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.

SDR P5CA0300893Aileron · malfunctionedAFTER ENG START CREW REPORTED AILERON INDICATION PROBLEMS DURING FLT CNTRL CHECK. CONFIRMED W/ VISUAL OPERATION THAT THE CONTROL SURFACES LOOKED NORMAL, DEFERRED IAW MEL 27-18-1Jul 6, 2003 · N451PA · Boeing 74746NFSDR ASOA03276Switch · inoperativeDUIRNG CRUISE, LEVELING AT 37,000 FT THE CREW RECEIVED STABILIZER, MACH AND PITCH TRIM MESSAGES. UNABLE TO GET STABILIZER CHANNELS ONE OR TWO TO RE-ENGAGE. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. THE AIRCRAFT LANDED Jun 24, 2003 · N709EV · Cndair CL6002C10SDR 2003FA0000537Bearing · failedDURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING. PROBABLE CAUSE IS A DESIGN FLAW IN THE CONTROL SYSTEM WHICH ALLOWS THE CONTROL ROD DEFLECTION TO EXCEED THE DESIGN LIMIT OF THE BEARING. RECOMay 12, 2003 · N864AF · Grob G120ASDR 2003FA0000366Rod End · brokenAVID AIRCRAFT LIFT STRUT, THREADED ROD-END FAILURE. THE PILOT OF AN AVID AIRCRAFT LOST CONTROL SHORTLY AFTER TAKE-OFF AND THE AIRCRAFT DESCENDED INTO THE GROUND IN AN UNCOMMANDED LEFT-HAND TURN CAUSING SUBSTANTIAL DAMAGE TO THE AIRFRAME. THE PILOT RECALLS HEApr 8, 2003 · Amtr AVID*SDR 2003F00370Warning Light · illuminatedFLT 6604 - PHX-LAX, AFTER TAKEOFF, PILOT RECEIVED A GROUND LIFT DUMPING UNSAFE CAUTION MESSAGE. FOLLOWED CFM PROCEDURES AND RETURNED TO PHX WITH NO PROBLEMS. MAINTENANCE RESET SYSTEM AND FOUND NO DEFECTS. AIRCRAFT CONTINUED ITS FLIGHT WITH NO FURTHER DIFFICMar 23, 2003 · N504MJ · Cndair CL6002C10SDR 2003FA0000582Control Wheel · failedPILOT SIDE CONTROL WHEEL FAILURE ON LANDING FLAIR. BRAKE ON TOP LT CORNER WHERE THE HAND GRIP MEETS THE MAIN CROSS SPOKE. THE BRAKE IS CLEAN AND SHOWS NO SIGN OF CRACKING BEFORE THE FAILURE OCCURED.Mar 19, 2003 · N2996Y · Cessna 182ESDR EIA2003048Pushrod TubeINTEERCONNECT TUBE BETWEEN PILOT AND COPILOT HAS SEVERE GOUGHING ON LEFT UPPER SIDE' RH UPPER SIDE SLIGHTLY GOUGED DUE TO BOLT LENGTH OF CENTER PEDESTAL AND PANEL INSTILLATIONREPAIRED AS PER ECRA 944-27-161-2 INTERCONNECT TORQUE TUBE REQUIRED SPLICE. CUT TORQUMar 5, 2003 · N944F · Doug DC933FSDR C2XA03SH032Bracket · crackedSHV-DURING C CHECK THE BRACKET SUPPORTING THE ELEVATOR PULLEYS WAS FOUND CRACKED AND DEFORMED LOCATED IN VERTICAL STABILIZER BY PANEL 325LR. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERFeb 27, 2003 · N13936 · Emb EMB145ERSDR 2003F00167Control Unit · intermittentFLAPS STOPPED AT 2 DEGREES POSITION WHEN FLAPS SELECTED TO 20 DEGREES. RESET CONVETERS AT FLAP CONTROL UNIT. FLAPS OPERATED NORMALLY FOR REMAINDER OF FLIGHT. CHANGED FLAP BDU. AIRCRAFT RETURNED TO SERVICE WITH NO PROBLEMS. (M)Feb 13, 2003 · N601VH · Cndair CL6002B16SDR ASOA03052Seal · leakingDURING CLIMB-OUT FROM XNA-ATL, WHILE RETRACTING THE FLAPS, THE CREW RECEIVED AN AMBER CAUTION FLAPS FAIL MESSAGE. AN EMERGENCY WAS DECLARED. THE FLAPS FAILED AT ZERO DEGREES AND A ZERO FLAPS LANDING WAS ACCOMPLISHED IN ATL WITHOUT INCIDENT. MAINTENANCE RE-RFeb 9, 2003 · N884AS · Cndair CL6002B19SDR WRNA200300003Circuit Breaker · unserviceableFlight control servo control lever lock circuit breaker tripsCorrective Action: R&R'd circuit breaker I/A/W MM 20-16-00 Op's check goodFeb 7, 2003 · N820SC · Airbus A300B4203SDR CA030120010Hinge Pin · fractured(CAN) TIME ON PIN IS UNKNOWN IT WAS NOTICED THAT THE SKIN FORWARD OF THE LT UPPER FORWARD WING SPAR NEAR THE WING FITTING WAS SOFT AND EASILY MOVED. DURING CLOSER INSPECTION THE PIN WAS FOUND NOT TO BE ENGAGED IN THE LAST 2 FT OF THE HINGE BY THE WING FITTINGJan 16, 2003 · Beech 99ASDR 2003FA0000035Skin · crackedWHILE DOING A DAILY INSPECTION A 1 3/4 INCH CRACK WAS FOUND IN THE LT WING JUST ABOVE THE INBOARD FLAP BELLCRANK. WE OPERATE A FLEET OF 26 550 SERIES AIRCRAFT WITH A LARGE PORTION HAVING A REPAIR TO THE LT OR RT WING AT ONE POINT OR ANOTHER. I HAVE FOUND SEVERJan 15, 2003 · Cessna 550SDR S03J27004Control Cable · out of rigB-18701 RUDDER DOES NOT FULL DEFECT TO RT (SHORT OF ABOUT 15-20 PERCENT). RUDDER & RUDDER TRIM SYSTEM RIG CHECK FOUND CONTROL CABLE. TENSION WAS OUT OF LIMIT. PERFORM RUDDER AND RUDDER TRIM CONTROL SYS ADJ IAW AMM 27-21-00. PERFORM RUDDER RATIO GROUND TJan 2, 2003 · Boeing 747400SDR RAIA00301001Stall Warning · inoperative5538-STL- STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE STALL WARNING VANE, OPS CK OK.Jan 1, 2003 · N571HK · Jetair JETSTM4101SDR 2002UALA01896Switch · failedEICAS MESSAGE "LE SLAT ASSY" DISPLAYED AFTER TAKEOFF. DIVERTED INTO HNL. SUPPLEMENTAL DATA UPDATE REPLACED #9 OUTBOARD SLAT PROXIMITY SWITCH S297. SYSTEM OPERATIONAL CHECK OK, NO ADDITIONAL OCCURENCES.Dec 26, 2002 · N676UA · Boeing 767322SDR SIMA200235105Switch · failedCLE - FLT 4248 - DURING CRUISE FLIGHT, A GUST LOCK FAIL WARNING. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO CLE. MAINTENANCE REMOVED AND REPLACED THE CONTROL YOKE POSITION SWITCH AND ADJUSTED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WDec 16, 2002 · N809AE · Emb EMB135KLSDR RAIA00212355Sensor · inoperative5594-STL- LEFT AOA SENSOR WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED THE LEFT AOA SENSOR, OPS CK OK.Dec 15, 2002 · N574HK · Jetair JETSTM4101SDR RAIA00212346Vane · inoperative5578-STL- RIGHT STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED R/H AOA VANE, OPS CK OK.Dec 9, 2002 · N566HK · Jetair JETSTM4101SDR HNAA0200085Cover · brokenCREW REPORTED