JASC 2710
Service difficulty reports · 2,967
Reports filed under 2710 · Aileron 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 = '2710' 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 = '2710' 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 SWAA053382Bearing · bindingSHUDDERING AND BINDING FELT IN AILERONS DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED AILERON CENTERING MECHANISM ROLLER BEARING IAW MM.SDR CA051018001Turnbuckle · chafedDURING PHASE 1-5 INSPECTION ON AIRCRAFT, TECHNICIANS DISCOVERED THAT THE LT AND RT AILERON CABLES WERE FOULING. THE RESULT WAS THAT THE LT TURNBUCKLE WAS CHAFED AND THE RT SIDE THE SAFETY CLIP WAS GONE AND THE TURNBUCKLE WAS ALSO CHAFED.SDR QXEA200501347Warning Light · illuminatedEN ROUTE TO SEA ON FLIGHT 2478 (FAT-SEA), OVER SMF, RECEIVED A FLT CONTROL AILERON MALFUNCTION MESSAGE. FLIGHT DIVERTED TO SMF AND ACCOMPLISHED A UNEVENTFUL LANDING. MTX IN SMF PERFORMED A DETAILED INSPECTION OF THE AILERON CONTROL SYSTEM AND A RIGGING CHECKSDR SB05128Actuator · faultyPHL - FLT1243 - ON APPROACH TO PHL, WHEN AUTO PILOT WAS MANUALLY DISCONNECTED AT 1,000 FT AGL, THE AIRCRAFT ROLLED TO THE LEFT. AILERON TRIM SYSTEM WAS FOUND TO BE INTERMITTENT. BOTH THE CAPTAIN AND FIRST OFFICER WERE REQUIRED TO REGAIN LEVEL FLIGHT. CREW NSDR MASA200500766Actuator · malfunctionedASH 7049 DEN, AILERON TRIM MALFUNCTIONED IN FLIGHT. PILOT DECLARED AND EMERGENCY. WORK IS IN PROGRESS. MX R2 AILERON RUDDER TRIM CONTROL PANEL AND AILERON TRIM ACTUATOR.SDR SWIA200515625Damper · malfunctionedFLUTTER DAMPER STATUS MSG. INFLIGHT LEFT AILERON. REPLACED LT AILERON FLUTTER DAMPER REF AMM 27-15-05. OPERATIONAL CHECK GOOD.SDR UPS05M45479Warning Light · illuminatedAILERON DEFLECTED DISAGREE MESSAGE. A/C WAS DIVERTED AND EMERGENCY WAS DECLARED. FUEL WAS DUMPED BELOW MAXIMUM LANDING WEIGHT TO 57000 POUNDS. REPLACED O/B AILERON DEFLECTION ACTUATOR UP TO SUB TASK 27-16-02-820-001 PG 8 PER MM 27-16-02-4. L/P 474801--COMPLETESDR VNAA0509012Warning Light · false activationDURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. A REJECTED TAKEOFF WAS PERFORMED. THE CREW RESET THE CONTROLS AND REPORTED THE TAKEOFF CONFIG SYSTEM OPERATIONALLY CHECKED GOOD. AFTER THE BRAKES COOLED, THE CREW CONTINUED THE FLISDR QXEA200501239Actuator · malfunctionedSEA FLIGHT NR 2070 AFTER TAKEOFF, THE AIRCRAFT WANTED TO ROLL RIGHT. ALL ENGINE INDICATIONS WERE NORMAL AND MATCHED, THE TURN COORDINATION WAS CENTERED, FULL LEFT AILERON TRIM WAS NEEDED TO RETURN CONTROL TO NEAR NORMAL. MAINTENANCE REPLACED THE RIGHT AILEROSDR MASA200500727Handle · pulledASH 2735 CLT - ELEVATORS DISCONNECTED. MAINTENANCE FOUND FLIGHT DECK ELEVATOR, DISCONNECT HANDLE PULLED. RESET HANDLE WITH NO FURTHER INCIDENT.SDR 2005FA0001326Control Cable · wornDURING 100 HOUR INSPECTION, WHILE INSPECTING AILERON CABLES, FOUND FLAT SPOT ON THE LT AILERON CROSSOVER CABLE AT THE AILERON CABLE ABRASION STRIP ATTACHED TO A RIB ASSEMBLY LOCATED AT WING STATION 71.19. FURTHER INVESTIGATION