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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA2012121700014Unknown · malfunctionedDURING TAKEOFF ROTATION OUT OF FLL, CREW REPORTED THE LEFT WING DROPS. TAKES CONSIDERABLE RIGHT AILERON UNTIL AIRCRAFT ACCELERATES. FLIGHT CONTINUED TO DESTINATION AT CLT. MAINTENANCE INSPECTED FLAPS AND TOGGLES, CHECKED FOR FLOATING SPOILERS, CHECKED AILEROSDR UALA2012121207198Unknown · vibrationIN CLIMB 310KTS STRONG VERTICAL VIBRATION FELT IN COCKPIT AND AFT GALLEY, WENT AWAY AT 300. ACCOMPLISHED ELEVATOR SERVO PLAY CHECK REF MM 27-34-00-200-001. EDGE PLAY WITHIN LIMITS LEFT BLUE 5.25MM LEFT GREEN 5.12MM RIGHT BLUE 4.20MM RIGHT YELLOW 5.60MM INSP SDR AALA20121211009Pressure Switch · inoperativeIAD - INFLIGHT MIA-DCA. CREW REPORTED FLIGHT CONTROL LOW PRESSURE EICAS MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLIGHT CONTROL MODULE PRESSURE SWITCH. SYSTEM GROUND CHECK NORMAL OPERSDR UALA2012121007156Computer · faultyOSCILLATING STAB TRIM. ELAC IN NR 2 POSITION IS MR27935 DASH 350 AND WAS REMOVED PREVIOUSLY FROM THIS ACFT FOR SAME ISSUE. REPLACE ELAC NR 2 PCN 482-9572 IAW AMM 27-93-34. REPLACED ELAC NR 2 GROUND FUNCTIONAL TEST GOOD. CAT III TEST OK IAW AMM 22-97-00 MR27SDR UALA2012121007144Unknown · malfunctionedEFCS OP TEST STBY PWR SP, ACCOMPLISH OPERATIONAL CHECK OF THE LOGICS ACTIVATING, ELAC 1, ELAC 2 AND SEC 1 STANDBY POWER SUPPLY, TO CONFIRM THE ABILITY OF SEC 1 AND SEC 2 TO ACHIEVE PITCH CONTROL, TO CONFIRM THE ABILITY OF SIDESTICK PRIORITY FUNCTION, PER MM SDR UALA2012121207186Computer · malfunctionedBOTH AUTOPILOTS OSCILLATE REPETITIVELY IN PITCH AXIS. TRIM WHEEL MOVING CONSTANTLY FWD-AFT. RE AUTOPILOT WRITEUP. DISCONNECTED A-THR-NO HELP. ALTITUDE CHANGES +-- 10 FT.10 SECOND. REPLACE NR 2 ELAC REF AMM. REMOVED AND REPLACED NR 2 ELAC PER MM, OPS CHECSDR GTIA2012120719Warning Light · false activationELAC 1 PITCH FAULT. PERFORMED RT BLUE ELEVATOR-SERVO CONTROL SERVO VALVE OPS TEST OF SIDE STICK ASSY. GROUND SCEN EFCS 1+2 NO FAULTS DETECTED. SYS CHECKS AND FUNCTION NORMAL.SDR UALA2012120707098Computer · faultySIDESTICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. - F-CTL WORK PER TSM 27-93-00-810-919-A LOSS OF SIDE STICK PRIORITY FOR ONE ELAC PER TOMC...REPLACED ELAC- 1...ELAC TEST OK AND FLIGHT CONTROLS EXERCISED WITH NO MESSAGES. AFS AND LAND TEST OKAY. PROBLEM RESDR UALA2012120607061Computer · faultySIDESTICK PRIORITY MESSAGES. REPLACED NR 2 ELAC COMPUTER REF AIRBUS. PERFORMED OPERATIONAL TEST OF ELAC COMPUTER. NO FAULTS FOUND.SDR YENA20121204656Control Panel · failedFLT 589 HPN-FLL, CREW DECLARED EMERGENCY AND DIVERTED TO MCO DUE TO MULTI EICAS MESSAGES APPEARED IN CRUISE. WINDSHEAR FAIL, GND PROX FAIL, FLAP FAIL, AT FAIL, SHAKER ANTICIPATOR, AOA LIMIT FAIL, AP FAIL, SPOILER FAULT, AUTO CONTROL TRIM FAIL. CLEARED FLAP ASDR SWIA201232170Unknown · malfunctionedRETURN TO FIELD DUE TO EXCESSIVE AND UNUSUAL CONTROL FORCES AND INPUTS TO MAINTAIN LEVEL FLIGHT. RUDDER & AILERON INPUT