JASC 2760
Service difficulty reports · 3,503
Reports filed under 2760 · Drag 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 = '2760' 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 = '2760' 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 TC8A98037Control Cable · brokenDURING FLIGHT CONTROL CHECK, NO SPOILER PRESSURE DROP ON AILERON CHECK WHEN CHECKING THE LEFT SIDE. FOUND LT OUTBD SPOILER RETRACT CABLE BROKEN. REPLACED CABLE AND TEST/ADJ AS PER MM 2736-0.SDR COMA9860170Secu · failedFLIGHT SPOILERS CAUTION MESSAGE. REPLACED THE NR 2 SECU.SDR COMA9860160Secu · malfunctionDURING TAKEOFF, CONFIG WARNING, SPOILERONS CAUTION MESSAGE. REPLACED THE NR 1 SECU.SDR CA980713019Line · leaking(CAN) ON WALK-AROUND, THE PILOT NOTED HYDRAULIC FLUID LEAKING FROM THE RIGHT HAND WING TRAILING EDGE. INVESTIGATION FOUND A PIN HOLE IN THE HYDRAULIC LINE FOR THE INBOARD ROLL SPOILER.SDR COMA9860150Bushing · missingC-CHECK INSPECTION, RIGHT HAND WING INBOARD FLIGHT SPOILER, PCU HINGE BUSHING IS MISSING. REPLACED MISSING BUSHING.SDR CA980616010Tube · leaking(CAN) NR 1 HYDRAULIC QUANTITY LOW. FOUND A LEAK ON A HYDRAULIC LINE GOING TO THE ROLL SPOILER ACTUATOR. PART TC: 25,786.SDR CKSA98338Mechanism · out of adjustFLIGHT CONTROLS ACT LIKE THEY ARE IN MANUAL REVERSION AT AIRSPEED GREATER THAN 230 KCAS. UNCOMMANDED ROLL TO THE LEFT OCCURS. DURING DESCENT AIRSPEED BELOW 230 KCAS SYSTEM OPERATES NORMALLY. ADJUSTED L-3 AND L-4 SPOILER PANELS IAW DACO MM 27-61-1, OPS CHECKSDR CA980602086Fitting · leaking(CAN) HYDRAULIC LEAK FOUND IN THE RIGHT HAND WHEEL WELL. FITTING ON SPOILER LIFT DUMP LINE FOUND LEAKING.SDR AU980989Brake · malfunctioned(AUS) RIGHT WING TIP BRAKE UNIT FAULTY. SUSPECT DUE TO MOISTURE INGRESS.SDR CA980602016Rod · bent(CAN) BINDING OF SPOILER CONTROL REPORTED. IT WAS FOUND THAT THE INPUT ROD FOR THROTTLE INTERLOCK WAS BENT AND INTERFERING ON THE CROSS SHAFT.SDR ABXA9800331Fitting · crackedDURING C-CHECK, FOUND THE RIGHT INBOARD SPOILER TORQUE TUBE CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-10-4.SDR AU980656Slat · jammed(AUS) WING SLATS JAMMED. INVESTIGATION FOUND LT WING TIP BRAKE VERY TIGHT IN OPERATION. PART TC: 5,190.SDR CA980406009Sensor · contaminated(CAN) ON TAXI, THE MANUAL SPOILER CAUTION LIGHT CAME ON. WOW SENSORS CLEANED AND FAULT CLEARED.SDR ORJA9860Warning · activatedABORTED TAKEOFF DUE TO SPOILER DEPLOYED ANNUNCIATION ON OAP. ASSIGNED TO DMI NR 13132 REF TO LOP PAGE 156711. SPOILER SYSTEM OPS CHECK NORMAL IAW MM 27-60-00. NO DISCREPANCIES NOTED CLEARS DMI NR 13132. (M)SDR