FOUND THE CABLE BEGINNING TO FRASDR DXTA200500965Aileron · looseWHILE IN FLIGHT AILERON HAS 3 TO 4 INCHES OF FREE PLAY WITH NO EFFECT ON MOVEMENT OF AILERONS.SDR MASA200500711Warning Light · illuminatedASH 7110 IAD. RETURNED TO THE GATE DUE TO AILERON CONFIG MESSAGE ON TAKEOFF ROLL. MAINTENANCE RESET SYSTEM, OPS TEST GOOD.SDR VTZA200500178Idg · underservicedIDG 2 CAUTION MSG AND SPOILERON CONFIGURATION MESSAGE ON TAKEOFF. SERVICED NR 2 IDG IAW CRJ AMM 12-13-24 SPOILER SYS HAS NO MESSAGE POSTED AND OPS CHECK GOOD IAW CRJ AMM 27-60-00.SDR SWIA200515513Control Cable · out of adjustAIRCRAFT REQUIRES EXCESSIVE AMOUNT OF RT WING DOWN TRIM. RETENSIONED LT AND RT AILERON CABLES IAW AMM 27-00-00.SDR 05FDEA02501Control Cable · brokenDURING POSTFLIGHT INSPECTION FOUND LEFT INBOARD AILERON CABLE BROKEN. INSPECTED CABLE PULLEYS NO FURTHER DAMAGE FOUND AT THIS TIME. FOUND CABLE BROKE IN HALF HANGING FROM THE LEFT WHEEL WELL JUST ABOVE APU FIRE BOTTLE AREA. A/C ARRIVED WITH INBOARD AILERON SDR VNAA0508010Warning Light · illuminatedDURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. THE CREW PERFORMED A REJECTED TAKEOFF. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AILERON TRIM SYSTEM IAW CRJ200 AMM 27-11-00-710-801 AND A REJECTED TAKEOFF INSPECTION IAW CRSDR 2005FA0001197Rod End · brokenON AUGUST 5TH, DURING THE FLIGHT CONTROL RIGGING OPERATION, THE LT AILERON IB PCU ROD END WAS FOUND BROKEN. THIS ROD END IS PART OF THE BENDIX PCU PN 317012-1 ASSEMBLY. EVIDENCE OF CORROSION IS APPARENT AT CRACKED LOCATION. UNKNOWN TIME.SDR RAIA00507021Control System · lack of lubeFLT 5404- STL- RESISTANCE IN RIGHT AILERON NOTICED ON TAXI OUT. MAINTENANCE LUBED AILERON CONTROL SYSTEM. OPS CHECKED GOOD.SDR 07252005BCentering Cam · malfunctionedGET AN AIL FLAG WITH AUTOPILOT ENGAGED. ACFT VERY HARD TO TURN TO THE RT, ACFT AUTOMATICALLY BANKS 30 DEGREES TO THE LT WHEN CONTROLS RELEASED. INSTALLED RT AILERON CENTERING MECHANISM. OPS CHECK GOOD.SDR SWAA052108Rod · wornDURING SCHEDULED C2 CHECK, RT WING AILERON FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT AILERON CONTROL ROD PER MM.SDR MASA200500550Control Cable · bindingASH 6332 FSD - ON ARRIVAL TO PHX, CAPT WROTE UP AILERON CONTROL WHEEL BINDS IN LEFT TURN. MAINTENANCE RIGGED AILERON/FUSE AND RT WING CABLES AND PCU.SDR DXTA200500835Yoke · out of rigIN LEVEL FLIGHT, LT CONTROL YOKE DEFLECTED 10 DEG - 15 DEG. LT CO-PILOTS YOKE LEVEL/ CENTERED. REMOVED FWD YOKE COVERS L/R YOKES. REMOVED AILERON BELLCRANK PANELS L/R WING. INSTALLED RIG PINS AT YOKES. BOTH YOKES VERIFIED AT NEUTRAL. GAINED ACCESS TO AILERSDR 2005FA0001109Control Cable · wornCABLES WORN BEYOND LIMITS AT A CABLE RUB STRIP IN RT WING BY AUTOPILOT SERVO AT STA RBL 102. (K)SDR 2005FA0000966Rib · crackedLEFT AILERON OUTBOARD HINGE HALF WAS CORRODED. AILERON WAS DISASSEMBLED TO REPLACE HINGE HALF. UPON REMOVING AN3 BOLTS AND HINGE HALF FROM NOSE RIB, THE LOWER BOLT HOLE IN THE NOSE RIB WAS FOUND TO HAVE A HALF INCH CRACK ADJACENT TO THE HOLE.IT