# Service difficulty reports: Meyers Industries 200A

A list on [Meyers Industries 200A](https://openairdocs.org/model/meyers-industries-200a.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA160322007](https://openairdocs.org/sdr/CA160322007.md): Relay · stuck · Mar 10, 2016 · Propjt 200A · Engine Thrust Reverser
  > (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. REPLACED HARNESS WITH A REPAIRED UNIT. AS A PRECAUTIONARY MEASURE WE REPLACED LEFT HAND INBOARD STOW RE
- [SDR CA160120005](https://openairdocs.org/sdr/CA160120005.md): Oil System · leaking · Jan 6, 2016 · Propjt 200A · Turbine Engine Oil System
  > (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 DURING LANDING. AFTER PARKING, CREW MADE AND EXTERIOR ENGINE CHECK. OIL LEVEL FOUND EMPTY AND OIL
- [SDR CA151229006](https://openairdocs.org/sdr/CA151229006.md): Engine · leaking · Dec 21, 2015 · Propjt 200A · Engine (Turbine/Turboprop)
  > (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 FOUND OIL IN THE LT BLEED DUCT.
- [SDR CA151203012](https://openairdocs.org/sdr/CA151203012.md): Terminal Block · loose · Dec 2, 2015 · Propjt 200A · Electrical Power System Wiring
  > (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 PANEL. TIGHTENING THESE TERMINALS SOLVED THE LIGHTING PROBLEM. IT WAS ALSO FOUND THAT MOST OF THE TERMI
- [SDR CA151117018](https://openairdocs.org/sdr/CA151117018.md): Unknown · odor · Nov 11, 2015 · Propjt 200A · Air Distribution System
  > (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. TECH WORKED ON THE RT ENGINE THE DAY BEFORE THIS EVENT FOR A LEAKING HYDRAULIC PAD AGB SEAL. TROUBLES
- [SDR CA151007004](https://openairdocs.org/sdr/CA151007004.md): Unknown · odor · Sep 28, 2015 · Propjt 200A · Air Distribution System
  > (CAN) THE OPERATOR REPORTED AN OIL ODOR IN THE CABIN. TROUBLESHOOTING ONGOING.
- [SDR CA151007003](https://openairdocs.org/sdr/CA151007003.md): Engine · leaking · Sep 28, 2015 · Propjt 200A · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED SMOKE IN CABIN DURING CLIMB AND THEY TURNED BACK WITHOUT ANY INCIDENT. DURING TROUBLESHOOTING, MAINTENANCE DISCOVERED BLEED AIR WAS FULL OF OIL AND LOW OIL PRESSURE EXCEEDANCE WERE FOUND ON FADEC MESSAGES.
- [SDR CA150728003](https://openairdocs.org/sdr/CA150728003.md): Engine · leaking · Jul 21, 2015 · Propjt 200A · Turbine Engine Oil System
  > (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 SMELL. CREW REFERRED TO FLIGHT MANUAL AND TRIED TO ISOLATE PROBLEM TO NO AVAIL. AT THIS POINT, ENGINE
- [SDR CA141024014](https://openairdocs.org/sdr/CA141024014.md): Warning Message · illuminated · Oct 6, 2014 · Propjt 200A · Engine Indicating System
  > (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 CONTACTED THE MFG FSR TO ADVISE THAT ON THE ICAS SYSTEM THE POSTED FAULTS WERE TA AND TB. THE THRUST
- [SDR CA140826032](https://openairdocs.org/sdr/CA140826032.md): Warning Message · false activation · Aug 21, 2014 · Propjt 200A · Central Warning
  > (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 FLAGGED WHICH IS LANE CONNECTED STATUS FAIL. RESET POWER. THE CREW FOLLOWED THE RECOMMENDATIONS PROVIDED
- [SDR CA140804007](https://openairdocs.org/sdr/CA140804007.md): Engine · leaking · Jul 24, 2014 · Propjt 200A · Engine (Turbine/Turboprop)
  > (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 INSPECTION. OIL WAS NOTED IN THE CABIN BLEED PORTS. ADDITIONAL TROUBLESHOOTING WILL CONTINUE TO DETERMIN
- [SDR CA140701005](https://openairdocs.org/sdr/CA140701005.md): Engine · vibration · Jun 2, 2014 · Propjt 200A · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE IT WAS REPORTED THAT THERE WAS AN ENGINE HARMONICS VIBRATION ISSUE AND OBVIOUS HARMONIC SOUND WAS NOTICED. DURING THE "ON GROUND TROUBLESHOOTING", THE CUSTOMER RAN THE ACFT AND PERFORMED THE N2 AND N1 VIBRATION CHECK AS REQUIRED. DOWNLOAD
