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 HALA2013110500166Unknown · malfunctionedAIR TURN BACK, RUDDER RATIO, AIRERON LOCKOUT & ALL THREE AUTOPILOTS WON'T ENGAGE. ACCOMPLISHED FIM TASK 73-21/892, 27-21-804 & 27-48-809 PROCEDURES. UNABLE TO DUPLICATE ON GROUND. PIMU BITE CHECKED, NO FAULTS FOUND. STAB TRIM AND RUDDER RATIO TRIM OPS CHECSDR CALA2013110592648Relay · failedFLT CTL SEC 1 FAULT ECAM RAN CHECK LIST WOULD NOT RESET. LND DIST REQ LESS THAN 4000 FT. REPLACED RELAY 41CE1, RERACKED SEC1 & OPERATIONS CHECKED IAW MM. TESTED NORMAL, NO FURTHER FAULTS, OPERATIONS NORMAL.SDR CALA2013110492583Computer · faultyELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CONFIRMED NR 2 ELAC COMPUTER IS BAD. SWAPPED BOX INTO THE NR 1 ELAC POSITION & MEL NR 1 ELAC SYSTEM INOPERATIVE. ACFT DOWNGRADED TO CAT 1. SN OF NR 1 ELAC IS 1039, SN OF NR 2 ELAC IS 5084. ALL DDPG IAW DF0980.SDR CALA2013103092520Unknown · malfunctionedAIRCRAFT NEEDED 4 - 5 UNITS LT TRIM IN CLIMB. NEEDS APPROXIMATELY 3.8 - 4.0 UNITS OF TRIM IN CRUISESDR CALA2013102992498Unknown · malfunctionedDUE TO REPORT OF UNCOMMANDED NOSE PITCH DOWN PERFORM THE FOLLOWING: AUTO FLIGHT FAULTS BITE FIM MM22-00-02-101, PAY PARTICULAR ATTENTION TO ANY FCC & STAB TRIM RELATED FAULTS. BITE OF BOTH SAM MODULES IAW MM27-09-00-150 FIG.106 & TEST SAMS IAW MM27-09-00 P21SDR CALA2013102492358Computer · faultyELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN, CAME UP DURING FLAP RETRACTION FROM 1 TO 0 AFTER TAKEOFF. REPLACED ELAC 2, OPERATIONS TESTED GOOD, AFS TESTED GOOD & AUTO LAND TESTED GOOD.SDR CALA2013101692101Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC 1 IAW AMM. TESTED GOOD IAW AMM 27-93-00. AIRCRAFT RETAINED TO CAT 3 FULL CAPABILITY IAW AMM 22-97-00.SDR CALA2013100991884Electronic Unit · faultyWHILE TROUBLESHOOTING FOUND NR 2 LT CSEU POWER SUPPLY FAULTING. REPLACED NR 2 LT CSEU POWER SUPPLY, OPERATIONS CHECKED NORMAL.SDR CALA2013100991883Electronic Unit · faultyLT FLT CONT ELEC EICAS BITE & STAB TRIM MX MESSAGES SHOW. FOUND 1L & 2L POWER SUPPLY MODULES FAULTED. REPLACED NR 1 LT CSEU, OPERATIONS CHECKED NORMAL. MESSAGES CLEARED.SDR SWIA201334901Unknown · malfunctionedASYMMETRIC ROLL NOTED IN FLIGHT WHEN FLAPS SELECTED TO 45 DEGREE. PAINT RIDGES NOTICED ON TOP OF FLAP LE. FLT#5553 INSPECTED ALL FLIGHT CONTROLS & FLAPS FOR ANY DEFECTS, NO DEFECTS NOTED. RAN ALL FLIGHT CONTROLS TO FULL TRAVELS & RAN FLAPS FROM 0 DEGREE TO SDR CALA2013100991919Lru · malfunctionedACE TEST FAILED SHOW RT ACE INTERNAL FAULT. MESSAGE 27-13003, 27-13002, 27-13001 & 27-13000 DISPLAYED AFTER ACE MONITOR TEST PASS INDICATED ON MX PAGE. THIS CONDITION OK IAW MM. ACCOMPLISHED ACE LRU REPLACED TEST TO UNLATCH FAULTS. ALL LRU REPLACEMENT TESTSDR DALA13049823226Rod · corrodedDURING INSPECTION, FOUND CORROSION ON TARGET AND PLAY ON ACTUATOR ROD AND PLAY ON BEARING AT INTERCONNECTING STRUT. LT SIDE. REPLACED INTERCONNECTING STRUT LT SIDE. IS DOCUMENTED ON AMDS CARD 2751-9202/101.SDR