# Meyers Industries 200A

- Type: Aircraft model (FAA registry)
- Registry code: 5650304
- Manufacturer (registry): MEYERS INDUSTRIES INC
- Model: 200A
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 4
- Weight class: Up to 12,499 lb
- Cruise speed: 153 mph
- Certification: Type certificated
- Data sheet: [TCDS 3A18](https://openairdocs.org/tcds/3A18) (OpenAirDocs)
- Holder: Interceptor Aircraft Inc
- Registered aircraft: 5
- Page: https://openairdocs.org/model/meyers-industries-200a

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 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 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 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 67-23-01](https://openairdocs.org/ad/67-23-01): Main Landing Gear · Interceptor 200, 200A, 200B and 2 more. Effective Aug 15, 1967
- [AD 66-28-01](https://openairdocs.org/ad/66-28-01): Elevator Trim System · Interceptor 200, 200A, 200B and 2 more. Effective Nov 19, 1966

## Information bulletins (advisory) (1)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018

## Registered aircraft (5)

- [N34380](https://openairdocs.org/aircraft/N34380): [Ackerman Kurt](https://openairdocs.org/faa-owner/ACKERMAN%20KURT), [Kingman, AZ](https://openairdocs.org/faa-place/AZ/Kingman), built 1960, S/N 262
- [N485C](https://openairdocs.org/aircraft/N485C): [Sundale Aviation Inc](https://openairdocs.org/faa-owner/SUNDALE%20AVIATION%20INC), [Erwinna, PA](https://openairdocs.org/faa-place/PA/Erwinna), built 1959, S/N 253
- [N492C](https://openairdocs.org/aircraft/N492C): [Smith David W](https://openairdocs.org/faa-owner/SMITH%20DAVID%20W), [Milaca, MN](https://openairdocs.org/faa-place/MN/Milaca), S/N 256
- [N495C](https://openairdocs.org/aircraft/N495C): [Smith David W](https://openairdocs.org/faa-owner/SMITH%20DAVID%20W), [Milaca, MN](https://openairdocs.org/faa-place/MN/Milaca), S/N 259
- [N749C](https://openairdocs.org/aircraft/N749C): [Thermoplastic Services Inc](https://openairdocs.org/faa-owner/THERMOPLASTIC%20SERVICES%20INC), [Dequincy, LA](https://openairdocs.org/faa-place/LA/Dequincy), built 1960, S/N 261

## NTSB investigations (13)

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 CEN22LA252](https://openairdocs.org/ntsb/CEN22LA252), Jun 16, 2022: Meyers Industries 200A (N489C), Weslaco, TX, substantial damage. Probable cause: A total loss of engine power for reasons that could not be determined.
- [NTSB ERA21LA235](https://openairdocs.org/ntsb/ERA21LA235), May 26, 2021: Meyers Industries 200A (N489C), Marathon, FL, substantial damage. Probable cause: The failure of the right main landing gear to fully extend during landing as a result of the underinflated right main landing gear oleo strut.
- [NTSB CHI01LA112](https://openairdocs.org/ntsb/CHI01LA112), Apr 2, 2001: Meyers 200A (N495C), Tecumseh, MI, substantial damage. Probable cause: The fuel starvation. Factors were the loose line at the distribution valve, the inadequate annual inspection the owner/pilot mechanic performed, the unsuitable terrain the pilot encountered during…
- [NTSB FTW96LA079](https://openairdocs.org/ntsb/FTW96LA079), Dec 27, 1995: Meyers MY-200A (N484C), Madill, OK, substantial damage. Probable cause: the deterioration of the fuel supply line resulting in line blockage, fuel starvation, and subsequent loss of engine power. A factor was the lack of suitable terrain for the forced landing.
- [NTSB FTW80DRA14](https://openairdocs.org/ntsb/FTW80DRA14), Dec 20, 1979: Meyers 200 (N495C), La Porte, TX, substantial damage
- [NTSB NYC77FGM20](https://openairdocs.org/ntsb/NYC77FGM20), Apr 18, 1977: Meyers 200A (N485C), West Mifflin, PA, substantial damage
- [NTSB CHI77FEC18](https://openairdocs.org/ntsb/CHI77FEC18), Feb 23, 1977: Meyers 200A (N494C), Monroe, MI, substantial damage
- [NTSB CHI71FEI46](https://openairdocs.org/ntsb/CHI71FEI46), Mar 24, 1971: Meyers 200-A (N34398), Vermilion, OH, destroyed
- [NTSB OAK70F0098](https://openairdocs.org/ntsb/OAK70F0098), Aug 2, 1969: Myers 200A (N489C), Vacaville, CA, substantial damage
- [NTSB SEA67D0239](https://openairdocs.org/ntsb/SEA67D0239), Feb 10, 1967: Meyers 200-A (N34381), Pomeroy, WA, destroyed
- [NTSB LAX66F0160](https://openairdocs.org/ntsb/LAX66F0160), Oct 23, 1965: Meyers 200A (N484C), Hawthorne, CA, substantial damage
- [NTSB CHI65F0114](https://openairdocs.org/ntsb/CHI65F0114), Mar 30, 1965: Meyers 200A (N495C), Kokomo, IN, substantial damage
- [NTSB UNK64X1410](https://openairdocs.org/ntsb/UNK64X1410), Apr 22, 1964: Meyers 200A (N34398), Washington, DC, substantial damage

