JASC 5302
Service difficulty reports · 965
Reports filed under 5302 · Rotorcraft Tail Boom, newest first.
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 jasc_code = '5302' 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 jasc_code = '5302' 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 CA120904004Fitting · cracked(CAN) UPPER ATTACH FITTING LT SIDE REPLACED WITH NEW PART, PN350A23422221.SDR QML2011102000003Frame · crackedDURING INSP OF THE TAILBOOM AND ATTACH POINT, CRACKING WAS NOTED IN THE UPPER STARBOARD ATTACH BOLT HOLE OF THE TAILBOOM ATTACH FRAME. PN 206-032-308-121, LOCATED AT STA 231.472. AXIAL STRESS EXERTED AT THIS LOCATION BY TAILBOOM FLEX, OVERTIME, CAUSES WEAKENSDR QML2011102000002Frame · crackedDURING INSP OF THE TAILBOOM AND ATTACH POINT, CRACKING WAS NOTED IN THE UPPER STARBOARD ATTACH BOLT HOLE OF THE TAILBOOM ATTACH FRAME, PN 206-032-308-121, LOCATED AT STA 231.472. AXIAL STRESS EXERTED AT THIS LOCATION BY TAILBOOM FLEX, OVERTIME, CAUSES WEAKENISDR CA111020004Bulkhead · cracked(CAN) DISCOVERED DURING A REGULAR INSPECTION, A .2500" CRACK COMING FROM THE AFT LT STUD HOLD FOR THE TAIL ROTOR GEARBOX MOUNTING ON THE TAIL BOOM.SDR HEEA20111019326Skin · corrodedTAILBOOM SKIN FOUND CORRODED, COMMON TO PREVIOUSLY INSTALLED LARSON ANTENNA PROVISIONS. THE TAILBOOM WILL THEN BE REPAIRED IAW THE FAA-APPROVED REPAIR DATA.SDR QMLA20111014001Attach Fitting · corrodedDURING 1800 HR INSP NOTICED CORROSION AROUND PATCH AT THE FLUX VALVE MOUNT, REMOVED PATCH AND DISCOVERED HEAVIER CORROSION.SDR HEEA20111012268Support · failedHORIZ STABILIZER SUPPORT STRUT FITTING FAILED. SUPPORT STRUT STRUCK BY TAIL ROTOR BLADES. REMOVED HORIZ STABILIZER ASSY.SDR CA121010008Bracket · broken(CAN) UPPER LT PN 350A23-4222-21, 388.9 TOTAL HOURS. BROKEN IN PIECES. LOWER RT PN 350A23-4223-20, 789.9 TOTAL HOURS. CRACKED UPPER LEFT PN 350A23-4222-21, STOP DRILLED AT 789.9, REPLACED AT 876.7 TOTAL HOURS CRACKED. THIS IS THE FIRST OF 3 SIMILAR BRACKETSDR 2011F00208Skin · crackedWHILE PERFORMING MX, A CRACK WAS DISCOVERED IN THE OUTER SKIN OF THE TAILBOOM ON THE LT SIDE AT THE FORWARD ROW OF RIVETS THAT SECURED THE TAIL ROTOR GEARBOX HOUSING. THE CRACK APPEARS TO HAVE STARTED AT ONE OF THE RIVETS, EXTENDED TO ANOTHER AND WAS CONTINUSDR CA120904002Fitting · cracked(CAN) PN 350A23-4222-20, UPPER, 350A23-4223-20 LOWER STABILIZER ATTACH BRACKETS RT REPLACED. WORK CARRIED OUT BY MFG FIELD SERVICE REPRESENTATIVE.SDR 2011FA0000629Structure · crackedCRACK IN TAIL BOOM.SDR IAVA201109140001Structure · crackedPILOT REPORTED THAT THERE WAS A VIBRATION IN THE ACFT. INVESTIGATION FOUND THE RIVETS WORKING AT TAILBOOM TO TAIL ROTOR GEARBOX CASTING MOUNT. FURTHER INVESTIGATION FOUND A CRACK IN THE TAIL BOOM AT THE 11:00 POSITION, APPROX 1.5 INCHES LONG AT THE ROW OF RISDR EVCA20110909005Attach Fitting · crackedFOUND CRACK IN LT UPPER AIRFRAME TAILBOOM ATTACH FITTING.SDR QMLA2011081711087Frame · crackedTHE MECHANIC FOUND A CRACK IN THE TAILBOOM AT FRAME 10L, DURING A SCHEDULED INSP.SDR 2011FA0000529Skin · crackedDURING INSPECTION, A LARGE CRACK WAS FOUND ON UPPER VERTICAL FIN NEAR THE FWD ATTACHMENT POINT. CRACK IS LOCATION ON L/E EXTENDING FROM RT SIDE TO LT SIDE OF ACFT IN THE AREA ABOVE THE FWD REINFORCEMENT. TOTAL LENGTH OF CRACK IS 8 INCHES. COULD BE IMPROPER SDR CA110802010Support Angle · crackedWHILE A DAILY CHECK WAS BEING CARRIED OUT BY THE PILOT, HE NOTICED A CRACK DEVELOPING ON THE FWD PART OF THE UPPER LT SUPPORT ANGLE THAT SUPPORTS THE HORIZONTAL STABILIZER TO THE TAILBOOM. ACFT WAS GROUNDED.SDR CA110629003Attach Fitting · crackedUPPER LT (FUSELAGE) TAILBOOM ATTACHMENT FITTING FOUND WITH 1" VERTICAL CRACK THROUGH 1 FASTENER HOLE. FOUND ON DAILY INSP. PART REPLACED WITH NEW FITTING. ACFT MFG RECENTLY INCREASED THE INSP CRITERIA FOR THE ADJACENT TAILBOOM ATTACHMENT FITTING REF: ASB 206SDR QML2ML0376Structure · crackedDURING A VISUAL INSPECTION OF THE ACFT FOUND AN AREA ON THE TAIL BOOM THAT LOOKED LIKE CORROSION AT LT SIDE BL 300 STA 7600 WL 2800. AFTER INSPECTING THE WHOLE TAIL BOOM ASSEMBLY, A CRACK WAS FOUND AT BL 50 WL 3000 STA 9400 RT SIDE 1 INCH IN LENGTH. REPLACED TSDR QML2ML0375Structure · crackedDURING A VISUAL INSPECTION OF THE ACFT FOUND AN AREA ON THE TAIL BOOM THAT LOOKS LIKE CORROSION AT LT SIDE BL 300 STA 7600 WL 2800. AFTER INSPECTING THE WHOLE TAIL BOOM ASSEMBLY A CRACK WAS FOUND AT BL 50 WL 3000 STA 9400 RT SIDE 1 INCH IN LENGTH. REPLACED SDR QML2ML0374Structure · damagedDURING A VISUAL INSPECTION OF THE ACFT FOUND AN AREA ON THE TAIL BOOM THAT LOOK LIKE CORROSION ON THE TAIL BOOM AT LT SIDE BL 300 STA 7600 WL 2800. AFTER INSPECTING THE WHOLE TAIL BOOM ASSEMBLY A CRACK WAS FOUND AT BL 50 WL 3000 STA 9700 RT SIDE 1 INCH IN LENSDR QML2ML0373Frame · crackedDURING A VISUAL INSPECTION OF THE ACFT FOUND AN AREA ON THE TAILBOOM THAT LOOK LIKE CORROSION ON THE TAIL BOOM AT LT SIDE WL 2800 STA 6800. AFTER REMOVING THE TAIL BOOM AND INSPECTING THE WHOLE TAIL BOOM ASSEMBLY A CRACK WAS FOUND AT THE 10L FRAME BULKHEAD 1/8SDR EVCA20110603001Fitting · crackedFOUND CRACK IN LT UPPER AIRFRAME TAILBOOM MOUNT FITTING.SDR UNFR2011052500003Skin · misrepairedPERFORMING INSP ON TAILBOOM AND DISCOVERED RIVETS IN TAILBOOM THAT WERE NOT CORRECTLY INSTALLED AT PREVIOUS REPAIR ON TOP SKIN BECAUSE OF DIMPLES IN SKIN DID NOT LINE UP WITH HOLES IN STRINGER CORRECTLY. PREVENTING SKIN TO RECESS CORRECTLY, THUS WITH GAP IN SDR EVCA20110511001Support Bracket · elongatedFOUND HANGER BRACKET HOLE ELONGATED ON TAILBOOM.SDR KBMA11FA0000298Structure · damagedVISUAL INSP OF VERTICAL FIN REVEALED LEADING EDGE MOVEMENT. REMOVAL OF ATTACHMENT BOLTS REVEALED SHEARED RIVETS.SDR CA110503008Bulkhead · cracked2 CRACKS FOUND ON TAILBOOM BULKHEAD. CRACKS GENERATED FROM THE HOLES FOR T/R GEARBOX STUDS, FOUND DURING TAIL ROTOR GEAR BOX ATTACHMENT CHECK ON 300 