JASC 2700
Service difficulty reports · 1,743
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 HALA2023031700047Servo Control · leakingOTHER - FLUID LEAKING FROM UNDER PANEL UNDER RT WING. FOUND INBD AILERON SERVO CTRL (7C52G) LEAKING. REMOVED & REPLACED INBD AILERON SERVO CTL REF AMM 27-14-51. UPTO STEP 4.C. (2). RII 386502. COMPLETED REMAINING STEPS PER A330 AMM 27-14-51-400-801-A. LEAK CHESDR JJBA20230315018Pressure Sensor · inoperativeRUDDER OVERBOOST ON EICAS AFTER TAKEOFF. REMOVED AND REPLACED RUDDER PRESSURE SW. LEAK AND OPS CHECK SAT. PERFORMED PITOT TEST. NO FURTHER DEFECTS NOTED.SDR J7SA2023031300352Unknown · unknownDIVERTED DUE TO GROUND SPOILER FAIL, PITCH TRIM NORMAL FAIL, NUMBER 2 SHED BUS OFF IN FLIGHT WHILE CLIMBING THROUGH 36,000FT. AIRCRAFT LANDED WITHOUT INCIDENT AT KATL. REPLACED FAILED #2 FLIGHT CONTROL ELECTRONICS UNIT. PREFORMED RIGGING OF MULTIFUNCTION SPOILSDR CALA2023030900667Indicator · inoperativeFLAPS WOULD NOT DELOY PAST 1/ALT FLAPS USED PHOTOS ADDED. LEFT TRAILING EDGE INDICATOR NEEDLE LAGS BEHIND RIGHT INDICATOR REPLACED TRAILING EDGE FLAP POSITION INDICATOR. OPERATION NOW THE FLAP LOCKOUT REPORT FOR THE EVENT IN DFD INDICATES THAT THE ADDING DFDSDR 7C7A2023030400015Solenoid Valve · failedROLL SPLR OUTBD CAUTION LIGHT ILLUMINATED AFTER SELECTING "FLIGHT" OUTBD ROLL SPOILERS REMAINED DOWN AT IDLE WITH "FLIGHT" SELECTED. R/R R/H #1 ROLL SPOILER LIFT DUMP SOLENOID VALVE.SDR CALA2023030300622Sensor · noneLE FLAP TRANSIT LIGHT ILLUMINATED OVERHEAD SLAT 1 LIGHT OFF REQUEST MEL 2704K.#1 SLAT INDICATION PROBLEM. LEADING EDGE FLAP INDICATIONS NORMAL, APPLYING MEL 2704K FOR #1 TRUE. WOULD BITE CHECK FSEU TO CONFIRM FULL EXTEND/RETRACT COMPARE RESISTANCE VALUES WITH SDR CALA2023030300605Fastener · missingPDA 3 REPORTED BY RAMP. #6 CANOE FAIRING HAS SEVERAL FASTENERS MISSING. ADDED PHOTO. REPLACED 4 EACH SCREWS ON #6 FLAP TRACK FAIRING TAIL CONE. REF IPC 27-51-18-01. ITEM 435.SDR UIEA2023022000138Rivet · noneNO.5 FLAP TRACK CANOE FAIRING DRIVE LINK RIVETS FOUND LOOSE.(<P>LOOSE RIVETS REPLACEMENT AS PER ATLAS AIR EO NO.4427A040 REV.9 PART 1 AND CMM 27-51-93.</P>)SDR NACA2023022700001None · noneLH OUTBOARD LEADING EDGE FLAP DAMAGED AT THROUGH HOLE FOR THE EXHAUST GATE CONTROL ROD. C/W INTERIM REPAIR TO LH MID OB FLAP LEADING EDGE @ WBL 205. INSTALL PERMANENT REPAIR OR REPLACE FLAP SECTION AT NEXT C CHECK.SDR CALA2023022700570Speed Brake · noneSPEED BRAKE DO NOT ARM LIGHT ILLUMINATED WHEN THRUST LEVERS WERE ADVANECED FOR TAKEOFF UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V939727 FIM 27-62- TASK 802. ORTIZ, FABIO (V939727) PLEASE CONTACT TOMC BEFORE COMMENSDR CALA2023022700565Flap System · noneTE FLAP DISAGEE LANDED FLAPS 20 FOUND ALT. FLAPS SET AT 20 AND TE & LE SWITCHES PUSH IN, RESET IT TO NORMAL, AND PERFORMED TASK 27-51-00-715-001 OPS CHECK GOODSDR J7SA2023030600001None · noneRUDDER FAIL CAS ON SHORT FINAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUDDER REMOTE ELECTRONICS UNIT 16. PERFORMED SUCCESSFUL RUDDER ACTUATING SYSTEM IBIT SUITE A TEST. PERFORMED SUCCESSFUL RUDDER FUNCTIONAL TEST. CLOSED LEFT AND RIGHT VERTICAL STABILSDR CALA2023022200499Flap Track · noneLEFT WING TRAILING EDGE INBOARD FLAP OUTBOARD UNDER SIDE T OR NE AR #3 FLAP TRACK HAS A REPAIR COMPOSITE IN NATURE 4" X 8". TRANS CRIBED FROM HAECO GSO NR 9284831 REPAIRED L/W T/E I/B MAIN FLAP LOWER SURFACE NOTED AREA IAW B757 -200 SRM 57-53-01-2R-1, 51-70-10SDR CALA2023022000494Computer · inoperativeSPD LIM SHOWS CAPTAIN'S SPD LIM FLAG CA SIDE. PERFORMED FIM 27-32 TASK 831. FOUND HISTORY OF FMC FAILURE. CURRENT FAULTS ON CAPT AOA. HISTORY FAULTS ON SMYD -1. REPLACED SMYD -1. REPLACED L/H AOA. REPLACED CAPTAINS FMC. CROSS LOADED SOFTWARE. ALL OPERATION CHSDR CALA2023022000487Module · faultyFL350 NORMAL CRUISE.. FLAP INDICATE POS 1 HANDLEUP.VISUALLY CONF IR MED UP. FLAP/SLAT ELEC T/S AS PER FIM TASK REF. 27-51 FAULT TREE 836. FOUND RIGHT FLAP REMAINS FULLY CAT CAPABLE. PARTS USED: 1444363,QTY :1 STABILIZER POSITION MODULE FAULTY. R & R FSPM AS PSDR CALA2023021600467Transmitter · inoperativeAHM: * TRAILING EDGE FLAP BYPASS VALVE ACTIVATION * DUE TO RECENT FLAP LOCKOUTS WITH ''DFD'' REPORT 272 SHOWING ON EXTENSION LT FLAP POSITION LAGGING, ( L/P 3843624 ) AND REFERENCING UAL BEST PRACTICES, SL 27-266, 27-196 PLZ REPLACE THE L FLAP POS X-MITTER & FSDR IPXA2023041195092Unknown · crackedDURING ACCOMPLISHMENT OF EO #86006-REQ1 STEPS 1,2,AND 3 FOUND TOP CHORD AFT END OF R/H STAB TIP CRACKED INSTALLED NEW NUT PLATES AND INSTALLED NEW T CHORD PER SRM 51-40-02SDR CALA2023021600443Rvdt · noneON APPROACH GOT TE FLAP DISAGREE WHEN ATTEPTING TO MOVE FLAPS F ROM 1 TO 5 PERFORMED BITE OF FSEU GOT MESSAGE NUMBER27-81041 L/E OUTBD PDU RVDT REQUIRES MORE T/S PARTS USED: 64-2781-3-0320,QTY :1 76-2781-3-0173,QTY :1 T/S IRW FIM 27-51 TASK 809. FOUND FAULT SDR IXXA2023021501Bracket · cracked#6 SLAT LEADING EDGE SUPPORT BRACKET CRACKED.SDR CALA2023021400442Flap System · inoperativeFLAPS DO NOT OPERATE WITH PRIMARY CONTROL EXTENDED NORMAL TO 5 WOULD