Boeing 727-222
Service difficulty reports · 1,723
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 = '727222' 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 = '727222' 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 RYN2002F00013Floor Support · crackedC-CHECK, FOUND CRACK IN FLOOR SUPPORT, AT FORWARD FUSELAGE INTERIOR LOWER LOBE, AT STATION 310.SDR RYN2002F00018Pressure Panel · crackedC-CHECK, FOUND CRACK IN WEB, AT LEFT MAIN LANDING GEAR, LOWER HALF OF OUTBOARD SIDE, AT STATION 870, WATER LINE 148.SDR RYN2002F00017Pressure Panel · crackedC-CHECK, FOUND CRACK AT RIGHT MAIN LANDING GEAR WEB, LOWER HALF OUTBOARD SIDE, AT STATION 870, WATER LINE 148.SDR RYN2002F00016Skin · corrodedC-CHECK, FOUND CORROSION AT NOSE LANDING GEAR DRAG BRACE SUPPORT FITTING, LEFT SIDE ON SKIN, AT STATION 344.0.SDR RYN2002F00015Bracket · corrodedC-CHECK, FOUND CORROSION AT NOSE WHEEL WELL, ON RIGHT SUPPORT BRACKET, AT STATION 294.5.SDR RYN2002F00014Fitting · corrodedC-CHECK, FOUND CORROSION AT NOSE WHEEL WELL FORWARD BULKHEAD, ON DOOR LINKAGE FITTING, AT STATION 227.8, LEFT SIDE.SDR RYN2002F00029Fitting · corrodedAT (C) CHECK, FOUND NOSE WHEEL WELL FORWARD BULKHEAD DOOR LINKAGE FITTING CORRODED, AT STATION 227.8, LEFT SIDE.SDR RYN2002F00021Frame · corrodedC-CHECK, FOUND CORROSION AT THE FORWARD ACCESSORY COMPARTMENT, LEFT SIDE DOOR CUTOUT, ON SHEAR TIE AND FRAME, AT STATION 211 TO 219.SDR RYN2002F00020Splice · corrodedC-CHECK, FOUND CORROSION IN THE E AND E COMPARTMENT, STRINGER 25R SPLICE, AT STATION 440.SDR RYN2002F00019Splice · corrodedC-CHECK, FOUND CORROSION IN E AND E COMPARTMENT, ON STRINGER SPLICE, AT STATION 440, STRINGER 24R.SDR 2002F00874Skin · dentedAT C-CHECK, FOUND DENT ON FUSELAGE SKIN AT STATION 481, BELOW STRINGER 18R. (M)SDR 2002F00628Actuator · leakingON DEPARTURE FROM DAY TO ICT, 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. ALL APPLICABLE CHECKLISTS WERE ACCOMPLISHED AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. (M)SDR GAIA2002F0000Duct · blownAFTER TAKEOFF, THE NR 3 FIRE WARNING CAME ON. THE CREW DECLARED AN EMERGENCY, SHUT DOWN NR 3 ENGINE AND THE WARNING LIGHT EXTINGUISHED. THE FLIGHT RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. MAINTENANCE FOUND THE 13TH STAGE DUCT FROM THE PRBC AND FUEL HEATSDR 2002F00449Trunnion · crackedAT C-CHECK, FOUND RIGHT MLG TRUNNION SUPPORT FITTING CRACKED. (M)SDR 2002F00185Smoke Detector · malfunctionedFOUND CARGO SMOKE DETECTOR LIGHT ILLUMINATED DURING CLIMB OUT FROM MDT. AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. (M)SDR 2002F00448Floor Support · corrodedAT C-CHECK, FOUND AFT PIT FLOOR SUPPORT CORROSION AT STATION 1163-1166 LBL 4. (M)SDR LCQ07Trunnion · crackedRIGHT MLG TRUNNION ATTACHMENT FITTING INBOARD LUG LWR OUTBOARD FACE HAS MINOR CORROSION. LATER FOUND FITTING TO BE CRACKED.SDR 2002F00513Frame · crackedAT C-CHECK, FOUND CRACKED FRAME (INSIDE COCKPIT) AT LEFT STATION 294.5 STRINGER 4L. (M)SDR 2002F00158Frame · crackedFOUND LEFT STATION 294.5 STRINGER 4L, INSIDE COCKPIT, FRAME IS CRACKED. (M)SDR 2002F00516Skin · chafedAT C-CHECK, FOUND