## FAA accident and incident reports (15)

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 20220616010459A](https://openairdocs.org/incident/20220616010459A), Jun 16, 2022: Meyers Industries Inc 200A (N489C), Weslaco, TX, Substantial damage. [privacy data omitted], A Meyers M200, took off from (ktxw) with approximately 65 gallons on board. Pilot reports that he was running off the right full aft…
- [Accident 20210526010109A](https://openairdocs.org/incident/20210526010109A), May 26, 2021: Meyers Industries Inc 200A (N489C), Marathon, FL, Substantial damage. Aircraft landed on runway with right main landing gear retracted.
- [Incident 20110519009439I](https://openairdocs.org/incident/20110519009439I), May 19, 2011: Meyers Industries Inc 200A (N749C), Lebanon, TN, Minor damage. Aircraft was taxiing to runway for first flight of the day. Right main gear collapsed while making a slow speed left turn.
- [Incident 20010602015219I](https://openairdocs.org/incident/20010602015219I), Jun 2, 2001: Propjt 200A (N492C), Cape Girardeau, MO, Minor damage. (-23) Pilot (martindale) was not able to fully extend left main gear on final approach to Cape Girardeau Municipal Airport (cgi). Pilot (martindale) contacted…
- [Accident 20010402011839A](https://openairdocs.org/incident/20010402011839A), Apr 2, 2001: Propjt 200A (N495C), Tecumseh, MI, No damage. (-23) Aircraft had taken off from Tecumseh airport (3TE) on runway 36, after clearing runway and retracting gear. The engine lost power. Aircraft stalled and…
- [Incident 19991121035589I](https://openairdocs.org/incident/19991121035589I), Nov 21, 1999: Propjt 200A (N492C), Austin, TX. (-23) Aircraft was inbound for landing at Austin international airport, runway 17L. On final, the engine failed (seized). Pilot landed aircraft in the field…
- [Accident 19951227042599A](https://openairdocs.org/incident/19951227042599A), Dec 27, 1995: Propjt 200A (N484C), Madill, OK, Substantial damage. Engine quit on climbout. Tried return. Hit a dtich short of runway. Rubber fuel line delaminated. Rubber fouled lin
- [Incident 19950622021339I](https://openairdocs.org/incident/19950622021339I), Jun 22, 1995: Propjt 200A (N492C), Portland, ME, Minor damage. Landed right gear still up. Tried all ideas but no green. Beleived light out. Gear dolor cable out of adjustment.
- [Incident 19931209051579I](https://openairdocs.org/incident/19931209051579I), Dec 9, 1993: Propjt 200A (N749C), New Orleans, LA, Minor damage. Pilot lost control on landing rollout. Veered left and stopped. Found left main gear scissors had broke.
- [Incident 19900421021259I](https://openairdocs.org/incident/19900421021259I), Apr 21, 1990: Propjt 200A (N484C), Ft Lauderdale, FL. Fuel exhaustion on short final. Landed short on grass. Ran tank dry and did not switch tanks.
- [Incident 19810824051509I](https://openairdocs.org/incident/19810824051509I), Aug 24, 1981: Intrcp 200A (N484C), Grant, NE, Substantial damage. Unsafe gear indication. Nose gear collapsed on landing. Found stearing horn broken. Probably when towed by tractor.
- [Accident 19791220033249A](https://openairdocs.org/incident/19791220033249A), Dec 20, 1979: Propjt 200A (N495C), Laporte, TX, Substantial damage. Engine quit shortly after takeoff. Landed wheels up in open field. Found fuel selector on empty tank.
- [Incident 19791219046269I](https://openairdocs.org/incident/19791219046269I), Dec 19, 1979: Propjt 200A (N484C), North Platte, NE, Minor damage. Left main gear folded after landing, cause unknown. Hydraulic system could not be checked.
- [Accident 19770418008719A](https://openairdocs.org/incident/19770418008719A), Apr 18, 1977: Intrcp 200A (N485C), West Mifflin, PA, Substantial damage. Struck rwy light.
- [Accident 19770223004179A](https://openairdocs.org/incident/19770223004179A), Feb 23, 1977: Intrcp 200A (N494C), Monroe, MI, Substantial damage

