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 SCNA00020Actuator · malfunctionedCREW OBSERVED TAKEOFF WARNING HORN AT THE BEGINNING OF THE TAKEOFF ROLL. REJECTED TAKEOFF, FOUND ACTUATOR FOR S867 (SPEED BRAKE WARNING SWITCH) OUT OF ADJUSTMENT. READJUSTED ACTUATOR AND PERFORMED TAKEOFF WARNING. CHECKED GOOD PER MM 31260. NO FURTHER PROBSDR 20000502SH005Housing · crackedHOUSING HAS A STRESS CRACK IN THE CYLINDER BORE. POSSIBLE CAUSE: OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING. (X)SDR CA000224003Fitting · cracked(CAN) HYDRAULIC LEAK IN VICINITY OF NR 4 FLAP TRACK LED TO REPLACEMENT OF TEE FITTING DUE TO CRACK.SDR 2000UALA00082Position Switch · out of rig''L/E SLAT ASSM'' EICAS WITH FLAPS SELECTED UP, FLAP POS IND, SHOWED BETWEEN 0 & 1. RTF. *S/D* SLAT MOVEMENT WAS INHIBITED BY THE FLAP/SLAT ELECT UNIT (FSEU) WHEN IT RECEIVED A SLAT POSITION LOGIC SIGNAL FROM THE PROXIMITY SWITCH ELECT UNIT (PSEU) INDICATINSDR DL72L000352Actuator · leakingLOST B HYDRAULIC SYSTEM PRESS AND FLUID IN FLIGHT. MADE UNSCHEDULED LANDING. FOUND NUMBER 3 SPOILER ACTUATOR LEAKING. REPLACED NR 3 SPOILER ACTUATOR.SDR 20000501SH045Housing · crackedHOUSING HAS A STRESS CRACK IN THE CYLINDER BORE. POSSIBLE CAUSE: OVERSTRESSED, WEAK POINT IN HOUSING FROM CASTING PROCESS AND/OR POSSIBLY HIGH HOURS ON THE UNIT. (X)SDR 20000501SH043Housing · crackedHOUSING HAS A STRESS CRACK IN THE CYLINDER BORE. POSSIBLE CAUSE: OVERSTRESSED, WEAK POINT IN HOUSING FROM CASTING PROCESS AND/OR POSSIBLY HIGH HOURS ON THE UNIT. (X)SDR ABXA000140Fitting · crackedDURING C-CHECK, FOUND LEFT WING INBOARD SPOILER ACTUATOR TORQUE TUBE CENTER MOUNT ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05.SDR CA000215042Actuator · broken(CAN) LEFT O/B ROLL SPOILER NOT DEPLOYING/ STAYED DOWN WITH CONTROL INPUT. MAINTENANCE DISCOVERED SUBSTANTIAL HYD LEAK FROM THE LEFT O/B ROLL SPOILER ACTUATOR. THE ACCESS COVER FOR THE INTERNAL PISTON ON THE ACTUATOR ITSELF HAD BROKEN OFF ALLOWING FLUID TO BYPSDR IXXA0000003Actuator · defectiveTOL - FLT 823 - DURING LANDING IN TOL, WHEN THE SPOILERS WERE DEPLOYED THE FLIGHT CREW SIGHTED SMOKE EMITTING FROM THE CENTER PEDESTAL. MAINTENANCE INSPECTED THE PEDESTAL AREA WHICH REVEALED THE AUTOMATIC SPOILER ACTUATOR DEFECTIVE. MAINTENANCE PLACED THE SYSDR 20000406SH005Piston · crackedPISTON IS CRACKED NI THE KEYWAY. (X)SDR 20000406SH004Piston · crackedPISTON IS CRACKED IN THE KEYWAY. FATIGUE/OVERSTRESSED. (X)SDR DL72S000227Bolt · looseAT MV2 FOUND NR 11 SPOILER ACT MOUNT BOX LOOSE, LWR I/B BOLT. REMOVED BOLT AND REPAIRED HOLE PER MM 57-42-0.SDR DL72S000226Mount · looseAT MV2 FOUND NR 12 SPOILER