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 PG92011F00000Skin · crackedON 3-14-11 DURING A PREFLIGHT INSP BY PILOT, A CRACK WAS DISCOVERED IN THE TAILBOOM SKIN ON THE RT SIDE WHERE THE HORIZ STABILIZER MOUNTS AFT LOWER CORNER. THE CRACK ORIGINATES THERE AND CONTINUES UNDER A SPAR (OVER 1 IN LONG). MFG HAS BEEN CONTACTED AND ALRSDR CA110329002Guard · cracked(CAN) TAIL ROTOR GUARD FOUND CRACKED AT UPPER MID ATTACHMENT POINT DURING GROUND HANDLING. GUARD REPLACED WITH SERVICEABLE PART.SDR 2011FA0000201Skin · crackedDURING THE QC FINAL INSP PHASE OF A 100 HR INSP THE INSPECTOR NOTED A CRACK EXTENDING LONGITUDINALLY FWD AND AFT FROM THE LT FWD NAV/VOR ANTENNA MOUNT. PHOTO`S AND INFOR SENT TO MFG FOR DETERMINATION. MFG SUGGEST REMOVAL AND REPAIR BY MFG. BELIEVE PART TO BSDR UOHR2011009Spar · crackedDURING MAJOR INSPECTIONS A CRACK WAS DISCOVERED ON THE TAILBOOM AT THE 10L FRAME ON THE SUPPORT ANGLE (PN 105-30251.44) SPLICE DOUBLER. THERE IS ALSO A CRACK IN THE VERTICAL FIN SPAR AT THE CAM LOC FASTENER. A TRAY IN THE VERTICAL FIN IS ALSO CRACKED AT THE SDR ALGAR2241151374Attach Fitting · crackedUPPER LEFT HAND INTERCOSTAL FITTING CRACKED ON FWD. LEFT HAND SIDE OF FITTING.SDR AC2R9JP02222011Fitting · crackedDURING ROUTINE 50 HR INSP, FOUND THE SUPPORT FITTING WHERE THE INTERMEDIATE GEARBOX ATTACHES TO THE TAILBOOM WAS CRACKED. REMAINING ACFT IN OUR FLEET WERE INSPECTED AND NO OTHER DESCREPANCIES WERE FOUND.SDR CA110221006Skin · cut(CAN) DURING ANNUAL INSPECTION, THE AFT DECK SKIN, PN 11115-1,WAS FOUND TO BE CHAFED THROUGH BY BEING IN CONTACT WITH THE VERICAL STABILIZER ASSY, PN 30501-1. THE CHAFED THROUGH CUT WAS APPROXIMATLY 15" IN LENGTH. THE VERTICAL FIN ASSY WAS TRIMMED TO ALLOW CSDR RMXA20110218001Skin · crackedFOUND CRACK ON UPPER RIGHT SKIN OF HORIZONTAL STABILIZER DURING INSPECTION. HORIZONTAL STABILIZER WILL BE REPLACED/REPAIRED.SDR KBMA2011030801Mount · crackedCRACK IN VERTICAL FIN MOUNT.SDR CA110214014Attach Fitting · cracked(CAN) CAP SECTION UNDER UPPER LEFT HAND TAIL BOOM ATTACHMENT FITTING FOUND CRACKED VERTICALLY TO EDGE ON DAILY INSPECTION. AIRCRAFT REMOVED FROM SERVICE. TAIL BOOM REMOVED FOR CAP REPLACEMENT.SDR QMLA2011020811022Plate · crackedRT VERTICAL END PLATE CRACKED AT KNOCK OUT PORTION OF THE STABALIZER.SDR EOPA020211397ALFrame · crackedFRAME WAS FOUND CRACKED AT APPROX STA 78 IN TAILBOOM ABOVE BAGGAGE COMPARTMENT.SDR