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 ALGA072710A1173Bearing · frozenUPON INSP OF BELLCRANK ASSY, FOUND BEARINGS FROZEN AND UNABLE TO MOVE.Jul 27, 2010 · N863AL · Skrsky S76CSDR A6WA201040541None · noneFLIGHT CONTROLS FELT VERY "MUSHY" WITH A LOT OF SLACK BETWEEN YOKE INPUTS AND PLANE REACTION. UNRESPONSIVENESS OCCURRED IN BOTH PITCH AND ROLL INPUTS FROM BOTH CAPTAINS AND F/O YOKES. INSPECTED FLT CONTROL SYS IAW 27-31-00. NO FAULTS FOUND ALL WORK DONE ON Jul 25, 2010 · N405AW · Cndair CL6002B19SDR CA100721009Electronic Unit · contaminatedSTICK LIMITER WAS NOISY WHILE OPERATING, UNIT REPLACED. DISASSEMBLED AND FOUND ELECTRIC MOTOR CONTAMINATED WITH GREASE FROM GEAR BOX.Jul 20, 2010 · Diamon DA42SDR F3LA2010071800471Computer · faultedREF: PILOT REPORT LOG PAGE 549851 ITEM 1. CLIMBING THROUGH FLIGHT LEVEL 380 ELAC NR 2 FAULTED, ACFT WENT INTO ALTERNATE LAW. AIR TURN BACK TO SMF. REPLACED NR 2 ELAC REF AMM 27-93-34 PAGE BLOCK 401, OPS CHECK GOOD. PERFORMED LAND CATAGORY III CAPABILITIES TESJul 15, 2010 · N939FR · Airbus A319111SDR R61A20100336Module · faultyCREW REPORTED AOA LIMIT FAIL/AP FAIL/PITCH CTRL DISC/FCND IN FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT DEN. MAINTENANCE REMOVED AND REPLACED P-ACE NR 2, AND LT INBOARD LVDT PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.Jul 13, 2010 · N162HL · Emb ERJ190100LRSDR X7PAN881VP070810Control Arm · brokenFOUND CONTROL LOCK SYSTEM PARTIALLY INOPERATIVE ON POSTFLIGHT INSPECTION, FURTHER INVESTIGATION DETERMINED LEFT AILERON LOCK ARM BROKEN AT LOCK FEATURE CONTACT AREA. CAUSE OF PART FAILURE IS UNKNOWN. PART APPEARS TO HAVE SUFFERED OVERLOADING AT CONTACT POIJul 8, 2010 · N881VP · Cessna 560XLSDR UALA2010062202193Computer · malfunctionedVIB WAS NOTED FROM TAKEOFF THRU APPROX FL 280 AND DISSIPATED. APPEARS WORSE IN BACK. ARTIFICIAL VIBRATION FELT WITH ELACS ON. REPLACED BOTH ELACS ARTIFICIAL VIBRATION DISAPPEARED, REPLACED IAW MM.Jun 21, 2010 · N809UA · Airbus A319131SDR ALGA641016868Bearing · bindingBEARING IS BINDING AND HAS AXIAL PLAY BEYOND LIMITS.Jun 4, 2010 · N404AL · Bell 407SDR UALA2010052801853Housing · crackedDURING NDT INSP IT WAS NOTED THAT THE BLOCKING AND RELIEF VALVE HOUSING IS CRACKED.May 28, 2010 · N578UA · Boeing 757222SDR UALA2010052001708Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CAME ON DURING DESCENT. CYCLE R20 FOR ELAC 2 ON 121VU PANEL, ACP ELAC SYS TEST. ELACS HAD BEEN SWAPPED, BAD ELAC NOW IN NR1 POSITION. REPLACED ELAC NR 1 IAW MM, CAT III LAND TEST PERFORMED, CF482. FOUND ELAC 1 IMPRMay 20, 2010 · N426UA · Airbus A320232SDR HNAA2010050800136Pulley · failedON TAKEOFF ROLL, CONTROLS FOR AILERON AND SPOILERS WHERE LOCKED UP. INSP SYS, FOUND PULLEY SEIZED IN RT CTR WING OF RT AILERON SPLITTER QUADRANT. R & R PULLEY IAW MM 