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 SWAA981472Flight Controls · shimmyAIR RETURN, ON CLIMBOUT A/C STARTED TO SHAKE/SHIMMY AT 160-180 KTS. FLAPS DOWN. AT 210-250 KTS CLIMBING CONTINUE SHAKE/SHIMMY LEVEL FLIGHT (10K) 230-250 KTS NOT AS BAD DURING DESCENT. CLEAN 230-210 KTS, SHAKING NOT AS BAD AS LEVEL FLT. FLAPS 5 GEAR DOWN 170Jul 24, 1998 · N312SW · Boeing 7373H4SDR 98ZZZX3111Bellows · wrong partBELLOWS REJECTED, NEW OUT-OF-BOX. INCORRECTLY PACKAGED. PARTS DO NOT MATCH PART NUMBER ON LABEL. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM.Jul 20, 1998 · N951AM · Bolkms BK117A3SDR 98ZZZX2558Flight Control · oscillationCLO/ADZ - FLT 1176 - STRONG PITCH OSCILLATION WAS FELT DURING FLIGHT. LEVELLED AT FL 240, SPEED 260 KNOTS, ENGINE ANTIICE ON. OUTER WING AND TAIL ANTI-ICE ON. CHECK LIST WAS PERFORMED. VISUAL INSPECTION PERFORMED ON ELEVATORS AND CONTROL SYSTEM. OPERATIOJun 15, 1998 · N504MM · Bac AVRO146RJ100SDR CA971104005Control Cable · frayed(CAN) DURING ROUTINE INSPECTION, WIRES/STRANDS OF FLAP CABLE ASSY WERE FOUND BROKEN. NEW CABLE INSTALLED AND SYSTEM RIGGED.Mar 31, 1998 · Cessna 414ASDR AU980432Bearing · seized(AUS) ALL ELEVATOR, ELEVATOR BELLCRANK AND RUDDER BEARINGS SEIZED.Mar 24, 1998 · Cessna 210KSDR CA971223003Circuit Breaker · chafed(CAN) THE POWERED FLIGHT CONTROL SYSTEM (PFCS) CIRCUIT BREAKER WAS TRIPPING. CB LOCATED ON THE LEFT 26VAC BUS, POSITION Q1. APPARENT CAUSE WAS THE CIRCUIT BREAKER LOAD TERMINAL WAS SHORTING TO GROUND VIA THE MOUNTING BRACKET SUPPORTING 2423-P1. BRACKET WAS Dec 10, 1997 · Dhav DHC8311SDR DL76L971846Sam Module · failedEICAS/OVERHEAD RUDDER RATIO AND AILERON LOCK-OUT MESSAGE CAME ON AFTER LEVEL OFF AND A/P DISCONNECT. TRIED RESET, NO HELP. A/C SUSTAINED LIGHTNING STRIKE AFTER TAKEOFF. REPLACED LEFT AND RIGHT SAM MODULES PER MM. MCDP TEST NUMBER 40 ALL OK. PERFORMED LIGHSep 19, 1997 · N189DN · Boeing 767332SDR CA970807043Cyclic · binding(CAN) ABNORMAL CYCLIC CONTROL NOTED BY PILOT. THROTTLE CABLE IN VERTICAL TUNNEL BINDING ON CONTROL TUBES WHEN CYCLIC MOVED TO EXTREME POSITIONS.Jul 4, 1997 · Bell 206BSDR AU970746Cable Guard · cracked(AUS) NUMEROUS CABLE GUARD ASSEMBLIES IN MAIN CABIN CABLE VERTICAL RUNS CRACKED AND EMBRITTLED - CABLE OPERATING SYSTEMS INCLUDED AILERON, WING FLAP, NOSEWHEEL STEERING AND LANDING GEAR BRAKES -IN ADDITION VERTICAL CABLE GUARDS IN FORWARD CARGO COMPARTMENTFOR May 16, 1997 · Boeing 747312SDR CA970605001Flight Control · severe pitch up(CAN) ON CLIMB, AIRCRAFT PITCHED NOSE