Boeing 727-200
Service difficulty reports · 2,835
Newest first. General aviation reporting is voluntary.
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 02FDEA00785Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 950B, STR 29R.SDR 02FDEA00770Frame · wornBS 1352 T-CHORD AFT FLANGE IS WORN IN SEVERAL LOCATIONS FROM 3-9 O'CLOCK AND KNIFE EDGED AT 5 O'CLOCK. R&R BS 1352 T-CHORD PER SRM 51-30-2.SDR 02FDEA00780Keelbeam · corrodedCORROSION ON KEELBEAM AT BS 950D TO 950E, STR 29 LT. REPAIRED KEEL BEAM STA 950D TO 950I STR 29L IAW FEDEX DWG SR 27-53-023.SDR 02FDEA00755Door Seal · defectiveON APPROACH TO CID-EXTENDED LAND GEAR, NOSE DOOR AMBER LT ON S/O PANEL & RED DOORS LIGHT ON. ELECTED TO DO MISS APPROACH & RECYCLE GEAR. LT WENT OUT. ON RE-EXTENSION RED GEAR DOOR LT WENT OUT. BELOW 200 KTS ON RECYCLE. CHECKED QRH. NO OTHER PROBLEM. FOUSDR 02FDEA00763Web · corrodedCORROSION ON WEB AT BS 1166, LBL 10, WL 140. R&R WEB PER SRM 53-10-1, 51-30-2, 51-20-1.SDR 02FDEA00764Web · corrodedCORROSION ON WEB AT BS 1166, RBL 10, WL 140. R&R WEB PER SRM 53-10-1, 51-30-2, 51-20-1.SDR 02FDEA00792Frame · dentedFRAME DENTED AT 970, LBL 30, STR 26L. R&R FRAME PER SRM 51-40-3 FIG & EA 7-5310-67055.SDR 02FDEA00761Frame · dentedFRAME DENTED AT STR 950F, LBL 30, STR 26L. REPAIRED FRAME IAW SRM 51-40-3 FIG 1 SHEET 3 & EA 7-5310-67056.SDR 02FDEA00762Frame · dentedFRAME IS DENTED AT BS 990, LBL 30, WL 146. R&R FRAME PER SRM 53-10-1.SDR 02FDEA00759Floorbeam · corrodedBULGE IN COCKPIT FLOOR. R&R BEAM PER SRM 51-30-2, 51-30-5, 51-30-8.SDR 02FDEA00760Skin · dentedEXTERNAL SKIN DENTED WITH TWO GOUGES AT BS 365, ABOVE STR 17L.SDR P9R2002F00010Strip · missingPHOTO LUMINESCENT STRIP IS MISSING FROM FORWARD GALLEY. RESECURED PHOTO LUMINESCENT IN FORWARD GALLEY. THE CAUSE OF THE MALFUNCTION WAS THE PHOTO LUMINESCENT STRIP COMING UNGLUED FROM FLOOR.SDR 02FDEA00749Warning System · malfunctionedAT FL 310 LOWER AFT BODY OVERHEAT LIGHT STARTED TO BLINK THEN STAYED ON UNTIL RED TAB WAS COMPLIED WITH, UPON CLOSING NR 3 BLEED, LIGHT WENT OUT. CONTINUED FLT. USING NR 2 BLEED SUPPLYING RIGHT PACK WITH NO FURTHER OVERHEAT INDICATION. INSPECTED AFT AIRSTAISDR 02FDEA00745Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 620, RBL 10, WL 208. R&R FLOORBEAM PER SRM 53-10-8.SDR 02FDEA00744Stringer · corrodedCORROSION ON STR 28L, BS 640-660. R&R STRINGER PER SRM 53-10-1, 53-10-3, 53-30-3.SDR 02FDEA00737Csd · faultyLEVEL AT FL 310 IN SMOOTH CONDITIONS, EXPERIENCED A THREE LIGHT TRIP. RAN QRH PROCEDURES, UNABLE TO RECOVER BTB, G/B OR FIELD. FREQS/VOLTS ON NR 2 GEN WERE ZERO (OFF SCALE LEFT). NO LIGHTS ON ELEC FAULT PANEL ILLUMINATED. NR 2 CSD WAS DISCONNECTED. AIR TUSDR 02FDEA00725Stringer · dentedDENT IN STR FLANGE AT BS 