NOT MOVE PAST 5 DEG. IN NRML MODE AL TERNATE WORKED OK REF FIM 27-51 TASK 801 FSEU BITE PROCEDURE GOT MSG 27-51427 SHOW,THEN THERE WAS AN INTERMITTENT FAULT.NO FURTHER FLAP LEVER .REF TASK SDR CALA2023021300422Unknown · noneREF AIR RETURN #10 SPOILER. MESSAGES 27-12833 AND 27-17771. #10 SPOILER SHOWS NO DATA ON MAINTENANCE PAGES AND SYNOPTIC PAGE. SPOILER UP IN FLT AND UPON LANDING. REMOVED SPOILER ELECTRIC MOTOR CONTROLLER UNIT REF ACP INTERFACE INSP OF # 10 SPOILER EMCU. VERIFSDR OEJA202302100001Transducer · intermittentON DEPARTURE, THIS MORNING THE AUTO PILOT KICKED OFF 3 TIMES THEN WORKED FINE. THE APPROACHING INTO DR WE HAD A RUDDER BOOST FAIL LIGHT FOLLOWED BY A YAW DAMP DISENGAGE. WE RESET THE YAW DAMPER AND THEN IT KICKED OUT AGAIN MULTIPLE TIMES. CONTINUED APPROACHSDR CALA2023021000394Transmission · trippedTE FLAP DISAGREE BITE SFEU 1,2,3 REF FIM 27-51 TREE 805. SFEU 1,2&3 SHOWED NO EXISTING FAULTS. SFEU1 FAULT HISTORY LEG 0 REPORTED MSG # 305. SFEU2 FAULT HISTORY LEG 0 REPORTED MSG# 327. SFEU3 HAD NO FAULT HISTORY FOR LOG 0. TROUBLESHOT LH SIDE OF FLAP SYSTEM ISDR CALA2023021000376Connector · burnedLE SLAT ASYM MSG DISPLAYED IN CRUISE. REPLACED CONNECTOR D41396P REF WDM 27-81-31-2 AND SWPM 20-61-11. CLEANED D41396J, VERIFIED NO CONTAMINATION OR DAMAGE PRESENT. PERFORMED OPS CHECK NO FAULTS FOUND.SDR TAMF20230210031Computer · fault messageAFTER TAKE-OFF FROM THE AIRPORT (PTY), THE FAULT MESSAGE “F/CTL SLAT SYS 2 FAULT” WAS SHOWN IN THE ECAM DISPLAY AND BY FACILITIES OF MAINTENANCE AND PARTS STOCK IT WAS DECIDED TO DIRECT THE AIRCRAFT TO THE MAIN BASE (MDE) AND NOT (LIM) AS IT WAS SCHEDULED.
THSDR CALA2023020800372Flap · not reportedLE FLAPS TRANSIT AMBER LIGHT ON ON APPROACH REF AMM 27-88-11-700-801, PERFORMED L/E FLAP/SLAT PROX SENSOR 27-88-11-400-802 PERFORMED GAP CLEARANCE CHECK OF L/E EXTEND TEST, TEST PASSED SENSOR NEAR/FAR INDICATIONS AND FLIGHT DECK PROX SENSORS FOUND WITHIN LIMITSDR 2023F00049Unknown · unknownAFTER TAKEOFF LE FALPS ASYM TRAILING EDGE FLAPS BETWEEN UP AND 1°. CORRECTIVE ACTION: PERFORMED FIM 27-81 FAULT TREE 809 STEP 1,2,3,4,5,11 AND WAS CLEANED CONNECTORS OUTER PDU SLAT IAW AMM 20-60-06 BITE FSEU OK.SDR ANCF20230602002Spoiler · not reportedPILOT REPORT:
03.FEB.2023 WO 17'034'722=> DURING CLIMB SPOILERS ANNUNCIATION APPEARS
DURING CLIMB SPOILERS ANNUNCIATION APPEARS
ACTIONS TAKEN:
