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 CA190814015Rivet · missing(CAN) IT WAS REPORTED TO BELL: DURING INSPECTION, 17 MISSING/LOOSE RIVETS FOUND AT TAILBOOM/TAIL ROTOR GEARBOX ATTACHMENT. (RELATED TO SDR 20190709012 AND 20190709013) (TC# 20190814015)SDR CA190806009Bolt · broken(CAN) DURING CRUISE FLIGHT THE PILOT HEARD "WHAT SOUNDED LIKE A SMALL BANG, A SOUND THAT IN THE PAST I HAD BEEN A METAL DRINK BOTTLE OR CELLPHONE DROPPING ONTO THE FLOOR." THE PILOT REDUCED POWER/AIRSPEED AND CHECKED THE GAUGES - NO VIBRATIONS OR ABNORMALITIESSDR ALGA201908090001Tail Boom · corrodedDURING CORROSION INSP CORROSION DAMAGE NOTED TO TAIL BOOM ASSY. OEM REPAIR IAW RS139-5352 ISSUE A.SDR CA190710003Bolt · damaged(CAN) UPPER BOLT ON CLOSURE PLATE WAS FOUND LOOSE DURING A DAILY INSPECTION. UPON REMOVAL OF CLOSURE PLATE IT WAS FOUND THAT THE BOLT HAD BEGUN TO ABRADE THROUGH THE CLOSURE PLATE, ELONGATING ITS BOT HOLE AND THE BOLT HEAD ITSELF WAS ABRADED DOWN PAST NOMINAL SDR CA190705001Fitting · cracked(CAN) DURING A SCHEDULED INSPECTION OF TAILBOOM ATTACHMENT FITTINGS THE UPPER L/H FITTING WAS SUSPECTED TO BE CRACKED. THE TAILBOOM AND COWLS WERE REMOVED FOR CLOSER INSPECTION. UPON CLOSER INSPECTION THE FITTING WAS FOUND TO BE CRACKED. TAILBOOM WAS REMOVED, SDR CA190709012Rivet · sheared(CAN) IT WAS REPORTED TO BELL:DURING INSPECTION TAIL ROTOR SUPPORT ASSEMBLY GEARBOX ATTACHMENT POINTS ,INSPECTOR COULD PULL OUT 6 RIVETS BY HAND. THEREFORE MAINTENANCE REMOVED THE PAINT AND FOUND OUT 17 SHEARED RIVETS AT THIS LOCATION.THIS AIRCRAFT DOES NOT HASDR QMLA2019062419055Skin · crackedTAIL BOOM SKIN CRACK AT STA 7000, WL 1065, 1.50 INCHES LONG, DISCOVERED DURING DAILY INSPECTION BY MECHANIC. ENGINES S/N33025 5579+35TT 17504.00FC S/N33028 5492:08TT 17205.00FC.SDR CA190709013Rivet · sheared(CAN) THE CUSTOMER REPLACED 7 RIVETS FROM THE TAIL ROTOR TRANSMISSION SUPPORT BECAUSE THE VIBRATIONS AFTER TAIL ROTOR BEARINGS FAILED IT WAS AT 1347.8HRS .70 HOURS LATER THEY HAVE 2 MISSING RIVETS, BOTH RIVETS COME APART IN DIFFERENT TIMES AFTER THE INSTALLATISDR AC2A201906163901Skin · corrodedCORROSION FOUND BETWEEN PREVIOUS REPAIR AND SKIN ON LEFT AFT TAILCONE AREASDR CA190607012Stabilizer · broken(CAN) IT WAS REPORTED TO BELL: VERTICAL FIN BROKE IN FLIGHT, FOLDED ON THE RH SIDE OF THE SHIP. SHIP FLIGHT TIME 16,000 HOUR +/-. (TC# 20190607012)SDR ALGA201908090003Stabilizer · crackedDURING 1200HR INSP CRACKS WERE FOUND ON TAILPLANE ASSY. OEM REPAIR: RS139-5511-0365 REV A.SDR CA190530007Doubler · cracked(CAN) A CRACKED DEVELOPED ON THE UPPER R/S DOUBLER WHERE THE HORIZONTAL STABILIZER IS SECURED TO THE TAIL BOOM. (TC# 20190530007)SDR CA190514011Skin · cracked(CAN) IT WAS REPORTED TO BELL: WE FOUND A CRACK IN OUR TAIL BOOM AT APPROX.F.S 120.75 ON THE L/H SIDE WHERE THE LOWER PLATE FOR THE HORIZONTAL PASSES THROUGH. (TC# 20190514011)SDR CA190521011Structure · broken(CAN) IT WAS REPORTED TO BELL:DOWNWIND LANDING TO A RIVER BED. PILOT REPORTED FEELING A VIBRATION BEFORE TOUCH DOWN BUT REPORTED NO UNUSUAL CONTROL PROBLEMS. LANDING WAS MADE WITH AN EXTREMELY TAIL LOW ATTITUDE AND PILOT REPORTED FEELING AN IMPACT AND HEARING SDR QMLA2019042549041Skin · crackedDURING A SCHEDULED MAINTENANCE EVENT, A CRACK WAS DISCOVERED ON TOP OF THE TAIL BOOM. THIS AIRCRAFT REMAINS OOS AT THE TIME OF THIS SUBMISSION AWAITING THE APPROVED REPAIR.SDR QMLA2019040279034Panel · delaminatedR/H TAILBOOM PANEL P/N 205 032 811 077 OUTER SKIN DELAMINATED APPROX. 24” X 3.5” BETWEEN BOOM STATIONS 77-101 WL 72.L/H TAILBOOM PANEL P/N H205 032 813 67 OUTER SKIN DELAMINATED APPROX. 15” X 2.75” BETWEEN BOOM STATIONS 73-88. ALSO PANEL HAS CORROSION ALONG TSDR QMLA2019032719030Tail Boom · crackedDURING AN ONGOING 600 HOUR/24 MONTH AIRFRAME INSPECTION, THE MECHANICS NOTICED ON THE REMOVAL OF THE TAIL ROTOR BLADE WHAT APPEARED TO BE A CRACK IN THE PAINT ON THE RIGHT HAND SIDE OF TAILBOOM. UPON FURTHER INSPECTION, THE CRACK EXTENDED 8 INCHES IN TOTAL. ITSDR 2A6R2019032551903Bearing Support · damagedUPON REMOVAL OF FWD TAIL ROTOR DRIVE SHAFT, FOUND THE NR 6 DRIVE SHAFT BEARING SUPPORT ATTACHMENT HOLES ELONGATED.SDR EVCA2019022700000Post · crackedDURING INSPECTION AT OUR SW-RMO FOUND CENTER POST WEB CRACKED. AFT RIGHT SIDE APPROXIMATELY WL 67. THE DAMAGE PORTION OF THE WEB WILL BE REMOVED AND REPLACED WITH THE NEW WEB AND SPLICE DOUBLER. ALL MAINTENANCE ACCOMPLISHED WITH REFERENCE TO SRM CHAPTER 5-1-1 SDR QMLA2019022619020Skin · crackedDURING A PREFLIGHT INSPECTION, THE MECHANIC FOUND A CRACK ON THE LOWER SKIN OF THE LT HORIZONTAL STABILIZER. THE CRACK WAS STOP DRILLED TO PROVIDE TEMPORARY RELIEF UNTIL THE MATERIALS NECESSARY TO ACCOMPLISH THE PERMANENT REPAIR ARRIVED. SRM, CHAPTER 51-70-51,SDR QMLA2019021419019Frame · crackedDURING A SCHEDULED INSPECTION EVENT, A CRACK WAS FOUND AT STATION 6616 APPROX. 2 O'CLOCK POSTION IN THE TAIL CONE AREA. THE REPAIR IS COVERED IN THE SRM FOR THIS AIRCRAFT. RECOMMENDED REENFORCEMENT TO AREA IAW SB 53-004 AS PER AIRBUS TECH REP. THIS AIRCRAFT RESDR EVCA201901142Attach Fitting · crackedTAILBOOM ATTACHMENT FITTING UPPER LEFT TAILBOOM SIDE CRACKED. AMT'S REMOVED AND REPLACED TAILBOOM FITTING.SDR QMLA2019011019016Frame · cracked2 CRACKS WERE FOUND IN THE TAILCONE OF AIRCRAFT DURING A 1200 HOUR INSPECTION ON A SECTION OF FRAME AT STATION 6616 AND THE ATTACHED DOUBLER. THESE CRACKS WERE REPAIRED AND DOCUMENTED ON AN FAA FORM 337 DATED 01/29/2019.SDR