HOUR AIRFRAME INSPECTION.SDR 2011FA0000311Skin · chafedDURING THE INSTALLATION OF A TAIL BOOM ON THE SAME MODEL ACFT THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALONG THE BOTTOM OF THE INNER TAIL BOOM SKIN UNDER THE WIRE HARNESSES. IN SOME CASES IT HAD PENETRATEDSDR 2011FA0000310Skin · chafedDURING THE INSTALLATION OF A TAIL BOOM ON THE SAME MODEL ACFT THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALONG THE BOTTOM OF THE INNER TAIL BOOM SKIN UNDER THE WIRE HARNESSES. IN SOME CASES IT HAD PENETRATEDSDR 2011FA0000309Structure · crackedDURING THE VALVE CHECK A MECHANIC NOTED A CRACK EXTENDING LONGITUDINALLY FROM THE LT FWD NAV/VOR ANTENNA MOUNT. MFG HAS PREVIOUS KNOWLEDGE OF THIS DEFECT AND HAS DEVISED A REPAIR SCHEME FOR THIS DEFECT. RDAS (REPAIR DESIGN APPLICATION SHEET) NR RDAS-AE11-014SDR 2011FA0000308Skin · chafedDURING THE INSTALLATION OF A TAILBOOM ON THE SAME MODEL ACFT THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALONG THE BOTTOM OF THE INNER TAIL BOOM SKIN UNDER THE WIRE HARNESSES. IN SOME CASES IT HAD PENETRATED SDR 2011FA0000307Skin · chafedDURING THE INSTALLATION OF THE TAILBOOM THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALONG THE BOTTOM OF THE INNER TAILBOOM SKIN UNDER THE WIRE HARNESSES. IN SOME CASES IT HAD PENETRATED THE COMPOSITE MATERIASDR QMLA2011050311053Frame · crackedDURING A 1200 HR INSP, THE MECHANIC FOUND A CRACK IN THE TAILBOOM AT UPPER FRAME 9L RUNNING VERTICAL FROM THE LOWER RT RIVET HOLE TO THE EDGE.SDR M7KA20110501#4134Skin · misrepairedDURING PREFLIGHT INSP, A CRACK WAS DISCOVERED RADIATING FROM THE INSIDE LOWER AFT RT CORNER OF THE TAIL BOOM TAIL CONE CUTOUT FOR THE HORIZ STABILIZER. AN OVER LYING DOUBLER WAS NOT CRACKED AND OBSCURED THE CRACK FROM EASY VIEWING. WITH THE HORIZ STABILIZER SDR M7KA20110501#4545Doubler · crackedDURING PERIODIC INSP, A CRACK WAS DISCOVERED IN THE INSIDE CORNER OF THE TAIL BOOM TAIL CONE DOUBLER. THIS DOUBLER WAS A MFG PART THAT WAS INTENDED AS A REPAIR OF A CRACK IN THE TAIL CONE SHEET METAL PREVIOUSLY REPORTED UNDER UNIQUE CONTROL NUMBER M7KA20101210SDR M7KA20110501#4173Skin · misrepairedDURING INSP A CRACK WAS DISCOVERED RADIATING FROM THE INSIDE LOWER AFT RT CORNER OF THE TAILBOOM TAIL CONE CUTOUT FOR THE HORIZ STABILIZER. AN OVER LYING SKIN DOUBLER WAS NOT CRACKED AND OBSCURED THE CRACK FROM EASY VIEWING. WITH THE HORIZ STABILIZER REMOVESDR M7KA20110423#4797Skin · damagedTAILBOOM CONE SKIN CRACK WAS DISCOVERED DURING ROUTINE PERIODIC INSPECTION IN THE LOWER AFT RT CORNER OF THE CUTOUT FOR THE HORIZ STAB. THE CRACK WAS CONSEALED UNDERNEATH THE TAIL CONE SKIN DOUBLER AND WAS OBSERVED BY VIEWING FROM THE LT SIDE OF THE HORIZONTASDR M7KA20110423#4437Skin · crackedDURING ROUTINE INSP, A VISIBLE RADIATING CRACK IN THE PAINT AROUND THE HEAD OF A COUNTERSUNK RIVET ON THE TAILBOOM CONE TO FENESTRON RING JUNCTION WAS NOTED. FOLLOWING CHEMICAL STRIPPING OF THE