UPS98226211Casting · wornINSPECTION TYPE-C, NR 9 GROUND SPOILER (ACTUATOR) CASTING HAS EXCESSIVE PLAY AT HINGE POINT. REPLACED ACTUATOR CASTING IAW MM 27-61-91.SDR UPS98226210Rod End · wornINSPECTION TYPE-C, NR 7 GROUND SPOILER CASTING AND ACTUATOR ROD END HAS EXCESSIVE PLAY. REPLACED SPOILER CASTING IAW MM 27-62-81 AND REPLACED ACTUATOR ROD END IAW OHM 27-60-01.SDR UPS98226209Rod End · wornINSPECTION TYPE-C, NR 6 GROUND SPOILER CASTING AND LINKAGE HAS EXCESSIVE PLAY. REPLACED WORN ACTUATOR CASTING LINKAGE ROD END AND BOLT IAW MM 27-6 2-81.SDR CA980311017Line · pin hole(CAN) HYDRAULIC LINE AT LEFT HAND SPOILER OUTBOARD ACTUATOR HAD A PIN HOLE LEAK AT THE BEND AT THE ACTUATOR. HYDRAULIC FLUID HAD FLOWED TO THE LEFT NACELLE GIVING AN INDICATION OF A FORWARD MLG DOOR ACTUATOR LEAK.SDR CA980313007Line · leaking(CAN) CREW REPORTED FUEL LEAK AROUND THE NR 1 MLG WHEEL WELL. INVESTIGATION FOUND A CRACKED HYDRAULIC LINE AT THE INBOARD ROLL SPOILER ACTUATOR.SDR CA980311015Tube · pin hole(CAN) HYDRAULIC LEAK NR 1 SIDE AT OUTBOARD SPOILER ACTUATOR. HYDRAULIC FLUID HAD FLOWED TOWARDS THE NACELLE AND LEAKED ON THE MAIN WHEEL GIVING THE IMPRESSION THAT THE MID-DOOR ACTUATOR WAS LEAKING.SDR P5CA9800412Cable Cover · crackedMAIN DECK LT STA 1250 SIDEWALL UPPER CONTROL CABLE PULLEY METAL COVER FOUND MOUNTING BRACKET CRACK AND DEFORMED. MOUNTING BRACKET REPLACED AS PER SRM 51-10-01 AND SPEED BRAKE CABLE RIGGING CHECKED PER MM 27-62-02.SDR AU980173Control Cable · worn(AUS) WING FLIGHT SPOILER CABLES WORN BEYOND LIMITS. CABLES LOCATED ATTHE FOLLOWING POSITIONS IN THE LH WING AT STN230LH:-1. CABLE PNO BACC2C3D02794EG AT WSB1-32. CABLE PNO BACC2C3D03216FG AT WSB2-33. CABLE PNO BACC2C3D02428EG AT WSA1-34. CABLE PNO BACC2C3D018SDR CA980317007Press Tube · leaking(CAN) DURING WALK-AROUND, NR 1 SYSTEM HYDRAULIC QUANTITY LOW. HYDRAULIC FLUID LEAKING FROM WING ROOT AREA. ROLL SPOILER PRESSURE LINE LEAKING.SDR M8XA9800002Indication · malfunctionedCREW REPORTED THAT THEY RECEIVED NO VISUAL EICAS INDICATION THAT THE GROUND SPOILERS WERE ARMED AFTER THE CONDITION LEVERS WERE ADVANCED TO THE TAKEOFF POSITION. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. CONTRACT MAINTENANCE PERFORMED GROUND SPOISDR VJ9800067Bracket · corrodedRT OUTBOARD SPOILER PULLEY BRACKET CORRODED. REPLACED BRACKET IAW DC9 MM 27-60-0.SDR CALA9800197Crank Assy · crackedTHE AUTO SPOILERS WOULD NOT DEPLOY WHEN REVERSE THRUST WAS SELECTED. MAINTENANCE FOUND A 1 INCH CRACK IN THE AUTO SPOILER CRANK ASSEMBLY. THE CRANK ASSEMBLY WAS REPLACED IAW MM 27-62-01.SDR AU980533Control