MUCH GREATER THAN NORMAL. (FLT 1352) COMPLIED WITH INSPECTION OF LEFT AND RIGHT AILERON BELLCRANKS, PRIMARY AILERON SERVO, PRIMARY RUDDERSDR UALA2012110706407Flex Line · leakingLOWER GUST SUPPRESSION TRANSDUCER REQUIRES LEAK CHECK DUE TO REPLACEMENT. FOUND RIGHT LOWER GUST SUP STATIC PORT LEAKING. REMOVED VERT STAB ACCES PANEL 322DL. FOUND LOOSE FLEX LINE ON TRANSDUCER. TIGHTENED SAME. LEAK TEST PASSED. CREATED CARD FOR PANEL RSDR UALA2012110706409Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. ALSO HAD SMALL-SLIGHT UNCOMMANDED ROLL. SAMC TEXT: WORK WITH TSM 27-10-00-810-842A. REMOVED AND REPLACED ELAC 1. REF TO AMM 27-93-34. OPS CHECK GOOD PER AMM 27-96-00-740-001. LAND VERIFY TEST PASSED PER TASK 2SDR UALA2012102206043Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL. RESET BOTH ELAC 1 & 2. PERFORMED OPERATIONAL TEST OF ELAC 1 AND 2 PER AMM. NO FAULTS. ELAC 2 FAULT SHOWED AGAIN AT POWER TRANSFER. REPLACED ELAC 2 PER AMM, OPS TESTED OKAY. PERFORMED CAT III PER AMM, OSDR UALA2012101005757Gearbox · out of toleranceGEARBOX EXCEEDED, NEEDS REPLACEMENT. SYSTEM TEST OF CONTROL LEAK CHECK, INSTALLED AND BOLTS REPLACED.SDR UALA2012100905716Computer · faultyREPLACE ELAC2 FOR T-S ACFT PITCH UP LOG. REPLACED ELAC2 PER AMM, OPS TEST PER MM CHECKED GOOD. ACCOMPLISHED CAT III AUTOLAND, TEST GOOD.SDR UALA2012100905712Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL REPLACED ELAC 2.SDR USAA2012100800003Unknown · malfunctionedAFTER TAKEOFF FROM PBI, AIRCRAFT ROLLED LEFT AND NEEDED RIGHT AILERON TO CORRECT. AS FLAPS WERE RETRACTED AND SPEED INCREASED, CONTROL RETURNED TO NORMAL. (ALL TRIMS ZERO IN CLIMB, CRUISE, AND DESCENT). FLIGHT CONTINUED ONTO CLT. MAINTENANCE ACCOMPLISHED ASDR UALA2012092505437Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ON SHUTDOWN. REPLACED ELAC COMPUTER. LAND VERIFY PASSED. AIRCRAFT REMAINS FULLY CAPABLE.SDR UALA2012090404986Computer · faultyELAC 1 FAULT. REPLACED NR 1 ELAC AND TEST AND TESTED OKAY.SDR UALA2012083004871Battery · inoperativeFLIGHT CONTROL BATTERY INOPERATIVE. REPLACED BATTERY ASSY.SDR UALA2012083004880Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. NO FAULT LIGHT ON ELAC1 BUTTON. JUST ECAM. SAMC TEXT: CFDS SHOWS "27-44-51 THS ACTR SERVO MOT2 9CE OF ELAC 1". REPLACED SEC1 PER AMM AND TESTED PER AMM, TESTS OK. CREW RAN ENGINES AND NO FAULTS NOTED.SDR UALA2012081604570Relay · faultySIDESTICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. - F-CTL. CREW COMMENTS: ECAM- F-CTL SIDESTICK PRIORITY. REPLACED TAKEOVER PRIORITY-2 RELAY 47CE2 (TSM27-92-00-810-830-A). ACCOMPLISHED OPERATIONAL TEST OF SIDESTICK PRIORITY, AMM TASK 27-96-00-710-003-A. TESDR UALA2012081404493Microphone · inoperativeFIRST OFFICER FLT STICK MICROPHONE INOPERATIVE. REPLACED FIRST OFFICERS SIDE STICK HANDLE IAW AMM.SDR SWIA201231457Unknown · vibrationIN CRUISE, WHOLE AIRCRAFT SHUDDERED AND VIBRATED MULTIPLE TIMES. (FLT 6345) PERFORMED GENERAL VISUAL INSPECTION OF AIRCRAFT INTERIOR, NO VISABLE DEFECTS NOTED. INFLIGHT TEST