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 UALA2013052303593Boot · tornCOPILOTS SIDE STICK BOOT TORN AFT INBD CORNER. SMALL TEAR INBD AFT SIDE OF JOY STICK. REPLACED COPILOTS JOYSTICK BOOT.May 22, 2013 · N404UA · Airbus A320232SDR AALA20130521002Unknown · malfunctioned(REPEAT ITEM), CREW REPORTED FLAPS WERE SELECTED TO 1 AND THERE WAS NO MOVEMENT OF FLAPS OR SLATS. THE FLAP HANDLE WAS RECYCLED 3 TIMES FROM UP TO 1 DEGREE AND BACK WITH NO MOVEMENT OF FLAPS OR SLATS. FLAP/SLAT INDICATOR NEEDLES WERE SPLIT THEN EVEN AFTER LAMay 18, 2013 · N918NN · Boeing 737823SDR C77A201305080001Battery · overheatedDURING ROUTINE MX, A BURNING ODOR WAS FOUND NEAR THE NOSE AREA OF THE ACFT. FOUND FLY-BY-WIRE BATTERY WITH OVERHEAT LIGHT ON, A BURNING ODOR AND HOT TO TOUCH. REPLACED FLY-BY-WIRE BATTERY IAW AMM, OPS CHECKED GOOD.May 8, 2013 · N639CZ · Emb ERJ170200LRSDR UALA2013050603146Fuse · leakingRIGHT INBOARD FLAP TRACK CANOE SHOWS FRESH HYD FLUID LEAKAGE. FOUND RT OUTBOARD FLAPERON HYD FUSE LEAKING, REPLACED FUSE PER MM. TESTED AND OPERATED NORMALLY AND NO LEAKS.May 3, 2013 · N216UA · Boeing 777222SDR CA130516009Rod End · loose(CAN) ROD END BEARING NOTED TO BE MOVING DUE TO LOOSE TAPER PINS IN FWD END OF RUDDER DRIVE ROD. ROD REPAIRED AND RE-INSTALLED.May 1, 2013 · Bnorm BN2A8SDR UALA2013050103044Transducer · failedFLIGHT CONTROL STATUS MESSAGE DISPLAYED ON THE LOWER ECAM SCREEN. INSTALLED REPAIRED FIRST OFFICER'S SIDE STICK ASSY & PERFORMED OP TEST TASK IAW 27-92-41-710-001-A. PERFORMED SAT AFS AND LAND TEST PER MM 22-97-00. A-C RETAINS CAT IIIB STATUS PER GMM 5-35-40Apr 30, 2013 · N456UA · Airbus A320232SDR C77A2013043001Battery · overheatedFLY BY WIRE BACK UP BATTERY OVER TEMP/FUMES DURING MX UNRELATED TO FLY BY WIRE BACK UP BATTERY.Apr 27, 2013 · N626CZ · Emb ERJ170200LRSDR UALA2013042602934Computer · malfunctionedAILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. REMOVED AND REPLACED NR 2 ELAC COMPUTER. PERFORMED OPS TEST OF ELACS IAW AMM. PERFORMED AFS LAND TEST. ALL TESTS PASSED, NO FAULTS NOTED.Apr 25, 2013 · N804UA · Airbus A319131SDR UALA2013042302832Computer · faultyNR 1 ELAC FAULT DISPLAYED ON UPPER ECAM SCREEN. UNABLE TO RESET. REPLACED NR 1 ELAC. FLIGHT CONTROLS GROUND CHECKED OK. AFS AND LAND TEST PASSED.Apr 22, 2013 · N806UA · Airbus A319131SDR C77A4201320074001Battery · overheatedDURING ROUTINE MX, AN ODOR WAS FOUND IN FWD CABIN FLIGHT DECK AREA. FOUND FLY BY WIRE BACK UP BATTERY SMOKING AND OVERHEAT LED LIGHT ON. REPLACED THE BATTERY IAW AMM. OPS CHECK GOOD.Apr 20, 2013 · N606CZ · Emb ERJ170200LRSDR C77A2013F00095Battery · overheatedDURING ROUTINE MX, AN ODOR WAS FOUND IN FWD CABIN