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 A0512001Jackscrew · failedON APPROACH, WITH FLAPS SELECTED TO 5 DEG, STAB TRIM WHEEL RAN AWAY FROM APPROX 5 UNITS NOSE UP TO 0 DEG AND BUFFETING WAS FELT IN FLT CONTROLS. AC STARTED A 2000 TO 4000 RPM RATE OF DESCENT, PILOTS TRIED TO INPUT UP ELEVATOR TO ARREST SINK RATE, THERE WAS NONov 22, 2005 · N720CK · Boeing 727200SDR DXTA200501089Warning Light · illuminatedTAKEOFF ABORTED BECAUSE OF 2 AMBER CAS MESSAGES. ONE WENT OUT BEFORE IT WAS IDENTIFIED. THE -LOWER YD OFF STAYED ON- YAW DAMP SYSTEM OPERATIONALLY CHECKS NORMAL IN ACCORDANCE WITH HONEYWELL PRIMUS 2000 MAINTENANCE MANUAL FOR CITATION X.Nov 16, 2005 · N960QS · Cessna 750SDR SIMA200530403Sensor · inoperativeCREW RECEIVED STABILIZER FAULT STATUS MESSAGE IN CRUISE. REPLACED HORIZONTAL STABILIZER ACTUATOR POSITION SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Oct 28, 2005 · N514AE · Cndair CL6002C10SDR VNAA0508028Fcu · malfunctionedDURING CRUISE FLIGHT WITH FLAPS AT 0 DEGREE THE FLAPS FAIL MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND PERFORMED A NO FLAP LANDING AT DESTINATION. MAINTENANCE INTERROGATED THE MDC, FECU, AND SDU. NO FAULTS WERE DISPLAYED. THE FLAP SYSTEM WAS RESET AAug 28, 2005 · N218PS · Cndair CL6002B19SDR CA050830003Link · chafed(CAN) DURING AIRCRAFT 1ST 12/24 MONTH INSPECTION, DISCOVERED RT AILERON CABLE FOUND INCORRECTLY ROUTED RESULTING IN CHAFING OF AUTOPILOT SYNCRO INPUT LINK. CABLE INSPECTED NFF AND RE-ROUTED. AREA LAST ACCESSED BY BOMBARDIER SERVICE CENTER, FOR AILERON PCU CHAug 21, 2005 · Cndair CL604SDR 05FDEA02210Flap System · stuckDURING SLAT/FLAP RETRACT FLAPS STUCK AT 15 DEG SLATS OK FLAPS SYS 1 & 2 LIGHTS ILLUMINATED AS WELL AS FLAPS LIGHT ON SFDI FLAPS STUCK RAN CHECKLIST LANDED UNEVENTFULLY. FAULT CODE NOT APP TO THIS A/C, ENGINEERING HAS CONTACTED AIRBUS. CYCLED FLAPS AND SLATSAug 2, 2005 · N414FE · Airbus A310203SDR F3LA200500029Computer · malfunctionedAIR RETURN. AFTER DEPARTURE AT 8500 FT, ACFT PFD DISPLAYED ALTN LAW, AMBER XXS AND ECAM VERIFIED LANDING WT 130,400 PER POST FLIGHT REPORT. NR 2 ELAC REPLACED. OPS CHECKED GOOD PER AMM 27-93-34-401 AND 27-93-00-710-001. GROUND SCAN DETECTED NO FAULTS PER AMJul 11, 2005 · N912FR · Airbus A319111SDR 2005FA0001108Control Cable · wornCABLES WORN BEYOND LIMITS AT A CABLE RUB STRIP IN RT WING BY AUTOPILOT SERVO AT STATION RBL 102. (K)Jul 8, 2005 · N53289 · Cessna 172SSDR F3LA200500031Actuator · unserviceableTHS FAILED SECTION -A- OF TASK CARD TC 27400-1. THS LOCKED IN FULL NOSE DOWN POSITION. REPLACED THS ACTUATOR PER MM 27-44-51-400-001. PERFORMED REQUIRED SYSTEM TEST PER MM 27-41-00-730-001 AND CHECKED GOOD.Jul 4, 2005 · N928FR · Airbus A319111SDR COMA0560379Flt