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 AUS20021361Fitting · cracked(AUS) TAIL ROTOR GEARBOX FITTING CRACKED.SDR CA031106002Skin · cracked(CAN) 206B3 OWNED BY FOREIGN OPERATOR: WHILE ROUTINE WALK AROUND, OBSERVED FRACTURE OF THE LOWER SKIN ON THE RT, FORWARD OF THE T/R GEARBOX SUPPORT.SDR Y3AR527YFitting · crackedDURING 100 HOUR ANNUAL INSPECTION FOUND LT UPPER FITTING ON THE FUSELAGE SIDE OF THE TAILBOOM ATTACHMENT CRACKED. REMOVED AND REPLACED FITTING (PN 206031329103S) MM. FITTING IS CRACKED ON THE OUTBOARD FLANGE BETWEEN THE 2 AFT RIVETS.SDR AUS20021040Longeron · cracked(AUS) TAIL BOOM LONGERON CRACKED AROUND TWO RIVET HOLES.SDR CA020918010Bulkhead · cracked(CAN) T/R FLIGHT CONTROL BELLCRANK SUPPORT ATTACHES TO BULKHEAD. THE BULKHEAD IS REINFORCED BY LOWER ANGLE AND UPPER ANGLE, SUSPECT THAT THE LOWER ANGLE CRACKED PROBABLY DUE TO CORROSION (NOT VERIFIED). THIS ALLOWED THE SUPPORT TO MOVE AND EVENTUALLY CRACKEDSDR CA020918004Longeron · cracked(CAN) WHILE AIRCRAFT WAS IN THE HANGAR FOR SCHEDULED MAINTENANCE, IT WAS NOTED THAT THERE WAS MOVEMENT OF THE TAILBOOM SKIN AND NO MOVEMENT OF FITTING WHEN THE TAILBOOM WAS MANUALLY FLEXED. FURTHER INVESTIGATION REVEALED THE LOWER FITTING OF THE LONGERON WAS CSDR 2002FA0001070Fitting · crackedDURING A 100 HOUR, INSPECTION, THE LEFT UPPER TAILBOOM ATTACH FITTING WAS FOUND TO BE CRACKED. THE CRACK WAS FROM THE LOWER AFT RIVET HOLE, THRU THE UPPER AFT RIVET HOLE, AND EXTENDED TO THE UPPER EDGE OF THE FITTING. (WPO12002B6504)SDR ALG2003F00033Support Angle · crackedDURING DAILY INSPECTION, CRACKED IN RADIUS DUE TO POOR FIT. LEFT LOWER SUPPORT ANGLE FOR HORIZONTAL STABILIZER. TB 4070133 WAS CW AT THIS DATE.SDR ERAA080462Skin · crackedTAILBOOM HAS CRACK ON SADDLE DOUBLER RT BASE OF VERTICAL FIN. FOUND SADDLE DOUBLER TO BOTH BE CRACKED AND LOWER SKIN BENEATH DOUBLERS CRACKED. REMOVED BOTH SADDLE DOUBLERS AND SKIN AND FOUND LOWER SKIN TO BE CRACKED. MUST BE SENT OFF TO REPAIR IN FIXTURE.SDR 2002F00765Support Fitting · crackedTAILBOOM SUPPORT FITTING CRACKED FROM EDGE THROUGH FIRST SCREW HOLE THEN UP RIVETED FLANGE BETWEEN 3RD AND 4TH FASTENER HOLES. CRACK APPEARS TO START FROM TOOLING MARKS DUE TO STRESS. INCREASE STRENGTH OF MATERIAL, POLISH EDGES TO REMOVE TOOLING MARKS, AND GSDR CA020702010Skin · cracked(CAN) CRACK IN TAILBOOM SKIN FOUND ON LEFT HAND SIDE EXTENDING FROM FORWARD RIVET ON UPPER LEFT HAND ANGLE SUPPORT P/N 