SWIA201334995Link Assy · corrodedTHE RT FLUTTER DAMPNER LINK ASSEMBLY IS HEAVILY CORRODED & PITTED ALONG WITH THE LINK ASSEMBLY HARDWARE. C-CHECK INSTALLED NEW RT FLUTTER DAMPENER LINK ASSEMBLY & HARDWARE IAW AMM.SDR CALA2013093091578Computer · faultyF-CTL ELEV SERVO FAULT. REPLACED NR 2 ELAC IAW MM 27-93-00-710-001-A & TESTED OK. ACCOMPLISHED CAT 3 AUTOLAND TEST IAW MM 22-97-00, CHECKED OKAY.SDR CALA2013093091574Computer · faultyECAM F-CTL SEC 1 FAULT. REPLACED SEC 1 IAW AMM & OPERATIONS TEST IAW AMM. TESTED OKAY. ACP CAT3 IAW AMM.SDR CALA2013093091548Computer · malfunctionedELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC NR 1 IAW MM 27-93-34 AFS & LAND VERIFICATION TESTED NORMAL IAW MM 22-96-00 & MM 22-97-00. AC RETURNED TO FULL CAT III CAPABILITY.SDR UHLA2013092500430Fmc · malfunctionedSPOILER FAULT MESSAGE ON EICAS DURING FLIGHT. DECLARED EMERGENCY, DIVERTED. LANDED WITHOUT INCIDENT. MX R & R FCM 4, OPS CHECKED GOOD.SDR CALA2013092791530Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC 1, ACP CAT 3 IAW AMM 22-96-00 & AMM 22-97-00.SDR CALA2013092591425Computer · faultyFLIGHT CONTROL ELAC 1 PITCH FAULT DURING FLIGHT CONTROL CHECK. RESET, NO HELP. ELAC NR 1 IAW MM 27-93-00. ALL GROUND TESTS GOOD. ACCOMPLISHED ACP LAND TEST IAW MM 22-97-00. ALL TESTS PASSED.SDR CALA2013092391353Control Switch · faultyLT WING FLT CONTROL SHUTOFF SWITCH ON AUX PANEL WAS FOUND IN OUT OFF POSITION. LT WING FLT CONTROL SHUTOFF VALVE DEFERRED INOPERATIVE IAW MEL. CONTROL SWITCH REQUIRED REPLACEMENT. MEL DEACTIVATION PROCEDURE & TEST ACCOMPLISHED.SDR ASMF201310003Control Cable · out of adjustAIRCRAFT RETURNED TO PLATFORM, DURING FLIGHT AILERONS CONTROLS TEST, THE RT SPOILER DID NOT RETURN TO NEUTRAL POSITION. MAINTENANCE PERFORMED FLIGHT CONTROL TEST, CONFIRMING THAT THE RIGHT SPOILER DID NOT RETURN TO NEUTRAL POSITION IAW AMM 27-61-00. THE RUDDSDR SIMA20130915001Unknown · unknownTHE CREW REPORTED THEY WERE UNABLE TO ROTATE ON TAKEOFF ROLL WITH YOKE FULL AFT. HIGH SPEED ABORT PERFORMED. THE ACFT WAS REMOVED FROM SERVICE. ELEVATOR DEFLECTION CHECK COMPLIED WITH IAW 27-31-00 ALSO OPS CHECK OF AURAL WARNING UNIT IAW AMM 31-51-00. ELEVASDR SIMA20130913005Sleeve · inoperativeTHE CREW REPORTED PACK NR 1 VALVE CLOSED DURING CLIMB, RESET IAW AOM V1, STAYED OK FOR 5 MINUTES THEN CLOSED AGAIN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 210 AND NR 230 LT ACM SLEEVES IN REFR SDR CALA2013081990544Computer · faultyDURING CRUISE FLT FELT BUMP IN TAIL AND ECAM F-CTL ELAC2 PITCH FAULT AND AIL SERVO FAULT MESSAGES APPEARED AND FELT ANOTHER BUMP AND MESSAGES CLEARED. TROUBLESHOTING & FOUND NO PEDAL MESSAGES, REPLACED ELAC 2, OPS TESTED GOOD.SDR YENA20130817177Computer · failedAIR RETURN TO DEPARTURE CAPT LEG, AFTER ROTATION NOTICED NEEDED FWD PRESSURE ON STICK TO KEEP ACFT FROM PITCHING UP. AT 1,000' ACCELERATED AND CLEANED UP ON SCHED. CONTINUED TO CLIMB, STILL HAD TO HOLD FWD PRESSURE ON STICK TO STOP ACFT FROM FURTHER PITCHING SDR CALA2013082090599Computer · faultyCREW REPORTED EXCESSIVE ACFT PITCH UP. AFTER TAKEOFF ACFT NEEDED FWD STICK PRESSURE. AT CRUISE SPEED CHANGES RESULTED IN LOSS OR GAIN OF ALTITUDE DUE TO SLOW TRIM RESPONSE. NOTED PITCH UP WAS MORE THAN 2.5 DEGREES PER MIN. AIRMAN SHOWS CFDS MSG "ELAC2 COM SDR CALA2013081490432Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL REPLACED ELAC 1 IAW AMM. ACCOMPLISHED LAND CAT 111 TEST IAW AMM. OPS CHECKED NORMAL, NO FAULTS.SDR CALA2013081290337Computer · faultyELAC1 FAULT, INSTALLED NEW ELAC1 IAW AMM. ACCOMPLISHED CAT 3 IAW 22-97-00, NO FAULTS.SDR CALA2013081290330Computer · faultyF-CTL ELAC 2 FAULT. ELAC 2 SHOWED AS WARNING ON AIRMAN-WEB WITH ELAC 2 FAILURE MESSAGE, RESET NO HELP. SWAPPED NR 1 AND NR 2 ELAC COMPUTERS AND FAULT FOLLOWED, NR 2 TEST OK. NR 1 ELAC NOW INOP AND COMPLIED WITH MEL 2793A.SDR CALA2013073090077Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL. REMOVED AND REPLACED NR 1 ELAC COMPUTER. PERFORMED OPS TEST PER AMM. ALL CHECKED GOOD. ACFT REMAINS AUTOLAND LIMIT CAT 3 SINGLE AS PER PLA SFR 4730 DUE TO NR 3 IRS ON PLACARD.SDR CALA2013072990012Pcu · inoperativeFLAPPER ON STATUS MESSAGE DISCONNECT CAP AND STOW FOR LT OTBD PCU. MSG 27-10301 SHOWN, PCU LEFT OTBD DOES NOT FOLLOW COMMAND. CB PULLED TO DEACTIVATE. PCU LT OTBD DOES NOT FOLLOW COMMAND. REPLACED LT OUTBOARD PCU IAW MM, OPS GOOD, NO MESSAGE.SDR UALA2013072505235Computer · faultyNR 2 ELAC FAULT LIGHT INOPERATIVE. NR 2 ELAC PITCH TRIM FAULT RESET SUCCESSFUL. ELAC FAULTED A SECOND TIME WHEN NR 2 ELAC TURNED OFF ACFT HAD A SUDDEN SLIGHT PITCH. REPLACED NR 2 ELAC IAW AMM AND ACCOMPLISHED TEST IAW AMM. ALL PASS NO FAULTS.SDR UALA2013072505233Computer · faultyFLIGHT CONTROL ELAC 2 FAULTED. LOSS OF THE RECEPTION OF ELAC 2 DISCRETES BY 1 FAC OR 1 FMGC. REPLACED FCDC2 AND TESTED IAW MM 27-95-34-400-001-A, NO FAULTS NOTED.SDR XCGA201307250001Unknown · unknownPILOT REPORTED AN UNCOMMANDED STICK MOVEMENT FORWARD, RESULTING IN PITCH DOWN AND AUTOPILOT TURNING OFF. MX RESET THE INTEGRATED AVIONICS COMPUTER AND CLEANED THE ELEVATOR SERVO CONNECTIONS. SEVERAL OPS CHECKS WERE PERFORMED WITH NO DISCREPANCIES NOTED, ACFSDR UALA2013071705019Computer · failedELAC 2 FAULTED. DUE TO REPETITIVE ELAC 2 FAULTS WITH NO CFDS FAULT ACTIVITY, AND MULTIPLE SUCCESSFUL RESETS, ACCOMPLISHED TSM TASK 27-93-00-810-947. ELAC 2 FAILED AND WAS SWAPPED WITH ELAC 1, OP CHECKED GOOD.SDR UALA2013071805035Computer · faultyCLASS II F-CTRL MESSAGE DISPLAYED ON LOWER ECAM. MESSAGE INITIALLY DISPLAYED ON LOWER ECAM WITH IRU'S ALIGNED. PERFORMED EFCS 1 AND EFCS 2 GROUND SCANS, BOTH SHOWED MESSAGE, ELAC 1 OR WIRING FROM B HYD PRESSURE TRANSMITTER 2065 GN 27-93-34. MESSAGE CLEAREDSDR REXA2013071601370Unknown · unknownAUTOPILOT IS LAGGING BEHIND ON ROLL OUT FROM TURNS. THE ELEVATOR CONTROLS ARE JERKING BACK AND FORTH WHILE AUTOPLIOT IS ON ESPECIALLY WHEN LEVELING OFF FROM DESCENTS. PERFORMED OPS CHECK OF FCC. OPS CHECKED GOOD IAW AMM 22-11-00. PERFORMED ELEVATOR SERVO ERRSDR