JASC 2700
Service difficulty reports · 1,745
Reports filed under 2700 · Flight Control 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 = '2700' 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 = '2700' 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 CALA2022032300762Proximity Sensor · failedLEADING EDGE TRANSIT LIGHT FROM FLAPS 5 TO 10 PERFORMED FSEU BITE LAST LEG FAULT FOR SL7 PROX O/B MSG: 27-81212. DURING INTIAL EVALUATION PER FIM 27-88 TASK 803 FOUND ON FULL EXTENDED SLATS S7 O/B PROX WAS SHOWING FAR INSTEAD OF NEAR REMOVED AND REPLACED #7 SLSDR CALA2022032100717Servo Valve · unserviceableRUDDER RATIO EICAS C THE RUDDER RATIO SYSTEM HAS A FAILURE. COMPLIED WITH FIM 27-09-00-815-814 & 27-09 FAULT TREE 814. NO CURRENT OR HISTORY FOUND REMOVED AND REPLACED THE RUDDER ELECTRO HYDRAULIC SERVO VALVE IA W AMM 27-21-15-422-024. OPS AND LEAK CHECKS GOODSDR A6WA202203188133None · noneLOST RUDDER TRIM IN FLIGHT. RUDDER TRIM FULL DEFLECTION NL. RUDDER TRIM SWITCH WILL NOT MOVE NR. A/C CONTROLLABLE WITH RH RUDDER INPUT. DIVERTED TO BUF, SMOOTH LANDING AT 47,100LBS ***AIRCRAFT REMOVED FROM SERVICE*** R&R AILERON/RDR TRIM PANEL IAW AMM 27SDR SWIA202265269None · failedLH ELEVATOR INBD PCU FAILED BACKLASH (C-CHECK RO 4/2/2022) REMOVED AND REPLACED THE BOLT, BUSHING AND NUT FOR THE LH ELEVATOR INBOARD PCU. SEE CONTINUATION CARD FOR WORK PERFORMED. PERFORMED BACKLASH TEST OF THE LH ELEVATOR IBD PCU. BACKLASH TEST GOOD ASDR AALA202203152557Computer · defectiveAIRCRAFT WAS NOT GROUNDED: ON CLIMB OUT, AIRCRAFT MAINTAINS A 3 DEGREE RIGHT BANK AIRCRAFT APPEARS TO BE IN TRIM, IN CLIMB ABOVE 10000 FT, CRUISE AND DECENT AIRCRAFT FLIES NORMAL. REPLACED #1 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34.SDR CALA2022031000633Transmitter · failedLEADING EDGE FLAPS AND SLATS DO NOT EXTEND DURING NORMAL SYSTEM OPERATION LOCKED L/P UNLOCKED TO UPDATE LOCKED DUE TO FAULT CODE 27-52261 FOUND DURING FSEU BITE PLEASE REMOVE PERFORMED FSEU BITE PROCEDURE 27-51 TASK 801 NO EXISTING FAULS AND REPLACE LEFT FLAPSDR CALA2022030700583Module · failedLE SLAT AND TE FLAP DISAGREE BWN F20 AND 25 DID GO AROUND AND DI D QRH LOCKED TO CONFIRM FIX UNLOCKED TO UPDATE LOG PAGE LOCKED FOR FIX CREW DEBRIEF - CREW STATED FLAP HANDLE SELECTED TO 25 AND FLAPS UPON ARRIVAL FOUND FLAPS STUCK AT 22 AND FLAP HANDLE BINDINSDR AALA202203032334Computer · warning messageAIRCRAFT WAS GROUNDED: ELAC 1 AND 2 PITCH FAULT DURING CRUISE. FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO PHX LANDING SAFELY. REPLACED ELEVATOR AND AILERON COMPUTER #1 (AALA202203032334) PER AMM 27-93-34, AND REPLACED SPOILER AND ELEVATOR COMPUTER #1 (AALA20SDR AALA202203033552Secu · unserviceableAIRCRAFT WAS GROUNDED: ELAC 1 AND 2 PITCH FAULT DURING CRUISE. FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO PHX LANDING SAFELY. REPLACED ELEVATOR AND AILERON COMPUTER #1 (AALA202203032334) PER AMM 27-93-34 AND REPLACED SPOILER AND ELEVATOR COMPUTER #1 (AALA202SDR A6WA202203028119None · noneAILERON TRIM SLIGHTLY OUT OF ZERO R WING DOWN. WILL NOT RESPOND TO L WING DOWN TRIM SWITCH MOVEMENTS. POSITIONED TO ZERO P2-F7 COLLARD C/B P2-F7. PLACARDED AND PLACED ON MEL. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED AILERON/RUDDER TRIM PANELSDR SWIA202265150None · misalignedRUDDER LOWER PCU ATTACH FITTING LOWER HAT BUSHING MIGRATED. (C CHECK RO 3-21-22) REPLACED RUDDER LOWER PCU ATTACH FITTING LOWER HAT BUSHING ON RACK. REF EMB 175 AMM 20-10-08. FINAL INSTALL OF RUDDER PCU FITTING ON CAMP 24320822SDR SWIA202265149None · damagedRUDDER UPPER AND LOWER PCU ATTACH BOLTS ARE SCORED. (C CHECK RO 3-21-22) REPLACED RUDDER UPPER AND LOWER PCU ATTACH BOLTS ON RACK. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05SDR UIEA2022021700145Skin · dentedRHW #18 VC-FLAP BALLNOSE SKIN LWR MID AREA FOUND DENT(<P>RHW #18 VC-FLAP BALLNOSE SKIN LWR MID OUT OF LIMITS DENT AREA EXTERNAL DOUBLER REPAIRED</P>)SDR UIEA2022022200153Flap · delaminatedRHW O/B MID FLAP L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2022022200154Flap · delaminatedRHW I/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)SDR UIEA2022022200155Flap · delaminatedLHW I/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)SDR UIEA2022022200156Flap · delaminatedLHW O/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)SDR UIEA2022022200158Flap · delaminatedRHW O/B AFT FLAP AFT O/B CORNER FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5G</SPAN></P>)SDR UIEA2022022200160Flap · delaminatedRHW O/B FORE FLAP L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2022022200161Flap · delaminatedLHW O/B AFT FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)SDR UIEA2022022200162Flap · delaminatedRHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)SDR CALA2022022400499Sensor · failedLE FLAPS EXT FLICKERD ON TAKEOFF INIT PWR UP GOT TAKEOFF CONFIG WRN ABORTED T/O APPX 10KTS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. ACCOMPLISH FSEU BITE, CONTACT TOMC. PER FIM 27-88 TASK 805 FOUND RECENT LEG SDR SWIA202265147None · failedRH ELEVATOR OUTBOARD PCU FAILED BACKLASH FUNCTIONAL TEST. (C CHECK RO 3-21-22) / REMOVED AND REPLACED RH ELEVATOR OB PCU TO ELEVATOR BOLT AND BUSHING. RETESTED BACKLASH, BACKLASH GOOD AT THIS TIME. REF. E175 AMM 27-32-01 AND AMM 27-30-00. TORQUE WRENCH ASSDR O2GA2022030186501None · noneON APPROACH, THE FLAPS DID NOT EXTEND FROM THE APPROACH POSITION TO THE SELECTED DOWN POSITION. FOLLOWED CHECKLIST AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE FLAP APPROACH DOWN LIMIT SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND SDR A6WA202202218115None · noneRECEIVED STALL FAIL CAUTION AT 500'. C/W QRH. DIVERTED TO DAY. ON GROUND PERFORMED GPWS TEST, GPWS FAIL STATUS MSG POSTED. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED GPWS TEST TO CLEAR GPWS FAIL MESSAGE. IAW AWA SUP 20-137. ALSO PERFORMED TEST OF SDR YENA2022021800081None · noneFLT # 1573, EWR-LAX. IN CRUISE FLIGHT FL340 .78M, MOUNTAIN WAVE +25KTS AIRSPEED INCREASE CAUSED EXCEEDANCE OF VMO BY APPROX 10 KTS FOR APPROX 10 SECONDS. SPEED BRAKES WERE DEPLOYED AND SPEED SLOWED BACK TO NORMAL.; PERFORMED CHAPTER FIVE INSPECTION PER AMM 05-SDR A6WA202202188109None · noneON APPROACH, RECEIVED SPOILERONS CAUTION MESSAGE AND. IB AND OB GROUND SPOILER FAULTS STATUS MESSAGES ***AIRCRAFT REMOVED FROM SERVICE*** C/W FIM RESET MESSAGES CLEARED. SPOILERS OPERATED NORMALSDR 3EJA95402/17/22None · noneIN SPEEDS IN EXCESS OF 250KTS THE ACFT ROLLS NOTICEABLY LEFT WHEN SPEED BRAKES EXTENDING AND THE SAME AMOUNT RIGHT AS RETRACTED. AFTER FLIGHT IT APPEARS THE LEFT OUTER SB PANEL DOES NOT EXTEND ALL THE WAY UP AND SLOWER THEN THE INBOARDSDR AALA202202205558Computer · unserviceableAIRCRAFT WAS GROUNDED: ECAM FLIGHT CONTROL ELAC 2 PITCH FAULT DURING CRUISE. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY AT AUS.. **SUPPLEMENTAL REPORT FOR AALA202202179463: REPLACED ELEVATOR AILERON COMPUTER, ELAC 2 PER AMM 27-93-34. REPLACED SPOILER ELEVASDR AALA202202209463Computer · unserviceableAIRCRAFT WAS GROUNDED: ECAM FLIGHT CONTROL ELAC 2 PITCH FAULT DURING CRUISE. FLIGHT DECLARED AN EMERGENCY AND LANDED SAFELY AT AUS.. **SUPPLEMENTAL REPORT FOR AALA202202179463: REPLACED ELEVATOR AILERON COMPUTER, ELAC 2 PER AMM 27-93-34. REPLACED SPOILER ELEVASDR YENA2022021800078Module · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-SDR YENA2022021800077Module · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-SDR YENA2022021800076Computer · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-SDR AALA202202141939Pressure Switch · faultyAIRCRAFT WAS GROUNDED: FAULT INDICATION FOR SYSTEM B FLIGHT CONTROLS, FLIGHT RETURNED TO FIELD. INTERMITTENT FAULT PER TROUBLESHOOTING IAW FIM 27-21-00-810-814; REPLACED SYSTEM B LOW PRESSURE SWITCH WITH NEW IAW AMM 27-09-61 AS PRECAUTION, LEAK AND OPS CHECK GSDR SWIA202264569None · wornLH ELEVATOR HINGE BOLTS #1 AND #2 SCORED. (C CHECK RO 2/20/2022) REMOVED AND REPLACED LH ELEVATOR HINGE BOLTS #1 AND #2 REF AMM 27-31-05SDR SWIA202264568None · corrodedRH ELEVATOR #1 HINGE BOLT AND WASHER IS SCORED. (C CHECK RO 2/20/2022) REMOVED AND REPLACED RH ELEVATOR #1 HINGE BOLT AND WASHER. REF. AMM 27-31-05SDR SWIA202264567None · corrodedRH ELEVATOR #3 HINGE BOLT GROOVED. (C CHECK RO 2/20/2022) REMOVED AND REPLACED RH ELEVATOR #3 HINGE BOLT. REF. AMM 27-31-05,SDR JJBA20220130034Not Reported · not reportedRH SPRING TAB RODS CORRODED. REMOVED RUST ON RH SPRING TAB ROD B-NUTSDR SWIA202265229None · corroded*THE RH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER HARDWARE FOR HINGE ATTACHMENT REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-05-400-801 STEPS 2.B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22SDR SWIA202265228None · corroded*THE RH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A THROUGH B / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUSDR SWIA202265226None · corroded* THE RH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A. THROUGH B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/SDR SWIA202265225None · corroded* THE LH SPOILERON HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW HARDWARE ON L/H SPOILERON, REF. CRJ-200 AMM 27-64-01-400-801. SEE CONTINUATION FOR WORK PERFORMED.SDR SWIA202265224None · corroded* THE LH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED SURFACE CORROSION FROM L/H SPOILERON HARDWARE, REF. CRJ-200 SRM 51-21-06 STEPS 7. A. [1] (A)-(B).SDR AALA202201245073Computer · malfunctionedAIRCRAFT WAS GROUNDED: VS IN OPEN DECENT AUTO PILOT DISCONNECTED AND AIRCRAFT PITCHED LEFT ON DECENT NUMEROUS TIMES. REPLACED ELEVATOR AILERON COMPUTER # 1 (ELAC) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 27-93-34.SDR MASA20220121061None · noneRIGHT AND LEFT WING AILERON PCU OUTPUT LINKS REMOVED DUE WEAR DAMAGE AND DETAIL VISUAL INSPECTION PERFORMED. INSTALLED SERVICEABLE LINKS ON LEFT AND RIGHT AILERONS CRJ7/9-27-0021 R1 AND COMPLIED WITH AD 2006-04-05 AS A MAJOR PERMANENT REPAIRSDR 2022FA0000090None · properICE FORMED INSIDE TAIL ROTOR SLIDER ASSEMBLY AFTER TAKE OFF DUE TO SUB FREEZING TEMPERATURES. NOTE: A/C EXPOSED TO RAIN PREVIOUS DAY AT OAT NEAR 60 F. AFTER FRONTAL PASSAGE OAT DROPPED TO 9*F, BUT AIRCRAFT WAS STORED IN DRY HANGER FOR 12 HOURS PRIOR TO FLIGHSDR J7SA2022012400307None · nonePRIOR TO DEPARTURE, CREW DISCOVERED THAT ELEVATOR FEELS THE ELEVATOR FEELS ABNORMALLY HEAVY WITH INTERFERENCE ON THE PILOT SIDE YOKE. REPLACED BEARING ON PILOT SIDE ELEVATOR TORQUE TUBE IN FORWARD FUSELAGE. PILOT YOKE NOW OPERATES SMOOTHLY. WORK COMPLETED IAW SDR AALA202201246451Unknown · vibrationAIRCRAFT WAS GROUNDED: AIRCRAFT VIBRATION IN TAIL DURING CLIMB AND CRUISE. AN EMERGENCY WAS DECLARED AND FLIGHT DIVERTED TO DFW LANDING SAFELY. ACCOMPLISHED AIRFRAME VIBRATION TROUBLESHOOTING JOB CARD 26L0000506. ACCOMPLISHED ELEVATOR HINGE LINE AND FREE PLSDR AALA202201206451None · noneAIRCRAFT WAS GROUNDED: AIRCRAFT VIBRATION IN TAIL DURING CLIMB AND CRUISE. AN EMERGENCY WAS DECLARED AND FLIGHT DIVERTED TO DFW LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR J7SA2022020100309None · noneSPOILER FAULT ON DESCENT INTO KDAL. REPLACED FCE #2 IAW EMB 505 AMM 27-03-01. P/N 462900-1017 S/N 1127.
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