UP. AIRCRAFT DIFFICULT TO CONTROL. AIRCRAFT LANDED SAFELY. INVESTIGATION IN PROGRESS TO DETERMINE CAUSE OF SEVERE PITCH UP.May 14, 1997 · Cvac 340CVACSDR HAIHEEA9644Cylinder · freezesSHAFT FREEZES DUE TO MOISTURE.Apr 29, 1997 · N3122G · Skrsky S76ASDR AU970640Flight Controls · loose(AUS) AIRCRAFT CONTROLS LOOSE - AIRCRAFT MADE AN EMERGENCY LANDING IN A PLOUGHED PADDOCK BREAKING THREE BOLTS AND A SADDLE ON THE LH MAIN LANDING GEAR, THE LH BRAKE LINE AND DAMAGING ALL THE SPATS - THIS DEFECT WAS RECEIVED FROM THE AUF AND IS FOR INFORMATION Apr 22, 1997 · Amtr JABIRUSKSDR 97ZZZX1637Control Cable · corrodedAIRCRAFT TOTAL TIME 3,075 HRS. AIRCRAFT BUILT AS LAND PLANE AND MODIFIED FOR FLOATS INSTALLATION IAW WIPAIRE STL SA1483GL. POH SUPPLEMENT REQUIRES 'OPERATION IN FRESH WATER ONLY' PLACARD DUE TO NO STAINLES STEEL CONTROL CABLES OR FUSELAGE INTERIOR PRIMER. CMar 17, 1997 · N7485Q · Cessna TU206FSDR AU970285Control Cable · faulty(AUS) CONTROL CABLES ATTACHED TO PRIMARY CONTROL QUADRANT IN CONTROL COLUMN YOKE HAD FAULTY SWAGING - DURING TESTING CABLES PULLED THROUGH THE NICOPRESS SLEEVES AT A LOAD OF 610 LBS (NORMAL FAILURE LOAD 2200 LBS TO 2300LBS) - AIRCRAFT IS IMPORTED FROM THE USA Mar 4, 1997 · Univar 415DSDR AWXA9700139Flight Controls · out of adjustA/C HAD ROLLING TENDENCIES THROUGHOUT FLT. INSPECTED NR 1, NR 2, NR 7 AND NR 8 CARRIAGE BEARINGS. SHOOK FLAPS. NO PROBLEMS FOUND. INSPECTED AILERON CABLES, PULLEYS, ECT L-R NO DEFECTS. AILERON TRIM CENTERING. OPS CHECK GOOD. C/W RUDDER PCU ADJ-TEST PER Feb 22, 1997 · N174AW · Boeing 73733ASDR 97ZZZX1986Pneu Drive Unit · fail testUNIT FAILED FUNCTIONAL TEST. FOUND DIAPHRAGM ASSY 886083-5 MISSING SPACER/SLEEVE P/N 113842-146. SPRING RETAINER P/N 3166820-1 MISSING. WRONG SPRING IN VALVE, SPRING P/N 3160871-1 IS NOT USED WITH VALVE 3290402-1. SB 27-1014 NOT C/W. SB 27-1042 PARTIALLY Feb 21, 1997 · Boeing 747*SDR VJ970047Bracket · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP., THE PULLEY BRACKET MOUNTED ON L-WHEELWELL FORWARD BULKHEAD SECURING PULLEYS FOR ALL LEFT WING FLIGHT CONTROL CABLES HAS EXTREMELY DEEP PITTING CORROSION ON UPPER AND LOWER MOUNTING LUGS. REMOVED AND REPLACED LEFT WFeb 7, 1997 · N922VV · Doug DC932SDR AU970239Control Cable · broken(AUS) UNKNOWN CABLE BROKEN - LIMITED INFORMATION PROVIDEDFeb 5, 1997 · Piper PA34200TSDR 97ZZZM229Flight Control · malfunctionDTW - FLT 874 - ON CLIMB-OUT OF 8,000 FT, HEARD A LOUD BANG FROM REAR OF THE A/C. COULD NOT DETERMINE THE SOURCE, DECLARED AN EMERG AND