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 CA151214015Bracket · cracked(CAN) CRACK ON TAILBOOM FROM TAIL ROTOR GEARBOX COWLING BRACKET. CRACK STARTED FROM 1 OF THE RIVET HOLES THAT HOLDS THE BRACKET ONTO THE TAILBOOM.SDR QMLA2015102015100Mount Bracket · crackedDURING A SCHEDULED MX EVENT FOR AAIP INSPECTION, A1040 300 HOUR / 12 MONTH INSPECTION, THE HORIZONTAL STABILIZER WAS PULLED. THE INSPECTION WAS PERFORMED ON THE INTERIOR OF THE TAIL BOOM & THE MOUNTING BRACKETS FOR THE HORIZONTAL STABILIZER. THE UPPER RT MOUSDR HDNA20151014001Frame · crackedDURING SCHEDULED INSPECTIONS FOUND UPPER FRAME 9LA CRACKED. REMOVED RIVETS & 9LA UPPER FRAME PN 117-30254.12 & RIVETED NEW 9LA UPPER FRAME IAW SRM 51-70-51 4-8.SDR 2017FA0000123Fitting · crackedTHE LH UPPER AFT TAILBOOOM ATTACH FITTING WAS FOUND CRACKED DURING A PHASE VISUAL INSPECTION. THE CRACK EXTENDED OVER 75% OF THE OUTBOARD FLANGE THROUGH THE FIRST ROW OF FASTENERS. NAVAIR ENGINEERING ANALYZED THE DAMAGE AND DETERMINED THAT AT THIS CRACK LENGTSDR CA150923015Support Angle · cracked(CAN) TAILBOOM, UPPER RT SUPPORT ANGLE CRACKED.SDR QMLA2015092215086Support · crackedDURING ZONE 10 INSPECTION FOUND CRACK IN TAIL BOOM AT SUPPORT ASSEMBLY FOR HORIZONTAL STABILIZER.SDR QMLA2015092215085Tail Boom · crackedFOUND 3 CRACKS & 8 J BOLTS LOOSE ON LT SIDE OF TAIL BOOM AT HORIZONTAL FITTING DURING AN AIRWORTHINESS CHECK. THIS DAMAGE WILL REQUIRE THE TAIL BOOM BE REMOVED & SENT TO MFG FOR REPAIR. THIS ACFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION.SDR EVGR20150904Mount · crackedDURING 100 HOUR INSPECTION, THE TAIL ROTOR GUARD MOUNTING BLOCK ASSY WAS FOUND TO BE CRACKED ON 3 SIDES OF THE SMALL BOLT HOLE CONTAINING A HELICOIL INSERT.SDR QMLA2015090315084Fitting · crackedDURING A RECENT INSPECTION, THE MECHANICS FOUND THE HORIZONTAL FIN, LT FWD ATTACH MOUNT BOLT HOLE CRACKED. THE DAMAGE HAS BEEN DETERMINED TO BE REPAIRABLE ONLY BY MFG. THE TAIL BOOM HAS BEEN SHIPPED TO THEM FOR REPAIR. THIS ACFT IS CURRENTLY OUT OF SERVICE SDR PG9R2015FA0000553Structure · crackedACFT WAS IN THE PROCESS OF A DAILY PREFLIGHT, DURING THE PREFLIGHT THE PILOT FOUND A CRACK ON THE TAILBOOM. THE CRACK WAS VALIDATED, IT IS 118.6250" AFT FROM THE TAILBOOM TO AIRFRAME ATTACHMENT BULKHEAD. THE LENGTH OF THE CRACK IS 1.6250". IT ORIIGINATES UNSDR CA150811005Attach Fitting · cracked(CAN) DURING ROUTINE 100 HOUR INSPECTION, THE UPPER LT TAIL BOOM ATTACH FITTING WAS FOUND CRACKED.SDR QMLA2015080315065Stringer · crackedDURING AAIP A1660 600 HR SCHEDULED INSPECTION, IT WAS DISCOVERED THAT THE STRINGER JUST BELOW THE BATTERY DOOR OPENING, IN THE TAIL BOOM HAS A CRACK APPROX 1 INCH IN LENGTH.SDR TLLL2016FA0000009Fitting · crackedDURING SCHEDULED 100 HR INSPECTION, FOUND UPPER LT FUSELAGE, SIDE TAILBOOM