## Service difficulty reports (44)

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

- [SDR CA160322007](https://openairdocs.org/sdr/CA160322007), Mar 10, 2016: RELAY. STUCK. (CAN) LEFT HAND TRUST REVERSER FAIL CAS MESSAGE WAS DISPLACED ON MFD. DURING TROUBLE SHOOTING FOUND STOW AND DEPLOY HARNESS SWITCH WAS FOUND TO BE AT FAULT. REP
- [SDR CA160120005](https://openairdocs.org/sdr/CA160120005), Jan 6, 2016: OIL SYSTEM. LEAKING. (CAN) DURING FLIGHT, WHEN CREW REDUCED POWER DURING LANDING RUN, A STRONG OIL ODOR AND SMOKE IN CABIN WAS NOTICED. SMOKE OUT OF THE TAIL PIPE WAS ALSO REPORTED 
- [SDR CA151229006](https://openairdocs.org/sdr/CA151229006), Dec 21, 2015: ENGINE. LEAKING. (CAN) THE OPERATOR REPORTED THAT UPON DEPARTURE THAT THE CABIN FILLED WITH OIL MIST. THE ACFT RETURNED TO THE POINT OF DEPARTURE. GROUND INSPECTION OF THE ACFT 
- [SDR CA151203012](https://openairdocs.org/sdr/CA151203012), Dec 2, 2015: TERMINAL BLOCK. LOOSE. (CAN) DURING TROUBLESHOOTING OF AN FMS UNIT BACKLIGHT FAILURE IT WAS FOUND THAT THERE WERE LOOSE CONNECTIONS ON A TERMINAL BLOCK IN THE LT COCKPIT JUNCTION PANE
- [SDR CA151117018](https://openairdocs.org/sdr/CA151117018), Nov 11, 2015: UNKNOWN. ODOR. (CAN) THE AIRCRAFT RETURN TO ORIGIN DUE TO AN OIL SMOKE ODOR IN THE CABIN AT 2000 FT WITH THE APU OFF. UPON TAKEOFF, THE CABIN AND COCKPIT FILLED WITH SMOKE. TE
- [SDR CA151007004](https://openairdocs.org/sdr/CA151007004), Sep 28, 2015: UNKNOWN. ODOR. (CAN) THE OPERATOR REPORTED AN OIL ODOR IN THE CABIN. TROUBLESHOOTING ONGOING.
- [SDR CA151007003](https://openairdocs.org/sdr/CA151007003), Sep 28, 2015: ENGINE. LEAKING. (CAN) CUSTOMER REPORTED SMOKE IN CABIN DURING CLIMB AND THEY TURNED BACK WITHOUT ANY INCIDENT. DURING TROUBLESHOOTING, MAINTENANCE DISCOVERED BLEED AIR WAS FULL
- [SDR CA150728003](https://openairdocs.org/sdr/CA150728003), Jul 21, 2015: ENGINE. LEAKING. (CAN) AIRCRAFT WAS AT LEVEL FLIGHT 35.0 K WHEN CREW NOTICED RT ENGINE LEAK INDICATION. NOT LONG AFTER THAT, PASSENGERS ON BOARD STARTED NOTICING A SMOKE/OIL SME
- [SDR CA141024014](https://openairdocs.org/sdr/CA141024014), Oct 6, 2014: WARNING MESSAGE. ILLUMINATED. (CAN) THE ACFT POSTED A POWERPLANT FAIL MESSAGE DURING TAKEOFF. THE PILOT RETURNED TO BASE TO ADVISE THE MAINTENANCE CREW OF THE EVENT. THE MAINTENANCE CREW CON
