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 = '5700' 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 = '5700' 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 CALA2021121002329None · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 12/07/2021. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00115, HANGER IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SESDR CALA2021121002328None · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 54.60 ACCOMPLISHED BY V905004 INSPECTED BY V912634 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL. SEE NSA EMX N/R 0012SDR MASA20211213608None · noneTHE L/H WING T/E STRUCTURE SUPPORT FITTING AT SPS 43.60 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 REO 670-57-51-341 AND SRM 51-26-00, 51-12-00.SDR CALA2021120802302Skin · crackedSUPPORT TASK- EA5725-01003 OP005 AD2018-11-14, 1EA CODE ''A'' FASTENER HOLE FOUND CRACKED AT LHW STR L-6.5 TRANSFER REF. NR LP 9131047 ORIGINATED BY EMP V924732 INTERVALS NOT TO EXCEED 12,000 CYCLES OR 32,000 FH''S (WHICHEVER COMES FIRST) THERE AFTER. DIP REQUSDR SWIA202163792None · damagedLH AILERON CENTER, OB HINGE LUG DAMAGED. (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON LEFT HAND AILERON OUTBD HINGE LUG PER MHIRJ REO 670-57-61-379 REV. -- DATED:2021-12-08. NO FURTHER ACTION REQUIRED AT THIS TIME. PLEASE REFER TO CONTINUATION CARD FOR SDR MASA20211213614None · dentedTHE RH WING OUTBOARD RIB AT WS 281.50 WAS FOUND WITH A DENT AT THE LOWER FLANGE OF THE RIB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-26-01, SRM 57-53-02-101-001-A01/57-53-01-101-001SDR MASA20211213612None · dentedDENT DAMAGE WAS FOUND ON RH WING OTBD FLAP LOWER SKIN. DENT WAS LOCATED ON OTBD AFT END AT WS 281.50 & MEASURED 7.779" LONG X 3.228" WIDE X0.120". PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-53-01-201-001-A01 TYPE II REPAIR-OUTBOARD FLAP SKINS-FLUSH REPAIRS.SDR CALA2021120802301Seal · missingLH WING MIDSPAN FIXED TRAILING EDGE FLEX PANEL END SEALS FOUND SEAL DAMAGED SEAL REPLACED IAW AMM DMC-B787-A-57-51-05-00A-520A-A, DMC-B787-A-57-51-05-00A-520A-A SEAL REPLACED IAW AMM DMC-B787-A-57-51-05-00A-520A-A, DMC-B787-A-57-51-05-00A-520A-ASDR CALA2021120802297Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED.SDR CALA2021120802296Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED.SDR CALA2021120802295Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACKED.SDR CALA2021120802293Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL15.04 IS CRACKED.SDR CALA2021120802292Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL40.87 IS CRACKED.SDR CALA2021120802298Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED.SDR CALA2021120802294Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED.SDR CALA2021120802289Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKED.SDR CALA2021120802288Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED.SDR CALA2021120802287Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED.SDR SWIA202164961None · corrodedLH WING SPOILERON HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SPOILERON HINGE AND KEEPER HARDWARE AS NEEDED IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202164960None · corrodedLH WING FLIGHT SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH FLIGHT SPOILER HINGE AND KEEPER HARDWARE AS NEEDED IAW CRJ-200 AMM 27-64-05-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202164958None · corrodedLH WING IB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) INSTALLED NEW HARDWARE ON LH WING IB GROUND SPOILER IAW CRJ 200 AMM 27-65-01-400-801SDR SWIA202164956None · corrodedLH WING OB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH OB GROUND SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202164955None · corrodedRH WING IB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH IB GROUND SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202164954None · corrodedRH WING OB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) INSTALLED SERVICEABLE HARDWARE IAW CRJ 27-65-01-400-801. REFERENCE CAMP #23963983 FOR OPS CHECKS.SDR SWIA202164953None · corrodedRH WING FLIGHT SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH FLIGHT SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-64-05-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202164951None · corrodedRH WING SPOILERON HINGE HARDWARE AND KEEPER PLATE HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVE AND REPLACED CORRODED HARDWARE ON RH SPOILERON HINGE AND KEEPER PLATE IAW CRJ-200 AMM 27-64-01-00/400-801.SDR JR2R20211206357Spar · corrodedRH SPAR 1 CORRODED AT WINGTIP ATTACH POINTSDR SWIA202164347None · corroded*ATTACH ANGLE IN L/H INBD WING DRY-BAY HAS AREA OF CORROSION. LOCATION IS IN THE WHEEL WELL OTBD FWD AREA. (C-CHECK RO 2/16/2022) REMOVED AND REPLACED