492, STR 23L. R&R STR FLANGE PER SRM 53-10-1, 53-10-3.SDR 02FDEA00724Skin · corrodedCORROSION ON SKIN LAP AT SHEAR TIE AT BS 720B, STR 26R. R&R SKIN PER SRM 53-10-5, 51-30-2, 51-30-5.SDR 02FDEA00729Frame · dentedFRAME DENTED AT BS 500, STR 23R - 24R. R&R FRAME PER SRM 51-40-3.SDR 02FDEA00728Skin · dentedDENT ON SKIN AT BS 465 BELOW STR 16R. R&R SKIN PER SRM 53-30-1, 53-30-3.SDR 02FDEA00723Switch · failedDURING FLAP RETRACTION FROM 2 DEG TO UP (NR 6 LE FLAP) NR 6 LED REMAINED AMBER, NO ADVERSE ROLL NOTED. REMOVED AND REPLACED NR 6 LEADING EDGE FLAP POSITION INDICATOR SWITCH PER MAINTENANCE MANUAL 27-82-001-4. OPERATIONAL CHECKS GOOD.SDR 02FDEA00722Indicator · stickingON INITIAL FLAP RETRACTION, THE OUTBOARD TRAILING EDGE FLAP STOPPED MOVING AT ABOUT 1 DEG AND THE LEFT AND RIGHT NEEDLES ON THE GAUGE SHOWED ONE NEEDLE WIDTH SPLIT. RED TAG PROCEDURES ACCOMPLISHED AND AIR ABORT ACCOMPLISHED. UPON INSP FOUND O/B FLAP IND STICSDR 02FDEA00747Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 45-55, WL 208. R&R UPPER CHORD PER ER 02-1505.SDR 02FDEA00726Seat Track · corrodedCORROSION ON SEAT TRACK I/B FLANGE UPR SURFACE AROUND NUTPLATE HOLES AT BS 760-848, LBL 24, WL 208. R&R SEAT TRACK PER SRM 51-30-2.SDR 02FDEA00734Skin · chafedSKIN CHAFED AT BS 720D+12 AT STR 19R. R&R SKIN PER SRM 53-30-03.SDR 02FDEA00730Skin · bulgedBULGING ON BELLY SKIN BETWEEN BS 1050 TO 1060, LBL 20. R&R SKIN PER SRM 53-30-1, 53-10-1, 53-30-3.SDR 02FDEA00732Frame · corrodedCORROSION ON BS 720E FRAME FWD SIDE STR 7L. R&R FRAME PER SRM 53-10-01 & EA 7-5310-67028 & SRM 53-10-14 FIG 1.SDR 02FDEA00733Skin · chafedSKIN CHAFED AT BS 720D+12 AT STR 19L. R&R SKIN PER SRM 53-30-3 FIG 14.SDR 02FDEA00731Floorbeam · corrodedCORROSION ON UPR CHORD FLOORBEAM AT BS 344, LBL 3, WL 208.SDR 02FDEA00702Warning System · malfunctionedLOWER AFT BODY OVERHEAT LIGHT BRIEFLY ILLUMINATED DURING FLIGHT. LIGHT FLICKERED ON AND THEN EXTINGUISHED APPROX 45 SECONDS ON THEN OFF FOR REMAINDER OF FLIGHT. INSPECTED RIGHT AND LEFT SECTION 48 OVERHEAT DETECTOR AND KEEL BEAM OVERHEAT DETECTOR, LIGHTLY SDR 02FDEA00692Clamp · out of positionFL290 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, COMPLETED QRH PROCEDURES LIGHT WENT OUT. REMAINDER OF FLIGHT CONDUCTED WITH NR 3 BLEED OFF, NR 2 PACK OFF NORMAL POWER ON NR 3 ENGINE. CHECKED AFT AIRSTAIR AND FOUND RT PURGE VALVE V BAND CLAMP OPENING LESS THSDR 02FDEA00688Actuator · failedAFTER FLAP RETRACTION, WITH FLAPS UP AND LED LIGHT GREEN, "A" SYSTEM QUANTITY DECREASED TO ZERO. WITH LOSS OF "A" SYSTEM PRESSURE RAN APPROPRIATE EMERGENCY CHECKLISTS. FOUND NR 4 SLAT ACTUATOR BODY FAILED AT ENDCAP WHERE ROD EXITS THE HOUSING. REMOVED AND RSDR 02FDEA00683Accessory Unit · faultyUPON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH LG LEVER IN THE UP POSITION. COMPLIED WITH RED TAB PROCEDURE. LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LANDING GEAR ELECTRONIC MODULE B727 M/M 32-09-121-4. REMOSDR 02FDEA00670Support · corrodedCORROSION ON BS 1176.9 REINFORCEMENT CHORD, RBL 50-70.5, WL 208. R&R CHORD PER SRM 51-30-2, 51-30-8, 51-30-5, 51-10-2 & MM 51-20-151-7.SDR 02FDEA00673Skin · gougedLT FUSELAGE EXTERIOR SKIN HAS A GOUGE AT BS 365.5 BETWEEN STR 16L - 17L. R&R SKIN PER SRM 53-30-3 FIG 3 & EA 7-5330-54319.SDR 02FDEA00681Frame · crackedCRACK IN FRAME FAILSAFE CHORD AT BS 804, STR 14R. R&R FRAME PER SRM 51-40-3.SDR 02FDEA00682Frame · crackedCRACK IN FRAME FAILSAFE CHORD BS 804, STR 14R. R&R FRAME PER SRM 51-40-3.SDR 02FDEA00689Floorbeam · damagedCORROSION IN FASTENER HOLES ON FLOORBEAM LOWER FLANGE AT BS 1070, LBL 45 TO RBL 45. R&R FLOORBEAM PER DWG SR27-53-034, SRM 53-10-8.SDR 02FDEA00680Skin · corrodedFOUND CORROSION ON SKIN AT BS 483-495, 528R. R&R SKIN PER SRM 53-30-3.SDR 02FDEA00679Stringer · corrodedCORROSION C53-111-01 ON STRINGER 328R, BS 480+5 FWD CARGO BAY. R&R STRINGER PER SRM 53-10-3.SDR 02FDEA00668Sensor · out of positionAT LEVEL OFF AT 28000 FT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH PROCEDURES. LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED WITH NR 3 BLEED VALVE CLOSED AND RIGHT PACK OFF. CHECKED SENSOR IN AFT AIRSTAIR AREA, REPOSITIONED TWO PLACES OF SDR 02FDEA00678Floorbeam · corrodedCORROSION LWR CHORD BS 720 FLOORBEAM, WL 208, LBL 55 - RBL 55. R&R CHORD PER SR 27-53-034.SDR 02FDEA00664Flap · looseAIRFRAME BUFFET OCCURRED DURING CLIMB OUT AT .65 MACH, SLOWING THE AIRCRAFT DECREASED THE BUFFET. NO BUFFET AT .58 MACH. INSPECTED FLAPS AND AILERONS FOR SECURITY. FOUND THE RT OUTBD AFT FLAP HAD EXCESSIVE PLAY. DROPPED FLAPS AND CHECKED THE AFT FLAP AFTSDR 02FDEA00658Floorbeam · corrodedCORROSION LWR CHORD BS 1130, WL 200, LBL 55 - RBL 55. R&R CHORD PER EA 7-5310-62008.SDR 02FDEA00659Frame · dentedDENTED FRAME AT BS 560, APPROX STR 24L. R&R FRAME PER EA 7-5310-65881.SDR 02FDEA00660Frame · dentedDENTED FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT. R&R FRAME PER EA 7-5310-65882.SDR 02FDEA00661Stringer · gougedSTRINGER 7L, BS 720B+14 IS GOUGED. R&R STRINGER PER SRM 53-10-3 FIG 3.SDR 02FDEA00654Skin · dentedDENTS ON FUSELAGE EXTERNAL SKIN AT BS 268 BETWEEN STR 19R & 20R. R&R SKIN PER SRM 53-30-2 FIG 24.SDR 02FDEA00690Skin · gougedLT FUSELAGE EXTERIOR SKIN HAS A GOUGE AT BS 294.5 JUST ABOVE STR 17L. R&R SKIN PER EA 7-5330-67012.SDR 02FDEA00691Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER CHORD AT BS 344, LBL 60 - RBL 4, WL 208. R&R FLOORBEAM PER SRM 53-10-8 FIG 9.
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