- [SDR CA140826032](https://openairdocs.org/sdr/CA140826032), Aug 21, 2014: WARNING MESSAGE. FALSE ACTIVATION. (CAN) THE CREW NOTICED LEFT HAND FADEC FAULTY DURING TAKEOFF ATTEMPT. TAKE OFF WAS ABORTED AND AIRCRAFT RETURNED TO HANGAR. CREW NOTED 4C MAINTENANCE CODE FLAGG
- [SDR CA140804007](https://openairdocs.org/sdr/CA140804007), Jul 24, 2014: ENGINE. LEAKING. (CAN) DURING CRUISE FLIGHT, SMOKE IN THE CABIN WAS OBSERVED. THE AIRCRAFT DIVERTED, WHERE THE PROBLEM WAS ISOLATED TO ONE OF THE ENGINES DURING POST-FLIGHT INSP
- [SDR CA140701005](https://openairdocs.org/sdr/CA140701005), Jun 2, 2014: ENGINE. VIBRATION. (CAN) DURING CRUISE IT WAS REPORTED THAT THERE WAS AN ENGINE HARMONICS VIBRATION ISSUE AND OBVIOUS HARMONIC SOUND WAS NOTICED. DURING THE "ON GROUND TROUBLESHOO
- [SDR CA140602025](https://openairdocs.org/sdr/CA140602025), May 28, 2014: INDICATION SYS. MALFUNCTIONED. (CAN) DURING CRUISE, REPORTED HIGH OIL PRESSURE, 175 PSI, ON RIGHT ENGINE. REDUCED THE POWER ON THE RIGHT ENGINE TO IDLE & THE OIL PRESSURE READING RETURNED TO 
- [SDR CA140117001](https://openairdocs.org/sdr/CA140117001), Dec 22, 2013: CASE. DAMAGED. (CAN) DURING TAKEOFF PROCEDURE, THE PILOT WAS NOT ABLE TO ACHIEVE REQUIRED THRUST DO TO OVER TEMPERATURE INDICATION. AFTER INVESTIGATION AND A REPAIR OF THE FAN
- [SDR CA130729003](https://openairdocs.org/sdr/CA130729003), Jul 16, 2013: OIL SYSTEM. FLUCTUATES. (CAN) DURING CLIMB AT FL50, THE OIL PRESSURE FLUCTUATED AND THEN DROPPED TO 0. THE ENGINE WAS SHUTDOWN AND THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE AN U
- [SDR CA130416007](https://openairdocs.org/sdr/CA130416007), Apr 2, 2013: OIL SYSTEM. LOW PRESSURE. (CAN) ABORTED TAKEOFF, DUE TO LOW OIL PRESSURE WARNING ON NR 2 ENGINE DURING TAKEOFF ROLL. THE OIL PRESSURE DROPPED TO ZERO. TROUBLESHOOTING IS ON-GOING.
- [SDR CA130401003](https://openairdocs.org/sdr/CA130401003), Mar 18, 2013: OIL SYSTEM. LEAKING. (CAN) THE CUSTOMER REPORTED THAT SMOKE AND THE ODOR OF OIL ENTERED THE CABIN DURING TAKE-OFF. THE ON GROUND INVESTIGATION REVEALED A LARGE QUANITY OF OIL IN THE
