Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 CAL950264Spindle · brokenDEN - THE LT OUTBOARD MID-FLAP INBOARD CARRIAGE SPINDLE WAS FOUND BROKEN IN TWO DURING B-CHECK INSPECTION WITH RESULTANT DAMAGE TO THE FLAP. BOTH THE LT OUTBOARD MID AND AFT TRAILING EDGE FLAPS WERE REMOVED AND REPLACED. THE FLAPS WERE RIGGED IAW MM 27-51-13SDR AALA950620Eel Wire · brokenMIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT IN FIRST CLASS CABIN FOUND INOPERATIVE. REPAIRED BROKEN WIRE TO BATTERY PACK IN CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)SDR AALA950618Eel Wire · brokenMIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 24 FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BETWEEN FLOOR LIGHTS AND BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)SDR 95ZZZX5185Diffuser · crackedIND - NR 3 ENGINE HAS A CRACK IN THE OUTER DIFFUSER DUCT. NR 3 ENGINE WAS REMOVED AND REPLACED.SDR CALA950247O-Ring · leakingEWR - FLT 0432 - THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO IN FLIGHT. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE GROUND SPOILER CONTROL VALVE IN THE LT WHEELWELL LEAKING AT FITTING. THE O-RING AND REDUCER WERE REMOVED AND REPLASDR CAL950245Hyd Line · chafedIAH - FLT 1498 - HYDRAULIC FLUID WAS LOST FROM THE B-SYSTEM WHILE IN-FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO B-SYSTEM HYDRAULIC LINES IN THE HYDRAULIC BAY CHAFED THROUGH. BOTH LINES WERE REMOVED AND RSDR CAL950240Fan · contaminatedOKC - FLT 0121 - SMOKE APPEARED IN THE CABIN WHILE EN ROUTE FROM IAH TO DEN. THE SMOKE CEASED AFTER THE AIR DISTRIBUTION FAN WAS TURNED OFF AND CIRCUIT BREAKERS WERE PULLED. THE SMOKE RE-APPEARED ABOUT 10 MINUTES LATER. THE SOURCE OF SMOKE COULD NOT BE ISOLSDR CAL950233Actuator · crackedFLL - FLT 0385 - THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO FLL. HYDAULIC LOSS CHECK LIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 3 LEADING EDGE SLAT ACTUATOR CRACKED AND LEAKING. THE SLAT ACTUATOSDR 95FDEA00315Overheat Light · illuminatedNR 1 ENG STRUT OVERHEAT LIGHT CAME ON PASSING 10,000 FEET CLIMBING OUT. ENG ANTI-ICE HAD JUST BEEN SHUTOFF, BOTH PACS ON, BLEEDS OPEN ON NR 1 AND NR 3. ABNORMAL PROCEDURES IN RED TABS COMPLIED WITH/ACCOMPLISHED. LIGHT STAYED OUT AS NR 1 THROTTLE READVANCEDSDR MZZA9513Sensor · failedGUM - FLT 990 - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO GUM. MAINTENANCE FOUND SENSOR M-682 GROUND SENSOR SHORTED. REPLACED SENSOR PER MM 32-09-221. SYSTEM CHECKED GOOD AND GEAR RETRACTION CHECKED NORMAL. (X)SDR 95ZZZW624Oxygen Reg · looseMKE - FLT 517 - DURING TAXI OUT CREW OXYGEN PRESSURE DROPPED FROM 1500 TO 1000 PSI. RESERVICED 0XYGEN, TIGHTENED FITTING ON OXYGEN REG/FE'S.SDR CAL950182Support · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FLOOR SUPPORT ANGLE U-CHANNEL AT BS 1030 ABOVE STRINGER 29R. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2. (W)SDR 95ZZZW327Uplock Switch · malfunctionSTL - FLT 491 - AFTER TAKEOFF UPON GEAR RETRACTION HAD NOSE GEAR UNSAFE INDICATION. RECYCLED GEAR, NO HELP. RAN ABNORMAL PROCEDURES, INDICATION REMAINED. REPLACED NOSE LANDING GEAR UPLOCK SWITCH. PIN WAS STUCK IN GROUND POSITION, PERFORMED REMOVAL/INSTALLASDR CAL950168Sealant · missingJAX - FLT 0364 - CABIN PRESSURE WAS LOST AT FL290 & OXYGEN MASKS DEPLOYED. CREW SWITCHED FROM AUTO TO STANDBY TO MANUAL, BUT CABIN PRESS COULD NOT BE CONTROLLED. BLEEDS WERE SWITCHED, BUT CABIN STILL WOULD NOT PRESS. ACFT DIVERTED TO JAX. MX FOUND AFT CARGSDR 95FDEA00167Tab Hinges · brokenA/C HAS A HEAVY YAW VIBRATION AND FLOOR VIBRATION ABOVE .72M AT FL 350. AT FL 280 VIBRATION STARTS AT .62M SPEEDBRAKES, CLIMB, DESCENTS AND TURNS HAVE NO EFFECT ON VIBRATION OR YAW. AIRCRAFT WAS FLOWN AT 62M AND FL280 FROM DAY-MEM. REMOVED LOWER TAB. FOUNSDR AALA950317Slide · defectiveORD - DURING SHOP VISIT FOUND 2 RUNWAY SEAM SEPARATIONS OF 8 INCHES AND A FRAYED LATCH ASSEMBLY ON THE EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (X)SDR CAL950131Warning