Boeing 727-200
Service difficulty reports · 2,835
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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 = '727200' 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 = '727200' 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 06FDEA0588Repair · unknownFOUND REPAIR LOCATED AT STA 188, STR 27L. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0587Repair · unknownFOUND REPAIR LOCATED ON MAIN CARGO DOOR LOWER FWD EDGE REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0586Repair · unknownFOUND REPAIR LOCATED ON UPPER SURFACE OF LEFT WING AFT OF NR 4 L/E FLAP, STA 410. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0585Repair · unknownFOUND 2 REPAIRS LOCATED ON UPPER SURFACE OF RT WING AFT OF NR 6 L/E, STA 546. REPAIRS REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0584Repair · unknownFOUND REPAIR ON LEFT I/B FORE FLAP UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0583Repair · unknownFOUND REPAIR ON RIGHT OUTBOARD FORE FLAP L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0581Skin · crackedNR 2 ENGINE INLET INNER SKIN AT 12 O'CLOCK POSITION WHERE IT MEETS THE 'S' DUCT IS BENT AND CRACKED. REPAIRED NR 2 ENGINE INLET INNER SKIN AT 12 O'CLOCK POSITION IAW FED EX EA 7-7160- 96621.SDR 06FDEA0579Skin · damagedLWR FUSELAGE SKIN HAS MULTIPLE NICKS AND GOUGES BETWEEN STA 1030 AND STA 1045 FROM STR 25R TO STR 30R. BLENDED SKIN STA 1030 AND 1045 STR 25R TO 30R FABRICATED & INSTALLED REPAIR DOUBLER IAW EA 7-5330-96596. THIS IS A MAJOR REPAIR.SDR 06FDEA0577Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON LOWER RUDDER, LT SIDE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-40-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMSDR 06FDEA0576Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON RT HORIZONTAL STAB LOWER I/B SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-10-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBESDR 06FDEA0575Repair · unknownFOUND PREVIOUS REPAIR INSTALLED AT RT HORIZONTAL STAB LOWER SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 55-10-3 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, SDR 06FDEA0574Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON NR 8 LEADING EDGE SLAT UPPER SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-3 FIG 10. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBSDR 06FDEA0573Repair · unknownFOUND PREVIOUS REPAIR INSTALLED AT STA 1183, STR 24L WAS NOT ACCOMPLISHED IAW FAA APPROVED DATA. REMOVED EXISTING REPAIR AND ACCOMPLISHED REPAIR IAW SRM 53-30-3 FIG 3A, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 06FDEA0572Repair · unknownFOUND PREVIOUS REPAIR INSTALLED AT STA 1183, STR 23R WAS NOT ACCOMPLISHED IAW FAA APPROVED DATA, REMOVED EXISTING REPAIR AND ACCOMPLISHED REPAIR IAW SRM 53-30-3 FIG 3A AND SRM 51-30-2, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 06FDEA0571Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON LT INBOARD FOREFLAP LEADING EDGE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-4 FIG 1. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERSDR 06FDEA0570Repair · unknownFOUND PREVIOUS REPAIR INSTALLED AT AFT END OF TAIL SKID CUTOUT, DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL SDR 06FDEA0569Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 360, STR 13L WAS DETERMINED TO BE ACCOMPLISHED IAW E.O. 7-5100-7-2307F, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERASDR 06FDEA0568Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050, STR 27L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENESDR 06FDEA0567Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT R/H WING LEADING EDGE 12 INCHES OUTBD OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-30-4, FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESSDR 06FDEA0566Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1050, STR 27R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENESDR 06FDEA0565Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT FWD END OF AFT AIRSTAIRS CUTOUT WAS DETERMINED TO BE ACCOMPLISHED IAW SR27-53-024, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, SDR 06FDEA0564Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT AFT CUT OUT AFT AIRSTAIRS WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-10-1 AND SRM 51-30-1, PARA F, BASED ON AN EXTERNAL VISUAL EVAULATION, CONSISTS OF LOCATION, SIZE AND SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SDR 06FDEA0563Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT RIGHT WING LEADING EDGE, ON