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 SWIA202161590None · corroded*RH WING OTBD GROUND SPOILER PCU HAS CORRODED HARDWARE AT ATTACH LINK (C-CHECK RO 10/4/2021) REMOVED AND REPLACED CORRODED HARDWARE FROM THE RH WING OTBD GROUND SPOILER PCU ATTACHMENT LINK REF CRJ 200 AMM 27-65-01-400-801. OPS CHECK OF GROUND SPOILERS GSDR J7SA2021090100295Electronic Unit · failedGROUND SPOILER FAIL ILLUMINATED IN FLIGHT. REPLACED FCE 2. OPS CHECKED GOOD. WORK COMPLETED IAW AMM 27-03-01. P/N S/N 0871.SDR SWIA202161323None · corroded*LH WING FLIGHT SPOILER OTBD ACTUATOR HAS CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REPLACED ONE NUT AND COTTER KEY ON THE LH WING FLIGHT SPOILER OTBD ACTUATOR PER THE CRJ 200 AMM 27-64-05-400-801 STEP 1 THRU 3.8(C). / OPERATIONAL TEST GOOD. NO DSDR SWIA202161321None · corroded*LH WING SPOILERON INBD AND OTBD ACTUATORS HAVE CORRODED ATTACHING HARDWARE (C-CHECK RO 9-30-21) REMOVED AND INSTALLED NEW SERVICEABLE HARDWARE ON THE LH WING SPOILERON INBOARD AND OUTBOARD ACTUATORS. REF - CRJ 200 AMM 27-64-01-400-801 STEP 1 THRU STEP 2SDR SWIA202161695None · failedLH WING SPOILERON IB PCU (HYD SYS 1&2) FAILED BACKLASH CHECK. PCU REQUIRES REPLACEMENT. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH SPOILERON IB PCU IAW CRJ 200 AMM 27-62-01-400-801. RIGS/OPS/LEAK CHECK "GOOD"SDR 4DPA2021073000001Unknown · abnormalAT 4000 FEET OF THE AIRCRAFT BEGAN YAWING TO THE RIGHT REQUIRING LEFT RUDDER. ATTEMPTED YAW TRIM AND FOUND YAW TRIM INOP. APPLIED FULL LEFT RUDDER. FOLLOWED QRH OAKS BROUGHT PLANE BACK. WHEN BACK ON GROUND TRIED YAW TRIM AGAIN AND SEEMED TO WORK FINE. PERFORSDR SWIA202161536None · leakingR/H ELEVATOR #3 INBOARD PCU WAS FOUND TO LEAKING AND FAILED THE BACKLASH CHECK, AT AN AVERAGE OF 0.075, .MAXIMUM ALLOWABLE IS 0.070. (C-CHECK RO 9/30/2021) REMOVED AND REPLACED RH #3 PCU IAW CRJ700 AMM 27-33-01-000/400-801-A01 AND USING TASK CARD 27-320-1SDR SWIA202161666Nut · corrodedLH WING FLIGHT SPOILER OUTBD HINGE NUT, # 3 AND # 4 HINGE NUTS AND IB HINE KEEPER BOLTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED NUT ON LH WING FLIGHT SPOILER OB HINGE, NUTS ON #3 AND #4 HINGE, AND BOLTS ON IB HINE KEEPER BOLTS IAW CRJ20SDR DALA2021072904287Computer · faultedSHIP 3137 - ATO - AT THROTTLE UP FOR TAKEOFF AIRCRAFT HAD ELAC 2 FAULT. PULLED OFF AND RESET SYSTEM AND ATTEMPTED 2ND TAKEOFF AND REJECTED AGAIN FOR SAME MESSAGE. CORRECTIVE ACTION: REPLACED ELAC 2.(7865938)SDR SWIA202161544None · failedLH ELEVATOR INBD PCU FAILED COMPENSATOR FUNCTIONAL TEST. MEASURED 0.40 IN DIMENSION AFTER 1 MIN OF HYD PRESSURE RELEASE. SHOULD BE 0.44 IN AS PER 1C TASK CARD 27-330-120-(CONFIG A01). PCU REQUIRES REPLACEMENT. (C-CHECK RO 9/30/2021) REMOVED AND REPLACED SDR JIKA2021072001Trim Cylinder · inoperativePILOT REPORTED HAVING A TRIM FAILURE IN FLIGHT. LANSING MAINTENANCE TROUBLESHOT TO THE TRIM ACTUATOR. PART ON HAND PENDING REPLACEMENT AT THIS TIME.SDR SWIA202161153None · gouged* RH WING OUTBOARD FLAP WS220.00 FOWARD HINGE FITTING OUTBOARD LUG GOUGED (MARKED) (C-CHECK RO 9-21-21) REPAIRED