- [SDR CA140602025](https://openairdocs.org/sdr/CA140602025.md): Indication Sys · malfunctioned · May 28, 2014 · Propjt 200A · Engine Oil Pressure
  > (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 NORMAL AFTER 5 MINUTES. NO FURTHER ENGINE ABNORMALITIES WERE NOTED. WILL INVESTIGATE TO ESTABLISH
- [SDR CA140117001](https://openairdocs.org/sdr/CA140117001.md): Case · damaged · Dec 22, 2013 · Propjt 200A · Engine Air Intake System
  > (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 CASE COATING THE ACFT WAS RETURN TO SERVICE.
- [SDR CA130729003](https://openairdocs.org/sdr/CA130729003.md): Oil System · fluctuates · Jul 16, 2013 · Propjt 200A · Engine Oil Pressure
  > (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 UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. POST FLIGHT INSPECTION FOUND OIL IN THE THRUST REVERSERS
- [SDR CA130416007](https://openairdocs.org/sdr/CA130416007.md): Oil System · low pressure · Apr 2, 2013 · Propjt 200A · Engine Oil Indicating System
  > (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.md): Oil System · leaking · Mar 18, 2013 · Propjt 200A · Turbine Engine Oil System
  > (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 NR 1 ENGINE CABIN BLEED PORT. MFG RECOMMENDED TO REPLACE THE ENGINE.
- [SDR CA130318003](https://openairdocs.org/sdr/CA130318003.md): Engine · power loss · Mar 8, 2013 · Propjt 200A · Engine (Turbine/Turboprop)
  > (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. TROUBLESHOOTING IS ON-GOING.
- [SDR CA130212016](https://openairdocs.org/sdr/CA130212016.md): Compressor · stalled · Feb 5, 2013 · Propjt 200A · Engine (Turbine/Turboprop)
  > (CAN) DURING THE TAKEOFF PROCEDURE, LOUD NOISE OCCURRED DURING THE ACCELERATION ASSOCIATED WITH A SEVERE VIBRATION NOTED BY THE PASSENGERS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE FBO. THE CREW HEARD WHAT THEY FELT SOUNDED LIKE A COMPRESSOR STALL, T
- [SDR CA121119017](https://openairdocs.org/sdr/CA121119017.md): Engine · overtemp · Nov 11, 2012 · Propjt 200A · Engine (Turbine/Turboprop)
  > (CAN) DURING DESCENT, WITH HEAT ON, THE ENGINE TEMPERATURE INCREASED AND STARTED FLASHING RED. THE THROTTLE WAS RETARDED TO IDLE AND THE TEMPERATURE STABILIZED NEAR MAXIMUM. SUBSEQUENT THROTTLE INPUTS HAD NO EFFECT. THE ACFT LANDED SAFELY BUT BY THEN THE ENG
- [SDR CA120813004](https://openairdocs.org/sdr/CA120813004.md): Unknown · smoke · Aug 1, 2012 · Propjt 200A · Air Distribution System
  > (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 LEG BACK TO BASE AND RT CABIN BLEED WAS DESELECTED AGAIN AND FLIGHT COMPLETED UNEVENTFULLY. ENG
- [SDR CA120802006](https://openairdocs.org/sdr/CA120802006.md): Compressor · stalled · Jul 23, 2012 · Propjt 200A · Turbine Engine Compressor Section
  > (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 RETURN TO POINT OF DEPARTURE AND PERFORMED A SAFE LANDING. OPS CHECK OF BOVS, INSPECTION OF 1ST STAGE CO
- [SDR CA120802002](https://openairdocs.org/sdr/CA120802002.md): Blade · damaged · Jul 18, 2012 · Propjt 200A · Turbine Engine Compressor Section
  > (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 UNEVENTFUL LANDING WAS ACCOMPLISHED. POST FLIGHT EXAMINATION FOUND OIL STREAKS ON THE COWLING AND IN
- [SDR CA120723010](https://openairdocs.org/sdr/CA120723010.md): Unknown · odor · Jul 18, 2012 · Propjt 200A · Air Distribution System
  > (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 AND RETURNED TO AIRPORT OF ORIGIN. OIL STREAKING NOTED IN THE ENGINE EXHAUST.
