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 2A6D20221109002Tail Boom · chafedDAMAGE WAS NOTED TO THE TAIL BOOM LH SKIN (P/N: L535A1601107) IN THE FORM OF CHAFE IN 2 LOCATIONS THAT ARE NEXT TO EACH OTHER. THE FIRST PART OF THE DAMAGE IS LOCATED AT BOTTOM SIDE OF THE TAIL BOOM WHERE BOTH LH AND RH SKIN JOIN NEAR HORIZONTAL STABILIZER LOCSDR AC2A2022103013901Tail Boom · unserviceableTAIL STRUCTURE HAS AREA OF DELAMINATION ON R/H SIDE.SDR 2A6R2022090264801Tail Boom · chafedDURING 1000 HOUR INSPECTION, FOUND TAILBOOM CHAFE MARK ON BOTTOM CENTER SURFACE ROUGHLY 3FT AFT OF FWD RING FRAME THAT APPEARS TO BE THRU MULTIPLE PLIES. PERFORMED REPAIR ON TAILBOOM CHAFE DAMAGE ON BOTTOM CENTER SURFACE AFT OF FWD RING FRAME USING ECS0031-12SDR CALA2022090202241None · damagedMAINTENANCE DISCOVERED STATION 1640 FUSELAGE FRAME WEB P/N 146N8 711-72 BETWEEN STRINGERS S-5R AND S-6R CHAFFED. THE DAMAGE WAS B LENDED SMOOTH PER THE REQUIREMENTS OF B757-200 SRM 53-00-07 ALLO WABLE DAMAGE 1, FIGURE 101, DETAIL II, WITH MINIMUM MEASURED REM SDR 2A6D20220707001Skin · chafedDAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.AL) IN THE FORM OF A CHAFE NEAR THE LOWER VERTICAL FIN MOUNTING BRACKET.SDR 2A6D20220707002Tail Boom · damagedDAMAGE TO THE INNER SKIN PLIES OF THE LH TAIL BOOM SKIN (PN: L535A1601107). THE INNER SKIN HAS BEEN DRILLED THROUGH AT 6EA POINTS OF A MOUNTING PLATE FOR THE VOR ANTENNASDR AC2A2022060813902Tail Boom · delaminatedTAIL STRUCTURE DELAMINATED INSIDE AND OUTSIDE AT R/H STA11020 UPPER AREA. CORRECTIVE ACTION - CARRIED FORWARD TO CRS AC2R685K SHEETMETAL SHOP W/O TASK C06456-1 FOR CORRECTIVE ACTION.SDR 2A6R2022051163701Frame · crackedDURING 1000 HOUR INSPECTION, FOUND THE AFT TAIL BOOM RING FRAME TO BE CRACKED. TAILBOOM PN: 211105701, SN: EVL362. REMOVED TAIL BOOM AND SENT TO AIRBUS FOR REPAIR.SDR SWAA2022040488909Doubler · missingEXTERNAL POWER DOOR CUTOUT HAS MISSING MATERIAL AT LOWER SETION THAN MEASURES 1.2' X .50' / [01] REPAIRED EXT POWER DOOR CUTOUT LOWER SECTION OF SURROUND DOUBLER PER SRM 53-10-15-2R-4.SDR 2022FA0000204Tail Boom · dentedDAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.22). THE CREASE AND GOUGE DAMAGES WERE DISCOVERED TO BE JUST FORWARD OF THE TAIL ROTOR GEAR BOX. THE CREASE DAMAGE IS APPROXIMATELY 0.40" WIDE AND THE GOUGE DAMAGE IS APPROXIMATELY 0.10" IN LENGTH, 0.05" SDR 2A6D20220315002None · usedCUSTOMER HAS REPORTED DAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.22). THE CREASE AND GOUGE
DAMAGES WERE DISCOVERED TO BE JUST FORWARD OF THE TAIL ROTOR GEAR BOX. THE CREASE DAMAGE IS APPROXIMATELY 0.40”