407-023-800-117 TO NEXT RIVET UP ON TAILBOOM SKIN. TAILBOOM REMOVED FROM SERVICE AND IS BEING SHIPPED TO BELL HELICOPTERS FOR EVALUATION. REPSDR HEEA079962Spar · corrodedSPAR HAS CORROSION PITTING IN SEVERAL AREAS.SDR HEEA079433Cover · crackedTAILBOOM TO HORIZONTAL RADIUS COVER CRACKED. REPLACED WITH SERVICEABLE PART.SDR HEEA079432Access Panel · debondedTAILBOOM BAGGAGE ACCESS PANEL DEBONDED.SDR KBMA133853Bolt · shearedVERTICAL FIN SUPPORT BRACKETT BOLT SHEARED. REPLACED WITH NEW BOLT.SDR HEEA078766Structure · corrodedTAIL BOOM HAS CORROSION AT TOP CAP AND LOWER STRINGER MOUNT AREAS.SDR ERAA079871Structure · cracked90 DEGREE GEARBOX FITTING EXFOLIATED / INNER GRAINULAR CORROSION, CRACKED HORIZONTAL STABILIZER DOUBLER LEFT SIDE, SEVERAL CORRODED RIVETS & NUT PLEATER. INSTALLED NEW 90 DEGREE GEARBOX FITTING, NEW HORIZONTAL STABILIZER DOUBLER AND REPLACED ALL NECESSARY NUSDR CA020507015Fitting · cracked(CAN) - FITTING LOOKED CRACKED ON REMOVAL, PART CRACKED IN HALF.- FITTING WAS PRO-SEALED TO TAILBOOM & HAD VERY LITTLE GIVE.SDR HEED089184Structure · crackedCRACKED ON UPPER AFT LT SIDE OF HORIZONAL STABLIZER OPENING. REPLACE UNIT.SDR XVI2002F00000Frame · crackedX-RAY INSPECTION REVEALED A CRACK IN THE FRAME FLANGE APPROXIMATELY .1250 INCH LONG CONTAINED BY ADJACENT FASTENER HOLE. THE CRACK IS LOCTED IN THE 3 OCLOCK POSITION, LOOKING FORWARD ON THE FRAME.SDR CA020521006Skin · cracked(CAN) A 1.5 INCH CRACK WAS FOUND EMMINATING FROM A RIVET ON THE LT SIDE OF THE BOOM AT STA 136.9. THE CRACK FORMED DOWNWARD TO THE EDGE OF THE UPPER SKIN AND UPWARD FOR APPROXIMATELY 1.25 INCHES. TAILBOOM WAS REPAIRED IN ACCORDANCE WITH BELL SRM. NR 1 BEARING SDR HEEA078381Structure · corrodedTAIL BOOM FIN IS SEPARATED AND CORRODED BEYOND LIMITS.SDR JJWA078248Rib · crackedREMOVED BOTH HORIZONTAL STABILIZERS THAT HAD BEEN LAST INSTALLED OVER 5 YEARS AGO. FOUND EXCESSIVE CORROSION IN SPAR CLAMP AREA ON RIB CLOSEST TO TAILBOOM. REQUIRES TOTAL RIBE REPLACEMENT OF $1966 RIB. INSPECTED OTHER RIB ALSO HAD CORROSION & PIECE MISSING SO SDR AUS20020292Bulkhead · damaged(AUS) TAIL BOOM BULKHEAD AND SKINS CRACKED. INCORRECT ANCHOR NUTFITTED.SDR AUS20020291Skin · cracked(AUS) TAIL CONE SKIN CRACKED IN AREA UNDER RADIO AERIAL.SDR AUS20020105Mount · cracked(AUS) TAIL ROTOR GEARBOX MOUNT CRACKED. CRACK EMANATES FROM A WELD AND PROGRESSED TO THE OUTER EDGE OF THE MOUNT PLATE.SDR CA020215008Tail Cone · cracked(CAN) 