MOUNT FITTING, PN 206-031-329-103 CRACKED. INSPECTION OF THIS PART IS ROUTINE IN THE CHECKLIST FOR 100 HR INSPECTION, REF BHT-206L1-MM-1, 5/19, 5-20. THIS PART APPEARED TO BE ORIGINALSDR QMLA2015072115062Skin · crackedCRACK FOUND, DURING 600 HR AIRFRAME INSPECTION, ON THE TAIL BOOM INNER SKIN AT THE AFT, LOWER CORNER OF THE RT SIDE STABILIZER OPENING, X-8610.0, Y-150.0, Z- 1847.13.SDR HDNA201507070001Frame · crackedCRACK FOUND DURING SCHEDULED INSPECTION IN TAIL CONE, ON FRAME AT STATION X6616 3 O'CLOCK POSITION, LOOKING IN TAIL CONE. REPAIR COMPLETED IAW FAA FORM 8110-3 AHI15-141 DATED 6 25 2015, HELICOPTERS REPAIR DESIGN APPROVAL SHEET RDAS-AHI15-0102 REV D DATED 6 24SDR QMLA2015063015051Frame · crackedDURING AN AIRFRAME ZONE 12 INSPECTION FOUND THE SHELF THAT THE ANTI-COLLISION LIGHT POWER SOURCE IS MOUNTED TO IS BROKEN & UPON FURTHER INSPECTION FOUND A CRACK IN UPPER FRAME 9LA.SDR CA150629011Tail Boom · cracked(CAN) CRACK FOUND AROUND RIVET ON LT SIDE OF TAIL BOOM ON HORIZONTAL STABILIZER SUPPORT STRUCTURE. CRACK IS ON REINFORCEMENT RIB FWD OF HORIZONTAL STABILIZER.SDR QMLA2015052015040Stabilizer · crackedFOUND APPROX 2.5" CRACK ON UPPER RT SIDE OF HORIZONTAL STABILIZER. APPROX 4" AFT OF THE STABILIZER MOUNT.SDR 2A6R201505193256Frame · crackedA CRACK EMANATING FROM A RIVET WAS DISCOVERED IN FRAME X3035, ITEM 43, AS DEPICTED IN SRM 53-31-01, 02. THIS FRAME IS A RING JUST FWD OF THE FISH MOUTH IN THE TAIL BOOM, THE CRACK IS AT APPROX THE 10:00 O'CLOCK POSITION IF STANDING IN THE REAR LOOKING FWD.SDR CA150519019Skin · unserviceable(CAN) AFTER A TRAINING FLIGHT, IT WAS NOTED THAT BOTH LT AND RT FIN ASSEMBLIES. VERTICAL FIN AT THE END OF HORIZONTAL STABILIZER ASSEMBLIES, PN 407-023-003-105 AND PN 407-023-003-107, WERE FOUND TO HAVE BEEN STRUCK BY MAIN ROTOR BLADES IN FLIGHT. THE ONLY DASDR EVCA20150324076Attach Fitting · crackedUPPER LT TAIL BOOM ATTACHMENT FITTING CRACKED.SDR CA150413002Skin · cracked(CAN) DURING INSPECTION. TAIL BOOM WAS FOUND CRACKED ON OUTER SKIN, AT STABILIZER ATTACHMENT POINT LT SIDE.SDR CA150324009Structure · cracked(CAN) VERTICAL FIN CRACKED. THE CRACK APPEARS TO HAVE ORIGINATED AT THE UPPER AFT ATTACH POINT. IT WAS DISCOVERED ON A DAILY INSPECTION.SDR QMLA2015031115015Frame · crackedDURING EVENING SHIFT PREFLIGHT, PILOT DISCOVERED A NOTICEABLE CRACK ON THE RT SIDE OF TAIL BOOM RING FRAME. REMOVED PAINT & INSPECTED AFFECTED AREA WITH DYE PENETRATE WHICH PRESENTED THE CRACK IN THE SUSPECTED AREA.SDR QMLA201503111502Stringer · gougedDURING PREFLIGHT OF ACFT, PILOT OPENED TAIL BOOM BATTERY COMPARTMENT DOOR TO EXAMINE CONTENTS. PILOT NOTICED A SMALL GAP BETWEEN THE TWO HALVES OF THE CLOSE OUT PLATES FWD OF THE BATTERY THAT ARE VELCRO'D TO THE BULKHEAD RING. EXAMINED MORE CLOSELY & NOTICEDSDR