03.FEB.2023 WO 17'034'722=> THIS ITEM IS DEFERRED TO DMI WO 17034722 MEL 27-61-02-01 CAT C MAINTENANCE PROCEDURSDR 2023FA0000063Flap · crackedDURING ROUTINE MX, NOTED THE RIGHT FLAP TRAILING EDGE UNDER THE ENGINE PYLON TO BE CRACKED AND SEPARATED ALONG THE TRAILING EDGE BEND RADIUS FOR APPROX 9" WITH 2 PROPAGATING CRACKS RUNNING FORWARD INTO THE AIRSTREAM.SDR 2023F00099Spoiler · failedSPOILERS WITH FAULT FRM276 461 00SDR 2023F00098Spoiler · failedSPOILERS WITH FAULT FRM276 461 00SDR DALA2023020300859Not Entered · not enteredSHIP 8127 - DIV - TO LIT DUE TO "R ELEVATOR FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED #3 REU. (LP# 9432468)SDR CALA2023020300311Module · not enteredSELECTED FLAPS ONE. GOT TRAILING EDGE DISAGREE. QRH RUN. UNEVENT FUL LANDING. REPLACED FLAP STAB MODULE.PARTS USED:76-2754-9-0001,QTY :1ROTABLE PARTS CHANGE WAS INDICATED - TT # 1147533 SN OFF 2812 FIM TASK 27-51 FAULT TREE 810 ACTIONED, FSEU BITE TEST SHOWED SDR CALA2023020100291Indicator · noneFLAPS DO NOT OPERATE WITH PRIMARY CONTROL TRAILING EDGE FLAPS DID NOT DEPLOY. PERFORMED ALT EXTENSION WAS SMOOTH, NO INDICATION OF FLAP LEVER MALFUNCTION. F/O STATES THAT CREW MOVED FLAP LEVER TO POSITION 1 AND NO HYDRAULIC ISSUES OR INDICATIONS. MAINTENANCE SDR 2023FA0000067Not Reported · not reportedAILERON DOES NOT GO BACK TO NEUTRAL LEFT & RIGHT FRM 271 060 48SDR 2023F00081Unknown · unknownMESSAGE "AFCS FAULT" EVERY TIME CAPTAIN MAKES FLIGHT CONTROLS CHECKSDR DALA2023012300512Fseu · faultedDECLARED EMERGENCY INTO ATL DUE TO PILOT REPORT OF TE FLAP AND LE SLAT DISAGREE. CORRECTIVE ACTION: PERFORMED FSEU BITE CHECK. FOUND FAULT CODE 27-51333 MULTIPLE LEGS. REPLACED FSEU OPS CHECKS GOOD. (9881802)SDR CALA2023011100092Flap · stuckON APP..FLAPS STUCK AT 5 AFFTR SLCTNG FLAP 10. BROKE OFF APP RAN FL DISAGREE CKLST..OPS NRML FRM THERE PERFORMED FSEU BITE PROCEDURE. BITE SHOWED NO EXISTING FAULTS AND NO FAULT HISTORY. CHECK DFD REPORT NONE NOTED, OPS CHECK FLAP DRIVE SYSTEM GOOD OK FOR FLIGSDR QXEA2023010800003Unknown · unknownAT CLEARED FOR TAKEOFF WITH TOGA POWER APPLIED, FO, AS PILOT FLYING, APPLIED FULL LEFT RUDDER PEDAL WITH NO A/C RESPONSE. WE REJECTED TAKEOFF BELOW 30 KTS WITH NO EICAS INDICATIONS. RETURNED TO THE GATE. FO MENTIONED THAT HE MIGHT HAVE INADVERTENTLY DISCONNECTSDR CALA2022122803516Yaw Damper · inoperativeREJECT AT 50 KTS DUE TO L YAW DAMPER.. FOLLOWED BY L GEN OFF HA PPENED TWICE RESET YAW DAMPER AND GEN FIELD YAW DAMPER OPS NORMAL PER AMM 22-21-00-715-001-002.SDR CALA2022122803515Warning Light · false activationFEEL DIFF PRESS LIGHT LIGHT ON ON APPROX 300FEET AFTER TAKEOFF. OFF SOMETIME AFTER LANDING BEFO RE BLOCKIN PERFORMED