PAINT IT WAS APPARENT VISUALLY THAT THE SUSPECT AREA OF THE RING JSDR 3S8R2011041600005Attach Fitting · crackedRIGHT ANGLE OF TAILBOOM ATTACH FITTING CRACKED. REPLACED WITH NEW, TAILBOOM FRAME 9000, RE-WORK SHEET 330530604.SDR 3S8R2011041600004Angle · crackedHORIZONTAL STABILIZER INTERNAL ANGLE CRACKED. TO BE REPLACED WITH NEW.SDR M7KA201104174356Structure · crackedDURING ROUTINE INSPECTION, A VISIBLE CRACK IN THE PAINT AROUND THE HEAD OF A COUNTERSUNK RIVET ON THE TAIL BOOM CONE TO FENESTRON RING JUNCTION WAS NOTED. FOLLOWING THE STRIPPING OF THE PAINT THROUGH CHEMICAL MEANS AND APPLICATION OF DYE PENETRANT INSPECTION SDR RMXADMR334393Skin · scratchedA .012" DEEP .3750" LONG SCRATCH WAS FOUND ON THE RT SIDE OF THE TAIL BOOM UNDER THE OMEGA STRINGER, 12 INCHES AFT OF THE CONNECTING FLANGE.SDR CA110408003Fitting · cracked(CAN) TAIL BOOM LOWER LT ATTACHMENT FITTING FOUND CRACKED ON DAILY INSPECTION. ACFT GROUNDED. R & R WITH NEW PART. CRACK EXTENDS FROM TAIL BOOM ATTACHMENT BOLT HOLE TO EDGE OF FITTING. ALSO, A SECOND CRACK FOUND PROGRESSING FROM THE BOLT HOLE IN THE OPPOSITSDR HC7A20110402001Fitting · crackedDURING ROUTINE INSPECTION, THE UPPER LEFT STATION 300 TAIBOOM FITTING WAS FOUND TO BE CRACKED. THE CRACK APPEARED TO START AT THE BOLT HOLE AND EXTEND TO LOWER EDGE. THE FITTING WAS REPLACED IAW SIKORSKY STRUCTURAL REPAIR MANUAL AND THE AIRCRAFT WAS RETURNED SDR QMLA2011033111040Structure · crackedCRACK DISCOVERED DURING INSPECTION ON VERTICAL FIN CAP AT STA 10950, BL 20, AND WL 4050. ACFT BEING FERRIED TO FACILITATE REPAIR.SDR CA110330004Fitting · cracked(CAN) ONE INCH CRACK IN LOAD FLANGE OF FITTING.SDR QMLA2011032311036Skin · crackedA RIVET HEAD WAS FOUND MISSING ON THE DOUBLER ON THE RT SIDE OF THE VERTICAL FIN AT THE TAILBOOM/ VERTICAL FIN TRANSITION. FURTHER INSP REVEALED A CRACK IN THE VERTICAL FIN FWD BULKHEAD/ SPAR STRUCTURE, STARTING FROM THE TOP RT AFT RECEPTACLE HOLE FOR THE TRASDR KBMA2011031802Structure · crackedCRACKED TAIL BOOM.SDR QMLA2011031711034Support · crackedTHE MECHANIC FOUND A CRACK WHILE PERFORMING AN AIRWORTHINESS INSP ON THE LT UPPER TAILBOOM TO HORIZ STABILIZER SUPPORT IN THE BEND RADIUS INTENDING TO OTBD EDGE FWD OF THE FIRST SCREW. NO HIDDEN DAMAGE WAS FOUND ON THE TAILBOOM UPON REMOVAL OF THE SUPPORT. TSDR PG92011F00002Skin · crackedON 3-15-11 DURING A 100 HOUR INSP, A CRACK WAS DISCOVERED IN TAILBOOM SKIN ON THE RIGHT SIDE WHERE THE HORIZ STAB MOUNTS AFT LOWER CORNER. THE CRACK ORIGINATES THERE AND CONTINUES UNDER A SPAR (OVER 1 INCH LONG). MFG HAS BEEN CONTACTED AND ALREADY HAS A REPASDR PG92011F00001Skin · crackedON 3-14-11 DURING THE INSP OF A 600 HR T INSP, A CRACK WAS DISCOVERED IN THE TAILBOOM SKIN ON THE RT SIDE WHERE THE HORZ STAB MOUNTS AFT LOWER CORNER. THE CRACK ORIGINATES THERE AND CONTINUES UNDER A SPAR (OVER 1 INCH LONG). MFG HAS BEEN CONTACTED AND ALREAD
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