# Service difficulty reports: Found Acft Canada FBA-2C1

A list on [Found Acft Canada FBA-2C1](https://openairdocs.org/model/found-acft-canada-fba-2c1.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2018FA0000199](https://openairdocs.org/sdr/2018FA0000199.md): Push-Pull Rod · corroded · Jun 29, 2018 · Found FBA2C1 · Elevator Control System
  > INTERNAL CORROSION FOUND ON ELEVATOR PUSH/PULL ROD. THE CORROSION PRESENTED ITSELF AS A SMALL BIT OF TOPICAL EXTERNAL CORROSION BUT WHEN UNIT WAS CLEANED FOR FURTHER INSPECTION AND ANALYSIS IT APPEARS CORROSION WAS INTERNAL TO EXTERNAL AND PENETRATED THE TUBIN
- [SDR CA120103016](https://openairdocs.org/sdr/CA120103016.md): Tire · failed · Dec 1, 2015 · Found FBA2C1 · Tire
  > (CAN) CHORD FAILURE. CAUSED WHEEL TO RUB ON FORK OF AMPHID NOSE GEAR.
- [SDR 2015FA0000194](https://openairdocs.org/sdr/2015FA0000194.md): Relay · faulty · May 4, 2015 · N706M · Found FBA2C1 · Rudder Tab Control System
  > ON CLIMBOUT WHILE MANUALLY DRIVING THE RUDDER TRIM WITH THE RUDDER TRIM SWITCH, THE RUDDER TRIM "RAN AWAY" FULL RT. PILOT COULD DRIVE IT BACK TO THE LT WITH THE TRIM SWITCH, BUT WHEN HE TRIED ADDING RT RUDDER TRIM IT WOULD KEEP DRIVING TO FULL DEFLECTION RT.
- [SDR CA141205003](https://openairdocs.org/sdr/CA141205003.md): Exhaust Duct · cracked · Dec 3, 2014 · Found FBA2C1 · Engine Collector/Tailpipe/Nozzle
  > (CAN) RIGHT HAND EXHAUST COLLECTOR CRACKED AT THE FLANGE FOR THE NR 1 CYLINDER. MUFFLER ALSO HAD SMALL CRACK ON NEAR/THE TOP SIDE OF THE EXIT DUCT.
- [SDR CA140514009](https://openairdocs.org/sdr/CA140514009.md): Cap · broken · May 14, 2014 · Found FBA2C1 · Landing Gear System
  > (CAN) ON LANDING, A SOUND WAS HEARD AND SOMETHING FELT BENEATH THE PILOT`S FEET. ON FURTHER INVESTIGATION IT WAS FOUND THAT THE LT REBOUND PUCK CAP HAD BROKEN INTO SEVERAL PIECES WHICH RESULTED IN ALLOWING THE TIE BOLT TO FALL THROUGH THE CAP ALLOWING THE REB
- [SDR CA140414012](https://openairdocs.org/sdr/CA140414012.md): Rotor · failed · Apr 12, 2014 · Found FBA2C1 · Magneto/Distributor
  > (CAN) DURING PRE-FLIGHT GROUND RUNUP, WHEN RT MAGNETO WAS SELECTED, THE ENGINE WOULD DIE. RT MAGNETO WAS R & R WITH A SERVICEABLE MAGNETO. ENGINE GROUND RUN AND MAGNETO FUNCTION CHECKED SERVICEABLE. REMOVED MAGNETO WAS DISASSEMBLED TO INSPECT FOR CAUSE OF
- [SDR IDCR2013FA0000565](https://openairdocs.org/sdr/IDCR2013FA0000565.md): Baffle · broken · Sep 27, 2013 · Found FBA2C1 · Reciprocating Engine Oil System
  > DURING ROUTINE INSPECTION, DISCOVERED BROKEN RIVET IN ENGINE OIL SUCTION SCREEN. BASED ON PREVIOUS EXPERIENCE, KNEW THIS MOST LIKELY CAME FROM A BROKEN OIL SUMP BAFFLING. CALLED MFG ENGINES TECH LINE TO CONFIRM THIS. MFG TECH FORWARDED A COPY OF MFG ENG SB
- [SDR CA111207007](https://openairdocs.org/sdr/CA111207007.md): Structure · detached · Sep 30, 2011 · Found FBA2C1 · Horizontal Stabilizer Structure
  > (CAN) ON DEPARTURE A BANG WAS HEARD. NO ADVERSE ENGINE OR ACFT PERFORMANCE WAS NOTED. AFTER LANDING, INSPECTION OF THE TAIL REVEALED THAT THE LT VENTRAL FINLET HAD DEPARTED IN FLIGHT. THE FWD ATTACH BRACKET WAS FOUND BROKEN WITH THE LOWER PORTION STILL ATT
- [SDR CA110919004](https://openairdocs.org/sdr/CA110919004.md): Valve · leaking · Sep 11, 2011 · Found FBA2C1 · Aircraft Fuel Distribution System
  > (CAN) FUEL VENT VALVE REPLACE IN RT WING. UPON FUELING THE ACFT, FUEL WAS OBSERVED WEEPING FROM THE FUEL VENT TUBE. ACFT DEFUELLED AND AND VENT VALVE REPLACED. ACFT RETURNED TO SERVICE.
