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 2000UALA00113Switch · malfunctionedUPON SLAT RETRACTION AFTER TAKEOFF, NR 5 SLAT INDICATED DOWN. CYCLED SLATS AND NR 5 REMAINS AMBER ON BOTH FORWARD AND AFT PANELS. RETURNED TO ORD. *S/D* REPLACED LEADING EDGE FLAP POSITON SWITCH NR 5 PER 27-85-01. OPERATIONALLY CHECKS NORMAL.SDR 2000UALA00112Circuit Breaker · faultyCIRCUIT BREAKER POPPED WHEN RADAR TURNED ON. RETURNED TO DEN. *S/D* AFTER SEVERAL LRU REPLACEMENTS, MAINTENANCE REPLACED THE T/R CIRCUIT BREAKER C862, NO FURTHER PROBLEMS WITH CIRCUIT BREAKER TRIPPING REPORTED.SDR 2000UALA00111Cooling Fan · failedON GROUND AT YVR, LEFT PACK TRIPPED WHEN TURNED ON AND SMOKE IN CABIN. COOLING FAN DID NOT COME ON. *S/D* COOLING FAN FOR PACK NOT TURNING ON. REPLACED COOLING FAN.SDR 2000UALA00109Coffeemaker · smokeAFT GALLEY COFFEEMAKER SMOKING AND SPARKING. *S/D* INSPECTED AREA WITH COFFEEMAKER ON, NO PROBLEMS. INSPECTED COFFEEMAKER AND MATING RECEPTACLE FOR SIGNS OF ARCING. CLEANED WET AREA AROUND COFFEEMAKER, NO CHAFING OR ARCING NOTED. REPLACED COFFEEMAKER PRECSDR 2000UALA00108Valve · malfunctionedUNABLE TO CONTROL CABIN ALTITUDE AT 24,000 FT. MANUAL OR STANDBY NO HELP. OUTFLOW VALVE INDICATED CLOSED. DESCENDED TO I0,000 AND REGAINED MANUAL CONTROL. RETURNED TO BNA. *S/D* THE CAUSE MAY HAVE BEEN A FAILURE OF THE LEFT CABIN OVER PRESSURE RELIEF VALSDR 2000UALA00106Receiver · failedBOTH NAVIGATION RECEIVERS ARE UNUSABLE BEYOND A 38 MILE RADIUS OF ANY VOR STATION. CREW NEEDED ATC ASSISTANCE WITH RADAR VECTORS TO FIND LAX. *S/D* REPLACED NR 1 NAV RECEIVER.SDR 2000UALA00104Bolt · looseCANNOT MOVE YOKE FORWARD DURING FLIGHT CONTROL CHECK. MOVES AFT NORMALLY. *S/D* FOUND BOLT AT LT ELEVATOR PCU TAB ROD ON FWD END BACKED OFF ANDINTERFERING WITH ELEVATOR MOVEMENT. REPLACED APPROPRIATEHARDWARE WITH NEW. OPERATIONALLY CHECKS GOOD.SDR 2000UALA00103Seal · tornUNABLE TO CONTROL PRESSURIZATION. RETURNED TO ORD. *S/D* FOUND LOUD SQUEAL AT DOOR 1L- UPPER CORNER OF DOOR SEAL TORN. REPAIRED SEAL PER MM 52-00-02 AND DOOR WAS RIGGED PER MM SPECS.SDR 2000UALA00100Nut · missingRIGHT MAIN LANDING GEAR FAILED TO EXTEND FOR LANDING AT DEN. USED MANUAL EXTENSION AND LANDED WITHOUT INCIDENT. *S/D* FOUND BOLT BACKED OUT OF LINK (NUT MISSING) AT RT MAIN LANDING GEAR DOOR OPERATED SEQUENCE VALVE. REINSTALLED BOLT AND NUT. OPS CHECKED GSDR 20000410AP005Fire Loop · out of adjFLT 112 - MDT - NR 3 GROUND FAULT LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 3 FIRE LOOP. (M)SDR 2000UALA00086Actuator · malfunctionedNR 1 LEADING EDGE FLAP DID NOT RETRACT ON CLIMBOUT AT FLAPS POSITION 2 BACK TO POSITION 5. RETURNED TO ORD. *S/D* REPLACED NR 1 L/E FLAP ACTUATOR PER MM 27-83-06. OPERATIONAL CHECK NORMAL. CHECKED ADJUSTMENT OF NR 1 L/E FLAP POSITION SWITCH PER MM 27-85-0SDR 2000UALA00080Accessory Unit · failedLEFT MAIN LANDING GEAR FAILED TO RETRACT. GEAR HANDLE WOULD NOT COME UP. RETURNED TO DEN. *S/D* REPLACED LANDING GEAR ACCESSORY UNIT PER MAINTENANCE MANUAL. SYSTEM CHECKS OK. NOTE: ALSO ENTERED ITEM TO REPLACE LG HANDLE LOCK SOLENOID AS PRECAUTIONARY