CA110211006Washer · damagedWHEN REMOVING THE NUT AND SPLINED WASHER USED TO SECURE THE TAIL ROTOR PITCH BEAM DURING SCHEDULED REPLACEMENT OF THE TAIL ROTOR PITCH CHANGE SHAFT, THE MASTER SPLINED WASHER WAS FOUND DISPLACED (ONCE THE NUT WAS REMOVED) THIS CANNOT BE READILY SEEN ONCE THE NSDR CA110206002Stiffener · crackedSTIFFENER, IN BASE OF FIN FOUND CRACKED ALONG FLANGE AGAINST SKIN.SDR EOPA012811397ALBulkhead · crackedFOUND .5 IN CRACK IN BULKHEAD ASSY LOCATED AT APPROX STA 185 IN TAILBOOM. CRACK WAS IN THE CTR RT PORTION OF THE FRAME.SDR ALGAR1281151434Hanger Assy · mismanufactured3EA HANGER SUPPORTS PN 206-033-412-123S, RADIUS OUTER EDGES RECEIVED NEW FROM MFG DEFORMED AND WILL NOT FIT IN FIXTURE.SDR QMLA2011011911011Frame · crackedTHE MECHANIC WAS INSPECTING IN THE TAILBOOM WHEN A CRACK WAS FOUND AT FRAME 10L ON THE RT SIDE OMEGA TUBE CUTOUT APPROX 14MM IN LENGTH. THE ACFT IS CURRENTLY AWAITING AN APPROVED REPAIR SCHEME.SDR M7KA201101104770Structure · crackedDURING ROUTINE PERIODIC INSPECTION A VISIBLE CRACK IN THE PAINT AROUND A COUNTERSUNK RIVET ON THE TAIL BOOM CONE TO FENESTRON RING JUNCTION WAS NOTED. FOLLOWING THE STRIPPING OF THE PAINT AND THE COMPLETION OF A DYE PENETRANT INSPECTION IT WAS DETERMINED THATSDR QMLRMD7083Structure · damagedVERTICAL STABILIZER HAD A CREASE THAT WAS BEYOND MFG LIMITS.SDR ALGA102910888259Cap · crackedUPPER L/E CAP PN 206-020-113-173 OF VERTICAL FIN CRACKED.SDR CA101105004Skin · damaged(CAN) VOIDS EXCEEDING ALLOWABLE LIMITS WERE DISCOVERED IN TAILBOOM UPPER SKIN RADIUS DURING DESTRUCTIVE TEST INSPECTION.SDR QMLDMR0254Skin · crackedCRACK IN TAIL BOOM SKIN AND DOUBLER AT RT TAIL ROTOR FLOOD LIGHT. TAIL ROTOR FLOOD LIGHTS WERE INSTALLED ON FAA FORM 337, DATED 6 APRIL 1988.SDR QMLDMR0253Bulkhead · crackedTAILBOOM BULKHEAD AT BOOM STA 164.23 CRACKED AT LOWER RT STR, LOWER RT LONGERON (2), LOWER LT LONGERON (2)AND UPPER LT LONGERON.SDR QMLDMR0252Rib · crackedTAILBOOM RIB AT BOOM STA 138 CRACKED 1.05" AT TOP.SDR QMLDMR0251Bulkhead · crackedTAILBOOM BULKHEAD AT BOOM STA 122.33 CRACKED AT INTERSECTIONS OF RT STRINGERS (2) AND LT LOWER LONGERON.SDR 2010FA0000922Skin · delaminatedWHILE CONDUCTING A POST FLIGHT INSP, THE FLIGHT CREW NOTICED THAT THE TAILBOOM HAD AN AREA THAT WAS DELAMINATED ON THE RT SIDE OF THE TAILBOOM. THIS IS IN THE SAME CRITICAL AREA THAT HAS BEEN ADDRESSED BY AD 2009-19-51. IN ADDITION TO THE DELAMINATED AREA, THESDR R29R2010001Support · crackedDURING A 300 HR, PART B INSP, IT WAS DISCOVERED THAT THE SUPPORTS (PN205-030-889-015) WERE FOUND CRACKED. 