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 = '5541' 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 = '5541' 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 AUS20011237Spar · cracked(AUS) RUDDER FORWARD SPAR CRACKED. FOUND DURING INSPECTION IAWAD/PA31/129.SDR QXEA0101861Rib · crackedPDX - RUDDER STRUCTURE RIB NR 5 IS CRACKED BETWEEN RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.SDR QXEA0101860Rib · crackedPDX - RUDDER STRUCTURE RIB NR 4 IS CRACKED BETWEEN RIVETS. REPAIRED IAW FOKKER SRM 51-31-01.SDR QXEA0101792Rib · crackedPDX - FOUND NR 6 RIB CRACKED BEHIND PANEL 573. REMOVED AND REPLACED RIB PER FOKKER SRM 51-31-01.SDR CA011029018Skin · cracked(CAN) THE PROBLEM WAS IDENTIFIED DURING "C1, 40,000 CYCLE INSP., 12M, 24M". INSPECTION OF THE ZONAL CARD "323E - EXTERNAL GENERAL VISUAL INSPECTION OF FORE RUDDER", WAS FOUND TO HAVE A CRACKED SKIN AT STA Z335.500. FURTHER INSPECTION OF THIS AREA INDICATED THESDR QXEA0101282Rib · crackedYYC-RIB 5 ON RUDDER IS CRACKED IN 2 PLACES. REPAIRED IAW FOKKER SRM 55-31-01, PAGE 2.SDR 01FDEA00403Rib · crackedDURING ROUTINE INSP LWR RUDDER, LWR THRUST HINGE RIB FOUND CRACKED AT FASTENER COMMON TO FIN REAR SPAR. *S/D* HFEC IND CRACK TERMINATED. REMOVED, REPLACED AND FAB PER IAW FEDEX DRAWING SRM 27-55-005, SRM 51-30-2.SDR 20010608CW003Rib · crackedWHILE C/U CHECKLIST ITEM FOR RUDDER BALANCE WEIGHT ON ANNUAL INSPECTION: FOUND WEIGHT LOOSE, YET BOLTS WERE TIGHT. INVESTIGATION SHOWED UPPER RIB ON RUDDER BROKEN OUT UNDER BALANCE WEIGHT. THIS ITEM INSPECTED 149 HOURS PREVIOUS AND FOUND TIGHT. PERIODIC RESDR SW15200112285Spar · crackedCRACK IN UPPER LIGHTING HOLE, UNDER THE TOP HINGE, IN THE LEADING EDGE RUDDER SKIN/SPAR. TO PREVENT RECURRANCE, REMOVE OR ELEMINATE LIGHTING HOLE IN NEW OR REPLACEMENT PARTS.SDR SWAA011254Spar · crackedDURING SCHEDULED 1/2D CHECK, FOUND RUDDER FWD SPAR CRACKED AT STA 27.95. REPAIRED PER BFG ER.SDR QXEA0100610Rib · crackedYYC- RIB 4 THROUGH 2 HAS SMALL CRACKS AT TRAILING EDGE RUDDER. REPAIRED IAW FOKKER SRM 55-02-01 PAGE 4, 55-02-07 PAGE 3 AND 51-31-01 PAGES 13 AND 14.SDR CA010510008Spar · cracked(CAN) 4 CRACKS WERE FOUND ORIGINATING FROM A 1.0 INCH DIA. LIGHTENING HOLE, 1.50 INCH BELOW UPPER RUDDER HINGE BRACKET. NOTE: REPLACEMENT SPAR WITH THE SAME P/N FROM CESSNA DOES NOT HAVE THIS LIGHTENING HOLE.SDR CALA0100322Rib · crackedINSPECTION FOUND A 1.38 INCH CRACK IN RIG PIN HOLE BOSS ON RIB WEB AT STA 56.48. A REPAIR WAS INSTALLED IAW ECRA 5530-01292, REV A PART 3.SDR QXEA0100374Rib · crackedYYC-RUDDER RIBS 3, 4, 5 CRACKED AND OR BROKEN. REPAIRED IAW FOKKER SRM 55-40-04, SRM 51-31-01, AND SRM 51-31-02.SDR QXEA0100146Rib · crackedYYC- CRACK FOUND ON RIB WEB STRUCTURE AT RUDDER BASE. