JASC 2761
Service difficulty reports · 1,071
Reports filed under 2761 · Drag Control Actuator, 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 = '2761' 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 = '2761' 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 HNAA2011112100394Actuator · crackedNR 1 HYD ISOLATION LIGHT ILLUMINATED ALONG WITH INBD ROLL SPOILER HYD CAUTION LIGHT. NR 1 HYD QUANTITY AT 1.1. FOUND BACK SIDE OF ACTUATOR CRACKED. R & R SPOILER ACTUATOR IAW MM 27-14-05. PERFORMED OPS CHECK IAW AMM 27-14-00. LEAKED CHECKED GOOD.SDR UALA2011112106342Actuator · out of adjustSPOILER EICAS MSG CAME ON IN CRUISE. CHECK RVDT ADJUSTMENT AND RIG ADJUSTMENT ON NR 4 SPOILER. CHECKED RVDT ADJUSTMENT AND ADJUSTED. CHECKED RIG ON SPOILER AND ADJUSTED NR 4 SPOILER. OP CHECKED GOOD.SDR UALA2011111606285Actuator · faultyEICAS MESSAGE 'SPOILERS' DISPLAYED. SPOILERS LIGHT ILLUMINATED WITH SPEEDBRAKE LEVER SELECTED TO DOWN. DEFERRED REF MEL 2761A LOCKED OUT SPOILERS 4 AND 9. FOUND NR 4 PCA RVDT OUT OF RANGE, WITH NO RESPONSE WHEN TRYING TO MAKE AN ADJUSTMENT. NEED TO REPLACESDR CA111027001Actuator · leaking(CAN) HYD SYS 2 FAILURE. AS A PRECAUTION, CREW DECLARED EMERGENCY DUE LONG LANDING ROLL AND LIMITED STEERING ON INVESTIGATION FOUND NR 5 MFS BROKEN. LT NR 5 MFS REPLACED AMM 27-65-01.SDR KPVA201112Actuator · crackedNR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY LOSS OF ALL HYDRAULIC FLUID IN NR 2 QUANTITY SYSTEM. MAINTENANCE REPLACED THE LT OUTBOARD SPOILER ACTUATOR DUE TO CRACKED HOUSING.SDR UALA2011102405754Actuator · defectiveON LANDING AUTOSPEED BRAKES ONLY DEPLOYED PARTIALLY 50 PERCENT. NO TIME. REPLACED AUTOSPEED BRAKE ACTUATOR & K217 & K218 RELAYS. OPS CHECKS NORMAL.SDR CA111004003Actuator · cracked(CAN) THE ACFT LOST ALL OF THEIR NR 1 HYD SYS FLUID IN THE CLIMB, THEY RETURNED TO THE DEPARTURE AIRPORT. MX INVESTIGATION FOUND THAT THE HOUSING OF THE RT INBD ROLL SPOILER ACTUATOR WAS FRACTURED AND WAS THE CAUSE OF THE LOSS OF FLUID. THE ROLL SPOILER ACTUASDR CA110927005Actuator · inoperative(CAN) REF: DEFECT-1013434, LT OTBD ROLL SPOILER WAS NOT MOVING ON THE PFCS AND CONFIRM VISUALLY NOT TO BE MOVING. LP 624597, DURING PRE FLIGHT CHECK, THE LT OTBD SPOILER WAS NOTED AS NOT MOVING ON PFCS AND VISUALLY CONFIRMED. ALL OTHER FLT CONTROLS NORMAL. HSDR SWAA116588Attach Fitting · crackedDURING SCHEDULED HC1 CHECK, FOUND LT WING I/B GROUND SPOILER O/B ACTUATOR ATTACH FITTING ON PANEL CRACKED. REMOVED AND REPLACED SPOILER PER MM.SDR UALA2011091404978Servo Valve · leakingNR 2 SPOILER ACTUATOR