# Diamond Aircraft Ind DA20-A1 - Type: Aircraft model (FAA registry) - Registry code: 2990000 - Manufacturer (registry): DIAMOND AIRCRAFT IND INC - Model: DA20-A1 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS TA4CH](https://openairdocs.org/tcds/TA4CH) (OpenAirDocs) - Holder: Diamond Aircraft Industries Inc. - Registered aircraft: 29 - Page: https://openairdocs.org/model/diamond-aircraft-ind-da20-a1 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 2026-16-11](https://openairdocs.org/ad/2026-16-11): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Aug 28, 2026 - [AD 2023-17-13](https://openairdocs.org/ad/2023-17-13): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Sep 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 2018-03-05](https://openairdocs.org/ad/2018-03-05): Reciprocating Engine · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Mar 20, 2018 - [AD 2016-23-06](https://openairdocs.org/ad/2016-23-06): Engine--Fuel and Control · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Dec 23, 2016 - [AD 2016-12-02](https://openairdocs.org/ad/2016-12-02): Engine Reciprocating · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Jul 15, 2016 - [AD 2013-17-04](https://openairdocs.org/ad/2013-17-04): Engine Reciprocating · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Sep 24, 2013 - [AD 2012-01-01](https://openairdocs.org/ad/2012-01-01): Engine · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Jan 26, 2012 - [AD 2011-14-09](https://openairdocs.org/ad/2011-14-09): Ignition · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Jul 25, 2011 - [AD 2010-23-17](https://openairdocs.org/ad/2010-23-17): Engine · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Dec 22, 2010 - [AD 2010-17-08](https://openairdocs.org/ad/2010-17-08): Engine Fuel and Control · Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango), HK 36 R SUPER DIMONA, HK 36 TC and 5 more. Effective Sep 22, 2010 - [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 97-13-02](https://openairdocs.org/ad/97-13-02): Placard - Spins Prohibited · Diamond Aircraft Industries DA20-A1. Effective Jul 14, 1997 - [AD 96-09-05](https://openairdocs.org/ad/96-09-05): Aileron Pushrod Fairings and Aft Wing Cavities · Diamond Aircraft Industries DA20-A1. Effective May 17, 1996 ## Information bulletins (advisory) (3) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-12-09](https://openairdocs.org/saib/CE-12-09): Landing Gear, Nose: Diamond DA20 Nose Landing Fork Assembly. Issued Dec 22, 2011 - [SAIB ACE-99-17](https://openairdocs.org/saib/ACE-99-17): . Issued Apr 2, 1999 ## Registered aircraft (29) - [N102DF](https://openairdocs.org/aircraft/N102DF): [Le Garrett P](https://openairdocs.org/faa-owner/LE%20GARRETT%20P), [Exeter, CA](https://openairdocs.org/faa-place/CA/Exeter), S/N 10029 - [N128MF](https://openairdocs.org/aircraft/N128MF): [Aircraft Guaranty Corp Trustee](https://openairdocs.org/faa-owner/AIRCRAFT%20GUARANTY%20CORP%20TRUSTEE), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 1995, S/N 10028 - [N143AA](https://openairdocs.org/aircraft/N143AA): [Torres Vincent Jimenez](https://openairdocs.org/faa-owner/TORRES%20VINCENT%20JIMENEZ), [Auburndale, FL](https://openairdocs.org/faa-place/FL/Auburndale), built 1996, S/N 10183 - [N144AA](https://openairdocs.org/aircraft/N144AA): [Piston Aviation LLC](https://openairdocs.org/faa-owner/PISTON%20AVIATION%20LLC), [Saint Charles, MO](https://openairdocs.org/faa-place/MO/Saint%20Charles), built 1996, S/N 10096 - [N175LE](https://openairdocs.org/aircraft/N175LE): [Phan Jerry](https://openairdocs.org/faa-owner/PHAN%20JERRY), [Santa Ana, CA](https://openairdocs.org/faa-place/CA/Santa%20Ana), S/N 10076 - [N179DA](https://openairdocs.org/aircraft/N179DA): [Dunne Robert W](https://openairdocs.org/faa-owner/DUNNE%20ROBERT%20W), [Mentor, OH](https://openairdocs.org/faa-place/OH/Mentor), S/N 10179 - [N191DA](https://openairdocs.org/aircraft/N191DA): [Qaiss Mohammed](https://openairdocs.org/faa-owner/QAISS%20MOHAMMED), [Phoenixville, PA](https://openairdocs.org/faa-place/PA/Phoenixville), S/N 10065 - [N192DA](https://openairdocs.org/aircraft/N192DA): [Rhodes Samuel S](https://openairdocs.org/faa-owner/RHODES%20SAMUEL%20S), [Roseville, CA](https://openairdocs.org/faa-place/CA/Roseville), built 1995, S/N 10060 - [N194DA](https://openairdocs.org/aircraft/N194DA): [Shively Orrin J](https://openairdocs.org/faa-owner/SHIVELY%20ORRIN%20J), [Pasadena, CA](https://openairdocs.org/faa-place/CA/Pasadena), built 1996, S/N 10102 - [N204RD](https://openairdocs.org/aircraft/N204RD): [Mastropietro Richard](https://openairdocs.org/faa-owner/MASTROPIETRO%20RICHARD), [Aptos, CA](https://openairdocs.org/faa-place/CA/Aptos), built 1995, S/N 10079 - [N227P](https://openairdocs.org/aircraft/N227P): [Herrick Kristopher Joseph](https://openairdocs.org/faa-owner/HERRICK%20KRISTOPHER%20JOSEPH), [Captain Cook, HI](https://openairdocs.org/faa-place/HI/Captain%20Cook), built 1995, S/N 10045 - [N273DA](https://openairdocs.org/aircraft/N273DA): [Metamorphosis Publishing LLC](https://openairdocs.org/faa-owner/METAMORPHOSIS%20PUBLISHING%20LLC), [Hamilton, MT](https://openairdocs.org/faa-place/MT/Hamilton), S/N 10173 - [N275DA](https://openairdocs.org/aircraft/N275DA): [Stevens David](https://openairdocs.org/faa-owner/STEVENS%20DAVID), [Flower Mound, TX](https://openairdocs.org/faa-place/TX/Flower%20Mound), built 1997, S/N 10269 - [N297DA](https://openairdocs.org/aircraft/N297DA): [Neumeuller Martin](https://openairdocs.org/faa-owner/NEUMEULLER%20MARTIN), [Powell Butte, OR](https://openairdocs.org/faa-place/OR/Powell%20Butte), built 1997, S/N 10297 - [N355NL](https://openairdocs.org/aircraft/N355NL): [Long Nicholas](https://openairdocs.org/faa-owner/LONG%20NICHOLAS), [Woodinville, WA](https://openairdocs.org/faa-place/WA/Woodinville), built 1997, S/N 10286 - [N521SS](https://openairdocs.org/aircraft/N521SS): [55840 LLC](https://openairdocs.org/faa-owner/55840%20LLC), [Lafayette, IN](https://openairdocs.org/faa-place/IN/Lafayette), S/N 