FIM 27-31 TASK 815, FOUND BOTH LEFT AND RIGHT RESTRICTOR VALVES CLOGGED. CLEANED AND RE-INSTALLED BOTH. PERFORMED OPERATIONAL AND LEAK CHECKS WSDR CALA2022122103462Transmitter · inoperativeFLAPS TRAILING EDGE FLAP LOCKOUT ON APROACH LOG PAGE LOCKED DUE TO CREW DECLARING EMERGENCY WORKING PERFORMED FSEU BITE AND FOUND MSG: 27-52260. T/S REF FIM 27-51 TASK 820. REMOVED AND REPLACED R/H FLAP TRANSMITTER REF AMM 27-58-01. CYCLED FLAPS SEVERAL TIMES,SDR GTIA2023011236873Computer · faultedF/CTL ELAC 1 AND 2 FAULT ALTERNATE LAW FOLLOWED BY DIRECT LAW-PERFORMED EFCS GND SCAN IAW TSM 27-40-00-810-802A AND TSM 27-40-00-804A. NO FAULTS DETECTED . PERFORMED OPS CHECK OF THS AND EFCS SYSTEM IAW AMM 27-96-00 OPS CHECK GOOD NO DEFECTS NOTED A/C GOOD FORSDR DALA2022121908202Computer · degradedSHIP 8110 - ATB - DUE TO PRIMARY FLIGHT CONTROL COMPUTERS 2 AND 3 DEGRADED. ALONG WITH PRIMARY POWER CONTROL UNIT INOP. REMOVED AND REPLACED #1 AFT REU.SDR AALA202212166396Switch · pilot errorAIRCRAFT WAS GROUNDED: ON DEPARTURE CAPTAIN AND FIRST OFFICER COULD NOT TRIM NOSE DOWN WITH SWITCHES TRIM, WHEEL WORKED FINE. FOUND TRIM GUARD SWITCHED IN OFF POSITION. ACCOMPLISHED FIM 27-41-00. NO FAULTS NOTEDSDR VQMA202212130001Flap System · faultedAIRCRAFT EXPERIENCED A FLAP FAILURE AND INDICATION WHILE ON APPROACH TO SLC TO DEN DUE TO A FLAP FAILURE. THE AIRCRAFT ABORTED APPROACH IN ORDER TO GO AROUND AND RUN CHECKLISTS. THE FLAP FAILURE COULD NOT BE RESOLVED BY CHECKLIST SO AN EMERGENCY WAS DECLAREDSDR DALA2022121208001Computer · failedSHIP 3121 - ATO - AT 65 KTS DUE TO A ELAC 1 PITCH FAULT. CORRECTIVE ACTION: REPLACED ELAC 1. (9715176)SDR HNAA2022120700315Actuator · damagedGUST LOCK WOULD NOT UNLOCK ON RUNWAY. PERFORMED ELECTRICAL RESET, FOUND GUST LOCK TO OPERATE NORMALLY. PERFORMED GUST LOCK OPS CHECK IAW AMM 27-70-00. OPS CHECK SATISFACTORY, ACFT OK FOR SERVICE. ACCESSED SOLENOID UNDER GUST LOCK LEVER MANUALLY DEPRESSED SOSDR DALA2022120107692Bushing · worn(LOG 2515226) DURING INSPECTION WEAR WAS FOUND ON RH INBD BUSHING OF UPPER JACKSCREW FITTING AT AFT ACCESORY COMPARTMENT. BUSHINGS OF UPPER JACKSCREW FITTING WAS REPLACED PER SOPM 20-50-03.SDR YENA2022112801163Computer · failedFLT#714, FLL-HPN. (AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO JFK) ' FTL/CTL SEC 1 FAULT COULD NOT RESET IN FLIGHT; PER TSM 27-94-00-810-860A, REMOVED ADN REPLACED SEC 1 COMPUTER IAW AMM 27-94-34 AND PERFORMED DUAL IDLE ENG RUN IAW AMM 71-00-00. OPS CHECK
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