GOOD - FLEW FROM DEN -COS AT 300KTS AND NOTICED NO VIBRATING OR SHUDDERS.SDR UALA2012080704246Servo · unknownAIRCRAFT VIBRATIONS WITH NO DEFECTS FOUND. REPLACED RUDDER PCU REF AMM . REPLACED RUDDER SERVO CONTROL.SDR UALA2012073004109Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. ATTEMPTED SEVERAL RESETS, NO JOY. REPLACED NR 1 ELAC REF AMM. ACCOMPLISHED LAND VERIFY TEST, ALL PASS.SDR HEEA20120724319Tube · crackedWHILE PERFORMING 100H/12M AIRFRAME INSPECTION, FOUND LONGITUDINAL CONTROL TUBE CRACKED AT SERVO END. MX REPLACED THE CONTROL TUBE.SDR UALA2012071903932Computer · malfunctionedELAC 2 FAULT TRIGGERS PRIORITY LEFT AURAL WARNING AND ALL AMBER INDICATIONS ON F-CTL. REPLACED ELAC 2 PER AMM, CHECKED NORMAL.SDR UALA2012071203773Computer · faultyON TAKEOFF, CLIMB-OUT HAD TO USE EXCESSIVE FORWARD STICK INPUT TO KEEP PITCH FROM INCREASING. REPLACED ELAC 2. REPLACED ELAC 2 AS PER MM, CHECKED GOOD PER MM. ACFT IS FULL LAND III CAPABLE.SDR UALA2012070903663Computer · faultyRUDDER TRIM ISSUE, RETURNED TO FIELD. RT AILERON SHOWS FULL DOWN DEFLECTION ON FLT CTL PAGE, AC IN 3 DEG LT BANK. FUEL LOAD IS BALANCED, ENGINE PARAMETERS NORMAL. REPLACED BOTH ELAC'S PER MM, OPS NORMAL AND COMPLETED CATIII CHECK.SDR REXA2012070101039Unknown · unknownAT SPEEDS ABOVE 250 KTS OR SLOW SPEEDS WITH FLAPS OUT AILERON CONTROL IS SLOPPY. IT THEN OPTS HARD THEN CATCHES IN THE BANK CAUSING OVER CONTROLLING. PERFORMED PA 27-0660 FOR AILERON BINDING. LUBRICATED REAR QUADRANT PULLEYS HEARINGS IAW AMM 12-20-07-640-80SDR YYFA20120618001Unknown · multiple failREF SDR : LOST PRIMARY TRIM AFTER DEPARTURE, PRIMARY LONGITUDINAL TRIM BRAKE C/B POPPED, RESET, POPPED AGAIN, ALT LONG TRIM WORKED NORMAL. STALL INDICATION FAILURE WENT OFF AND ON THROUGH FLIGHT, AUTO SLOT FAIL" CAUTION ILLUMINATED RANDOMLY.SDR UALA2012061403272Transducer · faultyELAC FAULT, RTFL SUPPLEMENTAL DATA UPDATE REPLACED CAPTAINS SIDE STICK ROLL TRANSDUCER (4CE1). REPLACED FIRST OFFICERS SIDE STICK ROLL TRANSDUCER (4CE2) PER MM. REPLACED ELAC NR 1 AND 2. REPLACED RT. BLUE SYS. SERVO VALVE, OPS CHECKED NORMAL.SDR UALA2012060803143Transducer · faultyDURING CHECK OF FAULT HISTORY PER JC 2-2020C (A-CHECK) FOUND FAULT 27-17018 (PRESS SIGNALS FROM GUST SUPPRESSION TRANSDUCERS UPPER AND LOWER DO NOT AGREE) HAS OCCURRED MORE THAN ONCE DURING LAST 5 FLT LEGS. REPLACED UPPER GUST SUPPRESSOR TRANSDUCER, OPS CHECSDR UALA2012060803118Fastener · looseVIBRATION AND NOISE ENCOUNTERED IN FLIGHT. SECURED FASTENER AT OTBD EDGE-PANEL 344 DB. CONDUCTED FIM PER AMM. FOUND TO BE WITHIN LIMITS IAW AMM.SDR REXA2012051000719Unknown · bindingFELT BINDING & RESISTANCE IN FLIGHT OFFICERS FLIGHT CONTROL. PERFORMED INSPECTION OF ELEVATOR CONTROL CABLES. NO DEFECTS NOTED. RANGE OF MOTION OF THE ELEVATOR FORWARD AND AFT WITHIN LIMITS, NO BINDING OR RESISTANCE NOTED IAW AMM 27-31-0. OK FOR SERVICE.SDR UALA2012051102758Computer · faultyAIRCRAFT HAS NOSE-UP PITCH TENDENCY WHILE HAND FLYING. EITHER SIDESTICK. NO ECAMS. REPLACED ELAC 2 AND OPS CHECKED OK IAW MM.SDR UALA2012050402635Rod End · faultyAIRFRAME VIBRATION ON CLIMB-OUT AT FL300. 