10081 - [N629AW](https://openairdocs.org/aircraft/N629AW): [Midlothian, TX](https://openairdocs.org/faa-place/TX/Midlothian), built 1995, S/N 10023, Sale reported - [N631DA](https://openairdocs.org/aircraft/N631DA): [Mongare Job](https://openairdocs.org/faa-owner/MONGARE%20JOB), [Athens, TX](https://openairdocs.org/faa-place/TX/Athens), built 1997, S/N 10301 - [N702PR](https://openairdocs.org/aircraft/N702PR): [Arroyo Jose R](https://openairdocs.org/faa-owner/ARROYO%20JOSE%20R), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1995, S/N 10015 - [N71LV](https://openairdocs.org/aircraft/N71LV): [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), built 1995, S/N 10070 - [N781WA](https://openairdocs.org/aircraft/N781WA): [Wilshone LLC](https://openairdocs.org/faa-owner/WILSHONE%20LLC), [Lake Forest, IL](https://openairdocs.org/faa-place/IL/Lake%20Forest), built 1995, S/N 10052 - [N83RF](https://openairdocs.org/aircraft/N83RF): [Hall John B](https://openairdocs.org/faa-owner/HALL%20JOHN%20B), [Lee, NH](https://openairdocs.org/faa-place/NH/Lee), S/N 10139 - [N854S](https://openairdocs.org/aircraft/N854S): [Shively W Bevin](https://openairdocs.org/faa-owner/SHIVELY%20W%20BEVIN), [Saint Peters, MO](https://openairdocs.org/faa-place/MO/Saint%20Peters), built 1996, S/N 10198 - [N855DF](https://openairdocs.org/aircraft/N855DF): [Lawler Glenn M](https://openairdocs.org/faa-owner/LAWLER%20GLENN%20M), [Mooresville, NC](https://openairdocs.org/faa-place/NC/Mooresville), built 1996, S/N 10169 - [N856DF](https://openairdocs.org/aircraft/N856DF): [Nassau County School Board](https://openairdocs.org/faa-owner/NASSAU%20COUNTY%20SCHOOL%20BOARD), [Fernandina Beach, FL](https://openairdocs.org/faa-place/FL/Fernandina%20Beach), built 1996, S/N 10170 - [N858DF](https://openairdocs.org/aircraft/N858DF): [Gibbs Alfred D](https://openairdocs.org/faa-owner/GIBBS%20ALFRED%20D), [San Pedro, CA](https://openairdocs.org/faa-place/CA/San%20Pedro), built 1996, S/N 10147 - [N87HA](https://openairdocs.org/aircraft/N87HA): [Fitzstephens Erik W](https://openairdocs.org/faa-owner/FITZSTEPHENS%20ERIK%20W), [North Pole, AK](https://openairdocs.org/faa-place/AK/North%20Pole), built 1995, S/N 10086 - [N930AG](https://openairdocs.org/aircraft/N930AG): [Uhlik Christopher R](https://openairdocs.org/faa-owner/UHLIK%20CHRISTOPHER%20R), [Vancouver, WA](https://openairdocs.org/faa-place/WA/Vancouver), built 1996, S/N 10196 - [N999RR](https://openairdocs.org/aircraft/N999RR): [Ryan R S](https://openairdocs.org/faa-owner/RYAN%20R%20S), [San Diego, CA](https://openairdocs.org/faa-place/CA/San%20Diego), built 1996, S/N 10069 ## NTSB investigations (19) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ERA26FA310](https://openairdocs.org/ntsb/ERA26FA310), Aug 20, 2026: Diamond Aircraft Ind DA20-A1 (N83RF), Bristol, ME, substantial damage, 1 fatal, investigation ongoing - [NTSB ERA11LA114](https://openairdocs.org/ntsb/ERA11LA114), Jan 14, 2011: Diamond Aircraft Ind DA 20-A1 (N840DF), Pompano Beach, FL, substantial damage. Probable cause: A total loss of engine power for undetermined reasons. - [NTSB CHI07CA116](https://openairdocs.org/ntsb/CHI07CA116), Apr 21, 2007: Diamond Aircraft Industries DA 20-A1 (N50ML), Warrenton, MO, substantial damage. Probable cause: The pilot's inadequate pre-flight planning which resulted in exhaustion of the fuel supply and the unsuitable terrain encountered for the forced landing. A factor in the accident was inaccurate fuel… - [NTSB DEN03LA104](https://openairdocs.org/ntsb/DEN03LA104), Jun 13, 2003: Diamond Aircraft Industries DA 20-A1 (N630DA), Eureka, UT, destroyed. Probable cause: the pilot's improper in-flight planning and failure to maintain aircraft control. Contributing factors include high density altitude, hilly terrain, low airspeed and the subsequent inadvertent… - [NTSB ATL02LA071](https://openairdocs.org/ntsb/ATL02LA071), Mar 31, 2002: Diamond Aircraft Industries DA 20-A1 (N122SE), Naples, FL, substantial damage. Probable cause: The loss of engine power for undetermined reasons. - [NTSB MIA99FA246](https://openairdocs.org/ntsb/MIA99FA246), Sep 4, 1999: Diamond Aircraft Industries DA20-A1 (N196DA), Cedar Key, FL, substantial damage. Probable cause: The pilot's failure to follow the checklist (turn Fuel Valve-On, and activate electric fuel boost pump) and the pilot's decision to continue flight with a known unairworthy condition (illumination of… - [NTSB LAX99LA264](https://openairdocs.org/ntsb/LAX99LA264), Aug 18, 1999: Diamond Aircraft Industries Katana DA 20-A1 (N854DF), San Carlos, CA, substantial damage. Probable cause: The release of the aircraft's left canopy latch following takeoff resulting in the subsequent opening of the canopy in flight. The opened canopy resulted in a degradation of aircraft control and the… - [NTSB NYC99LA176](https://openairdocs.org/ntsb/NYC99LA176), Jul 15, 1999: Diamond Aircraft Industries DA 20-A1 (N404EC), Sanford, ME, substantial damage. Probable cause: The pilot's failure to maintain control of the airplane - [NTSB DEN99LA060](https://openairdocs.org/ntsb/DEN99LA060), Mar 27, 1999: Diamond Aircraft Industries DA 20-A1 (N528SS), Coyote, NM, destroyed. Probable cause: The pilot-in-command's inadvertent flight into adverse weather, and his continued flight into instrument meteorological conditions. Factors were his failure to obtain an updated recorded weather… - [NTSB DEN99LA048](https://openairdocs.org/ntsb/DEN99LA048), Mar 6, 1999: Diamond Aircraft Industries DA 20-A1 (N189DA), Provo, UT, destroyed. Probable cause: The pilot exercising poor judgment by ignoring proper procedures/directives, his intentional selection of the wrong runway for takeoff, and his failure to maintain an adequate visual lookout. Factors… - [NTSB FTW99LA062](https://openairdocs.org/ntsb/FTW99LA062), Oct 1, 1998: Diamond Aircraft Industries DA 20-A1 (N527SS), Tomball, TX, substantial damage. Probable cause: The pilot's failure