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14.SDR QXEA0100145Rib · crackedYYC- RIB 6 IN RUDDER IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 PAGES 13 AND 14, 51-30-02 PAGES 9 AND 10, AND 55-40-04.SDR QXEA0100144Rib · crackedYYC- RIB 5 IN RUDDER IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 AND 14, 51-30-02 PAGES 9 AND 10 AND 51-31-05 PAGES 8, 9 AND 10.SDR CA001206008Rib · cracked(CAN) DURING AN INSPECTION THE TOP RIB OF THE RUDDER WAS FOUND CRACKED. THE CRACKS WERE LOCATED AROUND THE FORWARD ANCHOR NUT PLATES. THE RIB WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR L1GA200000540Skin · dentedDENT .027 X .250 INCH LONG LT SIDE OF RUDDER STATION XR 109, 18 INCHES FROM T/E. INSTALLED REPAIR DOUBLER.SDR L1GA200000539Skin · dentedDENT RT SIDE OF RUDDER STATION XR 97, 36 INCHES FROM TRAILING EDGE .018 X .170 INCHES LONG. INSTALLED DOUBLER REPAIR.SDR L1GA200000516Skin · dentedDENT 5 X 14 INCH ON RUDDER SKIN. INSTALLED DOUBLER REPAIR.SDR AU000724Torque Tube · worn(AUS) RUDDER TORQUE TUBE ASSEMBLY WORN BEYOND LIMITS. CHAFING MARKS ARE APPROXIMATELY 0.254MM (0.010IN) DEEP. THE MAXIMUM DEPTH PERMITTED IS 0.0762MM (0.003IN). SUSPECT CAUSE OF WEAR IS MISALIGNMENT OF THE PRESSURISATION SEAL AT INSTALLATION ALLOWING IT TO CONSDR AU000723Torque Tube · worn(AUS) RUDDER TORQUE TUBE ASSEMBLY WORN BEYOND LIMITS. CHAFING MARKS ARE APPROXIMATELY 0.254MM (0.010IN) DEEP. THE MAXIMUM DEPTH PERMITTED IS 0.0762MM (0.003IN). SUSPECT CAUSE OF WEAR IS MISALIGNMENT OF THE PRESSURISATION SEAL AT INSTALLATION ALLOWING IT TO CONSDR UPS00233540Skin · corrodedINSPECTION TYPE:C, CORROSION ON LWR RUDDER RT SKIN AT STA 120.6 IN BELOW FRONT SPAR. REPAIRED PER SRM 55-20-3 PG 1 STEP 3 & 4 AND SRM 51-40-5 PG 20 & 22 STEP 13 A-I.SDR 20000731SH008Rudder · corrodedRUDDER TAIL POST CORRODED AND BROKE JUST ABOVE LOWER RUDDER MOUNTING PIN AND FORMING TUBE BROKE OFF AT RUDDER POST. (X)SDR CA000719018Beam · cracked(CAN) FLUORESCENT LP EXAMINATION WAS CONDUCTED ON THE AIRCRAFT PILOT, COPILOT LT, RT RUDDER PEDAL TORQUE ARM RADIUS. RESULTS: COPILOT RUDDER SET REVEALED REJECTABLE CRACK INDICATIONS AS MARKED. IN SERVICE BULLETIN (PRECAUTIONARY EXAMINATION) THERE WERE NO RSDR QXEA0001409Rib · crackedPDX- RUDDER LEADING EDGE RIB NR 4 HAS A CRACK APPROXIMATELY 1.25 INCH LONG LOCATED AT LEFT HAND SIDE OF RIB. REPAIRED IAW HORIZON AIR EA 4-55-217.SDR KPVA200007Spar · dentedFORE RUDDER FRONT SPAR AT RIB 13 DENTED. REPAIRED RIB 13, FORE RUDDER FRONT SPAR IAW DHC-8 RD8-55-0870. (M)SDR QXEA0000196Rib · crackedPDX - THERE IS A 4 CRACK IN RUDDER RIB NR 4. REMOVED AND REPLACED RUDDER.SDR CA000110097Rib · cracked(CAN) RUDDER TIP RIB AND FORWARD BRACING CHANNEL WERE FOUND TO BE CRACKED DURING A 1000 HR INSPECTION. CRACKS WERE FOUND AROUND THE NUTPLATES HOLDING THE BALANCE WEIGHT ON TOP OF THE RUDDER. HARDWARE SECURING THE WEIGHT BECAME LOOSE AND WAS UNDETECTED UNTIL SDR CALA9901612Rib · crackedINSPECTION FOUND A 1 CRACK IN UPPER RUDDER AFT UPPER LEFT T/E RIB. A DOUBLER WAS INSTALLED IAW SRM 51-40-2.SDR CA991028062Spar · cracked(CAN) RUDDER SPAR CRACKED.SDR AU990923Spar · cracked(AUS) RUDDER SPAR CRACKED. REF: SEE MDR AU990922 FOR FURTHER INFORMATION.SDR AU990889Shaft · corroded(AUS) RUDDER POST CORRODED IN AREA OF LOWER BUSHING.SDR 20000622SH001Spar · crackedDURING SCHEDULED INSPECTION, FOUND