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 96ZZZX1949Filter · failedDURING MAINTENANCE INSPECTION OPERATION 10, ITEM CARD 27-20 INSPECTION REVEALED FILTER SEPARATED FROM MOUNTING FLANGE IN THE END OF ELBOW FITTING PERMITTING IT TO SLIDE BACK AND FORTH WITHIN THE FITTING. THIS NEGATES FILTERING. REPLACED ELBOW FILTER FITTING.SDR CA960321514Pcu · failed(CAN)ON APPROACH, SPOILER FAULT MESSAGE ON EICAS. INSPECTION FOUND LEFT INBOARD SPOILERON POWER CONTROL UNIT (PCU) AND ELECTRICAL HARNESS FAILED. HARNESS AND SPOILERON PCU REPLACED.SDR ABXA9600299Drive Link · crackedDURING COMPLIANCE OF AD 85-01-03; SB 27-228 REV 4, DURING EDDY CURRENT INSPECTION, FOUND THAT THE RIGHT INBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED LINK IAW DC-9 SUPP MM 27-61-01.SDR C1HA960099Rod End · brokenRIGHT OUTBOARD SPOILERS FLOATING, REQUIRES 10 UNITS OF LEFT RUDDER TRIM. FOLLOWED ABNORMAL SPOILER FLOAT PROCEDURE. FOUND ROD END FOR SPOILER CABLE TO NR 14 SPOILER BROKEN AT MIX BOX RIG BAR. REPLACED ROD END, RIGGED SPOILER CABLES AND SPOILERS PER MM 2761-SDR 96UAL900112Control Mech · out of adjustGROUND SPOILER ON THE LEFT WING IS FLOATING IN CRUISE, ESPECIALLY THE OUTBOARD AFT EDGE.SDR COMA9660028Secu · trippedDURING TAKEOFF, FLIGHT SPOILER CAUTION MESSAGE ON EICAS. RESET THE SPOILER ELECTRONIC CONTROL UNITS. NO DEFECTS FOUND.SDR RAIA960156Connector · contaminatedSTL - FLT 7460 - TOCW ILLUMINATED DURING TAKEOFF. MAINTENANCE CLEANED GYLCOL FROM CANNON PLUGS ON BOTH SPOILER ACTUATORS, PN TY176301C. OPERATION CHECK GOOD. (X)SDR 96ZZZM254O-Ring · extrudedFLT NR 860 - PHX/SAN - EMERGENCY LANDING AT SAN, YELLOW HYDRAULIC SYSTEM LEAK AND ALL FLUID LOST ON APPROACH. HYDRAULIC LEAK IN WHEEL WELL AREA. FOUND UNION ON AUTO BRAKE MODULE LOOSE. SECURED AND OPS CHECK NORMAL. ALSO, FOUND O-RING EXTRUDED FROM NR 2 SPOSDR 96UAL900062Pca Transformer · malfunctionedSPOILER HANDLE GOES TO FULL EXTEND AS SOON AS HANDLE IS ARMED. SUPPLEMENTAL DATA UPDATE: NR 3 FAULT ON THE SPOILER CONTROL MODULE. REPLACED NR 4 SPOILER PCA TRANSFORMER (RVDT). CLEARED FAULT, OPERATION NORMAL.SDR CA960131011Relay · intermittent(CAN)DURING TAXI FOR TAKEOFF THE SPEED BRAKE CONTROL TEST WOULD NOT SOUND DURING TAKEOFF WARNING TEST WITH SPOILERS SELECTED & SAFETY RELAY BY-PASS SWITCH SELECTED. SPEED BRAKE CONTROL RELAY AT FAULT. REPL ACED.SDR 96UAL900048Spring · failedSPOILERS FAILED TO RETRACT AFTER LANDING. HELICAL RETURN SPRING ON SPEEDBRAKE DRUM FOUND BROKEN. REPLACED SPRING.SDR P5CA9600096Bearing · corrodedFOUND LEVEL 1 CORROSION ON LEFT WING SPOILER POSITION TRANSMITTER FINE ADJUSTMENT ROD BEARING. END ASSEMBLY REPLACED, FUNCTION CHECK SATISFACTORY IAW SRM 27-68-00.SDR WRLA96001Act Arm Bolt · missingWHILE TAXIING, FLIGHT CREW WAS PERFORMING FLIGHT