JASC 3010
Service difficulty reports · 2,241
Reports filed under 3010 · Airfoil Anti/De-ice System, newest first.
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 jasc_code = '3010' 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 jasc_code = '3010' 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 20001011AP007Clamp · looseGTF - FLT 2550 - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 CELSIUS SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. THE AIRCRAFTSDR 20000717AP006Clamp · looseFLT 2550 - GTF - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 C SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. THE AIRCRAFT WAS SSDR 20000717AP005Clamp · looseFLT 2550 - GTF - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 C SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. THE AIRCRAFT WAS SSDR 20000614SH004Clamp · looseGTF - FLT 2550 - LT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMBOUT. (FLASHING IS 250 C SENSOR). CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LT GEN AND LT BLEED, RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. ACFT WAS SHUT DOWN ONCE CLSDR CA000516009Boot · unbonded(CAN) DURING PREFLIGHT INSPECTION, THE PILOT NOTICED THE DE-ICE BOOT HAD BECOME UNGLUED ON THE TOP FOR A DISTANCE OF ABOUT TWO FEET. THE BOOT WAS REPLACED WITH A NEW UNIT . THE SUBMITTER STATES THAT THE OLD BOOT WAS EASILY REMOVED AND DID NOT APPEAR TO BE PROSDR COMA0060375Sensor · malfunctionedWING OVERHEAT WARNING. REPLACED THE RIGHT HAND WING CONTROL SENSOR.SDR RAIA0004014Switch · failed6113-BOS-CCT, NR 3 DEICE BOOT FAULTED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED DEICE PRESSURE SWITCH.SDR RAIA0004012Boot · failedFLT 7217 - FWA, CIRCUIT NR 1 DEICE FAULT ILLUMINATED DURING TAXI. MAINTENANCE REPLACED RT HORIZONTAL STABILIZER LEADING EDGE.SDR SWIA971756Cover · leakingTHROUGH 10,000 FEET ON CLIMBOUT RIGHT ENGINE DUCT LEAK LIGHT, THREE CHIME AND AURAL WARNING OCCURRED. FOLLOWED QRH PROCEDURE, RIGHT ENGINE WAS SHUTDOWN IN FLIGHT. WARNINGS WENT AWAY AFTER APPROXIMATELY TWO MINUTES, LANDED SINGLE ENGINE AFTER RETURNING TO SFOSDR RAIA0003020Boot · failed7490-STL- SECOND CIRCUIT AIRFRAME DEICE FAULT IN AUTO AND MANUAL MODES DURING TAXI. MAINTENANCE REPLACED RIGHT OUTBOARD LEADING EDGE ASSEMBLY.SDR RRXA001919Baffle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E LWR DE-ICE HOLES BETWEEN STA XFS 322.750 AND 316.500 INSIDE ACCESS PANEL 522A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND SDR COMA0060258Boot · leakingWING DE-ICE FAIL WARNING. REPLACED THE RIGHT WING INBOARD DE-ICE BOOT.SDR SWIA971730Boot · failedAFTER DEPARTURE MIDDLE LEFT WING DEICE BOOT FAILED TWICE. RETURNED TO SFO. OPERATED LEADING EDGE DEICE THROUGH SEVERAL CYCLES, COULD NOT DUPLICATE PROBLEM. SWAPPED LEFT AND RIGHT MIDDLE