FRAME OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-10-4 FIG. 4, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTSDR 06FDEA0562Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT NR 1 LEADING EDGE SLAT , LOWER AFT SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-3 FIG.1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPASDR 06FDEA0556Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 950C, BETWEEN STRINGERS 26R AND 27R. REPAIRED PER SRM 51-40-3 MAJOR REPAIR.SDR 06FDEA0555Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 950B, BETWEEN STRINGERS 23L AND 24L. REPAIRED PER SRM 51-40-3.SDR 06FDEA0557Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 950F, BETWEEN STRINGERS 23L AND 26L. DENT FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME BS 950F BETWEEN STR 23L TO 26L USING 7075-T6 .071 M672773 PER SRM 51-40-3. FOUND TO BE A MAJOR REPAIR.SDR 06FDEA0561Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 1070, AT STR 26R. REPAIRED FRAME AT BS 1070 STR 26R IAW SRM 51-40-3.SDR 06FDEA0560Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 1050 ABOVE AND BELOW STR 26R. REPAIRED FRAME AT BS 1050 ABOVE & BELOW STR 26R IAW SRM 51-40-3.SDR 06FDEA0559Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 990, BETWEEN STR 25L AND 26L. REPAIRED FRAME AT BS 990, BETWEEN STR 25L AND 26L PER SRM 51-40-3.SDR 06FDEA0558Frame · dentedAFT CARGO BAY, FRAME UPPER FLANGE IS DENTED, BS 970, BETWEEN STR 25L AND 26L. REPAIRED FRAME BS 970 BETWEEN STR 25L AND 26L IAW SRM 51-40-3.SDR 06FDEA0553Support Fitting · gougedLEFT WING FORWARD TRUNNION SUPPORT FITTING INBOARD LUG IS GOUGED. LEFT WING FWD TRUNNION SUPPORT FITTING INBOARD LUG BLENDED, GOUGE IS WITHIN LIMITS PER FED EX EA 7-5710-96571.SDR 06FDEA0551Doubler · unknownEXTERNAL DOUBLER REPAIR APPROX 9 X 9 INCH, LT LWR FUSELAGE STA 680 TO 690 STRINGER 28L REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED & REPLACED REPAIR DOUBLER PER SRM 53-30-3.SDR 06FDEA0517Frame · misdrilledBS 990 FRAME HAS A FIGURE 8 HOLE AT STR 5 RT. REPAIRED FRAME AT BS 990 IAW SRM 53-10-4.SDR 06FDEA0514Stiffener · corrodedSTIFFENER BETWEEN BS 849 - BS 870, STR 3R-STR 4R, HAS SURFACE CORROSION. BS 849 - 870 STR 3R TO 4R, FOUND ONLY SLIGHT SURFACE CORROSION WITHIN LIMITS PER SRM 53-10-1.SDR 06FDEA0513Frame · corrodedCORROSION, UPPER FUSELAGE, BS 740 FRAME, AFT SIDE, STR 3L ATTACH CLIP HAS CORROSION. BS 740 FRAME, AFT SIDE STRINGER 3L CLIP CORROSION REMOVAL WITHIN LIMITS PER SRM 53-10-1.SDR 06FDEA0516Floorbeam · misdrilledWHILE WORKING CUST CARD N01118 DISCOVERED DBL DRILLED HOLES IN FLOORBEAM UPPER CHORD AT BS 740 LBL 45 WL 208. FLOOR BEAM UPPER CHORD AT BS 740 LBL 45 WL 208 REPAIRED IAW SRM 53-10-4SDR 06FDEA0508Repair · unknownSKIN REPAIR DOUBLER, 15" X 10" LOCATED AT BS 367-378, STR 27L, REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REINSTALLED PER E.O. 7-3450-7-3393SDR 06FDEA0506Stringer Clip · corrodedSTA 720C STR 2R, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA0505Stringer Clip · corrodedSTA 720C STR 2L, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA0504Stringer Clip · corrodedSTA 720C STR 1, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA0503Stringer Clip · corrodedSTA 720C STR 4L CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA0502Stringer Clip · corrodedCORROSION ON STRINGER CLIP BS 640 STR 6 RT. REMOVED AND REPLACED STRINGER CLIP IAW SRM 53-10-1, 51-30-2.SDR 06FDEA0501Stringer Clip · corrodedCORROSION ON STRINGER CLIP BS 640 STR 8RT . REMOVED AND REPLACED STRINGER CLIP IAW SRM 53-10-1, 51-30-2.SDR 06FDEA0500Stringer Clip · corrodedCORROSION STRINGER CLIP BS 640 S7R. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-1, 51-30-2.SDR 06FDEA0498Stringer Clip · damagedSTA 540 STR 7R, OPEN HOLES IN STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2.SDR 06FDEA0497Floorbeam · corrodedCORROSION ON FLOORBEAM STA 440, RBL 10, WL 208. REPAIRED FLOORBEAM IAW SRM 53-10-1, 53-10-4, 51-30-02.SDR 06FDEA0507Floorbeam · tool damageTOOLING DAMAGE ON FLOORBEAM BS 720F BBL0 WL 207. REPAIRED FLOOR BEAM AT 720F BL 0 WL 207 PER FED EX EA 7-5310-99423.SDR 06FDEA0499Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT FS 500 STR.30 WAS ACCOMPLISHED IAW SRM 53-30- 3, FIG. 24 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION OF THE REPAIR, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE, THICKNESS, GENERAL WORKMANSHSDR 06FDEA0493Stringer Clip · corrodedSTA 720C STR 3L, CORROSION ON STRINGER CLIP. REPLACED STRINGER CLIP PER SRM 51-30-2.
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