WIDE AND THE GOUGE DAMAGE IS APPROXIMATELYSDR QMLA2022030720014Frame · noneCRACK FOUND ON FRONT SIDE ANGLE OF STA 6616 AND ON AFT SIDE OF FRAME OF STA 6616. THE CRACK IN THE FRAME AND ANGLE ARE LOCATED ADJACENT TO THE RIGHT HAND OMEGA STRINGER, THE LENGTH OF EACH CRACK IS APPROXIMATELY 3/4" IN LENGTH.SDR QMLAFrame · usedCRACK FOUND ON FRONT SIDE ANGLE OF STA 6616 AND ON AFT SIDE OF FRAME OF STA 6616. THE CRACK IN THE FRAME AND ANGLE ARE LOCATED ADJACENT TO THE RIGHT HAND OMEGA STRINGER, THE LENGTH OF EACH CRACK IS APPROXIMATELY 3/4" IN LENGTH.SDR 2022FA0000080Skin · dentedSTABILIZER RECEIVED A SMALL INDENT WHEN IT WAS REMOVED FROM THE AIRCRAFT DURING MAINTENANCE. REPAIRED INDENT ON THE LEFT HAND, OUT BOARD, BOTTOM SIDE OF STABILIZER PN: 407-023-801-155, SN: VL00017251 (BONDED PANEL ASSY: PN: 407-023-801-105). INDENT DID NOT PESDR 2022FA0000034Tail Boom · chafedTAIL BOOM SERVO RH BEAM (PN: 350A23-4015.24) IN THE FORM OF A CHAFE. THE CHAFE DAMAGE WAS MEASURED TO BE APPROXIMATELY 0.50” X 0.10” AND 0.015” DEEP.SDR 2022FA0000033Skin · chafedTAILBOOM P/N 350A23-0000-0705 S/N TB4490 SKIN DAMAGE AT APPROXIMATELY X1219 RBL 228. THE DAMAGE IS MINOR CHAFING MEASURING 0.005” AT ITS DEEPEST.SDR 2A6R2021120162701Tail Boom · corrodedDURING 1000 HOUR AIRFRAME INSPECTION FOUND CORROSION AT THE TAIL BOOM AFT RING FRAME REINFORCEMENT WHERE SERVICE BULLETIN SB EC135-53-030 WAS PERFORMED. THE CORROSION HAS MITIGATED UNDER THE REINFORCEMENT P/N L535H2100202. REPLACING THE TAIL BOOM.SDR QMLA2021102920055Skin · dentedDAMAGE WAS NOTED TO THE TAIL BOOM LOWER FWD SKIN (PN: 350A23-0020.20) IN THE FORM OF MULTIPLE DENTS, AS WELL AS A DENT IN THE TAIL BOOM UPPER FWD SKIN (PN: 350A23-0020.21). THE LARGEST DENT IMPACTS BOTH THE LOWER FWD SKIN AND THE UPPER FWD SKIN AND WAS MEASURESDR 2A6D20210824001Skin · damagedDAMAGE WAS NOTED TO THE TAIL BOOM UPPER SKIN PANEL (PN: 350A23-0020.21) AS WELL AS THE YAW COMPENSATOR CHANNEL REINFORCEMENT (PN: 355A23-2000.20) IN THE FORM OF CHAFE DAMAGE. THE CHAFE DAMAGE TO THE TAIL BOOM UPPER SKIN WAS MEASURED TO BE 1.70” X 0.40” AND 0.0SDR 2A6D20200730002Tail Boom · chafed4685 LOWER FWD TAILBOOM SKIN HAS TWO CHAFING MARKS ON ITS RH LOWER INTERNAL FACE LOCATED BETWEEN THE TAILBOOM JUNCTION FRAME AND THE X620 CIRCUMFERENTIAL FRAME CAUSED BY A WIRE HARNESS. THE LARGER OF THE TWO WAS MEASURED AT APPROXIMATELY .007” IN DEPTH, 1.2” SDR 2A6D20210701001Frame · chafedFUSELAGE SIDE TAIL BOOM JUNCTION FRAME (PN 350A21-4503-20) HAS CHAFING DAMAGE FROM THE CABLE RUBBING ALONG THE EDGE OF A FEEDTHROUGH HOLE IN THE UPPER PORTION OF THE FRAME. THE DAMAGE IS UP TO 0.070” DEEP, 0.100” WIDE, AND 0.500” LONG.SDR 2A6R2021060260601Rib · corrodedDURING 1000 HR INSPECTION FOUND VERTICAL STAB TOP RIB HAS EXFOLIATION CORROSION BEHIND SEVERAL NUTPLATES.SDR QMLA2021042920021Tail Boom · crackedCRACK DAMAGE MEASURING 3" LONG WAS NOTED ON THE STA 4960 FRAME ASSY P/N 109-0340-03-261 AT WL 860/BL560. REPAIR OF THE DAMAGE WAS PERFORMED VIA REPAIR DOUBLER IAW AWPC-PSE-AW109-054 REV / DATED 22-APR-20. MULTIPLE (3 EA) CRACKS MEASURING .5" TO 1.25" LONG WESDR