to follow the checklist and secure the canopy, which resulted in the canopy separating from the airplane during takeoff initial climb. A factor was the pilot's failure to detect… - [NTSB LAX98LA272](https://openairdocs.org/ntsb/LAX98LA272), Aug 18, 1998: Diamond Aircraft Industries DA-20-A1 (N606F), Woodland, CA, substantial damage. Probable cause: The pilot's failure during a preflight inspection to detect the damaged propeller from the previous hard landing. The damaged propeller degraded the climb performance capability of the airplane. - [NTSB ATL98LA006](https://openairdocs.org/ntsb/ATL98LA006), Oct 21, 1997: Diamond Aircraft Industries DA20-A1 (N534SS), West Palm Beach, FL, substantial damage. Probable cause: the pilot's inadvertent use of the wrong runway, and his improper decision to continue the approach behind a large airplane (MD-80), which resulted in a wake turbulence encounter, loss of aircraft… - [NTSB MIA97LA240](https://openairdocs.org/ntsb/MIA97LA240), Sep 7, 1997: Diamond Aircraft Industries DA 20-A1 (N560SS), Concord, NC, substantial damage. Probable cause: The failure of the pilot to latch the canopy closed prior to takeoff. This resulted in the canopying opening while on approach to land and the pilot was unable to maintain altitude due to the… - [NTSB IAD97LA107](https://openairdocs.org/ntsb/IAD97LA107), Aug 10, 1997: Diamond Aircraft Industries DA 20-A1 (N278PL), Slatington, PA, substantial damage. Probable cause: The pilot's inadequate preflight planning/ preparation which resulted in fuel exhaustion. - [NTSB MIA97LA136](https://openairdocs.org/ntsb/MIA97LA136), Apr 13, 1997: Diamond Aircraft Industries DA 20-A1 (N124MF), Hollywood, FL, substantial damage. Probable cause: the student pilot's failure to maintain directional control during the landing/go-around, which led to subsequent in-flight collision with a fixed object (approach light/light bar/sign) and terrain.… - [NTSB LAX96LA319](https://openairdocs.org/ntsb/LAX96LA319), Aug 24, 1996: Diamond Aircraft Industries Katana DA20-A1 (N474B), S. Lake Tahoe, CA, substantial damage. Probable cause: The pilot's inadequate use of the brakes, which resulted in loss of directional control while taxiing in a non-movement area. - [NTSB LAX96LA285](https://openairdocs.org/ntsb/LAX96LA285), Jul 22, 1996: Diamond Aircraft Industries Katana DA-20-A1 (N236BR), Vacaville, CA, substantial damage. Probable cause: improper planning/decision by the instructor pilot, which resulted in subsequent fuel exhaustion and loss of engine power, due to an inadequate supply of fuel. - [NTSB LAX96LA051](https://openairdocs.org/ntsb/LAX96LA051), Nov 21, 1995: Diamond Aircraft Industries DA20-A1 (N402KT), San Carlos, CA, substantial damage. Probable cause: the pilot's improper recovery from a bounced landing and failure to maintain directional control, while landing at night. ## FAA accident and incident reports (43) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20110114000819A](https://openairdocs.org/incident/20110114000819A), Jan 14, 2011: Diamond Air DA 20-A1 (N840DF), Pompano Beach, FL, Substantial damage. While practicing touch & go's at kpmp, the pilot was on her second takeoff from runway 10. She had reached an altitude of approximately 100' MSL when the… - [Accident 20070421004589A](https://openairdocs.org/incident/20070421004589A), Apr 21, 2007: Diamon DA20A1 (N50ML), Warrenton, MO, Substantial damage. (-23) The pilot [privacy data omitted] was enroute to California after picking this aircraft up in doylestown, pa (kdyl). He had made a fuel stop at the… - [Incident 20050726017099I](https://openairdocs.org/incident/20050726017099I), Jul 26, 2005: Diamon DA20A1 (N96CF), Doylestown, PA, Minor damage. (-23) After touchdown, the airplane bounced and started to veer left off the runway. The student pilot tried to go-around, but stalled the airplane instead.… - [Incident 20040210001259I](https://openairdocs.org/incident/20040210001259I), Feb 10, 2004: Diamon DA20A1 (N303EC), Bedford, MA, Minor damage. (-23) During cruise flt a loud bang was heard, then the engine stopped. The aircraft was landed without power. It was determined that an engine connecting rod… - [Incident 20031001031599I](https://openairdocs.org/incident/20031001031599I), Oct 1, 2003: Diamon DA20A1 (N53HA), Chesapeake, VA, Minor damage. (-23) Number 2 exhaust valve failed and caused the engine failure while in flight. The pilot made off field emergency landing. There was no damage to the… - [Accident 20030613011359A](https://openairdocs.org/incident/20030613011359A), Jun 13, 2003: Diamon DA20A1 (N630DA), Little Sahara, UT, Substantial damage. (-23) Pilot was in cruise flight on the east side of a range of mountains that ran north and south. Aircraft entered descending (leeward side) air, pilot… - [Incident 20030211007449I](https://openairdocs.org/incident/20030211007449I), Feb 11, 2003: Diamon DA20A1 (N124MF), Hollywood, FL, Minor damage. (-23) 2/11/03 18:14Z hwo, private pilot james flavin, was taxiing aircraft, N124MF a pelican airways katana, west on taxiway lima to runway 36R. Just before… - [Incident 20020411005709I](https://openairdocs.org/incident/20020411005709I), Apr 11, 2002: Diamon DA20A1 (N402KT), Fremont, CA. (-23) Pilot gagot-rivera executed forced un-powered landing due to fuel exhaustion. No injuries to persons or damage to aircraft or property resulted. Flight… - [Accident 20020331005839A](https://openairdocs.org/incident/20020331005839A), Mar 31, 2002: Diamon DA20A1 (N122SE), Naples, FL, No damage. (.19) On March 30, 2002 at 1242 eastern standard time, a diamond aircraft industries da 20-A1, N122SE, registered to kissimmee air center, inc., crashed while… - [Incident 20010802020169I](https://openairdocs.org/incident/20010802020169I), Aug 2, 2001: Diamon DA20A1 (N930AG), San Carlos, CA. (-23) While student was practicing pattern work engine lost oil quantity and pressure causing engine to seize. Forced off field landing without injury or… - [Incident 20010516021099I](https://openairdocs.org/incident/20010516021099I), May 16, 2001: Diamon DA20A1 (N442PC), Haines City, FL. (-23) On may 16, 2001 the pilot took off from the kissimmee municipal airport (ism) toward the lake wales area for an overflight, when upon returning to ism… - [Incident 20010514010329I](https://openairdocs.org/incident/20010514010329I), May 14, 2001: Diamon DA20A1 (N606DA), Chandler, AZ, Minor damage. (-23)Aircraft engine stopped running due to fuel starvation. Aircraft was enroute from sedona, AZ. Pilot made an off airport landing in a field slightly… - [Incident 20010128002529I](https://openairdocs.org/incident/20010128002529I), Jan 28, 2001: Diamon DA20A1 (N925JS), Lincoln Park, NJ, Minor damage. (-23) On 1/28/2001 at approx. 