LEAKING. REPLACED NR 2 SPOILER ELECTRO SERVO VALVE & GASKET PLATE PER MM, LEAK CHECKS OKAY.SDR SAJF20110910001Warning Message · illuminated(B-18202) DURING ROLL TAXING, MESSAGE: "CONFIG SPOILER" ILLUMINATED, CREW ABORTED TAKEOFF AT 40 KTS, CREW CHECKED SPOILER & SPEED BRAKE HANDLE POSITION AND FOUND NORMAL, MESSAGE EXTINGUISHED. CREW DECIDED TO CONTINUE FLT. AFTER ACFT ARRIVED, SPOILER CONTROL SYSDR UALA2011082904635Actuator · malfunctionedSPOILER 13 MSG 27-10512. DUE TO BOEING AHM REPORTING 'FLIGHT CONTROL SYS' STATUS MESSAGE WITH CORRELATED MMSG 27-10512, REF FIM 27-61 TASK 812. ACCMP'D CONNECTOR CHECK, NO DAMAGE OR CONTAMINATION FOUND, OMED SPLR PCU EHV AND SPLR POSN XDCR PER, CHECKS OKAY.SDR CA110825001Actuator · failed(CAN) ACFT EXPERIENCED A ROLL SPOILER THAT FAILED TO EXTEND. ADDITIONALLY, THERE WAS A LOSS OF HYD FLUID. INVESTIGATION REVEALED ROLL SPOILER ACTUATOR PISTON CAP SEPARATION. ACTUATOR WAS REPLACED AND FUNCTION CHECK ACCOMPLISHED.SDR SWAA115749Actuator · brokenRT WING NR 5 GROUND SPOILER O/B ACTUATOR LOWER MOUNTING TAB BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.SDR AALA20110804TUL06Fitting · crackedCRACK IN OUTBOARD, FORWARD RADIUS OF LEFT GROUND SPOILER CASTING. REMOVED AND REPLACED GROUND SPOILER ACTUATOR FITTING PER SRM 51-30-05.SDR REXA201100473Pcu · failedCREW DECLARED AN EMERGENCY ON APPROACH TO ATL LEFT O/B SPOILERON FAILED MASTER CAUTION ALONG WITH OTHER SPOILER RELATED MESSAGES. REMOVED AND REPLACED RIGHT O/B SPOILER PCU IAW CRJ 900 AMM 27-62-01.SDR KPVA201107Mount Bracket · crackedLEFT OUTBOARD SPOILER ACTUATOR BRACKET CRACKED. REPLACED WITH POST MOD P/N 8570558-001.SDR SWAA115179Actuator · crackedDURING SCHEDULED MV1 CHECK, FOUND LT WING I/B GROUND SPOILER I/B ACTUATOR CRACKED. REMOVED AND REPLACED GROUND SPOILER ACTUATOR PER MM.SDR K11A2011090772203Support Fitting · crackedSPOILER ACTUATOR I/B SUPPORT FITTING CRACKED, 1X3 INCHES.SDR UALA2011071303508Actuator · leakingHYD FLUID ON BOTTOM SURFACE OF LEFT WING. OPERATED FLAPS AND SPEED BRAKES, NO LEAKAGE NOTED. CLEANED AREA AND CARRY FORWARD WITH RECHECK WITHIN 75 FLIGHT HOURS PER MM. FOUND AREA WET WITH HYD FLUID, CLEANED AREA. OPERATED HYD SYSTEMS IN AREA ON ACTIVE LEAKSDR XV6A2011070100011Actuator · leakingAIR TURNBACK: LOSS OF SYSTEM "A" HYDRAULIC FLUID. FOUND SEALS LEAKING AT NR 6 SPOILER ACTUATOR. O-RINGS (P/N NAS1612-12) REPLACED IAW BOEING CMM 27-60-41. LEAK AND OPS CHECK NORMAL. NOTE: PART IS "ON CONDITION" THEREFORE TIMES AND CYCLES ARE NOT TRACKED.SDR CA110610010Actuator · crackedHYD LEAK WAS NOTED