QMLA2015022315011Doubler · crackedDURING INSPECTION FOR CRACKS IAW AD 2014-12-51, A CRACK WAS FOUND IN THE LOWER RT DOUBLER PLATE FOR THE HORIZONTAL STABILIZER ON THE INTERIOR OF THE TAIL BOOM. THE INSPECTION OF THIS AREA DOES NOT FALL WITHIN THE SCOPE OF THE APPLICABLE AD. THE CRACK IS APPRSDR 3D9A201502200004Doubler · crackedDURING DAILY PREFLIGHT CHECK, FOUND A 55 MM CRACK ON LEFT HAND TAIL BOOM TO VERTICAL FIN DOUBLER.SDR HDNA201502190005Spar · crackedCRACK IN TAIL BOOM VERTICAL STABILIZER FIN SPAR PROPAGATING FROM A LIGHTING HOLE.SDR 2015FA0000004Barrel Nut · cracked1 OF 4 BARREL NUTS THAT ATTACH THE TAILBOOM TO THE AIRFRAME WAS FOUND TO BE CRACKED ACROSS THE THREADS ON 2 SIDES. THE NUT HAD BEEN REMOVED AS PART OF A MAJOR INSPECTION.SDR QMLA2014122614142Frame · crackedDURING INSPECTION OF TAIL BOOM FOUND CRACKS ON UPPER & LOWER FRAME 9LA & 7L. UPPER FRAME 9LA IS CRACKED AT RBL 200 & WL 3000, CRACK IS APPROX .25 INCHES. LOWER FRAME 9LA IS CRACKED AT RBL 200, LBL 200 & WL 3000, BOTH CRACKS ARE APPROX .5 INCHES. FRAME 7L ISSDR 9EKA02162015001Skin · debondedTAIL BOOM, EMPENNAGE METALLIC SKIN, HONEYCOMB STRUCTURE ON RT SIDE JUST AFT OF THE FWD VOR ANTENNA MOUNT WL 74, BS 294 HAS DISBONDED. INSPECTION WAS PERFORMED IAW BHT ALL SRM 2-13. TAIL BOOM IS BEING REPLACED WITH REPAIRED SERVICE TAIL BOOM. DAMAGED TAIL BOSDR CA141208014Angle · cracked(CAN) INSPECTION BEING CARRIED OUT IAW EASB: 05.00.70 CRACKS WERE NOTED RADIATING FROM THE NR 7 BOLT HOLE IN REINFORCEMENT BRACKET. ANGLE TO BE REPLACED.SDR 3D9A2014120600001Skin · cracked0.75 INCH CRACK ON FUSELAGE TAIL CONE SKIN UNDER TOP RIVET OF AFT UPPER ECU MOUNT DISCOVERED DURING 6000 HOUR/6 YEAR INSPECTION.SDR EVCA2014111700073Attach Fitting · crackedDURING ROUTINE MAINTENANCE THE INSPECTION REVEALED A CRACKED ON THE UPPER LT TAIL BOOM ATTACHMENT FITTING PN 206-032-409-001.SDR E3MA20141110001Fitting · crackedDURING A PERIODICAL INSPECTION A CRACK WAS FOUND IN THE 10L FITTING OF THE TAIL BOOM. THIS TAIL BOOM HAD SB-117-C-2-53-007 REINFORCEMENT KIT INSTALLED. THIS TAIL BOOM WAS ALSO REPAIRED 852.1 FH AGO FOR INCORRECT RIVETS INSTALLED IN THE TOP SKIN OF THE BOOM.SDR QMLA201410095232Structure · damagedTHE TAIL ROTOR GEAR BOX & THE VERTICAL STABILIZER BOLT MOUNTING POINTS ON TOP OF THE TAIL BOOM ARE DAMAGED & NEED REPAIR. FOUND THAT THE WINDINGS INSIDE THE BOLT HOLES AT THE MOUNTING POINTS HAD BEEN PARTIALLY GROOVED INTO BY THE BOLTS. THE STATION IS AT 380SDR CA140930008Skid · broken(CAN) SKID ASSEMBLY, STINGER, NOTED AS LOOSE ON ACFT DAILY INSPECTION. FURTHER INSPECTION FOUND IT BROKEN AT SINGLE ATTACHMENT POINT. EVIDENCE OF FRETTING AND CORROSION. THIS IS THE 2ND RECENT FAILURE OF THIS PART ON THIS ACFT TYPE. RESTRICTED TO THIS MFG SDR QMLA2014092414114Stabilizer · crackedWHILE PERFORMING