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 20010406CW002Housing · crackedHOUSING IS CRACKED.SDR 20010406CW006Housing · crackedHOUSING IS CRACKED AND BROKEN AT THE BEARING MOUNT LUG. OVERSTRESSED, FATIGUE, AND OR POSSIBLE FLAW IN HOUSING DESIGN.SDR CA010308012Actuator · leaking(CAN) AT APPROXIMATELY 20 MINUTES OUT, THE A SYSTEM HYDRAULIC LIGHT ILLUMINATED. THE HYDRAULIC FLUID GAUGE WAS CHECKED AND FOUND TO BE EMPTY. THE USE OF ALTERNATE FLAP AND GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE FIRE DEPARTMENT WSDR 20010323CW009Housing · crackedTHE THREADED AREA OF THE HOUSING ASSEMBLY IS CRACKED. OVERSTRESSING OF THE HOUSING IN THE LOCKED POSITION.SDR 20010315CW003Housing · crackedHOUSING IS CRACKED NEXT TO THE EXTEND PORT.SDR 20010315CW002Housing · crackedHOUSING ASSEMBLY IS CRACKED AROUND THE NUT FLANGE AREA. FATIGUED, OVERSTRESSED.SDR SWAA010394Actuator · brokenDURING SCHEDULED 1/4D CHECK, FOUND NR 5 GROUND SPOILER OUTBOARD ACTUATOR ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.SDR AWXA0001261O-Ring · crackedPHX - AIR TURNBACK - 1/31/01 - AFTER DEPARTURE FROM PHX THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY AND THE AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND A UNION ON THE NR 5 INBOARD GROUND SPOILER ACTUATOR LEAKING, CRACKED. THESDR AWXA0001257Actuator · leakingPHX- EMERGENCY LANDING, FLIGHT CREW HAD ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL. AN UNEVENTFUL LANDING WAS MADE. IN PHX MAINTENANCE FOUND THE RT NR 2 SPOILER SERVO CONTROL LEAKING. THE SERVO CONTROL WAS REPLACED AND THE YELLOW HYDRAULIC SYSTEM SESDR GAIA01010OPRod End · brokenFLT 2018 - MHR-SEA - ON DESCENT, THE FLIGHT CREW OBSERVED THAT ON SPEED BRAKE DEPLOYMENT THE AIRCRAFT ROLLED TO THE LEFT. A UNEVENTFUL LANDING WAS MADE AT SEA. INVESTIGATION REVEALED THAT THE NR 10 SPOILER ACTUATOR ROD END WAS BROKEN. THE NR 10 SPOILER ROD SDR CA010105006Housing · broken(CAN) DURING INSPECTION, 17C CHECK OF NR 4 GROUND SPOILER, SPOILER FOUND TO BE LOOSE. FOUND NR 4 SPOILER ACTUATOR, BODY END THAT ENCLOSED THE BEARING, BROKEN AWAY. ACTUATOR REPLACED AS PER WORK CARD 51160.SDR COMA0061084Control Unit · failedSPOILER FAULT CAUTION DURING CRUISE FLIGHT. RESET THE SPOILER ELECTRONIC CONTROL UNITS.SDR 20010125CW015Housing · crackedHOUSING IS CRACKED AT THE EXTERIOR OF THE RETRACT PORT. PROBABLE CAUSE OVERSTRESSED, FATIGUE, AND OR POSSIBLE FLAW IN HOUSING DESIGN.SDR 20010126CW008Housing · brokenHOUSING IS BROKEN AT THE BEARING LUG.PROBABLE CAUSE: STRESS, FATIGUE AND OR HIGH TIME ON