UALA2013071504943Computer · faultyELAC 2 (2CE2) BCU (10GG) CLASS 3 MESSAGE DISPLAYED. REPLACED ELAC 2, OPS CHECK OK.SDR F3LA2013071700885Unknown · vibrationAIR TURN BACK DUE TO SEVERE AIRFRAME VIBRATION. BEGAN AT 25,500 FT AND AROUND 330 KIAS. DID NOT STOP UNTIL SPEED MANUALLY FLOWN LESS THAN 300 KIAS. EMERGENY DECLARED. R & R LT AND RT ELEVATOR ATTACH HARDWARE AND BEARINGS REF AMM 27-34-41, PAGE BLOCK 401. SDR UALA2013071004801Pcu · faultyFLIGHT CONTROL SYSTEM STATUS MESSAGE 27-10306, FLAPPER ON POWER CONTROL UNIT RT INBD BYPASS SOLENOID OPERATED, VALVE IS NOT IN COMMANDED POSITION. TROUBLESHOT IAW FIM 27-11, TASK 906. WIRING CHECK FOUND BYPASS SOILENOID OPEN CIRCUIT. REPLACED RT INBD FLAPERSDR UALA2013070904780Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL. PROG TEXT: ITEM ROLLED FWD. REF TSM 27-90-00-810-812. BERG TOMC. R & R ELAC 1 COMPUTER IAW AMM REF 27-93-34-000-001A AND 27-93-34-400-001A. OPS TEST GOOD. LAND VERIFY TEST ACCOMPLISHED IAW AMM 22 -97SDR CALA20130709003Computer · faultyAFTER RESETTING CB TO CLEAR "ELAC 1 PITCH FAULT" MSG RETURNED. REPLACED THE NR 1 ELAC IAW MM, SYS OK. CAT III TESTED OK IAW MM. SYSTEM OK, ACFT IS FULL AUTOLAND CAPABLE.SDR UALA2013070904794Computer · faultyAFTER RESETTING CIRCUIT BREAKER TO CLEAR NR 1 ELAC PITCH FAULT, MESSAGE RETURNED. I REPLACED THE NR 1 ELAC IAW MM, SYS OK. CAT III TESTED OK IAW MM. SYS OK, ACFT IS FULL AUTOLAND CAPABLE.SDR UALA2013071004814Computer · failedCREW REPORTED ELECTRICAL ODOR IN COCKPIT AND MID CABIN. TURNED OFF RIGHT RECIRCULATION FAN AND HAD F/A'S TURN OFF GALLEY POWER. ODOR DID DISSIPATE, SHORTLY THEREAFTER, LOST F/O FLIGHT DIRECTOR BARS AND RECEIVED A NO LAND III ASA. FOUND FCC BOX BURNED. RASDR UALA2013062604432Computer · faultedELAC 2 FAULTED. R & R ELAC 2 IAW MM 27-93-00-710-001. OPS CHECKED GOOD.SDR UALA2013062504400Computer · faultyELAC 1 PITCH FAULT, RESET UNSUCCESSFUL. REPLACED ELAC 1 AND ALSO PERFORMED CAT II CK. ALL SYSTEMS PASSED HAD NO MESSAGE AND NO FAULTS.SDR UALA2013062504391Computer · faultyELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL PAGE HAS AMBER BOX ON LT B. PFR FAILED ELAC 1. REPLACED ELAC 1. LAND 3 TESTS PASS REF AMM. ACFT IS IN CAT IIIB STATUS.SDR UALA2013061804207Seal · unsecureAIRFRAME VIBRATION FROM T/O THROUGH 17K FT. SUSPECT LOWER F/O NOSE AREA. ENGINE PARAMETERS NORMAL, FOUND SEAL AT PANEL 191BT AND 191DT SPLIT AND PROTRUDING OUT OF THE GAP. TAPED OVER DAMAGED AREA IAW AMM MT 53-004. COMPLETED VIBRATION SHEET AND TROUBLESHOSDR UALA2013061304065Computer · failedSIDE STICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC1 & ELAC 2 IAW AMM 27-93-34, RETURNED ACFT TO FULL CAT III CAPABILITY AFS AND LAND VERIFICATION TESTS NORMAL, IAW AMM 22-96-00 AND 22-97-00.SDR ASOA20130609328Switch · failedMAIN PITCH TRIM INOPERATIVE MESSAGE ON CLIMBOUT, AUTO TRIM FAIL, ELEVATOR MISTRIM. R & R PITCH TRIM SWITCH AND ACTUATOR. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.
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