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 2026FA0000299Tail Boom · corrodedDURING THE PERFORMANCE OF THE GENERAL VISUAL INSPECTION AS SPECIFIED IN THE CONDITIONS OF PSE/TQ/2025/215289 REPAIR DEFERRAL LETTER, EVIDENCE OF PROPAGATION AND WORSENING CONDITIONS WAS DETERMINED OF THE CORROSION AT STA 8700, BL0.0 LOWER STRUCTURE OF 9Y-ELL TSDR 2A6R2026040675204Skin · crackedDURING AN INSPECTION A CRACK WAS FOUND ON THE TOP OF THE HORIZONAL STABILIZER MEASURING 4.25 IN LONG. THE HORIZONTAL WAS REMOVED AND REPLACED. FOR MORE INFORMATION, PLEASE SEE MG752 UNDER CRS2A6R933B.SDR 2A6R2026031675203Stator · corrodedDURING A 12-YEAR INSPECTION, THE STATOR WAS REMOVED AND FOUND TO HAVE MULTIPLE LEGS WITH CORRODED BASES. THE DEPTH OF CORROSION VARIED FROM .020 TO .030 DEEP. PER AIRBUS TE-2026-EC130-00406, THE STATOR ASSEMBLY WAS REMOVED AND REPLACED. FOR MORE INFORMATIONSDR U0GA VP000639Tail Boom · corrodedTHIS AIRCRAFT HAS BEEN GROUNDED AT OUR REPAIR STATION ON VP-000639-2024 SINCE THE DATE OF DISCOVERY. THE REPAIR IS AS FOLLOWS; REPLACE LT SIDE PANEL, P/N 3G5350A07431C1 AND STA 8700 BULKHEAD FRAME, P/N 3G5306P14811 ON TAILBOOM P/N 3G5350A00135 S/N PZL003 TAILBSDR 2026FA0000022Stabilizer · crackedREFENCES ARE MADE TO SDR UNIQUE CONTROL #2026FA0000017, #2026FA0000018 AND #2026FA0000020 RAISED PREVIOUSLY. #2026FA0000017 - ERRORS WERE MADE WHEN ENTERING THE AIRCRAFT SERIAL NUMBER (9Y-TKB) THIS SHOULD READ "41395" AS CORRECTED, #2026FA0000018 - DIFFICULTY SDR 2026FA0000017Stabilizer · crackedDURING A VISUAL INSPECTION OF 9Y-TKB AFTER FLIGHT THE LINE SUPERVISORS DISCOVERED THE CRACK ON THE TAILPLANE ASSEMBLY LEFT LEADING EDGE LOWER PANEL. LOCATION OF CRACK IS ESTIMATED TO BE STA 12370 AND BL (-940 THRU -718). A LOGBOOK ENTRY (LBE 206/25) WAS RAISESDR EVCA20251028001Fitting · installedUPPER L/H TAILBOOM ATTACHMENT FITTING CRACKEDSDR 2A6R1024202574601Rail · chafedCHAFING DAMAGE WAS FOUND ON THE TAIL BOOM L/H TRDS SUPPORT RAIL/STIFFENER SHEET (P/N: 350A231028.66) JUST FORWARD OF THE #3 TRDS BEARING SUPPORT. THIS DAMAGE IS A 0.25” IN LENGTH AND 0.1” IN HEIGHT SECTION THAT IS CHAFED THROUGH THE FULL THICKNESS OF THE RAIL.SDR QMLA2025102720109Mount · crackedHORIZONTAL STAB RH LOWER MOUNT CRACKED, FELL OFF WHEN REMOVING HORIZONTAL STABILIZER FOR 300 HR INSPECTION. LEVEL 4
REPAIR. AIRBUS REPLACED FITTING AND APPLIED SB 55-001 FOR REPAIR.SDR 2A6R 09222025743Skin · crackedDURING THE 600 HOUR / 24 MONTH AIRFRAME INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM SKIN (TAILBOOM P/N: 350A2307150002 S/N: TB7538) ON THE UPPER R/H CORNER OF THE BATTERY COMPARTMENT DOOR DOUBLER MEASURING 1.35" IN LENGTH AND STOPPING AT A RIVET HOLE. THIS CSDR QMLA2025092220097Skin · crackedDURING THE 600 HOUR / 24 MONTH AIRFRAME INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM SKIN (TAILBOOM P/N: 350A2307150002 S/N: TB7538) ON THE UPPER R/H CORNER OF THE BATTERY COMPARTMENT DOOR DOUBLER MEASURING 1.35" IN LENGTH AND STOPPING AT A RIVET HOLE. THIS CSDR EVCA20250502001Structure · crackedCRACK EXCEEDING THE MANUFACTURES LIMITS IN THE HORIZONTAL STABILIZERSDR UIEA2025032500386Bulkhead · crackedRH BS 1480 B/HEAD VERTICAL WB I/B AREA FOUND CRACK(<P>VERTICAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201 AND RI-53-40-17541 REV B. NO FURTHER DEFECTS NOTED</P>)SDR QMLA2025010820045Skin · crackedDURING INSPECTION FOUND 