Controls · vibrationMODERATE VIBRATION IN CONTROLS AT SPEED GREATER THAN 260. INSPECTED FUSELAGE, VERTICAL STAB FAIRINGS AND FLIGHT CONTROLS. NO DEFECTS NOTED.Jul 4, 2005 · N716CA · Cndair CL6002B19SDR TRBA2005043Connector · damagedWHILE TAXIING, AILERON AND RUDDER TRIM INDICATORS HAVE NO ELECTRICAL POWER. AIRCRAFT RETURNED TO BLOCKS. REPOSITIONED PIN C-13 IN CONNECTOR PLUG 15 AX. (K)Jun 13, 2005 · N355AT · Aerosp ATR72212SDR VNAA0505017Unknown · unknownTHE CREW ABORTED THE TAKEOFF AFTER RECEIVING A CONFIG TRIM VOICE WARNING AT 80 KTS. AFTER CONFERRING WITH MAINTENANCE CONTROL, THE CREW PUT THE AIRCRAFT INTO PROPER TAKEOFF CONFIGURATION. THE CONFIGURATION WARNING SYSTEM OPS CHECKED GOOD. THE AIRCRAFT THEN May 31, 2005 · N251PS · Cndair CL6002B19SDR SIMA200515701Pitch Control · malfunctionedALB - FLT 4230 - TAKEOFF PITCH TRIM RECEIVED BY CREW DURING TAKEOFF. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK IAW EMB MM AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 29, 2005 · N811AE · Emb EMB135KLSDR GNB2005F00006Control Cable · wornCABLE BLENDED AT PULLEY. PROBABLE CAUSE, SOFTER NEW STYLE STAINLESS STEEL CABLE MATERIAL. SERVICE LIFE IS ONLY FRACTIONS OF OLD STYLE STEEL CABLES. (K)May 25, 2005 · N305AT · Cessna 402CSDR SIMA200510807Cartridge · out of adjustCREW NOTED IN CRUISE, THE GUST LOCK LIGHT CAME ON AND LANDED AT THE NEAREST AIRPORT WITH NO PROBLEMS. ADJUSTED GUST LOCK SPRING CARTIRIDGE MECHANISM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Apr 16, 2005 · N810AE · Emb EMB135KLSDR MASA200500263Warning Light · intermittentASH 7289 DSM-DEN. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITH GLD UNSAFE MSG. MAINTENANCE WAS CALLED AND THE PROBLEM SEEMED TO BE INTERMITTENT. SECURED THE SYSTEM IN THE OFF MODE AND FERRIED THE AIRCRAFT TO TUS FOR REPAIR.Mar 31, 2005 · N503MJ · Cndair CL6002C10SDR A6WA200540115Unknown · malfunctionedDURING APPROACH, WHEN SELECTING FLAPS FROM 30 TO 45 AIRCRAFT STARTED ROLLING LT, REQUIRED HALF AVAILABLE AILERON TRIM AND RT CONTROL WHEEL INPUT TO KEEP WINGS LEVEL. FLAP TRAVEL APPEARS UNEVEN. PERFORMED FLAP RIG CHECK, OPS CHECK GOOD. SPOILER SYSTEMS OPS CMar 20, 2005 · N426AW · Cndair CL6002B19SDR DJFA2005084Flt Controls · malfunctionedDURING STALL TEST AT 120 KIAS, EXPERIENCED AN UNCOMMANDED, UNCONTROLLED RT BANK. NO STALL HORN, STICK SHAKER OR PUSHER IND. APPROX 90 DEG BANK, A/C ROLLED FURTHER RT, & APPROX 140 DEG BANK, A/C ROLLED TO RT AGAIN. CONTINUED ROLL AFTER PASSING INVERT. RECOVEMar 3, 2005 · N725TA · Raythn HAWKER800XPSDR GTIA050037Motor · inoperativePRIMARY LONG TRIM INOPERATIVE, TAIL SWAP WITH AIRCRAFT 829. REMOVED AND REPLACED LONG TRIM MOTOR AND REPAIRED MOTOR GROUNDS, SYSTEM OPS CHECK GOOD. (K)Feb 23, 