ACSDR 2000UALA00079Actuator · leakingDIVERTED TO DEN DUE TO A HYDRAULIC SYSTEM PRESSURE AND FLUID LOSS. *S/D* FOUND NR 2 L/E FLAP ACUATOR LEAKING FROM SWIVEL. REPLACED NR 2 L/E FLAP ACTUATOR, OPERATIONAL CHECK AND LEAK CHECK PERFORMED. SYSTEM OPERATIONAL OK. NO LEAKS NOTED.SDR 2000UALA00077Splice · faultyALL CABIN EMERGENCY LIGHTS ILLUMINATED WITH FLIGHT DECK SWITCH IN THE ARMED POSITION. *S/D* REPAIRED FAULTY SPLICE SM34. EMERGENCY LIGHT OPERATION RESTORED TO NORMAL.SDR 2000UALA00070Rod · brokenLIGHT SMOKE IN CABIN. MAINTENANCE NOTICED SPARKS FROM FLOW MULTIPLIER. *S/D* BROKEN SUPPORT ROD CAUSED FAILURE OF FLOW MULTIPLIER, UNIT SEIZED. REPLACED FLOW MULTIPLIER AND ROD.SDR 2000UALA00071Fitting · corrodedDURING A HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON THE LUG HOLE OF THE VERTICAL STABILIZER UPPER CLOSURE RIB FITTING (P/N 65-4233-16). THE CORROSION WAS REMOVED BY SPOTFACING AND OVERSIZING OF THE LUG BORE. A BUSHING WAS INSTALLED TO RESTORE THE HOLE TOSDR 2000UALA00064Connector · dirtyAFTER TAKEOFF, THE NR 2 LEADING EDGE FLAP INDICATOR DISPLAYED INTRANSIT AND THE NR 2 SLAT AMBER LIGHT WAS ILLUMINATED. RETURNED TO YYZ. *S/D* CLEANED NR 2 FLAP CONNECTOR AND OPERATION CHECKED NORMAL.SDR 2000UALA00065Seat · looseSEAT ROW 16ABC INBOARD FOOT LOOSE. *S/D* SHEARED RIVETS ON ANCHOR NUT. REF:IPC 25-00-XX-060K ITEM 16-17) HAVE SHEARED OFF DUE TO INCORRECT INSTALLATION OF SEAT ASSEMBLY. BRACKET (PCN 020-1834) WAS REPLACED BY LINE AMT.SDR 2000UALA00062Spar · crackedDURING INSPECTION PER S/B 727-57A0182 AS MANDATED BY AD97-25-15 ON THE REAR SPAR WEB, RBL 34.00, ONE FASTENER HOLE WAS FOUND CRACKED. FATIGUE THE FASTENER HOLE WAS OVERSIZED UNTIL THE CRACK WAS REMOVED (0.327 IN DIA) AND VERIFIED WITH NDT. THEN OVERSIZED TO SDR 2000UALA00057Shutoff Valve · stuckUNABLE TO CONTROL CABIN PRESSURE ON CLIMBOUT OF DEN. RETURNED TO DEN. CORRECTED THE AIRCRAFT FROM 7762 TO 7763. *S/D* ENG 3 BLEED SHUT OFF VALVE STICKING. REPLACED ENG 3 SHUTOFF VALVE.SDR 2000UALA00047Seat · looseSEAT 12 ABC APPEARED TO BE LOOSE IN TRACK. *S/D* FINDINGS INDICATE FORWARD ATTACH POINT EXTENDED TOO FAR PUTTING PRESSURE ON MONEL RIVETS RATHER THAN ON ATTACH BRACKET. ISOLATED INCIDENT.SDR 2000UALA00046Battery Pack · failedRIGHT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT STAYS ON. *S/D* REPLACED BATTERY AND PACK. OPERATIONAL CHECK NORMAL.SDR GAIA0045Flap · malfunctionedFLT 1760 - FWA-MEM - THE CREW RAISED THE FLAPS AND HAD THE OUTBOARD FLAPS STICK AT 4 DEGREES. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. MAINTENANCE USED THE ALTERNATE METHOD TO RAISE THE FLAPS TO ZERO DEGSDR 2000UALA00036Switch · failedAIRCRAFT RETURNED TO DEN AFTER NR 5 LEADING EDGE FLAP WOULD NOT RETRACT. *S/D* ADJUSTED NR 5 LEADING EDGE FLAP SWITCH. INDICATIONS AND OPERATION NORMAL PER MAINTENANCE MANUAL.SDR 2000UALA00033Module · failedAFTER TAKEOFF FROM DEN ON RETRACTION OF LEADING EDGE FLAPS FROM 5 TO 2 THE GREEN LIGHT REMAINED ILLUMINATED. THE SECOND OFFICERS FLAP PANEL SHOWED FLAP NR 5 EXTENDED. RETURNED TO DEN. *S/D* MEGGERED WIRES. WIRES CHECK OK. REPLACE L/E