RH WING OUTBOARD FLAP WS220.00 FOWARD HINGE FITTING OUTBOARD LUG IAW MHI RJ REO 670-57-53-291 REV --, DATED 2021-07-29 ALL STEPS 1-4 ARE COMPLSDR AALA202107124978Pressure Switch · inoperativeAIRCRAFT WAS GROUNDED: A LOW PRESSURE LIGHT ILLUMINATED DURING FLIGHT CONTROL CHECK JUST BEFORE TAXI TO ACTIVE RUNWAY. RETURN TO GATE. LOW PRESSURE WARNING SWITCH REPLACED IAN AM 27-09-61 PB 401.SDR 2021FA0000391None · wornPILOT REPORTS AOA INDICATION IS OFF BY 1 DEGREE DURING CRUISE. COMPLIED WITH R&R OF AOA TRANSMITTER. OPS CHECKED OK. AIRCRAFT OK FOR RTS.SDR FDEA202106221579Unknown · malfunctionedDURING APPROACH, LOWERING FLAPS FROM 20 TO 25, WITH WINGS LEVEL. LT AUTOPILOT USED 2 UNITS LT WING DOWN TO MAINTAIN HEADING. WITH AUTOPILOT DISENGAGED, ACFT HAD A STRONG RT ROLL. 2 UNITS OF LT TRIM REQUIRED FOR TRIMMED FLT. PREFORMED INBD AILERON DROOP CK ISDR SWIA202162339None · unserviceableRECORD PART #, SERIAL #, COMPLETE SW M19: FLUTTER DAMPENERS REPLACED ON ROUTINE TASK CARD 27-900-120 (C-CHECK RO 11-05-2021) REMOVED L/H AILERON FLUTTER DAMPER (P/N: 1023100-7)(S/N: HAI7329) AND R/H AILERON FLUTTER DAMPER (P/N: 1023100-7)(S/N: HAI5128) ANDSDR SWIA202162337None · damagedROUTE LH AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON LH AILERON PER AMM (C-CHECK RO 11-05-2021) REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS ON L/H AILERON REF. CRJ 700 AMM 20-31-00-400-SDR SWIA2021081860341Bolt · seizedRIGHT-HAND WING, FLUTTER DAMPENER, FORWARD BOLT IS SIEZED. (C-CHECK RO 8/16/2021) REMOVED SIEZED BOLT FROM THE RIGHT-HAND WING, FLUTTER DAMPENER, BY REMOVING FLUTTER DAMPENER BRACKET. REF. CRJ700 SRM 51-42-21-001-001-A01. INSTALLED NEW FLUTTER DAMPENER SDR YENA2021061400365Computer · failedFLT 6122, PBI-MCO. AFTER DEPARTURE WE NOTICE THE AIRPLANE IN A SLIP AND IN A 5 DEGREE BANK RIGHT TURN WITH AUTO PILOT ON. TURNING OFF THE AUTOPILOT THE PLANE 3 BANK INCREASES FURTHER & AGRESSIVELY; PERFORMED TSM TASK 27-10-00-810-842A. R & R ELAC1 (2CE1) PER ASDR HNAA2021051200200Solenoid · stickingGUST LOCK WILL NOT DISENGAGE. MAINTENANCE PERFORMED: INSPECTED GUST-LOCK AND FOUND PLUNGER FOR GUST-LOCK SOLENOID STICKING, CLEANED AND LUBED PLUNGER. OPERATED GUST-LOCK SEVERAL TIMES. OPS CHECK GOOD.SDR JJBA20210510039None · noneRH ELEVATOR UPPER SKIN NEAR I/B SPRING TAB O/B MOUNT HAS TEAR. REPAIRED RH ELEVATOR UPPER SKIN NEAR I/B SPRING TAB O/B MOUNT.SDR QMLA2021051120024Flt Controls · oscillatesAS PILOT DEPARTED KAPA FOR KRAP, THE WEATHER CONDITIONS IN APA WAS LOW CEILINGS WITH RAIN. PILOT DEPARTED FROM RUNWAY 35R AND INITIALLY CLIMBED TO 8000 FEET. AS PILOT BEGAN CLIMBING AND ENTERED THE CLOUD LAYER, PILOT ENCOUNTERED SNOW AND SOME LIGHT MIXED ICE. SDR MFGA20210414002Unknown · unknownON WEDNESDAY, 14 APRIL 2021, THE CREW OF N412GJ WAS OPERATING UNDER FAR PART 135 CONDUCTING A PASSENGER CHARTER FLIGHT FROM KPBI TO KAVL. IMMEDIATELY AFTER LIFTOFF FROM THE RUNWAY, THE AIRCRAFT PITCHED TO AN UNUSUALLY HIGH NOSE UP ATTITUDE. THE CREW WAS ABLE TSDR QXEA2021041200183Control Unit · inoperativePITCH TRIM MASTER CAUTION IN-FLIGHT PREFORMED