Boeing 727-100
Service difficulty reports · 288
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 = '727100' 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 = '727100' 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 02FDEA00620Skin · crackedCRACKS NOTED IN FASTENER HOLE AT BS 488, STR 3L, AFT HOLE OF FILLER IN ALL LAYERS INCLUDING FILLER, EXCEPT INNERMOST SKIN CRACKS ENDS MARKED. REMOVED AND REPLACED FASTENER HOLES PER EA 7-5330-65875.SDR 02FDEA00619Skin · crackedCRACKS NOTED IN FASTENER HOLES 5 EA AT BS 610-614, STR 3L IN ALL LAYERS EXCEPT INNERMOST AND FILTER. REMOVED AND REPLACED FASTENER HOLES PER EA 7-5330-65875.SDR 02FDEA00618Structure · crackedCRACK AT AFT CARGO AFT LWR CORNER 4TH FASTENER FROM CORNER OF DOOR CUTOUT. REMOVED AND REPLACED CARGO DOOR PER SRM 51-10-7.SDR 02FDEA00607Rib · chafedLEFT HORIZONTAL STAB T/E RIB AT ELEVATOR BS 209, I/B SIDE HAS CHAFING DAMAGE. REMOVED AND REPLACED RIB PER SRM 51-30-2.SDR 02FDEA00604Connector · faultyDURING TAKEOFF MSY RWY 19 AT V1 APPROXIMATELY 100 KNOTS, WARN BELL SOUNDED WITH NO OTHER LIGHTS OR INDICATIONS IN COCKPIT ATOGW 131.4 - ABORT INITIATED BELL W/N SILENCE ON INITIAL ATTEMPTS. MAIN CARGO SMOKE DET IS INOP. FOUND PTT SW ON THE MAIN CARGO SMOKE DSDR 02FDEA00600Web · corrodedCORROSION ON BOTTOM SIDE OF SHEAR WEB AT BS 1136, RBL 64, WL 208.SDR 02FDEA00589Skin · lightning strikeLIGHTNING STRIKE ON OUTER SKIN AT BS 401, STR 10R. REMOVED AND REPLACED SKIN PER SRM 53-30-3.SDR 02FDEA00576Skin · lightning strikeLIGHTNING STRIKE LWR FUSELAGE AT BS 181, STR 19R.SDR 02FDEA00579Stringer · crackedSTRINGER 8R CRACKED AT BS 600. REMOVED AND REPLACED STRINGER PER SRM 53-10-01, 51-40-4.SDR 02FDEA00578Web · crackedCRACKED WEB BS 600 BETWEEN STR 1 & 2 LT. REMOVED AND REPLACED WEB PER SRM 51-30-2, 51- 30-5, 51-20-1.SDR 02FDEA00577Web · crackedCRACKED WEB BS 613 BETWEEN STR 1 & 2 LT.SDR 02FDEA00558Skin · damagedNUMEROUS NICKS IN LWR EXTERNAL FUSELAGE SKIN BETWEEN BS 368, STR 19L TO 20L. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 1.SDR 02FDEA00560Stringer Clip · crackedCRACKED STR CLIP AT BS 1050, STR 6 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2.SDR 02FDEA00559Stringer Clip · crackedCRACKED STR CLIP BS 1070, STR 7R.SDR 02FDEA00564Fitting · corrodedSTRINGER END FITTING CORRODED AT BS 740, STR 9L. REMOVED AND REPLACED FITTING PER SRM 51-30-2.SDR 02FDEA00562Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 1030, STR 4 RT.SDR 02FDEA00554Skin · bulgedLWR EXT FUSELAGE HAS BULGING SKIN AND SHEARED RIVET BETWEEN STR 28R AND 29R AT BS 352 AND 358. REMOVED AND REPLACED SKIN PER SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2.SDR 02FDEA00555Frame · corrodedCORROSION CIRCUMFERENTIAL CHORD CORRODED AT BS 351 BETWEEN STR 26L AND 26R.SDR 02FDEA00571Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 1000, STR 9 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5.SDR 02FDEA00572Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 1030, STR 9 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5.SDR 02FDEA00573Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 1030, STR 7 LT. REMOVED AND REPLACED CLIP PER SRM 51-30-2, 51-30-5.SDR 02FDEA00570Bulkhead · crackedCRACK ON WEB AT BS 178, RBL 10, WL 235. REMOVED AND REPLACED WEB PER SRM 53-10-9.SDR 02FDEA00523Engine · malfunctionedNR 3 ENGINE OIL TEMPERATURE WENT INTO YELLOW BAND APPROX 10 MINUTES AFTER T/O. STARTED 15 MINUTE TIMING & COMPLIED WITH RED TABS. WHEN THRUST LEVER WAS RETARDED TOWARDS IDLE, OIL TEMP WENT INTO RED BAND. RED TABS DIRECTED AND ENGINE SHUTDOWN. AFTER SHUTDOWSDR 02FDEA00521Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 968, RBL 3-5, WL 