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 DXTA200701983Unknown · unknownSTAB MISCOMPARE AND HYD PRESS LIGHT CAME ON OUT OF APPROX 3000 FT WITH THE GEAR UP AND FLAPS UP SPEED APPROX 220 KTS. RAN CHECKLIST . PULLED HYD CONTROL CB. HYD CONTROL CB. HYD PRESS WENT OUT. CONFIGURED FOR LANDING . WITH FLAPS 15 STAB MISCOMP WENT OUT. PSDR RAIA00701030Gust Lock · malfunctionedFLT NR 7885 - SYR - GUST LOCK WILL NOT DISENGAGE. MAINTENANCE DEFERRED THE ELECTROMECHANICAL GUSTLOCK PER THE MEL.SDR SWIA200717651Unknown · unknownON FINAL APPROACH INTO BURBANK, SPOILERONS CAUTION MESSAGE APPEARED. DIVERTED TO LAX. RESET CBS 1N8, 2N8, 4A2, 4A3. OPERATIONAL CHECKS GOOD.SDR DL757070002Isolation Valve · leakingLEFT HYD SYS PRESS LIGHT .17 HYD FLUID IN RESEVIOR. FOUND LT SYSTEM EMPANAGE ISOLATION VALVE LEAKING. REPLACED VALVE PER AMM SERVICED LT HYD SYS CLEANED AFFECTED AREA OF HYD FLUID VALVE LEAK AND OPS CKS NORM.SDR CA061221006Cable Assy · incorrect(CAN) WHEN AN OPERATOR TRIED TO INSTALL ONE OF THESE CABLE ASSEMBLIES HE FOUND THAT THE END THAT ENGAGES THE SERVO CAPSTAN WOULD NOT FIT PROPERLY SO THAT THE LOCK SCREW COULD BE INSTALLED. UPON INVESTIGATION IT WAS FOUND THAT THE ORIGINAL DRAWING FOR THE CABLESDR NOCA21506Torque Tube · corrodedCORROSION PITS ON INBOARD TORQUE TUBE SPLINES NR 17, 24, 25 AND 26. REMOVED AND REPLACED TORQUE TUBE.SDR 0602549861Unknown · unknownCREW REPORTED FLIGHT CONTROL PROBLEMS DURING CRUISE AT ALTITUDE. AIRCRAFT DECLARED AN EMERGENCY, WAS CLEARED TO LOWER ALTITUDE IN ATTEMPT TO THAW ANY POSSIBLE ICING OF CABLES, AND DIVERTED TO BUF. THE LANDING WAS NORMAL AND WITHOUT FURTHER INCIDENT. MAINTENSDR P5CA0601506Pdu · inoperativeLE SINGLE DRIVE STATUS MSG NR 3 LED INOP PNEUMATICALLY. REPLACED LE PDU.SDR CA061120003Control Cable · severed(CAN) PILOT REPORTED LOSS OF EFFECTIVE ELEVATOR CONTROL DURING ROUTINE TRAINING FLIGHT. AIRCRAFT RETURNED TO BASE WITH STABILATOR CONTROL MANAGED MAINLY BY STABILATOR TRIM SYSTEM. AIRCRAFT LANDED SAFELY. INITIAL INSPECTION OF STABILATOR SYSTEM CONFIRMED LIMITSDR NOCA20006Actuator · unknownEICAS MSG ASSOCIATED WITH ANNUNCIATOR. PCA NR 8 AT FAULT ON SCM2-1. REMOVED AND REPLACED NR 8 PCA PER MM 27-09-00, OPS CHECK OK. CI CLEARED WITH MCC CHAN.SDR HALA0600855Unknown · unknown2 UNITS OF RUDDER TRIM REQUIRED IN NOSE LEFT DIRECTION WHILE IN CRUISE. OBSERVER IN BACK OF PILOT SAID IT LOOKED LIKE THE FLAPS MAY NOT BE FULLY RETRACTING. ON EXTENDING FLAPS FOR APPROACH RUDDER TRIM HAD TO BE REMOVED. NO RUDDER TRIM LIMITS FOR IN SERVICE PSDR DXTA200601614Unknown · unknownTO MAINTAIN LEVEL FLIGHT AT 5000 FT MSL, 240KIAS, A/C NEEDS 1/2 OF RIGHT RUDDER TRIM TRAVEL TO CENTER BALL AND 3 ROLLS OF AILERON TRIM. A/C ROLLS LEFT WITH TRIMS CENTERED (WILL ROLL INVERTED IF NOT HELD WITH 25-30 LBS OF FORCE. C/W RIG/TRAVEL CHECKS ON ALL PSDR CHQA200600125Unknown · unknownFLIGHT 6393 - CVG-BNA - DURING CRUISE AT 16,000 FT & APPROX 310 KIAS, ACFT STARTED SHAKING & FLUTTERING WITHOUT WARNING. AUTOPILOT ENGAGED AT THE TIME. LATER, MASTER WARNING LIGHT & CHIME SOUNDED, WITH MESSAGES -PITCH TRIM MAIN INOP- &-PITCH TRIM BACKUP INOSDR DXTA200601589Switch · dirtyT/O CONFIG ILLUMINATES WHEN T/O POWER APPLIED. COMPLETED CHECKLIST, ALL ITEMS WERE IN PROPER CONFIGURATION. TESTED SEVERAL MORE TIMES STATIC (ON TAXI WAY) MALFUNCTION CONTINUED AFTER TRIMS RESET, PARKING BRAKE CYCLED, AIR BRAKE RECYCLED. GAINED ACCESS TO FLSDR SIMASUP200624201Unknown · unknownDAY - FLT 4193 - ON DESCENT, WITH AUTO PILOT ENGAGED RECEIVED BACKUP PITCH TRIM INOPERATIVE MSG FOLLOWED BY ANOTHER RED MSG THE CREW COULDN’T READ. CAPT FELT A SMALL VIBRATION IN THE YOKE, VIBRATION ASSOCIATED WITH AUTO PILOT. ISSUED MEL 22-01, COMPLIED WITHSDR SIMA200622001Trim Switch · failedCMH - FLT 3589 - ON TAKEOFF, FIRST OFFICERS TRIM SWITCH WAS IN USE AND IT STARTED TO SMOKE. STOP USING THE FIRST OFFICERS TRIM SWITCH AND CAPTAIN TRIM WORKED NORMAL, RETURNED TO FIELD NO OTHER PROBLEMS NOTED. RAI FIRST OFFICERS TRIM SWITCH, OPS CHECK GOOD. SDR SIMA200620002Transducer · failedRECEIVED AMBER SPOILER FAIL MESSAGE ON EICAS DURING TAKEOFF ROLL, EICAS = SPOILERS OPEN, HANDLE = CLOSE. RAI NR 3 WHEEL SPEED TRANSDUCER IAW EMB 145 AMM 32-41-03, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M)SDR SIMA200619504Control Unit · malfunctionedCREW ELECTED TO RETURN TO FIELD, STABILIZER FAULT STATUS MESSAGE ILLUMINATED ABOVE 10,000 FEET ACCELERATING TO 290 KIAS. CAPTAIN REPORTS HAD FAILED TQ LIMITER MESSAGE ON THE MDS. RESET SSCU 1 AND 2 AS PER ETN CR-27-011. OPS CHECKED GOOD. RETURN AIRCRAFT TOSDR MASA200601718Unknown · malfunctionedASH 6796 PHX - FLIGHT CONTROLS HEAVY IN FLIGHT. MX PERFORMED A ELEVATOR FORCE CHECK AND IT WAS WITHIN LIMITS.SDR NSVA200600094Control Quadrant · warning messageAMBER "FLIGHT IDLE STOP OPEN" LIGHT CAME ON AFTER T/O AND REMAINED ON DURING ENTIRE FLIGHT. REMOVED AND REPLACED CONTROL QUADRANT IAW 76-10-05-04 PN ON/OFF 53170-4, SN ON 148, SN OFF 004.SDR MASA200601623Ecu · malfunctionedGLD UNSAFE CAUTION MESSAGE IN FLIGHT. MX RESET THE SECUS. OPS CHECK GOOD.SDR MASA200601556Unknown · unknownASH 7196 ORD - PILOT REPORTS A/C ROLLS RIGHT WITH GEAR DOWN AND FLAPS AT 45. MX PERFOMED TEST FLIGHT WITH CREW. TEST FLIGHT WAS SATISFACTORY AND WITHIN LIMITS.SDR MKW2006F00000Bellcrank · looseNUTS NEED TO BE SECURED ON ROD. (AUTOPILOT HOOK UP ROD). SHOULD BE TIGHTENED UP, OR REMOVED FROM AIRCRAFT FROM FACTORY. THIS IS SECOND AIRCRAFT IN ONE WEEK THAT THIS ROD HAS BEEN LOOSE. (K)SDR P5CA0601476Indicator · stuckCREW REPORTED LEFT HAND AILERON INDICATOR STUCK IN FULL DOWN POSITION. TRANSFERRED TO DMI 35831 PER MEL 27-01.SDR MASA200601123Circuit Card · faultyASH 7153 ORD - GLD UNSAFE CAUTION MSG. SWAPPED SSCU CARDS.SDR MASA200601101Indicator · malfunctionedASH 7259 MEM - STALL FAIL CAUTION, RUDDER LIMIT FAULT AND SPOILER STAB FAULT. ACFT FERRIED TO IAD WHERE MAINTENANCE REMOVED AND REPLACED ISI. OP'S CHECK GOOD.SDR MASA200601088Warning System · malfunctionedASH 5049 ILM - SPOILER STAB, PITCH FEEL, RUDDER LIMIT, FLAPS 1/2 SPEED. CLEARED INHIBITS. OP'S CHECK GOOD.SDR P5CA0601460Actuator · crackedCREW REPORTED DURING CRUISE, NR 1 HYDRAULIC SYSTEM LOST ABOUT 1 GALLON IN 1 HOUR. TURNED ADP OFF AND EDP TO DEPR PER CHECKLIST. FOUND LEFT CCA LEAKING. REPLACED LEFT CCA IAW AMM 27-61-08. CHECKED FOUND ALL WORKING. ADDED HYDRAULIC FLUID TO SYSTEM NR 1 IAWSDR CA060410008Rod End · damaged(CAN) DURING A SCHEDULED INSPECTION OF THE ROD ENDS, IT WAS NOTED THAT THE BEARING WAS SHOWNING EVIDENCE OF MOVEMENT. BEARING WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20060410008)SDR MASA200600959Unknown · unknownASH 5006 IAH. STAB FAULT STATUS. PERFORMED SPOST 1 W/FLIGHT CREW. NO FURTHER FAULTS NOTED.SDR MASA200600933Unknown · unknownASH 7351 ORD - AIRCRAFT ROLLS RIGHT IN LANDING CONFIQURATION. MAINTENANCE OPS CHECKED ALL FLIGHT CONTROL SYST/AUTOPILOT SYS GOOD.SDR MASA200600919Unknown · unknownASH TUS - GLD UNSAFE CAUTION MESSAGE. MAINTENANCE RESET THE SYSTEM. OP'S NORMAL.SDR DJFA2006213Unknown · unknownNORMAL YOKE BACK PRESSURE WAS BEING APPLIED AT ROTATION, DID NOT SEEM TO RESPOND. FURTHER FORCE WAS APPLIED, STILL DID NOT RESPOND. PAST V1 SPEED, FELT CERTAIN AIRCRAFT WAS NOT GOING TO LIFT OFF. TAKEOFF ABORTED. HEAVY BRAKING APPLIED, THRUST REVERSERS DIDSDR 2006FA0000363Cable · frayedWHILE CONDUCTING AN ANNUAL INSPECTION PRIOR TO PLACING THE AIRCRAFT ONLINE AFTER PURCHASING IT FROM A LOCAL OPERATOR, BOTH FORWARD RUDDER CABLES WERE FOUND TO BE BADLY WORN AND FRAYED. RESEARCH OF THE MAINTENANCE RECORDS SHOWED THAT THE PREVIOUS OWNERS HAD FASDR MASA200600616Unknown · unknownASH 6428 PHX - PITCH FEEL CAUTION MESSAGE. MX PERFORMED THE SPOST RESET PROCEDURE. OP'S CHECK GOOD.SDR MASA200600615Unknown · unknownASH 7275 PHX - MACH TRIM CAUTION. MX PLACED THE MACH TRIM ON MEL. MX CND.SDR 2006FA0000258Flt Controls · seizedAIRCRAFT HAD BEEN TREATED WITH ACF-50 OVER THE LIFE OF THE AIRFRAME. SEVERAL PULLEYS IN THE AILERON, ELEVATOR AND FLAP SYSTEMS WERE FOUND SEIZED OR GUMMED UP WITH ACF-50. LAST APPLICATION OF ACF-50; 18MO.SDR 2006FA0000186Torque Tube · wornINSPECTED THE FLIGHT CONTROL SYSTEM IAW SB AND FOUND FREE PLAY AT THE TORQUE TUBE/ END FITTING INTERFACE ON BOTH SIDES. THE RIGHT SIDE WAS MORE PORNOUNCED THAN THE LEFT. MFG CONSIDERS THIS SB TO BE OPTIONAL, HOWEVER THE CONTINUED USE WITH THIS DEFECT WILL RESDR 2006FA0000185Torque Tube · wornINSPECTED THE FLIGHT CONTROL SYS IAW SB AND FOUND FREE PLAY AT THE TORQUE TUBE/ END FITTING INTERFACE ON BOTH SIDES. THE RT SIDE WAS MOR PRONOUNCED THAN THE LT. MFG CONSIDERS THIS SB TO BE OPTIONAL, HOWEVER THE CONTINUED USE WITH