- [SDR CA130318003](https://openairdocs.org/sdr/CA130318003), Mar 8, 2013: ENGINE. POWER LOSS. (CAN) AFTER A NORMAL STARTUP, APPROXIMATELY 10 SECONDS INTO TAXI, THE LT ENGINE FAN SPEED N1 DROPPED TO 12 PERCENT AND THE ENGINE TEMPERATURE ROSE TO 900C. TROU
- [SDR CA130212016](https://openairdocs.org/sdr/CA130212016), Feb 5, 2013: COMPRESSOR. STALLED. (CAN) DURING THE TAKEOFF PROCEDURE, LOUD NOISE OCCURRED DURING THE ACCELERATION ASSOCIATED WITH A SEVERE VIBRATION NOTED BY THE PASSENGERS. THE CREW ABORTED THE
- [SDR CA121119017](https://openairdocs.org/sdr/CA121119017), Nov 11, 2012: ENGINE. OVERTEMP. (CAN) DURING DESCENT, WITH HEAT ON, THE ENGINE TEMPERATURE INCREASED AND STARTED FLASHING RED. THE THROTTLE WAS RETARDED TO IDLE AND THE TEMPERATURE STABILIZED 
- [SDR CA120813004](https://openairdocs.org/sdr/CA120813004), Aug 1, 2012: UNKNOWN. SMOKE. (CAN) DURING REVENUE FLIGHT, ON DESCENT CREW NOTICED SMOKE IN CABIN. SMOKE DISAPPEARED AS RT CABIN BLEED WAS SELECTED OFF. PROBLEM RESURFACED ON SECOND FLIGHT L
- [SDR CA120802006](https://openairdocs.org/sdr/CA120802006), Jul 23, 2012: COMPRESSOR. STALLED. (CAN) THE ENGINE HAD A COMPRESSOR STALL DURING ACCELERATION AND CLIMBOUT, AND WHEN THE THROTTLE WAS PULLED BACK THE ENGINE STABILIZED. THE CREW ELECTED TO RETUR
- [SDR CA120802002](https://openairdocs.org/sdr/CA120802002), Jul 18, 2012: BLADE. DAMAGED. (CAN) 5 MINUTES AFTER T/O, A "PLASTIC" ODOR WAS NOTED IN THE CABIN, FOLLOWED BY A MIST AND SMOKE. AN EMERGENCY RETURN TO THE DEPARTURE POINT WAS MADE AND AN UNE
- [SDR CA120723010](https://openairdocs.org/sdr/CA120723010), Jul 18, 2012: UNKNOWN. ODOR. (CAN) DURING REVENUE FLIGHT, 5 MINUTES AFTER TAKEOFF, FLIGHT CREW REPORTED ODOR OF BURNING PLASTIC IN THE CABIN WITH A MIST OF SMOKE. PILOTS DECLARED EMERGENCY 
- [SDR CA120702011](https://openairdocs.org/sdr/CA120702011), Jun 28, 2012: FUEL CONTROL. UNKNOWN. (CAN) IN FLIGHT RECEIVED L/T FADEC FAULTY ICAS MSG AND EICAS COMPARITOR FAIL WITH YELLOW DASH LINES IN THE ITT. ABOUT 5 MIN LATER WE FELT A LIGHT SHUTTER ASSOCI
- [SDR CA111114014](https://openairdocs.org/sdr/CA111114014), Nov 6, 2011: UNKNOWN. SMOKE. (CAN) AFTER TAKEOFF, SMOKE APPEARED IN THE CABIN. THE CREW ELECTED TO ABORT THE FLIGHT AND RETURN TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL LANDING WAS ACCOM