- [SDR CA120702011](https://openairdocs.org/sdr/CA120702011.md): Fuel Control · unknown · Jun 28, 2012 · Propjt 200A · Fuel Control/Turbine Engines
  > (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 ASSOCIATED WITH THE ENGINE ROLLING BACK AND FAILED. AFTER ABOUT 30 SEC THE ENGINE AUTO LIGHTED. NO ABNO
- [SDR CA111114014](https://openairdocs.org/sdr/CA111114014.md): Unknown · smoke · Nov 6, 2011 · Propjt 200A · Air Distribution System
  > (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 ACCOMPLISHED. TROUBLESHOOTING IS ON-GOING.
- [SDR CA111030007](https://openairdocs.org/sdr/CA111030007.md): Unknown · smoke · Oct 18, 2011 · Propjt 200A · Air Distribution System
  > (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 AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE. TROUBLESHOOTING IS ON-GOING.
- [SDR CA111019001](https://openairdocs.org/sdr/CA111019001.md): Unknown · haze · Oct 6, 2011 · Propjt 200A · Air Distribution System
  > (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. ON OCT 6TH AFTER T/O FOR A RE-POSITIONING FLIGHT, SMOKE HAZE AGAIN ENTERED THE CABIN, THE FLIGHT WAS
- [SDR CA110330007](https://openairdocs.org/sdr/CA110330007.md): Line · misinstalled · Mar 25, 2011 · Propjt 200A · Hydraulic System, Main
  > (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 SERIES OF FLIGHTS. TROUBLE SHOOTING THE TRANSFER OF FLUID WAS INITIATED. DETAILED INSPECTION OF RECENT
- [SDR CA110315008](https://openairdocs.org/sdr/CA110315008.md): Unknown · odor · Mar 10, 2011 · Propjt 200A · Air Distribution System
  > (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 DEPARTURE. TROUBLESHOOTING FOUND NO MAJOR ANOMALIES AND A FERRY FLIGHT BACK TO BASE WAS AUTHORIZED, THE
- [SDR CA101122009](https://openairdocs.org/sdr/CA101122009.md): Engine · vibration · Nov 18, 2010 · Propjt 200A · Engine (Turbine/Turboprop)
  > (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 INDICATOR. IT WAS REPORTED THAT SPARKS WERE COMING OUT FROM THE EXHAUST. THE FLIGHT CANCELLED AND THE AI
- [SDR CA101004009](https://openairdocs.org/sdr/CA101004009.md): Actuator · failed · Oct 1, 2010 · Propjt 200A · Elevator Control System
  > 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 SERVICED. OCTOBER 01/2010, PILOTS REPORT ELEVATOR FEEL FAIL BETWEEN 1-6 TIMES IN FLIGHT, TROUBLESHOT AND
- [SDR CA101006004](https://openairdocs.org/sdr/CA101006004.md): Bleed Valve · failed · Sep 29, 2010 · Propjt 200A · Compressor Bleed Valve
  > 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 THE ACFT TAXIED TO THE RAMP. SUBSEQUENT GROUND RUN SHOWED THE ENGINE HANGING AT 25 PERCENT N2, CONFI
- [SDR CA100921003](https://openairdocs.org/sdr/CA100921003.md): Engine · leaking · Sep 10, 2010 · Propjt 200A · Turbine Engine Oil System
  > 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 MADE. POST FLIGHT INSP FOUND OIL ON THE FAN AND THE CABIN BLEED PORT. TROUBLESHOOTING IS ON-GOING.
