Rockwell International 114
Service difficulty reports · 30
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 = '114' 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 = '114' 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 2025FA0000758Spar · crackedCRACK EMANATING FROM UPPER LEFT CORNER OF THE RUDDER SPAR AND DOWN BEHIND THE HINGE CONNECTION PLATE FOR APPROXIMATELY 3.5" AND THEN TURNS INBOARD FOR A DISTANCE OF 1/2 THE WIDTH OF THE SPAR. THE CRACK WAS FOUND DURING THE REMOVAL OF THE RUDDER TO CHANGE THE BSDR 2025FA0000234Tire · damagedRETREAD TIRES - SHRINKING AND SEPARATION OF TIRE CAP BETWEEN TREAD CHANNELS. ALSO, CRACKING AT RETREAD CAP MATING AREA ON SIDEWALL. MANUFACTURER P/N'S AS FOLLOWS: 500-5 6 PLY RT AND 700-6 6 PLY RTSDR 2024FA0000657Actuator · overpressuredREAR ATTACH BOLT FAILURE ON NOSE GEAR RETRACT SERVO. WE SERVICE 3 COMMANDER 114'S AND ALL THREE HAVE THE SAME PROBLEM. ONE FAILED COMPLETELY CAUSING THE NOSE GEAR TO EXTEND ABOVE EXTENSION SPEED, THE OTHER TWO WERE FOUND TO BE BENT AT ANNUAL INSPECTION.SDR 2023FA0000666Tire · failedAIRCRAFT PURCHASED IN JUNE, 2020 & IN HANGAR FOR REPAIRS & REWORK TO RETURN AIRCRAFT TO AIRWORTHY
CONDITION. TIRES RECAPPED OR RETREAD, CONCERN IS THAT TIRES ARE CRACKING BETWEEN THE TREAD - IN WHAT WOULD BE THE WATER CHANNEL OF THE TIRES. ALSO, IT HAS BEENSDR 2023FA0000464Tire · damagedAIRCRAFT PURCHASED IN JUNE, 2020 AND PLACED IN HANGAR FOR REPAIRS AND REWORK TO RETURN AIRCRAFT TO AIRWORTHY
CONDITION. LAST TIME AIRCRAFT HAS FLOWN WAS IN JUNE 2020. AIRCRAFT HAS NOT BEEN MOVED FROM HANGAR SINCE
PURCHASED. TIRES PURCHASED IN OCTOBER, 2020 SDR 2017FA0000656Drag Brace · brokenTHE NOSE LANDING GEAR DRAG BRACE FAILED AND IS DETERMINED TO BE THE PRIMARILY CAUSE OF THE FAILURE OF THE NOSE GEAR DOWN AND LOCKED POSITION AND THE FALSE INDICATION TO THE PILOT. PILOT STATED WHEN HE LOWERED THE LANDING GEAR TO LAND HE INITIALLY RECEIVED TWO SDR 2013FA0000460Seat Track · wornDURING LANDING, SEAT SUDDENLY SLID TO ITS FULL AFT POSITION, WAS NOT ABLE TO REACH CONTROLS. LT WING TIP DAMAGED ON THE UNDERSIDE FROM SCRAPING RUNWAY.SDR 2011FA0000156Spar · crackedDURING THE ACCOMPLISHMENT OF SL-114-17 A SMALL HAIRLINE CRACK WAS DISCOVERED. THE CRACK IS APPROX. 2.35" IN LENGTH, ON THE RT ELEVATOR SPAR, BELOW THE OUTBOARD ELEVATOR HINGE ATTACH POINT. THE AREA OF CONCERN IS LOCATED ON THE RH ELEVATOR 69.35 FROM C/L & FS 2SDR 2008FA0000743Spar · crackedSPAR IS CRACKED AND BROKEN OUT AT UPPER HINGE ATTACH POINT. THIS SPAR WAS REPLACED WITH NEW 1-1-99 FOR SAME CONDITION. THIS CONDITION WAS FOUND BY CLOSE EXAMINATION OF AREA DURING ANNUAL INSPECTION. WE ARE IN RECEIPT OF INFORMATION OF SAME FAILED CONDITION OSDR 2006FA0000092Riser · crackedTURBO SYSTEM INSTALLED IAW STL, BOTH LT AND RT EXHAUST RISERS HAD MANY CRACKS AND DEEMED UNSERVICEABLE. 207.8 HRS SINCE NEW, REPLACED UNITS FAILED IN 140.0 MORE. (K)SDR QC42002F00001Housing · crackedTHE BENDIX DRIVE HOUSING CRACKED COMPLETELY THROUGH AND THE FORWARD BEARING SECTION FELL OFF THE AIRCRAFT. IAW LOG BOOKS, THIS STARTER HAS BEEN OVERHAULED TWICE WITHIN 240 HOURS OF OPERATION. THE LOGS DO NOT STATE THE REASON FOR THE OVERHAULS.SDR YBU2002F00000Brace · crackedPILOT REPORTED NORMAL LANDING. THEN LOST CONTROL OF AIRCRAFT. AIRCRAFT CAME TO REST OFF THE LT SIDE OF THE RUNWAY, LT MAIN GEAR COLLAPSED. LT MAIN GEAR, UPPER DRAG BRACE SPLIT IN TWO. SUSPECTED METAL FAILURE, DUE TO IMPURTIES AND FATIGUE.SDR AUS20021238Bolt · broken(AUS) NOSE LANDING GEAR ACTUATOR REAR MAIN ATTACHMENT BOLT BROKEN INAREA OF SHAFT.SDR AUS20011280Control Cable · misinstalled(AUS) LT RUDDER CONTROL CABLE INCORRECTLY ROUTED UNDER SUPPORT BRACKET. CABLE RUBBING ON PULLEY SUPPORT BRACKET. ELEVATOR TRIM CABLE ALSO INCORRECTLY ROUTED AND FOULING ON STRUCTURE. PERSONNEL/MAINTENANCE ERROR.SDR 20000918SH023Seat · brokenSEAT FRAME TUBE FAILED AT LOCATIONS RESULTING IN SEAT BACK GOING TO A FULL RECLINE POSITION. SEAT FRAME HAD BEEN MODIFIED PER SB 114-21A, REF AD 85-03-04R2. (X)SDR AU000555Bolt · separated(AUS) NOSE LANDING GEAR RETRACTION RAM TO NOSE LANDING GEAR STRUT SEPARATED DUE TO BOLT, NUT, WASHER AND SPLIT PIN SECURING THE TWO ITEMS COMING LOOSE.SDR AU000179Bolt · broken(AUS) MAIN LANDING GEAR STRUT TRUNNION PIN RETAINING BOLT CRACKED. TRUNNION PIN ALSO WORN.SDR 99ZZZX975Spar · crackedRUDDER SPAR CRACK AT UPPER HINGE FITTING (PN 44254-501) WAS DISCOVERED DURING AN ANNUAL INSPECTION.SDR AU980624Bolt · broken(AUS) NOSE LANDING GEAR ACTUATOR UPPER ATTACHMENT BOLT SHEARED.SDR 98ZZZX485Spar · crackedDURING ANNUAL INSPECTION, FOUND RUDDER SPAR CRACKED ON EDGE OF ALUMINUM SPACERS MOUNTED UNDER TOP RUDDER HINGE. CRACK SEEMS TO ORIGINATE FROM EDGE OF ALUMINUM SPACERS POSSIBLY FROM FLEXING IN THIS AREA. THIS IS A VERY HARD AREA TO SEE WELL DURING NORMAL INSPESDR AU970314Mount · broken(AUS) ENGINE MOUNT ASSEMBLY TUBE CRACKED AT LH NLG TRUNNION - TRUNNION PIN DEFORMED - AIRCRAFT USED FOR PILOT TRAININGSDR AU961130Bolt · corroded(AUS) ELEVATOR HINGE BOLT CORRODED - FOUND DURING ELEVATOR BEARING CHANGE WHEN ELEVATORS REMOVEDSDR AU961014Relay · mis wired(AUS) OVERVOLTAGE RELAY INCORRECTLY WIRED - 'BATTERY' AND 'LOAD' LEADS TRANSPOSED CAUSING OVERVOLTAGE RELAY TO MALFUNCTION - LOSS OF BATTERY VOLTAGE - LOGBOOK FAILED TO REVEAL ANY WORK CARRIED OUT IN THIS AREA - PERSONNEL/MAINTENANCE ERRORSDR 96ZZZX1519Spar · crackedAIRCRAFT CAME IN FOR AN ANNUAL. AFTER SEEING JANUARY, 1996 ALERTS, DECIDED TO CHECK THIS AREA AND FOUND A 2.50 INCH CRACK ON LT SIDE OF RUDDER FITTING ATTACH HOLES.SDR EY2R9600296Steel Ball · corrodedSTEEL BALL CORRODED.SDR 95ZZZX6428Spar · crackedRUDDER SPAR CRACKED UNDER UPPER HINGE AND PROTRUDED PAST HINGE. CRACK RAN ALONG THE SIDE OF SHIM, PN 40113-3. SL-114-17 ADDRESSES THIS PROBLEM.SDR 95ZZZX2740Bolt · misinstalledDURING ANNUAL INSPECTION, TRIM TAB ACTUATOR-TO-ROD BOLT WAS FOUND INSTALLED BACKWARDS CAUSING END OF THE BOLT TO SHEAR OFF. THIS COULD HAVE CAUSED LOSS OF CONTROL, ELEVATOR FLUTTER, AND SUBSEQUENT LOSS OF ELEVATOR. THIS IS AN EXREMELY HARD BOLT TO GET IN PROSDR 95ZZZX905Drag Brace · failedON TAKEOFF FROM LUK, PILOT HEARD A LOUD CRACK AT GEAR RETRACTION. NOSE GEAR WOULD NOT RETRACT. PILOT CYCLED GEAR DOWN AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT AND FOUND UPPER DRAG BRACE CRACKED. REPLACED WITH NEW UNIT.SDR 95ZZZX600Spar · crackedUPON REPLACEMENT OF OUTBOARD HINGE ATTACHMENT OF RT ELEVATOR, CRACKS WERE FOUND IN SPAR. INSPECTION OF LT ELEVATOR REVEALED SAME CRACKS ONLY WORSE. CRACKS ARE FOUND BY BOLT HOLES FOR OUTBOARD HINGE ATTACHMENTS. CRACKS CAN BE SEEN THROUGH HOLES IN OUTBOARD RSDR 95ZZZX599Spar · crackedUPON REPLACEMENT OF OUTBOARD HINGE ATTACHMENT OF RT ELEVATOR, CRACKS WERE FOUND IN SPAR. INSPECTION OF LT ELEVATOR REVEALED SAME CRACKS ONLY WORSE. CRACKS ARE FOUND BY BOLT HOLES FOR OUTBOARD HINGE ATTACHMENTS. CRACKS CAN BE SEEN THROUGH HOLES IN OUTBOARD R
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