FIRST OFFICERS CONTROL YOKE WAS BINDING. FOUND PIECES OF THE FO'S CONTROL COLUMN UPPER PLASTIC COVERS BROKEN OFF AND LODGED IN THE CONTROL CHAIN UPPER SPROCKET. REMOVED PLASTIC PIECES AND TRIMED COVERS PER EO.Dec 3, 2002 · N936HA · Dhav DHC8102SDR U30A200200028Computer · malfunctionedPRIOR TO DEPARTURE OF FLT 9263 ORD-ELP, THE NR 1 ELEVATOR AND AILERON COMPUTER (ELAC) [PITCH] FAULTED ON ECAM. DEFERRED ELAC NR 1 PER MEL 27-93-01-2. ALL MAINTENANCE AND OPERATIONS REQUIRED ITEMS ACCOMPLISHED. REPLACED NR 1 ELAC PER AMM 27-93-34 AND OPS CHECKENov 15, 2002 · N263AV · Airbus A320214SDR ABXA020256Flange · crackedRIGHT FLAP INBOARD FIXED VANE GOUGED ON UPPER SURFACE DUE TO CRACKED ATTACH ANGLE. REPLACED FIXED VANE AND CRACKED VANE ATTACH ANGLE IAW DC-9 SRM 51-30-05 AND DC-9 MM 27-51-03-2-0002.Oct 21, 2002 · N980AX · Doug DC932SDR 2002FA0001281Cartridge · defectiveDURING COMPLIANCE WITH SB, REPLACEMENT OF TRIM CARTRIDGE NUT THE YAW TRIM CARTRIDGE FAILED TORQUE CHECK. THE ROD FOR THE TRIM CARTRIDGE APPEARS TO BE UNDERSIZE THEREFORE THE NUT WILL ONLY HOLD AT 1 INCH POUND OF TORQUE RATHER THAN 3 INCH POUNDS AS REQUIRED INOct 17, 2002 · N18DN · Cirrus SR22SDR AWXA200200992Computer · malfunctionedFLT 0462 - ON TAKEOFF AT YVR EN ROUTE FOR PHX ELEVATOR AILERON COMPUTER (ELAC) NR 2 FAULTED ON UPPER ECAM AS THRUST WAS BEING ADVANCED TOWARD "FLEX". REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED ELAC 2 IAW AMM 27-93-34-400-001, OPERAOct 7, 2002 · N643AW · Airbus A320231SDR 02FDEA00773Attach Fitting · broken#4 RH SPOILER ACTUATOR ATTACH FITTING IS BROKEN. FWD I/B SIDE OF FITTING IS MISSING. ** S/D ** COMINGSep 28, 2002 · N450FE · Airbus A310SDR 02262649Power SupplyDuring flight, the crew reported that the rudder and aileron were self trimming and that the flap position indication oscillated regardless of the selected flap position. The flight continued to HPN and landed without incident. Maintenance personnel removed Sep 19, 2002 · N649BR · Cndair CL6002B19SDR U30A200200022Computer · intermittentAFTER FLIGHT 256, EWR - PUJ, WHILE ON THE GATE AT PUJ, NR 2 ELAC (ELEVATOR AILERON COMPUTER) FAULTED ON ECAM. SWAPPED NR 1 & 2 ELAC'S PER AMM 27-93-34. PERFORMED OPS CHECK FOR BOTH ELAC'S PER AMM 27-93-00-710-001 AND TESTED OK. DEFERRED NR 1 ELAC PER MEL 27-9Sep 18, 2002 · N261AV · Airbus A320214SDR 02260649Power SupplyDuring flight, the crew reported that the rudder indicated full right deflection with some control problems. The aircraft was returned to IAD and landed without incident. Maintenance personnel removed and replaced the flight control position indication power Sep 17, 2002 · N649BR · Cndair CL6002B19SDR ARWA20020810TransducerLOG PAGE # 