- [SDR CA091008005](https://openairdocs.org/sdr/CA091008005.md): Trim Tab · cracked · Sep 30, 2009 · Propjt 200A · Rudder Tab Control System
  > (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 BELLCRANK TO RUDDER TRIM TAB. THIS WAS FOUND DURING SCHEDULE MX ON THE ACFT WHILE CARRYING OUT (A)
- [SDR CA090727004](https://openairdocs.org/sdr/CA090727004.md): Actuator · binding · Jul 23, 2009 · Propjt 200A · Leading Edge Slat Actuator
  > (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 WAS FAILED ON THE SYS. ACFT PROCEEDED TO COMPLETE A FERRY FLIGHT WITH SLATS RETRACTED USING BYPA
- [SDR CA090724004](https://openairdocs.org/sdr/CA090724004.md): Fire Loop · failed · Jul 23, 2009 · Propjt 200A · Fire Detection
  > (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 LIST HAD BEEN COMPLETED AND AS A PRECAUTIONARY MEASURE PROCEEDED TO SHUTDOWN ENG IN FLIGHT. ACFT WAS
- [SDR CA090715002](https://openairdocs.org/sdr/CA090715002.md): Terminal · misinstalled · Jul 14, 2009 · Propjt 200A · Window System Wiring
  > (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 MM. THIS REQUIRED WIND-SHIELD REPLACEMENT. ON REMOVAL OF THE WINDSHIELD, FOUND ONE (1) OF THE PWR CA
- [SDR CA090601002](https://openairdocs.org/sdr/CA090601002.md): Wire · broken · May 29, 2009 · Propjt 200A · Flight Control System Wiring
  > (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 ACCESS PANELS REMOVED IN COCKPIT AREA AND FOUND HARNESS ROUTING VERY TIGHT. ALLOWING WIRES TO WORK A
- [SDR CA060601003](https://openairdocs.org/sdr/CA060601003.md): Packing · misinstalled · May 27, 2006 · Propjt 200A · Turbine Engine Oil System
  > (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 MISINSTALLED OIL CAP O-RING PACKING. (TC NR 20060601003)
- [SDR CA060531022](https://openairdocs.org/sdr/CA060531022.md): Seal · damaged · May 24, 2006 · Propjt 200A · Engine Oil Pressure
  > (CAN) DURING CRUISE, THE ENGINE LOW OIL PRESSSURE WARNING ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INVESTIGATION REVEALED A DAMAGED AND LEAKING ACCESSORY GEARBOX LIP SEAL. (TC NR 20060531022)
- [SDR CA060129011](https://openairdocs.org/sdr/CA060129011.md): Engine · shutdown · Jan 11, 2006 · Propjt 200A · Engine (Turbine/Turboprop)
  > (CAN) ON ROLL OUT FOLLOWING LANDING, THE PILOT REPORTED AN UNCOMMANDED ENGINE SHUT DOWN. THE ENGINE BLEED VALVES AND BLEED VALVE SOLENOID WERE SUBSEQUENTLY REPLACED. (TC NR 20060129011)
- [SDR 95ZZZX6436](https://openairdocs.org/sdr/95ZZZX6436.md): Wheel Bail Cable · attach incorrect · Jun 22, 1995 · N492C · Propjt 200A · Landing Gear Door Retract Section
  > 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 FORWARD OF THE AFT CORNER. PROPER POSITION SHOULD BE APPROXMATELY AT THE AFT CORNER.
- [SDR 95ZZZX4307](https://openairdocs.org/sdr/95ZZZX4307.md): Control Cable · misinstalled · Jun 22, 1995 · N492C · Propjt 200A · Landing Gear Retraction/Extension System
  > 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 TERMINAL WAS INSTALLED ALLOWING THE CABLE TO BIND AT THE ATTACHMENT. THIS BINDING, AND SHORTNESS, CA

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '200A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/meyers-industries-200a/reports

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