Aero Commander 690B
Service difficulty reports · 73
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 = '690B' 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.
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 = '690B' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 99ZZZX946Tire · leakingTIRES WERE REPLACED BECAUSE THEY WOULD NOT HOLD AIR. INSPECTION REVEALED DILATING HOLES ALLOWING AIR LOSS TO CONTINUE AFTER SEVERAL DAYS. LEAKAGE BECAME WORSE TO THE POINT RE-INFLATION WAS NEEDED AFTER EACH FLIGHT. HIGH RISK OF LANDING WITH FLAT TIRE ON TRISDR 98ZZZX3586Windshield · crackedPILOT REPORTED CRACKED WINDSHIELD IN-FLIGHT, CRACK PROGRESSED FROM ONE CORNER TO SEVERAL CRACKS. PILOT MADE AN EMERGENCY LANDING. WINDSHIELD WAS REPLACED. WINDSHIELD WAS RE-CERTIFIED 71 HOURS PRIOR TO INCIDENT. WINDSHIELD RE-CERTIFIED BY FAA RS OX4R403M.SDR 98ZZZX1541Spar · crackedINSPECTION FOUND AILERON SPARS CRACKED. LOCATION: INBOARD HINGE BRACKET ATTACH POINT. LT AILERON HAD .75 INCH CRACK. RT AILERON HAD 2.25 INCH CRACK. CAUSE COULD BE RELATED TO TOTAL TIME.SDR 98ZZZX1540Spar · crackedINSPECTION FOUND AILERON SPARS CRACKED. LOCATION: INBOARD HINGE BRACKET ATTACH POINT. LT AILERON HAD .75 INCH CRACK. RT AILERON HAD 2.25 INCH CRACK. CAUSE COULD BE RELATED TO TOTAL TIME.SDR 98ZZZX1370Pulley Bracket · crackedDURING 100-HOUR MANUFACTURER'S INSPECTION, FOUND LEFT INBOARD FLAP MASTER PULLEY BRACKET CRACKED ON INBOARD SIDE. BRACKET IS ACCESSIBLE THROUGH AFT BAGGAGE COMPARTMENT.SDR 98ZZZX288Governor · seizedON TAXI, ENGINE HAD TO BE SHUT DOWN DUE TO LOW RPM AND HIGH ITT IN BETA. MAINTENANCE DISCOVERED PROPELLER GOVERNOR HAD FAILED INTERNALLY CAUSING MODERATE AMOUNTS OF GROUND METAL TO BE PUMPED INTO NOSE CASE. GOVERNOR SHAFT SEIZED. ENGINE REMOVED FOR TEAR-DOWSDR 98ZZZX112Governor · failedBETA LIGHT FLICKERED IN-FLIGHT. NO OTHER DISCREPANCIES ON NEXT DEPARTURE DURING TAXI OPERATION . PROPELLER WENT TOWARD COURSE PITCH UNCOMMANDED. ITT WENT TO RED LINE, PILOT SHUT ENGINE DOWN. INTERNAL FAILURE OF PROP GOV RESULTED IN METAL EXITING THE PROP GSDR 98ZZZX109Cam Assy · wornDURING ENGINE REPAIR RESULTING FROM CATASTROPHIC FAILURE OF PROPELLER GOVERNOR, DISSASSEMBLY OF PROPELLER PITCH CONTROL REVEALED SEVERE WEAR OF CAM SLOT AND PIN ON SLEEVE ASSY 869647-5. THERE IS LITTLE DOUBT THAT THIS ASSY WOULD HAVE FAILED LONG BEFORE SCHEDUSDR 97ZZZX2002Snap Ring · failedWHILE ATTEMPTING TO LAND, THE PILOT PUT THE GEAR HANDLE DOWN AND CONFIRMED THE NOSE GEAR DID NOT GO DOWN AND LOCKED. THIS AIRCRAFT WAS LANDED WITH THE NOSE GEAR UP WITH DAMAGE TO THE FUSELAGE STRUCTURE. UPON INSPECTION, IT WAS FOUND THE NOSE GEAR LOWER STRUTSDR 97ZZZX1479Actuator · leakN2 SYSTEM SHOWED HIGH PRESSURE. FOUND HYDRAULIC FLUID IN N2 SYSTEM. DRAINED SYSTEM AND RESERVICED WITH N2. SUSPECT CAUSE IS MAIN LANDING GEAR EMERGENCY EXTEND ACTUATOR HAS LEAKING SEAL.SDR CA970206009Window · cracked(CAN) LATERAL CRACK RUNNING ALONG THE FASTENING SCREWS OF THE OUTBOARD WINDOW. THE CRACK COULD NOT BE SEEN WITH A PRISM AND WAS ONLY DETECTED WHEN IT SPLIT THE WINDOW IN TWO AT THE