RUDDER SPAR CRACKED AT UPPER LIGHTENING HOLE NEAR THE UPPER HINGE BRACKET. AFTER EXAMINATION OF 6 OTHER 152''S IN THE FLEET, FOUND 2 OTHERS WITH SIMILAR CRACKS, CESSNA SEB 94-3 PERTAINS TO THIS SUBJECT. REPLACED SPAR WITH SSDR AALA994138Spar · disbondedAFW - RUDDER FRON SPAR SKIN SHOWS DISBOND INDICATIONS AT STATION 226.5-228. CUTOUT DELAMINATION. PUT DRY CYCLE AND CUTOUT REPAIR PLYS, LAYUP AND COOK. TOP CHECK OK. (M)SDR UPS99830125Rib · crackedINSPECTION TYPE:C2, LEADING EDGE RUDDER RIB CRACKED. FABRICATED AND INSTALLED NEW RIB IAW DC8 SRM 51-1-24, 51-1-22 & 51-1- 21.SDR CA990630057Spar · cracked(CAN) THE RUDDER WAS REMOVED TO REPAIR SOME LOOSE RIVETS ON THE TORQUE TUBE, BUT A CRACK ABOUT 1 CENTIMETER LONG WAS DISCOVERED ON THE RUDDER SPAR (P/N 96-630000-307). THE SPAR WAS ALSO FOUND TO BE CRACKED IN BEHIND. THE CRACKS ORIGINATED FROM THE NUTPLATE ISDR 99ZZZX2724Bracket · crackedTHE BRACKET IS THE RUDDER BOTTOM ATTACH POINT. INTERGRANULAR CORROSION EXTENDING THROUGH THE RIVETS AND SPLITTING THE SEAM. PICTURES PROVIDED.SDR 99ZZZX2723Bracket · crackedTHE BRACKET IS THE RUDDER TOP ATTACH POINT. CORROSION APPEARS TO HAVE STARTED BETWEEN THE ATTACH POINT BRACKET AND THE AFT SPAR. EVENTUALLY CRACKING THE SPAR AND BRACKET.SDR 20000714SH009Rudder · corrodedAN INTERNAL INSPECTION OF THE RUDDER SPAR RECEIVED CORROSION. AD 78-08-09 REQUIRES AN EXTERNAL VISUAL INSPECTION EACH 300 HRS. SUBMITTER RECOMMENDED AN INTERNAL INSPECTION AT EACH ANNUAL AND FOR ALL G-164 SERIES AIRCRAFT. (X)SDR RRXA991080Fitting · damagedDURING A MAINTENANCE VISIT FOUND AN OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR=61.156. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHING IAW FAA APPROVED TIMCO DER ENGINEERING SSDR 99ZZZX1304Skin · corrodedDUIRNG A C-CHECK, CORROSION NOTED ON LOWER RUDDER LEFT SURFACE.SDR CA981230030Rib · cracked(CAN) .75 INCH CRACK FOUND ON RIGHT RUDDER UPPER RIB WHERE THE MASS BALANCE WEIGHT ATTACHES. REPLACEMENT RIB FABRICATED PER SRM AND AC43.13 GUIDELINES.SDR 99ZZZX975Spar · crackedRUDDER SPAR CRACK AT UPPER HINGE FITTING (PN 44254-501) WAS DISCOVERED DURING AN ANNUAL INSPECTION.SDR 99ZZZX387Spar · crackedWHILE COMPLYING WITH AD 93-24-03, FOUND SMALL CRACK UNDER UPPER RUDDER HINGE BRACKET. INSTALLED GENERAL FORMING DW-1 AND DW-2 BRACKETS PER STC SA00044LA. CRACK WAS NOT VISIBLE UNTIL DYE PENETRANT INSPECTION PERFORMED.SDR QXEA9801897Rib · crackedPDX - RUDDER RIB 5 CRACKED AT LEFT AND RIGHT STRINGER CLIPS. REPAIRED IAW HORIZON AIR EA 4-55-105.SDR QXEA01554Rib · crackedINSIDE THE RUDDER THE NR 5 RIB HAS 2 CRACKS PASSING THROUGH ATTACH CLIPS. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 51-31-01.SDR AU981247Rib · cracked(AUS) RUDDER TOP RIB CRACKED IN TWO PLACES EITHER SIDE OF THE BALANCE WEIGHT ATTACHMENT BOLT. PART TC: 2,294.SDR CA980928010Rib · missing(CAN) WHILE INVESTIGATING MINOR SKIN DIAMAGE, IT WAS NOTED THAT RIBS 073100-49 AND -50 WERE MISSING. ALL OF THE RIVET HOLES WERE PLUGGED WITH RIVETS.
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