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 QMLA20171107125Skin · crackedDURING A PREFLIGHT, THE TAILBOOM WAS FOUND TO HAVE A CRACK APPROXIMATELY 128MM LONG ON THE RIGHT SIDE.SDR QMLA2017110717125Tail Boom · crackedDURING A PREFLIGHT/ AIRWORTHINESS THE AFT FUSELAGE(TAILBOOM) WAS FOUND TO HAVE A CRACK APPROXIMATELY 128MM LONG ON THE RIGHT HAND SIDE. THE CRACK WAS JUST FORWARD OF THE HORIZONTAL STABILIZER. THE CRACK RUNS VERTICALLY.SDR 2017F00164Attach Fitting · crackedDURING SCHEDULED AIR FRAME INSPECTION, DISCOVERED A CRACK IN THE UPPER LEFT HAND TAIL BOOM ATTACH FITTING. (AIR-FRAME SIDE OF TAIL BOOM.) PERFORMED DYE PENETRATE TEST THAT CONFIRMED CRACK LOCATION BETWEEN THE TWO AFT OUTBOARD RIVET LOCATIONS.SDR EVCA2017091400001Bulkhead · crackedDURING INSPECTION OF TAILBOOM ATTACHMENT FITTINGS IAW AD 2013-25-10 IT WAS NOTED THAT TAILBOOM RING WAS CRACKED. CRACK MEASURED APPROXIMATELY 3.2 INCHES LONG AND EXTENDS THROUGH BOTH FLANGES OF TAILBOOM RING.SDR EVCA201707180001Attach Fitting · crackedFOUND LT TAILBOOM ATTACHMENT FITTING PN: 206-031-403-005 TO HAVE A 1.6" LONG CRACK. FITTING LOCATED ON TAILBOOM SIDE OF BULKHEAD.SDR EVCA201707061Attach Fitting · crackedUPPER LT ATTACH FITTING ON THE TAILBOOM WAS FOUND TO BE CRACKED THROUGH THE RIVETS AT THE FORWARD END. CRACK MEASURES 1.34 INCHES.SDR QMLA2017070317064Skin · deformedA 1.5 INCH LONG BLUNT SCRATCH WITH SKIN DEFORMATION WAS FOUND ON THE LT SIDE OF THE TAILBOOM AT STATION 9100, RBL 75, Z 1720. DURING PILOT PREFLIGHT CHECK. IAW AMM 53-31-00, 8-1 F NO DEFORMATION WILL BE ACCEPTED ON THE LT SIDE OF THE TAIL BOOM SKIN. OPENSDR EVCA201706151Fitting · crackedUPPER LEFT FITTING ON TAILBOOM HAS CRACK LENGTH OF 2 INCHES.SDR I7LA201705110103Attach Fitting · crackedDURING A 1200 HOUR INSPECTION, A CRACK WAS FOUND IN THE LOWER LT TAIL BOOM ATTACH FITTING. AFTER REMOVING THE TAIL BOOM, FOUND A CRACK IN THE BULKHEAD & FRAME ASSEMBLY.SDR QMLA2017031317028Doubler · crackedON TAIL ROTOR GEARBOX, 2 CRACKS WERE FOUND ON TAIL BOOM END FRAME DOUBLERS LEFT AND RIGHT, ONE CRACK EACH SIDE.SDR QMLA2017030817025Rib · crackedDURING INSPECTION, FOUND MISSING RIVET ON VERTICAL STABILIZER, DURING FURTHER INSPECTION OF VERTICAL, WAS ABLE TO POP RIVET HEADS OFF OF 4 MORE OF THE REMAINING RIVETS BY HAND ON THE UPPER VERTICAL FORWARD LOWER RIB, THEN FOUND LEFT SIDE OF RIB WAS CRACKED THRSDR JYDR20170306065Bolt · brokenDURING POST FLIGHT, MECHANIC FOUND A DING IN THE LEADING EDGE OF 1 TAIL ROTOR BLADE. FURTHER INSPECTION REVEALED A BROKEN STABILIZER BOLT HEAD. TRB WAS