- [SDR CA111030007](https://openairdocs.org/sdr/CA111030007), Oct 18, 2011: UNKNOWN. SMOKE. (CAN) DURING CLIMB AFTER T/O, THE CABIN FILLED WITH SMOKE AT APPROXIMATELY 400 FT ALTITUDE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO THE DEPARTURE AIR
- [SDR CA111019001](https://openairdocs.org/sdr/CA111019001), Oct 6, 2011: UNKNOWN. HAZE. (CAN) FOLLOWING TROUBLESHOOTING FOR THE SAME PROBLEM ON OCT 2ND, THE CABIN BLEED DUCT FOR THE RT ENGINE WAS CLEANED AND THE OIL PUMP WAS REPLACED IAW SB 25299. 
- [SDR CA110330007](https://openairdocs.org/sdr/CA110330007), Mar 25, 2011: LINE. MISINSTALLED. (CAN) ON DAILY INSPECTIONS THE ENGINEERS NOTICED A SLOW TRANSFER OF HYDRAULIC FLUID FROM ONE THE LEFT HYDRAULIC SYSTEM TO THE RIGHT HYDRAULIC SYSTEM AFTER A SER
- [SDR CA110315008](https://openairdocs.org/sdr/CA110315008), Mar 10, 2011: UNKNOWN. ODOR. (CAN) OIL SMOKE & ODOR IN CABIN DURING TAKE OFF, THE CREW EXPERIENCED SMOKE AND OIL ODOR IN THE CABIN NEAR 700 FEET. THE A/C SAFELY RETURNED TO THE POINT OF DEP
- [SDR CA101122009](https://openairdocs.org/sdr/CA101122009), Nov 18, 2010: ENGINE. VIBRATION. (CAN) PILOT COMMANDED IFSD WHILE ON HOLD FOR TAKEOFF, AS POWER WAS INCREASED, A LOUD NOISE WAS HEARD WITH AN AMBER WARNING LIGHT ON THE COCKPIT VIBRATION INDICA
- [SDR CA101004009](https://openairdocs.org/sdr/CA101004009), Oct 1, 2010: ACTUATOR. FAILED. SEPTEMBER 30/2010 PILOTS REPORT ELEVATOR FEEL FAIL REPEATEDLY ILLUMINATION IN FLIGHT. TROUBLESHOT BY MFG, ACFT HYD SYS BLED AND ACFT RELEASE FOR RETURN TO SERVI
- [SDR CA101006004](https://openairdocs.org/sdr/CA101006004), Sep 29, 2010: BLEED VALVE. FAILED. LOW OIL PRESSURE/IFSD JUST AFTER LANDING, THE CREW OBSERVED A LOW OIL PRESSURE WARNING, HIGH TEMP AND DECAYING ENGINE PARAMETERS. THE ENGINE WAS SHUTDOWN AND TH
- [SDR CA100921003](https://openairdocs.org/sdr/CA100921003), Sep 10, 2010: ENGINE. LEAKING. SMOKE IN CABIN DURING CLIMB AT FL 50, SMOKE STARTED ENTERING THE CABIN. THE CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL LANDING WAS MAD
- [SDR CA091008005](https://openairdocs.org/sdr/CA091008005), Sep 30, 2009: TRIM TAB. CRACKED. (CAN) THIS WAS FILED ON SEPT 30/2009. DID NOT GET ANY CONFORMATION RESUBMITTED OCT 8TH 2009. CRACK ON FWD AND AFT ENDS OF RUDDER TRIM TAB LWR ROD, FROM ACTUATOR
