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 CA120202001Bellcrank · worn(CAN) AFT RT BELLCRANK UNDER TRANSMISSION DECK FOUND CONTACTING AN AIRFRAME GUSSET AND CAUSING A TEAR IN THAT GUSSET. AFT LT AND RT, 350A27-1452-03, LT AND -02 RT ARE OFFSET AND HAVE TO BE INSTALLED AT THE CORRECT LOCATION TO AVOID ANT CONTACT WITH ITS SURROUSDR ANCF2012013000111Computer · faultyREJECTED TAKE OFF DUE TO AILERON SERVO FAULT, IAW AMM 27-93-24-000/400-001A THE ELAC 2 WAS REPLACED TEST ON GROUND SATISFACTORY IAW AMM 27-93-00-710-001-A AND 22-97-710-001-A.SDR UALA2012010300012Flt Controls · warning messageFLIGHT CONTROL SYSTEM ADVISORY. ON ARRIVAL, FOUND MESSAGE 27-1030 6 AND NOT ACTIVE. CARRIED OUT GROUND TEST, TEST FAILED. ACCOMPLISHED FIM 27 -11 TASK 906. REPLACED ACE-L2 NO HELP, BACK TO ORIGINAL. ACCOMPLISHED WIRE CHECK BETWEEN D4422J AND DM27210, CHECKESDR E81R2011121302271Flt Controls · unknownINVESTIGATED IN-FLIGHT "AP PITCH TRIM FAIL" ANNUNCIATOR INDICATION. VERIFIED AUTOPILOT NOSE UP PITCH TRIM FUNCTION INOPERATIVE. SWAPPED NR 1 AND NR 2 FCC-4007 CARDS FOR TROUBLESHOOTING, NO FAULTS INDICATED. AUTOPILOT NOSE-UP TRIM CONTROLLED BY NR 2 FCC-4007 CSDR UALA2011122707105Unknown · malfunctionedFLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS. STATUS MSG02- ACTIVE CRUISE HARD; PITCH TRIM CHANNEL (CENTER) DOES NOT FOLLOW TRIM UP COMMAND. DB- PRIMARY FLIGHT COMPUTER (LEFT) MSG03- ACTIVE CRUISE HARD; PITCH TRIM CHANNEL (CENTER) DOES NOT FOLLSDR UALA2011121406854Battery · failedON ARRIVAL RECEIVED MESSAGE 24-50243, & STATUS MESSAGE FOR FLIGHT CONTROL SYS. PER FIM 24-35 TASK 802 CHK FOUND FCDC CENTER BATTERY IS BAD PER MM. REPLACED WITH NEW BATTERY, MSG GONE. OPERATION TEST FINE, NO FAULT FOUND.SDR NOCA11511Unknown · unknownAIRCRAFT HAD AN AIR TURNBACK DUE TO UNCOMMANDED RAPID LEFT RIGHT YAW MOVEMENT FOR APPROX 3 SEC NO EICAS OR WARNING LIGHTS OR INDICATIONS ON STATUS PAGE NOTICED AFTER THE EVENT. NO TURBULENCE ENCOUNTERED WITHIN THE GENERAL TIME OF THIS EVENT.SDR DALA1503819235Jackscrew · unknownHORIZONTAL STABILIZER JACKSCREW ASSY, REPAIRED IAW AA 2740-01071.SDR UALA2011112106349Warning System · false activationSTATUS PAGE SHOWED FLIGHT CONTROL STATUS FOR SHORT PERIOD OF TIME. FOUND MSG FAULT CODE 270 071 00. PERFORMED MAT TEST PRIMARY FLIGHT CONTROL SYSTEM TRANSMITTER RESET TEST. PASSED, MSG ALREADY GONE UPON ARRIVAL.SDR UALA2011111506245Ace · malfunctionedFLT CTL SYS STATUS MSG. FOUND CB 'BATT INTLK' OPEN ON FACE OF PSA RIGHT, RESET AND TRIPPED AGAIN. PCN 566-9015. ACCOMPLISHED TROUBLESHOOTING PER MAINT MESSAGE 27-15102 FIM 27-02 TASK 851, FOUND ACE R M 27221 CAUSING CB D8-R AT POWER SUPPLY RIGHT M24201 POPPSDR UALA2011111406226Computer · faultyAT LANDING GEAR DEPLOYMENT A-C ROLLED HARD LEFT. HALF CONTROL. STICK INPUT TO STOP ROLL. SAMC TEXT: *UPDATE* NO WIND OR WAKE PRESENT WHEN ROLLING MOMENT OCCURED. INBD CREW REPORTS A-S 190 KTS, FLAPS 1, SPEED BRKS FULLY EXTENDED, ROLL OCCURRED AT MOMENT GEASDR UALA2011102805830Transducer · failedELAC FAULT. REPLACED