27-12-00.CHECKED CABLE ENSIONS IN ACCORDANCE WITH MM 27-00-00. TENSIONS WITHIN TOLERANCE. ALLMay 8, 2010 · N975 · Dhav DHC8102SDR UALA2010041901293Computer · faultedSUBSTANTIAL YAW TO RT ON ROTATION. SUSPECT TIRE OR UNCOMMANDED RUDDER INPUT. REPLACED ELAC 1. OP CK'D GROUND SCAN AND MSG FOR ELAC 1 DID NOT APPEAR.Apr 19, 2010 · N806UA · Airbus A319131SDR DALA1405309217Jackscrew · damagedHORIZONTAL STABILIZER JACKSCREW ASSY DAMAGED. REPAIRED IAW AA 2740-01071.Apr 9, 2010 · N917DN · Doug MD9030SDR ANCF2010031900059Unknown · multiple failREJECTED TAKEOFF. RTO PERFORMED DUE TO AIR SPEED DISAGREE - FLAPS DISAGREE RAD BACKUP CTL, AOA DISAGREE *RISK OF UNDUE STALL WARN* IN STATUS PAGE. THE TFU. 27-90-00-36. WAS APLIED WITH RESET OF THE BOTH ´FCDC´CB AND ALL THE SYS BACK TO NORMAL OPERATION.Mar 19, 2010 · N967CG · Airbus A330243SDR C77A248526Unknown · unknownON TAKE-OFF, AT V1 ACFT PULLED HARD TO THE LT. ON LANDING, NOTHING ABNORMAL NOTICED. MX PERFORMED NOSE GEAR STEERING INSP IAW AMM 32-49-01, NO DEFECTS NOTED ACFT OK FOR SERVICE AT THIS TIME. ALSO INTERROGATED CMC NO LATCHED MESSAGES.Mar 18, 2010 · N624CZ · Emb ERJ170200LRSDR APC2010F00000Bolt · brokenON PREFLIGHT, THE PILOT FOUND THE STABILATOR TO BE EXTREMELY LOOSE AND NOTIFIED MX. WHEN REMOVED TAIL CONE FOUND A BROKEN BOLT ON THE RT THAT HAD BACKED OUT. IMMEDIATELY GROUNDED THE WHOLE FLEET UNTIL SUCH TIME AS WE COULD INSPECT ATTACHING POINTS, BEARINGS Mar 12, 2010 · N36319 · Piper PA34200TSDR C2XA10IA083Unknown · malfunctionedIAH - FLIGHT 2257, DURING TAKEOFF THE CREW REPORTED THAT THE FLIGHT CONTROLS FELT AS THOUGH THEY WERE POPPING AND CATCHING WHEN MOVED LEFT OR RIGHT OF CENTER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OFeb 25, 2010 · N13955 · Emb EMB145LRSDR UALA2010021700610Trim System · unknownRUDDER TRIM BEYOND LIMITS. CHECKED FOR FLOATING SPOILERS. FOUND RT AILERON DOWN .3 ADJUST AILERON PCU IAW MM TO .060 DOWN. CHECKED RIG OF RATIO CHGER AND PCU'S. RATIO CHANGER CKD GOOD. BROUGHT RUDDER IN RIG BY ADJUSTING PCU'S. RUDDER CENTERED .050 DIFF WHENFeb 16, 2010 · N569UA · Boeing 757222SDR HNAA2010022400045Unknown · unknownREACHING V1 SPEED 110/115 KNOTS, ACFT FAILED TO ROTATE. REJECTED TAKEOFF. VISUALLY INSPECTED ELEVATOR, TRIM TABS, GUST LOCK CONTROL COLUMN QUADRANT CABLES UNDER COCKPIT FLOOR AND CABLE RUNS THROUGH AFT BAY TO VERTICAL STAB. CHECKED OPERATION OF ELEVATOR GUSTFeb 10, 2010 · N328EN · Dhav DHC8311SDR 2010FA0000165Roll Pin · failedTHE ROLL PIN THAT SECURES THE CHAIN SPROCKET TO THE TRIM WHEEL SHAFT NEXT TO THE TRIM WHEEL, SHEARED OFF AND WAS TURNING FREELY ON THE SHAFT. RENDERING THE ENTIRE STABILIZER TRIM SYS, INOPERATIVE.Feb 9, 2010 · N7551K · Cessna 180JSDR YJX2010F00000Pushrod · failedDURING POST-INSP CHECKS OF THE FLIGHT CONTROLS, A CLICKING NOISE WAS NOTICED