ACT MOUNT BOX LOOSE, LWR MOUNTS. REMOVED I/B AND O/B LWR FITTING BOLTS. O/B LWR HOLE WITHIN LIMITS PER MM 57-42-0. INSTALLED LWR BOLT PER SAME, REPAIRED I/B LWR BOLT PER MM 57-42-0.SDR AU000059Housing · cracked(AUS) LH GROUND SPOILER OUTBOARD ACTUATOR HOUSING CRACKED.SDR CA000209052Panel · broken(CAN) FLIGHT SPOILER DEPLOY MESSAGE, NO SPOILER DEPLOYED ON APPROACH TO WASHINGTON WHEN FLAPS SELECTED AT 45 DEG. A/C ROLLED SHARPLY RIGHT WING DOWN, MANUAL FLIGHT LANDED WITH 30 DEG FLAP. FOUND RIGHT HAND SPOILER PANEL I/B POWER CONTROL ACTUATOR ATTACH HINGE SDR CA000118015Switch · contaminated(CAN) THE CREW REJECTED TAKEOFF DUE TO AN INBOARD ROLL SPOILER CAUTION LIGHT. MAINTENANCE FOUND THE POWER LEVER MICROSWITCHES WERE CONTAMINATED. THE SWITCHES AND ACTUATORS WERE CLEANED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR TWAA0000501Actuator · wornAFTER TAKEOFF AT GEAR RETRACTION CAPTAIN NOTED SPARKS COMING FROM CENTER PEDESTAL NEAR HIS RIGHT FOOT. ALSO, NOTICED A BURNING SMELL. FLIGHT RETURNED TO ATL. FOUND THE GROUND SPOILER ACT HAD FAILED. PLACARDED THE ACT PER MEL FOR LATER REPLACEMENT. CHECK-CSDR CA000118036Housing · cracked(CAN) THE FLIGHT CREW REPORTED THAT THE LEFT OUTBOARD ROLL SPOILER DID NOT DEPLOY DURING LANDING. MAINTENANCE FOUND THAT THE SPOILER ACTUATOR WAS LEAKING FROM A CRACK IN THE HOUSING AT THE PRESSURE INLET FITTING.SDR 2000ZZZX194Housing · leakingHOUSING HAS A PINHOLE NEXT TO THE PORT. OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DEESIGN.SDR CA000110087Actuator · leaking(CAN) GREEN HYD SYS QUANTITY DROPPED TO ZERO, 1 & 4 PUMPS SHUT OFF AND ALTERNATE GEAR SELECTION CARRIED OUT. INVESTIGATION REVEALED NR 5 RT SPOILER SERVO ACTUATOR LEAKING.SDR 2000ZZZX188Housing · crackedHOUSING IS CRACKED ON SIDE OPPOSITE OF PORTS. OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DESIGN.SDR UPS99531163Actuator · leakingPILOT REPORT, CENTER HYD QTY LOSS IN FLIGHT. REMOVED AND REPLACED NR 1 SPOILER ACTUATOR.SDR CA991116016Pcu · leaking(CAN) NR 1 HYDRAULIC SYSTEM WAS LOSING FLUID ON EICAS, UP TO 10 PERCENT AFTER TOUCH DOWN. RIGHT INBOARD SPOILER PCU LEAKING BETWEEN THE TORQUE MOTOR AND VALVE BODY.SDR 99ZZZX4646Actuator Housing · crackedHOUSING IS CRACKED ON SIDE OPPOSITE OF PORTS. OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DESIGN.SDR CA991209052Actuator · leaking(CAN) AFTER TAKEOFF, SUBSTANTIAL RIGHT AILERON INPUT WAS REQUIRED TO KEEP THE AIRCRAFT LEVEL. MAINTENANCE FOUND THE RIGHT HAND SPOILER ACTUATOR TO HAVE AN INTERNAL LEAK. THE SPOILER ACTUATOR WAS REPLACED AND A TEST FLIGHT WAS CARRIED OUT.SDR 99ZZZX4325Restrictor · failedSPOILERS ACTUATED