CAPT'S ROLL SIDE STICK TRANSDUCER 4CE1 REF AMM AND COMPLETED REJECTION FOLLOW-UP #RFU224068.SDR UALA2011102805854Computer · faultyCLASS II MAINT MSG F-CTL DISPLAYED LOWER ECAM. REPLACED SEC 1. OP CHECKED PER MM.SDR UALA2011102805853Computer · faultyREPLACED ELAC 2 PER MM. OPS NORMAL.SDR ASOA201101988Flt Controls · erraticACFT AGGRESSIVELY ROLLED RT WHEN FLAPS SELECTED FROM 30 TO 45. REQUIRED MORE THAN HALF SCALE LWD AILERON TRIM, AT WHICH TIME AILERON CONTROL BECAME ERRATIC DURING NORMAL CORRECTIONS. THERE WAS 'NULL' ZONE AT CENTER OF AILERON TRAVEL AND 'JERKS' WITH SMALL LT SDR UALA2011101405578Unknown · unknownACFT BANKS TO LEFT, FLIGHT DIVERTED. INSPECTED, NO DEFECTS NOTED.SDR UALA2011101405573Computer · malfunctionedCYCLIC VERTICAL BUMPING-PITCHING FELT AT CRUISE. FLIGHT CONTROL SD SHOWED LT & RT AILERONS MOVING UP & DOWN IN UNISON WITH BUMPING. CONSULTED FMC ELAC 1-2 FAULT, IRREGULAR. TURNED OFF ELAC 1, AILERON MOVEMENT STOPPED. NO FURTHER OCCURRENCE OF BUMPING-PITCHSDR CA111021008Unknown · unknown(CAN) BEFORE TOUCHDOWN NEAR TO GROUND (GOOD SPEED, ABOVE VREF), ACFT BANKED TO THE LEFT, TRIED TO RECOVER WITH INPUT BY AILERONS TO THE RT AND LOWERING THE NOSE. DURING THAT UNEXPECTED BANKING TO THE LT THE AURAL WARNING: BANK ANGLE, BANK ANGLE, BANK ANGLE SDR UALA2011101005487Sensor · failedFLAP-SLAT SKEW SENSORS FAILURE OF ONE OR MORE SLAT AND-OR FLAP SKEW DETECTION SENSORS.SDR UALA2011092805263Shutoff Valve · stickingRIGHT FLIGHT CONTROL SHUTOFF VALVE STICKING. REPLACED RIGHT FLIGHT CONTROL SHUTOFF VALVE, OPS CHECKED GOOD.SDR UALA2011092605164Unknown · unknownCREW REPORTS ON TAKEOFF ROLL AT 130 KIAS (ALL 3 GEAR STILL ON THE GROUND), CREW FELT A MOMENTARY JOLT-YAW-LATERAL MOVEMENT NOSE LEFT. CREW COUNTERED WITH SLIGHT RT RUDDER. CREW DID NOT FEEL ANY MOVEMENT IN RUDDER PEDALS PRIOR TO COUNTERING THE YAW. RUNWAY WSDR UALA2011091604998Servo Control · malfunctionedMOD - TO HEAVY MOD VIBRATION FELT DURING CLIMB 339IAS. FL250 CLIMBING VIBRATION CAME ON ABRUPTLY AND FELT AS IF SOMETHING WAS GOING TO COME OFF. AFT FLT ATTENDANT THOUGHT IT WAS SEVERE, 100 TIMES STRONGER THAN ANYTHING SHE HAS EVER FELT. OPBLM FIELDS. SAMSDR CALA2011091600600Unknown · malfunctionedDURING DESCENT STARTING AT 15000 FT 3 DIFFERENT TIMES THE AIRCRAFT SNAP ROLLED TO APPROXIMATELY 30 DEG OF RIGHT BANK REMAINED THERE FOR A SECOND OR TWO THEN ROLLED AGGRESSIVELY BACK TO WINGS LEVEL OVER SHOOTING WING LEVEL CONTINUED ON NEXT LOG PAGE. T/S PER FISDR UALA2011091204946Computer · faultyPFC LANE FAULT 27-14012. BOEING AHM PROGRAM HAS DETECTED REPEAT FAULT MSG 27-14012 PFC R LANE 1 FAULT. REPLACE THE PFC-R (483-9216) PER MM, CONFIRM PFC SOFTWARE IS CORRECT FOR ALL 3 PFC'S. ACP PFC LANE RESET TEST TWICE TO UNLATCH REMAINING FAULTS. IF PFC-R SDR UALA2011082204485Computer · faultyFLT CONTROL ELAC NR 1 PITCH FAULT. RESET ELAC NR 1 TWICE, COMES BACK ON FLT CONTROL CHECK. REPLACED ELAC NR 1 PER MM AND CAT III AUTOLAND PER MM. OPS CHECKED OKAY.SDR DALA1514449229Jackscrew · not reportedHORIZONTAL