FROM THE LT SIDE WING NACELLE AREA DURING ENGINE START UP. UPON CLOSER INSP AFTER ENGINE SHUTDOWN, IT WAS CONFIRMED TO BE COMING OFF THE LT OTBD SPOILER ACTUATOR. THE HSG ON THE ACTUATOR WAS FOUND CRACKED. ACTUATOR REPLACED, ACFT GROUND RSDR KPVA201106Actuator · crackedNR 2 HYD ISO VLV (CAUTION) LIGHT ILLUMINATED WITH FLUID LOSS IN NR 2 HYDRAULIC SYSTEM. FLIGHT CREW DECLARED EMERGENCY, DIVERTED TO HNL AND USED ALTERNATE EXTENSION. MAINTENANCE DISCOVERED THE LT OUTBOARD SPOILER ACTUATOR HOUSING FAILED (CRACKED) AND REPLACESDR CA110607005Actuator · failed(CAN) ON TAKEOFF (AT ABOUT 50 IN THE CLIMB) THE LT INBD ROLL SPOILER DEPLOYED UN-COMMANDED. PASSING THROUGH 1500 IT RETRACTED. THE ACFT RETURNED TO THE BASE WITH NO FURTHER ISSUES. THE LT INBD ROLL SPOILER ACTUATOR WAS FOUND AT FAULT AND WAS REPLACED. SPOISDR UALA2011052302501Actuator · leakingLEFT SYSTEM HYD QTY LOW. PRESSURIZED LEFT SYSTEM. FOUND RIGHT WING OUTBOARD SPOILER ACTUATOR LEAKING. REPLACED SPOILER NR 12. NO LEAKS NOTED.SDR SAJFCALS100014Actuator · malfunctioned(B-18609) "SPEED BRAKE DO NOT ARM" LT ILLUMINATED WHEN ACFT ROLLING AT SPD 90 KTS. ACFT ABORTED TAKEOFF AT SPD 100 KTS AND THEN RETURNED TO GATE. AUTOSTOW ACTUATOR REPLACED IAW AMM 27-62-33 AND TEST NML. PERFORM AMM 05-51-07 HIGH ENERGY STOP/HEAT DAMAGE CONDISDR CA110504007Actuator · leaking(CAN) FLIGHT EXPERIENCED A GRADUAL FAILURE OF HYD SYS 1 AND DETECTED HYD FLUID SMELL IN THE COCKPIT FLIGHT DIVERTED AND DECLARED AN EMERGENCY FOUND NR 3 MF, 12H, SPOILER ACTUATOR LEAKING, REPLACED RT NR 3MF SPOILER ACTUATOR IAW AMM 27-65-01-00801A CARRIED OUT SDR SWAA113174Actuator · brokenDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER O/B ACTUATOR FWD ATTACH LUG BROKEN. REMOVED AND REPLACED ACTUATOR PER MM.SDR UALA2011040101569Actuator · faultyAUTO SPEEDBRAKE FAILURE OF AUTO SPEEDBRAKE LEVER ACTUATOR OR AUTO SPEEDBRAKE SYSTEM. STATUS MSG01- LATCHED ROLL OUT MODE DEPENDENT; AUTO SPEEDBRAKE ACTUATOR IS NOT IN COMMANDED POSITION. DB- PRIMARY FLIGHT COMPUTER (LEFT) MSG-2710600 LATCHD RO MODE. CB'S ONSDR COZA20110331004Actuator · leakingDURING INSPECTION, THE NR 8 FLIGHT SPOILER ACTUATOR WAS FOUND STATICALLY LEAKING FROM THE INPUT LINKAGE ASSEMBLY. THE FLIGHT SPOILER WAS OPERATED WITH NO CHANGE TO THE LEAK RATE. THE ACTUATOR WAS REPLACED AND OPERATIONALLY CHECKED WITH NO LEAKS FOUND. THERESDR CA110315012Actuator · damaged(CAN) NR 1 SYSTEM HYDRAULIC DEPLETING DURING TAXI OUT. RT INBOARD ROLL SPOILER ACTUATOR FOUND TO HAVE MAJOR FAILURE. ACTUATOR REMOVED AND AREA CLEANED. ACTUATOR SECURED