REPLACED. AIRCRAFT MANUFACTURE WAS CONTACTED FOR AN DER APPROVED REPAIR. AFTER AUTHORIZED REPAIR WAS PERFORSDR QMLA2017022717022Frame · crackedFOUND A .780 INCH CRACK FOUND IN THE UPPER FRAME DURING INSPECTION OF TAIL BOOM AFTER REMOVAL OF HORIZONTAL STABILIZER. REPLACED THE UPPER AND LOWER FRAMES.SDR QMLA2017022217021Splice · crackedCRACK FOUND IN SPLICE WHILE PERFORMING SCHEDULED MAINTENANCE ON AIRCRAFT. NO EVIDENCE OF ANY NICKS OR DAMAGE THAT MIGHT HAVE CAUSED CRACK. SUSPECT CRACK WAS CAUSED BY FATIGUE.SDR M7FR170101Structure · corrodedDURING PERIODICAL INSPECTION, IT WAS DISCOVERED THAT THE HORIZONTAL STABILIZER HAD SOME AREAS OF SUSPECTED SEVERE CORROSION. THE STABILIZER WAS REMOVED AND SENT FOR FURTHER EXAMINATION. IT WAS DETERMINED THAT THERE WERE MANY AREAS OF SEVERE CORROSION. IT WAS DSDR ULXR201701300001Bracket · brokenNUMBER 5 HANGER BEARING BRACKET FAILED. WAS FOUND DURING 100 HOUR INSPECTION.SDR QMLA2017011117009Doubler · crackedDURING DAILY AIRWORTHINESS CHECK, AN APPROXIMATELY 1/2" CRACK WAS FOUND ON THE RIGHT HAND TAILROTOR GEARBOX MOUNT BULKHEAD DOUBLER PN 109-0373-21-104. CRACK IS LOCATED IN THE RADIUS BEND OF DOUBLER TOWARDS UPPER RIGHT HAND EDGE BEHIND NUTPLATE.SDR QMLA2017011117008Frame · crackedTWO CRACKS FOUND ON FRAME DURING INSPECTION AT STATION 6616 APPROX. 2 O'CLOCK POSITION. RECOMMENDED RE-ENFORCEMENT TO AREA IAW SB 53-004 .SDR QMLA2017010917007Bracket · crackedCRACKS FOUND ON THE LT BRACKET AFT PORTION OF THE VERTICAL FIN BETWEEN NUT PLATES WHERE THE CAP MOUNTS ONTO.SDR QMLA2017010517004Frame · crackedAPPROXIMATELY 20MM (.78") CRACK FOUND IN 9LA UPPER FRAME STRUCTURE PN B535M2093202 NEAR BOTTOM RIVET ON RIGHT SIDE DURING INSPECTION OF TAIL BOOM AFTER REMOVAL OF HORIZONTAL STABILIZER. WAS ADVISED BY TECH REP TO ACCOMPLISH SERVICE BULLETIN 53-011 REQUIRING RESDR ALGA201612200009Hanger Assy · crackedDURING ROUTINE INSPECTION NUMBER 1 TAIL ROTOR DRIVESHAFT HANGAR BEARING MOUNT WAS FOUND TO BE CRACKED ON INSIDE OF TAILBOOM, LEFT SIDE. OPENSDR EVCA201612071Bulkhead · crackedTAIL BOOM RING/BULKHEAD ASSY PN: 206-032-400-027 HAS APPROXIMATELY ONE 1/2 - 3/4 INCH CRACK AROUND THE UPPER LEFT SIDE OF THE UPPER LEFT INTERCOSTAL/MOUNT POINT.SDR EVCA201611181Fitting · crackedUPPER LEFT TAILBOOM FITTING ON THE TAILBOOM SIDE OF THE BULKHEAD IS CRACKED FROM EDGE TO EDGE OF THE FITTING.SDR 3D9A2016110300008Angle · brokenAFT RIGHT TAIL ROTOR DRIVE SHAFT FAIRING MOUNT ANGLE BROKEN OFF ALLOWING IT TO CONTACT AND CHAFE TAIL BOOM SKIN.SDR QMLA2016110216121Arm · cracked#1 STATOR ARM CRACKED AT LH