STABILIZER JACKSCREW ASSY REPAIRED IAW AA 2740-01071.SDR UALA2011081204258Computer · faultyELAC 2 FAULT. REPLACED ELAC 2 PER AMM. TESTS OKAY. ACCOMPLISHED CAT3 TEST. TESTS SATISFACTORILY.SDR UALA2011080304055Computer · failedELAC FAULT - WILL NOT RESET. ELAC 2 FAILS ONLY AFTER HYD SYS IS OFF. SYSTEM TRIMS THS OKAY. REPLACE 2CE2.SDR IPXA11668384Control Module · inoperativeCREW EXPERIENCED AUTOPILOT WARNING AND INABILITY TO OPERATE THE STABILIZER TRIM MANUALLY - AIR TURN BACK. TROUBLESHOOTING CARRIED OUT THROUGH AMM & FIM INDICATING STAB TRIM CONTROL MODULE FAILURE. BOTH STCM'S HAVE NOW BEEN REPLACED AND IN PROGRESS OF REPLACISDR UALA2011072703851Computer · intermittentECAM FLT CNTL - ELAC 2- CYCLED ELAC 2. OPS OK, OCCURRED ON GROUND. ELAC2 FAULT INTERMITTENT, ALSO ORDERED FCDC2 ON AOG. ACP TSM27-93-00-810-836. REPLACED ELECTRONIC MODULE N1 ON PITCH TRIM ACTUATOR. OPS CHECKED OK. FAULT CLEARED.SDR UALA2011072603825Computer · faultedWITH AP OFF A-C PITCHES UP UNCOMMANDED AT 3DEG PER SEC. MUST HOLD STICK FWD TO MAINTAIN ATT. SAMC TEXT: *UPDATE* CREW REPORTS WITH AP ON LIMITED TO .5 DEG PITCH TRIM, BUT ACFT STABLE. CFDS SHOWS HISTORY OF ELAC 2 AND ACCELEROMETER ISSUES. ELAC 2 PREV REPLASDR UALA2011072603824Computer · faultyFLT CTL MSG DISPLAY ON LOWER ECAM, FOUND ON PFR AND PLR MSG SEC 2 OR WIRING FROM ACCLRM 3 12CE3. ACP TSM 27-94-00-810-825 EFCS TEST SEC 2 FAULT MSGE,SWAPPED WITH SEC 3 FOR MAINTENANCE PURPOSES, AND FLT CTL MSG NO LONGER PRESENT ON ECAM AND SEC FAULT MSG NO DSDR UALA2011072503805Flt Controls · malfunctionedON 2 LEGS NOTED EXCESSIVE YAWING IN BACK OF A-C. PASSENGERS GETTING SICK FLYING IN SMOOTH AIR. PERFORMED AFS BITE=BOTH FAC COMPUTERS=NO FAULTS. PERFORMED OPERATIONAL TEST OF THE YAW DAMPER FUNCTION OF SYSTEM 1 AND SYSTEM 2=NO FAULTS.SDR UALA2011072203742Computer · faultyELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL ELAC PITCH FAULT WILL NOT RESET PER SYS RESET. CIRCUIT BREAKER RESET NO HELP, ELAC 1 REPLACED: NO HELP, FAILS DURING FLT CONTROL CHECK WITH FAULT CODE "ELAC 1 COM OR WIRING TO L.B. ELEV SERVO 34CE3". SDR UALA2011072203738Computer · faultedELAC2 AND ELEVATOR SERVO FAULT DISPLAYED. ATTEMPTED RESET, NO HELP. REPLACED ELAC 2. CHECKS NORMAL IAW AMM. AC REMAINS IN CAT III.SDR CA110721011Unknown · unknownDURING A TRAINING FLT, AFTER LANDING WHILE SLOWING BELOW 100 KNOTS, AS THRUST REVERSERS DEPLOYED, THE ACFT PITCHED UP AND BECAME AIRBORNE. AFTER TOUCHING DOWN AGAIN, THE ACFT BOUNCED AND ROLLED TO THE RT. THE RT WING TIP THEN CONTACTED THE RUNWAY. THERE WERSDR CA110713001Control Cable · wornWHILE DOING A 1200 HOURS CHECK ON A LR-45, AILERON, RUDDER AND ELEVATOR CONTROL CABLES WERE FOUND DAMAGED 40-50 PERCENT. AMM 27-00-00, PAGE 234 FOR DAMAGE LIMITS. THOSE CABLES ARE SUPPOSED TO BE SERVICEABLE FOR 4800 HOURS, BUT THE ACFT IS AT 2887.47 HOURS ANDSDR UALA2011070703386Computer · faultyAIL SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN - F- CTL. REPLACED ELAC 1 PER MM, MSG CLEARED. SEPARATE WRITE UP MADE FOR CAT