IS NOT POSSIBSDR CA050711008Cable · failed(CAN) FOUND FWD AILERON CABLE TENSION AT ZERO. CROSSOVER CABLES FOUND TO BE LOOSE. REMOVED AILERON CROSSOVER CABLES FROM CNTRL COLUMNS WITHOUT DISTURBING HUMBUCKLE LOCKING. INSPECTED CABLES, CHAINS, SWAGES AND HUMBUCKLE. DETERMINED ONE OF CROSSOVER CABLE CHAISDR MASA200500509Control Cable · obstructedAILERONS MOMENTARILY -JAMMED- THE CAPTAIN WAS ABLE TO REGAIN TOTAL CONTROL AND LAND WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GPWS. MX FOUND ROOT CAUSE TO BE A DISLODGED DISTRIBUTION DUCT THAT BLEW COLD AIR INTO THE INSULATION BLANKET WHICH CAUGSDR GNB2005F00005Control Cable · wornWEAR FROM BLENDING DUE TO SOFTER MATERIAL USED IN NEW STYLE CABLE.SDR MASA200500488Control Cable · lockedABORTED TAKEOFF AT 40 KTS. AILERON CONTROLS LOCKED, PILOT'S COULD NOT MOVE BOTH CONTROL COLUMNS. MAINTENANCE REPLACED IC600 AND AILERON CABLE FAINLADS.SDR MASA200500482Aileron · unknownASH 2641 CLT, THE CAPTAIN ABORTED TAKEOFF AND RETURNED TO THE GATE WHEN THE AILERONS FELT LIKE THEY WERE BINDING. INITIAL REPORT FROM MX IS SMOOTH OPERATION. MAINTENANCE PERFORMED A HIGHLY DETAILED INSPECTION OF THE AILERON SYSTEM. NO DEFECTS WERE NOTED. RSDR 2005FA0000945Control Cable · slippedAILERON CABLE SLIPPED OUT OF THE INBOARD NICOPRESS SLEEVE ON THE FORWARD AILERON CABLE IN THE LEFT WING. ALL 4 (LEFT AND RIGHT WING) CABLES WERE PURCHASED NEW FROM AMERICAN CHAMPION AIRCRAFT IN AUG, 2002 AND INSTALLED DURING THE REBUILD OF THE AIRCRAFT. ALL SDR 2005FA0001002Control Cable · wornLT AND RT PRIMARY AILERON CABLES SEVERELY WORN AT WING PULLEYS LOCATED AT WS 49.25. CABLES HAVE APPROXIMATELY 4725.4 TT. THIS DEFECT IS NOT A RESULT OF BINDING PULLEYS BUT MOST PROBABLY DUE TO SUB-STANDARD CABLE USED DURING MFG, SPECIFICALLY STAINLESS STEEL SDR DXTA200500784Controller · malfunctionedFLIGHT CONTROL FAULT CAS AND AILERON CONTROL LIGHT FLASHING. INSTALLED DMU . FOUND FORCE FIGHT BETWEEN PCU'S. ALL 4 TRANSDUCERS FUNCTION NORMALLY, ADJUSTED PCU'S. OPS CHECK NORMAL. WORK IAW CESSNA 750 MM CHAPT 27-10-01SDR 06172005BTrim System · lack of lubeAILERON TRIM NOT MOVING. INSPECTED AND LUBED TRIM KNOB.SDR EVAS094002Actuator · malfunctionedDURING CLIMB, AIRCRAFT RECEIVED AILERON DEFLECTION DISAGREE WARNING MESSAGE, CAPTAIN DECIDED TO AIR RETURN. ON GROUND CHECK, FOUND LEFT AILERON DEFLECTION ACTUATOR FUNCTION NO GOOD. REPLACED ACTUATOR AND OPERATION CHECK NORMAL.SDR CA050615004Bolt · misinstalled(CAN) WHEN REINSTALLING THE LT AILERON AFTER MAINTENANCE, THE ENGINEER NOTICED THAT THE AILERON BOLTS WERE INSTALLED INCORRECTLY AT BEARING NR 1 AND NR 3 ATTACH POINTS. THE RT AILERON BOLTS WERE ALSO CHECKED AND FOUND TO BE INSTALLED INCORRECTLY. BOLTS WERE SDR CHQA200500113Warning Light · activatedDURING CLIMB AT FL210, RECEIVED "AILERON SYS 1 FAIL" EICAS MESSAGE. LEVELED OFF AT FL230 AND TOLD ATC TO STAND BY. FOLLOWED QRH AND TURNED OFF AILERON SYSTEM 1 AND SLOWED TO 250 KIAS. EMERGENCY DECLARED WITH ATC AND F/A PREPARED CABIN FOR EMERGENCY LANDING.SDR