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 aircraft_model_key = '72721' 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 aircraft_model_key = '72721' 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 FDEA200906202191Fitting · crackedINSIDE THE NR 1 PYLON RT SIDE HAS CRACKED ON THE TOP CORNER OF FITTING P/N 311N5220-56 AT PP STA 186. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 96 AND DWG 311N5044 SHEET 5 REV. C. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.SDR 2006FA0000814Frame · damagedDURING SCHEDULE INSP REQUIRED BY AD, FOUND 8.5 WEB SEPARATION AT FUSELAGE BS 950, RT BETWEEN STRINGER S-9 AND S-10. PARTIAL FRAME REPLACEMENT BETWEEN S-9 AND S-12 WAS ACCOMPLISHED. INSTALLED KIT NR 65C35283-2. ALL WORK DONE IAW DWG, SRM, SB, AND AD. (K)SDR RYN2004F00026Actuator · splitAFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. GREEN LIGHT ON, RED L DOOR LIGHT OUT, AND HYDRAULIC PRESSURE NORMAL. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR. OPERATIONAL CHECK OF THE LANDING GEAR NORSDR MP011603BSpar · corrodedDURING AD COMPLIANCE, A CLOSE VISUAL AND NDT HFEC INSP OF WING REAR SPAR, A CRACK AND CORROSION WAS FOUND IN THE HEEL OF THE INBOARD PORTION OF THE DETERMINED TO BE OUT OF LIMITS IAW MFG SRM. ENGINEERING WAS CONTACTED AND REPAIRS WERE DRAWN. A SECTION OF THESDR 2003F00340Support · corrodedLEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM, AFT LOWER FLANGE, AT 21 INCHES AND 30 INCHES FROM INBOARD END. ELEVATOR STATION 17.20 TO 47.20, CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-06. (M)SDR 2003F00338Support · corrodedLEFT HORIZONTAL STABILIZER, INTERGRANULAR CORROSION ON AFT LOWER SUPPORT BEAM UPPER FORWARD FLANGE, 27 INCHES FROM INBOARD END AT ELEVATOR STATION 17.20 TO 44.20 CUTOUT CORRODED AREA PER SRM 51-10-1. REPAIRED PER SRM 55-10-6. (M)SDR 2003F00346Bearing · wornLOWER RUDDER TRIM TAB BEARINGS WORN. REMOVED AND REPLACED ROD END BEARINGS IAW MM 27-20-0. (M)SDR 2003F00349Housing · wornLEFT ELEVATOR BEARING HOUSING POSITION NR 4 AND NR 7 WORN BEYOND LIMITS. REMOVED AND REPLACED NR 4 AND NR 7 BEARING HOUSING ASSEMBLIES IAW MM 27-30-5. (M)SDR 2003F00341Housing · wornRIGHT ELEVATOR BEARING HOUSING, POSITIONS NR 5 AND NR 7 WORN BEYOND LIMITS. REMOVED AND REPLACED NR 5 AND NR 7 BEARING HOUSING ASSEMBLIES IAW MM 27-30-5. (M)SDR 2003F00348Bracket · corrodedLEFT ELEVATOR, INBOARD TRIM BRACKET, HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED BRACKET PER SRM 51-10-1. (M)SDR 2003F00347Skin · corrodedPBI - EXFOLIATED CORROSION AT BS 660, RIGHT LAP JOINT STRINGER 19. REMOVED CORROSION, REPAIRED PER SRM 53-30-3, FIG 5 AND 27. (M)SDR 2003F00352Duct · corrodedCORROSION ON SKIN OF NR 2 'S' DUCT AT RIB STATIONS 9, 10, 12, 16, 17, 27, 30, 37 AND 38. REMOVED CORROSION AND REPAIRED WITH EXTERIOR SKIN REPAIRS IAW SRM 54-10-3. (M)SDR 2003F00246Line · crackedIN LEVEL CRUISE FLIGHT FROM DAY TO PHX, COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. PERFORMED ALL RYAN 'A' SYSTEM HYDRAULIC LOSS CHECKLIST. EMERGENCY DECLARED. AIRCRAFT LANDED PHX WITHOUT INCIDENT. REMOVED AND REPLACED SPOILER RETURN LINE. (M)SDR 2003F00247Line · crackedON DESCENT INTO RDU, SYSTEM PRESSURE WAS LOST ON 'A' SYSTEM HYDRAULICS. EMERGENCY WAS DECLARED AND EMERGENCY CHECKLIST WAS COMPLIED WITH. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR PRESSURE LINE. (M)SDR 2002F00115Frame · corrodedFOUND LOWER END OF FRAME AND BRACKET AT STATION 312 RBL 40 EXFOLIATED. (M)SDR 2002F00114Skin Panel · corrodedFOUND FUSELAGE SKIN PANEL CORRODED AT STATION 320 STRINGER 19R. (M)SDR LCQ05Wedge · damagedRIGHT WING OUTBOARD FWD FLAP T/E WEDGE COMPOSITE HAS DELAMINATION AND 17 FT 2 INCHES OF THE SECTION OF WEDGE MISSING AND 42 INCHES OF HONEYCOMB REMAINING.SDR 2002F00116Wedge · damagedFOUND RIGHT WING OUTBOARD FORWARD FLAP TRAILING EDGE WEDGE COMPOSITE HAS DELAMINATION AND APPROXIMATELY 75 PERCENT OF THE SECTION OF WEDGE IS MISSING. (M)SDR 2003F00339Flap Track · crackedRIGHT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK ON FUSELGE IS CRACKED AT WBL 70.597. REMOVED AND REPLACED RIGHT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK. (M)SDR 2003F00335Spar · corrodedLEFT WING FRONT SPAR UPPER CAP, LOWER LEG, HAS CORROSION AT WS 222.0 AND 224.5. CORROSION FOUND OUT OF LIMITS. REPAIRED SPAR PER DRAWING RFB275710-122601. (M)SDR 2003F00334Skin · delaminatedLEFT INBOARD FORE FLAP DELAMINATED AT TRAILING EDGE JUST ABOVE MIDDLE TRACK. REMOVED FLAP, REPAIRED IAW B727 MM 27-51-11. REINSTALLED FLAP. (M)SDR 2003F00333Flap Track · crackedLEFT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK ON FUSELAGE IS CRACKED IN SEVERAL PLACES AT WBL 70.5. REMOVED AND REPLACED ROLLER BEARING TRACK. (M)SDR 2003F00336Flap Track · crackedLEFT WING NR 4 FLAP TRACK FAIRING OUTBOARD TRACK, BEARING GUIDE, CRACKED. REMOVED AND REPLACED TRACK IAW B727 SRM 51-10-01. (M)SDR 2002F00274Doubler · dentedFOUND DENT IN CARGO DOOR DOUBLER AT BS 540 TO BS 560 STRINGER 19L AND 20L. REPAIRED FUSELAGE SKIN AT BS 540 TO BS 560 STRINGER 19L AND 20L IAW SIDE REPAIR DRAWING 1-10-8-01 AND 727 SRM 51-30-2. 2024-T3 .050 INCH 16.5 INCH BY 14.5 INCH AND 2024-T3 .100 INCH 1SDR 2001F00464Skin · damagedRIGHT HORIZONTAL STABILIZER UPPER SURFACE SKIN DAMAGED AT INBOARD END AFT OF LEADING EDGE SKIN. (M)SDR 2001F00428Door Frame · crackedMAIN CARGO DOOR CUTOUT, FORWARD FRAME SKIN HAS A CRACK APPROXIMATELY AT BS 502 ABOVE STRINGER 14L. (M)SDR 2001F00426Skin · corrodedFOUND FUSELAGE UPPER LOBE INTERIOR WING CENTER SECTION UPPER SKIN HAS CORROSION AT RBL 24-45.5 BETWEEN STATION 740 AND 870. ACCOMPLISHED WING CENTER SECTION UPPER SKIN CORROSION REPAIR AT STATION 752 BETWEEN STRINGER 20C AND STRINGER 21C IAW AVHM-2430RO-1 REVSDR 2001F00465Rub Strip · bulgedVERTICAL STABILIZER UPPER FORWARD RUB STRIPS, FOR HORIZONTAL STABILIZER PATH, HAS BULGED AREAS ON BOTH RIGHT AND LEFT SIDES. (M)SDR 2002F00861Attach Fitting · crackedWING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP, SMALL ANGLE, CRACKED AT BS 870 AND BBL 0. (M)SDR 2002F00688Frame · corrodedFOUND STATION 351 HAS CORROSION AT LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M)SDR 2002F00687Structure · corrodedFOUND FS 344 HAS CORROSION ON LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M)SDR 2002F00686Frame · corrodedFOUND STATION 351 HAS CORROSION AT LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M)SDR 2002F00685Frame · corrodedFOUND CORROSION AT STATION 351 AFT SIDE UNDER FRAME CHORD 6 INCHES INBOARD OF STRINGER 26L. (M)SDR 2001F00463Doubler · crackedCABIN FUSELAGE STATION BS 480 STRINGER 17L LOWER FLOORBEAM ANGLE STRAP REPAIR CRACKED. (M)SDR 2001F00462Frame · corrodedFUSELAGE STATION 351 FRAME LOWER FLANGE INBOARD OF STRINGER 26R HAS CORROSION. (M)SDR 2001F00409Clip · crackedWING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP (SMALL ANGLE) CRACKED AT BS 870 AND BBL 0. REMOVED AND REPLACED ATTACH CLIP IN WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD BS 870 AND BBL 0 AS PER B727 SRM 51-30-2. (M)SDR 2002F00717Stringer · crackedFOUND LOWER CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 STRINGER 20L SHOWS CRACK TO CENTER. ALSO, BS 700 FRAME TIED TO FUSELAGE IS CRACKED FROM TOP FASTENER. (M)SDR 2002F00707Pressure Panel · corrodedFOUND NOSE WHEEL WELL STATION 312 TO STATION 285 LEFT VERTICAL WEB LOWER EDGE HAS CORROSION ON OUTBOARD SIDE. (M)SDR 2001F00461Fitting · corrodedNOSE LANDING GEAR DRAG SUPPORT FITTING HAS CORROSION ON LOWER SURFACE. (M)SDR 2001F00429Stringer · crackedLOWER FORWARD CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 STRINGER 20L SHOWS CRACK TO CENTER. ALSO, BS 700 FRAME TIED TO FUSELAGE IS CRACKED FROM TOP FASTENER. INSTALLED STRINGER REPAIR AT LOWER FORWARD CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 AT STRINGERSDR 2002F00709Frame · crackedFOUND FRAME LOWER FLANGE CRACKED AT STATION 320 BELOW STRINGER 26R. (M)SDR 2002F00708Frame · corrodedFOUND FRAME LOWER FLANGE HAS CORROSION AT STATION 312 BELOW STRINGER 26R. (M)SDR 2002F00691Pressure Panel · corrodedNOSE WHEEL WELL STATION 285 TO STATION 312 RIGHT VERTICAL WEB LOWER EDGE HAS CORROSION ON OUTBOARD SIDE. (M)SDR 2002F00690Pressure Panel · corrodedNOSE LANDING GEAR WHEEL WELL STATION 328 TO STATION 351 RIGHT VERTICAL WEB HAS CORROSION ON INBOARD SIDE LOWER EDGE. (M)SDR 2002F00689Pressure Panel · corrodedNOSE LANDING GEAR WHEEL WELL STATION 328 TO 351 LEFT VERTICAL WEB HAS CORROSION ON INBOARD SIDE LOWER EDGE. (M)SDR 2002F00697Floor Support · corrodedFOUND CORRODED COCKPIT FLOOR SUPPORT ANGLE AT BS 295 RBL 10 INCHES. (M)SDR 2002F00696Floor Panel · corrodedFOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL FROM BS 259.5 TO BS 282.5 AT LBL 8. (M)SDR 2002F00695Floor Panel · corrodedFOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL BS 259.5 FROM RBL 0 TO 12 AND FROM LBL 0 TO LBL 32. (M)SDR 2002F00694Floor Panel · corrodedFOUND CORROSION ON UNDERSIDE OF COCKPIT FLOOR PANEL NR 2301. (M)SDR 2002F00693Floor Panel · corrodedFOUND CORROSION ON COCKPIT FLOOR PANEL 2303, UNDER FACE. (M)
Back to Boeing 727-21