E&A CHECKLIST AND RETURNED TO FIELD. ALL LANDING PARAMETERS NORMAL. REMOVED FROM SERVICE. CDS FAULTS - FCECU FAILURE 67, 63, E7, E3. REMOVED AND REPLACED FCECU IAW Q400 AMM 27-00-01-000-802 AND 27-00-01-400-802. SDR J7SA2021040500283Electronic Unit · malfunctionedPTRIM BKP FAIL CAS MESSAGE WILL NOT EXTINGUISH. REPLACED # 1 FCE IAW EMB 505 AMM 27-03-01. RIGGING AND OPS CHECK GOOD. P/N 462900-1017; S/N 1277.SDR 2021FA0000087Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (9 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PASDR K11A2021030100046Unknown · vibrationDURING FUNCTIONAL FLIGHT FOR FLAP REMOVAL EXPERIENCED HIGH FREQUENCY BUFFET CLIMBING THROUGH FL 240 @ 280 KIAS, CLEAN WING. INSPECTED AND OPS CHECK TRAILING EDGE FLAPS, LEADING EDGE FLAPS AND KRUEGER FLAPS IAW AMM 27-51-00, 27-81-00 NO DEFECTS NOTED. AIRCRAFTSDR SWIA202157704Bolt · corroded*UPPER ATTACHMENT BOLT FOR R/H MULTI-FUNCTIONAL PCU CORRODED(MARKED (C-CHECK RO 4/21/2021) UPPER ATTACHMENT BOLT FOR R/H MULTI-FUNCTIONAL OUTBOARD PCU REMOVED AND REPLACED REF CRJ700 AMM 27-62-01-000-801 (A01) 27-62-01-400-801 (A01) / TUC9291 CAL DUE 3SDR 2021FA0000028Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHT BELOW TOLERANCE AT LEFT ELEVATOR: HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G), WEIGHT HAS BEEN REPLSDR 2021FA0000019Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT RIGHT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (2 EACH BELOW MINIMUM OF 84G). ALL WEIGHTS HAS BESDR 2021FA0000018Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (12 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PSDR 2021FA0000017Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (12 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PSDR 2021FA0000014Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE: RUDDER ADJUSTABLE WEIGHTS PART NUMBER PE915109-L27 (19 EACH BELOW MINIMUM OF 455G), WE ALSO NOTED THE FOLLOWINGSDR 2021FA0000015Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (13 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PSDR SWIA202155508Servo · overservicedFIRST OFFICER LEG, ON FINAL APPROACH AFTER DISCONNECTING AUTOPILOT, FLIGHT CONTROLS LOCKED UP AND FO HAD TO APPLY FAIRLY STRONG FORCE TO GET PITCH MOVEMENT OF YOKE TO UNLOCK. THEN TO MAKE ROLL ADJUSTMENTS IN FLIGHT, HAD TO APPLY SIMILAR FORCE TO UNLOCK ROLL MSDR HALA2021010500002Computer · faultyETOPS FOUND FCPC 1 FAULTING. REMOVED AND REPLACED FCPC 1, PER AMM 27-93. COMPUTER, FLT C OFF 33-2791-9-0007 06100 ON 33-2791-9-0007 06629.SDR HNAA2020123100383Gust Lock · malfunctionedGUST LOCK WOULD NOT UNLOCK THEN THE GUST LOCK WOULD NOT LOCK. PERFORMED OPERATIONAL CHECK, IAW AMM 27-71-00. OPERATIONS CHECK GOOD. OK FOR SERVICE.SDR J7SA2021010400260Flt Controls · malfunctionedDURING DESCENT, SPOILER FAIL CAS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 FCE, IAW PHENOM 300 AMM 27-03-01-400-801. PERFORMED ALL ASSOCIATED RIGGING AND OPERATIONS CHECKS, PER TASK 37-03-01-400-801. ALL OPERATIONS CHECKS GOOD. SDR 2021FA0000000Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (6 