2005 · N808NK · Doug DC983SDR AU510002215Actuator · leakingACTUATOR LOCATED IN LT WING LEAKING. LIMITED INFORMATION PROVIDED.Feb 12, 2005 · Boeing 737200SDR AMTA200500061Panel · delaminatedNR 2 R SPOILER HAS LARGE DELAMINATION. REMOVED AND REPLACED NR 2R SPOILER PANEL IAW MM. OK FOR SERVICE. (K)Jan 17, 2005 · N164AT · Lkheed 10113853SDR QXEA200500109Flt Controls · sluggishDURING THE INITIAL ROTATION, THE FIRST OFFICER NOTED GREATER THAN NORMAL BACK PRESSURE AND SLOWER THAN NORMAL ROTATION TIME AFTER ANTI ICING WITH TYPE III FLUID IN PASCO. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROLS INCLUDING THE ELEVATOR SYSTEM, ELEVATJan 17, 2005 · N353PH · Dhav DHC8202SDR 2005FA0000026Control Panel · wornAIRCRAFT WAS SUBSTANTIALLY DAMAGED DURING A LANDING ACCIDENT. PILOT WAS UNABLE TO FLARE AIRPLANE. DURING A POST ACCIDENT INSPECTION BY FAA INSPECTORS, IT WAS DISCOVERED THAT THE AIRPLANE'S CONTROL TEE PULLEYS FOR THE AILERON SYSTEM WOULD GET (HUNG UP) ON THE Jan 13, 2005 · N8803B · Cessna 172SDR VNAA0501002Actuator · failedSHORTLY AFTER TAKEOFF FROM CLT THE AMBER PITCH FEEL CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO CLT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AFTER TROUBLESHOOTING REMOVED & REPLACED THE NR 2 PITCH FEEL ACTUATOR IAW CRJ 700 AMM 27-31-23-400-801Jan 6, 2005 · N703PS · Cndair CL6002C10SDR MASA200400644Warning Light · illuminatedASH 7230 DEN - ABORTED TAKEOFF FOR TAKEOFF CONFIG MESSAGE AT 80 KNOTS. MAINTENANCE CURRENTLY TROUBLESHOOTING. 11/19/2004 MAINTENANCE PERFORMED CONFIGURATION OPS CHECK AND ALL CHECKS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE.Nov 19, 2004 · N507MJ · Cndair CL6002C10SDR 2005FA0001120Roll Servo · defectiveAIRCRAFT WENT INTO UNCOMMANDED TURN WITH AUTOPILOT ENGAGED. REMOVED DEFECTIVE ROLL SERVO KS271C WITH 3.4 HOURS ON IT SINCE OVERHAUL BY MFG. (K)Nov 11, 2004 · N658RA · Beech 58SDR 2005FA0001119Roll Servo · bindingFOUND FLIGHT CONTROLS BINDING WHEN YOKE TURNED. BINDING WAS CAUSED BY PARTIALLY SEIZED OUTPUT BEARING IN AUTOPILOT ROLL SERVO. FOUND BEARING AND MOTOR DEFECTIVE. INSTALLED EXCHANGE SERVO. (K)Nov 1, 2004 · N658RA · Beech 58SDR F3LA200400112Computer · inoperativeAIR TURNBACK. FLIGHT CREW REPORTED FLIGHT CONTROL RIGHT AILERON FAULT ON ECAM. PERFORMED OVERWEIGHT LANDING AND LANDED IN DEN WITHOUT INCIDENT. CABIN CREW REPORTED HYDRAULIC FLUID COMING FROM LT WING AND AN ELECTRICAL SMOKE ODOR WHEN LANDING GEAR WAS EXTENDOct 8, 2004 · N804FR · Airbus A318111SDR A6WA200440140Unknown · malfunctionedAFTER GEAR SELECTED DOWN, AIRCRAFT STARTED UNCONTROLLED ROLL LT (AUTO-PILOT OFF), STOPPED AFTER 5 SECONDS. THEN HAPPENED SECOND AND THIRD TIME 3 MILE END-TO-END TRAILING B737. ALL ROLLS TO LT. M/C (FIRST