COMING FROM THE AILERON/RUDDER INTERCONNECT AREA. INSP OF THE AILERON/RUDDER INTERCONNECT SYS NOTED THE NTERCONNECT ROD ASSY AT THE AILERON/ RUDDER INTERCONNECT SPRING END WAS ROCKINFeb 5, 2010 · N236LB · Cessna 560XLSDR UALA2010012500304Cable · shortedPRIMARY FLT CONTROL MSG 27-13006. FOUND NR 1 SPOILER PCU CABLE SHORTED TO SHIELD BETWEEN CONNECTORS DM27116 AND D2139P. REPLACED CABLE ASSY (PN 23351-001). ACE TEST FAILED AGAIN WITH 2 NEW MESSAGES (27-13057 AND 27-13058). RT AIMS M10 HAS INTERNAL FAULT. REJan 25, 2010 · N224UA · Boeing 777222SDR 2010FA0000035Control Cable · frayedDURING FLAP & AILERON CABLE INSP FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS & WAS ABLE TO CATCH FRAYED WIRES WITH A RAG & COULD SEE A SUBSTANTIAL GROOVE IN CARRY-THRU CABLE. CABLE TENSIONSJan 8, 2010 · N558ER · Cessna 172SSDR 2010FA0000034Control Cable · groovedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS AND WAS ABLE TO CATCH FRAYED WIRES WITH A RAG AND COUJan 8, 2010 · N558ER · Cessna 172SSDR UALA2010011100140Module · faultyCTR SYS WILL NOT TRIM NOSE DOWN. ACFT WILL NOT TRIM NOSE DOWN WITH CTGTR SYS, NOSE UP OK. SINGLE CHANNEL CHECKS OK, LT SYS TRIMS NORMAL, ALT TRIMS NORMAL. OPS CHK INDICATES RT WILL NOT TRIM IN PRIMARY AND ALTERNATE. REPLACED RT STAB TRIM LOCKOUT MODULE. ACFJan 8, 2010 · N651UA · Boeing 767322SDR UALA2009122403993Shutoff Valve · leakingHYD LEAK FROM LT FLT CONTROL SHUTOFF VALVE BODY. FOUND LEFT LATEREAL CONTROL SHUTOFF VALVE LEAKING. REPLACED LEFT LATEREAL CONTROL SHUTOFF VALVE. DEVICE WORKS FINE. NO LEAKS DETECTED ON GROUND TEST.Dec 23, 2009 · N643UA · Boeing 767322SDR UALA2009121603897Pca · malfunctionedWHEN ACCOMPLISHING FLIGHT CONTROL CHECK, ELEVATOR CHATTERS. DOES NOT FEEL LIKE CONTROL COLUMN PROBLEM, POSSIBLY HYDRAULIC OR FLT CONTROL PROBLEM, PER CREW. REPLACED LT ELEVATOR CENTER SYSTEM PCA. LEAK CHECK AND OPS CHECK GOOD.Dec 16, 2009 · N665UA · Boeing 767322SDR UALA2009121103812Computer · faultyALT LAW ECAM, RTFL. REPLACED NR 1 ADIRU & ELAC 2. OPERATIONAL CHECKS OKAY.Dec 11, 2009 · N850UA · Airbus A319131SDR AALA20091203TUL05Tab · damagedLEFT ANTI-FLOAT TAB TRAINING EDGE HAS STATIC BURNS. INSTALLED HOT BOND DOUBLER PER ESO 80084.Dec 3, 2009 · N237AA · Doug DC982SDR GTIA0900033Computer · odorELAC 1 FAILED AND STRONG ODOR OF ELEC BURNING, IDENTIFIED AS ELAC 1.Nov 19, 2009 · N517NK · Airbus A319132SDR UALA2009090802800Computer · faultedELAC 2 PITCH FAULT, FLIGHT DIVERTED. SWAPPED ELAC 1 AND 2 FAULT FOLLOWED BOX REPLACED ELAC2. ACP OPS TEST OF ELAC2 AND CAT III MM 22-97-00 PASSED CAT III LAND TEST.Sep 8, 2009 · N433UA · Airbus A320232SDR UIEA200900053Unknown · unknownFLYING WITH AUTOPILOT OFF, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, ACFT ROLLED HARD LEFT, INTERMITTENT. WITH AUTOPILOT ENGAGED, EXTENDED