UNIT.SDR 20010126CW007Housing · brokenHOUSING IS BROKEN AT THE BEARING LUG.PROBABLE CAUSE: STRESS, FATIGUE AND OR HIGH TIME ON UNIT.SDR 20010126CW006Housing · crackedHOUSING IS CRACKED BELOW THE RETRACT PORT. PROBABLE CAUSE: STRESS AND OR FATIGUE.SDR AU001218Bolt · missing(AUS) NT 4 SPOILER ACTUATOR ROD END BOLT / NUT / BUSHING MISSING.SDR USAASB00342O-Ring · cutBWI - FLT 2718 - AS FLIGHT LEVELED OFF AT FL170, EN ROUTE TO FLL, CREW LOST ALL FLUID AND PRESSURE IN A-SYSTEM HYDRAULICS. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND TURNED OFF BOTH A-SYSTEM HYDRAULIC PUMPS WITHIN ONE MINUTE FROM LOW PRESSURE LIGHTSDR CA001211017Pcu · failed(CAN) THE FLIGHT CREW REPORT THAT WHILE DEPLOYING THE FLIGHT SPOILERS AT FL90, THE LT FLIGHT SPOILER DEPLOYED, THE RT FLIGHT SPOILER DID NOT DEPLOY. THE RT FLIGHT SPOILER CAUTION MESSAGE APPEARED. THE CREW THEN RETRACTED THE FLIGHT SPOILER. THE MAINTENANCE CRESDR SWAA002413Rod · brokenAIR TURNBACK - DURING TAKEOFF, RECEIVED T/O CONFIG WARNING, GEAR HANDLE WOULD NOT RETRACT AND A/C WOULD NOT PRESSURIZE. MX FERRY TO PHX. REMOVED AND REPLACED SPOILER INTERLOCK VALVE ROD ASSY PER MM.SDR USAASB00308Actuator · leakingCLT - FLT 1975 - ON DESCENT INTO CLT, FROM ROC, SYSTEM A HYDRAULIC QUANTITY DROPPED TO ONE-THIRD. FLUID WAS NOTICED ON TOP OF THE LEFT WING. CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED NORMALLY TO THE GATE. MAINTENANCE JACSDR CA010112016Actuator · cracked(CAN) A REPORTED HYDRAULIC LEAK WAS FOUND TO BE CAUSED BY A CRACKED ROLL SPOILER BODY. UNIT REPLACED WITH NEW ACTUATOR AND AIRCRAFT RETURNED TO SERVICE.SDR DL72L001965Actuator · looseAT HMV THE NR 3 SPOILER ACTUATOR WAS FOUND TO HAVE LOOSE MOUNT BOLTS ON BOTTOM ATTACHED TO REAR SPAR. REPAIRED PER MM 57-42-0.SDR USAASB00284Actuator · leakingEWR - FLT 2636 - EN ROUTE FROM PBI TO LGA, CAPTAIN NOTICED THAT SYSTEM A HYDRAULIC QUANTITY HAD DECREASED FROM 2.2 GALLONS TO 1.2 GALLONS. ON DESCENT TO LGA, AS AIRCRAFT SLOWED AND FLAPS WERE EXTENDED, HYDRAULIC QUANTITY WENT TO .5 GALLONS. CREW WAS ABLE TO SDR CA001024008Control Unit · failed(CAN) AFTER TAKEOFF A FLIGHT SPOILERS FAULT STATUS MESSAGE APPEARED ON ED2. THE MAINTENANCE REPLACED THE SECU NR 2 AND THE LEFT FLIGHT SPOILER OUTBOARD PCU (P/N: 27000-3, S/N: MAL.3438).SDR TWAA0013501Rod · brokenCREW REPORTED SPOILER I/B FAIL MESSAGE. FOUND THE RIGHT I/B SPOILER HOLD DOWN ACTUATOR ROD END BROKEN. REPLACED PER M99-27-02. NO CHECK-C.SDR 20000911SH007Housing · crackedHOUSING IS CRACKED NEXT TO LOWER BEARING MOUNTING FLANGE. FATIGUE, STRESS