14:30 EST, [privacy data omitted]lost control of katana N925JS while landing in a left crosswind, on runway 01, at Lincoln Park… - [Incident 20001106018339I](https://openairdocs.org/incident/20001106018339I), Nov 6, 2000: Diamon DA20A1 (N125MF), Pembroke Pines, FL, Substantial damage. (-23) Pilot in command reported smoke in the cockpit - landed near /0B/ at highway U.S. 27 and Pines boulevard-a/c caught fire, two (2) soles on board-no… - [Incident 19990928027529I](https://openairdocs.org/incident/19990928027529I), Sep 28, 1999: Diamon DA20A1 (N193DA), Burbank, CA. (-23) Operator experienced low oil pressure indication on climb. Operator returned to airport and made a normal landing. The airport fire units responded to a… - [Incident 19990904039099I](https://openairdocs.org/incident/19990904039099I), Sep 4, 1999: Diamon DA20A1 (N196DA), Cedar Key, FL, Minor damage. N196DA right wing tip struck spinner of parked N2938D while manuvering on ramp area. - [Accident 19990904025329A](https://openairdocs.org/incident/19990904025329A), Sep 4, 1999: Diamon DA20A1 (N196DA), Cedar Key, FL, Substantial damage. (.19) On September 4, 1999, at about 1845 eastern daylight time, a diamond DA20-A1, N196DA, registered to sky king aviation, operating as a 14 CFR part 91… - [Incident 19990903032269I](https://openairdocs.org/incident/19990903032269I), Sep 3, 1999: Diamon DA20A1 (N846DF), Spanish Fork, UT, Minor damage. (-23) On 09-03-99, Mr. Matthew b. rix (a student) took off on an authorized solo flight where he planned to stay in the local area. During the flight, the… - [Accident 19990818012699A](https://openairdocs.org/incident/19990818012699A), Aug 18, 1999: Diamon DA20A1 (N854DF), San Carlos, CA, Substantial damage. Acft canopy opened on departure as acft turned downwind for landing, pilot declared an emergency and commenced a right downward descent with impact… - [Incident 19990716014779I](https://openairdocs.org/incident/19990716014779I), Jul 16, 1999: Diamon DA20A1 (N175LE), Wilcox, AZ. Airman did planning and preflight properly. Airman knew that he was running out of time, but elected to continue because the fuel gauge indicated 1/4 tank.… - [Accident 19990715046089A](https://openairdocs.org/incident/19990715046089A), Jul 15, 1999: Diamon DA20A1 (N404EC), Sanford, ME, No damage. (-23) A diamond aircraft industries, DA20-A1 (katana), N404EC, piloted by student pilot lauren k. graham, certificate #BB007817, lost direction control during… - [Accident 19990326022059A](https://openairdocs.org/incident/19990326022059A), Mar 26, 1999: Diamon DA20A1 (N528SS), Coyote, NM, Destroyed. (From .4) the pilot and his pilot-rated passenger were flying cross-country for the purpose of building flight time. The pilot assumed the role of PIC for the… - [Accident 19990306002032A](https://openairdocs.org/incident/19990306002032A), Mar 6, 1999: Diamon DA20A1 (N189DA), Provo, UT, Destroyed. Acft was making touch and go landings on rwy 31 when it collided with N4312A, a Piper PA-28 acft, which was taking off from intersecting rwy 18, both acft were… - [Incident 19981205042199I](https://openairdocs.org/incident/19981205042199I), Dec 5, 1998: Diamon DA20A1 (N524SS), Glendale, AZ, Minor damage. (-5)Incident occurred on dec. 5, 1998 during a dual training flight in a katana DA20 N524SS at Glendale Municipal Airport, runway 19. Wx: VMC, wind condition… - [Incident 19981122043219I](https://openairdocs.org/incident/19981122043219I), Nov 22, 1998: Diamon DA20A1 (N87HA), Chesapeake, VA, Minor damage. (-5) Dn landing, norse wheel broke off where axis attaches to the wheel fork. Both sides of fork broke [privacy data omitted] - [Accident 19981001042209A](https://openairdocs.org/incident/19981001042209A), Oct 1, 1998: Diamon DA20A1 (N527SS), Houston, TX, Substantial damage. (.19) On October 1, 1998, at 1230 central daylight time, a diamond aircraft industries da 20-A1 airplane, N527SS, was substantially damaged during takeoff from… - [Incident 19980916038019I](https://openairdocs.org/incident/19980916038019I), Sep 16, 1998: Diamon DA20A1 (N11UV), Provo, UT, Minor damage. (-5)On 09/16/98 at 1615 MDT, student jon demron landed a diamond DA-20 katana on runway 18, at Provo, (pvu). The instructor was mike goodrich. Mr. Demron… - [Incident 19980826027739I](https://openairdocs.org/incident/19980826027739I), Aug 26, 1998: Diamon DA20A1 (N221DA), El Cajon, CA. After the Gillespie field (see) departure, cruise power setting FL035, the pilot noticed the engine RPM exceeded red line. The engine power was reduced and air… - [Accident 19980818021259A](https://openairdocs.org/incident/19980818021259A), Aug 18, 1998: Diamon DA20A1 (N606F), Woodland, CA, Substantial damage. Katana acft reported engine problems shortly after takeoff and crashed into a field. (.4) the student pilot reported that while landing at the airport she made… - [Incident 19980327017139I](https://openairdocs.org/incident/19980327017139I), Mar 27, 1998: Diamon DA20A1 (N50ML), Lancaster, PA, Substantial damage. Power loss on climb from touch go. Engine failed on final. Throw rod cracked case. Oil vapors ignited. - [Incident 19980113002009I](https://openairdocs.org/incident/19980113002009I), Jan 13, 1998: Diamon DA20A1 (N104KS), Palo Alto, CA, Minor damage. Narrative: on touchdown the nose of the aircraft came up. The pilot over reacted and pushed the stick forward hard, causing the nose to strike the runway too… - [Incident 19971028034049I](https://openairdocs.org/incident/19971028034049I), Oct 28, 1997: Diamon DA20A1 (N535SS), Kingman, AZ, Minor damage. Narrative: student pilot on a solo cross country. Porpoised on landing at Kingman Airport and damaged the propeller-the student pilot and sole occupant was not… - [Accident 19971021030779A](https://openairdocs.org/incident/19971021030779A), Oct 21, 1997: Diamon DA20A1 (N534SS), West Palm Beach, FL, Substantial damage. On final MD80 passed homebuilt. Landing on 27R. Wake rolled the DA20 upside down. Crashed. Had deviated into wake. (-23) 10/21/97, about 1220 local was cleared… - [Accident 19970907025619A](https://openairdocs.org/incident/19970907025619A), Sep 7, 1997: Diamon DA20A1 (N560SS), Concord, NC, Substantial damage. Canopy came off on final. Added power but settled into trees. Crashed inverted. Should be capable make runway. (.4)the pilot forgot to latch the canopy closed… - [Accident 19970809021489A](https://openairdocs.org/incident/19970809021489A), Aug 9, 1997: Diamon DA20A1 (N278PL), Slatington, PA, Substantial damage. On August 9, 1997, at 2258 eastern daylight time, a diamond da 20-A1, N278PL, was substantially damaged when it collided with trees during a forced landing… - [Incident 19970507015089I](https://openairdocs.org/incident/19970507015089I), May 7, 1997: N668DA, Farmingdale, NY, Minor damage. Narrative: student pilot while taxiing misjudged taxiway clearance around a parked van. Aircrafat wing tip struck van and caused aircraft to swing around to… - [Accident 19970413010129A](https://openairdocs.org/incident/19970413010129A), Apr 13, 1997: Diamon DA20A1 (N124MF), Hollywood, FL, Substantial damage. (.19) On April 13, 1997, about 1347 eastern daylight time, a diamond aircraft DA-20, N124MF, operated by pelican airways, while on a title 14 CFR part 91… - [Accident 19960824025269A](https://openairdocs.org/incident/19960824025269A), Aug 24, 1996: Diamon DA20A1 (N474B), South Lake Taho, CA, Substantial damage. Reported right brake failed turning on ramp. Hit 2 parked aircraft. Misused steerable brake system. No defects. - [Incident 19960812032589I](https://openairdocs.org/incident/19960812032589I), Aug 12, 1996: Diamon DA20A1 (N523SS), Tulsa, OK, Minor damage. Narrative: on August 12, 1996, during an instructional flight with instructor pilot kevin clark and student pilot leonel rocha, the aircraft landed at r.j.… - [Accident 19960722019169A](https://openairdocs.org/incident/19960722019169A), Jul 22, 1996: Diamon DA20A1 (N236BR), Vacaville, CA, Substantial damage. Forced landing on dual flight. Fuel tanks empty. Student had questioned CFI about fuel prior. Hit sign on a street. - [Incident 19960617028769I](https://openairdocs.org/incident/19960617028769I), Jun 17, 1996: Diamon DA20A1 (N530SS), Minor damage. Narrative: pilot forgot to fuel the aircraft prior to an instructional flight and took off with approximately 2.5 gallons of fuel on board. The engine quit… - [Incident 19960602025239I](https://openairdocs.org/incident/19960602025239I), Jun 2, 1996: Diamon DA20A1 (N859DF), Gallup, NM, Minor damage. Narrative: on June 2, 1996, at approximately 0305 zulu, aircraft N859DF, a DV30, landed short of it's intended destination due to fuel starvation. The fuel… - [Accident 19951120037839A](https://openairdocs.org/incident/19951120037839A), Nov 20, 1995: Diamon DA20A1 (N402KT), San Carlos, CA, Substantial damage. Made two attempts to land too fast. On third try landed ballooned twice exited runway. Collided runway sign. ## Service difficulty reports (207, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190429015](https://openairdocs.org/sdr/CA190429015), Apr 29, 2019: PUMP. MALFUNCTIONED. (CAN) AFTER TOUCH-AND-GO, AT 300 FEET AGL, 2 SECONDS AFTER SWITCHING ELECTRIC FUEL PUMP TO OFF, SIGNIFICANT POWER LOSS OCCURRED. ELECTRIC FUEL PUMP WAS SELECTED - [SDR CA180404021](https://openairdocs.org/sdr/CA180404021), Mar 27, 2018: RISER. MISSING. (CAN) REPORTED BY OPERATOR, EXPERIENCED VIBRATIONS DURING FLIGHT, PILOT ELECTED TO RETURN TO FIELD AND LAND, UPON INSPECTION ONE EXHAUST PIPE (RISER) WAS MISSIN - [SDR CA151105010](https://openairdocs.org/sdr/CA151105010), Nov 5, 2015: HINGE. CRACKED. (CAN) DURING A 1000HR SCHEDULED AIRCRAFT INSPECTION, ALL AILERON HINGE BUSHINGS WERE FOUND WORN AND IN NEED OF REPLACEMENT TO REMOVE EXCESSIVE PLAY. UPON CONTRO - [SDR CA150414007](https://openairdocs.org/sdr/CA150414007), Apr 10, 2015: PEDAL. WORN. (CAN) DURING A PRE-FLIGHT CHECK OF THE ACFT, THE PILOT REPORTED THE LT RUDDER PEDAL OF THE CO-PILOT`S RUDDER PEDAL ASSY WOULD JAM IN THE FULL AFT POSITION. UPON - [SDR 2014FA0000625](https://openairdocs.org/sdr/2014FA0000625), Oct 24, 2014: CIRCUIT BREAKER. TRIPPED. PILOT NOTICED THAT THE FLAP LIGHT ON THE FLAP CONTROLLER WAS NOT ILLUMINATED AND THAT THE FLAP CIRCUIT BREAKER HAD TRIPPED. - [SDR CA140925007](https://openairdocs.org/sdr/CA140925007), Sep 25, 2014: ENGINE. SEIZED. (CAN) PILOT REPORTED SMELLING SMOKE, THEN NOTICED ENGINE RUNNING ROUGH, ENGINE STOPPED IN ABOUT 30 SECONDS. PILOT MADE SUCCESSFUL FORCED LANDING, AT THE AIRPORT - [SDR CA140623002](https://openairdocs.org/sdr/CA140623002), Jun 20, 2014: RISER. SHEARED. PILOT REPORT A LOUD NOISE FROM ENGINE. ACFT RETURNED AND A VISUAL INSPECTION WAS CARRIED OUT. THE LT AFT EXHAUST RISER WAS FOUND SHEARED IN HALF. RT AFT RISER W - [SDR CA140505017](https://openairdocs.org/sdr/CA140505017), May 5, 2014: EXHAUST DUCT. BROKEN. (CAN) AFTER TOUCHDOWN PILOTS NOTICE ERRATIC ENGINE INDICATIONS. DURING THEIR COCKPIT MANAGEMENT THE STUDENT NOTICE SMOKE FROM THE COWLING. THE PILOTS NOTIFIED T - [SDR CA130814001](https://openairdocs.org/sdr/CA130814001), Aug 11, 2013: HOSE. SPLIT. (CAN) PILOT REPORTED THAT RED OVERHEAT INDICATOR LIGHT CAME ON IN FLIGHT, PILOT REQUESTED