FLAP SWITCH AND L/E SDR 2000UALA00031Seat · looseSEATS 3A AND 3B LOOSE NOT ATTACHED TO FLOOR PROPERLY. *S/D* UNKNOWN CAUSE FOR LOOSE SEAT ASSYS, NO RECENT MAINTENANCE ACTION IN THIS AREA. SUBSEQUENT FIX WAS TO TIGHTEN SEAT ATTACH FITTINGS.SDR 2000UALA00049Slide · leakingDURING SHOP OVERHAUL PROOF PRESSURE TEST EVACUATION SLIDE MR 25699-447 FAILED TO HOLD AIR. THE LEAK WAS AT THE JOINT BETWEEN THE ASPIRATOR TUBE AND THE SLIDE MAIN TUBE. SENT SLIDE ASSEMBLY TO VENDOR FOR WARRANTY REPAIR.SDR 2000UALA00024Duct · leakingJUST AFTER TAKEOFF ROTATION, NR 3 FIRE BELL/WARNING ALERTED. ENGINE SHUT DOWN. LIGHT WENT OUT AND BELL SILENCED. RETURNED TO BUFFALO. *S/D* 8TH STAGE PNEUMATIC EXTENSION DUCT BETWEEN SADDLE DUCT AND STUB WING LEAKING. REPLACED DUCT AND NO LEAKS WERE NOTESDR 2000UALA00016Gasket · missingNR 1 STRUT OVERHEAT LIGHT ON, BLEEDS ON AND BLEEDS OFF. PULLED THROTTLE BACK TO IDLE AND SHUT BLEED OFF AND LIGHT EVENTUALLY WENT OUT. INCREASED THROTTLE TO APPROXIMATELY 92 PERCENT AND LIGHT CAME ON AGAIN. RETURNED TO AUS. *S/D* MASSIVE LEAKS WERE FOUND SDR 2000UALA00017Rib · crackedDURING INSPECTION PER SB 727-57-0112 AS MANDATED BY AD94-07-08 ON THE LBL 70.5 RIB CHORD AT STATION 760.95, TWO CRACKED FASTENER HOLES WERE FOUND. CAUSE WAS FATIGUE. BOTH HOLES WERE OVERSIZED UNTIL THE CRACKS WERE ELIMINATED AND OVERSIZED FASTENERS INSTALLEDSDR 2000UALA00015Battery · failedLEFT WING FORWARD DOOR EXIT LIGHT INOPERATIVE. *S/D* REPLACED BATTERY, CHECKS GOOD.SDR 2000UALA00014Landing Gear · failedUNABLE TO RETRACT NOSE GEAR . RETURNED TO ORD. *S/D* PERFORMED GEAR SWING. OPS CHECKED NORMAL ON GROUND. NOTE: ENGINEERING CALLOUT WAS ADDED TO REPLACE NLG RETRACT ACTUATOR, NLG LOCK ACTUATOR, TRANSFER CYLINDER AND RESTICTOR AS PREVENTATIVE ACTION.SDR 2000UALA00013Regulator · failedON CLIMBOUT OF ORD, NR 2 DUCT OVERHEAT OCCURRED WITH ANTI-ICE ON. RETRACTED THROTTLE NR 2 AND DUCT TEMPERATURE REDUCED AND STABLIZED. *S/D* THERMOSTATIC REGULATOR REPLACED.SDR 2000UALA00012Elbow · crackedWITH FUEL PANEL CONFIGURED TO BURN OUT OF NR 2 TANK ONLY, 900 POUNDS OF FUEL WERE USED FROM TANK NR 3. ALL X-FEEDS WERE OPEN AND FORWARD PUMPS WERE OFF IN TANKS NR 1 AND NR 3. AFTER CORRECTING IMBALANCE BETWEEN TANKS NR 1 AND NR 3, RECONFIGURED FUEL PANEL TOSDR 2000ZZZM188Duct · crackedFLT 0114 - BWI - CLIMB-OUT, NR 1 STRUT OVERHEAT, ACCOMPLISHED CHECKLIST AND LIGHT REMAINED OUT. REPLACED NR 1 ANTI-ICE SHUTOFF VALVE DUCT. (M)SDR 2000UALA00011Control Cable · out of adjLEADING AND TRAILING FLAPS STOPPED BETWEEN 3 AND 5. *S/D* INSPECTED SYSTEM AND FOUND 3-32ND CABLES WFA AND WFB AT 25 LBS. HANDLE WAS SLUGGISH IN EITHER DIRECTION. ADJUSTED CABLES TO 58 LBSAT 60 DEG. HANDLE OPERATION SMOOTH AND FLAPS OPERATING WITHINNORMASDR 2000UALA00008Actuator · bypassingRIGHT MAIN GEAR DOOR OPEN IN FLIGHT AT 305 IAS. RECYCLED GEAR TO UP AND OFF. LIGHT WENT OUT. *S/D* REPLACED RIGHT MLG DOOR ACTUATOR PER MAINTENANCE MANUAL. OPS CHECK OK. SERVICED HYDRAULICS TO FULL.SDR 2000UALA00007Bypass Valve · leakingHYDRAULIC SYSTEM A PRESSURE AND QUANTITY ZERO. ENGINES 1 AND 3 PUMPS LIGHTS ON