FLT DECK AREA. FOUND FLY-BY-WIRE BACK UP BATTERY SMOKING AND OVERHEAT LED LIGHT ON. REPLACED THE BATTERY IAW AMM, OPS CHECK GOOD.Apr 20, 2013 · N606CZ · Emb ERJ170200LRSDR UALA2013042202750Computer · faultedCREW REPORTED NR 1 ELAC FAULT. NR 1 ELAC BOX FAULTED. SWAPPED WITH NR 2 ELAC, FAULT FOLLOWS BOX. REPLACED NR 1 ELAC PER MM. FAULTS CLEARED.Apr 18, 2013 · N464UA · Airbus A320232SDR C77A20130416001Battery · overheatedDURING A ROUTINE MX CHECK, AN ODOR WAS NOTICED IN THE FWD CABIN, FLIGHT DECK, AND OUTSIDE OF THE ACFT. UPON FURTHER INSPECTION THE FLY BY WIRE BACK-UP BATTERY HAD THE "SMOKING AND OVERHEAT" LED LIGHT ON. THE BATTERY WAS REPLACED IAW AMM, OPS CHECKED GOOD, NOApr 16, 2013 · N626CZ · Emb ERJ170200LRSDR C77A2013F00096Battery · overheatedDURING A ROUTINE MX CHECK, A ODOR WAS FOUND IN FWD CABIN, FLIGHT DECK, AND OUTSIDE OF ACFT. ON FURTHER INSPECTION FOUND FLY BY WIRE BACK UP BATTERY SMOKING AND OVERHEAT LED LIGHT ON. BATTERY WAS REPLACED IAW AMM, OPS CHECK GOOD, NO OTHER DEFECTS FOUND.Apr 16, 2013 · N626CZ · Emb ERJ170200LRSDR C77A2013F00097Battery · overheatedDURING ROUTINE MX, AN ODOR IN THE FORWARD CABIN, FLIGHT DECK, AND OUTSIDE THE ACFT. UPON FURTHER INSPECTION FOUND THE FLY BY WIRE BACK-UP BATTERY SMOKING AND THE OVER HEAT LED LIGHT ON. THE BATTERY WAS REPLACED IAW AMM, OPS CHECK GOOD AND NOW OK FOR SERVICE. Apr 16, 2013 · N626CZ · Emb ERJ170200LRSDR UALA2013041502583Computer · failedFLT CONTROL CHECK, RT AILERON OUT OF LIMITS. FOUND 33CE2 RIGHT GREEN AILERON SERVO TRANSDUCER INPUT TO ELAC CAUSES INDEX NOT TO INDICATE CORRECTLY. DOES NOT SHOW FULL DEFLECTION FOR RIGHT AILERON DOWN. REPLACED NR 1 ELAC PER AMM 27-93-34-401. FAULT CLEAREApr 13, 2013 · N832UA · Airbus A319131SDR C77A20131104001Battery · overheatedDURING ROUTINE MX, DISCOVERED BURNING SMELL COMING FROM FRONT OF ACFT. DISCOVERED FLY BY WIRE BACK UP BATTERY SMOKING AND OVERHEAT LIGHT ON. REPLACED BATTERY IAW AMM. OPS CHECKED GOOD.Apr 11, 2013 · N639CZ · Emb ERJ170200LRSDR C77A2013F00101Battery · overheatedDURING A MX STOP. AN ODOR WAS FOUND IN THE ACFT. UPON FURTHER INSPECTION ODOR WAS FOUND TO BE COMING FROM THE FLY BY WIRE BATTERY THAT WAS SMOLDERING/SMOKING. THE BATTERY'S OVER HEAT LED WAS ON. THE BATTERY WAS REPLACED IAW THE AMM, OPS AND FUNCTIONAL CHECApr 11, 2013 · N639CZ · Emb ERJ170200LRSDR SIMA20130411003Unknown · malfunctionedON FLIGHT 4578 THE CREW REPORTED THAT AFTER TAKEOFF THEY NOTICED HEAVY AILERON CONTROL AND AT TIMES YOKE FELT LIKE IT WAS LOCKED. IT REQUIRED MORE FORCE THAN NORMAL TO DISPLACE AT TIMES IT BANKED EASY LEFT BUT HARD RIGHT AND THEN IT WOULD REVERSE AND BANK HARApr 9, 2013 · N502BG · Amd FALCON2000SDR