150. REPAIRED SHEAR TIE IAW SRM.SDR 02FDEA00513Oil Filter · damagedNR 1 ENGINE, HIGH OIL TEMP (OFF SCALE HIGH) FOUND BAD CONNECTION AT OIL TEMP SENSOR. PER CREW INFO WINDMILLING WAS LESS THAN 30 MIN. FOUND BROKEN WIRE AT C/P ON NR 1 ENG OIL TEMP BULB. REMOVED AND REPLACED C/P D530 IAW SWPM. PERFORMED ENGINE WINDMILLING INSDR 02FDEA00508Shear Tie · gougedSHEAR TIE GOUGED AT BS 540, JUST BELOW STR 14R. REPAIRED SHEAR TIE BS 540 BELOW STR 14R IAW SRM 53-10-4, 53-10-2.SDR 02FDEA00488Odor · detectedWHEN POWER LEVER WAS PULLED TO IDLE,THERE WAS AN ACRID SMELL IN THE COCKPIT. ODOR SMELLS LIKE AN OVERHEATED ELECTRIC MOTOR. SMELL OCCURRED WITH GASPER FAN ON OR OFF. RAN ALL ENGINES WITH PACKS ON AND GASPER ON & OFF, NO ODORS DETECTED AND NO BURNING NOTED. SDR 02FDEA00416Skin · dentedSKIN DENTED AT BS 720, STR 16R.SDR 02FDEA00397Engine · leakingLOST OF OIL QUANTITY AND PRESSURE IN NR 3 ENG. SHUTDOWN PER CHECK LIST AND LANDED. INSPECTED CHIP DETECTORS, AND FILTER FOUND TO BE CLEAN. FOUND OIL PUDDLED IN TAILPIPE, NO EVIDENCE OF OIL IN COLD STREAM AREA. SERVICED ENG OIL AND MOTORED. OIL QTY DROPPEDSDR 02FDEA00382Module · shortedON TAKEOFF, AFTER RAISING THE GEAR HANDLE THE PRESS TO TEST & LIGHTS C/B (P6-3, LANDING GEAR) POPPED. 1ST & 2ND VERTI ROWS ON THE DOOR LIGHT PANEL LIGHT UP. ON RECOVERY, NONE OF THE GEAR LIGHTS WOULD LIGHT. M/GEAR EXT ACCOMP. F/O NOTICED A SPARK BEHIND 3 SDR 02FDEA00332Clamp · leakingDURING INITIAL CLIMB, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, WING ANTI ICE VERIFIED CLOSED, NR 1 ENG BLEED AIR SWITCH CLOSED AND NR 1 ENG THRUST LEVER TO IDLE IAW RED TABS, STRUT OVERHEAT LIGHT EXTINGUISHED AFTER 3 MINS AND OVERHEAT SYSTEM TESTED SATISFACTSDR 02FDEA00314Turbine · damagedNR 2 ENGINE COMPRESSOR STALLED EXCESSIVE VIBRATION. INTAKE HAD NO APPARENT DAMAGE, EXHAUST SHOWED THE TURBINE BLADES HAD DAMAGE AND POOLS OF OIL. REMOVED AND REPLACED NR 2 ENGINE. OK FOR SERVICE.SDR CA020322003Cage · failed(CAN) THE NR 3 CSD/GEN TRIPPED, FOLLOWED BY LOW ENGINE OIL PRESSURE WHICH RESULTED IN AN IFSD DUE TO LACK OF OIL AND PRESSURE. GROUND MAINTENANCE ADDED 6 LITERS/QTS OF OIL TO THE ENGINE AND TOPPED OFF THE CSD. THERE WERE NO REPORTED NOR ANY SIGNS OF EXTERNAL LSDR 01FDEA01090Roller · out of positionCLIMBOUT UNABLE TO PRESSURIZE - TRIED MANUALLY TO PRESSURIZE, NO HELP. ALL DOOR LIGHT INDICATIONS NORMAL. UPON ARRIVAL IN RST MAIN ENTRY DOOR UPPER AFT GUIDE ROLLER OUT OF GUIDE, CAUSING DOOR TO NOT PROPERLY SEAT. OPENED/CLOSED DOOR FROM INSIDE/OUTSIDE SEVESDR XNA01005Light · illuminatedNR 3 START VALVE OPEN LIGHT CAME ON START OF T/O RUN, MADE LOW SPEED ABORT (80 KTS). ON TAXI BACK - INDICATION WAS DETERMINED TO BE FALSE. MADE NORMAL DEPARTURE. LIGHT WENT OUT IN CRUISE (310) CAME BACK ON IN DESCENT (2000 FT). TRANSFERRED TO DMI LOG 1125 SDR 99FDEA00099Switch · inop99-0067 - DOOR LIGHTS RED WOULD NOT GO OUT AT GEAR RETRACTION. NOSE GEAR HAD A FAULTY GREEN LIGHT, RED NOSE GEAR LIGHT NOW STAYS ON. REMOVED AND REPLACED DOWN LOCK SWITCH. OPER CK NORM PER MM 32-61-0-21-4.SDR CA980317046Pump · failed(CAN) AT TOP OF DESCENT, AIRCRAFT BEGAN TO LOSE A-SYSTEM HYDRAULIC FLUID, A-SYSTEM PRESS FLUCTUATING BETWEEN 3,000 AND 2,500 PSI. ACFT STOPPED ON RUNWAY AND T OWED TO RAMP. FOUND HEAVY LEAK AT NR 2 ENG HYDRAULIC PUMP AND NR 1 CASE DRAIN HAD CARBON RUBBER CONSDR 96ZZZX4161Fitting · corrodedAFT PORTION OF ONE CARRIAGE SUPPORT FITTING FOUND EXFOLIATION ONCE THE LEADING EDGE CAP WAS REMOVED FROM SPAR. FND CORROSION ON MATING SURFACES OF L/E CAP AND SPAR. FLAP IN SHOP FOR COMPLETE HONEYCOMB/SKIN REPLACMENT AND OVERHAUL. DUE TO DESIGN, AFT PORTION
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