VOLTAGE REGULATOR AND ALTERNATOR. WIRE MAY HAVE CHAFFED OR BEEN UNDER STRESS.
- [SDR XGNA2020051100008](https://openairdocs.org/sdr/XGNA2020051100008), May 10, 2020: CIRCUIT BREAKER. NOT CLOSED. PILOTS REPORTED GEAR WOULDN'T COME UP. RETURNED TO BASE WITHOUT FURTHER INCIDENT.
- [SDR XGNA2020042000005](https://openairdocs.org/sdr/XGNA2020042000005), Apr 19, 2020: LANDING GEAR. INTERMITTENT. IMMEDIATELY UPON ROTATION DEPARTING MQY THE GREEN GEAR INDICATOR LIGHT WENT OFF. ONCE AIRBORNE, THE PILOT TRIED TO RETRACT THE GEAR, BUT NOTHING HAPPENED. HE TH
- [SDR CA190308025](https://openairdocs.org/sdr/CA190308025), Mar 6, 2019: CYLINDER. CRACKED. (CAN) OIL NOTED ON LOWER COWLING, INSPECTION SHOWED OIL LEAKING FROM PUSHROD HOUSING ON NR 1 CYLINDER. PART REMOVED AND FOUND TO BE CRACKED AROUND 50% OF ITS CI
- [SDR 2019FA0000055](https://openairdocs.org/sdr/2019FA0000055), Jan 7, 2019: ACTUATOR. FAILED. LEFT LANDING GEAR FAILED TO FULLY EXTEND IN THE DOWN AND LOCKED POSITION AFTER PILOT SELECTED GEAR DOWN FOR LANDING. THE FOLLOWING STATEMENT IS FROM THE PILOT: 
- [SDR 2017FA0000288](https://openairdocs.org/sdr/2017FA0000288), Jul 17, 2017: ACTUATOR. MALFUNCTIONED. LANDING GEAR FAILED TO RETRACT AND EXTEND AFTER TAKEOFF. MLG DOOR ACTUATOR MALFUNCTIONED.
- [SDR 2016FA0000461](https://openairdocs.org/sdr/2016FA0000461), Sep 23, 2016: HYDRAULIC LINE. FAILED. THE GEAR FAILED TO EXTEND AND LOCK PRIOR TO LANDING, PILOT ATTEMPTED EMERGENCY GEAR PROCEDURES (MANUAL PUMP) WHICH FAILED TO POSITION GEAR TO THE DOWN AND LOCKE
- [SDR 2016FA0000123](https://openairdocs.org/sdr/2016FA0000123), Mar 9, 2016: CYLINDER. CRACKED. NR 3 CYCLINDER BARREL CRACKED AT APPROXIMATELY 1" BELOW TOP DEAD CENTER. CRACK IS .75 PERCENT OF WAY AROUND AND DID NOT SEPARATE BARREL FROM HEAD.
- [SDR CA150727016](https://openairdocs.org/sdr/CA150727016), Jul 21, 2015: POWERPACK. FAULTY. (CAN) ON TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED THE LANDING GEAR HYDRAULIC POWER PACK CONTINUED TO RUN EVERY 10 SECONDS. WHEN GEAR DOWN WAS SELECTED THE FR
- [SDR CA150716009](https://openairdocs.org/sdr/CA150716009), Jul 4, 2015: PUMP. FAILED. (CAN) DURING A ROUTINE LANDING, AFTER TOUCHDOWN, AS THE AIRCRAFT WAS SLOWING THE ENGINE STOPPED. THE PILOT RESTARTED THE ENGINE AND TAXIED OFF THE RUNWAY TO HIS
- [SDR CA150716008](https://openairdocs.org/sdr/CA150716008), Jul 4, 2015: RIB. CRACKED. (CAN) DURING A 100 HR INSPECTION A CRACK WAS FOUND ON THE TOP SKIN OF THE L/H HORIZONTAL STABILIZER P/N 1232600-29 LEADING EDGE COMING FROM ONE OF THE RIVETS AT
- [SDR 2015FA0000334](https://openairdocs.org/sdr/2015FA0000334), May 1, 2015: CONNECTING ROD. FAILED. NR 4 PISTON CONNECTING ROD FAILED AT CONNECTING ROD CAP BEARING AREA CAUSING SEPARATION OF CRANK SHAFT TO CONNECTING ROD. CRANKSHAFT REMAINED AS 1 PIECE WITH PI
- [SDR BSYA20140715001](https://openairdocs.org/sdr/BSYA20140715001), Jul 15, 2014: BATTERY. FAILED. PILOT HAD A COMPLETE ELEC FAILURE AFTER TAKEOFF & RETURNED SAFELY.