FORWARD CORNER DOWN TO THE MIDWAY POINT. SUBMITTER STATES THE CRACK PROBABLY CRSDR 97ZZZX493Control Cable · frayedPILOT REPORTED A FRAYED CABLE IN AFT FUSELAGE. THE CABLE FOR THE ELEVATOR TRIM WAS FRAYED AT ELECTRIC ELEVATOR TRIM SERVO LOCATION. CAUSE OF FRAYING WAS DUE TO AN IMPROPERLY INSTALLED CAPSTAN, P/N 49A26, ON THE SERVO ASSY WHICH CAUSED THE GROOVE IN THE CAPSTSDR 97ZZZX492Capstan · misinstalledPILOT REPORTED A FRAYED CABLE IN AFT FUSELAGE. THE CABLE FOR THE ELEVATOR TRIM WAS FRAYED AT ELECTRIC ELEVATOR TRIM SERVO LOCATION. CAUSE OF FRAYING WAS DUE TO AN IMPROPERLY INSTALLED CAPSTAN, P/N 49A26, ON THE SERVO ASSY WHICH CAUSED THE GROOVE IN THE CAPSTSDR 96ZZZX5259Tube · failedAIRCRAFT ABORTED TAKEOFF DUE TO NOSE WHEEL SHIMMY. FULL REVERSE AND BRAKES APPLIED. NOSE GEAR COLLAPSED. MCCREARY 6.00 X 6 TUBE APPEARS TO HAVE FAILED ALONG A MOLD LINE. TUBE IS MARKED 77-2-015 AND 120 113 09E. THE OPERATOR WILL SEND THE TUBE OUT FOR EVALSDR 96ZZZX2476Windshield · crackedWINDSHIELD CRACKED UNDER NORMAL AND PROPER OPERATING CONDITONS WITH ONLY 550 HOURS ON WINDSHIELD.SDR 96ZZZX2475Windshield · crackedWINDSHIELD CRACKED UNDER NORMAL AND PROPER OPERATING CONDITIONS WITH 3,400 HOURS ON WINDSHIELD.SDR 96ZZZX2223Control Cable · frayedDURING C/W TWIN COMMANDER SB 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS CABLE STRANDS BROKEN. THE INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL OR INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THIS PROCEDURE IS THESDR 96ZZZX2222Control Cable · frayedDURING C/W TWIN COMMANDER SB 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS CABLE STRANDS BROKEN. THE INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL OR INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THIS PROCEDURE IS THESDR 95ZZZX6317Control Cable · frayedDURING C/W TWIN COMMANDER SB NR 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS CABLE STRANDS BROKEN. THE INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL OR INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THE SB PROCEDURE SDR 95ZZZX6316Control Cable · frayedDURING C/W TWIN COMMANDER SB NR 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS CABLE STRANDS BROKEN. THE INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL OR INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THE SB PROCEDURE SDR 95ZZZX5249Control Cable · frayedDURING C/W TWIN COMMANDER SB NR 195B, FOUND BOTH AFT RUDDER CABLES TO HAVE NUMEROUS STRANDS BROKEN. INSTRUCTIONS IN THE SB DO NOT ADDRESS THE REMOVAL AND INSPECTION AS OUTLINED IN AC 43.13-1A, CHAPTER 4, PARAGRAPH 198, FIGURE 4.14. THIS IS THE ONLY WAY TO PRSDR 95ZZZX4033Battery · damagedUPON ROUTINE INSPECTION. LEAD FOUND SPRAYED ALL OVER THE BATTERY INTERIOR. THE CONNECTOR BOX SEALANT WAS MELTED AND CRACKED. SEALANT AND LEAD ALSO CAME OUT CONNECTOR PIN AND ALSO RUINED THE ELON CONNECTOR BEYOND FURTHER USE.SDR 95ZZZX2074Spar Cap · crackedUPPER FORWARD STABILIZER SPAR CAP FOUND CRACKED IN RADIUS OF UPPER FLANGE ABOVE UPPER RIGHT ATTACH BOLT.
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