78MLT VIBRATION IN COCKPIT LT-MOD VIBRATION IN AFT GALLEY. CREW REPORTED VIBRATION IN AFT CABIN RATED AT MODERATE. BLUE AND YELLOW ROD ENDS REPLACED. SSDR UALA2012043002541Computer · faultyCREW REPORTS ELAC 2 FAULT ON CLIMB OUT OF DEN. 2ND REPEAT FAULT. REPLACED NR 2 ELAC. ALL TESTED OK INCLUDING SIDE STICK OPS, REF AMM 27-93-00. ALSO, PERFORMED AFS LAND TEST, 22-97-00.SDR UALA2012041502284Shutoff Valve · stuckLEFT WING FLIGHT CONTROL SHUTOFF VALVE IS STUCK IN CLOSED POSITION. VALVE CLOSED LIGHT WILL NOT GO OUT. REPLACED LEFT WING FLIGHT CONTROL SHUTOFF VALVE.SDR CA120417018Cable · worn(CAN) DURING ELEVATOR AND RUDDER MAIN CABLE INSPECTION, ALL 4 CABLES WERE FOUND TO HAVE WEAR, BLENCHED CABLES, IN THE AREA WHERE THE CABLES RUN THROUGH GAMMA TUBES, BS 498-596, FURTHER INVESTIGATION FOUND THAT GAMMA TUBES WERE BOWING AND CAUSING CABLES TO RUB SDR USAA2012041300012Actuator · failedCAPTAIN REPORTED LOSS OF AUTO PILOTS 1 & 2 FOLLOWED BY ELAC 1 & 2 PITCH FAULTS, FLIGHT CONTROL STABILIZER JAM, AND ALTERNATE AND DIRECT LAW FAULTS. FLIGHT DIVERTED. REMOVED AND REPLACED TRIMMABLE HORIZONTAL STABILIZER ACTUATOR IAW MM 27-44-51-401.SDR UALA2012040502115Control Unit · no testOP CHECK OF ACE MONITORING FUNCTION PER 3SV FAILED. REPLACED L1 ACE, NO HELP. SWAPPED L1 AND L2 ACE, LRU TESTS PASSED, ACE MONITOR TEST PASSED.SDR UALA2012040202059Computer · failedAILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED NR 2 ELAC PER AMM. ACCOMPLISHED TEST PER MM TASK. LAND III CAPABILITY TEST PER AMM. ALL TESTED OK. EFCS-1 & EFCS-2 GROUND SCANS RECORDED NO FAULTS. ORD TST NOTED DURING CONFERENCE CALL THAT UNISDR BHKA2012032100001Flt Controls · malfunctionedAFTER TAKE OFF, ACFT EXPERIENCED AN UN-COMMANDED ROLL. FULL RT YOKE REQUIRED FOR STRAIGHT AND LEVEL FLIGHT. FULL DOWN TRIM TO RIGHT REQUIRED FOR STRAIGHT AND LEVEL FLIGHT. DUMPED 1500 LBS OF FUEL AT 7000", 15-20 NAUTICAL MILES OVER SEA.SDR UALA2012030801514Computer · faultyAFTER ENG START FLIGHT DECK SMELLED OF A STRONG ELECTRICAL BURNING SMELL. FOUND ODOR AT SEC3 COMPUTER. REMOVED & REPLACED SEC 3. SEE SEQ#1886001. ODOR NOW DISSIPATING. OPERATION CHECKING GOOD PER TASK.SDR UALA2012022001020Control Cable · out of rigAT CRUISE ACFT WOULD START TO ROLL LEFT AND HAD TO INPUT RUDDER TRIM TO LEVEL OFF. ACCOMPLISHED REVIEW OF AMIS HSI, AND AILERONS. ACCOMPLISHED RIG CHECK OF AILERON AND AILERON TRIM CONT SYS REF MM 27-11-00-501. ACCOMPLISHED STEP 3H, FOUND NO DISCREPANCIESSDR SWAA2012022401669Pcu · leakingAIR TURNBACK - A-SYSTEM QUANTITY DROPPED TO 1/4 INFLIGHT. FOUND HYDRAULIC LEAK IN NR 1 WHEEL WELL. REMOVED AND REPLACED "A" SYSTEM AILERON PCU IAW MM.SDR UALA2012020600709Trim Switch · inoperativeCAPTS YOKE TRIM SWITCH INOP. REPLACED CAPT YOKE PITCH TRIM SWITCH. REMAINING CONTROL WHEEL PITCH TRIM SW OPERATING NORMALLY. OPERATIONAL CHECK ON BOTH SIDES REVEALS NO FAULTS.
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