SPEEDBRAKES TO FLIGHT DETENT, YOKE MOVES RIGHT APPROX 2 UNITS TO MAINT WING LEVEL, ALSO INTERMITTENT. ACCOMPLISHED VISUAL ISep 2, 2009 · N496MC · Boeing 74747UFSDR CA090903001Bungee · broken1/16 STABILATOR BUNGEE CABLE SEPARATED AT UPPER PULLEY WHERE IT MAKES A 90 DEGREE BEND.Aug 31, 2009 · Piper PA23250SDR SWIA200922418Unknown · malfunctionedLOUD POP AFTER TAKEOFF WITH ASSOCIATED VIBRATION IN NOSE AREA. AIRCRAFT CONTROLS SLUGGISH ON APPROACH. (FLT 4580) INSPECTED NOSE SECTION, DOORS, AND LANDING GEAR WITH NO DEFECTS FOUND. ACCOMPLISHED FLIGHT CONTROL CHECKS AND GEAR SWINGS, ALL CHECKS NORMAL.Aug 20, 2009 · N803SK · Cndair CL6002D24SDR CA090821004Control Cable · dislodgedFOUND THS CONTROL CABLE HAS CUT INTO FLOORBEAM C14 AT PULLEY ATTACH BRACKET. GOUGE IS APPROX 1/4" DEEP. THIS CABLE FOUND TO BE NOT IN THE GROOVE OF THE ASSOCIATED PULLY. THE RETAINER IS IN PLACE, BUT THE CABLE HAS JUMPED PAST AND HAS STARTED TO "SAW" A GROOAug 19, 2009 · Airbus A320211SDR AALA2009051100002Unknown · unknownELEVATOR SYMETRY STATUS MESSAGE DURING CLIMBOUT. RETURNED ORD WITHOUT INCIDENT. RESET FAULT BALL AND PERFORMED THE REST OF THA SAM BITE PROCEDURE AND THE SYSTEM CHECKS OK. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)May 11, 2009 · N7667A · Boeing 757223SDR DLM90090840Control Unit · failedELEVATOR SPLIT MESSAGE ON EOAP FOR LOSS OF LEFT ENG GENERATOR. TROUBLESHOT PER MD-90 TSM 27-30 PAGE 5. DUE TO LEFT GENERATOR POWER FAULT SUSPECT ACS SYSTEM LOST LEFT ELEVATOR POSITION INDICATION CAUSING FAULT. CLEARED ELEVATOR SPLIT MESSAGE THROUGH MCDU. May 8, 2009 · N913DN · Doug MD9030SDR UALA2009043001263Computer · malfunctioned"FLIGHT CONTROL SYS" STATUS MESSAGE IS DISPLAYED. FAILS ACE MONITOR GROUND TEST MSG27-13007. REPLACED RT ACE-NO HELP. PERFORMED ALL STEPS FOR FIM 27-02 TASK 809 AND IT STILLS FAILS GROUND TEST. REPLACED R-ACE WITH A KNOWN GOOD ACE FROM AC2982. NO HELP, REApr 30, 2009 · N793UA · Boeing 777222SDR DXTA2009042803621Unknown · unknownAT FL390 WITH AUTOPILOT ON THE ACFT APPEARED TO BE DUTCH ROLLING. WITH AP OFF, ACFT AILERONS ARE VERY STIFF AND DIFFICULT TO OPERATE. ROLLS STARTED AT 2 DEGREES AND FINALLY WAS DOING 15 DEGREES. SAT WAS -60 AND WHEN WE DESCENDED TO FL 270 THE PROBLEM WAS GREATApr 28, 2009 · N712QS · Gulstm 200SDR F3LA2009042100078Computer · inoperativePILOT REPORTED AFTER TAKEOFF THE AIRCRAFT DID NOT AUTO TRIM, CONSTANT FORWARD PRESSURE WAS REQUIRED TO MAINTAIN DESIRED PITCH. SAME RESULT ON BOTH STICKS. AIRCRAFT TRIMMED NOSE UP IF NO STICK INPUT RUNAWAY NOSE UP. MAINTENANCE REMOVED AND REPLACED THE NR 2 Apr 20, 2009 · N801FR · Airbus A318111SDR DXTA2009041303588Unknown · unknownIN FLIGHT, NOTICED LACK OF RESPONSIVENESS OF FLIGHT CONTROLS FWD AND AFT. APPLIED HYDRAULIC POWER TO A AND B SYSTEMS. PERFORMED TRAVEL CHECKS. MEASURED