AU510002001Fork · corrodedRT AILERON BELLCRANK FORK CORRODED. FOUND DURING INSPECTION IAW AWB 27-1. AIRCRAFT HAS SPENT MOST OF ITS LIFE OUTDOORS.SDR SWIA200515121Damper · leakingFLUTTER DAMPER STATUS MSG ILLUMINATED ON DESCENT. REPLACED RT AILERON FLUTTER DAMPER IAW CRJ MM 27-15-05. OPERATIONAL CHECK GOOD.SDR MASA200500444Warning System · activatedASH 6445 - PHX - AIRCRAFT RTG WITH CONFIG WARNING MESSAGE ON TAKEOFF ROLL. MX TROUBLESHOT AND COULD NOT DUPLICATE THE PROBLEM.SDR 71141Spring · brokenCREW REPORTED DURING INTERMEDIATE CLIMB, IT TOOK FULL RIGHT AILERON TRIM TO KEEP THE AIRCRAFT WINGS LEVEL. CREW NOTED NO CONTROLLABILITY PROBLEMS. CRUISE TRIM SETTING APPEARED MORE NORMAL AT 3 RIGHT. AIRCRAFT REQUIRED NO AILERON RETRIMMING DURING DESCENT. SDR SWAA051595Actuator · faultyAIR TURNBACK/DECLARED EMERGENCY. AILERONS FEEL UNRESPONSIVE WITH A NOTICEABLE DEAD BAND. REMOVED AND REPLACED AILERON TRIM ACTUATOR PER MM.SDR CA050527004Pin · mismanufacturedPDA PART ROD SECURING PIN DEHAVILLAND P/N C6CWM1043-27 INCORRECTLY MANUFACTURED. PIN OUTSIDE DIAMETER TOO LARGE TO FIT INTO 'H' BEAM HOLE. REFERENCE DHC-6-300 IPC CHAPTER 27-10-00 FIGURE 4 ITEM 560. 'H' BEAM ATTACHMENT HOLE EDGE DISTANCE MAY BE TOO SMALL IF SDR SWIA200515073Damper · malfunctionedCREW REPORTS FLUTTER DMAPER STATUS MSG INFLIGHT. REPLACED FLUTTER DAMPER ON RIGHT HAND AILERON IAW MM CHAPTER 27-15-05. OPERATIONAL CHECK GOOD.SDR SWIA200515036Damper · malfunctionedINTERMITTENT FLUTTER DAMPER STATUS MESSAGE IN FLIGHT. REPLACED LEFT AILERON AND NR 4 ELEVATOR FLUTTER DAMPER IAW 27-15-05, 27-34-05 CRJ MM. OPERATIONAL CHECK GOOD. P/N: 1023100-7, S/N OFF: HAI5124, S/N OFF: HAI5118.SDR DXTA200500731Rod End · out of adjustDURING FLIGHT, REQUIRED LARGE AMOUNT OF RIGHT AILERON TRIM FOR LEVEL FLIGHT AMOUNT INCREASED TO AT LEAST ONE QUARTER TRIM DEFLECTION (RIGHT WING DOWN TRIM) AT 250 KIAS. DID NOT INCREASE SPEED ABOVE 250 KIAS AS TRIM REQUIRED INCREASED WITH SPEED. REMOVED R/H ASDR F3LA200500020Computer · inoperativeFLIGHT CREW REPORTED ELAC 2 FAULT. ON SHORT FINAL LOST BOTH AILERONS WENT TO DIRECT LAW. REPLACED NR 2 ELAC. OPERATIONAL CHECK GOOD PER MM 27-93-34, PAGE 401. PERFORMED LAND CAT 3 TEST, OPS CHECK GOOD PER MM 22-97-00-710-001. UMP STATUS REMAINED CAT 3B. SDR DXTA200500729Trim System · malfunctionedAILERON TRIM APPEARS TO BE FREEZING UP IN FLIGHT AT FL 380 AT -28 C RAT. THE ROLL TRIM ANNUNCIATOR ILLUMINATED, WAS UNABLE TO MOVE THE AILERON TRIM KNOB UNTIL THE RAT WAS +10 C. THE RUDDER TRIM WAS MOVING FREELY AT -28 RAT BOTH OPERATE NORMALLY ON THE GROUNDSDR FAAAL01002Turnbuckle · crackedFSDO SENT INFO LETTER TO ALL IA`S IN DISTRICT REGARDING TURNBUCKLES CRACKING AT ENDS THUS LOOSING STRUCTURAL INTEGRITY OF TURNBUCKLE ON PRIMARY FLT CONTROLS AS A RESULT OF SURVEILIANCE CONDUCTED IN DISTRICT, DISCOVERING PROBLEM. AS A RESULT OF LETTER MECHANICSDR VTZA200500074Link · crackedLEFT AILERON LINK ON THE OUTBOARD PCU IS CRACKED IN HALF.
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