AN AIRWORTHINESS CHECK, A CRACK WAS FOUND ON THE UPPER SURFACE OF THE HORIZONTAL STABILIZER ON THE LT SIDE. THE CRACK BEGAN IN THE RIVET LINE OF THE METAL LAP ATTACHMENT POINT ALONG THE TAIL BOOM AT APPROX 3 INCHES FROM THE TE & CURVED FORWARSDR K97A2014F00157Skin · crackedWHEN THE LEFT HORIZONTAL STABILIZER WAS REMOVED FOR ELECTRICAL TROUBLESHOOTING, 7 CRACKS IN THE SHEET METAL WERE FOUND ON THE INBD RIB AND FORE AND AFT SPARS WHERE THEY ATTACH TO THE INBD RIB. CRACKS CANNOT BE SEEN WITH THE STABILIZER INSTALLED. A TORQUE TUBSDR EVCA2014092200071Attach Bracket · crackedMECHANIC FOUND CRACKED UPPER ATTACHMENT BRACKET PN 206-023-119-063 FOR LT FINLET.SDR QMLA2014090414106Cap · crackedPILOT REPORTED OIL RESIDUE ON TAIL ROTOR GEARBOX & SCRATCH ON LEADING SIDE NEAR LT BOLT AFTER FLIGHT. AFTER FURTHER INSPECTION WITH TAIL ROTOR GEARBOX REMOVED, FOUND 1/2 INCH CRACK IN TAIL STRUCTURE AIRFRAME TOP CAP.SDR EVCA2014082900070Attach Fitting · crackedDURING ROUTINE INSPECTION FOUND TAIL BOOM ATTACHMENT FITTING PN 206-032-409-001 CRACKED.SDR EVCA2014082500069Attach Fitting · crackedDURING ROUTINE INSPECTION FOUND TAIL BOOM ATTACHMENT FITTING PN 206-032-409-001 CRACKED.SDR CA140826026Rib · cracked(CAN) WHEN CARRYING OUT A 300 HR INSPECTION ON THE ACFT, A CRACK WAS FOUND ON THE LT STABILIZER ATTACHMENT FITTING OF THE INBD RIB. THERE WERE NO DEFECTS FOUND ON THE ADJACENT TAILBOOM AREA. THIS ATTACHMENT FITTING ALLOWS FOR FASTENING THE STABILIZER TO THE SDR EVCA2014073000066Attach Fitting · crackedDURING ROUTINE INSPECTION FOUND THE UPPER LT TAIL BOOM ATTACHMENT FITTING CRACKED.SDR CA140708005Doubler · cracked(CAN) CRACK WAS DISCOVERED DURING DAILY INSPECTION. THE CRACK WAS LOCATED IN THE TAIL BOOM DOUBLER BELOW THE 42" GEAR BOX WHERE IT IS NOTCHED TO ACCOMMODATE THE VERTICAL FIN SPAR. IT WAS APPROXIMATELY 1" IN LENGTH.SDR CA140702016Skin · cracked(CAN) DURING MAINTENANCE VISIT, EDDY CURRENT INSPECTION AT STA 9900 TAILBOOM FITTINGS OF EASA REGISTERED ACFT, IT WAS DISCOVERED THAT CRACKS PROPOGATED FROM 3 OF THE 4 FITTINGS ON THE TAILBOOM. UPPER RT AND LT TAILBOOM ATTACH FITTINGS AND RT LOWER ATTACH FITTISDR QMLA2014062514078Skin · crackedCRACK FOUND ON INNER SKIN LOCATED IN THE BATTERY COMPARTMENT UPPER LT CORNER FWD OF RING FRAME NR 6.SDR 9EKA20140624007Angle · crackedCRACKS FOUND IN TAIL BOOM PYLON RIB AREA 455 & FAILURE OF THE CONNECTING ANGLE BETWEEN RT SIDE SKIN & TRANSMISSION DECK.SDR IGAL2014FA0000404Support Bracket · defectiveDURING SCHEDULED 100 HOUR INSPECTION AND COMPIANCE WITH ASB206-12-129, REV C DATED 09 JUNE 2014 FOR INSPECTION ONLY, WHICH IS DIRECTLY APPLICABLE TO THE PART THAT WAS FOUND DEFECTIVE, THE SUPPORT BRACKET WAS FOUND BOTH CRACKED AND BROKEN. MFG WAS NOTIFIED AT
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