- [SDR CA090727004](https://openairdocs.org/sdr/CA090727004), Jul 23, 2009: ACTUATOR. BINDING. (CAN) PILOTS REPORTED ALL SYS NORMAL. ON PRE-FLIGHT THE PILOTS COULD NOT GET THE SLATS TO MOVE WHEN SELECTED FLAPS DOWN. MX WAS CALLED AND COULD NOT DETECT WHAT
- [SDR CA090724004](https://openairdocs.org/sdr/CA090724004), Jul 23, 2009: FIRE LOOP. FAILED. (CAN) ON CLIMB OUT AT APPROX 18,000 FEET, ACFT ROUTED ON EICAS THE PILOTS REPORTED THAT THE LT ENG FIRE DETECTOR INDICATED FAILED. PILOTS REPORTED THAT CHECK LI
- [SDR CA090715002](https://openairdocs.org/sdr/CA090715002), Jul 14, 2009: TERMINAL. MISINSTALLED. (CAN) WHILE CONDUCTING THE 1200HR INSP OF THE RT WINDSHIELD ‘ANTI STATIC COATING’ ON G200, IT WAS FOUND UNSERVICEABLE AND DID NOT MEET THE SPEC BY THE MFG IAW M
- [SDR CA090601002](https://openairdocs.org/sdr/CA090601002), May 29, 2009: WIRE. BROKEN. (CAN) PILOT`S SIDE PITCH TRIM SWITCH IN-OP. MX INVESTIGATED AND FOUND PITCH TRIM WAS INTERMITTENT WHEN THE CONTROL COLUMN WAS OPERATED AFT (PULLED AFT). FLOOR A
- [SDR CA060601003](https://openairdocs.org/sdr/CA060601003), May 27, 2006: PACKING. MISINSTALLED. (CAN) THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED IN CRUISE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED OIL LOSS ASSOCIATED WITH A M
- [SDR CA060531022](https://openairdocs.org/sdr/CA060531022), May 24, 2006: SEAL. DAMAGED. (CAN) DURING CRUISE, THE ENGINE LOW OIL PRESSSURE WARNING ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUE
- [SDR CA060129011](https://openairdocs.org/sdr/CA060129011), Jan 11, 2006: ENGINE. SHUTDOWN. (CAN) ON ROLL OUT FOLLOWING LANDING, THE PILOT REPORTED AN UNCOMMANDED ENGINE SHUT DOWN. THE ENGINE BLEED VALVES AND BLEED VALVE SOLENOID WERE SUBSEQUENTLY REPL
- [SDR 95ZZZX6436](https://openairdocs.org/sdr/95ZZZX6436), Jun 22, 1995: WHEEL BAIL CABLE. ATTACH INCORRECT. RIGHT GEAR, INBOARD DOOR WHEEL BAIL CABLE ATTACH POINT INSTALLED IN THE WRONG POSITION. ATTACH POINT WAS LOCATED ON THE TOP OF THE BAIL APPROXIMATELY 2 INCHES F
- [SDR 95ZZZX4307](https://openairdocs.org/sdr/95ZZZX4307), Jun 22, 1995: CONTROL CABLE. MISINSTALLED. RIGHT MAIN GEAR FAILED TO EXTEND. INVESTIGATION REVEALED THE WHEEL BAIL CABLE WAS PREVIOUSLY REPLACED. THE CABLE WAS 2 INCHES TOO SHORT AND THE WRONG SWAGED TER