UPPER CORNER. THIS AIRCRAFT REMAINS OOS AT THE TIME OF THIS SUBMISSION.SDR ALGA201611010001Support · crackedCRACK WAS NOTED LOCATED ON TAIL BOOM NEXT TO TRDS BEARING SUPPORT ON L/H SIDE. CRACK IS APPROX 5IN LONG. DEBONDING WAS FOUND ON R/H SIDE OF TAILBOOM IN SAME AREA.SDR ALGA102020164055Skin · damagedDURING DAILY SERVICE CHECK, THE TECHNICIAN FOUND A BULLET HOLE IN DRIVESHAFT COWLING. THE COWLING WAS REMOVED AND REPLACED,NO FURTHER DAMAGE WAS NOTED.SDR ALGA102120169Y003Tail Boom · corrodedCORROSION WAS FOUND AT BS 9499.5 , BL 121.0 MAJOR REPAIR PERFORMEDSDR ALGA102120169Y002Skin · corrodedCORROSION WAS FOUND ON THE RIGHT SIDE OF TAILBOOM AT BS 11750, WL 2470. MAJOR REPAIR PERFORMED.SDR QMLA2016092116107Frame · crackedDURING AIRFRAME ZONE 6 INSPECTION, A SMALL CRACK WAS DISCOVERED IN THE TAILBOOM AFT FRAME. CRACK IS LOCATED ON THE RIGHT SIDE AT THE SMALL LIGHTENING HOLE AND IS APPROX 1/4 INCH IN LENGTH PROPAGATING HORIZONTALLY THROUGH THE LIGHTENING HOLESDR EVCA201608061Attach Fitting · crackedUPPER LT TAILBOOM ATTACHMENT FITTING, PN: 206-032-409-001P, CRACKED.SDR QMLA2016080116088Skin · buckledFOUND SKIN BUCKLED AND DENTED JUST AFT OF TAIL BOOM JUNCTION FRAME.SDR HDNA201607240001Spar · crackedDURING INSPECTION, FOUND A 3 INCH CRACK ON VERTICAL FIN SPAR PROPAGATING FROM LIGHTNING HOLE. REPAIRED IAW RDAS-AHI16_0246, REV IR, REPAIR SHEET AHI2016-0115, REV IR, AND 8110-3 AHI16-146.SDR QMLA2016070516072Doubler · crackedDURING AIRWORTHINESS CHECK, FOUND CRACK IN BATTERY COMPARTMENT DOOR FRAME, UPPER AFT RADIUS ON L/H SIDE OF TAILBOOM. REMOVED PAINT AND CONFIRMED SUSPICION ON CRACK THROUGH DOUBLER AS WELL AS SKIN UNDERNEATH AS SEEN FROM INSIDE THE TB WITH MIRROR.SDR ALGA201607071234Attach Bracket · crackedDURING ROUTINE MAINTENANCE LOWER ATTACHMENT BRACKET FOR HORIZONTAL STABILIZER WAS FOUND TO BE CRACKED AT LOWER SECTION, OTBD OF
HI-LOCK.SDR YEWA201606240001Fitting · crackedPERFORMED ASB206L-09-158B UPPER LT TAILBOOM FITTING INSPECTION. FOUND UPPER LT TAILBOOM FITTING, PN 206-032-409-001 CRACKED. R & R FITTING WITH NEW.SDR 2016FA0000227Structure · corrodedFOUND CORROSION ON UNDERSIDE OF TAILBOOM AT BS 334.0 THRU BS 334.03.SDR QMLA2016041216039Skin · crackedDURING ROUTINE MX, THERE WAS A CRACK DISCOVERED ON THE HORIZONTAL STABILIZER. IT IS ON THE TE OF THE RT SIDE OF THE STABILIZER. THAT SECTION OF THE STABILIZER IS A SINGLE SKIN WITH NO DOUBLED OR BACKUP SUPPORT.SDR QMLA2016032216027Skin · crackedAT SHIFT CHANGE, DURING PRE-FLIGHT OF ACFT NOTED A CRACK IN SKIN ON RT SIDE OF VERTICAL FIN IN THE SHAPE OF A BACKWARD C OF ABOUT 5 INCHES, AFTER MEASUREMENT POSSIBLY THROUGH 2 RIVET LOCATIONS.SDR 9EKA20160318004Skin · crackedSTRUCTURAL CRACK FOUND ON INTERNAL STIFFENER, IN THE VERTICAL TAIL PYLON FROM PREVIOUS REPAIR FAILURE. 