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 = '72729' 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 = '72729' 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 96ZZZM486Floor Beam · corrodedDURING C-CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT STATION 560 BETWEEN RBL 45.5 AND RBL 24.75. REMOVED DAMAGED AREA PER SRM 53-10-8 AND INSTALLED REPAIR PER SRM 53-10-8 FIG 3. ALODINED AND PRIMED AREA PER SRM 52-10-2. SIZE 27 INCH 7075-T6 AND SIZE 27 SDR 96ZZZM485Skin · missingDURING C-CHECK, FOUND SECTION OF FUSELAGE SKIN MISSING APPROX 3 SQUARE INCHES AT AFT AIRSTAIR CUT OUT FWD LEFT CORNER. REMOVED FASTENERS PER SRM 51-30-2, CUT OUT PER SRM 51-10-1, INSTALLED FILLER REPAIR PER SRM 53-30-3 4.5 INCH BY 1.75 INCH 2024-T3 .40 INCH.SDR 96ZZZM484Skin · wornDURING C-CHECK, FOUND AT STATION 178 TOP SKIN DOUBLER JUST AFT OF RADOME HINGES, DOUBLER L/E IS BENT UP AND WORN THIN AT EDGES ONLY. REPLACED SKIN DOUBLER AS PER SRM 51-10-1 PAR 4.SDR 96ZZZM483Angle · corrodedDURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT ANGLE CORRODED, ATTACHED TO CREASE BEAM WEB BS 836 TO BS 850 RBL 65. CUT OUT DAMAGE AREA PER SRM 51-10-1 AND INSTALLED NEW ANGLE PER SRM 51-10-1 PAGE 4 ON BS 836 AND BS 850 RBL 65 27.5 INCH BY 2 INCH BY 2 INCH 7SDR 96ZZZM482Seat Track · corrodedDURING C-CHECK, FOUND SEAT TRACK EXTRUSION AT RBL 45.5 CORRODED BETWEEN STATION 480 AND STATION 600. REMOVED DAMAGED SEAT TRACK AND REPLACED SEAT TRACK IAW SRM 51-10-1 PAR 4 AND SRM 51-30-2.SDR 96ZZZM481Skin · dentedDURING C-CHECK, FOUND SKIN DENTED BELOW LAP SEAM STRINGER 18L, STATION 203.8. CUT OUT DAMAGED AREA 3 INCH BY 4 INCH, INSTALLED EXTERNAL DOUBLER 2024-T3 .050 11 INCH BY 11 INCH AS PER SRM 53-30-3, SEALED EDGE WITH PRC PER SRM 51-20-4.SDR 96ZZZM480Skin · dentedDURING C-CHECK, FOUND SKIN HAS DENT AT APPROX STATION 270 STRINGER 20R ABOVE EXTERIOR POWER DOOR. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER 2024-T3 .050 3 INCH BY 13 INCH, REPAIR FILLER 3 INCH BY 3 INCH 2024-T3 .040 IAW SRM 53-30-3. TREATED AND PRIMED SDR 96ZZZM478Angle · corrodedDURING C-CHECK, FOUND FORWARD SERVICE DOOR 'Z' ANGLE UNDER THRESHOLD HAS CORROSION FULL LENGTH. CUT OUT DAMAGED AREA OF 'Z' ANGLE 26 INCHES APPROX, ALODINED AND PRIMED AREA PER SRM 51-10-6. INSTALLED NEW ANGLE 7075-T6 .080 1.25 INCH BY 1 INCH BY 26 INCH PER SDR 96ZZZM477Door Frame · crackedDURING C-CHECK, FOUND MCD SUPPORT ANGLE AND DOOR FRAME CRACKED AT FWD ACTUATOR AREA NEAR HINGE. REMOVED SUPPORT ANGLE AND DOOR FRAME PER SRM 51-30-2. INSTALLED NEW ANGLE PER SRM 51-10-1 PAGE 4 AND FABRICATED AND INSTALLED NEW FRAME SECTION PER SRM 51-40-3. SDR 96ZZZM476Angles · crackedDURING C-CHECK, FOUND MCD FORWARD AND AFT SUPPORT ANGLES CRACKED IN AFT ACT, CUT OUT AREA NEAR HINGE. REMOVED CRACKED ANGLES FWD AND AFT PER SRM 51-30-2. FABRICATED AND INSTALLED NEW ANGLE SUPPORT AT FWD AND AFT POSITION 4 INCH BY 2 INCH BY 1 INCH, 7075-T6 PSDR 96ZZZM475Angle · crackedDURING C-CHECK, FOUND SUPPORT ANGLE FOR KEEL BEAM TO BS 870 WEB CRACKED. REMOVED AND REPLACED SUPPORT ANGLE FOR KEEL BEAM RT SIDE TO BS 870 AS PER SRM 51-10-1 PAR 4 AND 51-30-2. REINSTALLED PANELS PER SRM 51-30-2.SDR 96ZZZM474Web · crackedDURING C-CHECK, FOUND RIGHT AFT STAIRWELL AREA, VERTICAL WEB OF LOWER TORQUE BOX CRACKED APPROX .75 INCH FROM OUTBOARD TO INBOARD AT STATION 1263. INSTALLED TYPICAL WEB REPAIR AS PER SRM 51-40-2 AT VERTICAL WEB OF LOWER TORQUE BOX STATION 1263. MATERIAL 7075SDR 96ZZZM473Beam · crackDURING C-CHECK, FOUND RIGHT AFT STAIRWELL AREA APPROX .25 INCH CRACK RUNNING FROM UNDER DOUBLER ON UPPER FRAME BEAM OF LOWER RIGHT TORQUE BOX, JUST BELOW ACTUATOR BRACKET AT APPROX STATION 1273. INSTALLED DOUBLER OVER STOP DRILL HOLE. DOUBLER 7075-T6 .063 PESDR 