110608. DISCREPANCY: NEAR END OF TAKEOFF ROLL PTY MAIN GEAR SPOILER INOPERATIVE LIGHT CAME ON. CORRECTIVE ACTION:REMOVED AND REPLACED #5 ANTISKID TRANSDUCER OPERATIONAL CHECK NORMAL IAW 27-35-0.Aug 30, 2002 · N426FB · Doug DC85F54SDR UG82002F00008Damper · misinstalledAMBER YAW DAMP NOT CENTERED, MESSAGE ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED. YAW DAMPER NOT CENTERED. CREW REFERENCED AND FOLLOWED APPROVED FLIGHT MANUAL PROCEDURES OF AFM. SYSTEM RESET WAS NORMAL. CREW CONTINUED TRIP.Aug 22, 2002 · N5113 · Cessna 750SDR M02115Damper · failedYAW DAMPNER NR 2 WILL NOT ENGAGE. MECHANIC T/S SYSTEM. REMOVED AND REPLACED NR 2 YAW DAMPNER ACTUATOR NO FURTHER DEFECT. AIRCRAFT RETURNED TO SERVICE.Aug 7, 2002 · N17156 · Cndair CL6002B19SDR AUS20020916Cable · corroded(AUS) CONTROL CABLE RUSTED IN AREA OF REAR FUSELAGE.Aug 5, 2002 · Cessna 172MSDR AUS20020913Cable · corroded(AUS) CONTROL CABLE CORRODED WITH APPROXIMATELY 50% OF THE STRANDSBROKEN/FRAYED.Aug 5, 2002 · Cessna 172MSDR DLM88020822Aileron · stiffDURING CLB-OUT EWR PILOT NOTED AILERONS FELT VERY STIFF. AILERON REPONSE WAS NORMAL. FLIGHT RETURNED TO EWR. PILOT REPORTED AILERON FELT NORMAL ON APPROACH TO EWR. MTC INSPECTED AILERON SYSTEM WITH NO OBVIOUS DEFECTS NOTED. LUBRICATED AIL ERON MECHANISM IN MAJul 16, 2002 · N935DL · Doug MD88SDR AUS20020671Control Quadrant · faulty(AUS) UNCOMMANDED ROLL DISCONNECT. INVESTIGATION COULD FIND NO DEFINITE CAUSE FOR THE DEFECT BUT FOUND THE CABLES MARGINALLY SLACK AND ASLIGHT SMEARING OF GREASE ON THE CLUTCH FACES.Jul 1, 2002 · Dhav DHC8102SDR VNAA0206015Circuit BreakerDURING TAKE OFF, THE CREW RECEIVED A TAKEOFF MISCONFIGURE CAS MESSAGE AND ABORTED TAKE OFF. MAINTENANCE ADVISED THE CREW TO RECYCLE THE IAC CIRCUIT BREAKER AND THE MESSAGE CLEARED. FLIGHT 4182 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITHOJun 24, 2002 · N425JS · Dorner DO328100SDR SIMA200217709Hydraulic System · inoperativeIN CRUISE FLIGHT MAIN PITCH TRIM WAS ENGAGING BY ITSELF CREW DROP OFF AUTO PILOT AND IT WAS STILL DOING IT. CALLED MOC AND HAD THE CREW PULL THE NO 1 TRIM C/B STILL DID NOT HELP. CREW ELECTED TO DIVERT TO GET THE AIRCRAFT ON THE GROUND AS SOON AS POSSIBLE. Jun 24, 2002 · N609AE · Emb EMB145SDR KZ52002F00000Torque Shaft · corrodedDURING A SCHEDULED INSPECTION OF THE TAIL AREA THE TECHNICIAN DISCOVERED CORROSION HAD PENETRATED THROUGH THE TORQUE SHAFT. TUBE IS MADE OF STEEL AND IS SUBJECT TO RUST.Jun 19, 2002 · N7207E · Beech C99SDR SIMA200217102Actuator · inoperativeDISC-PITCH TRIM AUTO MSSG ON EICAS IN FLIGHT WITH AUTOPILOT ON THEN ALL PITCH TRIM SWITCHES FAILED. C/A MAINTENANCE REMOVED AND INSTALLED A NEW HORIZONTAL STABILIZER ACTUATOR.Jun 19, 2002 · N631AE · Emb EMB145LRSDR MAS2002F00004Flap · inoperativeDECLARED AN EMERGENCY AND RETURNED TO FIELD DUE TO FLAP SYSTEM. FAILED DURING TAKEOFF. MECHANIC WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE RIGHT OUTBOARD FLAP TWISTED AND BOUND UP. MECHANICS ARE IN THE PROCESS OF REPLACING ALL RELATED FLAP COMP. 3/20/02 Jun 16, 2002 · N7260 · Cndair CL6002B19SDR COMA0260367AileronFLIGHT 5224 AIRCRAFT HAS A TENDENCY TO ROLL RIGHT DURING FLIGHT MOST NOTICEABLE DURING APPROACH.INSPECTED A/C AND FOUND NOTHING THAT WOULD RELATE TO A ROLL TENDENCY.Jun 10, 2002 · N978CA · Cndair CL6002B19SDR FX72002F00000Jackscrew · inoperativeWHILE DOING (C) CHECK, ROUTINE CARD 65-C-1 FOUND METAL SHAVINGS IN AUX BRAKE CAVITY. REMOVED AND REPLACED STABILIZER JACKSCREW PER MM. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.Jun 7, 2002 · N296SC · Boeing 727224SDR S02427035Carriage · crackedCRACKS WERE FOUND IN NR 4 AND NR 7 CARRIAGES DURING THE OVERHAUL. THE CARRIAGE WERE REPAIRED AS PER BOEING'S SUGGESTION AND OHM. THE DETAILED OF SHOP FINDINGS AND REPAIRED PROCEDURES WILL BE PROVIDED BY MB SHOP.Jun 6, 2002 · Boeing 747400SDR AUS20020798Relay · faulty(AUS) FLIGHT CONTROL TAKEOFF WARNING RELAY FAULTY. CONNECTOR LOCATED AT REAR PRESSURE BULKHEAD DIRTY.May 15, 2002 · Fokker F28MK4000SDR TI12002F00000Control Rod · crackedDURING AIRFRAME INSPECTION FOUND THE COLLECTIVE FLIGHT CONTROL ROD END COLLAR CRACKED.May 13, 2002 · N311LS · Bolkms BK117B1SDR RAIA00204136Vane · inoperative5251-RIC- ADVISORY SYSTEM REPORTED STALL PROTECTION SYSTEM INOP. MAINTENANCE REMOVED AND REPLACED THE #1 AOA VANE.Apr 24, 2002 · N809HK · Emb EMB145SDR C2XA02SH003Spring · corrodedSHV - DURING C-CHECK INSPECTION, THE RIGHT HAND INBOARD AND OUTBOARD FLAP LOWER SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 19, 2002 · N17928 · Emb EMB145ERSDR GTIA020287Switch · failedDTW - FLT 595 - DURING SLAT EXTENSION, THE AUTO SLAT FAIL LIGHT ILLUMINATED AND THE SLAT DISAGREE LIGHT REMAINED ON. BOTH STALL WARNING SYSTEM PROPERLY. AUTO SLAT FAIL LIGHT REMAINED ILLUMINATED WITH SLATS RETRACTED. REMOVED AND REPLACED FLAP HANDLE SWITCH Apr 11, 2002 · N810NK · Doug DC981SDR ABXA010868Fitting · crackedLEFT WING STATION 340, FLAP SUPPORT FITTING WAS CRACKED. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP SUPPORT FITTING IAW DC-8 MM 20-14-00 AND 20-16-00. REMOVED AND REPLACED THE LEFT WING STATION 340 FLAP ACTUATOR CYLINDER AND OPS CHECKED GOOD IAW DC-8Apr 9, 2002 · N842AX · Doug DC861SDR RAIA00204120Sensor · inaccurate5502-STL- LEFT STALL WARNING DURING TAXI. MAINTENANCE REMOVED AND REPLACED LEFT AOA SENSOR.Apr 9, 2002 · N560HK · Jetair JETSTM4101
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