IN THE FAST MODE IN BOTH 'AIT' AND 'GROUND AUTO' POSITIONS. IN-FLIGHT ACTIVATION CAUSED FAST ACTUATION AND SUDDEN ALTITUDE LOSS. DETERMINED THAT RESTRICTOR THAT WAS INSTALLED PER SABRELINER S.O.K. 81-5 HAD FAILED INTERNALLY AND ALLOWED FLUISDR CA991028036Actuator · jammed(CAN) CREW HAD A SPOILER JAM INDICATION ON THE GROUND. THE CREW CONFIRMED THAT BOTH LEFT ROLL SPOILERS WERE JAMMED UP. ACTUATOR REPLACED.SDR DL733992265Actuator · crackedAFTER LANDING, LOST HYD SYS A GROUND PERSONNEL REPORTED LEAK RT WING AREA. FOUND NR 8 GROUND SPOILER ACT LEAKING, REPLACED SAME. .SDR CA991027025Actuator · leaking(CAN) HYDRAULIC LEAK WAS DISCOVERED IN THE AREA OF THE LEFT OUTBOARD ROLL SPOILER ACTUATOR. LINE REPLACED.SDR AWXA9900346Actuator · failedAIR TURNBACK, AIRFRAME VIBRATION, LOG 7555408, ON CLIMB-OUT OF MCI, AFTER FLAPS RETRACTED AND ACCELERATION THROUGH FL230, STARTED FEELING VIBRATION THROUGHOUT A/C. DID NOT GO AWAY AFTER PWR REDUCTION ON EACH ENGINE. TROUBLESHOT AND RSDR 99ZZZM804Actuator · failedABRUPT LEFT ROLL WHEN SPEED BRAKES APPLIED. B-SYSTEM OFF, NO ROLL. A-SYSTEM OFF, ABRUPT LEFT ROLL. LANDED WITHOUT INCIDENT. FOUND THE NR 14 SPOILER ACTUATOR BYPASSING. REPLACED ACTUATOR IAW MM 27-61-81, OPS CHECKED NORMAL, LEAK CHECKED OK. (M)SDR CA991007094Actuator · cracked(CAN) DURING PRE-FLIGHT, PILOTS NOTICED THAT ROLL SPOILERS WOULD NOT STOW WITH INBOARD, OUTBOARD FAILURE INDICATION AND NO HYDRAULIC FLUID IN NR 2 SYSTEM. INVESTIGATION REVEALED THE HOUSING FOR THE ROLL SPOILER ACTUATOR WAS CRACKED COMPLETELY AROUND ITS CIRCUSDR 99ZZZX4064Housing · crackedINNER BORE OF HOUSING IS CRACKED IN TWO LOCATIONS POSSIBLY DUE TO FATIGUE.SDR UIEA99081Fitting · crackedDURING ROUTINE INSPECTION, FOUND NR 6 SUPPORT ACTUATOR SUPPORT FITTING CRACKED ON SPOILER SUPPORT BEAM. REPLACED SUPPORT FITTING PER SRM 51-30-02. (M)SDR DL72E992139Actuator · looseAT HV2, FOUND NR 13 SPOILER ACTUATOR MOUNT BOX IS LOOSE AT LOWER MOUNT BOLTS 2, I/B MOUNT POINT IS MISSING SHIMS. SHIMS REPAIRED PER MM 57-42-0.SDR UPS99230561Actuator · failedINSPECTION TYPE:N/A, ON HIGH SPEED CLIMB PROFILE 340 FLTS A/C REQUIRED 10 DEG RIGHT AILERON INPUT. A/C TRIMMED IAW AOM PROCEDURE. LEFT RUDDER TRIM 1/4 TURN AILERON TRIM 1/2 TURN. A/C LANDED FLAPS 30 AT 140 KNOTS WITH 20 DEG RIGHT AILERON REQUIRED TO KEEP WISDR ABXA9900650Actuator · corrodedDURING C-CHECK, FOUND LEFT OUTBOARD SPOILER ACTUATOR VALVE BODY EXFOLIATED AND VALVE LINK MOUNT AREA CRACKED. REPLACED ACTUATOR IAW ABX EA 2760D019-001.SDR SWAA991334Casting · crackedDURING SCHEDULED 1/4D CHECK, FOUND CRACKED CASTING FOR NR 4 GROUND SPOILER ACTUATOR ATTACH FITTING. REPAIRED