2 INCH CRACK FOUND ON TOP SKIN OF TAIL CONE AT LOCATION OF AFT FACTORY INSTALLED VHF ANTENNA MOUNT 51.5 TO 53.5 INCHES AFT OF FORWARD TAIL CONE SKIN. CRACK APPEARS TO HAVE ORIGINATED FROM TAPERED FACTORY SHIM PN B322-1.SDR ALG2002F00010Frame · crackedROUTINE INSPECTION, UPPER SECTION OF FRAME CRACKED ABOVE RIGHT ATTACHMENT CASTING. PROBABLE CAUSE: RIGHT UPPER SHIM ON TAILBOOM (407-030-810-119) NOT BURNISHED AT EDGES.SDR CA020131002Fitting · broken(CAN) VERTICAL LOWER FIN FITTING FOUND ATTACHMENT LUG BROKEN OFF ON A PRE FLIGHT.SDR HEEA077662Structure · crackedTAIL BOOM STRUCTURE IS CRACKED.SDR HEEA077659Structure · crackedDURING POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED CRACK IN TAIL BOOM VERTICAL PYLON STRUCTURE.SDR 2002FA0000145Support · mismanufacturedTRIED TO PUT SUPPORT IN FIXTURE TO LOCATE TO TAILBOOM. RADIUS BEND IS TOO WIDE. BETER QUALITY CONTROL AT MFG.SDR 2002FA0000144Support · mismanufacturedTRIED TO PUT SUPPORT IN FIXTURE TO LOCATE TO TAILBOOM. RADIUS BEND IS TOO WIDE. BETTER QUALITY CONTROL AT MFG.SDR 2002FA0000143Support · mismanufacturedTRIED TO PUT SUPPORT IN FIXTURE TO LOCATE TO TAILBOOM. RADIUS BEND IS TOO WIDE. BETTER QUALITY CONTROL AT MFG.SDR OMNIDMR01Structure · crackedHORIZONTAL STABILIZER CRACKED ON TRAILING EDGE AND TRIM TAB CRACKED ON LEADING EDGE DUE TO EXCESS FLUTTER. CRACKING CONCENTRATED AROUND AREA OF DAMPER WEIGHTS. TABS WERE TOO LONG AND ARE SUPPORTED ONLY BY RIVETS LOCATED ON LEADING EDGE,THE DAMPER WEIGHTS ADDESDR OMNIDMR04Structure · crackedHORIZONTAL STABILIZER CRACKED ON TRAILING EDGE ABD TRAIM TAB CRACKED ON LEADING EDGE DUE TO EXCESSIVE FLUTTER. CRACKING IS CONCENTRATED AROUND AREA OF DAMPER WEIGHTS. TABS WERE TOO LONG AND ONLY SUPORTED BY RIVET ON THE LEADING EDGE, CAUSING EXCESSIVE FLUTTESDR CA020109001Flange · corroded(CAN) TAILBOOM SENT FROM A CUSTOMER IN THE USA FOR REPAIR OF A DAMAGED SKIN. DURING DISASSEMBLY THE TAILBOOM TO FUSELAGE ATTACHMENT RING FOUND CORRODED. AT THE 1:00 AND 11:00 O'CLOCK POSITION DEPTH 1 MM AT THE 2:00 AND 10:00 O'CLOCK POSITION 0.2 MM AT THE 6SDR CA020405025Bulkhead · cracked(CAN) CRACK FOUND DURING INSPECTION IN AFT LT TAIL ROTOR GEARBOX MOUNTING AREA.SDR AUS20011164Structure · cracked(AUS) TAIL BOOM CRACKED.SDR HEEA077207Cap · crackedDENTED AND CRACKED AT LEADING EDGE.SDR HEEA077036Hanger Assy · mismanufacturedWILL NOT FIT IN SUPPORT ON AIRCRAFT. HOLES MILLED IN WRONG AREA.SDR 