UALA2013041002423Computer · faultyF-CTL ELAC 1 PITCH FAULT PROG TEXT: - ITEM ROLLED FORWARD. (COMPLIED WITH MEL) RPR- :T/S FAULT TO ELAC 1. REMOVED AND REPLACED ELAC 1, OPS CHECK GOOD. CAT THREE PERFORMED, SEE SEQ 2692006.Apr 9, 2013 · N837UA · Airbus A319131SDR UALA2013040402250Computer · failedSPOILER ELEVATOR COMPUTER (SEC) 2 INOP - F-CTL. CREW COMMENTS: SEC 2 FAIL. RESET OK FOR 10 MIN. FAIL AGAIN RESET OK FOR 5 MIN. FAIL AND LEFT OFF. REPLACED SEC 2 COMPUTER PER AMM, OPS TEST OKAY.Apr 2, 2013 · N443UA · Airbus A320232SDR CA130401023Gust Lock · cracked(CAN) MULTIPLE CRACKS FOUND ON GUST LOCK HANDLE. GUST LOCK LEVER, REPLACED.Mar 28, 2013 · Dhav DHC8311SDR UALA2013032501830Computer · faultedELAC 1 INDICATION INOPERATIVE ON FLIGHT CONTROL SYSTEM ECAM PAGE IN FLIGHT. REPLACED ELAC 1, NO HELP. ACCOMPLISHED OP CHECK OF ELAC AS PER AMM 27-93-00-710-001A. ALL OK, ALSO CAT III CAPABILITY CHECK OK. PER MM 22-97-00,501. ACFT FULL AUTOLAND.Mar 23, 2013 · N426UA · Airbus A320232SDR UALA2013031901690Computer · faultedELAC 2 FAULT ON GROUND WHEN PILOTS BOARDED AIRCRAFT. REPLACED NR 2 ELAC PER MM, OPS TEST PER MM IS GOOD.Mar 19, 2013 · N452UA · Airbus A320232SDR UALA2013031901694Unknown · unknownAIRCRAFT HAS POOR TRIM QUALITIES. 0 RUDDER TRIM WINGS LEVEL EVEN POWER LEVEL FUEL REQ OVER 1 RIGHT AILERON TRIM. THE ELEVATOR POSITION SHOWS RT ELEVATOR LOWER THAN LEFT. POOR TRIM WITH AND WITHOUT AUTO-PILOT, PER CREW. CHECKED ELEVATOR POSITION FOR BEING SMar 18, 2013 · N551UA · Boeing 757222SDR UALA2013031801650Transducer · faultyELAC 2 FAULTS IN CRUISE, RESET. CFDS SHOWS "27-44-51, FLT PHASE 6, THS ACTR POS ERROR 9CE OF ELAC 2". ELAC 2 ALREADY REPLACED. REPLACED "MONITOR POSITION TRANSDUCER" OF THE THS ACTUATOR.Mar 15, 2013 · N452UA · Airbus A320232SDR UALA2013031501586Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. AT FL 360. BUMP IN FLIGHT PATH WITH FAULT. REPLACED ELAC 1, OPS CHECK OK PER MM 27-93-00-710-001A AND ACCOMPLISHED CAT III CHECK, ALL OK.Mar 14, 2013 · N472UA · Airbus A320232SDR UALA2013031301489Computer · faultyECAM FLIGHT CONTROL-ELAC 2 PITCH FAULT, RESET NORMAL. REPLACED ELAC PER AMM, OPS CHECKED OKAY.Mar 12, 2013 · N452UA · Airbus A320232SDR UALA2013031101450Actuator · faultyNEED TO REPLACE LEFT SIDE UPPER LCCA ACTUATOR. REPLACED LEFT HYD SYS LCCA AND ADJUSTED, OPS CHECKED GOOD.Mar 10, 2013 · N657UA · Boeing 767322SDR SWIA201332963Unknown · malfunctionedUNCOMMANDED ROLL TO THE RIGHT WHEN SELECTING FLAPS 45 DEGREES. (FLT 4716) VISUALLY INSPECTED BOTH LEFT AND RIGHT WINGS, FLAPS AND SPOILERS. CLEANED GREASE, SAND AND LOOSE PAINT FROM SPOILERS AND FLAPS IAW AMM. NO DEFECTS NOTED ON WING BODY AT THIS