WITH BOLTS AND TORQUED. FUNCTION CHECKS IN PROGRESS.SDR AALA20110220TUL04Actuator · leakingSDQ - INFLIGHT PAP-MIA. CREW REPORTED CENTER HYDRAULIC SYSTEM FAILED INFLIGHT. FLAPS WOULD ONLY EXTEND TO 1 DEGREE. EMERGENCY DECLARED FLIGHT DIVERTED SDQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 9 SPOILER ACTUATOR LEAKING AT BLSDR CA110221003Actuator · crackedDURING A WALK AROUND, A HYD LEAK WAS NOTICED FROM THE LT WING. ENGINEERING FOUND THE LT OTBD SPOILER ACTUATOR LEAKING FROM THE ACTUATOR HSG, HSG THREADS HAD FRACTURED ABOUT THE CYLINDER END CAP OF THE ACTUATOR. THE ACTUATOR WAS SUBSEQUENTLY REPLACED BY A SERVSDR COZA20110308002O-Ring · defectiveHYDRAULIC SYSTEM-B FLUID LOSS. UPON LANDING, THE CREW REPORTED A SIGNIFICANT DECREASE SYSTEM-B HYDRAULIC QUANTITY AND FLUID ON THE AFT FUSELAGE AND RIGHT INBOARD FLAP, ESPECIALLY THE NUMBER SIX FLAP CANOE. SUBSEQUENT INVESTIGATION ON THE GROUND COULD NOT POSISDR CA110124006Actuator · failedFLIGHT CREW REPORTED THAT DURING APPROACH A FLIGHT SPOILER PANEL REMAINED DEPLOYED WITH ASSOCIATED ACFT ROLL. THE AUTOPILOT WAS DISCONNECTED AND THE REMAINDER OF THE APPROACH WAS HAND FLOWN. AFTER LANDING IT WAS CONFIRMED THE NR 1 SPOILER PANEL ON THE LT SISDR CA110125021Control Module · unserviceable(CAN) DURING APPROACH A FLIGHT SPOILER PANEL REMAINED DEPLOYED WITH ASSOCIATED AIRCRAFT ROLL. THE AUTOPILOT WAS DISCONNECTED AND THE REMAINDER OF THE APPROACH WAS HAND FLOWN. AFTER LANDING IT WAS CONFIRMED THE ONE SPOILER PANEL ON THE LEFT SIDE WAS STILL DEPLOSDR UALA2011012000343O-Ring · leakingL/E SLATS WILL NOT REACTIVATE. FOUND NR1 SPOILER POWER CONTROL ACTUATOR LEAKING HYD FLUIDS. REPLACED LEAKING O-RING ON ACTUATOR PLUG-BLEEDER. L/E SLAT BYPASS VALVE RED LEVER WHEN MOVED OUT OF POSITION (2) DOES NOT RETURN ELECTRICALLY TO ORIGINAL POSITION. RSDR UALA2011012000342O-Ring · leakingFOUND NR1 SPOILER POWER CONTROL ACTUATOR, LEAKING HYD FLUIDS. REPLACED LEAKING O-RING ON ACTUATOR PLUG-BLEEDER.SDR SWAA110060Actuator · brokenON LANDING, AFTER MAIN GEAR STRUT COMPRESS AND BEFORE NOSE GEAR TOUCH DOWN, THE AIRCRAFT ROLLS/ PULLS LEFT. REMOVED AND REPLACED BOTH NR 5 GROUND SPOILER ACTUATORS PER MM.SDR ERAA201100001Actuator · fracturedON LANDING PILOT REPORTED TWO CAUTION LIGHTS, NR 1 HYD ISO VLV AND ROLL SPLR INBD HYD AND LOSS OF BRAKING. MAINTENANCE FOUND RIGHT, INBOARD ROLL SPOILER ACTUATOR HOUSING FRACTURED AROUND END CAP LEADING TO LOSS OF NR 1 HYDRAULIC SYSTEM FLUID. TOTAL TIME AND CSDR UALA2010122704716Actuator · malfunctionedSPOILERS EICAS MESSAGE ON DESCENT WHEN SPOILER