BOOT DEICE PRESSURE SWITCHES FOR TROUBLESHOOTING, OPS CHECK GOOD.SDR SWIA971727Boot · failedINBOARD RIGHT STABILIZER AMBER CAUTION LIGHT ILLUMINATED IN FLIGHT WITH LEADING EDGE DEICING SYSTEM OPERATING. RETURNED TO SFO. REPLACED BAD PRESSURE SWITCH FOR RIGHT INBOARD STABILIZER BOOT. RAN BOTH ENGINES. CYCLED BOOTS SEVERAL TIMES, ALL CHECKS GOOD.SDR 0000859852Duct · dirtyDURING APPROACH INTO MKE, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ASSOCIATED ROLL TO THE LEFT ON SLAT EXTENSION. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED USING FLAPS ONLY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBRICATED ANTI-ICE TESDR CA000306005Regulator · failed(CAN) GASKET FOUND BLOWN OUT FROM NR 2 POSITION AFT DE-ICE PRESSURE REGULATOR. NR 2 AFT DE-ICE REGULATOR REPLACED.SDR SWIA971706Switch · failedOUTBOARD RIGHT STABILIZER FAILED ON BOTH TIMERS 1 AND 2. RETURNED TO THE FIELD. REMOVED AND REPLACED OUTBOARD HORIZONTAL STABILIZER PRESSURE SWITCH. ALSO, REMOVED AND REPLACED HORIZONTAL STABILIZER OUTBOARD EJECTOR VALVE. OPS CHECKS GOOD, PN ON: 211C11718SDR CA000301014Poppet Valve · damaged(CAN) POPPET CAME APART INSIDE UNIT CAUSING MALFUNCTION. FRAGMENTS FOUND IN EJECTION TUBE.SDR SWIA971701Regulator · failedVERTICAL FIN AND RT O/B STAB DEICE BOOTS INOP IN CLIMB AND CONTINUING 7,000 TO 12,000 MSL UNABLE TO RESET TIMER 1 AND 2 WORKED OK ON GROUND RETURNED TO SLC. REMOVED AND REPLACED VERTICAL FIN BOOT IAW MM 301000 (S/N MF92350) ON, (S/N M325040) OFF. REMOVED SDR SWIA971699Switch · failedOUTBOARD RIGHT STABILIZER INOP, LIGHT ILLUMINATED IN FLIGHT. CYCLED THROUGH BOTH TIMERS AS WELL AS HEAVY AND LIGHT MODES. DIVERTED FROM MCE TO FAT. REPLACED RIGHT OUTBOARD STABILIZER DEICE PRESSURE SWITCH AND INSTALLED THREE DEICE PATCHES, OPS CHECKS GOOD.SDR SWIA971694Switch · failedI/B LEFT STABILIZER DEICE LIGHT ILLUMINATED IN FLIGHT, LIGHT CAME ON TIMERS 1 AND 2 AND REMAINED ON WITH SWTICH OFF. RETURNED TO PDX. REPLACED I/B LEFT STABILIZER PRESSURE SWITCH IAW MM 30, OPS CHECKS GOOD. (S/N N122) ON, (S/N L216) OFF.SDR MALA000155Deice Module · malfunctionedLT ENGINE INTAKE LIGHT ILLUMINATED. MX REMOVED AND REPLACED DE-ICE MODULE IAW SP340, CHAPTER 30, RAN FOR 30 MINUTES. ALL OPS CHECK GOOD.SDR A6WA0000016Ejector Valve · failedAIRFOIL DE-ICE FAILED IN FLIGHT IN ALL MODES. REMOVED AND REPLACED LEFT AND RIGHT EJECTOR FLOW CONTROL VALVES AND PATCHED SEVERAL HOLES IN LT WING OUTBOARD BOOT AND RIGHT INBOARD BOOT. P/N''S REMOVED 3D3556-01 S/N''S LT 0922 TSN 3507:22 CSN 4332, RIGHT S/N 0SDR SWIA971692Warning Light · illuminatedLEADING EDGE VERTICAL FIN LIGHT ILLUMINATED ON ICE PROTECTION PANEL. RETURNED TO PDX. INSTALLED SERVICEABLE VERTICAL FIN DEICE BOOT IAW 301000, OPS CHECK GOOD. (P/N 29S70513539) ON, (S/N ME27100) ON, (S/N ME314140) OFF.SDR RAIA0002003Thermostat · failed6309 - BOS - HORIZONTAL STABILIZER ANTI-ICE FAILED IN FLIGHT. MAINTENANCE REPLACED STABILIZER BLEED LEAK THERMOSTAT.SDR 20000808SH019Check Valve · failedDURING ROUTINE MAINTENANCE, DISCOVERED 2 UNSERVICEABLE CHECK VALVES, PN''S 1H37-4, FOR THE PNEUMATIC DEICE SYSTEM. BOTH VALVES HAVE 21 MONTHS AND 705.1 HOURS SINCE NEW. THESE VALVES CALL FOR YEARLY INSPECTIONS STARTING AT 5 YEARS FROM NEW THOUGH 10 YEARS REPSDR SWIA971679Deice Boot · damagedRIGHT OUTBOARD WING DEICE FAILED ON BOTH TIMER. RETURNED TO SFO. PATCHED HOLE IN RIGHT OUTBOARD WING DEICE BOOT. RAN ENGINES, OPS CHECK GOOD.SDR COMA0010017Deicer · leakingHORIZONTAL STABILIZER DE-ICE FAILED. REPLACED THE LEFT HORIZONTAL STABILIZER DE-ICE BOOT.SDR RAIA0001026Switch · failed6315 - BOS - STABILIZER ANTI-ICE FAIL EICAS MESSAGE CAME ON, VALVE OPEN INDICATION ON ICE PROTECTION PANEL DID NOT ILLUMINATE. MAINTENANCE DEFERRED PER MEL. MAINTENANCE REPLACED ICE PROTECTION PANEL OPEN INDICATOR SWITCH.SDR 00FDEA00041Tube · failed00-22 AT CR FL 310 SEL, WING ANTI-ICE ON, HAD NR 1 MANIFOLD FAILURE LIGHT ILLUM. PNEU SUPPLY OFF FOR NR 1 ON FOR 2/3, ISOL VLV 1-2 OPEN AT TIME OF FAILURE. REMOVED AND REPLACED NR 4 L/E SLAT PER DC10-30 MM 27-80-01-4-2, LEAK AND OPS CK GOOD. INSTALL NR 4 SSDR DHL200080327CDeflector · missingAT C-CHECK, NR 3 ENGINE INLET COWL ANTI-ICE DEFLECTOR MISSING 2 O''CLOCK. COMPLIED WITH S/B 71-97. N/R 7126SDR DHL200080325CDeflector · missingAT C-CHECK, NR 4 ENGINE INLET COWL ANTI -ICE DEFLECTOR MISSING AT 11 O''CLOCK POSTION. PERFORMED S/B 71-97. N/R 7127.SDR CA000201017Boot · detached(CAN) CREW REPORTED A SEVERE VIBRATION CLIMBING THROUGH 10,500 FEET. THE CREW DECENDED, DECLARED AN EMERGENCY AND RETURNED FOR LANDING. MAINTENANCE FOUND THE LT HORIZONTAL STABILIZER BOOT HAD BEGUN TO DETACH FROM THE LEADING EDGE.SDR AU000201017Deice Boot · detached(AU) CREW REPORTED A SEVERE VIBRATION CLIMBING THROUGH 10,500 FEET. THE CREW DESCENDED, DECLARED AN EMERGENCY AND RETURNED FOR LANDING. MAINTENANCE FOUND THE LT HORIZONTAL STABILIZER BOOT HAD BEGUN TO DETACH FROM THE LEADING EDGE.SDR AALA20000051Valve · failedLGA - FLT 1911 - ON CLIMB-OUT WITH POWER IN CLIMB AND WING AND ENGINE ANTI-ICE SELECTED THE AIRFOIL ICE PROTECTION, ABNORMAL LIGHT ILLUMINATED WITH LEFT/RIGHT ICE PROTECTION LOW AND LEFT AIRCRAFT SUPPLY TEMPERATURE HIGH LIGHTS ILLUMINATED. ACCOMPLISHED PROCEDSDR SWIA971642Boot · failedRIGHT INBOARD STAB BOOT FAILED ABOVE 10,000, RESET ON DESCENT BELOW 10,000. RETURNED TO SEA. PERFORMED FUNCTIONAL TEST OF EMPENNAGE LEADING EDGE DE-ICERS USING ENGINE PNEUMATIC POWER PER MM 301000. SYSTEM OPERATED PER FUNCTIONAL TEST REQUIREMENTS, UNABLE TOSDR COMA9960818Check Valve · malfunctionedRIGHT WING ANTI-ICE CAUTION MESSAGE. REPLACED THE RIGHT HAND BLEED AIR CHECK VALVE.SDR COMA0060008Anti-Ice