TIME. OMar 9, 2013 · N659BR · Cndair CL6002B19SDR UALA2013031101404Actuator · faultyFLT CONTROLS BIND A LITTLE BIT AFTER A LEFT TURN WHEN RETURNING THE CONTROL TO CENTER. REPLACED LY HYD SYS LCCA (FOUND INPUT OUTPUT ROD OUT OF ADJUSTMENT).Mar 9, 2013 · N657UA · Boeing 767322SDR UALA2013030801390Computer · faultedCREW REPORTED ELAC 2 FAULT MESSAGES. REPLACED NR 2 ELAC IAW AMM 27-93-00-710-001A, TESTED OK.Mar 7, 2013 · N465UA · Airbus A320232SDR UALA2013030501313Unknown · bindingCREW REPORTS DURING FLIGHT CONTROL CHECK TO THE LEFT, CONTROL WHEELS BINDS AND IS SLOW TO RETURN. WORKS NORMALLY TO RIGHT TURN. FLAPS DOWN OR UP. HYD PRESS AND INDICATIONS NORMAL. OPERATED ALL FLIGHT CONTROLS SEVERAL TIMES AND OPERATION FOUND SMOOTH AND NOMar 4, 2013 · N657UA · Boeing 767322SDR UALA2013022101042Warning System · activatedSTATUS MESSAGE FLIGHT CONTROL SYS WITH FLIGHT CONTROL MODE CAUTION MESSAGE. MAINT MESSAGE 27-15101 LATCHED IN MAT. CORRELATED STATUS MESSAGES ARE (SAARU.AUTO SPEED BRAKE, THRUST ASYM COMP AND NO AUTOLAND). REPLACED CENTER PSA PER MM, NO HELP. RE-INSTALLED OFeb 21, 2013 · N785UA · Boeing 777222SDR UALA2013021901007Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL REPLACED ELAC 1, OPS CHECK GOOD.Feb 19, 2013 · N840UA · Airbus A319131SDR 2013F00064Flt Controls · malfunctionedENROUTE, IN LEVEL FLIGHT AT FL400. SAW A WHITE CAS MESSAGE STATING THAT THE AUTOPILOT HAD FAILED. ENSURED SYS HAD SWITCHED TO THE OTHER AUTOPILOT. WHITE CAS MESSAGE WENT AWAY. OVER THE NEXT SEVERAL MINUTES, WHITE CAS MESSAGE REPEATED ITSELF AND THEN RECEFeb 18, 2013 · N510CT · Amd FALCON2000EXSDR UALA2013021400876Computer · malfunctionedELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL REPLACED ELAC 1 PER AMM. OPERATIONAL TEST CHECKED NORMAL. ACCOMPLISHED LAND CAT 3 CAPABILITY TEST PER AMM, TEST WAS OK.Feb 13, 2013 · N456UA · Airbus A320232SDR UALA2013020600722Computer · unknownAIRFRAME VIBRATION, FLIGHT DIVERTED. REPLACED SEC 2 PER MM, SYSTEM RETURNED TO NORMAL. DAMPING MEASUREMENT TESTED, OPS NORMAL. FOUND LOOSE FASTENERS AT REAR OF BELLY FAIRING. TIGHTENED FASTENERS. NO OTHER FINDINGS.Feb 5, 2013 · N446UA · Airbus A320232SDR UALA2013020400678Computer · failedELAC 1 ELEVATOR PITCH FAULT DISPLAYED. ATTEMPTED RESET OF ELAC 1 - NO JOY. REPLACED ELAC 1, SYSTEM CHECKS NORMAL AT THE GATE.Feb 1, 2013 · N853UA · Airbus A319131SDR UALA2013012800490Unknown · vibrationCREW REPORTS VIBRATION. VIBRATION STARTED WHEN GEAR WAS PUT DOWN, FULL FLAPS. VIBRATION REMAINED UNTIL TOUCHDOWN. ACCOMPLISHED MT 27-005, NO MIGRATION NOTED VERIFIED UPPER AND LOWER KINK AND CUSHION SEAL ARE OK. NO DEFECT NOTED ON GENERAL VISUAL FLAP INSJan 26, 