THIS DEFECT WILL RESULT IN TSDR DXTA200601242Flt Controls · out of positionON TAKEOFF WARNING HORN CAME ON ABORTED TAKEOFF AT 50 KNOTS FLIGHT CONTROLS APPEARED TO BE IN CORRECT POSITION. COMPLIED WITH TAKEOFF WARNING HORN CHECK IAW RAYTHEON 400/400A M/M 27-40-00 OPS CHECKS SATISFACTORY NO DEFECTS NOTED AT THIS TIME.SDR 02072006AUnknown · unknownWHEN LANDING GEAR IS EXTENDED AIRCRAFT YAWS TO THE RIGHT. PERFORMED OPERATIONAL TEST OF AILERON AND RUDDER INTERCONNECT IAW 27-10-08 AND LANDING GEAR TEST IAW 32-30-00. NO DEFECTS NOTED DURING BOTH TEST.SDR 2006UALA00081Warning Light · illuminatedFLIGHT DIVERTED DUE TO MACH SPEED TRIM EICAS AND LIGHT ILLUMINATED. A NUISANCE FAULT TRIPPED THE AIR/GROUND FAULT BALLS ON THE LT AND RT STABILIZER/ELEVATOR ASYMMETRY MODULES (SAMS), WHICH GENERATED THE MACH TRIM EICAS MESSAGE AND CAUTION LIGHT. THE AIR-GRSDR QXEA200600117Unknown · unknownDEN - ON TAKEOFF FOR FLIGHT 4309, WHEN RIGHT AUTOPILOT TURNED ON CONTROL YOKE IT HAS AN EXTRA CATCH FEEL BEFORE NEUTRAL, BOTH CAPTAIN AND FO YOKES. NOT NOTICED WITH AP ON. INSPECTED CABLE RUNS, PULLEYS AND QUADRANTS OF RT AILERON CIRCUIT FOR INTERFERENCE WITHSDR MASA200600029Unknown · unknownASH 7062 DEN, RUDDER TRAVEL WAS RESTRICTED TO 12 DEG TO THE LEFT SIDE, WITH FLAPS AT 5. MX OPS CHECKED.SDR 06FDEA0100Spring · unknownFOUND CARTRIDGE SPRING ASSY ITEM 820 P/N ARH 1694-1 WITHOUT EO# 8-2780-7-4308 APPLICABLE. ACCOMPLISHED EO# 8-2780-7-4308 P1 ATTACHED, IN CONJUNCTION WITH NRC FEDEX, N00263/F160263.SDR VNAA0512014Warning Light · unknownTHE FLAPS FAIL MESSAGE ILLUMINATED WHEN FLAPS WERE AT 25 SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET & TESTED THE FLAP SYSTEM IAW BOMBARDIER CRJ200 SL 00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WSDR AU510001741Shutoff Valve · failedFLAP/SLAT SHUTOFF VLV LOCATED IN RT W/W LEAKING. INSPECTION FOUND CAP P/N 732-18718 HAD AN OPEN CRACK AT LAST/OUTERMOST THREAD RUNNING 270 DEGREES AROUND ITS CIRCUMFERENCE (CRACKED THROUGH). HEX-NUT END OF ALUMINUM CAP HAD LIFTED BY 0.1 INCHES UNDER HYD PRESSDR AU510001562Computer · failedFLIGHT CONTROL PRIMARY COMPUTER (FCPC) FAILED. FCPC REMOVED AND SENT FOR TEST AND REPAIR. INVESTIGATION FOUND THE POWER SUPPLY FAULTY.SDR 20018Indicator · false indicationON TAKE OFF ROLL, PFCS INDICATOR SHOWED RT SIDE SPOILERS DEPLOYED AFTER ADVANCING TAKEOFF POWER WITH CONTROLS IN NEUTRAL POSITION. REMOVED AND REPLACED PFCS INDICATOR IAW PSM 1-8-2, 27-05-00 PG. 201-203. OPS CHECK PASS IAW PSM 1-8-2, 27-00-05 PG. 204-206.SDR 2005FA0001621Control Cable · out of rigDURING INSPECTION OF FLIGHT CONTROL SYSTEM, DURING INITIAL 200 HOUR PHASE 1 INSPECTION, IAW SAFETY COMMUNIQUE NR 265, FOUND RUDDER CABLE TENSIONS, RUDDER TAB CABLE TENSIONS, AND ELEVATOR TAB CABLE TENSIONS BELOW APPLICABLE MM SERVICE LIMITS. NO OTHER FAULTS N
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