ATTACH ANGLE IN LH INBD WING DRY BAY. REF CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ 900 SRM 51-42-06-00SDR SWIA202164235None · damagedINDICATIONS NOTED ON THE RH LOWER WING PLANK AROUND THE CIRCUMFERENCE OF THE LAND FOR ACCESS PANEL 650BB 100% FULL SCREEN HEIGHT FAILING NDT. (C CHECK RO 2-11-2022) REPAIRED CORROSION ON RH LOWER WING PLANK AROUND THE CIRCUMFERENCE TO INCLUDE IN THE CRITICSDR DALA2021121007630None · noneSHIP 691 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589445-14 REV A. CORRECTIVE ACTION: REF ERA 589445-14 REV A. (2038125)SDR DALA2021121007628None · noneSHIP 6808 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589123-14 REV A. CORRECTIVE ACTION: REF ERA 589123-14 REV A. (2037100)SDR REXA2021120701122Fitting · wornBUSHING LUGS ON RH AILERON LABELED B, C, F AND G WORN. AIL STA 338.424 - 342.123 C/A: REPAIRED LUGS IAW MHIRJ REO 670-57-61-237 REV --, DATED 2017-07-25 & REO 690-57-61-237 REV--, DATED 2021-10-20.SDR IXXA20220111001Rib · noneLW L/E AIR LOAD RIB FORMER AT LES 441 IS BENT AND HOLES ARE ELONGATEDSDR FDE2022F00000None · crackedDURING E.A NO.T6-5710-114908 B P2 FOUND HOLE 6 LHS DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-114908 C P4 (SEQ NO: 000895) AND A300-600 SRM 5SDR FDEA202111292949None · crackedDURING E.A NO.T6-5710-114908 B P2 FOUND HOLE 6 LHS DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-114908 C P4 (SEQ NO: 000895) AND A300-600 SRM 5SDR UIEA2021111902426None · noneLT WING INBD MAIN FLAP LOWER SURFACE LOWER SKIN PANEL HAS SEVERAL BULGING AREAS , APPROX 33" FROM THE INBD END DOT 129-054(<P>BLENDED THE CORROSION ON THE "T" CHORD IAW B767-300 SRM 51-10-02. UPON THE EVALUATION THE LOWEST REMAINING MATERIAL IS 0.062" AND WASDR SWIA202163998None · corrodedFWD JACK FITTING SUPPORT WEB RH CORRODED IN MULTIPLE SPOTS (C-CHECK RO 1/19/2022) CORROSION ON FWD JACK FITTING RH SUPPORT WEB FOUND TO BE OUT OF LIMITS. REPLACED SUPPORT WEB REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01, AND DWSDR JJBA20211124046Unknown · unknownRIVET FOUND ON LEADING EDGE II RH. DENT AT RIVET LOCATION OF LEADING EDGE II RH FOUND OUT OF LIMITS AND NEEDS REPAIR PARTS FOR REPAIR SPLICE AND FILLER FABRICATED. REPAIR SPLICE AND FILLER INSTALLEDSDR 2021F00364Skin · corrodedCORROSION ON LEFT WING TIP UPPER SKIN P/N 6923140-3. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ32554 - DATED NOVEMBER 20, 2021; 680A-0053 N515QS REPAIR RECOMMENDATION.SDR 2021F00363Skin · corrodedCORROSION ON LEFT WING TIP LOWER SKIN P/N 6923150-3. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ32552 - DATED NOVEMBER 20, 2021; 680A-0053 N515QS REPAIR RECOMMENDATION.SDR FDEA202111232926Slat · delaminated#6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED SLAT PER B757 AMM 27-81-01-4SDR SWIA202163981None · corroded* FWD JACK FITTING SUPPORT WEBS CORRODED IN MULTIPLE SPOTS (MARKED) (C-CHECK RO 1/19/2022) REMOVED AND INSTALLED NEW LH WEB AT FWD JACK FITTING SUPPORT REF-CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01 AND DGW DWG: CC670-32050 SDR DALA2021112907317None · noneSHIP 6713 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 586380-14 REV A. CORRECTIVE ACTION: REF ERA 586380-14 REV A. (2026726)SDR SWIA202164225None · elongatedRIGHT HAND WING PANEL 684CB HAS AN ELONGATED FASTENER HOLE IN IT AND IN SUPPPORTING STRUCTURE. (C CHECK RO 2-11-2022) REPAIRED RH INBOARD FLAP AT PANEL 684CB IAW MHIRJ REO 601R-57-2441 REV -- DATED 2022-01-27. ATTACHED COMPLETED MAJOR REPAIR TASK CARD 51-SDR REXA2021122701188Fitting · gougedINSPECTED THE L/H WING AILERON BUSHING BORE AT WS 343.50 AND FOUND DAMAGE TO THE TOP CENTER OF THE O/B BUSHING BORE. - FOUND L/H WING AILERON BUSHING BORE TOP CENTER OF THE I/B BUSHING BORE REPAIRED BORE IAW MHIRJ 670-57-51-455, REV.A DATED 2021-11-10.SDR SWIA202165216None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW 8EA BUSHINGS FROM THE RH AILERON REAR SPAR HINGE POINTS REF CRJ 200 AMM 20-26-00-910-802 , CRJ200 ASDR SWIA202165215None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3-25-22) REMOVED AND REPLACED BUSHINGS ON L/H AILERON WING AFT SPAR, REF. CRJ-200 AMM 20-26-00-910-804. SEE CONTINUATION FOR WORK PERFORMED.SDR SWIA202165102None · wornREMOVE & REINSTALL RH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM 27-15-01-000-801. COMPLY WITH TASK CARD 27-900-1001-SKY (C-CHECK RO 3/14/2022) REMOVED & INSTALLED NESDR SWIA202165101None · wornREMOVE & REINSTALL LH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM 27-15-01-000-801. COMPLY WITH TASK CARD 27-900-1001-SKY (C-CHECK RO 3/14/2022) REMOVED & REINSTALLED SDR SWIA202165100None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3/14/2022) REMOVED AND REPLACED BUSHINGS WITH 15 EA NEW BUSHINGS RIGHT AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804. HARDWARE REPL
Back to JASC 5700