LT ELEVATOR 18.8 DEGREES UP AND 14.0 DEGREES DOWN. MEASURED RT ELEVATOR 18.9 DEGREES UP AND 14.1 DEGREES DOApr 12, 2009 · N938QS · Cessna 750SDR DXTA2009040603583Bellcrank · stiffROLL CONTROL IS VERY TIGHT IN BOTH DIRECTIONS. INVESTIGATED AND FOUND RT SPOILER BELLCRANK STIFF, LUBRICATED AND OPS CHECK WAS SATISFACTORY IAW MM 27-12-03.Apr 3, 2009 · N921QS · Cessna 750SDR DXTA2009040603581Bellcrank · stiffACFT REQUIRES LARGER THAN NORMAL INPUTS ON ROLL AXIS. PARTICULARLY NOTICEABLE AT SLOW SPEEDS DURING LANDING. DURING LANDING WITH 10 KT CROSSWIND, YOKE WAS AT LT STOP AND COULD NOT STOP ACFT ROLL. FOUND LT ROLL SPOILER PCU BELL CRANK STIFF. LUBRICATED AND CApr 3, 2009 · N947QS · Cessna 750SDR HYIA525RHServo · inoperativeON APPROACH, CREW REPORTED THAT THE AUTO-PILOT WOULD NOT DISENGAGE THROUGH NORMAL MEANS. AUTO PILOT AND ELECTRIC TRIM (ELEVATOR) CIRCUIT BREAKERS WERE PULLED TO DISCONNECT AUTO-PILOT. MAINTENANCE INSPECTED AIRCRAFT AND AUTO-PILOT FUNCTIONED NORMALLY, BUT FOMar 29, 2009 · N525RH · Cessna 402CSDR FDEA200903271095Controller · failedON FINAL WHEN MOVING FROM FLAP 20 TO FLAP 40 THE FLAPS STUCK AT 20. RECYCLE WITH NO HELP. LANDED WITH FLAPS 30/20. REMOVED AND REPLACED NR 1 SFCC IN REF TO MM 27-51-18-4 , CYCLED SLAT/FLAPS NO FAULTS NOTED, OK FOR SERVICE.Mar 27, 2009 · N730FD · Airbus A300B4622RSDR A6WA200940144Adc · malfunctionedLOST DIR CONTROL AT V1, TOOK PLANE AIRBORNE, DID A FLYBY THEN LANDED. RT WING LIFTED SUDDENLY AND LOST 15 KTS IND AIRSPEED ON F/O SIDE, MORE BRISK THAN A WIND DIRECTION SPEED, WAKE TURBULENCE WAS NOT AN ISSUE. REMOVED AND REPLACED ADC 2 FOR VAR CIRCUITRY 350Mar 22, 2009 · N461AW · Cndair CL6002B19SDR QXEA2009031600182Unknown · unknownPDX- AIL TRIM STUCK AT FULL LEFT WING DOWN POSITION. C/W OPS CHECK OF AILERON TRIM SYSTEM IAW AMM TASK 27-11-00-710-802. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.Mar 10, 2009 · N619QX · Cndair CL6002C10SDR HALA2009022500066Bearing · damagedIN ORDER TO FLY STRAIGHT AND LEVEL THE AILERON TRIM AND RUDDER TRIM HAD TO BE ALIGNED GREATLY TO THE RIGHT. VISUAL CKS OF A/C FLT CONTROL, CONDITION SECURE CKS OK. NO DEFECTS NOTED. FOUND RT INBD MOVEABLE VANE TRACK SUPPORT BOTTOM BEARING DAMAGED. REMOVED Feb 25, 2009 · N478HA · Boeing 717200SDR HNAA2009020700047Unknown · unknownUNABLE TO ROTATE ACFT ON TAKE OFF ROLL. VISUAL AND OPS INSPECTION OF ACFT ELEVATOR FLIGHT CONTROLS AND SURFACES, NO DEFECTS NOTED. OK FOR SERVICE. ACFT RELEASED FOR AN EVALUATION FLIGHT DUE TO UNABLE TO ROTATE ACFT ON TAKE-OFF, MX ACTION COMPLETE SUBJECT TOFeb 3, 2009 · N330EN · Dhav DHC8311SDR CA090129008Tensioner · stuckDURING AN INSPECTION IN THIS AREA AN A/C ENGINEER FOUND THIS PART COMPLETELY JAMMED. THERE IS NO TASK FOR THAT PART IN THE PSP 495.Jan 29, 2009 · Cndair CL2156B11215
Back to JASC 2700