QMLA2019010819004Rib · crackedWHILE CONDUCTING INSPECTION AAIP A 2210 – 1200 HOUR UNDER SECTION 2.3 AMM CH53-53-00, 6-1 AND FOLLOWING AMM CH 53-53-00, 4-2 TO COMPLETE INSPECTION, I REMOVED THE HORIZONTAL STABILIZER LEFT HAND END PLATE TO GAIN ACCESS TO INTERIOR OF HORIZONTAL STABILIZER FORSDR 2A6R201812055101Frame · crackedTAIL BOOM 3035 RING FRAME CRACKED AT 11:00 POSITION AT SKIN LAP.SDR HDNA2018100100000Frame · crackedTHE AFT RING FRAME (X9227 FRAME) CRACKED ON THE LEFT SIDE APPROX. 2 INCHES BELOW THE BOLT USED FOR ELECTRICAL GROUNDING PURPOSES.SDR EVCA201809052Attach Fitting · crackedTAILBOOM ATTACHMENT FITTING UPPER LEFT TAILBOOM SIDE CRACKED. AMT'S REMOVED AND REPLACED TAILBOOM FITTING.SDR QMLA2018081618097Mount · crackedDURING A PREFLIGHT, A CRACK WAS NOTICED NEAR UPPER LEFT CORNER OF TAIL ROTOR GEARBOX MOUNTING PAD. INVESTIGATED A POSSIBLE CRACK AND CLEANED AREA OF PAINT. INSPECTED THE UNDERSIDE OF THE MOUNTING PAD. AFTER CLEANING AND REMOVING PAINT A LARGE NOTICEABLE CRSDR AC2A2018080740701Bulkhead · crackedFOUND FORWARD TAILBOOM BULKHEAD CRACKED DURING PHASE A, 300 HOUR INSPECTION. THE CRACK WAS LOCATED BETWEEN THE UPPER TWO RIVETS AT THE 12 O'CLOCK POSITION, TERMINATING AT EACH RIVET HOLE. THE BULKHEAD WAS REMOVED AND REPLACEDSDR EVCA201807051Attach Fitting · crackedTAILBOOM ATTACHMENT FITTING UPPER LEFT TAILBOOM SIDE CRACKED. AMT'S REMOVED AND REPLACED TAILBOOM FITTING.SDR QMLA2018062918076Bulkhead · crackedAFT BULKHEAD CRACKS AT STA 9725 WL 1564.1 DISCOVERED DURING DAILY INSPECTION BY MECHANIC.SDR EVCA20180523211Mount Flange · crackedWHILE PERFORMING A SCHEDULED 100 HR INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM MOUNTING RING PN: 206-032-400-027 APPROXIMATELY 3 INCHES IN LENGTH BELOW THE UPPER LEFT ATTACHMENT FITTING.SDR 2A6R201805254743Skin · chafedDURING INSPECTION, FOUND DAMAGE IN THE FORM OF CHAFING TO THE INSIDE SURFACE OF THE LOWER FORWARD SKIN OF THE TAILBOOM. THE DAMAGED AREA IS APPROXIMATELY 0.017" DEEP AND 0.75" LONG. A DOUBLER REPAIR WAS ACCOMPLISHED IAW RDAS-53-027-18, REV A.SDR QMLA2018041318044Structure · crackedFOUND A CRACK ON THE RIGHT SIDE OF THE TAILBOOM AT THE AFT. LOWER CORNER OF THE STABLIZER CUT OUT.SDR ULXR201804050001Skin · delaminatedMAJOR DELAMINATION ON THE TAILBOOM SKIN.SDR QMLA2018040118037Shelf · crackedDURING INSPECTION, FOUND THE BATTERY SHELF CRACKED AFT OF TB FRAME 2285.8 STARTING AT 4 INCHES AND IS APPROXIMATELY 1.75 INCHES LONG, ANOTHER CRACK 3 INCHES AFT OF THAT, APPX 4.5 INCHES LONG WITH MULTIPLE CRACKS AND MISSING MATERIAL.SDR HEER20180322907Structure · separatedSEPERATION INSIDE BOOM IN VERTICAL PYLON AREA BOOM STATION 11,951 TO 12,052. REPLACED WITH NEW TAIL STRUCTURE.SDR HEER20180322906Structure · separatedLEFT SIDE BONDED PANEL SEPERATED ON SIDE SKIN AT BOOM STATION FROM 9970 TO 10.149 ON INSIDE SKIN TWO PLACES BOOM STATION 9817 TO 9868 AND 9970 TO 10.274. REPLACED TAIL STRUCTURE.SDR QMLA2018031718032Frame · crackedDURING A 300 HOUR INSPECTION OF THE HORIZONTAL STABILIZER, FOUND THE UPPER RT ATTACH FITTING BROKEN, AND THE FRAME IN THE TAILBOOM CRACKED.SDR QMLA2018022618020Doubler · crackedDURING A PREFLIGHT AIRWORTHINESS CHECK, FOUND CRACK IN THE UPPER AFT CORNER OF DOUBLER AROUND THE OPENING OF THE BATTERY COMPARTMENT IN THE TAILBOOM. CRACK MEASURED 1 3/8 INCHES IN LENGTHSDR 2018F00115Structure · crackedCRACK FOUND INSIDE THE TAIL BOOM CONESDR EVCA201802211Attach Fitting · crackedDURING INSPECTION AND COMPLIANCE WITH RECURRING AD 2013-25-10 FOUND THE UPPER LT TAIL BOOM ATTACHMENT FITTING TO BE CRACKEDSDR 2018FA0000062Spar · chafedWHILE PERFORMING A 500HR VERTICAL STABILIZER ANTI-COLLISION LIGHT CONDUIT CLAMP INSPECTION, DAMAGE WAS FOUND. THE FASTENER FOR THE UPPER CONDUIT CLAMP WAS PULLED THROUGH THE SPAR. THE HOLE MEASURES 7/32 X 5/16, THE WASHER THAT IS ON THE HEAD SIDE OF THE RIVSDR EVCA201802061Attach Fitting · crackedDURING SCHEDULED INSPECTION AND COMPLIANCE WITH FAA AD 2013-25-10 MAINTENANCE TECHNICIAN FOUND A 1.125" CRACK IN UPPER LEFT HAND TAILBOOM ATTACH FITTING PN: 206-032-409-001. UPON REMOVAL OF THE TAILBOOM FROM THE AIRCRAFT TO FACILITATE REPAIR MAINTENANCE TECHNISDR EVCA201802021Mount · crackedWHILE PERFORMING SCHEDULED 100 HOUR INSPECTION, NOTED A 1.5 INCH CRACK IN THE TAILBOOM MOUNTING RING EXTENDING FROM THE UPPER LT MOUNTING HOLE TO THE EDGE OF THE BULKHEAD.SDR QMLA2018012318010Skin · dentedA DENT WAS FOUND ON THE RT SIDE OF TAILBOOM JUST ABOVE HORIZONTAL STAB APPROXIMATELY 5 INCHES IN LENGTH.SDR QMLA2017121917140Skin · crackedAFTER PILOT WASHED AIRCRAFT, BS 8081, WL 1300 ON PILOTS SIDE OF TAIL BOOM THERE WAS A 2.5 INCH CRACK SEEN BETWEEN THE MOUNTED STRINGER RIVET LINES. A SECOND CRACK WAS LOCATED AT BS 8085, WL 1400 ON PILOTS SIDE OF TAILBOOM THERE WAS A 2.25 INCH CRACK NOTED ASDR QMLA2017121517138Door Frame · crackedFOUND CRACK IN AFT BATTERY DOOR FRAME. CRACK IS APPROXIMATELY ONE INCH LOCATED IN THE AFT UPPER CORNER STARTING AT THE OPENING EXTENDING ONE INCH DIAGONALLY.SDR QMLA2017120717135Mount · crackedDURING SCHEDULED 600HR AIRFRAME INSPECTION FOUND LOWER R/H STABILIZER MOUNT FITTING CRACKED. INFORMATION BELOW IS FOR THE NEXT HIGHER ASSY AS THE PARTS ARE NOT SERIALIZED AND NOT PROCURABLE FROM IPC, REPAIR AND PARTS ARE ONLY ALLOWED FROM AIRBUS ONLYSDR QMLA2017112017127Attach Fitting · crackedCRACK FOUND IN THE RT UPPER HORIZONTAL STAB ATTACH FITTING DURING DAILY INSPECTION.
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