AN IMMEDIATE LANDING FROM THE TOWER AND LANDED WITHOUT INCIDENT. MAINT - [SDR CA130716006](https://openairdocs.org/sdr/CA130716006), Jul 16, 2013: PEDAL. LOOSE. (CAN) DURING A 200 HR INSPECTION THE RT PEDAL WAS FOUND LOOSE. A MORE IN DEPTH INSPECTION, IT WAS FOUND THAT THE BUSHING ON THE INSIDE OF THE LOWER PART OF THE - [SDR CA130221011](https://openairdocs.org/sdr/CA130221011), Feb 21, 2013: TUBE. SPLIT. (CAN) AFTER LANDING AND TAWIING DOWN TAXIWAY, PILOT NOTICED HE HAD A RT FLAT TIRE. ACFT WAS BROUGHT INTO HANGAR, WHEEL REMOVED AND FOUND TUBE WITH A .1250" LONG - [SDR CA130221010](https://openairdocs.org/sdr/CA130221010), Feb 21, 2013: TUBE. SPLIT. (CAN) AFT WAS FOUND WITH RT MAIN TIRE COMPLETELY FLAT DURING THE WALKAROUND. ACFT HAD ALREADY HAD 2 FLIGHTS THAT DAY. WHEEL REMOVED AND FOUND TUBE TO HAVE A .5" - [SDR CA130122004](https://openairdocs.org/sdr/CA130122004), Jan 6, 2013: LIFTER. WORN. (CAN) CYLINDERS REMOVED FOR VALVE LAPPING DUE TO LOW COMPRESSION. LIFTERS FOUND TO HAVE PITTING AND WEAR ON CAM CONTACT SURFACE. CAM LOBES OK BUT SHOWING SOME S - [SDR CA120507019](https://openairdocs.org/sdr/CA120507019), May 4, 2012: LIFTER. FLAT. (CAN) ENGINE CYLINDER COMPRESSION FOUND TO BE LOW AND GETTING LOWER EACH INSPECTION. HEADS REMOVED AND SENT FOR REPAIR. VALVE TRAIN FOUND DAMAGED, INCLUDING VAL - [SDR CA120404006](https://openairdocs.org/sdr/CA120404006), Apr 4, 2012: TUBE. SPLIT. (CAN) ACFT TAXIED OUT TO RUNUP AREA AND THE RT MAIN TIRE SUDDENLY WENT COMPLETELY FLAT. UPON DISSASSEMBLY A .5" LONG SPLIT WAS FOUND IN THE SIDE OF THE TUBE. TH - [SDR CA120319007](https://openairdocs.org/sdr/CA120319007), Mar 17, 2012: TUBE. SPLIT. (CAN) WHILE TAXIING OUT ON TAXIWAY THE RT TIRE SUDDENLY WENT FLAT. THE WHEEL AND TIRE WERE REMOVED AND DISSASSEMBLED AND THE TUBE WAS FOUND TO HAVE A 2" LONG SP - [SDR CA111212002](https://openairdocs.org/sdr/CA111212002), Dec 11, 2011: TUBE. SPLIT. (CAN) WHILE ACFT WAS TAXIING OUT ON TAXIWAY, THE LT MAIN TIRE WENT FLAT. WHEN WHEEL DISSEMBLED TUBE WAS FOUND TO HAVE A .5 INCH LONG SPLIT. THIS HAS BEEN AN ONG - [SDR 2011FA0000726](https://openairdocs.org/sdr/2011FA0000726), Oct 18, 2011: ATTACH BOLT. SHEARED. THE SINGLE BOLT THAT HOLDS VALVE COVER ON THE NR 2 CYLINDER SHEARED IN FLIGHT. ALL OIL LEFT THE ENGINE. EMERGENCY LANDING IN A FIELD. - [SDR CA110607013](https://openairdocs.org/sdr/CA110607013), Jun 6, 2011: TUBE. SPLIT. AFTER LANDING PILOT DISCOVERED RT TIRE WAS FLAT. TIRE WAS REMOVED AND DISSASSEMBLED AND LARGE SPLIT FOUND IN TUBE (THERE WAS NO EVIDENCE OF PUNCTURE). THIS HAS - [SDR CA110601006](https://openairdocs.org/sdr/CA110601006), May 20, 2011: LIFTER. WORN. WHILE TROUBLESHOOTING HIGH OIL CONSUMPTION THE OWNER DISCOVERED UNUSUAL WEAR ON NR 2 EXHAUST LIFTER. THE LIFTER CONTACT SURFACE WAS FOUND TO BE WORN WITH PITTIN - [SDR CA110516011](https://openairdocs.org/sdr/CA110516011), May 13, 2011: TUBE. FAILED. AFTER A NORMAL LANDING, THE PILOT FOUND THE ACFT PULLING TOWARD THE RT AND ENDED UP STOPPING IN GRASS BESIDE THE RUNWAY. FOUND THAT THE RT MAIN TIRE WAS COMPLET - [SDR CA110107005](https://openairdocs.org/sdr/CA110107005), Jan 6, 2011: PIPE. WORN. DURING ROUTINE INSPECTION, IT WAS NOTICED THAT THE SPRINGS, WHICH HOLD THE EXHAUST MUFFLER ON, WERE RUBBING AGAINST THE RIGHT RADIATOR PIPE. PIPE WAS REMOVED FO - [SDR CA101126004](https://openairdocs.org/sdr/CA101126004), Nov 24, 2010: IGNITION SWITCH. DAMAGED. ENGINE STARTED WHEN PROP WAS ROTATED TO CHECK OIL LEVEL AS PER POH. IGNITION SWITCH WAS OFF AND KEY REMOVED. IGNITION SWITCH FOUND TO HAVE CARBON TRACKING BETWE - [SDR CA100729002](https://openairdocs.org/sdr/CA100729002), Jul 24, 2010: TUBE. CUT. FOLLOWING A NORMAL LANDING, THE ACFT SUFFERED A FLAT TIRE ON TAXI BACK TO THE RAMP. UPON DISASSEMBLY OF THE WHEEL, IT WAS DISCOVERED THAT THE INNER TUBE WAS CUT - [SDR CA100726013](https://openairdocs.org/sdr/CA100726013), Jul 21, 2010: LEG ASSY. FAILED. AFTER START-UP ON THE GRASS APRON, THE ACFT NLG FAILED AT THE AXLE WHILE TAXIING, 1 BLADE OF PROPELLER STRUCK GROUND AND TIP SEPARATED. - [SDR CA100907006](https://openairdocs.org/sdr/CA100907006), Jun 11, 2010: BOLT. MISSING. DURING ANNUAL INSP, DISCOVERED EXCESSIVE FORE AND AFT PLAY IN RT WING, PN 22-5708-00-00WIP. MX RECORD REVIEW INDICATED THAT THE RT WING WAS REPLACED ON 4/25/09. - [SDR CA100208008](https://openairdocs.org/sdr/CA100208008), Feb 3, 2010: BRACKET. LOOSE. (CAN) ELT DEPARTED MOUNTING BRACKET. THE CORRECT PIN BRACKET IS USED. MOUNTED IN THE FACTORY LOCATION. THE ELT WAS PLACED CORRECTLY IN THE BRACKET WITH THE LANY - [SDR CA100115003](https://openairdocs.org/sdr/CA100115003), Jan 14, 2010: HOUSING. DAMAGED. (CAN) WHEN PERFORMING OTHER MX, OIL LINE FROM THE OIL PUMP TO THE GOVERNOR NEEDED TO BE LOOSENED. WHEN ATTEMPTING TO TIGHTEN THE OIL LINE BANJO BOLT TO THE SPEC - [SDR CA091007006](https://openairdocs.org/sdr/CA091007006), Oct 5, 2009: SLEEVE. SLIPPED. (CAN) INSTRUCTOR AND STUDENT WERE PRACTICING SIDE-SLIPS AND THE LT RUDDER CABLE BROKE FREE OF AFT RUDDER BELLCRANK. INSP REVEALED CABLE PULLED OUT OF NICO PRESS - [SDR CA091021013](https://openairdocs.org/sdr/CA091021013), Sep 23, 2009: THROTTLE CABLE. BROKEN. (CAN) TWO CONTROL CABLES ARE BOLTED TO A SINGLE THROTTLE CONTROL LEVER IN THE CABIN PEDESTAL. THESE INNER CABLES ARE THEN ROUTED THROUGH THEIR OWN RESPECTIVE OU - [SDR CA090928014](https://openairdocs.org/sdr/CA090928014), Sep 21, 2009: CONTROL CABLE. WORN. (CAN) FWD 4 RUDDER CABLES ARE ROUTED FROM RUDDER PEDAL ASSYS TO RUDDER BELLCRANK (AFT OF THE MAIN SPAR) THROUGH NYLON GUIDE TUBES THAT PASS UNDER THE SPAR THROU - [SDR CA090806011](https://openairdocs.org/sdr/CA090806011), Aug 5, 2009: ENCODER. MALFUNCTIONED. WHEN VHF COM WAS KEYED, THE MODE C ALTITUDE REPORTING WOULD JUMP BY 200 TO 500 FEET. REPLACED SSD120 ALTITUDE ENCODER WITH NEW SSD120 ENCODER CORRECTED DEFECT. - [SDR CA090812004](https://openairdocs.org/sdr/CA090812004), Jul 30, 2009: OIL SYSTEM. LEAKING. A STUDENT PILOT PERFORMED AN OVERSHOOT OF THE RUNWAY