III CHECK.SDR UALA2011070703385Dcu · malfunctionedFLIGHT CONTROL DATA CONCENTRATOR (FCDC) 2 INOP - F-CTL. SAMC TEXT: REPLACE FCDC2 482-9544 OR DEFER PER 2795A. NO TIME TO TROUBLESHOOT. INSTALLED NEW FCDC POS 2 PER MM AND OPS CHECKED PER MM, NO FAULTS.SDR UALA2011062903220Computer · faultedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL, ACFT PITCHED UP ABRUPTLY WHILE AP 2 ON. POST FLIGHT REPORT SHOW THS ACTR POS ERROR 9CE OF ELAC 2 MSG 274451. REPLACED ELAC 2 COMPUTER, NO HELP. SWAP WITH ELAC 1, NO HELP. REINSTALL TO ORIGINSDR UALA2011062903198Computer · faultyFLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS. REPLACED AND OPS CHECKED CENTER ACE AND CENTER PFC PER MM. ALL TESTS PASSED.SDR DXTA2011061704618Control Cable · out of rigINITIATED A 15 DEGREES LEFT TURN & HAD A BINDING IN SPOILER SYS. NO PROBLEMS ROLLING RT. AT 0-10 NORMAL 10-15 DEGREES BINDING BEGINS & AROUND 15, PRESSURE POPS OFF TO LESS THAN NORMAL. AT 18, NORMAL PRESSURE & CONTROL. OBSERVED ON BOTH CONTROL COLUMNS AT MUSDR WRNA201100006Actuator · malfunctionedAFTER T/O DURING FLAP AND SLAT RETRACTION LEVEL 2 ALERT "AIL DEFLECT DISAG" ILLUMINATED. FOLLOWED PROCEDURE ESTABLISHED IN VOL I (QRH). DUMPED APPROX 63000 KGS OF FUEL TO ACHIEVE ACCEPTABLE LANDING WT. RETURNED TO AIRFIELD, LANDING NORMAL. MX TROUBLESHOT SSDR UALA2011060802810Computer · inoperativeELAC 1 FAULT MSG. CYCLE CB'S B11+A01 (105VU COMPT) PER MM. ELAC1 INOP, PER MEL 2793A DEACTIVATED AND ACFT IS DOWNGRADED TO CAT2. REPLACED AND TESTED ELAC 1 PER MM, ACP CAT III AUTOLAND TEST PER MM, CHECKED OK.SDR UALA2011060602780Module · faultyR FLT CONT STATUS MSG. FLT CONT POWER SUPPLY 2R FAULTBALL WILL NOT RESET. REPLACED MODULE 2R AND MSG CLEARED.SDR SWIA201126381Computer · defectiveAIRCRAFT BEGAN TO YAW LEFT AND RIGHT AND CONTINUED TO YAW WITH AUTO-PILOT AND YAW DAMPERS DISENGAGED. (FLT 1179) REPLACED BOTH FLIGHT CONTROL COMPUTERS, BOTH YAW DAMENERS, AND BOTH HIRF CARDS.SDR UALA2011053102632Pcu · faultyFLIGHT CONTROL SYS ANY CONDITION OF THE FLIGHT CONTROL SYSTEM OR IT'S SYSTEM INTERFACES WHICH WOULD PREVENT DISPATCH. FLIGHT CONTROLS SYSTEM BELOW MINIMUM DISPATCH REQUIREMENTS. STATUS MSG01- LATCHED INITIAL CLIMB HARD; RUDDER POWER CONTROL UNIT (UPPER) EHSV SDR NOCA05511Pulley Bracket · crackedFWD SIDE OF STATION 246 CENTER CONTROL CABLE PULLEY BRACKET CRACKED. REMOVED CRACKED BRACKETS INSTALLED NEW BRACKETS AS PER BOEING DRAWING 255T4472.SDR CALA2011051600368Cable Assy · disconnectedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF LANDING WEIGHT 148.0 SMOOTH LANDING REF FIM 32-30-00-810-813. FOUND GSBV INTERLOCK ACTUATING CABLE DISCONNECTED. RECONNECTED REF AMM 27-12-00-820-803 FIM REPAIR CONFIRMATION GOOD.SDR UALA2011051102329Unknown · vibrationVIBRATION - NOISE ENCOUNTERED IN FLIGHT. REF FLT MANUAL 12.20.1. NEED TO COMPLETE VIBRATION REPORTING CHECKLIST AND DEBRIEF MAINTENANCE (SAMC) ON ARRIVAL TO DESTINATION STATION. CREW COMMENTS: SLIGHT VIBRATION IN AFT CABIN ON CLIMB TO FL230 FELT IN COCKPIT
Back to JASC 2700