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.

SDR UPS99829023Bracket · corrodedINSPECTION TYPE:C2 LWW, FWD OF SPOILER LATERAL CONTROL MECHANISM BRACKET CORRODED. REMOVED SPOILER MINER MECHANISM AND REMOVED BRACKET AND VERIFIED MAT ID. BYE PEN TEST MIL STD 271F. NO CRACK NOTED. ALODINED AND PRIMED AND INSTALL. OPS CK TO BE DONE ON UPFeb 17, 1999 · N810UP · Doug DC873FSDR SWAA990308Warning · soundedABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. SPEED BRAKE HANDLE WAS CYCLED AND WARNING HORN SILENCED. ALL SYSTEMS CHECKED NORMAL.Feb 17, 1999 · N383SW · Boeing 7373H4SDR P2EA99075Handle · out of positionFLT - 612 - MYR - TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, FLAPS 1, TRIM 5.4. CREW REPORTS, ABORTED AT 40 KNOTS. FOUND SPEED BRAKE HANDLE OUT OF DETENT. CYCLED SEVERAL TIMES, OPS CHECKED OK PER MM 31-26-0. (M)Feb 6, 1999 · N603DJ · Boeing 737222SDR P5CA9900169Control Cable · wornLEFT WING NR 2 SPOILER CONTROL CABLE WORN AT NR 3 AND NR 4 CONTROL DRUM AREA. REPLACED PER MM 20-11-03.Feb 5, 1999 · N854FT · Boeing 747122SDR P5CA9900164Control Cable · wornNR 11 SPOILER CONTROL CABLE FOUND WORN AT DRUM ASSEMBLY. REPLACED PER MM 20-11-05.Feb 5, 1999 · N854FT · Boeing 747122SDR COMA9960051Warning · activatedTAKEOFF CONFIG WARNING SPOILERS. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF SPOILER SYSTEM WAS NORMAL.Jan 30, 1999 · N912CA · Cndair CL6002B19SDR CA990129022Link · damaged(CAN) WITH AIRCRAFT ON STANDBY AT AIRPORT, AN UNCOMMANDED DEPLOYMENT OF THE RIGHT FLIGHT SPOILER OCCURRED. STATUS MESSAGE 'FLT SPOILERS' ON EICAS AND ON THE SYNOPTIC PAGE, RT SPOILER SHOWED TO BE AT 26 DEGREES. COMFIRMED VISUALLY. RIGHT HAND SPOILER LINK TOJan 26, 1999 · Cndair CL6002B19SDR CA990311065Speed Brake · failed(CAN) SPEED BRAKES WOULD NOT RETRACT AFTER LANDING. LEFT WING TRAILING EDGE WIRE FROM P63 PIN F TO J239 PIN 6 FOUND WIRE BROKEN FOR DOWNLIMIT SWITCH. INSULATION ALSO MISSING FROM 2 OTHER WIRES. FRETTING OCCURRED FROM TYE-WRAP ATTACHMENT AT WS 78 ON RIGHT WIJan 19, 1999 · Cessna 560CESSNASDR COMA9960036Control · out of positionCON FIG SPOILERS WARNING DURING TAKEOFF. FOUND SPOILER CONTROL NOT STOWED. OPERATIONAL CHECK OF SYSTEM NORMAL.Jan 18, 1999 · N920CA · Cndair CL6002B19SDR QXEA9900139Bearing · loosePDX - SPEED BRAKE AIRFRAME CONNECTION LINK PIVOT POINT, UPPER AND LOWER BEARINGS ON LEFT-HAND AND RIGHT-HAND SIDES ARE LOOSE IN HOUSINGS. REPAIRED IAW HORIZON AIR EA 4-53-652.Jan 15, 1999 · N499US · Fokker F28MK4000SDR QXEA9900147Support Link · wornPDX - RIGHT-HAND SPEED BRAKE CROSSHEAD TO SUPPORT LINK PUSH ROD HAS APPROXIMATELY .050 RADIAL PLAY AT SUPPORT LINK. REPAIRED IAW HORIZON AIR EA 4-53-651 AND EA 4-55-108.Jan 11, 1999 · N499US · Fokker F28MK4000SDR QXEA9900145Bearing · wornPDX - LEFT-HAND SPEED BRAKE CROSSHEAD TO SUPPORT LINK PUSH ROD AFT BEARING HAS APPROXIMATELY .030 RADIAL PLAY. REPAIRED IAW HORIZON AIR EA 4-53-651 AND EA 4-55-108.Jan 11, 1999 · N499US · Fokker