2 OTHER ACFT IN THE FLEET WERE CHECKED AND FOUND TO HAVE WORKING RIVETS IN THE SAME LOCATION. THIS CAUSES PLAY IN THE ELEVATORS AND IF LEFT UNDETECTED, CSDR 2010FA0000841Support · crackedDURING A 300 HOUR, PART B INSP, IT WAS DISCOVERED THAT THE SUPPORTS (PN - 205-030-889-015) WERE FOUND CRACKED. 2 OTHER ACFT IN THE FLEET WERE CHECKED AND FOUND TO HAVE WORKING RIVETS IN THE SAME LOCATION. THIS CAUSES PLAY IN THE ELEVATORS AND IF LEFT UNDETECTSDR RMXA072820107103Skin · crackedDURING MX A 1" LONG CRACK WAS DISCOVERED IN THE TAILBOOM VERTICAL FIN OUTER SKIN STARTING FROM AN ACCESS OPENING AT THE UPPER END OF THE VERTICAL FIN. REPAIR SCHEME REQUEST WAS SUBMITTED FROM THE MFG.SDR YTRA1020302Attach Fitting · crackedDURING ROUTINE INSP FOUND UPPER LT TAILBOOM ATTACH FITTING CRACKED. REMOVED CRACKED TAILBOOM ATTACH FITTING AND INSTALLED NEW FITTING.SDR QMLA2010070610030Fairing · cracked30 MM CRACK AT THE OUTER CIRCUMFERENCE (ADJACENT TO ONE OF THE ATTACH SCREWS) ON FAIRING ASSY PN L642A2028102. THE CRACK EXTENDS TOWARD THE CTR OF THE FAIRING ASSY. THE CRACK WAS DISCOVERED DURING A WALK AROUND OF THE ACFT.SDR YTRA1020301Attach Fitting · crackedDURING ROUTINE INSP, FOUND UPPER LT TAILBOOM ATTACH FITTING CRACKED. REMOVED CRACKED TAILBOOM ATTACH FITTING AND INSTALLED NEW FITTING.SDR QMLA20100623Spar · crackedFOUND CRACK IN FWD FIN SPAR LEG APPX .3125" LONG AT RT AFT CAMLOCK RECEPTACLE FOR TAILROTOR DRIVESHAFT TRANSITION COVER. CRACK EXTENDS FROM AFT EDGE OF HOLE & RELIEVED ITSELF AT THE EDGE OF PANEL.SDR QMLDMG1345Spar · chafedWHILE INSPECTING THE AIRFRAME FOUND THE MAIN SPAR OF THE TAIL BOOM CHAFED BY THE VERTICAL TAIL FAIRING. HAD TO SEND THE TAIL BOOM FOR REPAIR.SDR CA100820004Bolt · loose(CAN) DURING A SCHEDULED INSPECTION, THIS BOLT (IPC PAGE 2-4 ,FIGURE 2-5, ITEM NR 15) WAS FOUND LOOSE. THIS IS THE THIRD AIRCRAFT IN THE FLEET ON WHICH THIS BOLT WAS FOUND LOOSE, ALL AIRCRAFT WERE UNDER 1000HRS TSN. IT IS VERY NOTICEABLE WHEN WIGGLING THE TAISDR ALGA52510557Angle · crackedUPON MAJOR INSPECTION OF AFT SPAR AREA, FOUND CRACK IN AFT EDGE OF SPAR THROUGH HIGH LOC HOLE, .500 IN. LONG AT WL 111, STA. 103.4.SDR EVCA00005Fitting · crackedUPPER LT ATTACHMENT FITTING FOUND CRACKED DURING INSPECTION OF TAILBOOM. UPPER