## STCs that may be installed (OpenAirDocs) (107, 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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC 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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC 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 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 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 SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC 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 SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC 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 SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [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 SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [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 SA10682SC](https://openairdocs.org/stc/SA10682SC): Installation of alternator and voltage regulator. Hartzell Engine Technologies, LLC
- [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 SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc

All 107: https://openairdocs.org/model/meyers-industries-200a/stcs.md

## PMA parts (OpenAirDocs) (153, 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.

- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179090575020260806152323.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127157111920260806152416.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151287534520250508133544.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179121247320240221143424.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101651715820230707211334.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [V674UL94](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114988333720220809101851.0001): UL94 Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Aug 3, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193292261820220525194352.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151325093720220525194505.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113452921820220525194227.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199599570320240229155257.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161235958620240229155302.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153553820120240229155308.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116287696420240229155313.0001): Final Assembly KCP 100 Control Panel(Landscape). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID951343096220210921142553.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID866447543620210923143723.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID829293115820210923143824.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID377421564520210702175228.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/E2B30B020A91DE91862585DE00509F79.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE, as used in alternators ALT… · Sep 1, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/C617AAB83C6B799B862585DE0050A01D.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA, as used in alternators ALY… · Sep 1, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/B7CC6ECA46AA2F14862585DE00509E71.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS, as used in alternators ALE… · Sep 1, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/9F424D3467678943862585DE00509EFC.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS, as used in alternators ALE… · Sep 1, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/68353ACEF594EACF862585DE0050A127.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/6583E821C11FC24F862585DE0050A086.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS, as used in alternators… · Sep 1, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/0388185039CFC4DD862585DE00509DDD.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/D6FF39FD09272684862585A80035E2C3.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS as used in Kelly… · Jul 14, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/BDCE1BF615C7C07F862585A80035E30E.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS as used in Kelly Aerospace… · Jul 14, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/7D10ABF30982F851862585A80035E125.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/653EDB41D36E637B862585A80035E22A.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/5023594FC72E2A5F862585A80035E1DF.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/4077186575E9032A862585A80035E272.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA as used in Kelly Aerospace… · Jul 14, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/2B2BE444A62E7876862585A80035E196.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS as used in Kelly Aerospace… · Jul 14, 2020
- [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
- [600-1132](https://drs.faa.gov/browse/excelExternalWindow/F7CEABC973D1F41E862585690051C63C.0001): Air Medical System. LifePort, LLC. · PMA PQ0172NM · Modification part · Jul 31, 2019
- [MDL 103216-000](https://drs.faa.gov/browse/excelExternalWindow/A5FAC4121A00318086258569004A2249.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jul 14, 2019
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/CB6B45C441A97D20862585510065ECA1.0001): SkyTrax 100B. Avidyne Corporation · PMA PQ4035CE · Replaces N/A · May 13, 2019
- [EA-15000](https://drs.faa.gov/browse/excelExternalWindow/BA487E6B82EF95E786258258006F0EA8.0001): Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Feb 20, 2018
- [10-357487-241](https://drs.faa.gov/browse/excelExternalWindow/97597E2D77D67D7F8625810200794D5C.0001): Starting Vibrator, S200 Series, 24 Volts DC -. Continental Motors Inc · PMA PQ1269CE · Replaces 10-357487-241 · Feb 16, 2017
- [10-176487-121](https://drs.faa.gov/browse/excelExternalWindow/64AB1D34CCF7D2468625810200794153.0001): Starting Vibrator, S-200 Series, 12 Volts DC. Continental Motors Inc · PMA PQ1269CE · Replaces 10-176487-121, 10-176487-121, 63333… · Feb 16, 2017
- [EIS-61000-1M](https://drs.faa.gov/browse/excelExternalWindow/F9CDFE44FEA0578B86257FAB0068FA29.0001): Electroair Electronic Ignition System (Kit). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EIS-61000-1C](https://drs.faa.gov/browse/excelExternalWindow/458B8938A6B43D5186257FAB0068FA27.0001): Electroair Electronic Ignition System (Kit). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EA-13000](https://drs.faa.gov/browse/excelExternalWindow/B3C7B4E82732240986257EF40059ADFC.0001): Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Oct 29, 2015

All of them: https://openairdocs.org/model/meyers-industries-200a/pma.md

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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.