F28MK4000SDR AT9900109Pulley · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT WIND NR 2 SPOILER PULLEY QUADRANT HAS PITTING CORROSION ON TOP FORWARD AFT BOLT THROUGH HOLE. CHEMICALLY REMOVED CORROSION, REMOVED AND REPLACED INBOARD SPOILER PULLEY BRACKET, RIG CHECK COMPLIED WITH ON SPOILJan 8, 1999 · N806AT · Doug DC932SDR ABXA9900032Support · crackedDURING C-CHECK, FOUND LEFT INBOARD SPOILER TORQUE TUBE INBOARD SUPPORT CRACKED. REPLACED SUPPORT IAW DC9 SRM 51-30-1.Jan 8, 1999 · N986AX · Doug DC932SDR 99FDEA00004Retract Mech · malfunctionedNR 1 SPOILER DEPLOY DURING TAKEOFF ROLL, SPEED 90 KTS. TAKEOFF REJECTED. FOUND NORM OPS TEST OF GROUND SPOILERS AND SPEED BRAKES, CARRIED OUT IAW MM 27-61-00 PG 511, PARA 2 FOUND NORMAL.Jan 6, 1999 · N420FE · Airbus A310222SDR AT9900085Torsion Bar · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE SPOILER SUPPORT ROD END AND TORSION BAR LEVER CORRODED AT STA 50 AND STA 68. REMOVED AND REPLACED THE END SUPPORT ROD END AND TORSION BAR AND OPERATIONAL ADJUSTMENT TEST ACCOMPLISHED IAW DC9 MM 27-61-2, 20-10-Jan 5, 1999 · N849AT · Doug DC932SDR COMA9860394Warning · activatedFLIGHT SPOILER CAUTION MESSAGE DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. SYSTEM TEST NORMAL.Dec 17, 1998 · N924CA · Cndair CL6002B19SDR COMA9860379Circuit Breaker · trippedSPOILERON CAUTION MESSAGE. RESET CIRCUIT BREAKERS, SYSTEM TEST NORMAL.Dec 9, 1998 · N927CA · Cndair CL6002B19SDR AU981648Manifold · cracked(AUS) AFTER STARTING ALL ENGINES, NR 2 HYDRAULIC SYSTEM PRESSURE FELL TO ZERO AND THE ANNUNCIATOR LIGHT ILLUMINATED. INSPECTION REVEALED TOTAL LOSS OF FLUID FROM TWO 3.81 CM (1.5 INCHES) AXIAL CRACKS IN THE FLIGHT SPOILER MANIFOLD BODY CYLINDER WALL.Dec 3, 1998 · Dhav DHC7102SDR CA981230059Line · leaking(CAN) LEFT HAND SPOILER LINE REPLACED BECAUSE OF A PIN HOLE. SEE IPC 29-00-00-35-190.Dec 2, 1998 · Dhav DHC8102SDR CA990310006Switch · shorted(CAN) IN-FLIGHT, ROLL SPOILER INBOARD CAUTION LIGHT ILLUMINATED. LEFT UPPER ROLL SPOILER MICROSWITCH FOUND SHORTED INTERNALLY, SWITCH REPLACED.Nov 25, 1998 · Dhav DHC8102SDR 98ZZZX4639Fitting · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON NR 9 GROUND SPOILER MOUNT LUG.Nov 12, 1998 · N64319 · Boeing 727231SDR USAAF98090Actuator · leakingPHL - FLT 1809 - WHILE CLIMBING OUT FROM HPN AT 16000 FT, CREW RECEIVED A 'HYD SYS 1 LOW QTY, ALERT. CREW PERFORMED THE ABNORMAL PROCEDURE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO PHL. FLIGHT LANDED PHL WITHOUT FURTHER INCIDENT. MAINNov 8, 1998 · N853US · Fokker F28MK0100SDR CA981125011Lever · broken(CAN) UPON SELECTION OF AIRBRAKE/SPOILER, THE HANDLE BROKE OFF.Nov 5, 1998 · Bag BAE146200ASDR CA981113006Line · leaking(CAN) DURING MAINTENANCE, NR 1 SYSTEM'S HYDRAULIC WAS PRESSURIZED AND A CLOUD OF HYDRAULIC FLUID MIST WAS NOTED COMING FROM THE LEFT OUTBOARD WING REAR SPAR AREA. THE LEFT INBOARD ROLL SPOILER LIFT DUMP PRESSURE LINE WAS FOUND LEAKING.Oct 30, 1998 · Dhav DHC8102SDR CA981109045Pcu · failed(CAN) SUSPECTED UNCOMMANDED DEPLOYMENT OF RT FLIGHT SPOILER. AT FL 290, WITH A/P ON AIRPLANE INCLINED TO RIGHT. A/P DISCONNECTED, CAUTION MESSAGE 'R FLT SPLR', FOLLOWED BY STATUS MESSAGES 'FLT SPLRS FAULT' AND 'O/B GND SPLR FAULT'. MAINTENANCE FOUND RT FLOct 30, 1998 · Cndair CL6002B19SDR VJ9800619Mechanism · corrodedRT O/B SPOILER CAM ARM, TORSION ARM AND TORSION BAR AT XRS 307, SERRATION FOUND PITTED CORRODED. REPLACED TORSION BAR (3920944-503), CAM ARM ASSY ( 3923153-505) AND TORSION ARM (3920944-503) IAW DC9 MM 27-61-1 AND 27-61-6.Oct 22, 1998 · N937VV · Doug DC932SDR VJ9800602Torsion Bar · corrodedRT O/B SPOILER TORSION BAR SERRATION AT STA XRS307 PITTED CORROSION BEYOND LIMIT. REMOVED TORSION BAR AND REPLACED WITH SERVICEABLE PARTS. INSTALLED TORSION BAR ASSY AND CHECK SYSTEM IAW DC9 MM 27-61-6, OPS CHECKED GOOD IAW MM 27-61-6.Oct 22, 1998 · N937VV · Doug DC932SDR 98UAL900502Control Mech · malfunctionedWHEN THE SPEED BRAKE IS DEPLOYED, AIRCRAFT BANKS TO THE LEFT EXCESSIVELY. AILERON TRIM SET AT 0. WHEN THE B-SYSTEM IS OFF, THE AIRCRAFT DOES NOT ROLL.Oct 14, 1998 · N7455U · Boeing 727222SDR UPS98228009Support Rod · shearedINSPECTION TYPE:C NR 8 SPOILER I/B HINGE SUPPORT ROD SHEARED. SUPPORT ROD REMOVED AND REPLACED IAW MM SRM 51-30-2.Oct 12, 1998 · N936UP · Boeing 727108CSDR DHL9980101CHardware · wornAT C-CHECK, LT WING T/E UPPER AREA NR 5 SPOILER PANEL PRESENTS PLAY AT ATTACH POINTS. REMOVED AND REPLACED WORN HARDWARE PER MM 27-61-1.Oct 11, 1998 · N801DH · Doug DC873FSDR QXEA9801496Bearing · wornLEFT-HAND SPEED BRAKE LEVER ASSEMBLY LOWER BEARING IS WORN. REPAIRED IAW HORIZON AIR EA 4-55-93.Oct 9, 1998 · N491US · Fokker F28MK4000SDR USAAF98084Sensor · out of adjustCLT - FLT 1856 - AFTER TAKEOFF FROM CLT, CREW RECEIVED SEVERAL LIFTDUMPER UNSAFE WARNINGS AND LIFTDUMPER FAULTS. NO EMERGENCY WAS DECLARED, HOWEVER, FLIGHT RETURNED TO CLT. FLIGHT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED RIGHT SIDE LIFTDUMPOct 8, 1998 · N895US · Fokker F28MK0100SDR 98ZZZM933Skin · delaminatedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 11 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 18.5 INCHES BY 6 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Oct 7, 1998 · N626DH · Boeing 727277SDR QXEA9801506Fitting · damagedSPEED BRAKE LEFT-HAND LEVER ASSEMBLY VARIOUS DAMAGE EXISTS ON AFT END UPPER AND LOWER EARS ADJACENT TO STRAIGHT PUSHROD BOLT HOLE. REPAIRED IAW HORIZON AIR EA 4-55-86.Oct 1, 1998 · N491US · Fokker F28MK4000SDR QXEA9801504Lever · chafedSPEED BRAKE RIGHT-HAND LEVER ASSEMBLY ON AFT END OF UPPER SURFACE OF LOWER EAR ADJACENT TO STRAIGHT PUSHROD BOLT HOLE CHAFED. REPAIRED IAW HORIZON AIR EA 4-55-86.Oct 1, 1998 · N491US · Fokker F28MK4000SDR QXEA9801502Fitting · wornSPEED BRAKE LEFT-HAND LEVER ASSEMBLY LOWER BUSHING HOLE FOR STRAIGHT PUSHROD IS ENLARGED AND OUT OF ROUND. REPAIRED IAW HORIZON AIR EA 4-55-86.Oct 1, 1998 · N491US · Fokker F28MK4000SDR CA981019003Line · cracked(CAN) GROUND HANDLING PERSONNEL NOTED A FLUID LEAK AT THE LEFT GEAR AND NACELLE. THE LIFT DUMP PRESSURE SYSTEM LINE FOUND CRACKED AND SPRAYING FLUID ON JET PIPE. HYDRAULIC LINE AT FLIGHT SPOILER LIFT DUMP SOLENOID VALVE REPLACED.Oct 1, 1998 · Dhav DHC8102SDR AU981205Warning System · activated(AUS) MANUAL SPOILER FAULT LIGHT ILLUMINATED. SYSTEM CHECKED, BUT NO REASON FOR THE FAULT COULD BE FOUND. DEFECT HAS NOT OCCURRED SINCE.Sep 21, 1998 · Bag BAE146100ASDR COMA9860258Secu · malfunctionCONFIG SPOILER WARNING DURING TAKEOFF. REPLACED THE LT AND RT SECU.Sep 10, 1998 · N916CA · Cndair CL6002B19SDR 98UAL900407Control Cable · looseAIRPLANE AIR-GROUND SWITCH STUCK IN GROUND MODE. *S/D* SECURED GROUND SPOILER INTERLOCK CABLE TO TORSION LINK.Aug 23, 1998 · N389UA · Boeing 737322SDR DLM88981686Link · wornAT 20,000 FT AND 300 KTS ATTEMPED TO DEPLOY SPEEDBRAKES, AIRCRAFT_ROLLED RIGHT. SPEED BRAKE RETRACTION STOPPED ROLL. REPLACED RT INBOARD FLIGHT SPOILER LINK.Aug 14, 1998 · N925DL · Doug MD88SDR DHL9872174DPulley · crackedAT D-CHECK, PULLEY FOUND CRACKED FOR SPOILER AT WS 253 RT WING. REMOVED AND REPLACED PULLEY PER MM 20-20-4. N/R 2664.Aug 6, 1998 · N721DH · Boeing 727228SDR ABXA9800698Link · crackedDURING C-CHECK, FOUND THE LEFT INBOARD SPOILER DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 SMM 27-61-1 AND MM 27-61-0.Aug 6, 1998 · N935AX · Doug DC933FSDR ABXA9800697Link · crackedDURING C-CHECK, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 SMM 27-61-1 AND MM 27-61-0.Aug 6, 1998 · N935AX · Doug DC933FSDR CALA9801371Torsion Bar · corrodedINSPECTION FOUND RT WING INBOARD TORSION BAR CORRODED. THE TORSION BAR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 27-61-6.Jul 30, 1998 · N14534 · Doug DC932SDR CA980814014Rod · out of adjust(CAN) WHEN TAKEOFF POWER APPLIED, CONFIGURATION WARNING HORN CAME ON AND ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE SPOILERS ANNUNCIATED, LEVER IN FORWARD DOWN POSITION, TAKEOFF REJECTED. SPEED BRAKE CONTROL ROD ADJUSTED PER MM 27-62-04. AUTO SPEED BRAKJul 30, 1998 · Boeing 767233SDR JBXA980046Actuator · crackedDURING GEAR EXTENSION, LOST NR 1 HYDRAULIC SYSTEM. LANDED WITH GEAR DOORS EXTENDED. HYDRAULIC QUANTITY READS ZERO. INSPECTED AND FOUND SPEED BRAKE ACTUATOR FILTER HOUSING CRACKED. REMOVED AND REPLACED SPEEDBRAKE ACTUATOR IAW F-100 MM 27-61-02. OPERATIONALJul 23, 1998 · N132ML · Fokker F28MK0100SDR ORJA98170Annunciator · malfunctionedABORTED TAKEOFF DUE TO SPOILED FLAP EXT ANNUNCIATOR CAME ON DURING TAKEOFF ROLL AT ABOUT 90 KTS. SYSTEM OPERATIONS CHECK WAS NORMAL PER MM 27-60-00. NO DEFECTS NOTED AT THIS TIME. (M)Jul 18, 1998 · N834RA · Doug DC983SDR UPS98227944Quadrant · crackedINSPECTION TYPE:C NR 1 SPOILER QUADRANT IS CRACKED AT CABLE GUARD. NR 11 SPOILER QUADRANT REPLACED IAW 27-61-81 MM.Jul 10, 1998 · N936UP · Boeing 727108C
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