- [SDR BSYA201404](https://openairdocs.org/sdr/BSYA201404), Feb 14, 2014: UNKNOWN. MALFUNCTIONED. EN ROUTE FROM BUF TO TEB, PILOT LOST ALL INTERIOR LIGHTS & NOTICED SPARKS COMING OUT OF THE INSTRUMENT PANEL. PILOT DECLARED AN EMERGENCY & DIVERTED, LANDED SAF
- [SDR BSYA201401](https://openairdocs.org/sdr/BSYA201401), Jan 9, 2014: ENGINE. POWER LOSS. 20 MILES FROM ADS, PILOT NOTICED LOSING POWER FROM THE ENG & STARTED FLUTTERING & MISFIRING. PILOT DECLARED AN EMERGENCY WITH ADS TOWER. PILOT WAS ABLE TO KEEP 
- [SDR BSYR20131128001](https://openairdocs.org/sdr/BSYR20131128001), Nov 28, 2013: ENGINE. POWER LOSS. EN ROUTE FROM TEB TO BUF, ENG LOST ALL POWER. PILOT ATTEMPTED TO LAND ON A ROAD, IN PROCESS, ACFT CLIPPED A POWER LINE & CRASHED NEAR SR 706 IN MONTROSE PA. PIL
- [SDR 2013FA0000585](https://openairdocs.org/sdr/2013FA0000585), Oct 1, 2013: RESTRAINT. CUT. HAD THE SEAT RESTRAIN MOD MADE TO ACFT TO KEEP SEAT FROM GOING BACKWARD IF PINS FAILS. THE RELEASE CABLE BROKE AND YOU COULD NOT RELEASE SEAT. IT WOULD ONLY GO 
- [SDR BSYR201309052057](https://openairdocs.org/sdr/BSYR201309052057), Sep 5, 2013: LANDING GEAR. INOPERATIVE. ON APPROACH, LANDING GEAR WOULD NOT EXTEND. PILOT PROCEEDED TO PUMP GEAR DOWN AND LOCKED AND LANDED SAFELY WITHOUT INCIDENT. MX IS INSPECTING.
- [SDR BSYR20130905056](https://openairdocs.org/sdr/BSYR20130905056), Sep 4, 2013: ALTERNATOR. ABNORMAL. AFTER TAKEOFF, PILOT NOTICED ALTERNATOR CYCLING ON AND OFF. PILOT NOTIFIED TOWER OF ISSUE AND RETURNED AND LANDED SAFELY WITHOUT INCIDENT. MX IS INSPECTING.
- [SDR BSYR20130828055](https://openairdocs.org/sdr/BSYR20130828055), Aug 27, 2013: LANDING GEAR. INOPERATIVE. ON APPROACH, NOSE GEAR WOULD NOT COME DOWN WHEN EXTENDED. PILOT HAND PUMPED GEAR DOWN AND LANDED SAFELY WITHOUT INCIDENT. OPEN
- [SDR BSYR20130723054](https://openairdocs.org/sdr/BSYR20130723054), Jul 22, 2013: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. PILOT RETURNED AND LANDED SAFELY WITHOUT INCIDENT. OPEN
- [SDR BSYR20120515048](https://openairdocs.org/sdr/BSYR20120515048), May 14, 2013: ALTERNATOR. FAILED. EN ROUT FROM MLS TO BIL, PILOT EXPERIENCED ALTERNATOR FAILURE APPROXIMATELY 20 MINUTES AFTER DEPARTING. ATC WAS NOTIFIED AND PILOT PROCEEDED TO BIL AND LANDED S
- [SDR BSYR20120503046](https://openairdocs.org/sdr/BSYR20120503046), May 2, 2013: INDICATOR. OUT OF TOLERANCE. FLIGHT DEPARTED OMA FOR DSM, JUST AFTER AIRCRAFT LEVELED OFF THE AIRSPEED INDICATOR QUIT WORKING. PILOT DECLARED AN EMERGENCY AND CONTINUED TO DSM. PILOT SAID H
- [SDR 5RJR2013020811562](https://openairdocs.org/sdr/5RJR2013020811562), Jan 25, 2013: CRANKCASE. CONTAMINATED. ACFT ON RAMP OVERNIGHT 0-10 FARENHEIT. OPERATOR HAD HARD TIME STARTING ENGINE. AIRCRAFT WARMED UP. LATER STARTED NORMAL. CREW TOOK OFF NORMAL. ABOUT 15-20 MINUT
- [SDR FPI2012F00011](https://openairdocs.org/sdr/FPI2012F00011), Jun 29, 2012: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION, COMPRESSION TEST, LEAK CHECK WITH SOAPY WATER FOUND A CRACK IN CYLINDER HEAD FROM TOP OF SPARK PLUG HOLE TO INTAKE VALVE. REPLACED WIT
- [SDR FPI2012F00010](https://openairdocs.org/sdr/FPI2012F00010), Jun 29, 2012: CYLINDER. LEAKING. DURING A 100 HOUR INSPECTION, COMPRESSION TEST LEAK CHECK WITH SOAPY WATER, A CRACK WAS FOUND AT FIRST FIN, INTO COMBUSTION CHAMBER. REPLACED WITH NEW CYLINDER 
- [SDR 2012F00094](https://openairdocs.org/sdr/2012F00094), May 18, 2012: CONTROL PANEL. INOPERATIVE. EMERGENCY LIGHTS COMING ON WHEN AIRCRAFT POWER TURNED OFF.
