# Service difficulty reports: Beech A24R A list on [Beech A24R](https://openairdocs.org/model/beech-a24r.md). Newest first. General aviation reporting is voluntary. - [SDR 2006FA0000423](https://openairdocs.org/sdr/2006FA0000423.md): Drag Brace · broken · Apr 19, 2006 · N8015R · Beech A24R · Landing Gear Retraction/Extension System > THE AIRCRAFT TOUCHED DOWN UNEVENTFUL. DURING ROLLOUT, THE NOSE GEAR COLLAPSED ABOUT 1500 FT AFTER TOUCHDOWN. THE DRAG BRACE FAILED AT THE YOKE WHERE IT ATTACHES TO THE NOSE GEAR. (K) - [SDR CA020723005](https://openairdocs.org/sdr/CA020723005.md): Bearing · corroded · Jun 26, 2002 · Beech A24R · Horizontal Stabilizer Miscellaneous Structure > (CAN) WHEN INSPECTING CONTROL SURFACES, IT WAS NOTICED THAT THE HORIZONTAL STABILATOR HAD AN ABNORMAL FORE / AFT MOVEMENT. UPON DISINSTALLATION, THE HORIZONTAL STAB BUSHINGS AND BEARINGS WERE FOUND TO BE WORN AND THE BOLTS WERE FOUND TO BE CORRODED. - [SDR CA020723003](https://openairdocs.org/sdr/CA020723003.md): Handle · cracked · Jun 26, 2002 · Beech A24R · Trailing Edge Flap Control System > (CAN) FLAP HANDLE PEDESTAL IS CRACKED AT BEND ON LOWER RT FORWARD CORNER. - [SDR CA020723002](https://openairdocs.org/sdr/CA020723002.md): Arm · worn · Jun 26, 2002 · Beech A24R · Trailing Edge Flap Control System > (CAN) FLAPS WERE FOUND TO BE LOOSE. AFTER INVESTIGATION IT WAS FOUND THAT THE FLAP ARMS THAT JOIN THE FLAP CONTROL TUBE TO THE FLAP RODS HAD ELONGATED BOLT HOLES DUE TO WEAR. THE ELONGATED HOLES ARE THE ONES WHERE THE CLEVIS BOLTS ATTACH THE ARMS TO THE FLAP C - [SDR CA020723001](https://openairdocs.org/sdr/CA020723001.md): Bracket · corroded · Jun 26, 2002 · Beech A24R · Main Landing Gear Attach Section > (CAN) UPON VISUAL INSPECTION OF THE LT WHEEL WELL, THE ANGLE HOLDING THE UPLOCK HOOK BRACKET WAS IDENTIFIED AS BEING HEAVILY CORRODED, SHOWING SIGNS OF ADVANCED EXFOLIATION CORROSION. UPON DISASSEMBLY, INTERGRANULAR CORROSION WAS ALSO FOUND ON THE UPLOCK HOOK - [SDR CA020606005](https://openairdocs.org/sdr/CA020606005.md): Motor · worn · Jun 5, 2002 · Beech A24R · Trailing Edge Flap Actuator > (CAN) NOISE IN FLAP MOTOR CAUSED FURTHER INSPECTION. UPON ACCESSING MOTOR UNDER REAR SEAT, SPARKS WERE NOTED COMING OUT OF DRIVE AND OF MOTOR DURING ACTUATION. ARMATURE MOTOR BUSHINGS WERE WORN TO THE EXTENT THAT THERE WAS CONTACT WITH THE END PLATE DURING OPE - [SDR 20001128SH001](https://openairdocs.org/sdr/20001128SH001.md): Hinge · corroded · Nov 2, 2000 · N8022R · Beech A24R · Horizontal Stabilizer Structure > THE PAINT WAS CRACKED AROUND THE HINGE PLATE ON THE RT SIDE. A FINGERNAIL WOULD GO UNDER A COUPLE OF THE RIVETS. WHEN THE RIVETS WERE DRILLED OUT, SEVERAL SPUN AND BROKE BEFORE THE BIT WENT THROUGH. THE BACK SIDE OF THE HINGE PLATES WAS RUSTED AND BLACK GA - [SDR CA990804034](https://openairdocs.org/sdr/CA990804034.md): Spar · hole oversized · Jul 20, 1999 · Beech A24R · Wing, Fuselage Attach Fittings > (CAN) REQUIRED WASHERS NOT INSTALLED BETWEEN BUSHING AND FUSELAGE FITTING. THIS ALLOWED BUSHING TO MOVE FORWARD. BECAUSE THERE WAS NOT ENOUGH BEARING SURFACE, THIS ALLOWED BUSHING