- [SDR CA110707007](https://openairdocs.org/sdr/CA110707007.md): Bearing · failed · Jul 7, 2011 · Found FBA2C1 · Wheel/Ski/Float
  > BEARING FAILED, LEADING TO OUTER COTTER PIN SHEARING OFF. NUT TIGHTENING WITH TIRE ROTATION, AND WHEEL + TIRE SEIZING COMPLETELY. APPROX 2 HR SPENT ON RUNWAY TO GET WHEEL UNSEIZED AND ACFT CLEAR OF RUNWAY.
- [SDR CA100709003](https://openairdocs.org/sdr/CA100709003.md): Tie Bolt · broken · Jun 27, 2010 · Found FBA2C1 · Main Landing Gear Attach Section
  > DURING A NORMAL LANDING, THE PILOT HEARD A BANG AND INVESTIGATED AND FOUND THE TIE BOLT BROKEN. THERE WAS NO FURTHER DAMAGE TO THE AIRCRAFT, PILOT OR PASSENGERS. A NEW BOLT REPLACED THE BROKEN BOLT AND NO FURTHER ISSUES WERE REPORTED. THE BROKEN BOLT WAS RE
- [SDR 2010FA0000497](https://openairdocs.org/sdr/2010FA0000497.md): Baffle · cracked · May 13, 2010 · N798 · Found FBA2C1 · Reciprocating Engine Oil System
  > DURING ENGINE MAINTENANCE THAT REQUIRED THE REMOVAL OF THE OIL SUMP THE INTERNAL OIL SUMP BAFFLE (P/N 56G23399) WAS FOUND BADLY CRACKED (APPROX. 4" LONG) ON THE PAN SHEET, ALONGSIDE THE RIVET LINE FOR THE BACK BONE STIFFENER. ADDITIONALLY, 5 OF THE 6 MOUNTING
- [SDR CA100526005](https://openairdocs.org/sdr/CA100526005.md): Tie Bolt · bent · May 6, 2010 · Found FBA2C1 · Main Landing Gear
  > GEAR TIE BOLT WAS REPLACED AFTER IT FAILED ON LANDING IN EARLY 2009 WITH NEW AND IMPROVED VERSION IAW SB -32-08 LATEST REV. DURING A 100 HR INSP, IT WAS OBSERVED THAT THE RT TIE BOLT (PN U369) WAS BENT. THE ACFT WAS REMOVED FROM WHEEL GEAR AND INSTALLED ON
- [SDR CA090925004](https://openairdocs.org/sdr/CA090925004.md): Attach Fitting · broken · Sep 24, 2009 · Found FBA2C1 · Nose/Tail Landing Gear
  > (CAN) LEFT AFT TIE WIRE LUG FOUND BROKEN AT FUSELAGE. (TC# 20090925004)
- [SDR EN02009F00000](https://openairdocs.org/sdr/EN02009F00000.md): Pump · failed · Jun 1, 2009 · N818ES · Found FBA2C1 · Engine Fuel Pump
  > FUEL EDP DID NOT MAKE FULL FUEL PRESSURE/GPH AT TAKE OFF RPM. NORMAL TAKEOFF FUEL FLOW ONLY REACHED WHEN AUX FUEL PUMP WAS ON. WHEN AUX PUMP SWITCHED OFF AT TAKEOFF RPM, ENGINE WOULD LOSE 5-7 GPH OF FUEL FLOW. EGT WOULD RISE ABOVE NORMAL & RPM`S & MANIFOLD
- [SDR CA090403011](https://openairdocs.org/sdr/CA090403011.md): Tie Bolt · failed · Mar 27, 2009 · Found FBA2C1 · Main Landing Gear Strut/Axle/Truck
  > (CAN) IT WAS THE USUAL ON TOUCHDOWN, BUT WE HAD A 15-20 KNOT WIND TO HELP SLOW THINGS DOWN AND FOUND THE LANDING NOT REMARKABLE IN ANY WAY. SAME WITH TAKEOFF, THEN 3 MORE HOURS OF FLYING AND CARIBOU SURVEY, AND BACK. AS THE WEIGHT CAME OFF THE WINGS ONTO THE