2013 · N479UA · Airbus A320232SDR UALA2013012800494Boot · unsecureCAPTAIN`S SIDE STICK BOOT IS MISSING SECURING STRING. SECURED BOOT WITH REQUIRED TIE STRING AND ADHESIVE.Jan 25, 2013 · N836UA · Airbus A319131SDR UALA2013012100376Computer · faultedUNCOMMANDED PITCH UP WITH AUTO PILOT ON AND AIRSPEED DROP 30 KTS BEFORE DIS-ENGAGING. ON APPROACH AUTO PILOT DEGRADED TO CAT 2. ACP WITH LOG 1. REPLACED ELAC 2 PER AMM, OPS CHECK. OPERATIONAL L AND CAT III BY 106663 TEST OK AC MAINTAIN CAT III STATUS.Jan 21, 2013 · N821UA · Airbus A319131SDR DXTA2013011805249Pulley · damagedDURING CLIMB OUT, ACFT SUDDENLY PITCHED NOSE DOWN. ON DETECTING THE PITCH CHANGE, AUTOPILOT WAS DISENGAGED. CONTROLS WERE DIFFICULT TO MOVE ALONG VERTICAL AXIS AND EACH CONTROL INPUT REQUIRED EXCESSIVE FORCE TO PITCH THE ACFT IN A CLIMB OR DESCENT. CONTROL Jan 13, 2013 · N662QS · Cessna 560XLSDR UALA2013011400247Computer · warning lightFCTL SEC 1 FAULT ECAM. RESET PER FLT MANUAL, RESTORED. REPLACED SEC NR 1, OPS CHECKED GOOD.Jan 11, 2013 · N413UA · Airbus A320232SDR UALA2013011100194Computer · faultedFLT CONTROL ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM. PRECEEDED BY SLIGHT PITCH NOSE DOWN. PERFORMED WIRING CHECK FROM ELAC 2 TO TRANSDUCER, ALL WIRING CHECKED GOOD. STATUS MESSAGE CLEARED REF 27-93-00-810-877-A. REPLACE RACK CONNECTOR 2CE2A, PCN (565-1Jan 9, 2013 · N440UA · Airbus A320232SDR RU3A20130108001Unknown · malfunctionedON LANDING IN FLARE, POWER IN IDLE, APPROX 3-5 FEET ABOVE RUNWAY, AIRCRAFT VIOLENTLY YAWED LEFT APPROX 30-40 DEGREES. POWER WAS ADDED AND RUDDER USED TO ALIGN AIRCRAFT WITH RUNWAY. AIRCRAFT TOUCHED DOWN HARD AND BOUNCED ONCE. UPON INSPECTION AFTER LANDING, Jan 3, 2013 · N83 · Beech 300BEECHSDR UALA2012122707425Computer · faultyACFT HAS CONSTANT PITCH *UP* WHILE HAND FLYING. CREW HAD TO APPLY CONSTANT FORWARD PRESSURE ON STICK TO KEEP FROM CLIMBING. ACFT FLIES OK IN WITH AUTOPILOT ENGAGED. PREV HISTORY SHOWS ELAC 2 COM OR WIRING ACCLRM4 12CE4. REF TSM 27-93-00-810-818A. CHECKED Dec 26, 2012 · N455UA · Airbus A320232SDR UALA2012122107345Module · faultyRIGHT FLT CONTROL CUTOFF WONT STAY IN. REPLACED RIGHT FLIGHT CONTROL SWITCH MODULE ON P-61 PNL. SWITCH OP'S CHECK GOOD.Dec 19, 2012 · N551UA · Boeing 757222SDR UALA2012121707263Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. CREW CYCLED B11 FAULT CLEARED. REPLACED ELAC 1 REF AMM. FAULT CLEARED. OPS TEST GOOD NO FAULTS.Dec 15, 2012 · N826UA · Airbus A319131SDR CA121231003Relay · defective(CAN) PRIMARY PITCH TRIM FAILED TO TRIM NOSE UP, RELAY 72C FOUND DEFECTIVE AND REPLACED.Dec 14, 2012 · Gulstm G100
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