RIGHT INBOARD MID FLAP UPPER SKIN CHAFFED AT OUTBOARD SIDE WBL 243. (M)SDR 2002F00515Bracket · crackedAT C-CHECK, FOUND LOWER MOUNT BRACKET FOR THE OIL PRESSURE LIGHT SWITCH ON NR 2 ENGINE CRACKED. (M)SDR 2002F00514Skin · gougedAT -CHECK, FOUND LEFT LOWER FUSELAGE SKIN GOUGED AT STATION 1200 19 AND 20L. (M)SDR 2002F00178Skin · gougedFOUND LEFT LOWER FUSELAGE SKIN IS GOUGED AT STATION 1200 STRINGER 19 AND 20L. (M)SDR 2002F00519Skin · crackedAT C-CHECK, FOUND L1 DOOR EXTERIOR SKIN CRACKED AT THE FORWARD LOWER CORNER STATION 317 APPROXIMATELY SIX INCHES FROM FORWARD EDGE OF DOOR. (M)SDR RRX2001F00000Actuator · leakingLOST (A) SYSTEM HYDRAULIC PRESSURE DURING CLIMB OUT FROM MSY. ACCOMPLISHED EMERGENCY CHECKLIST RELATING TO LOSS OF (A) SYSTEM HYDRAULICS. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 3 SLAT ACTUATOR ASSEMBLY AND OPERATIONAL CHECK SYSTSDR 2001UALA02224Starter · failedSHORTLY AFTER TAKEOFF THE AIRCRAFT EXPERIENCED A NUMBER THREE ENGINE FIRE INDICATION. AIRCRAFT RETURNED TO FIELD. ENGINE FIRE OCCURRED DUE TO OIL LINE/CSD RUPTURE, CAUSED BY UNCONTAINED STARTER FAILURE. UPON RETURN TO FIELD, CSD WAS FOUND CRACKED. THE STARSDR 2002F00273Engine · malfunctionedON APPROACH TO ATLANTA INTERNATIONAL AIRPORT AT 1000 AGL NR 3 ENGINE MOMENTARILY LOST POWER. FULL POWER WAS RESTORED WITH NORMAL ENGINE PARAMETERS AND AIRCRAFT LANDED WITHOUT INCIDENT. ENGINE TO BE RMEOVED AND REPLACED DUE TO SUSPECTED INTERNAL ENGINE DAMAGESDR 2001UALA02108Structure · damagedFUSELAGE DAMAGE FOUND DURING MAINTENANCE CHECK. MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGE. OPERATIONS CHECK NORMAL.SDR 2001UALA02092Hydraulic System · malfunctionedAIRCRAFT LOST B-SYSTEM HYDRAULIC PRESSURE IN FLIGHT. THE AIRCRAFT DIVERTED TO DTW. HYDRAULIC SYSTEM CHECKED PER THE 727 MAINTENANCE MANUAL. NO FAULTS FOUND. NO HYDRAULIC ISSUES IN AIRCRAFT HISTORY SINCE THIS INCIDENT.SDR 2001UALA02085Lamp · failedEMERGENCY EXIT LIGHTING IN FIRST CLASS AISLE IS INOPERABLE. *S/D* LAMPS FAILED. REPLACED LAMPS. OPERATIONS CHECK NORMAL.SDR 2001UALA02082ActuatorAIRCRAFT LOST SYSTEM "A" HYDRAULIC PRESSURE AND QUANTITY DURING LANDING. SUPPLEMENTAL DATA UPDATE FOUND RT MLG DOOR ACT BROKEN, LARGE LEAK. REPLACED ACTUATOR. SYSTEM CHECKS NORMAL.SDR 2001UALA02076Structure · dentedDENT ON NR 8 LEADING EDGE KRUEGER FLAP FOUND APPROXIMATELY 5 INCHES LONG, 0.750 INCHES WIDE AND 0.250 INCHES DEEP. DENT REPAIRED. MAJOR REPAIR ACCOMPLISHED.SDR GAIA01309Light · inoperativeDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT HAD ONE EACH BULB BURNED OUT. MAINTENANCE RELAMPED THE LIGHT BULB IN THE COCKPIT EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICSDR 2001UALA02032Pressure Panel · crackedNOSE WHEEL WELL PRESSURE DECK WEB CRACKED AT BODY STATION 282, RBL 4.SDR 2001UALA02077Battery Pack · dischargedRT FORWARD AND REAR OVERWING EMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED BATTERY PACK. OPERATIONS CHECK NORMAL.SDR 2001UALA01996Pressure Panel · crackedNOSE LANDING GEAR WHEEL WELL TOP PRESSURE PANEL CRACKED AT FASTENER HOLES AT BODY STATION 284. REPAIRED PRESSURE PANEL WEB. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01982Battery · failedOVERHEAD EMERGENCY LIGHTS IN CABIN AT ROW 9 AND 20 ARE NOT OPERATING. *S/D* BATTERY FAILED. FOUND LIGHTS AT ROW 9 NORMAL, REPLACED BATTERY AT ROW 20. OPERATION CHECK NORMAL.SDR 2001UALA01997Pressure Panel · crackedNOSE LANDING GEAR WHEEL WELL TOP PRESSURE PANEL IS CRACKED AT FASTENER HOLES BS 275, RBL 13, AND BS 284, RBL 6. REPAIRED PRESSURE PANEL WEB. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01983Light · inoperativeRIGHT HAND FORWARD OVERWING EMERGENCY LIGHT IS INOPERABLE. *S/D* DURING OPERATIONAL CHECK ALL EMERGENCY LIGHTS ARE FUNCTIONING NORMALLY.SDR 2001UALA01981Check Valve · leakingACARS DISPLAYED A STRUT OVERHEAT LIGHT ON NUMBER 1 ENGINE. *S/D* FOUND SENSE LINE LEAKAGE AT 6TH STAGE CHECK VALVE. REPLACED AND WRENCHED CHECKED LINES. OPERATIONS CHECK NORMAL.SDR 2001UALA01793Battery Pack · failedEMERGENCY EXIT LIGHTS OVER LT OVERWING EXIT ARE INOPERABLE. *S/D* REPLACED BATTERY PACK. OPERATIONS CHECK NORMAL.SDR 2001UALA01792Connector · damagedEMERGENCY EXIT LIGHTS AT SEAT 18C TO 24C ARE INOPERABLE. REPAIRED BAD CONNECTION. OPERATIONS CHECK NORMAL.SDR 2001UALA01765Frame · crackedRIB INTERCOSTAL STATION 360 IS CRACKED LENGTHWISE, AND STRINGER SUPPORT UNDER INTERCOSTAL IS BENT. SUPPLEMENTAL DATA UPDATE REPAIRED FRAME AT BS 380 BETWEEN STRINGERS S15 AND S16 AT THE ASSOCIATED SKIN ATTACHMENT.MAJOR REPAIR ACCOMPLISHEDSDR 2001UALA01728Ferrule · leakingAIRCRAFT DIVERTED TO MIA DUE TO IDLE POWER CONDITION FROM NR 1 ENGINE. *S/D* THE CAUSE WAS A FUEL LEAK FROM THE FUEL LINE FROM THE FUEL/OIL COOLER TO THE P&D VALVE. THIS LINE WAS MISSING A FERRULE AT THE P&D VALVE CONNECTION. THIS ENGINE HAD ONLY 370 HRS SDR 2001UALA01725Indicator · malfunctionedAIRCRAFT HAD SPLIT FLAP INDICATION ON APPROACH. OUTBOARD FLAP POSITION INDICATOR FAILED. REPLACED OUTBOARD FLAP POSITION INDICATOR. SYSTEM TESTS NORMAL.SDR 2001UALA01719Cover · leakingNR 3 ENGINE WAS SHUT DOWN DURING LANDING. *S/D* ENGINE WAS SHUT DOWN TO LOSS OF OIL FROM THE THE MAIN OIL SCREEN. THE OIL PRESSURE DROPPED TO 38 PSI. CAUSE WAS STUDS PULLED ON THE MAIN OIL SCREEN COVER AND WAS REPAIRED.SDR 2001UALA01726Battery · failedAFT AIRSTAIRS EMERGENCY LIGHT IS INOPERABLE. SUPPLEMENTAL DATA UPDATE THE BATTERY FAILED. REPLACED BATTERY. OPERATIONS CHECK NORMAL.SDR 2001UALA01609Pump · failedAIRCRAFT EXPERIENCED B-HYDRAULIC SYSTEM ZERO QUANTITY INDICATION DURING CRUISE. AIRCRAFT CONTINUED TO ORD. THE NR 1 ENGINE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE HYDRAULIC PUMP, SYSTEM TESTS NORMAL.SDR 2001UALA01608Tire · failedUPON LANDING THE TWO LEFT MAIN LANDING GEAR TIRES BURST. *S/D* HARD LANDING INSPECTION ACCOMPLISHED. ANTISKID FUNCTIONAL TEST ACCOMPLISHED. OPERATIONAL CHECK FOUND NO DISCREPANCIES.SDR 2001UALA01593Control Cable · obstructedCREW REPORTS STEERING TILLER BINDS, ESPECIALLY IN A LEFT TURN. *S/D* FOUND OBSTRUCTION IN NOSE METERING VALVE CABLE SYSTEM. CLEARED OBSTRUCTION AND INSPECTED CABLE SYSTEM. OPS CHECKS NORMAL.
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