2 CRACKS IN THE TOP SKIN OF THE TAILBOOM.SDR QMLA2025021820019Mount Bracket · crackedFOUND HORIZONTAL STABILIZER UPPER MOUNT BRACKETS CRACKED ON PRE-FLIGHT INSP.SDR 2025FA0000061Skin · crackedFUSELAGE – TAIL BOOM - TOP SKIN CRACKEDSDR HDNA202412300324Tail Boom · crackedMULTIPLE CRACKS FOUND ON THE 6135 FRAME OF THE TAIL BOOM.SDR 2024FA0000955Mount · chafedTAIL GEARBOX MOUNTING PLATE CHAFE DAMAGE.SDR 4DSR202412050001Support Bracket · corrodedDURING A SCHEDULED 12YR (144M) INSPECTION OF THE TAIL BOOM SECTION, THE NO. 6 BEARING SUPPORT BRACKET WAS FOUND TO HAVE MAJOR CORROSION TO THE INSIDE BOTTOM LEFT CORNER OF THE BRACKET. AIRBUS TECH REP WAS CONTACTED AND DETERMINED TO BE A MINOR REPAIR. R&R OF TSDR EVCA20241204001Stiffener · crackedVERTICAL TUNNEL AFT RH STIFFENER CRACKED. VERTICAL TUNNEL SKIN CRACKED AT WL 65.0SDR HEEA202411190001Support · looseT/R GEAR BOX MOUNTING CAN ON AFT END OF TAILBOOM HAS LOOSE FASTENERS.SDR SWAA2024121060475Scuff Plate · crackedCRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-715085<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A23272257; DUE DATE: 15-JAN-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :185943 ; DUE DATE : 10/MAR/25;[03] TOOL USED RADISDR EVCA20241119001Skin · damagedBIRD STRIKE WHILE IN CRUISE FLIGHT RETURNING TO BASE. PILOT LANDED IN FIELD NEAR FORUM AR. AMT NOTED DAMAGE TO VERTICAL FIN LOWER LEADING EDGE. REPLACED VERTICAL STABILIZERSDR 2A6R2024101872002Skin · crackedCRACK DAMAGE WAS DISCOVERED ON THE TAIL BOOM LOWER SKIN (PN: 350A23-4288-20) AT THE UPPER AFT AREA OF THE BATTERY DOOR OPENING. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130SDR 2024F00249Rib · crackedNOSE RIB 1S FOUND CRACKED ON VERTICAL SECTION OF THE TAIL BOOM.SDR FXTA20240926001Cap · crackedCAP ON TOP OF THE VERTICAL THAT BEACON MOUNTS TO CRACKED IN MULTIPLE PLACES ALLOWING THE BEACON TO BECOME LOOSE ON TOP OF THE VERTICAL STABILIZER.SDR 4DSR202409110001Skin Panel · crackedAIRBUS AS350B3E: DURING A SCHEDULED 12YR INSPECTION, THE TAIL BOOM WAS INSPECTED FOR CRACKS. A CRACK WAS DISCOVERED ON THE RIGHT-SIDE SKIN PANEL. THE CRACK IS NEAR THE AFT EDGE FEED THROUGH OPENING FOR THE HORIZONTAL STABILIZER. AIRBUS WAS CONTACTED AND A REPSDR 2A6R2024082971107Skin · corrodedCRACK DAMAGE WAS DISCOVERED ON THE TAIL CONE SKIN (PN: L533M1022262) ON THE RH SIDE. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-1344, ISSUE A DATED 06 MAY 2024.SDR EVCA202408120001Attach Fitting · crackedUPPER LEFT TAILBOOM ATTACHMENT FITTING, TAILBOOM SIDE, CRACKED FROM EDGE TO EDGE ACROSS TWO FWD OUTBOARD RIVETSSDR HEEA2024061100443Pylon · corrodedCORROSION INSIDE HORIZONTAL STABILIZER IN NUMEROUS AREAS ON FITTINGS AND LONGERONS.SDR 2024FA0000389Tail Boom · crackedMULTIPLE CRACKS/RIVETS FOUND IN TAIL BOOM. CRACK ON THE OMEGA THAT GOES UNDER THE 10L CRACKS AT FASTENERS ON BOTH SIDES
L/H WEDGE RIVETS MAKING A GOOD BIT OF MUD AT MULTIPLE SEAMS & RIVETS.SDR 2A6D20240425008Stiffener · corrodedDAMAGE TO THE TAIL BOOM LH FWD STIFFENER MEASURED TO BE APPROXIMATELY 0.85” X 0.85” X 0.0125” IN THE FORM OF CORROSION.SDR S6GA202404080113Skin · crackedA CRACK WAS DISCOVERED IN THE TAIL BOOM SKIN JUST AFT OF THE RH ELEVATOR TORQUE TUBE MOUNTING HOLE. APPROXIMATELY 2.5" LONG AT APPROXIMATE STATION 8540. REPAIR IS LISTED IN LEONARDO ASRP AND COMPLIED WITH ASRP CH. 3C-A-53-51-02-05A-664A-D.SDR