3 INCH CRACK CONNECTING 3 RIVETS ON THE SKIN UNDERNEATH AN EXISTING REPAIR. ON THE INSIDE OF THE SKIN THE FACTORY BELL STIFFENER 212-030-099-028, CRACKED FSDR HDNA201603250091Frame · crackedFOUND A CRACK AT RING FRAME X9227, DURING MAINTENANCE.SDR HDNA2016F00083Frame · crackedFOUND A CRACK ON TAIL BOOM RING FRAME X9227.SDR HDNA2016031600003Skin · crackedTOP SKIN, PN 105-30251.57, OF TAIL BOOM, FOUND CRACKED DURING INSPECTION. CRACK IS LOCATED ON LT SIDE TOP SKIN, RT BEFORE THE VERTICAL FIN TRANSITION ON THE TAIL BOOM. REPLACED TAIL BOOM WITH SERVICEABLE.SDR QMLA2016022916012Stringer · crackedDURING 600HR INSPECTION, THREE CRACKS FOUND AROUND TAIL BOOM BATTERY DOOR OPENING. TWO ON THE STRINGER RUNNING FORE & AFT ON THE BOTTOM OF THE DOOR OPENING & THE LARGEST OF THE THREE ON THE UPPER AFT CORNER OF THE DOOR ON THE PRIMARY SKIN OF THE TAIL BOOM.SDR E3MA20160226001Tail Boom · crackedDURING A PERIODICAL INSPECTION, A 7 INCH CRACK WAS DISCOVERED ON THE LT SIDE OF THE TAIL BOOM. THE CRACK WAS MOSTLY LOCATED UNDERNEATH THE LT HORIZONTAL FITTING.SDR ALGA20160307001Skin · debondedDURING INVESTIGATION FOLLOWING A HUMS RED TRDS INDICATION & A SHARP RISE NOTED ON TRDS FSA S001A7 AT CRUISE. DARF BR-WH-021 INSPECTIONS REVEALED DE-BONDED SKIN UNDER THE SUPPORT STRUCTURE FOR THE TRDS BEARING. CURRENTLY WAITING FOR A REPLY FROM ENGINEERING.SDR HDNA20160210001Angle · crackedDURING SCHEDULED INSPECTIONS CRACKS WERE FOUND IN THE TAIL CONE AT STATION 6616, LOWER AREA. REPLACED FRAME ANGLE 117-22122-001 02-100 & INSTALLED REPAIR LIT 117-SB20-101-3 1 IAW SB MBB BK117-20-101 SECTION 2 B 1 2.SDR QMLA2016020216005Stringer · damagedDURING AAIP A 0312 ZONE 12 AIRFRAME INSPECTION, DISCOVERED DAMAGE ON INTERIOR TAIL BOOM OMEGA STRINGER. DAMAGE IS LOCATED ON THE INSIDE TAIL BOOM UPPER RT OMEGA STRINGER 130MM FROM FLANGE OPENING. DAMAGE IS 10MM X 7MM WITH A MAX DEPTH OF .030 INCHES. SUSPECSDR E3MA20151217001Stator · crackedCRACKS IN 5 TAIL ROTOR STATORS WERE FOUND DURING AN INSPECTION.SDR HDNA201511030001Skin · crackedTAIL BOOM LT SIDE, JUST ABOVE THE LE OF HORIZONTAL STABILIZER CRACKED IN STIFFENER. UPON REMOVAL OF STIFFENER PN 117-30252.17 FOUND 4 ADDITIONAL CRACKS IN TAIL BOOM SKIN AROUND HORIZONTAL STABILIZER CUT OUT. TAIL BOOM BEING SHIPPED FOR REPAIR.
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