CONTROL CHECK. LEFT INBOARD SPOILER WOULD NOT INDICATE 'FULL-UP' ON TEST. FLIGHT CREW ELECTED TO RETURN TO GATE FOR CORRECTIVE ACTION. AIRCRAFT RETURN TO GATE WITHOUT FURTHER INCIDENT. MAINTENACNE TROUBLE SHSDR DL72S960044Mount Bolts · looseNR 2 SPOILER POWER PACK BOTTOM MOUNT BOLTS ARE LOOSE. REMOVED SPOILER ACTUATOR ATTACH FITTING. REMOVED AND REPLACED ANGLE PER MM 57-42-0 PG 804. INSTALLED POWER PACK, ACTUATOR AND MOUNT FITTING.SDR DLM88954768Spoiler Light · illuminatedSPOILER DEPLOYED, MESSAGE ILLUMINATED ON OAP. MSG ON WITH HANDLE ARMED. ALL SPOILERS DOWN FWD TO MCO AND PLAC PER MEL 27-00-32. NO MRR, REJECTED 12-28-95 GT 595.SDR CA951222009Panel · chafed(CAN)ALL FLEET AIRCRAFT CHECKED AND ONE FOUND WITH PANEL RH 532DB AND LH 632DB CHAFED THROUGH HONEYCOMB. CLAMPS WERE CHANGED AND REINSTALLED SO THAT CURVED PORTION OF CLAMP FACES UP, CREATING MORE ROOM BET WEEN CLAMP AND FLAP CLOSURE PANEL.SDR 9521279102Control Cable · bindingEN ROUTE GSO-MSP, AIRCRAFT WAS CONTINUOUSLY ROLLING 3 TO 4 DEGREES LEFT AND RIGHT. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING INBOARD SPOILER RETRACT CABLE DEFLECTED AND HUNG ON ADEL CLAMP. FREED CABLE AND RIGGED. OPERATISDR CAL951149Bolt · brokenDEN - INSPECTION FOUND RT INBOARD GROUND SPOILER FORWARD ACTUATOR PIVOT BOLT BROKEN. THE FORWARD ACTUATOR PIVOT BOLT WAS REMOVED AND REPLACED. (X)SDR COMA9560618Spoiler Message · activatedINBOARD AND OUTBOARD GROUND LIFT DUMP SPOILERS FAULT MESSAGE ON EICAS. ACFT RETURNED TO FIELD. COULD NOT DUPLICATE, NO FAULT CODES LOGGED IN SPOILER ELECTRONIC CONTROL UNIT. ACFT RETURNED TO SERVICE.SDR CA960109007Panel · gouged(CAN)RUBBING EVIDENT ON RH ROLL SPOILER PANEL.SDR CA960109006Panel · gouged(CAN)CLAMP WEAR EVIDENT ON BOTH ROLL SPOILER PANELS. OTHER P/N 632DB.SDR CA960109005Panel · gouged(CAN)SLIGHT CABLE RUB EVIDENT ON BOTH PANELS. P/N OF OTHER 632DB.SDR CA951122003Line · cracked(CAN)LOSS OF ALL #1 HYDRAULIC FLUID. RH INBOARD ROLLL SPOILER ACTUATOR LINE FOUND CRACKED.SDR 9DEA01780Mixer Bracket · crackedLT LATERAL CONTROL MIXER BRACKET ASSY WAS FOUND CRACKED ON HFEC INSP, PART 1 OF EO 8-2760-7-3310 C1. CRACK IS .25 INCH LONG ON RT LEG OF BRACKET AT RADIUS.SDR CA951130013Pipe · cracked(CAN)CREW NOTICED FLUID LEAK IN AREA OF LEFT OUTBOARD ROLL SPOILER. PRESSURE LINE TO SPOILER FOUND CRACKED.SDR 95ZZZM768Spoiler Cable · wornDURING INSPECTION, THE LEFT WING ROLL SPOILER CABLE WAS FOUND TO BE WORN 50 PERCENT AT YW 90 BY A FAIRLEAD. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. (M)SDR CA951120007Control Cable · worn(CAN)LEFT WING ROLL SPOILER CABLE FOUND 50 PERCENT WORN AT STA. YW90 NEAR FAIRLEAD.SDR COMA9560595Pcu · defectiveFLIGHT SPOILERS STATUS MESSAGE ON EICAS. REPLACED THE LT FLIGHT SPOILER POWER CONTROL UNIT.SDR 95ZZZM671Return Line · brokenEN ROUTE FROM RIC TO IND, THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC PRESSURE AND QUANTITY. ACCOMPLISHED EMERGENCY CHECKLIST PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND 'A' SYSTEM RETURN LINE FROM NR 2 SPOILER ACTUATOR BROKEN. TRAILING EDGE COVE SUPPORSDR 9517289866Mechanism · lack of lubeDURING DESCENT WITH SPEED BRAKE FULLY EXTENDED, THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. CREW DISCONNECTED AUTOPILOT AND RETRACTED SPEED BRAKES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND ACCUMULATION OF ICE IN THE RIGHT SPOILER CONTROL. REMOVED THE ICE AND LUSDR 95ZZZX6418Spring · brokenWHILE USING SPEED BRAKES IN IMC CONDITION, PILOT REPORTED AIRCRAFT MADE HARD LEFT TURN. IT WAS LATER DETERMINED THE RETURN SPRING DID NOT ALLOW THE SPEED BRAKE IN ONE WING TO FULLY RETRACT CAUSING THE TURN SITUATION. THE RETURN SPRING WAS BROKEN AND WOULD NOSDR 96ZZZM878Rod End · corrodedLEFT WING INBOARD FLIGHT SPOILER NR 5 ACTUATOR INPUT ROD END BEARING CORRODED. REPLACED ACTUATOR ROD PER MM 27-61-9 AND OPS CHECKED SPOILERS PER MM 27-61-00 PQ 530 TO 531 FIG 515, NR 5 PANEL OPS CHECKED GOOD. (M)SDR CA951108020Line · holed(CAN)PILOT NOTICED RH HYDRAULIC GAUGE LOOSING QUANTITY. FLUID TRANSFERRED FROM LEFT SIDE. MAINTENANCE FOUND A LEAK IN LH OUTBOARD GROUND SPOILER PRESSURE LINE.SDR ABXA9600461Drive Link · crackedDURING COMPLIANCE OF AD 85-01-03 AND SB'S 27-228, 27-229 AND 27-240, FOUND THE LEFT WING OUTBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED THE LEFT WING OUTBOARD SPOILER DRIVE LINK IAW DC-9 MM 27-61-01.SDR COMA9560584Manifold · defectiveOUTBOARD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE GROUND SPOILERS MANIFOLD ASSEMBLY.SDR COMA9560589Pcu · defectiveTHE RIGHT FLIGHT SPOILER DEPLOYS UNCOMMANDED. REPLACED THE RIGHT FLIGHT SPOILER POWER CONTROL UNIT.SDR COMA9560582Ecu · reqd resetSPOILERS FAULT MESSAGE ON EICAS. RESET THE NR 1 AND NR 2 SPOILERON ELECTRONIC CONTROL UNITS.SDR 95ZZZM660Return Line · crackedEN ROUTE FROM IND TO DEN, THE AIRCRAFT STARTED LOOSING 'A' SYSTEM HYDRAULIC QUANTITY. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 2 SPOILER ACTUATOR RETURN LINE CRACKED AT T-FITTING B-NUT. REPLACED LINE, BOTH 'A' SYSTEM HYDRAULIC PUMPS AND 'A' SYSTEM RETURN SDR 95UAL900214Module · malfunctionedSPEED BRAKE DID NOT DEPLOY ON LANDING WITH SPEED BRAKE ARMED LIGHT ON. MANUALLY WOULD ONLY DEPLOY TO FLIGHT POSITION. REPLACED THE AUTO SPEED BRAKE ACCESSORY MODULE PER MM 27-62-35. CHECKS O.K. THE MODULE WAS ROUTED TO THE SHOP WHERE NO FAULTS WERE FOUND.SDR CA951020016Actuator · stuck(CAN)DURING PRE-FLIGHT ROLL CONTROL CHECK, PILOT REPORTED THAT RH OUTBOARD ROLL SPOILER WOULD ONLY EXTEND HALFWAY. IN GROUND MODE IT WAS OK. INSPECTION