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PASDR DXTA2020121904497Flt Controls · defectiveUPON DESCENT OUT OF FL390, WE EXPERIENCED THE FOLLOWING INDICATIONS: SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, SPOILER FAULT ALONG WITH A FLASHING MAX SPEED WARNING WHILE OUR INDICATED SPEED 20 KNOTS SLOWER THAN BOTTOM OF BARBER POLE. WE ALSO EXPERIENCED A LOSS SDR F2PA2020121000488Flap System · intermittentON APPROACH, FLAPS CAS MESSAGE INDICATED FLAP FAIL WHEN TRANSITIONING FROM FLAP POSITION 3 TO FLAP POSITION 4. PER THE QRM, FLAPS WERE RESET, AND THEN WORKED NORMALLY TO FLAP POSITION 4. NORMAL LANDING WAS THEN MADE. ISSUE WAS REPEATED ON GROUND ONCE, IN TESDR 2020FA0000553Pulley · damagedREMOVED DAMAGED PULLEY FROM BRACKET AND FOUND BRACKET INCORRECTLY DIMPLED WHERE PULLEY BOLT RUNS THROUGH BRACKET. CONSULTED CESSNA TECH SUPPORT AND THEY RECOMMEND REPLACEMENT OF BRACKET AND PULLEY. NEW BRACKET AND PULLEY INSTALLED.SDR GTIA2020120735488Unknown · unknownON TAKE OFF ROLL THE AIRCRAFT SWERVED A BIT. WE NOTICED ON CLIMB OUT WE NOTICED THE SPEED BRAKES WERE FLASHING AS IF THEY WERE OUT. THE SPEED BRAKES "AMBER" WENT AWAY. HOWEVER, DURING THE CLIMB IT WAS SHOWING A BANK TO THE LEFT. THE RIGHT AILERON WAS SHOWISDR AALA202012049007Unknown · unknownAIRCRAFT WAS GROUNDED. AIRCRAFT PITCHED OVER IN OPEN DESCENT DESCENDING THROUGH FLIGHT LEVEL 340. AIRCRAFT OVERSPEED, 1 BAR, FOR APPROXIMATELY 10-20 SECONDS. POST FLIGHT REPORT SHOWED NO LAST LEG FAULTS. GROUND SCAN OF ELECTRONIC FLIGHT CONTROL SYSTEM SHOWSDR AALA202012039016Unknown · unknownAIRCRAFT WAS GROUNDED. WHEN SPEED BRAKE WAS USED & FLAPS 2, 180 KNOTS AIRCRAFT WENT INTO A 5-10 DEGREE BANK. HAPPENED AT 9000 FEET AND AGAIN AT 4000 FEET. NO ECAM MESSAGES DISPLAYED DUE TO A UNCOMMANDED ROLL INCIDENT. TROUBLESHOT, REF TSM 27-10-00-810-842-ASDR J7SA2020121100255Flt Controls · malfunctionedDIVERTED DUE TO PTRIM NML FAIL, GND SPLR FAIL, AND SPOILER FAULT CAS ACCOMPANIED BY MULTIPLE "X" INDICATIONS OVER TRIM POSITIONS. AIRCRAFT LANDED WITHOUT INCIDENT AT KSLC. REMOVED AND REPLACED NR 2 FCE, IAW EMB 505 AMM 27-03-01. ALL RII PROCEDURES C/W. OPESDR 2020FA0000504Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (4 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PASDR 2022F00198None · abnormalDURING TAXING, INTERMITTENT MESSAGE "FLICHT COUNTROL NO DISPATCH" IN EICARS P-ACE 3 WAS REPLACED AIW AMMII 03-27-03/400 AIRCRAFT GOOD FOR SERVICSDR JGVR202011111001Counterbalance · damagedWHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE AND REQUIRING REPLACEMENT: RT ELEVATOR (10 ADJUSTABLE BALANCE WEIGHTS P/N PE915109-L33), RT ELEVATOR (BALANCE WEIGHT HORN P/N PE915109-L42), RT ELEVATSDR AALA202011099001Transducer · defectiveAIRCRAFT WAS GROUNDED. ON DESCENT FLT CONT ELAC 1 PITCH FAULT AND FLT CONT ELAC 2 PITCH FAULT ECAM CAUTION ILLUMINATED. FOUND THE POS ERROR 9CE OFF ELAC 1+2 DURING EFCS BITE. REPLACED THE THS MONITOR AND COMMAND TRANSDUCER, PER AMM 27-44-56. ACCOMPLISHED S
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