AND/OR POSSIBLY HIGH TSN/TSO. (X)SDR CALA0001204Actuator · burnedBOTH CREW MEMBERS NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT DURING CLIMB OUT OF TPA. CREW WAS UNABLE TO ISOLATE THE SOURCE AND THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO SPOILER ACTUATOR IN FORWARD PEDSDR UPS00233514Connector · looseINSPECTION TYPE:N/A, DURING CLIMB AT FL 180 ORANGE LED LIGHT CAME ON NR 4 LED WAS OUT. SELECTED FLAP 2 DEGREE, NO GREEN LIGHT. RETRACTED FLAPS AND LIGHT EXTINGUISHED. SHORTLY THEREAFTER AMBER LIGHT ILLUM, 4-5 MIN LATER LIGHT EXTINGUISHED. AFTER CREW DEBRIESDR AWXA0000495Actuator · leakingEMERGENCY DECLARED, ON DESCENT FLIGHT SPOILERS WERE DEPLOYED ECAM MSG SPOILER FAULT FOLLOWED BY HYDRAULIC Y ENGINE 2 PUMP LOW PRESSURE. REPLACED LT WING SPOILER ACTUATOR, RIGGED, ADJUSTED AND OPS CHECKED GOOD.SDR DL738001309Limit Switch · failedON LANDING AFTER AUTO SPOILERS DEPLOYMENT, AUTO SPOILERS MOTOR CONTINUES TO RUN EVEN THOUGH SPOILERS ARE FULLY DEPLOYED. BURNING ELECTRICAL SMELL IS PRESENT AFTER MANUAL STOW MOTOR DISENGAGES. REPLACED AUTO SPOILER ACTUATOR.SDR P2EA00210Actuator · unserviceableFLT 414 - MDW - FOUND LOST A SYSTEM HYDRAULIC PRESSURE AND QUANTITY WHILE TAXING TO GATE. REMOVED AND REPLACED THE NR 1 GROUND SPOILER ACTUATOR PER BOEING MM 27-62-10. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (M)SDR CA000706007Actuator · failed(CAN) LT ROLL SPOILER SLOW TO FULLY EXTEND ON LANDING. LT OUTBOARD ROLL SPOILER ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR AU000515Housing · cracked(AUS) LT INBOARD GROUND SPOILER OUTBOARD ACTUATOR HOUSING CRACKED.SDR DL72S001139Actuator · looseAT HMV, THE NR 2 SPOILER ACTUATOR WAS FOUND LOOSE AT LWR FWD AND SUPPORT FIXTURE LOOSE AT LWR ATTACH POINTS. SPOILER ACTUATOR REPLACED ON ROUTINE OP 7053 RC 494. RESECURED LWR ATTACH POINTS OF SUPPORT FIXTURE.SDR JBU000001Actuator · leakingJFK/FLL - FLT 11 - AIR TURN BACK TO JFK DUE HYDRAULIC YELLOW RESERVOIR LOW LEVEL ON ECAM. ON INSPECTION, FOUND RT WING NR 4 SPOILER ACTUATOR LEAKING. REMOVED NR 4 SPOILER ACTUATOR REF AMM 27-64-51, INSTALLED SPOILER ACTUATOR PER AMM 27-64-51, OPS CHECK AND LSDR DL76L000845Cap · leakingDIVERTED TO FRA DUE TO C SYSTEM HYDRAULIC LEAK. FOUND NUMBER 3 SPOILER ACTUATOR FINGER FILTER CAP LEAKING. REPLACED CAP SEAL.SDR TWAA0006307Casting · crackedDURING CHECK-C MAINT, THE LT WING FWD END OF GROUND SPOILER ATTACH CASTING WAS CRACKED BOTH I/B AND O/B SIDE OF ACT ATTACH FWD END. STOP DRILLED CRACKS PER SRO 9570010-5. INSTALLED DOUBLER FILLER AND STIFFENER PER