- [SDR FPI2012F00007](https://openairdocs.org/sdr/FPI2012F00007), Apr 11, 2012: CYLINDER HEAD. CRACKED. DURING A 100 HR INSP, COMPRESSION TEST AND SOAP BUBBLE TEST FOR CRACKS FOUND NR 1 CYLINDER HEAD CRACKED.
- [SDR FPI2012F00005](https://openairdocs.org/sdr/FPI2012F00005), Mar 2, 2012: CYLINDER. CRACKED. DURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LON
- [SDR FPIA2012F00004](https://openairdocs.org/sdr/FPIA2012F00004), Mar 2, 2012: CYLINDER. CRACKED. DURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LON
- [SDR FPI2012F00002](https://openairdocs.org/sdr/FPI2012F00002), Jan 3, 2012: CYLINDER. CRACKED. DURING A 100 HR INSP COMPRESSION TEST, FOUND NR 2 CYLINDER HEAD CRACKED FROM 1ST FIN INBD OF UPPER SPARK PLUG OVER EXHAUST VALVE TO UPPER SPARK PLUG HOLE USING 
- [SDR FPI2012F00000](https://openairdocs.org/sdr/FPI2012F00000), Dec 20, 2011: CYLINDER HEAD. CRACKED. DURING A 100 HR INSP, COMPRESSION TEST FOUND NR 1 CYLINDER HEAD CRACKED ABOVE EXHAUST VALVE TO SPARK PLUG UPPER USING SOAP WATER SOLUTION DURING COMPRESSION TES
- [SDR FPI2011F00010](https://openairdocs.org/sdr/FPI2011F00010), Oct 28, 2011: CYLINDER HEAD. CRACKED. DURING A 100 HR INSPECTION, FOUND NR1 CYLINDER CRACKED BETWEEN THE COOLING FINS OF THE EASTHEAD ABOVE THE INTAKE PORT BEHIND FUEL NOZZLE PORT.
- [SDR FPI2011F00004](https://openairdocs.org/sdr/FPI2011F00004), Jul 20, 2011: CYLINDER. CRACKED. DURING A 100 HR INSPECTION FOUND THE CYLINDER AHEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TES
- [SDR FPI2011F00003](https://openairdocs.org/sdr/FPI2011F00003), Jul 20, 2011: CYLINDER. CRACKED. DURING A 100 HR INSPECTION FOUND THE CYLINDER AHEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TES
- [SDR FPI2011F00002](https://openairdocs.org/sdr/FPI2011F00002), Jul 20, 2011: CYLINDER. CRACKED. DURING A 100 HR INSPECTION FOUND THE CYLINDER HEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TEST
- [SDR FPI2011F00001](https://openairdocs.org/sdr/FPI2011F00001), Mar 30, 2011: SHAFT. OUT OF POSITION. RECEIVED NEW FUEL SELECTOR SHAFT AND WAS FOUND TO BE ASSEMBLED 180 DEGREES OUT. THE HANDLE TO SELECT FUEL TANK POINTS TO THE OPPOSITE TANK OF WHICH IS BEING USE
- [SDR 2011FA0000053](https://openairdocs.org/sdr/2011FA0000053), Jan 27, 2011: WHEEL HALF. FAILED. LT WHEEL ASSY CAME APART AT OUTER WHEEL HALF DURING TAXI OF ACFT.
- [SDR FPI2010F00002](https://openairdocs.org/sdr/FPI2010F00002), Nov 1, 2010: SHUTTLE VALVE. BROKEN. DURING ANNUAL INSP OF ACFT, INSP OF SHUTTLE VALVE OF STANDBY VACUUM SYS FOUND THE VACUUM PUMP SIDE, VALVE SPRING BROKEN. REPLACED WITH NEW PART.