96ZZZM472Chord · corrodedDURING C-CHECK, FOUND AFT CABIN, REINFORCEMENT CHORD IS HEAVILY CORRODED AT FS 1176.9 AT LBL 63 UPPER SIDE OF CHORD. CUT OUT DAMAGED AREA AT LBL 50.5 AND INSTALLED NEW CHORD ANGLE AND SPLICE AS PER 95PMSI067D-1.SDR 96ZZZM470Floor Web · crackedDURING C-CHECK, FOUND AFT CABIN, CURVED FLOOR WEB BETWEEN FS 1176.9 CHORD AND FS 1183 BULKHEAD CRACKED, JUST FORWARD OF WIRE BUNDLE CONDUIT AT RBL 31. STOP DRILL CURVED FLOOR PER SRM 51-10-1 AND INSTALLED DOUBLER PER SRM 51-40-2, 3 INCH BY 2 INCH 2024-T3 .032SDR 96ZZZM469Bracket · crackedDURING C-CHECK, FOUND RT WING NR 7 LEADING EDGE SLAT ACTUATOR INBOARD VERTICAL MOUNT BRACKET CRACKED AT UPPER END. REPLACED MOUNT BRACKET DOUBLER PER SRM 51-40-2 7075-T6 7 INCH BY 3 INCH .100 AND SRM 51-30-2.SDR 96ZZZM468Angle · crackedDURING C-CHECK, FOUND LEFT MAIN GEAR UPLOCK SUPPORT FITTING SUPPORT ANGLE CRACKED BS 910 BETWEEN STRINGER 18 AND 18R. COMPLIED WITH BOEING SERVICE BULLETIN 727-53-165 INSTALLED FRAME MODIFICATION AT BS 910 AND 913.5 BETWEEN STRINGER 18A AND 18, LEFT MAIN W/W.SDR 96ZZZM467Keel Beam · crackedDURING C-CHECK, FOUND LEFT W/W KEEL BEAM WEB CRACKED FWD OF APU CUTOUT. CUT OUT DAMAGED AREA AND INSTALLED WEB REPAIR AS PER SRM 51-40-2 .063 7075-T6 4 INCH BY 13 INCH.SDR 96ZZZM466Skin · crackedDURING C-CHECK, FOUND MCD INNER SKIN CRACKED UNDER PRESSURE SEAL AT FWD AND AFT UPPER CORNERS. REMOVED FWD AND AFT CORNERS. INSTALLED NEW CORNER AT FWD AND AFT POSITION AS PER SRM 51-10-1 PAR 4. CLOSED INNER SKIN PER SRM 51-30-2.SDR 96ZZZM465Frame · bentDURING C-CHECK, AFT LOWER DOUBLER DAMAGED/BENT MCD FRAME OPENING. REPLACED DAMAGED DOUBLER WITH 7075-T6 .063 4 INCH BY 6 INCH AS PER SRM 51-40-2 AND 51-30-2. SEALED WITH PRC PER SRM 51-20-4.SDR 96ZZZM464Angle · crackedDURING C-CHECK, AFT STAIRWELL LOWER RT TORQUE BOX INBOARD CHORD ANGLE CRACKED 6 INCHES IN RADIUS RUNNING AFT FROM UNDER STAIR ACTUATOR BRACKET AT APPROX STA 1273. REPAIRED ANGLE AS PER SRM 51-40-3. RE-ASSEMBLED AFT AIRSTAIR ACTUATOR AND STRUTS IAW MM 52-62-7SDR 96ZZZM463Angle · corrodedDURING C-CHECK, FOUND FORWARD EXTERIOR DOOR UNDER THRESHOLD 'U' ANGLE HAS CORROSION SEVERAL PLACES. REMOVED PANEL PER MM 53-20-11. CUT OUT DAMAGED SECTION AND REMOVED CORROSION PER SRM 51-10-6. REMOVED AND REPLACED U-CHANNEL PER SRM 51-10-1 PAGE 4 AND INSTASDR 96ZZZM462Floor Panel · corrodedDURING C-CHECK, FOUND CORROSION ON AND UNDER COCKPIT FLOOR PANEL AT F/E RT SEAT TRACK. REPLACED SEAT TRACK SUPPORT ANGLE AND CORRODED FLOOR PANEL PER SRM 51-10-1 PAR 4 AND SRM 51-30-2.SDR 96ZZZM461Skin · crackedDURING C-CHECK, FOUND LEFT WING LEADING EDGE OUTBOARD OF LANDING LIGHT DENTED. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR 7075-T6 .071 AND .063 9 INCH BY 9 INCH. FILLER 2 INCH BY 4 INCH AS PER SRM 57-30-4. SEALED WITH RTV PER SRM 51-20-4.SDR 96ZZZM460Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 540 RT SIDE. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 8 INCH BY 1 INCH AS PER SRM 51-40-3 AND 51-30-2.SDR 96ZZZM459Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 560 RT SIDE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 8 INCH BY 1 INCH AS PER SRM 51-40-4 AND 51-30-2.SDR 96ZZZM458Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 580 RT SIDE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 6 INCH BY 1 INCH AS PER SRM 51-40-3 AND 51-30-2.SDR 96ZZZM457Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 600 RT SIDE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 8 INCH BY 1 INCH AS PER SRM 51-40-3 AND 51-30-2.SDR 95ZZZW85Switch · dirtyNOSE GEAR DOOR LIGHT DOES NO ILLUMINATE DURING GEAR EXTENSION (ON S/O PANEL). CLEANED AND LUBED NOSE GEAR DOOR SWITCH PLUNGERS LIGHTS AND SWITCHES, OPS CKS GOOD.
Back to Boeing 727-29