Cessna 337A

Service difficulty reports · 16

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = '337A'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA041020011Bolt · missing(CAN) WHILE TAXING TO PARK, THE LEFT WHEEL STARTED TO SMOKE AND THE AIRCRAFT STARTED TO SHAKE. AFTER APPLYING BRAKES EVERYTHING WENT BACK TO NORMAL. UPON INSPECTION THE TIRE HAD WORN ALMOST THROUGH AND ONE OF THE THREE WHEEL BOLTS WAS MISSING. AFTER THE WHEEL Oct 19, 2004 · Cessna 337A · Wheel/Ski/FloatSDR CA040225014Control Cable · frayed(CAN) FLAP CABLES REMOVED FOR INSPECTION, REFERENCE SD ALERT AL-2003-05 IB FLAP CABLE, RT SIDE, PART NR 1460100-7 FRAYED APPROX 50 PERCENT AT IB BELLCRANK. 1 INCH FROM SWAGGED TERMINAL. ALSO BOTH OB CABLES PN 1460100-8 FRAYED AT IB BELLCRANK, APPROX. 1 INCH FRFeb 24, 2004 · Cessna 337A · Trailing Edge Flap Control SystemSDR CA040225011Control Cable · frayed(CAN) FLAP CABLES REMOVED FOR INSPECTION DUE TO SERVICE DIFFICULTY ALERT AL-2003-05. LT AND RT OUTBOARD FLAP CABLES FOUND TO BE FREYED AT THE INBOARD BELLCRANK, APPROXIMATELY 1 INCH FROM THE SWAGGED TERMINAL. BOTH CABLES ARE ORIGINAL CESSNA FLAP CABLES AND WERFeb 24, 2004 · Cessna 337A · Trailing Edge Flap Control SystemSDR CA030606010Control Cable · frayed(CAN) INSPECTION OF FLAP CABLES IAW SERVICE DIFFICULTY ALERT NR AL-2003-05, FOUND THREE FRAYED CABLE ENDS, ONE AT OUTBOARD BELLCRANK.Jun 6, 2003 · Cessna 337A · Leading Edge Slat Control SystemSDR AUS20030264Control Cable · corroded(AUS) FLAP CONTROL CABLES PN 14601007 AND PNO 14601008 CORRODED AND FRAYED.Mar 3, 2003 · Cessna 337A · Trailing Edge Flap Control SystemSDR CA021125010Bracket · cracked(CAN) CRACK FOUND ON BOTH INBOARD RUDDER TORQUE TUBE MOUNTING BRACKETS. THE CRACK BEGAN AT THE AFT END OF THE BRACKET, EXTENDING FORWARD APPROXIMATELY 3-4 INCHES ON THE LT BRACKET AND 1/2 INCH FORWARD ON THE RT BRACKET. THE CRACK OCCURRED AT THE BEND RADIUS ONNov 21, 2002 · Cessna 337A · Rudder Control SystemSDR AU990416Bearing · missing(AUS) NOSE LANDING GEAR OLEO STRUT BEARING MISSING. SUSPECT BEARING HAD BEEN LEFT OUT AT THE LAST INSPECTION WHEN NEW SEALS HAD BEEN FITTED.Apr 29, 1999 · Cessna 337A · Nose/Tail Landing Gear Strut/AxleSDR 98ZZZX154Support Assy · crackedPILOT COMPLAINED OF INCONSISTENT RUDDER TRIM INPUTS TO MAINTAIN COORDINATED FLIGHT AND 'FUNNY' RUDDER CONTROL INPUTS. INSPECTION REVEALED BOTH CENTER RUDDER BAR SUPPORTS CRACKED ALLOWING RUDDER BAR TO WANDER WHEREVER IT WANTED TO GO. AIRCRAFT HAS HISTORY OF LDec 26, 1997 · N9739D · Cessna 337A · Rudder Control SystemSDR 98ZZZX153Support Assy · crackedPILOT COMPLAINED OF INCONSISTENT RUDDER TRIM INPUTS TO MAINTAIN COORDINATED FLIGHT AND 'FUNNY' RUDDER CONTROL INPUTS. INSPECTION REVEALED BOTH CENTER RUDDER BAR SUPPORTS CRACKED ALLOWING RUDDER BAR TO WANDER WHEREVER IT WANTED TO GO. AIRCRAFT HAS HISTORY OF Dec 26, 1997 · N9739D · Cessna 337A · Rudder Control SystemSDR 98ZZZX140Plate · failedUPON LANDING, LEFT BRAKE CALIPER TORQUE PLATE BROKE AT UPPER REAR BOLT ATTACH HOLE CAUSING BRAKE CALIPER TO SHIFT INTO THE INSIDE OF THE BRAKE DISC CAUSING THE LEFT WHEEL TO LOCK UP. THE TORQUE PLATE IS DRILLED OVERSIZED AND THEN BUSHED DOWN TO ACCEPT AXLE ATDec 26, 1997 · N9739D · Cessna 337A · BrakeSDR EY2R9601265Locknut · corrodedLOCKNUT CORRODED.Dec 1, 1996 · Cessna 337A · Propeller AssemblySDR EY2R9601264Blade · corrodedBLADE, SN D2514YS, FOUND CORRODED.Dec 1, 1996 · Cessna 337A · Propeller Blade SectionSDR EY2R9601263Hub · corrodedHUB FOUND CORRODED.Dec 1, 1996 · Cessna 337A · Propeller Hub SectionSDR EY2R9601262Act Pin · corrodedACT. PIN FOUND RUSTED.Dec 1, 1996 · Cessna 337A · Propeller AssemblySDR CA960819201Pushrod · sheared(CAN) PILOT REPORTED BACKFIRE DURING GROUND RUN-UP. INVESTIGATION FOUND REAR ENGINE #3 CYLINDER EXHAUST PUSHROD SNAPPED APPROXIMATELY 1" FROM THE TIP. RETAINER P/N 628059 WAS ALSO FOUND FAILED. ENGINE WAS RETURNED TO OVERHAUL SHOP.Aug 7, 1996 · Cessna 337A · Reciprocating Engine Cylinder SectionSDR 95ZZZX3483Taper Pin · shearedUPON SELECTING GEAR DOWN, THE LEFT MAIN GEAR DANGLED IN AN INTERMITTENT POSITION. ALL ATTEMPTS TO DOWN AND LOCK THE LEFT GEAR WERE UNSUCCESSFUL. RT MAIN AND NOSE DOWN AND LOCKED NORMALLY. AIRCRAFT LANDED WITH RT MAIN AND NOSE GEAR DOWN. DAMAGE TO BOTH LEFTJun 7, 1995 · N6384F · Cessna 337A · Landing Gear Retraction/Extension System
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