QMLA2021040920016Tail Boom · crackedA 3.8 INCH CRACK WAS FOUND ON THE TAIL BOOM NEAR THE LOWER FIN MOUNTING AREA. UPON FURTHER INSPECTION, DELAMINATION OF THE TAILBOOM SKIN (AROUND THE CRACK) WAS ALSO DISCOVERED (APPROXIMATELY 10.5" X 1.0 "). SMALL DEFORMATIONS IN THE SKIN (0.016" MAX) WERE ALSOSDR EVCA2021021904Structure · crackedCRACKS IN VERTICAL FAN.SDR 2A6R202101045882Plate · corrodedDURING 12 YEAR INSPECTION FOUND LT HORIZONTAL STABILIZER FLANGE DOUBLER P/N 350A23002AS51 CORRODED BEYOND LIMITS. REPLACING DOUBLER.SDR EVCA2020112201Bulkhead · crackedDURING ROUTINE INSPECTION, FORWARD TAILBOOM BULKHEAD FOUND CRACKED AT THE 7 O'CLOCK POSITION.SDR 2A6D20201112001Skin · dentedAC 4613 HAS A SMOOTH DENT ON THE TAILBOOM’S RT SKIN LOCATED AT APPROXIMATELY STA 8098, WL 1829, AND BL 70R JUST FORWARD OF THE HORIZONTAL STABILIZER OPENING. THE DENT IS .4 BY .4 AND .035 AT ITS DEEPEST.SDR EVCA20200824001Bulkhead · crackedDURING ROUTINE INSPECTION, VISUALLY FOUND CRACK IN TAILBOOM FWD BULKHEAD PN: 206-032-400-027 AT APPROXIMATELY THE 10 O'CLOCK POSITION.SDR 2A6D2020082002601Skin · chafedCHAFING ON THE RT INTERIOR SIDE OF THE TAILBOOM SKIN LOCATED AT APPROXIMATELY STA 7898, WL 2089, AND BL 90R JUST FORWARD OF THE HORIZONTAL STABILIZER OPENING. THE CHAFE IS .95” BY .12” AND IS .007” AT ITS DEEPEST POINT.SDR SWAA2021071502009Angle · crackedSUPPORT ANGLE CRACKED ABOVE AND I/B OF THE #1 TANK AFT BOOST PUMP ON REAR SPAR. / REMOVED AND REPLACED ANGLE PER SRM 51-40-02SDR 2A6D202006176001Skin · chafedAC 4539 HAS CHAFFING ON THE RT BATTERY TRAY SUPPORT AND ON THE INTERNAL SIDE OF THE TAIL BOOM SKIN. DAMAGE BEING OVER 12 INCHES LONG WITH A MAX DEPTH OF .020 . DAMAGE BEING LOCATED AT APPROXIMATELY BS 7948, BL 190R, AND WL 2039. IT HAS A MAX DEPTH OF .010 IN ASDR QMLA2020060220025Frame · crackedAFT RING FRAME CRACKED ON LEFT HAND SIDE OF TAILBOOM. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION PENDING AN APPROVED REPAIR.SDR 2A6D20200429001Skin Panel · dentedTHE TAILBOOM FWD LOWER SKIN PANEL HAS DENT DAMAGE. THE DENT LOCATION IS JUST AFT OF THE AFT FUSELAGE JUNCTION FRAME AND IS APPROX. 1.5” IN DIAMETER.SDR QMLA2020042320016Attach Fitting · crackedDURING AIRWORTHINESS CHECK BY THE MECHANIC, HE FOUND A 1.75" CRACK IN LH UPPER HORIZONTAL STABILIZER ATTACH FITTING. *** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION WHILE A BELL APPROVED CUSTOMER SERVICE FACILITY COMPLETES THE PART REPLSDR EVCA2020032500000Longeron · crackedDURING ROUTINE INSPECTION, THE LH UPPER TAILBOOM ATTACHMENT FITTING LONGERON PN: 206-031-314-037 WAS VISUALLY FOUND TO BE CRACKED.SDR QMLA2020032420015Angle · crackedCRACKS FOUND IN 5 PIECES OF SUPPORTING STRUCTURE OF # 1 TAILROTOR DRIVESHAFT BEARING MOUNT. AM SERVICE ENGINEERING WORKING WITH AGUSTA ON REPAIR. *** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION PENDING AN APPROVED REPAIR FOR THESE CRACKSDR EVCA2020031611Attach Fitting · crackedUPPER L/H TAILBOOM ATTACH FITTING CRACKED. REMOVED DAMAGED FITTING PN 206-032-409-001P AND INSTALLED NEW FITTING PN 206-032-409-001P IAW BHT-206-SRM-1 6-3-1.SDR QMLA2020031320011Structure · crackedWHILE CONDUCTING SCHEDULED MAINTENANCE, THE MECHANIC FOUND A CRACK ON THE VERTICAL FIN FLANGE THAT MOUNTS THE TAIL ROTOR GEAR BOX COVER TO VERTICAL FIN TOP AFT CORNER. ** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION PENDING REPAIR. **SDR 2020FA0000297Tail Boom · crackedFOUND A 1 INCH CRACK RT SIDE OF TAIL BOOM FORWARD OF HORIZONTAL STABILIZER OPENING.SDR 2A6R2020013055301Bearing Support · crackedFOUND NUMBER 5 BEARING SUPPORT CRACKED.SDR QMLA2020012815205Skin · crackedDURING A SCHEDULED HEAVY MAINTENANCE EVENT, THE MECHANIC FOUND A SMALL CRACK ON THE LH SIDE OF THE TAILBOOM, JUST FORWARD OF THE LEADING EDGE OF THE HORIZONTAL STABILIZER. *** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THIS TIME WHILE THIS CRACK IS REPAIRED PER OSDR QMLA2019123119100Frame · crackedCRACK FOUND AT FRAME 5A RIGHT TOP MOST HOLE EMANATING FROM RIVET HOLE TO EDGE OF DOUBLER APPROX .25 IN LENGTH.
WILL REPAIR CRACK AT FRAME 5A IAW EA 23-5310-EA-1480 REV. DATED 06/23/2016 FRAME PROCEDURE ON FAA FORM 337.SDR EVCA20191112001Attach Fitting · crackedDURING 300 HOUR INSPECTION, UPPER RH TAILBOOM ATTACHMENT FITTING FOUND CRACKED.SDR QMLA2019111119084Structure · crackedDURING A 600 HOUR INSPECTION, THE MECHANIC FOUND 4 CRACKS UNDER THE DEVORE LIGHT DOUBLER ON THE TOP RIGHT HAND SIDE OF THE HORIZONTAL STABILIZER. *** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION ***SDR QMLA2019111019083Bolt · looseDURING 600 HOUR INSPECTION, FOUND TORQUE LOSS ON UPPER VERTICAL FIN BOLTS WHERE IT ATTACHES TO THE TAILBOOM. REMOVED UPPER AND LOWER FIN ASSY.FOUND THAT DOUBLER HOLDING NUT PLATES IS WORKING AGAINST TAILBOOM RING FRAME. HEARD A POPPING CRACKLING SOUND FROM UPPSDR EVCA20191029002Attach Fitting · crackedDURING INSPECTION, THE TAILBOOM UPPER LH ATTACHMENT FITTING WAS VISUALLY IDENTIFIED AS CRACKED.SDR IAVA2019101600001Skin · crackedCRACK ON UPPER TAIL BOOM SKIN AT STATION 172 FROM 3RD RIVET FORWARD OF CASTING ON SKIN SPLICE SEAM TO 4TH RIVET AT TAIL ROTOR GEARBOX CASTING ATTACHMENT RIVET LINE.SDR QMLA2019100819078Structure · crackedDURING SCHEDULED HEAVY MAINTENANCE EVENT, TWO CRACKS WERE FOUND UNDER THE STRAKE OF THE VERTICAL STABILIZER TRAILING EDGE. ONE CRACK IS 3.5" IN LENGTH, AND THE OTHER IS 1.5" IN LENGTH. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION AWAITINSDR 2A6R2019092654001Structure · damagedDURING INSPECTION OF TAIL BOOM FOUND DAMAGE BENEATH 2 ANTENNAS AT FS 5315 & FS 6730. AWAITING ENGINEERING AUTHORIZATION TO REPAIR BY BONDING AND RIVETING DOUBLERS.
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