OF RH WING SPOILER CLUTCH AT PANEL 632DB LOCATED AT R H LOWER WING WAS FOUND RUBBING AGAINST LOWER MICROSWITSDR 95UAL900177Pickup · out of adjustAILERON CONTROL IS SLUGGISH WITH EXCESSIVE DEADBAND EITHER SIDE OF NEUTRAL. ACFT HAS PRONOUNCED LEFT ROLLING TENDENCY AT LOW SPEEDS AND RIGHT ROLLING TENDENCY AT HIGH SPEEDS. ALSO, ACFT ROLLS LEFT WITH SPEED BRAKES EXTENDED. ADJUSTED SPOILER PICKUP PER MM 2SDR 95ZZZX6236Control Mech · malfunctionedATW - FLT 265 - UNCOMMANDED OPENING OF AIR BRAKE ON APPROACH INTO ATW. ADJUSTED AND TESTED COMMAND AND FEED BACK POTENTIOMETER IAW 27-63-00, PAGE 501, PARAGRAPH 1C. CLEANED AND ADJUSTED LEVER FRICTION DAMPENERS AND TESTED IAW 27-63-00, PAGE 509. TESTED SENSSDR CA951012002Actuator · jammed(CAN)ROLL CONTROL JAMMED DURING APPROACH AT 50 FEET. CREW WERE TRYING TO INPUT RIGHT ROLL. A FORCE OF 10 LBS WAS APPLIED TO CONTROL AND CONTROL CAME FREE. AIRCRAFT LANDED OK. LH AND RH ROLL SPOILER QUADRANT, LOWER JAM SWITCH WIRE CLAMP RUBBING ON ACCESS PANELSSDR COMA9560562Caution Message · activatedOUTBOARD GROUND SPOILERS CAUTION MESSAGE ON EICAS FLIGHT SPOILERS FAULT MESSAGE. THE PROBLEM COULD NOT BE DUPLICATED AND CLEARED FAULT MESSAGES FROM SECU. AIRCRAFT RELEASED FOR TEST FLIGHT AND NO FURTHER DISCREPANCIES NOTED.SDR SRAA99509Switch · out of adjustMIA - FLT 101 - ON TAKEOFF, SPOILER WARNING HORN CAME ON. ABORTED TAKEOFF AND RETURNED TO BLOCK. ADJUSTED SPOILER ARMED SWITCH, SYSTEM OPS CHECKED GOOD PER MM CHT 27. (X)SDR COMA9560556Ecu · malfunctionedDURING LIFT OFF, OUTBOARD GROUND LIFT DUMP INDICATED DEPLOYED. ALSO, AMBER MESSAGE ON EICAS AND FLIGHT CONTROL PAGE INDICATED DEPLOYED, ACFT RETURNED TO FIELD. RESET THE SPOILER ELECTRONIC CONTROL UNIT AND SYSTEM TEST NORMAL.SDR COMA9560552Quadrant · defectiveDURING LANDING, GROUND LIFT DUMP DEPLOYS NORMALLY, THEN RETRACTS AND REDEPLOYS. REPLACED THE THROTTLE QUADRANT.SDR ABXA9500739Link · failedDURING GEAR EXTENSION ON APPROACH, THE SPOILER EXTEND LIGHT ILLUMINATED; NO BUFFET WAS FELT. EXTENDED SPOILERS MANUALLY, LIGHT REMAINED ON AFTER THEY WERE RETRACTED. FOUND LT MOST INBOARD SPOILER PANEL DRIVE LINK AND OUTBOARD TOP DRIVE LINK BROKEN. ALSO, LTSDR ABXA9500738Link · failedDURING GEAR EXTENSION ON APPROACH, THE SPOILER EXTEND LIGHT ILLUMINATED; NO BUFFET WAS FELT. EXTENDED SPOILERS MANUALLY, LIGHT REMAINED ON AFTER THEY WERE RETRACTED. FOUND LT MOST INBOARD SPOILER PANEL DRIVE LINK AND OUTBOARD TOP DRIVE LINK BROKEN. ALSO, LTSDR ABXA9500737Drive Link · failedDURING GEAR EXTENSION ON APPROACH, THE SPOILER EXTEND LIGHT ILLUMINATED; NO BUFFET WAS FELT. EXTENDED SPOILERS MANUALLY, LIGHT REMAINED ON AFTER THEY WERE RETRACTED. FOUND LT MOST INBOARD SPOILER PANEL DRIVE LINK AND OUTBOARD TOP DRIVE LINK BROKEN. ALSO, LT
Back to JASC 2760