Light · illuminatedEWR - FLT 0894 - THE RED NOSE GEAR WARNING LIGHT REMAINED ILLUMINATED WITH NO NOSE GEAR GREEN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. ALL INDICATIONS WERE NORMAL WITH 3 GREEN AFTER THE GEAR WAS CYCLED. A NOSE GEAR RETRACTION AND EXTENSION TEST WERE SDR 95FDEA00135Engine · failedCGN - ENG NR 2 FAILED JUST AFTER LIFT OFF CGN; FLAPS 15 DEG A/C VIBRATION, WITH NR 2 ENG N1, N2 DROPPING, FUEL FLOW DROPPING, OIL QTY AND PRESS NORMAL. ENG SHUTDOWN WITH APPROPRIATE CHECKLIST ACCOMPLISHED.SDR CAL950150Warning Light · illuminatedFLT NR 0603 - EWR - THE RT MLG RED UNSAFE LIGHT AND RT GEAR DOOR LIGHTS ILLUMINATED IN FLIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PEFORMED EXTENSION AND RETRACTION OF THE LANDING GEAR AND NO DEFSDR AALA950166Slide · defectiveORD - DURING SHOP VISIT, FOUND GIRT COMING UNPLUGGED AT MATING SURFACE, ALSO HAD RUNWAY SEAM SEPARATION ON EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W)SDR CAL950074Hyd Line · leakingEWR - FLT 518 - THE ACFT LOST 'A' SYSTEM HYDRAULICS ON APPROACH WITH THE NR 1 PUMP LOW PRESSURE LIGHT FLICKERING ON AND OFF. THE GEAR AND FLAPS WERE EXTENDED USING ALTERNATE MEANS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAUSDR CAL950070Pressure Web · corrodedGSO - INSPECTION FOUND THE RT AFT LAVATORY FLOOR PRESSURE WEB CORRODED. THE FLOOR PRESSURE WEB WAS REMOVED, AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-40-2, 51-30-2 AND 51-10-2. (W)SDR CAL950069Blkhd Support · corrodedGSO - INSPECTION FOUND THE RT AFT LAVATORY FWD BULKHEAD SUPPORT CORRODED. THE CORRODED SUPPORT ANGLE WAS REMOVED, AND A NEW ONE WAS INSTALLED IAW SRM 53-10-2, 51-30-2, AND 51-10-1. (W)SDR CAL950068Support · corrodedGSO - INSPECTION FOUND THE FWD LAVATORY AFT WALL I/B CORNER FLOOR SUPPORT STRUCTURE CORRODED AT STA 344, RBL 17. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-10-2, 51-30-2, AND 51-10-2. (W)SDR CAL950067Floor Support · corrodedGSO - INSPECTION FOUND THE FLOOR SUPPORT ANGLE CORRODED AT STA 1070, RBL 30-45. THE CORRODED SECTION OF THE FLOOR SUPPORT ANGLE WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2. (W)SDR CAL950066Floorbeam · corrodedGSO - INSPECTION FOUND LT END OF FLOORBEAM AT STA 1090 CORRODED. THE CORROSION WAS REMOVED AND DOUBLER AND FILLER WERE INSTALLED IAW EC 5310-01102. (W)SDR CAL950065Intercostal · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN CABIN FLOOR INTERCOSTAL AT STA 400-420, BL 0. REMOVED CRACKED INTERCOSTAL TOP ANGLE AND INSTALLED NEW ANGLE IAW SRM 53-10-2, 51-10-1, 51-30-2, AND 51-10-2. (W)SDR MZZA9502Sensor · failureFLT NR 963 - GUM - LEFT GEAR UP LIGHT DID NOT EXTINGUISH ON RETRACTION. ALL GEAR DOORS DID CLOSE. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE FOUND LEFT GEAR UPLOCK SENSOR AT FAULT DURING GEAR UP SIMULATION OF PROX SENSORS. REPLACED SENSOR, PERFORMED GESDR CAL950034Oven · inoperativeTPA - FLT 0591 - SMOKE BEGAN COMING FROM VENTS ABOVE AND ON SIDE OF OVEN IN THE FORWARD GALLEY WHILE IN FLIGHT. CIRCUIT BREAKERS WERE PULLED AND THE SMOKE CEASED. THE LT FORWARD GALLEY OVEN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. THE RT FORWARDSDR CAL950028Transmission · bindingIAH - FLT 0407 - THE INBOARD FLAPS FAILED TO RETRACT INITIALLY DURING FLAP RETRACTION AFTER TAKEOFF. THE FLAPS RETRACTED USING ALTERNATE FLAP RETRACTION PROCEDURES. THE INBOARD FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES DURING LANDING. THE INBOARD FLAPS HAD ASDR 95FDEA00013Wire · chafedNR 3 FUEL ICING LIGHT CAME ON AT LEVEL OFF. ABNORMAL PROCEDURES COMPLIED WITH HOWEVER THE LIGHT REMAINED ON. WE WERE BURNING FROM TANK NR 2 AT THE TIME. FOUND CHAFED WIRE GROUNDED TO ENG CASE NEAR FUEL FITLER PRESSURE SWITCH REPAIRED SAME. NR 3 ENG FUEL DESDR 95FDEA00006Door · req rigFWD ENTRY DOOR OPENED APPROX 3 0R 4 INCHES AFTER A/C WAS DEPRESSURIZED ON TAXI IN AT MEM. RIGGED DOOR IAW MM 52-11-01, PG 514 (3 A-D). REINSTALLED LINER AND SLIDE.
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