TIME FLAPS AT 0. SECOND FLAPS AT 20, THIRD FLAPS. PESep 30, 2004 · N434AW · Cndair CL6002B19SDR AWXA200400886Motor · bindingON CLIMB-OUT OF PHX EN ROUTE FOR SJC AT APPROXIMATELY 3000 FT, FLIGHT CONTROLS SHOOK VIOLENTLY FROM SIDE TO SIDE AS IF IN SEVERE TURBULENCE. NOTICED FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, ADJUSTED AILERON TRIM AND ONCE AILERON INPUT WAS ACHIAug 13, 2004 · N182AW · Boeing 737277SDR F3LA200400078Module · malfunctionedAIR TURN BACK. FLIGHT CREW REPORTED ELAC2 PITCH FAULT AFTER TAKEOFF. SWAPPED ELAC2 ELECTRONIC MODULE OF THE PITCH FROM ACTUATOR WITH ELAC1/SEC1 ELECTRONIC MODULE IAW MM 27-44-57-000-002 AND MM 27-44-57-400-002. PERFORMED SYSTEM TEST OF THE THS ACTUATOR ELECAug 12, 2004 · N921FR · Airbus A319111SDR F3LA200400076Switch · malfunctionedBLOCK TURNBACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. RESET ELAC 2 SWITCHES AND FAULT CLEARED.Aug 12, 2004 · N921FR · Airbus A319111SDR SIMA20040501Control Unit · inoperativeORD - FLT 4057 - DURING CLIMB, CREW REPORTED A PITCH TRIM 1 INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT, IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Jul 20, 2004 · N639AE · Emb EMB145LRSDR 04FDEA02026Control Cable · crossedAFT PIT BEHIND STATION 1967, 36 INCHES, LEFT BUTT LINE CABLES CROSSED BELOW MAIN CABIN FLOOR. OPENED CEILING PANELS AND REMOVED LEFT HAND VERTICAL ACCESS PANELS. REMOVED AND REPLACED PULLEYS AND 2 EACH CABLES, RIGGED AND OPS CHECKED GOOD, ROUTE CHECKED AND IJul 7, 2004 · N386FE · Doug MD1010FSDR F3LA200400068Transducer · inoperativeFLIGHT CREW REPORTED FLIGHT CONTROL ELAC 2 FAULT AFTER NR 2 ENGINE START. PERFORMED AFS TEST PER TASK 22-66-00-810-851. NO FAULTS FOUND. SWAPPED ELAC NR 1 AND NR 2. PERFORMED ELECTRONIC FLIGHT CONTROL SYSTEM TEST. LT AND RT ELEVATOR AND LT AND RT AILERON Jun 26, 2004 · N921FR · Airbus A319111SDR CA040513001Unknown · unknown(CAN) DURING A FULL THRUST TAKEOFF AT APPROX 100 KNTS IAS, ACFT SNAPPED TO THE LT REQUIRED ABRUPT RT RUDDER. AGAIN AT APPROX 130 KNTS IAS, ACFT VEERED LT THOUGH LESS ABRUPT. ALL OTHER INDICATIONS NORMAL AND FLIGHT CONTINUED ON TO DESTINATION. AC TO BE REMOMay 13, 2004 · Airbus A320211SDR 2004F00265Control Cable · out of rigCONTROL YOKES SHOW 25 DEGREE RIGHT BANK DURING STRAIGHT AND LEVEL. RIGHT AILERON IS UP ND LEFT ELEVATOR IS UP. PITCH CONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. VERIFIED THAT AIRCRAFT FLIGHT CONTROL SURFACES NEMay 13, 2004 · N5115 · Cessna 750SDR SWIA200413279Control Panel · inoperativeLT WING DOWN AILERON TRIM IS INOPERATIVE. REMOVED AND REPLACED THE AILERON/RUDDER TRIM PANEL ASSEMBLY. BOTH SYSTEMS CHECK GOOD.May 5, 2004 · N452SW · Cndair CL6002B19SDR 2004FA0000235Structure · chafedSTABILATOR