RETURNED TO DTW. ALSO, EXPERIENCING UNCOMMANDED ROLL AND RUDDER FLUCTUATIONS WHICH INCREASED WITH SPEED ABOVE 10,000 FT. Jan 24, 1997 · N934ML · Doug DC931SDR AU970396Computer · faulty(AUS) NO1 AND NO2 ELAC (ELEVATOR/AILERON COMPUTER) FAULTY - WORKSHOP TESTING FOUND FAULTS WITH BOTH COMPUTERS BUT COULD NOT CONFIRM THAT THE FAULTS CONTRIBUTED TO THE FAILURESJan 3, 1997 · Airbus A320212SDR MALA965222Flight Controls · buffetingFLT 3090 - ON CLIMB-OUT FROM MSP, THE CREW NOTED AN AERODYNAMIC BUFFETING EVERY 5 SECONDS IN AIRSPEED RANGES BETWEEN 160-230 KNOTS. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE PERFORMED TROUBLESHOOTING TO THE HYDRAULIC SYSTEM, FLIGHT CONTROL CABLE TENSION. ALNov 27, 1996 · N438MA · Swrngn SA227ACSDR 96ZZZX4714Body · corrosionCONTROL SURFACE DAMPER'S ALUMINUM BODY HAS EXCESSIVE CORROSION IN THE INSIDE DIAMETER.Aug 26, 1996 · Lkheed 1011*SDR CA960802004Cables · worn(CAN) WHILE CARRYING OUT AN ITRAN INSPECTION, A MOUSE NEST PROMPTED AN INSPECTION FOR CORROSION UNDER THE COCKPIT FLOOR. CABLES IN THAT AREA WERE FOUND TO HAVE AN UNACCEPTABLE AMOUNT OF BROKEN WIRES IN THE AREA OVER THE PULLEYS. THE PREVIOUS LOGS SHOW THAT TJul 26, 1996 · Let L13BLANIKSDR 96FDEA01346Bracket · crackedSNRM 6004 R/H WING - O/B SLAT DRIVE MECHANISM, OUTER BRKT HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. R/R SLAT DRIVE MECHANISM BRACKET PER MM 27-83-02.Jul 26, 1996 · N321FE · Doug DC1030SDR AWXA960329Elac · failedBOS - FLT 2821 - AIR TURNBACK. ELAC 1 FAILED IN-FLIGHT. RESET NO GOOD. REMOVED AND REPLACED ELAC 1 PER MM 27-93-34. SYSTEM CHECKS GOOD. PART TOTAL CYCLES, 4,501. (X)Jul 5, 1996 · N639AW · Airbus A320232SDR AWXA960297Flight Cntrl Sys · malfunctionedBUR/PHX - FLT 2545 - UNCOMMANDED ROLL TO LEFT ON DESCENT. 1,800 FEET AUTOPILOT ON VNAV AND LNAV JUST STOWED SPEED BRAKE AND ACFT ROLLED VIOLENTLY TO LEFT. HAPPENED 2ND TIME WITH A/P OFF HAND FLYING. C/W BITE AND FUNCTION CHECK, NO DEFECTS NOTED. C/W BOTH AJun 29, 1996 · N303AW · Boeing 7373G7SDR AWXA960193Elac · failedPHX - FLT 845 - ABORTED TAKEOFF, ELAC PITCH TRIM FAULT. REMOVED AND REPLACED ELEVATOR AILERON COMPUTER. (M)Apr 13, 1996 · N624AW · Airbus A320231SDR PLG4396DG4Cables · chafedDURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND IN LEFT INBOARD AND OUTBOARD CONTROL CABLES AT SEVERAL FRAMES. BOTH CABLES WERE REPLACED IN FORWARD AREA OF CABIN IAW SAAB AMM CHAPTER 27. ALL RIGGING AND REQUIRED CHECKS WERE PERFORMED PER AMM CHAPTER 27. REApr 3, 1996 · N359BE · Saab 340BSDR 