- [SDR CA080303009](https://openairdocs.org/sdr/CA080303009.md): Sump · unserviceable · Mar 1, 2008 · Found FBA2C1 · Reciprocating Engine Oil System
  > (CAN) OIL SUMP WAS REMOVED TO INSPECT SUMP BAFFLE IAW SB. INTERNAL CRACK IN THE SUMP WAS FOUND NEAR ONE OF THE MOUNTING LUGS. IAW THE SB, THE OIL SUMP BAFFLE HAD A LACK OF CLEARANCE AND HAD BEEN RUBBING THE BOTTOM OF THE SUMP. BAFFLE, AND SUMP HAD SIGNS OF WE
- [SDR 2007FA0000761](https://openairdocs.org/sdr/2007FA0000761.md): Baffle · cracked · Jul 16, 2007 · N794 · Found FBA2C1 · Reciprocating Engine Oil System
  > ENGINE OIL SUMP BAFFLE CONTACTED BOTTOM OF OIL SUMP CRACKING BAFFLE SUPPORT ATTACH POINTS AND SHEARING RIVETS ATTACHING BAFFLE CENTER REINFORCEMENT.
- [SDR 2007FA0000760](https://openairdocs.org/sdr/2007FA0000760.md): Baffle · cracked · Jul 16, 2007 · N796 · Found FBA2C1 · Reciprocating Engine Oil System
  > ENGINE OIL SUMP BAFFLE CONTACTED BOTTOM OF OIL SUMP CRACKING BAFFLE SUPPORT ATTACH POINTS AND SHEARING RIVETS ATTACHING BAFFLE CENTER REINFORCEMENT. SHEARED RIVET LODGED IN OIL PRESSURE RELIEF VALVE CAUSING LOSS OF OIL PRESSURE. ENGINE REMOVED FOR OVERHAUL.
- [SDR 2007FA0000951](https://openairdocs.org/sdr/2007FA0000951.md): Baffle · broken · Jul 13, 2007 · N796 · Found FBA2C1 · Turbine Engine Oil System
  > OIL BAFFLE IN SUMP RUBBING ON BOTTOM OF SUMP. 4 OUT OF 6 HOLES CRACKED OUT AROUND MOUNTING AREA. 2 HOLES COMPLETELY WORN THROUGH AND STILL HAD PARTS OF BAFFLE UNDER WASHER AND MOUNTING SCREW. (K)
- [SDR CA070413003](https://openairdocs.org/sdr/CA070413003.md): Pedal · cracked · Apr 11, 2007 · Found FBA2C1 · Landing Gear Brake System
  > (CAN) DURING CLEAN UP AFTER THE REPLACEMENT OF THE FUEL GAUGE ON AC 52 MECHANIC NOTICED THAT THE CO-PILOTS BRAKE-PEDAL ASSY WAS CRACKED. AFTER DISCUSSION WITH CHIEF ENGINEER HE NOTED THAT THIS WAS THE SECOND TIME, IT HAD HAPPENED PREVIOUSLY TO AC 53. FOUND MFG
- [SDR CA080915001](https://openairdocs.org/sdr/CA080915001.md): Fitting · undertorqued · Aug 2, 2006 · Found FBA2C1 · Aircraft Fuel Distribution System
  > (CAN) FOUND NUMEROUS FUEL FITTINGS WHICH CONNECT THE FUEL LINES TO THE HEADER TANKS TO BE SEEPING FUEL. APPROXIMATE TIME OF SERVICE 532 HRS. PIPE THREAD FITTINGS HAD NO THREAD LUBE/SEALANT. THE VENDOR NOTED THAT THE FUEL FITTINGS WERE NOT PROPERLY TORQUED. THI

## 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 = 'FBA2C1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/found-acft-canada-fba-2c1/reports

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