Cable · frayed(AUS) WING FLIGHT SPOILER CABLES CONTAINED BROKEN STRANDS IN THE AREA ADJACENT TO PULLEY AT STN 230: LT WS B1-3, P/N BACC2A3A02794EG. WS B2-3, P/N BACC2A3A03216FG. WS A2-3, P/N BACC2A3A01853FG. WS A1-3, P/N BACC2A3A02428EG. RT WS B1-4, P/N BACC2A3A02625FGSDR AU980179Control Cable · frayed(AUS) WING FLIGHT SPOILER CABLES FRAYED AT WING STN 230:- 1. CABLE PNO BACC2A3A03216FG LOCATED AT LH WSB2-3 2. CABLE PNO BACC2A3A02794EG LOCATED AT LH WSB1-3 3. CABLE PNO BACC2A3A03051FG LOCATED AT RH WSB2-4 FOUND DURING SPECIAL INSPECTION IAW B737-3-97A.SDR 9801376305Control Mech · out of adjustDURING TAKEOFF, RECEIVED A SPOILER CONFIGURATION TAKEOFF WARNING. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED THE SPEED BRAKE CONTROL SYSTEM AND REPLACED THE AUTO SPEED BRAKE ACTUATOR, OPERATIONAL CHECK GOOD.SDR AU980171Control Cable · worn(AUS) WING FLIGHT SPOILER CABLE LOCATED RH SIDE AT WSB2-4 AT WS136 PULLEY WORN BEYOND LIMITS. FOUND DURING SPECIAL INSPECTIONB737-3-97A.SDR AU980052Control Cable · frayed(AUS) FLIGHT SPOILER CABLES (3OFF) LOCATED IN RH WING ADJACENT TO STN 230 CONTAINED BROKEN STRANDS. FOUND DURING INSPECTION IAW SPECIAL INSPECTION B737/3/97A.SDR AU980170Control Cable · damaged(AUS) WING FLIGHT SPOILER CABLES FRAYED. CABLES LOCATED IN THE FOLLOWING POSITIONS:- 1. CABLE PNO BACC2A3A02794EG AT LH WSB1-3 2. CABLE PNO BACC2A3A03216FG AT LH WSB2-3 3. CABLE PNO BACC2A3A03051FG AT RH WSB2-4 4. CABLE PNO BACC2A3A02652FG AT RH WSB1-3 FOUND DSDR JBXA980031Spoiler · malfunctionedRDU - FLT 448 - WHILE DEPARTING RDU FOR ALT CAPTAIN ABORTED TAKEOFF, AT 100 KTS DURING TAKEOFF ROLL A LIFT DUMPER FAULT WAS ANNUNCIATED ON THE LEFT MFDU. ASSIGNED TO DMI D04842 PER MEL 27-63-1-5. (M)SDR AU980180Control Cable · frayed(AUS) WING FLIGHT SPOILER CABLES FRAYED AT WING STN 230 IN THE FOLLOWING LOCATIONS:- 1. CABLE PNO BACC2A3A02794EG LOCATED AT LH WSB1-32. CABLE PNO BACC2A3A02625FG LOCATED AT RH WSB1-43. CABLE PNO BACC2A3A03051FG LOCATED AT RH WSB2-4FOUND DURING SPECIAL INSPECTSDR AU980172Control Cable · worn(AUS) FLIGHT SPOILER CABLES WORN BEYOND LIMITS. CABLES LOCATED IN THE FOLLOWING POSITIONS AT LH WING REAR SPAR STN 210:-1. CABLE PNO BACC2C3D02428EG AT WSA1-32. CABLE PNO BACC2C3D01853FG AT WSA2-3FOUND DURING SPECIAL INSPECTION MSI-B737-3-97A.SDR AU980062Control Cable · frayed(AUS) LH AND RH WING SPOILER CABLES FRAYED. CABLES AFFECTED, PNO WSB1-4 AND PNO WSB2-4 IN RH WING AND PNO WSB2-3 AND PNO WSB1-3 IN LH WING.SDR DHL99803002Valve · failedON CLIMB-OUT ABOVE 6000 FT AND AT OR ABOVE 230 KTS, FELT EXCESSIVE