SRO 9570010-5, FIG 6 PAGE 45-62.SDR TWAA0006306Actuator · crackedDURING CHECK-C MAINT, THE RT WING FWD END OF GROUND SPOILER ACTUATOR ATTACH CASTING WAS CRACKED I/B AND O/B SIDE AT FWD END, PER BOEING DAC SB 57-180 VIEW DD CONDITION 4. ACCOM HIGH FREQ EDDY CURRENT PER TWA NDT 51-00-01 PART 6 FOR CRACK CONTAINMENT. STOP DRSDR DL72S000758Actuator · leakingLOSS OF SYSTEM A HYDRAULIC IN FLIGHT. INITIAL 0 QTY INDICATION WITH NO OTHER ABNORMALS. THEN SYS A ENG 1 AND 2 PUMPS FLICKERED AND RECOVERED SEVERAL TIMES. POM PROCEDURES FOR LOSS OF SYS A COMPLIED WITH. LANDED JFKL AND TOWED TO GATE. ZERO QTY INDICATION SDR 20000609AP002Actuator · leakingON TAKEOFF ROLL, A SYSTEM QUANTITY RAPIDLY DECREASED AND HELD STEADY AT 1.8 GALLONS HYD SYSTEM B CONTINUOUSLY DECREASED TO O QUANTITY WHEN B SYSTEM HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. AOM PROCEDURES ACCOMPLISHED, DIVERTED TO MIAMI, NO FUEL DUMPED. FOUNDSDR SPAA0000018Actuator · crackedFLIGHT 214 IFP-SAT AFTER LANDING, DURING TAXI TO GATE, AIRCRAFT EXPERIENCED LOSS OF HYDRAULIC FLUID. IT WAS DETERMINED THAT THE NR 8 GROUND SPOILER ACTUATOR HOUSING HAD CRACKED AT THE PISTON END. THE ACTUATOR WAS REPLACED PER BOEING MM 27-62-101. HYDRAULSDR SWAA000663Actuator · leakingDURING FLIGHT @ 28000 FEET, LOST A-SYS HYDRAULICS. R&R NR 3 FLIGHT SPOILER ACTUATOR DUE TO LEAK.SDR 20000501SH021Housing · crackedHOUSING IS CRACKED AT THE EXTERIOR OF THE RETRACT PORT. OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DESIGN. (X)SDR 20000501SH028Piston · crackedPISTON IS CRACKED IN THE KEYWAY. WEAK POINT, FATIGUE. (X)SDR CA000410014Nut · loose(CAN) REPORTS OF IN-FLIGHT VIBRATION LED THROUGH ONGOING TROUBLESHOOTING TO THE DISCOVERY OF SEVERAL LOOSE ROD ENDS TO PISTON JAM NUTS. JAM NUTS TORQUED AND VIBRATION DISAPPEARED. OPERATOR IS INVESTIGATING WITH OWNER REGARDING PREVIOUS MAINTENANCE PERFORMED ISDR CA000320006Actuator · failed(CAN) RIGHT OUTBOARD ROLL SPOILER ACTUATOR LEAKING HYDRAULIC FLUID DUE TO O-RING. O-RING REPLACED.SDR USAASB00062O-Ring · failedBWI - FLT 2635 - DURING CRUISE, EN ROUTE FROM BOS TO FLL, FLIGHT LOST SYSTEM A HYDRAULICS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE. SDR UPS00232250Fitting · corrodedINSPECTION TYPE:C, CORROSION ON NR 2 SPOILER ACTUATOR FITTING AROUND SPOILER PANEL HINGE BOLTS. REPLACED NR 2 SPOILER ACTUATOR FITTING PER MM 27-61-81 AND MM 27-51-131.SDR COMA0060234Pcu · malfunctionedCONFIG SPOILER WARNING DURING TAKEOFF. REPLACED THE LEFT FLIGHT SPOILER PCU.
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