EVCA20240403244Support Bracket · wornDRIVESHAFT BEARING SUPPORT MOUNTING HOLE ELONGATEDSDR QMLA20240402234Bulkhead · crackedSUSPECTED BULKHEAD TO BE CRACKED NEAR UPPER RH BOLT HOLE. COULD SEE AN ANOMALY WITH A BORESCOPE, BUT COULD NOT VERIFY TILL THE TAILBOOM WAS PULLED. CRACK WAS THEN VERIFIED.SDR 2A6R2023101366804Unknown · unknownDURING A 1000 HOUR INSPECTION, FOUND CRACK ON THE RIGHT SIDE OF THE TAIL CONE SKIN P/N L533M102216. PERFORMING A REPAIR I.A.W. AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2023-2976SDR 2A6R2023083067903Tail Boom · dentedDENT DAMAGE TO THE TAIL BOOM UPPER SKIN PANEL (PN: 350A23-0750.20) WAS IDENTIFIED JUST AFT OF THE FUSELAGE-TAIL BOOM JUNCTION ON THE UPPER RIGHT HAND SIDE NEAR TAIL BOOM FRAME 156. THE DENT IS APPROXIMATELY 8MM (0.315”) IN DIAMETER AND 0.012” DEEP.SDR GVNA2023F00199Spar · crackedDURING ROUTINE SCHEDULED INSPECTION FOUND CRACK IN TOP L/H SIDE OF THE VERTICAL FIN MAIN SPAR.SDR SWAA2023061952592Intercostal · corrodedFWD LAV; AFT IB MOUNT AT STA 303.9 LBL 13 HAS CORROSION UNDER NUTPLATE.<[01] REMOVED FWD LAV. AFT I/B MOUNT FITTING AND NUT PLATE PER SRM 51-40-02.<BR>BLENDED OUT CORROSION AT LAV ATTACH FASTENER HOLE PER SRM 51-10-02. FOUND PITTING AND CRACK WITHIN FASTENER HSDR 2NVA2023052501Tail Boom · dentedFOLLOWING A ROUTINE TRAINING FLIGHT, DENTS WERE NOTED AT THE FORWARD END OF THE TAIL BOOM. THE TRAINING FLIGHT INCLUDED HOVERING AUTOROTATIONS WHICH WERE NOT RECEIVED OUT OF THE ORDINARY. CONTACTED OEM FOR INPUT.SDR QMLA2023052620040Tail Boom · crackedDURING VISUAL INSPECTIONS FOUND A CRACK AT THE 0900 O'CLOCK POSITION ON THE 11L FRAME OF THE TAIL BOOM. DURING DISASSEMBLY AND FURTHER INSPECTION FOUND CHAFE DAMAGE AT THE 0300 O'CLOCK POSITION ON THE 11L FRAME AND ALSO A CRACK ON THE SPAR ABOVE THE 10L FRAME SDR 2A6D20230421002Tail Boom · chafedDAMAGE TO THE TAIL BOOM LH SKIN (P/N: 350A23-4288.20) IN THE FORM OF A CHAFE DUE TO
DRILL START LOCATED AT LOWER FORWARD SIDE OF THE AFT BATTERY BOX AREA. THE DAMAGE MEASURED TO BE
APPROXIMATELY 0.1285” X 0.1285” AND 0.0175” DEEP.SDR EVCA03062023Attach Fitting · crackedCRACK FOUND IN L/H UPPER ATTACHMENT TAILBOOM FITTING P/N 206-032-409-001P DURING 50 HOUR INSPECTIONSDR SWAA2023031502023Angle · crackedCRACK ANGLE FLOOR STRUCTURE STA 685 PLUS 7 INCH LBL 24.75 WL 208.1 AT PASSENGER CABIN 2023-119348<[01] REPLACED ANGLE LOC. FLOOR STRUCTURE STA 685 PLUS 7 INCH LBL 24.75 WL 208.1 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0 DWG 111A6000 REV ?. SEE INDIVISDR EVCA202301170001Tail Boom · cracked1/2 INCH CRACK AT UPPER LH INBOARD SIDE OF TAILBOOM RINGSDR EVCA010320233Ring · cracked1/2 INCH CRACK AT UPPER LH INBOARD SIDE OF TAILBOOM RING.SDR 2A6R2022122803Tail Boom · crackedDURING 1000-HOUR INSPECTION, A CRACK WAS DISCOVERED ON TAIL CONE UPPER FRAME 7 (PN: L533M1022215) ON THE FLANGE. THE CRACK MEASURES APPROXIMATELY 0.30” LONG.SDR EVCA202212090001Attach Fitting · crackedCRACK FOUND IN LT UPPER ATTACHMENT TAILBOOM FITTING DURING 100 HOUR INSPECTION.SDR EVCA202212010001Attach Fitting · crackedDURING COMPLETION OF AD 2013-25-10 INSPECTION FOUND THAT THE UPPER LEFT TAILBOOM ATTACHMENT FITTING WAS CRACKED.SDR EVCA20221111001Attach Fitting · crackedCRACK FOUND IN L/H UPPER ATTACHMENT TAILBOOM FITTING P/N 206-032-409-001P DURING 100 HOUR INSPECTION
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