- [SDR WUMR2011001](https://openairdocs.org/sdr/WUMR2011001), Oct 28, 2010: ACTUATOR. FALSE ACTIVATION. DURING FLIGHT THE LT GEAR "DOWNLOCK ACTUATOR" FAILED WHILE THE GEAR WAS IN THE "UP" POSITION. THE DOWNLOCK HAS AN INTERNAL FAILURE WHICH ALLOWED IT TO COLLAPSE 
- [SDR CA101018013](https://openairdocs.org/sdr/CA101018013), Oct 15, 2010: SWITCH. FAILED. SNAG: LANDING LIGHT SWITCH TO VERIFY, LANDING LIGHT SWITCH (1) PN: TA-201-TW-B. REPLACED NEW IAW SB SEB09-6 (DUE SPARKING COMING OUT THROUGH KNOB WHEN PUTTING S
- [SDR CA100719005](https://openairdocs.org/sdr/CA100719005), Jul 14, 2010: FASTENER. MISSING. (CAN) UPON TAXI, PILOT NOTICED RIGHT MAIN WHEEL LOCKED UP DURING TAXI. MAINTENANCE WAS DISPATCHED AND UPON INVESTIGATION WAS FOUND THAT RIGHT MAIN WHEEL ASSEMBL
- [SDR FPI2010F00001](https://openairdocs.org/sdr/FPI2010F00001), Jun 18, 2010: SPRING. INOPERATIVE. ENGINE WAS REMOVED FOR INTERNAL VIBRATION AND REPAIRED BY MFG. REPLACED CRANKSHAFT ENGINE, REINSTALLED IN ACFT. AFTER APPROXIMATELY 16 CYCLES, THE STARTER WAS E
- [SDR FPI2010F00000](https://openairdocs.org/sdr/FPI2010F00000), Mar 25, 2010: CABLE ASSY. BROKEN. MFG SERVICE KIT: PN SK210-174. CABLE ASSY CABLE BROKEN AT SWEDGE END EYELET AT THREADED END.
- [SDR CA100116001](https://openairdocs.org/sdr/CA100116001), Jan 15, 2010: TERMINAL. SHORTED. (CAN) ON APPROACH, THE PILOT SELECTED GEAR DOWN IN ANTICIPATION FOR LANDING. AFTER DOING THIS, SPARKS WERE NOTICED BEHIND THE INSTRUMENT PANEL BELOW THE RADIO S
- [SDR CA090929003](https://openairdocs.org/sdr/CA090929003), Sep 27, 2009: LANDING GEAR. OBSTRUCTED. (CAN) UPON APPROACH, PILOT SELECTED MLG DOWN, & DID NOT GET A MLG DOWN INDICATION & HYDRAULIC MOTOR DID NOT SHUT-OFF. PILOT PULLED MLG CIRCUIT BREAKER & USED EM
- [SDR CA090622020](https://openairdocs.org/sdr/CA090622020), Jun 19, 2009: EXHAUST VALVE. STUCK. (CAN) ACFT WAS UNDERGOING A 50 HR INSP. INSP REVEALED AN OIL LEAK ON RT SIDE OF ENG. INVESTIGATION REVEALED EXHAUST PUSH TUBE SEALS WERE LEAKING. REMOVAL OF THE
- [SDR 2008FA0000302](https://openairdocs.org/sdr/2008FA0000302), Apr 19, 2008: GASKET. FAILED. THE OIL COOLER ADAPTER GASKET TAILED IN FLIGHT CAUSING (2) QUARTS OF OIL IN ONE HOUR TO BE PUMPED INTO THE ENGINE COWLING. THIS ENGINE IS A FACTORY REMANUFACTUR
- [SDR 2008FA0000222](https://openairdocs.org/sdr/2008FA0000222), Nov 16, 2007: DOWNLOCK SWITCH. BROKEN. EXAMINATION OF THE LANDING GEAR SYSTEM REVEALED THAT THE LT LDG DOWN LIMIT SWITCH PLUNGER WAS DAMAGED AND STUCK IN THE DEPRESSED POSITION WITH APPROX .012 INCH 
- [SDR CA070410003](https://openairdocs.org/sdr/CA070410003), Mar 27, 2007: BOLT. BROKEN. (CAN) ON SCHEDULED INSPECTION APPRENTICE FOUND ONE ATTACH BOLT BACKED OUT OF HOLE. ON REMOVING THE BOLT FULLY HE FOUND THE BOLT TO BE BROKEN. THE AIRCRAFT WAS J

All 184: https://openairdocs.org/model/cessna-210l/reports.md

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