LT ATTACHMENT FITTING IAW ASB 206L-09-158. UPPER LT ATTACHMENT FITTING R & R.SDR QMLR MD270 3Frame · crackedFRAME X6166 HAS NUMEROUS CRACKS.SDR QMLRMD2702Spar · crackedAFT SPAR CRACKED AT A CAMLOC FASTENER.SDR QMLR MD270 1Support Angle · crackedSUPPORT ANGLE CRACKED AT TOP OF 10L FRAME.SDR QMLR MD270Stringer · crackedFRAME 2L CRACKED AT STRINGER CUTOUT.SDR 2010FA0000443Strut · broken(OG5S) DURING UNSCHEDULED MX THE LOWER DRIVE SUPPORT STRUT WAS FOUND TO BE CRACKED 90 PERCENT THROUGH THE TUBE WHERE THE UPPER ATTACH LUG IS WELDED. UPON REMOVAL THE LUG COMPLETELY SEPARATED FROM THE TUBE. IF TUBE HAD SEPARATED DURING FLIGHT LOSS OF MAIN ROTOSDR QMLA2010042710010Frame · crackedNUMEROUS CRACKS IN TAILBOOM STRUCTURE REQUIING ENGINEERED REPAIR. PN 117-22122-15 FRAME 2L CRACKED AT OMEGA STRINGER CUTOUT. PN 105-30251-44 SUPPORT ANGLE CRACKED AT THE TOP OF THE 10L FRAME. PN 105-304061 AFT SPAR CRACKED AT A CAMLOC FASTENER. PN 117-22122-51SDR CA100427006Skin · cracked(CAN) DURING A SERVICEABILITY CHECK, A 3/8 INCH LONG CRACK WAS NOTICED ON THE RT SIDE OF THE TAILBOOM (STA 6000, WL 2500).SDR S9H2010F00000Structure · crackedDURING ROUTINE 100 HR INSPECTION OF TAIL ROTOR DRIVE SHAFT BEARINGS, FOUND CRACK IN THE UPPER VERTICAL STABILIZER. REPLACED VERTICAL STABILIZER WITH SERVICEABLE UNIT.SDR ALGA033110535ALFrame · crackedDURING DAILY SERVICE CHECK/ AD COMPLIANCE, MX FOUND FINESTRON ATTACH RING FRAME CRACKED. TAILBOOM REPLACED.SDR EVCA00001Skin · crackedDURING A ROUTINE INSPECTION, MECHANIC FOUND CRACK ORIGINATING FROM A NUTPLATE ON THE AFT SKIN OF THE TAILBOOM (T/R GEARBOX LOWER CLOSE OUT SKIN). AFT SKIN REMOVED AND REPLACED.SDR QMLA2010F00116Frame · cracked3 SPIDER CRACKS FOUND STARTING AT A RIVET HOLE UNDER TAIL COWLING BRACKET ON 11L FRAME.SDR RMXA020420107013Rib · crackedDURING A DAILY INSP, A CRACK WAS DISCOVERED ON THE UPPER TAILBOOM VERTICAL FIN NOSE RIB PN 105-30402.18. THE CRACK WAS APPROX. 1.5 -2" IN LENGTH. THE NOSE RIB WAS DRILLED OFF TO INSPECT THE TAIL ROTOR GEARBOX MOUNTING CASTING LOCATED UNDERNEATH THIS NOSE RIBSDR HEEA127223Frame · crackedCRACKS FOUND IN LOWER FLANGE OF FRAME BETWEN LOWER LT AND RT TAILBOOM ATTACH FITTINGS/INTERCOSTALS. CRACKS EXIST BETWEEN CONSECUTIVE RIVETS AT APPROX THE 5 O`CLOCK AND SEVEN O`CLOCK POSITION. THE FLANGE OF THE CRACKED FRAME APPEARS TO HAVE MILLING MARKS AROU
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