AS REQUESTED BY TOWER AND EXPERIENCED ROUGH RUNNING ENG WHICH GOT PROGRESSIVELY WORSE UNTIL THE ENG QUIT, S - [SDR CA081218001](https://openairdocs.org/sdr/CA081218001), Dec 8, 2008: SKIN. CRACKED. (CAN) DURING ROUTINE MAINTENANCE, A 1 1/2 INCH LONG CRACK WAS NOTICED IN THE LEADING EDGE OF THE HORIZONTAL STABILIZER. TAP TESTING INDICATED POSSIBLE DELAMINAT - [SDR CA071218001](https://openairdocs.org/sdr/CA071218001), Dec 8, 2007: HOSE. LEAKING. (CAN) PILOT LANDED NORMALLY AND SHUTDOWN AFTER NOTICING FALLING OIL PRESSURE INDICATION. THIS WAS ON INITIAL TEST FLIGHT OF A NEW ENGINE INSTALLATION, ON INSPEC - [SDR CA070911014](https://openairdocs.org/sdr/CA070911014), Aug 16, 2007: RUDDER PEDAL. WORN. (CAN) THE LT PILOT SIDE RUDDER CABLE PASSES THROUGH A TUBE ON THE PILOT RUDDER PEDAL. THIS TUBE WEARS AWAY DUE TO CHAFING AND IS UNDETECTABLE UNTIL THE CABLE HA - [SDR 2006FA0000482](https://openairdocs.org/sdr/2006FA0000482), May 1, 2006: ELT. MISINSTALLED. WHEN REMOVING ELT FROM AIRCRAFT TO REPLACE ELT BATTERY, FOUND THAT SOMEONE HAD PUT THE ELT IN BACKWARDS. THE DIRECTION OF FLIGHT ARROW WAS POINTING AFT. THIS IN - [SDR CA050301002](https://openairdocs.org/sdr/CA050301002), Mar 1, 2005: SPRAG CLUTCH. LOOSE. (CAN) ENG WAS FOUND TO HAVE SEVERAL OIL LEAKS AND HARD STARTING. DURING INSP IT WAS NOTED THAT CRANKCASE SEALANT WAS NOT IAW MFG REC. SEALANT HAD RUBBERY/SILICO - [SDR CA041122002](https://openairdocs.org/sdr/CA041122002), Nov 14, 2004: ENGINE. FAILED. (CAN) SMOKE ENTERED COCKPIT. PILOT RETURNED TO BASE. ENGINE LOST POWER AND BEGAN TO MISSON FINAL AND WAS SHUT DOWN. - [SDR CA040219001](https://openairdocs.org/sdr/CA040219001), Feb 16, 2004: EXHAUST STACK. BROKEN. (CAN) THE RT REAR EXHAUST STACK WAS FOUND TO BE COMPLETELY FRACTURED IN TWO AT THE BEND NEAR THE CYLINDER HEAD. THIS FAILURE IS THE SECOND COMPLETE FRACTURE NOT - [SDR CA040213003](https://openairdocs.org/sdr/CA040213003), Feb 9, 2004: EXHAUST STACK. CRACKED. (CAN) THE RT REAR EXHAUST STACK WAS FOUND CRACKED APPROX .5000 WAY AROUND THE CIRCUMFERENCE AT THE BEND NEAR THE CYLINDER. THIS CRACK WAS IN A SIMILAR LOCATION - [SDR CA040213001](https://openairdocs.org/sdr/CA040213001), Feb 9, 2004: EXHAUST STACK. FRACTURED. (CAN) THE LT REAR EXHAUST STACK WAS FOUND COMPLETELY BROKEN AND SEPARATED AT THE BEND NEAR THE CYLINDER. - [SDR CA040203013](https://openairdocs.org/sdr/CA040203013), Jan 23, 2004: MUFFLER. BROKEN. (CAN) TAILPIPE NEARLY SNAPPED OFF FROM MUFFLER, INTERNAL BAFFLES LOOSE AND OBSTRUCTING EXHAUST OUTLET PART, CAUSING THE BACK PRESSURE TO RISE AND FAILURE OF TAI - [SDR CA040108005](https://openairdocs.org/sdr/CA040108005), Dec 31, 2003: SPRING. BROKEN. (CAN) THE LT CANOPY SPRING CLIPS BROKE OFF AT BOTH ENDS OF THE CANOPY SPRING SIMULTANEOUSLY. THE ENERGY RELEASED DURING THE FAILURE WAS SUFFICIENT TO ALLOW ONE - [SDR CA031223006](https://openairdocs.org/sdr/CA031223006), Dec 19, 2003: SOCKET. CRACKED. (CAN) A CRACKED DEVELOPED AROUND APPROX. .5000 THE CIRCUMFERENCE OF THE SOCKET ABOUT .2500 INCH BEYOND THE TREADS. THE LOCATION OF THE CRACK IS APPROX. COINCIDE - [SDR CA031008004](https://openairdocs.org/sdr/CA031008004), Oct 6, 2003: DIAPHRAGM. SWOLLEN. (CAN) WHEN THE CARBURETOR WAS DISASSEMBLED THE DIAPHRAGM WAS FOUND TO BE SWOLLEN AND WHEN INSTALLED IN THE CARBURETOR IT DID NOT SEAT PROPERLY. THE AIRCRAFT IS - [SDR CA031008003](https://openairdocs.org/sdr/CA031008003), Oct 6, 2003: DIAPHRAGM. SWOLLEN. (CAN) WHEN THE CARB WAS DISASSEMBLED THE DIAPHRAGM WAS FOUND TO HAVE SWOLLEN AND WAS BUBBLED UP WHEN INSTALLED IN THE CARBURETOR. THE AIRCRAFT OPERATES PRIMARIL - [SDR CA030730003](https://openairdocs.org/sdr/CA030730003), Jul 21, 2003: EXHAUST PIPE. CRACKED. (CAN) NOTED SLIGHT DISCOLORATION OF COWL ON ROUTINE DAILY INSPECTION, REMOVED UPPER COWL FOUND LOWER COWLING WITH SLIGHT BURNED AREA AROUND NR 1 CYLINDER REMOVE - [SDR CA030730004](https://openairdocs.org/sdr/CA030730004), Jul 7, 2003: EXHAUST PIPE. CRACKED. (CAN) DURING ENGINE ROUTINE INSPECTION, WE NOTICED SOME DISCOLORATION ON THE EXHAUST WRAP WHEN COWLS WAS REMOVED (SB 20 78 04A). WHEN EXHAUST WRAP WAS REMOVED, - [SDR CA030627017](https://openairdocs.org/sdr/CA030627017), Jun 27, 2003: STOP. BROKEN. (CAN) THE ELEVATOR STOP WAS FOUND BROKEN OFF THE RT ELEVATOR HINGE BLOCK. EXTENSIVE CORROSION WAS FOUND IN THE AREA OF THE FAILURE. THE AIRCRAFT WAS OPERATED FO All 207: https://openairdocs.org/model/diamond-aircraft-ind-da20-a1/reports.md ## STCs that may be installed (OpenAirDocs) (81, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA12066IB](https://openairdocs.org/stc/SA12066IB): Installation of the MT-Propeller Entwicklung GmbH model MTV-21-A/170-05 propeller. MT-Propeller Entwicklung GmbH - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA11838IB](https://openairdocs.org/stc/SA11838IB): Installation of the MT-Propeller Entwicklung GmbH model MTV-21-A/170-05. MT-Propeller Entwicklung GmbH - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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 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 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 SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [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 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 SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc - [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc - [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 SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC All 81: https://openairdocs.org/model/diamond-aircraft-ind-da20-a1/stcs.md ## PMA parts (OpenAirDocs) (101, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [066-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151613801320260723131532.0001): Rivet. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026 - [066-106](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133993339720260728184415.0001): Brake Lining. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026 - [RAP164-24200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174359675820250829181752.0001): Brake Disc. Rapco Inc · PMA PQ2101CE · Replaces 164-24200 Cleveland · Aug 27, 2025 - [TAU03323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141518357520240221143038.0001): AV/Cabin Heat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Dec 14, 2023 - [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127691626620230707211316.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023 - [APS66-10600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102361413820221020170314.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10600 · Aug 10, 2022 - [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID238148476420210921142542.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID232909988720210702175220.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021 - [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020 - [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020 - [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020 - [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020 - [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/80F9B5EC9801FD16862586330061456E.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020 - [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID670268927520220125131357.0001): DAC International · PMA PQ0986SW · Jul 31, 2020 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID572288387520220125131340.0001): DAC International · PMA PQ0986SW · Jul 31, 2020 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID518702817320220125131321.0001): DAC International · PMA PQ0986SW · Jul 31, 2020 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID509142493720220125131503.0001): DAC International · PMA PQ0986SW · Jul 31, 2020 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID310362461920220125131416.0001): DAC International · PMA PQ0986SW · Jul 31, 2020 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106265693420220125131440.0001): DAC International · PMA PQ0986SW · Jul 31, 2020 - [V674UL94](https://drs.faa.gov/browse/excelExternalWindow/26465837A7672E7A86258583004BE923.0001): UL94 Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Nov 25, 2019 - [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [9100-001-H](https://drs.faa.gov/browse/excelExternalWindow/1AEB415100FB45D8862585690040159F.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019 - [01-0771833-20](https://drs.faa.gov/browse/excelExternalWindow/FFF505DF238D9E3E86258557004EB967.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0771833-25](https://drs.faa.gov/browse/excelExternalWindow/D17366A21258BFC186258557004EB9A2.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0771833-10](https://drs.faa.gov/browse/excelExternalWindow/D0F0E113B870DF1C86258557004EB8E0.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0771833-15](https://drs.faa.gov/browse/excelExternalWindow/CB6A5B42DF6A574686258557004EB925.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0790750-10](https://drs.faa.gov/browse/excelExternalWindow/8FBCEA35A3837D6386258557004EB9D7.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [01-0790750-20](https://drs.faa.gov/browse/excelExternalWindow/5919E033D600DA3386258557004EBA0C.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019 - [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/CB6B45C441A97D20862585510065ECA1.0001): SkyTrax 100B. Avidyne Corporation · PMA PQ4035CE · Replaces N/A · May 13, 2019 - [87-05208-001](https://drs.faa.gov/browse/excelExternalWindow/C4B8A8A2B2422B728625822E007853B6.0001): Assembly, Light, PAR 46 Landing. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0790750-20 · Jan 23, 2018 - [87-05207-002](https://drs.faa.gov/browse/excelExternalWindow/4BE4BA39295AB01E862581760058C64D.0001): Assembly, Light, PAR 36 Taxi. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0771833-25 · Aug 1, 2017 - [87-05207-001](https://drs.faa.gov/browse/excelExternalWindow/4ACD6BDF5990D9C7862581760058C571.0001): Assembly, Light, PAR 36 Landing. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0771833-20 · Aug 1, 2017 - [W-2763-DR](https://drs.faa.gov/browse/excelExternalWindow/9BC49150DA5F709A86257FE90065596C.0001): Diamond Wing Landing Light Lens Cover (Drilled). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces D41-3347-51-90 · Jun 29, 2016 - [W-2763](https://drs.faa.gov/browse/excelExternalWindow/1831473B774D874186257FE9006558CD.0001): Diamond Wing Landing Light Lens Cover (Undrilled). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces D41-3347-51-90, 20-3350-01-01 · Jun 29, 2016 - [01-0771833-20](https://drs.faa.gov/browse/excelExternalWindow/C4A392C20DA3333A86257FCC006EBC03.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016 - [01-0771833-25](https://drs.faa.gov/browse/excelExternalWindow/618915409FDEC97186257FCC006EBC05.0001): LED Taxi Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016 - [01-0771833-15](https://drs.faa.gov/browse/excelExternalWindow/466B93ACC46B636486257FCC006EBC01.0001): LED Taxi Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016 - [01-0771833-10](https://drs.faa.gov/browse/excelExternalWindow/3073DD83C9E2984D86257FCC006EBBFD.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016 - [01-0790750-20](https://drs.faa.gov/browse/excelExternalWindow/2D8AB0D7C6000CA786257FCA00724738.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016 - [01-0790750-10](https://drs.faa.gov/browse/excelExternalWindow/0ABFC613100772D586257FCA00724733.0001): LED Landing Light. Whelen Engineering Co Inc · PMA PQ0610NE · Modification part · Apr 20, 2016 - [LSM-500-122](https://drs.faa.gov/browse/excelExternalWindow/B813BC1475317B1A86257F0F006403C5.0001): Installation Instructions, LZR LED. LoPresti Speed Merchants · PMA PQ1372CE · Modification part · Oct 27, 2015 All of them: https://openairdocs.org/model/diamond-aircraft-ind-da20-a1/pma.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.