96ZZZX2271Cables · chafedDURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND IN LEFT INBOARD AND OUTBOARD CONTROL CABLES AT SEVERAL FRAMES. BOTH CABLES WERE REPLACED IN FORWARD AREA OF CABIN IAW SAAB AMM CHAPTER 27. ALL RIGGING AND REQUIRED CHECKS WERE PERFORMED PER AMM CHAPTER 27. REApr 3, 1996 · N359BE · Saab 340BSDR CA960327007Trim Motor · shorted(CAN)THE TRIM MOTOR WAS NOT WORKING. INSPECTION FOUND THE ARMATURE HAD SHORTED AGAINST THE HOUSING. A NEW ARMATURE WAS INSTALLED.Mar 8, 1996 · Beech 100BEECHSDR 9604843221Computer · malfunctionedDURING TAKEOFF ROLL, RECEIVED F/CTL ELAC 2 PITCH FAULT MESSAGE. TAKEOFF WAS ABORTED AT APPROXIMATELY 80 KNOTS. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REPLACED THE NR 2 ELEVATOR AILERON COMPUTER, OPERATIONAL CHECK OK.Feb 22, 1996 · N321US · Airbus A320211SDR 96FDEA00288Flt Cont Cables · brokenDURING REPLACEMENT OF HYD REVERSABLE MOTOR PUMP SHUTOFF VALVE, BROKEN FLIGHT CONTROL CABLES WERE FOUND IN CENTER GEAR WELL. REMOVED AND REPLACED BOTH FLAP INPUT AILERON LOCKOUT CABLE RUNS. ADJUSTED AS PER 27-10-00 PAGE 515, RII REQUIRED. OPS CK GOOD, (P/N SFeb 17, 1996 · N317FE · Doug DC1030SDR COMA9531195Flight Controls · vibrationDURING TAKEOFF, A FORE AND AFT VIBRATION WAS NOTED IN CONTROL YOKES. FLIGHT CONTROL SYSTEM WAS INSPECTED AND NO DEFECTS NOTED. ACFT RELEASED FOR FLIGHT CHECK WHICH WAS SATISFACTORY.Nov 17, 1995 · N158CA · Saab SF340ASDR 95ZZZX6048Cables · frayedFOUND FLAP FOLLOW-UP CABLE, ELEVATOR CABLE, AND AILERON CABLE AT CONTROL LOCK ASSY FRAYED WITH 4 BROKEN STRAINS. FOUND RUDDER CABLES UNDER PILOTS FLOORBOARDS FRAYED AT FAIRLEADS. PART NUMBERS INVOLVED, 6565007-188, 6565007-193CR, 6565007-3, AND 6565007-135. Oct 19, 1995 · N551CF · Cessna 551SDR 95UAL900171Controls · out of trimUNPLANNED STOP IN DEN, ABNORMAL TRIM INDICATIONS DURING CLIMBOUT AND CRUISE, WITH INCREASING AIRSPEED .82M FL 310 UP TO 3 UNITS OF RUDDER AND 0 UNITS OF AILERON, OR 3 UNITS OF AILERON AND 0 UNITS OF RUDDER. CHECKED FUEL LOAD UPON ARRIVAL AT DENVER, FUEL IMBAOct 4, 1995 · N7298U · Boeing 727222SDR SWIA95640Tip · damagedRT WING TIP DAMAGED AND DELAMINATING, NEEDS TO BE REPLACED. FITTED NEW WING TIP FOR RT WING.Sep 22, 1995 · N212SW · Emb EMB120ERSDR 95FDEA01363Arm · crackedUPON DISASSEMBLY OF CONTROLS, ARM AP NR 7202-5 WAS FOUND CRACKED AT SPLINE SHAFT MOUNT END. CRACK ORIGINATED IN CLAMP UP BOLT PLANE AND FOLLOWS GRAIN OF PART LENGTH. THIS CONDITION FOUND ON 2 OF ARMS FROM THIS A/C AND THE ARMS WERE REPLACED.Sep 15, 1995 · N301FE · Doug DC1030FSDR 95ZZZX5637Torque Tube · crackedINSPECTION FOUND STICK TORQUE TUBE FORWARD PIVOT CRACKED, ON LEFT SIDE.Sep 13, 1995 · N89994 · Piper PA18150SDR REXA95053Control Wheel · stuckLANDING AT GTR, CONTROL WHEEL GOT STUCK AND HAD TO FORCE FOR OUT GO-AROUND TO UNSTICK IT. IN PATTERN AT GTR CONTROL WHEEL HARD TO MOVE LEFT, RIGHT, FORWARD AND BACK. REF AML'S 344376, 344377, 344380, 344381, 344383 AND 344383 FOR INSPECTION OF AIRCRAFT AND DAug 21, 1995 · N304PX · Bag JETSTM3101SDR 95UAL900105Flight Controls · yaw rightRETURNED TO THE FIELD UNDER AMBER ALERT DUE TO A HARD YAW TO THE RIGHT ON TAKEOFF. BEFORE ROTATION DURING TAKEOFF ROLL, AIRCRAFT FELT AS IF RT MAIN TIRE BLEW OR NR 3 ENGINE FAILED. VIBRATION ALSO FELT. ONCE AIRBORNE, EVERYTHING NORMAL. ACCOMPLISHED A GENERAAug 21, 1995 · N7289U · Boeing 727222SDR 95ZZZX3096Terminal · separatedDURING FABRICATION OF A REPLACEMENT PRIMARY FLIGHT CONTROL CABLE FOR A TRANSPORT CATAGORY AIRCRAFT UTILIZNG AN AT-520TK CABLE TERMINAL SWAGER KIT, AN A AND P TECHNICIAN EXPERIENCED A TOTAL SEPARATION OF THE THREADED PORTION OF A MS2126066-LH TERMINAL AT THE CUMay 19, 1995 · N659WL · Gulstm G1159SDR 9506963231Computers · malfunctionedAT 25,000 FEET DURING CLIMB, THE AIRCRAFT ROLLED RIGHT AND ELAC NR 1 FAULTED. RESET WAS OK, THREE MINUTES LATER THE AIRCRAFT ROLLED AGAIN WITH FAULT DISPLAY SYSTEM INDICATING ELAC NR 2 MALFUNCTION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLAApr 28, 1995 · N331NW · Airbus A320211SDR VTZA95146Computer · failureFLT NR 6523 - IAD-PWM - DURING CRUISE RETURNED TO IAD DUE TO THE AUTOPILOT FAILING AND MODE C INOP. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE SELECTED ATC WINDOW TO READ ATC ALTITUDE. PERFORMED TRANSPONDER CHECKS, OPS CHECKS GOOD. OPENED DMI NApr 21, 1995 · N318UE · Jetair JETSTM4101SDR 95ZZZX1311Control Cable · mismanufacturedDURING AN ANNUAL INSPECTION ON A PIPER SUPPER CUB PA-18A, FOUND NEW STAINLESS CABLES HAD BEEN PREVIOUSLY INSTALLED. INSPECTION OF THE CABLES SHOWED THE COPPER N1COMPRESS SLEEVES WERE INSTALLED ON THE STAINLESS CABLES IN PLACE OF THE SILVER COLORED N1COMPRESS SFeb 28, 1995 · Piper PA18ASDR 95UALA32012Flight Controls · malfunctionedCREW REPORTED THAT AFTER TAKEOFF, AIRCRAFT WANTED TO FLY RIGHT WING DOWN, NOT STRAIGHT. AFTER ALTITUDE WAS REACHED, PROBLEM WENT AWAY. AFTER REACHING AN ALTITUDE OF 12788 CREW STATED THAT IN CLIMB AIRCRAFT TENDED TO FAVOR LT WING LOW AND AT HIGHER THAN NORMAFeb 28, 1995 · N417UA · Airbus A320232
Back to JASC 2700