APPROXIMATELY 5 MINUTES AFTER ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ON. CONTINUED TO DESTINATION. *S/D* FOUND ELEVATOR HYDRAULIC BYPASS VALVE ASSEMBLY DAMAGED AND LEAKING. SDR 99UAL900662Light · inoperativeRIGHT EXTERIOR OVERWING EMERGENCY LIGHTS INOP.SDR 99UAL900660Fire Loop · out of positionENGINE 1 STRUT OVERHEAT LIGHT CAME ON. COMPLETED IN FLIGHT ENGINE SHUTDOWN, LIGHT REMAINED ON. *S/D* THE STRUT OVERHEAT LIGHT ILLUMINATION IN-FLIGHT WAS AN INDICATION PROBLEM. ALL DUCTS WERE FOUND INTACT. THE OVERHEAT LOOP WAS FOUND RESTING ON THE 13TH STSDR GAIA99267Case · damaged'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND FIBERGLASS PATCH DETERIORATED AND PEELING AT THE 12 O'CLOCK POSITION BETWEEN IGV HEAT VALVES AND SIX INCHES AFT ON OUTER CASE OF NR 3 ENGINE. SDR GAIA99266Strap · damaged'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND 9G BUYLKHEAD SAFETY STRAP DRILLED INTO STR 2-3L. REAPIRED IAW ATS EDR 99-002 AND BOEING SRM. AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GAIA99264Floorbeam · damaged'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND FLOORBEAM AT STA 400, BL 44 HAS DOUBLE DRILLED HOLES. REPAIRED IAW ATA EDR 99-008 AND BOEING SRM. AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GAIA99263Stringer · corroded'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND CORROSION ON STR S20R, STA 990. REMOVED AND REPLACED STR S20R, STA 990 IAW BOEING SRM. AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GAIA99262Fitting · gouged'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). UPON REMOVAL OF LT WING AFT BOTTLE BOLT BUSHING, FOUND INNER RACE GOUGED. REPAIRED GOUGE IAW REO W00008 AND 8110-3, DATED 12-2-99. AIRCRAFT WAS RETSDR GAIA99261Fitting · damaged'NO FLIGHT' - FOUND DURING HEAVY C-MAINTENANCE CHECK AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND STA 940 FITTING MISDRILLED. REPLACED STA 940 FITTING IAW BOEING SB 727-53-0018 AND BOEING DRAWING 65C15732. AIRCRAFT WAS RETURNED TO SERVICE.SDR GAIA99260Floorbeam · damaged'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND ONE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 380, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22035, AND 8110-3, DATED 11-1-99. AIRCRAFT WSDR GAIA99259Floorbeam · damaged'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND ONE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 440, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22034, AND 8110-3, DATED 11-1-99. AIRCRAFT WSDR GAIA99258Floorbeam · damaged'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND ONE EACH DOUBLE DRILLED HOLE ON FLOOR BEAM CAP AT STA 460, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22033, AND 8110-3, DATED 11-1-99. AIRCRAFT SDR GAIA99257Floorbeam · damaged'NO FLIGHT' - FOUND DURING 'HEAVY C-MAINTENANCE CHECK' AT TIMCO HEAVY MAINTENANCE FACILITY (WINSTON/SALEM, NC). FOUND ONE EACH DOUBLE DRILLED HOLE ON FLOORBEAM CAP AT STA 480, LBL 64. C/W REPAIR IAW RFTS 180AX-36-22032, AND 8110-3, DATED 11-1-99. AIRCRAFT W
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