RUBS AGAINST FUSELAGE SCREW. .5 INCH GAP ON LT SIDE, .2500 INCH GAP ON RT SIDE. (GL13200405339)Feb 6, 2004 · N622AM · Amtr ALARUSCH2TSDR 04FDEA00224Fairlead · crackedCOMPLY WITH EA 8-5310-73870. FUSELAGE-REPAIR OF CONTROL CABLE FAIRLEAD AT STA 575 AND LBL 41.5. CLOSING ACTION ON 01/25/04.ON N/R S00011.COMPLIED WITH EA 8-5312-73870.Jan 26, 2004 · N373FE · Doug DC1010SDR EOO2004F00000Bracket · damagedFOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SORT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (KJan 6, 2004 · N511SB · Hughes 369DSDR SPAA0000035Bracket · damagedFOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SORT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (KJan 6, 2004 · N511SB · Hughes 369DSDR MASA200300519Unknown · unknownASH 2609 - PITCH OSCILLATIONS IN YOKE AT 200KIAS DURING DESCENT WITH AP ENGAGED. FLAPS UP, GEARUP. PERFORMED GVI OF FLIGHT CONTROL SYSTEMS AND CHECKED CABLE TENSION. ALL CHECKED GOOD. MX COULD NOT DUPLICATE. NO PARTS USED.Dec 28, 2003 · N860MJ · Emb EMB145LRSDR MASA200300503Pcu · out of toleranceASH 6320 PHX-GJT, ABORTED T/O FOR SPOILER CONFIG WARNING MSG. MX REPLACED THE PCU. OP CHECKS GOOD.Dec 19, 2003 · N77278 · Cndair CL6002B19SDR CA031215002Control Cable · frayed(CAN) CABLE INSPECTION REVILED WEAR & FRAYING AT THE POINT WERE THE CABLE CHANGES DIRECTION ENTERING THE FUSELAGE.Dec 10, 2003 · Cessna A185ESDR CA040827007Motor · malfunctioned(CAN) THE AIRCRAFT HAD BEEN THROUGH A MAJOR INSPECTION AT CONTRACTOR 4 MONTHS PREVIOUS. THE VALVE HAD BEEN REMOVED FOR ACCESS TO OTHER AREAS. THE PILOT REPORTED CIRCUIT BREAKER POPPED DURING TAXI. PILOT RETURNED TO HANGAR. INVESTIGATION FOUND RODS CONNECTED TODec 4, 2003 · Amd FALCON20SDR CA040105007Control Cable · frayed(CAN) CABLE INSPECTION REVEALED WEAR AT THE POINT WHERE THE CABLE CHANGES DIRECTION ENTERING THE FUSELAGE.Dec 3, 2003 · Cessna A185ESDR BAQA089604Lever · damagedROLL CRANK LEVER DAMAGED. REPLACED WITH SERVICEABLE UNIT 10/15/03.Oct 6, 2003 · N915ME · Aerosp AS365N2SDR XNOA01153Control Cable · lack of lubeFLIGHT CONTROLS LOCKED TO LEFT ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KTS. INSPECTED AIL CABLES AND TENSION REG. LUBED TENSION REG. OPS CHECK NORMAL IAW A300 MM 27-11-00. INSP. AIL HYD ACT. SYS IAW A300 MM 27-14-00. NO DEFECTS NOTED.Sep 6, 2003 · N473AS · Airbus A300B4203SDR WRLA200318Sensor · malfunctionedAFTER TAKEOFF APPROX 800 FT LEVEL 3, NR 2 ENGINE ANTI-ICE DUCT ILLUMINATED TRI TONE SOUND. SHUT DOWN ENGINE NR 2 AS PER VOLUME 1, DUMPED FUEL AS PER VOLUME 1 RETURNED TO FIELD, DEPARTURE FIELD JTY. REPLACED NR 2 ANTI-ICE VALVE. SWAPPED NR 2 AND NR 3 PRESSURAug 31, 2003 · N277WA · Doug MD11
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