HANDLE IN USE INFLIGHT. FOUND "PCA 7 FAULT" DISPLAYED ON 3 LT SPOILER CONTROL MODULE M532, TYPE: INTERMIT, PHASE: DESCENT. DID NOT CLEAR MODULE MEMORY. SPOILER 6 AND 7 ARE LOCKED OUT IN THE DOWN POSITION. PERFSDR UALA2010122704708Actuator · bypassingFOUND NR 12 SPOILER BYPASSING. REF VIBRATION WITH FLAPS 5. REMOVED NR 12 SPOILER PCA, REPLACED NR 12 SPOILER PCA.SDR UALA2010122004647Pca · malfunctionedSPOILERS EICAS MSG FAULT IS HITTING PCA FOR MOD 1R. REPLACED SCM. NO HELP STILL HITTING PCA ON 1R SUSPECT THE PCA ON RT SIDE AS WHEN DOING OPS CHECK ALWAYS FAILS WHEN TURNING CONTROL WHEEL TO RT SIDE. REINSTALLED OLD SCM FAULT IS ON FLT SPOILERS 2 OR 11. RESDR HALA10121600588AActuator · malfunctionedAFTER ENG START SPOILERS EICAS REMAINED ON. PERFORMED BITE CK ON SPOILER SYS CONTROLLER & FOUND PCA 9 SPOILER FAULT. REMOVED & REPLACED NR 9 OTBD SPOILER ACTUATOR IAW AMM27-61-02 PERFORMED OPS CK & LEAK CHECK. NO DEFECTS NOTED.SDR CA101223006Rod End · separated(CAN) DURING OVERNIGHT ROUTINE MAINTENANCE AND TROUBLESHOOTING AN OPEN MEL ITEM FOR NR 2 & 3 SPOILER FAULT THAT WAS PLACED ON MEL (SYSTEM DEACTIVATED) PRIOR TO AIRCRAFT ARRIVAL, MAINTENANCE DISCOVERED THE NR 2 RT SPOILER ACTUATOR THREADED ROD END ASSEMBLY HAD SDR UALA2010112904359Actuator · faultySPOILERS EICAS AND OVERHEAD LIGHT ON. SPOILER CONTROL MODULE 3L HAS PCA FAULT, SPOILERS NR 4 AND NR 9 PER FIM. COMPLIED WITH MEL 2761A, DL8057 CREATED TO MONITOR. REPLACED NR 4 GRD SPOILER ACTUATOR PER MM, OPS TEST GOOD.SDR SWAA107150Actuator · leakingIN CRUISE FLIGHT HYDRAULIC B QUANTITY DECREASED. "B" ENGINE DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED FLIGHT SPOILER ACTUATOR PER MM.SDR CA101115012Control Unit · failed(CAN) CREW REPORTED THAT AT FL60 THE AMBER (FLT SPOILER FAULT) AND THE CYAN (STAB TRIM FAULT) MSGS ILLUMINATED. GROUND SPOILERS DID NOT DEPLOY ON LANDING. CREW HAD TO USE EMERGENCY MODE TO DEPLOY THEM.SDR UALA2010110504103Actuator · leakingSPOILERS FAILURE OF ONE OR MORE SPOILER PAIRS. ADVISORY MSG01-LATCHED DESCENT MODE DEPENDENT; SPOILER POWER CONTROL UNIT (4) DOES NOT FOLLOW COMMAND. DB- PRIMARY FLIGHT COMPUTER (RIGHT) MSG-2710503 LATCHD DC MODE. NR 4 SPOILER PCA FAULTING AND LEAKAGE INTOSDR UALA2010110104040Actuator · bypassingOPERATED HYD & TURNED CONTROL WHEEL LEFT, CAN FEEL SHUTTER, VIBRATION IN COCKPIT AIRFRAME, CONTROL WHEEL & FROM INBD AILERON TO OTBD AILERON WHILE IT STILL HELD IN LT TURN. ISOLATED TO CTR HYD SYS. NO VIB IN RT & LT HYD SYS ON. RT WING AILERON OK NO VIBS. I
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