TO ENLARGE HOLE IN SPAR AND FILLER CAUSING CRACKS TO RADIATE FROM HOLE AND ALL - [SDR CA990804033](https://openairdocs.org/sdr/CA990804033.md): Spar · hole oversized · Jul 15, 1999 · Beech A24R · Wing, Fuselage Attach Fittings > (CAN) WASHERS ARE REQUIRED BETWEEN BUSHING AND FUSELAGE ATTACH FITTING TO HOLD BUSHING IN PLACE. THESE WASHERS WERE MISSING AND ALLOWED THE BUSHING TO MOVE FORWARD. THERE WAS NOT ENOUGH BEARING SURFACE AVAILABLE, SO THE BUSHING MOVED ENLARGING THE HOLE IN TH - [SDR 98ZZZX1980](https://openairdocs.org/sdr/98ZZZX1980.md): Side Brace · cracked · May 4, 1998 · N66TX · Beech A24R · Landing Gear Retraction/Extension System > DURING AN ANNUAL INSPECTION, A CRACK WAS DISCOVERED ON THE MLG UPPER SIDE BRACE WELD ASSEMBLY NEAR THE AFT ATTACH POINT. - [SDR 98ZZZX518](https://openairdocs.org/sdr/98ZZZX518.md): Blade · corroded · Jan 20, 1998 · N8015R · Beech A24R · Propeller Blade Section > CORROSION FOUND BELOW THE PTICH LINE IN THE THREADS CAUSING THE BLADE TO BE UNAIRWORTHY PER MCAULEY SM NR 720415. SUBMITTER STATED ADHERING TO PROPER COMPLIANCE TIMES OF AD 91-15-04 MAY HAVE PREVENTED THIS. - [SDR 98ZZZX517](https://openairdocs.org/sdr/98ZZZX517.md): Blade · corroded · Jan 20, 1998 · N8015R · Beech A24R · Propeller Blade Section > CORROSION WAS FOUND BELOW TTE PITCH LINES OF THE BLADE THREADS CAUSING THE BLADE TO BE UNAIRWORTHY PER MCCAULEY SM NR 720415. SUBMITTER STATED ADHERING TO COMPLIANCE TIMES OF AD 91-15-04 MAY HAVE PREVENTED THIS CONDITION. - [SDR 98ZZZX516](https://openairdocs.org/sdr/98ZZZX516.md): Hub · cracked · Jan 20, 1998 · N8015R · Beech A24R · Propeller Hub Section > A CRACK WAS FOUND IN THE THREADS OF HUB RENDERING IT UNAIRWORTHY PER AD 91-15-04. THE DEFECT POSSIBLY COULD HAVE BEEN FOUND AT AN EARLIER DATE IF COMPLIANCE TIME OF THE AD HAD BEEN ADHERED TO. - [SDR CA971031003](https://openairdocs.org/sdr/CA971031003.md): Cylinder · worn · Oct 23, 1997 · Beech A24R · Propeller Hub Section > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CYLINDER FOUND WORN AND WAS REPLACED. THE PROPELLER BLADE (P/N S78FBM-1.5) WAS FOUND NICKED ON THE LEADING EDGE AND THE FACE AND WAS TRIMMED. - [SDR 96ZZZX1107](https://openairdocs.org/sdr/96ZZZX1107.md): Swivel Rod · broken · Feb 1, 1996 · N9710Q · Beech A24R · Landing Gear Retraction/Extension System > NOSE WHEEL DID NOT EXTEND NORMALLY. FOUND NOSE WHEEL SWIVEL ROD BROKEN WHICH DID NOT ALLOW WHEEL TO STRAIGHTEN OUT AS IT LEFT WHEELWELL. FOUND ONE CLEVIS, PN 169-820037-3, TIGHTENED TO THE POINT WHERE IT WOULD HARDLY MOVE WITH THE ROD HOOKED. THIS TIGHTNESS - [SDR 95ZZZX2615](https://openairdocs.org/sdr/95ZZZX2615.md): Block · rivets sheared · Mar 5, 1995 · N101CM · Beech A24R · Trailing Edge Flap Control System > THREE CR3212-5-10 CHERRY FASTENERS SHEARED AT THE ATTACHMENT POINT OF THE BLOCK AND TUBE IN THE FLAP SYSTEM. FLAPS WERE SELECTED ON LANDING WITH NO RESPONSE. THIS IS A HIGH-TIME TRAINING AIRCRAFT. ## 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 = 'A24R' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/beech-a24r/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.