VIBRATION THOUGH OUT AIRFRAME. REMOVED AND REPLACED LATERAL CONTROL SPOILER POWER CYLINDER AND CONTROL VALVE (LEFT WING). OPS AND LEAK CHECKED PER MM 27-62-9.SDR AU971640Control Cable · broken(AUS) NO6 FLIGHT SPOILER CABLE WSB2-4 FAILED ADJACENT TO THE PULLEYS AT RH WING STN 230 AT WBL157.0. EVIDENCE OF ADVANCED INTERNALCORROSION.SDR MZZA98019Control Rod · corrodedKUL - LEFT WHEEL WELL AREA SPPED BRAKE CONTROL VALVE ROD CONNECTING TO QUADRANT FOUND CORRODED. CORROSION BLENDED OUT IAW ECRA 2760-01157. PENETRANT INSPECT IAW OHM 20-20-02. ALODINE REWORKED AREA IAW OHM 20-43-03. PRIME WITH BMS 10-11 TYPE PRIMER, FINISH SDR COMA9760243Control Unit · malfunctionSPOILERONS CAUTION MESSAGE DURING FLIGHT. REPLACED THE NR 1 SECU.SDR TSAA9727342Control Cable · brokenFLT 65 - HNL-LIH - OUTER RGT SPOILER PANEL STAYS FAIRED DURING TURNING OF YOKE (ALERON INPUT). FOUND NR 7 FLT SPOILER 'WSA1-4' CABLE BROKEN APPROX 2 FT INBOARD OF NR 7 SPOILER QUADRANTS. INSTALLED NEW CABLE AND RIGGED IAW MM 261-0. OPS CHECK OK. NO OTHER DSDR CA971219042Tube · hole(CAN) PIN HOLE IN NR 2 HYDAULIC SYSTEM SPOILER LINE. IPC 29-00-00-20-50. PART TC: 33,653.SDR QXEA9700779Switches · dirtyBLI - ROLL SPOILER INBOARD/OUTBOARD CAUTION LIGHTS AND ADVISORY LIGHTS ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. CLEANED AND LUBRICATED SWITCHES ON QUADRANT. OPERATIONAL CHECK IS GOOD, NO COMPONENTS WERE REPLACED.SDR CA971219043Tube · leaking(CAN) ROLL SPOILER HYDRAULIC LINE FOUND LEAKING. PART TC: 29,237.SDR QXEA9700763Switches · dirtyBZN - ABORTED TAKEOFF ROLL, INBOARD/GROUND OUTBOARD SPOILER CAUTION LIGHTS ON. CLEANED PEDESTAL SWITCHES WITH CLEANER. NO PARTS REPLACED. GROUND RAN AT TAKEOFF POWER WITH NO FURTHER DEFECTS NOTED.SDR CA971210015Tube · leaking(CAN) PIN HOLE FOUND IN LEFT HAND SPOILER UNLOADING VALVE HYDRAULIC LINE. PART TC: 29,779.SDR CA971210006Line · cracked(CAN) HYDRAULIC LEAK FOUND COMING OUTBOARD SIDE OF RIGHT HAND NACELLE. ROLL SPOILER ACTUATOR LINE HAD A CRACK AT THE BEND IN THE LINE.SDR COMA9760223Pcu · malfunctionedCONFIG SPOILERS WARNING DURING TAKEOFF. REPLACED LEFT HAND OUTBOARD SPOILERON PCU.SDR 98ZZZX1225Mounting · crackedATW - RT LIFT SPOILER VALVE MOUNTING PLATE CRACKED. REMOVED AND REPLACED RT SPOILER VALVE MOUNTING PLATE. NO DISCONNECTING OF VALVE REQUIRED.SDR UPS97224873Control Cable · damagedINSPECTION TYPE-N/A, A/C ROLLS NOTICEABLY TO THE LEFT WHEN SPEED BRAKES EXTENDED 15-20 DEGREES AT 250 KTS. REPLACED SPOILER CABLE WSAZ AND RIGGED PER MM 27-61-31, OPS CKS GOOD.
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