CASTING PER SWA RA NR 1-A57-0571.SDR TWAA9910401Plug · failedABOUT 15 MINUTES INTO FLIGHT LOST B HYDRAULIC SYSTEM FLUID. RETURNED TO STL. THE NUMBER 5 SPOILER PLUG BLEW OUT OF THE ACTUATOR. REPLACED THE PLUG. CHECK-C 12-13-98 MCI.SDR RAIA990731Actuator · failedDCA - FLT 7740 - SPOILER WILL NOT DEPLOY. MAINTENANCE REPLACED SPOILER ACTUATOR ON RT SIDE. (X)SDR 99ZZZX3013Housing · crackedHOUSING IS BROKEN ACROSS THE BEARING MOUNTING LUG. HOUSING OVERSTRESSED, HIGH TOTAL TIME HOURS.SDR SCNA99086Actuator · failedDURING DESCENT, CREW OBSERVED 'A' SYSTEM HYDRAULIC FAILURE. HYDRAULIC QUANTITY AND PRESSURE READ ZERO. ALL COM PROCEDURES WERE COMPLIED WITH AND LANDING WAS UNREMARKABLE. INSPECTED AND FOUND A BLOWN O-RING ON THE NR 2 ACTUATOR FOR THE SPOILER. REMOVED AND RSDR DHL9970221CFitting · crackedC CHECK NR 6 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED AT TOP FLANGE. CUT OUT DAMAGED AREAS I/B AND O/B SIDE OF NR 6 SPOILER ACT FITTING IAW AVITAS ENG. REPAIR ORDER NR 99AVHM .045R0-1 REV 1R SIZE OF CUT OUT 1 BY 1.5. EDDY CURRENT PER B727 NDT MAN. PART 6SDR 99ZZZM782Pcu · malfunctionedDEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, FIRST OFFICER INITIATED A RIGHT TURN TO FINAL COURSE. AILERON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS OF FORCE. CAPTAIN ASSDR 99ZZZM385Actuator · malfunctionedDEN - ON FINAL APPROACH, AT ABOUT 8,000 FT AND 10 MILES OUT, F/O INITIATED A RIGHT TURN TO FINAL COURSE. AILERON CONTROL BECAME EXTREMELY STIFF AND FIRST OFFICER COULD NOT ROLL AIRCRAFT OUT OF THE TURN, EVEN USING APPROX 80 LBS OF FORCE. CAPTAIN ASSISTED F/O SDR SWAA990766Actuator · leakingAIR TURNBACK, MASTER CAUTION HYDRAULIC, AND BOTH ENGINE DRIVEN PUMPS LOW PRESSURE LIGHTS CAME ON AT ROTATION. BRAKE ENERGY APPROX 18 FOOT POUNDS AFTER LANDING. FOUND NR 6 FLIGHT SPOILER ACTUATOR LEAKING (BLOWN SEAL). REMOVED AND REPLACED ACTUATOR PER MM.SDR VTZA990040Actuator · failedFLT 7370 - ILM-IAD - DURING LANDING, AIRCRAFT LEFT SPOILER CAP WAS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT SPOILER ACTUATOR. OPS CHECK GOOD. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (M)SDR DHL9970169DBracket · crackedAT D-CHECK, RT WING O/B BRACKET CRACKED AT MLG BEAM PANEL AND NR 8 SPOILER ACTUATOR BRACKET. FABRICATED NEW BRACKET SUPPORT PER SRM 57-20-1, 9 X 5.SDR EISA99070Support · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK-CARD, FOUND CRACK AT NR 13 SPOILER ACTUATOR INBOARD SUPPORT ANGLE ON REAR SPAR. REMOVED CRACKED SUPPORT AND FABRICATED NEW PAR PER SRM 51-10-1. INSTALLED SUPPORT PER SRM 51-10-1 AND 51-30-2. (M)
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