System · malfunctionedRIGHT WING ANTI-ICE DUCT WARNING. REPOSITIONED WIRE TERMINAL AT T/B 44WK THAT WAS SHORTED TO GROUND.SDR COMA9960816Warning System · activatedANTI-ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED SYSTEM, NO DEFECTS FOUND. OPERATIONAL CHECK NORMAL.SDR 2000ZZZX107Deice Element · mismanufacturedHORIZONTAL STABILIZER ANTI-ICE LEADING EDGE. THIRD NEW LEADING EDGE RECEIVED FROM CESSNA KS. HAS ONE TEMPERATURE SWITCH BROKEN LOOSE FROM MOUNTING POINT. DEFECT FOUND DURING RECEIVING INSPECTION. SUBMITTER RECOMMENDED NEW TYPE OF BONDING OF TEMPERATURE SWISDR 2000ZZZX108Deice Element · mismanufacturedHORIZONTAL STABILIZER ANTI-ICE LEADING EDGE. SECOND NEW L/E RECEIVED FROM CESSNA KS. HAS TWO HEATING ELEMENT DEFECTS, ONE 26 INCHES FROM OUTBOARD EDGE AND ONE 15 INCHES FROM OUTBOARD EDGE. DEFECTS FOUND DURING RECEIVING INSPECTION.SDR 2000ZZZX106Deice Element · mismanufacturedHORIZONTAL STABILIZER ANTI-ICE LEADING EDGE. NEW FROM CESSNA KS HAD ONE TEMP SWITCH LOOSE IN MOUNTING, AND ONE TEMP SWITCH BROKEN OUT OF MOUNTING POINT. LEADING EDGE IS ELECTRICALLY HEATED. LOSS OF TEMPERATURE CONTROL WILL RESULT AND ALSO LOSS OF ANTI-ICE PRSDR QXEA9902644Connector · corrodedPDX - INSPECT DEICE DISTRIBUTOR CANNON PLUGS AND PRESSURE SWITCHES FOR CORROSION AND SERVICEABILITY. REMOVED AND REPLACED PRESSURE SWITCHES. (S/N 6503, 3509, 7020 AND 6951).SDR SWIA971627Switch · failedDURING CLIMB-OUT, MIDDLE RIGHT WING LIGHT ON THE LEADING EDGE OVERHEAD ICE PANEL ILLUMINATED. RETURNED TO SEA. REMOVED AND REPLACED RIGHT WING MIDDLE DE-ICE PRESSURE SWITCH IAW MM 301005. OPS CK GOOD, SN ON: 0115 SN OFF: 0497.SDR COMA9960758Sensor · malfunctionedLEFT WING ANTI-ICE MESSAGE. REPLACED THE LEFT WING TEMP SENSOR.SDR 99FDEA00494Warning Light · illuminatedNR 3 PNEUMATIC FAIL LIGHT ILLUM. COMPLETED RED TABS.SDR CA991208043Sensor · shorted(CAN) AIR LOW TEMP WARNING LIGHT ON IN-FLIGHT WITH WING DEICE SELECTED ON. NR 4 DUCK OVERTEMP SWITCH SHORTED CAUSING AIR VALVE TO CLOSE RESULTING IN LOW PRESSURE. OVERTEMP SWITCH REPLACED.SDR 2000ZZZX224Deice System · inoperativeNOTED THAT DE-ICE FOR VERTICAL STABILIZER INOPERATIVE. FURTHER INVESTIGATION REVEALS HOSES TIED OFF. REPLACED HOSES, PATCHED BOOT. OPS CHECKED, WORKS FINE. TOATL TIME AT INSTALLATION UNKNOWN.SDR CA991208017Deice Boot · leaking(CAN) FLIGHT CREW REPORTED THAT THE RIGHT NR 3 LEADING EDGE DEICE BOOT WOULD NOT INFLATE. MAINTENANCE FOUND THE DEICE BOOT TO BE INTERNALLY CONTAMINATED WITH WATER. SUBMITTER SUGGESTED WATER ENTERED THROUGH A NUMBER OF HOLES INCLUDING ONE HOLE WHICH HAD BEENSDR SWIA971604Deice Boot · failedOUTBOARD, MIDDLE LEFT WING AND VERTICAL STABILIZER DEICE BOOTS FAILED. RETURNED TO SLC. REMOVED AND REPLACED DEICE MONITOR IAW 30-00-01, OPS CHECKS GOOD.
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