2001FA0000542Fitting · crackedAFTER THE PILOT REPORTED UNUSUAL TAILBOOM MOVEMENT DURING HIS PREFLIGHT IHSPECTION , ONE OF OUR MECHANICS REMOVE THE TAILBOOM ATTACHMENT FAIRING. HE FOUND THE RT UPPER TAILBOOM ATTACH BOLT HAD FRACTURED , AND THE BOLT HEAD WAS HELD ONLY BY SAFETY WIRE.WE THEN SDR 2001FA0000541Angle · crackedDURING INSPECTION OF THE RT UPPER TAILBOOM MOUNT WE FOUND P/N 500N3129-6 ANGLE CRACKED. TO INSPECT, YOU MUST REMOVE THE RIVETED CLOSURE ,ON THE SIDE OF THE FUSELAGE. WE HAVE FOUND CRACKS ,ON ALL 3, OF OUR 600N MODELS.SDR 2001FA0000540Angle · crackedINSPECTED RT UPPER TAILBOOM ATTACH FITTING ON FUSELAGE . WE FOUND A CRACK IN ANGLE P/N 500N3129-6. THIS ANGLE CAN ONLY BE SEEN BY REMOVAL OF THE RIVETED PANEL ON THE SIDE OF THE FUSELAGE. WE HAVE FOUND CRACKS ON ALL 3 OF OUR 600N MODELS .SDR 2001FA0000488Bolt · brokenDURING PREFLIGHT PILOT FOUND TAILBOOM BOLT MOVED. MAINTENANCE REMOVED COVER FOUND BOLT SAFETIED, BUT BROKEN 2.5 THREADS FROM SHANK BOLT REMOVED AND REINSTALLED 265.2 HOURS BEFORE.SDR ERAA076682Structure · crackedTAILBOOM REMOVED FROM AIRCRAFT DUE TO CRACKED SKIN RT SIDE BASE OF VERTICAL FIN. FOUND RUSTED, CORRODED & PITTED TAIL SKID BRACKETS. CORRODED FWD MOUNTING FLANGES. CORROSION & PITTED SPOTS ON 90 DEGREE GEARBOX FITTING BOLT HOLES. ACTION TAKEN: INSTALLED NESDR ERAA076671Structure · crackedTAILBOOM IS CRACKED. RT SKIN CRACKED PN 105-30251-56, LT CONTOUR SKIN PN 105-30101-14 CRACKED, SPAR PN 105-30401-16-001 CRACKED, 90 DEGREE GEARBOX FITTING PN 105-30402-12 HAS CORROSION, STRINGER PN 105-30251-25 IS CRACKED, STRINGER PN 105-30251-26 IS CRACKESDR ERAA076670Structure · crackedNO. 2 BULKHEAD CRACKED ABOVE ROOF PANEL. STINGER BULKHEAD UPPER SUPPORT ANGLE CRACKED. STIFFNER P/N 212-030-099-028 CRACKED. ROOF PANEL PN 205-032-815-127 HAS CORROSION & SEPERATED. VERTICAL FIN SUPPORT BULKHEADS PN 212-030-127-029 AND 021 CRACKED. L/H LOSDR NYS2002F00000Support · crackedDURING AN ENGINE INSPECTION FOUND NR 1 HANGER BEARING SUPPORT CRACKED. INSPECTED ALL RELATED COMPONENTS AND FOUND NO DEFECTS. REMOVED BRACKET AND INSTALLED NEW.SDR CA011029016Skin · cracked(CAN) A 6 INCH LONG CRACK FOUND ON TAILBOOM FWD UPPER SKIN UNDER N5 BEARING MOUNT SUPPORT AT BOOM STA A868. TAILBOOM INST IN EUROCOPTER APPRD AS350/355 TAILBOM REPAIR FIXTURE FOR REPL OF UPPER SKIN&FOUND N5SUPPORT HAD BADLY MISALIGN TO FIXTURE: N5 BEARING MOUN
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