JASC 2720
Service difficulty reports · 3,131
Reports filed under 2720 · Rudder 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 = '2720' 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 = '2720' 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 GTIA2023101937549Hinge Arm · damagedDURING ACCOMPLISHMENT OF TI 5533-1603-NKS FOUND ELONGATED HOLES ON HINGE ARMS #3. RAF-01 3347943-02 GENERATED-PERFORMED PERMANENT REPAIR OF THE RUDDER HING ARM #3 IAW EA# 55-0374-23 EC EA 5536-23-13. SPIRIT REPAIR ASSESMENT FORM LOG PAGE 3347943-02SDR YENA2023101801272Actuator · failedFLT#126, TPA-JFK. 'IN CLIMB THROUGH FL 130 EXPERIENCED UNCOMMANDED FLIGHT RUDDER INPUTS AS WELL AS AIRCRAFT VIBRATION. RUDDER TRIM INDICATIONS WERE VARYING BETWEEN 0.7L AND 0.1R. RECEIVED RUDDER INPUT AGAIN IN DECENT TO LEFT FROM 0.4L TO 1.4L ON RUDDER TRIM INSDR CALA2023103003231Fitting · crackedLH ELEVATOR INBD SERVO CONTROL HINGE FITTING BOLT ANTI ROTATION FOUND WITH CRACK, REQUIRES FURTHER EVALUATION. TASK PERFORMED BY LHT EMP 5P0722 & INSP BY LHT EMP 5H0619 AS RECORDED ON LTPR NR# 5001264906-0020. DURING INSPECTION OF LH ELEVATOR, FOUND CRACK ON LSDR DALA2023100908300Unknown · unknownSHIP 3127 BLUE SYS RUDDER SERVO HAS EXCESSIVE PLAY. CORRECTIVE ACTION: REMOVED BLUE SYS RUDDER SERVO PER A319 AMM 27-24-51. (0005175)SDR DXTA2023100297020Motor · defectiveVENTRAL RUD FAIL WHITE CAS: DURING ENROUTE CLIMB AT ABOUT FL350 WE GOT AN INTERMITTENT VENTRAL RUD FAIL WHITE CAS WHICH THEN STAYED ON PERMANENTLY UNTIL LANDING. WE LEVELED OFF AT FL380 AND MAINTAINED APPROXIMATEY 210KTS INDICATED FOR THE REST OF THE FLIGHT. SDR AALA202309132771Adiru · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO UNCOMMANDED YAW RIGHT AT 130 KIAS ON TAKEOFF. AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED STALL MANAGEMENT YAW DAMPER BITE TEST PROCEDURE PER FIM 27-32-00-810-801. FOUND SDR QXEA2023090800126Unknown · unknownFLIGHT CONTROLS NOT MOVING NORMALLY DURING AFTER START CHECK. RUDDER STIFF AND CHATTERING. REMOVED FROM SERVICE. DUE TO RECENT HISTORY, BLED #1 HYD SYS, REF AMM TASK 29-10-00-870-803-A. C/W OPS TEST OF RUDDER CONTROL SYSTEM PER AMM TASK 27-20-00-710-802-A. NO SDR HNAA2023090500324Unknown · unknownRUDDER SYSTEM 2 INOP AFTER TAKEOFF......TROUBLESHOT PER FIM 27-22-00-810-804-A STEPS 1 AND 8. FOUND RUDDER SYS 2 PRESS SWITCH BAD. R&R RUDDER SYS 2 PRESSURE SWITCH PER AMM 237-23-04. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE... ACTUAL LP 288223-1.SDR AALA202309080865Pcu · leakingAIRCRAFT WAS GROUNDED: STRONG ODOR ON CLIMB OUT AND ON APPROACH. STRONG SMELL IN FLIGHT DECK AND CABIN. **SUPPLEMENTAL REPORT FOR AALA202309010865: MAINTENANCE TROUBLESHOOT HYDRAULIC FLUID LEAK TO MAIN RUDDER POWER CONTROL UNIT. MAIN RUDDER PCU WAS REMOVED ANDSDR HNAA2023091800333Unknown · unknownE992000 RUDDER 2 UPPER HINGE FITTING ELONGATED AT HAT BUSHING. REMOVED AND INSTALLED SERVICEABLE RUDDER 2 UPPER HINGE FITTING IAW EMB145 SRM 55-40-02SDR HNAA3032091800332Unknown · unknownE991999 RUDDER 1 LOWER HINGE FITTING WORN. REMOVED WORN RUDDER 1 LOWER HINGE FITTING AND INSTALLED SERVICEABLE RUDDER 1 LOWER HINGE FITTING ASSEMBLY IAW EMB145 SRM 51-40-02 AND AMM 20-10-01.SDR AALA202307211634Actuator · malfunctionedAIRCRAFT WAS GROUNDED: 30 MINUTES INTO FLIGHT, SMOOTH AIR AT 34000 RUDDER SUDDENLY MOVED RIGHT.9. FLIGHT CREW FELT THE YAW ON UNCOORDINATED FLIGHT, GRADUALLY THE RUDDER RETURNED TO NORMAL. THE FLIGHT CREW REPORTED THAT LATER ON DURING THE FLIGHT IT RE-OCCURREDSDR AALA202307197797Relay · faultyAIRCRAFT WAS GROUNDED: UNCOMMANDED RUDDER MOVEMENT TO THE LEFT. RUDDER TRIM WENT TO 1.0 THEN SLOWLY MOVED BACK TO 0.0. AUTOPILOT 1 WAS ENGAGED. PERFORMED TSM TASK 22-62-00-810-809-A. REMOVED AND REPLACED RELAY RUDDER TRIM 1 (7CC1).SDR VNAA202307121111Pcu · unserviceableINTERMITTENT ABNORMAL VIBRATION AT HIGHER AIRSPEED AND POWER, UN-COMMANDED SLIGHT RUDDER MOVEMENT, VIBRATION NOT HARMONIC WITH ENGINES, SLIGHT RIGHT PULL AT AUTO PILOT DISCONNECT. REMOVED AND REPLACED SPHERICAL BALL, BOLT AND BUSHING ON RUDDER PCU SYSTEM 3 IAWSDR NI6R202306270059Pulley Bracket · misrepairedDURING 150 HOUR INSPECTION MECHANIC FOUND SIGNIFICANTLY FRAYED RUDDER INTERCONNECT CABLE. UPON INSTALLATION OF NEW CABLE AND NEW PULLEY IT WAS DISCOVERED THAT A PREVIOUS REPAIR ON A PULLEY BRACKET HID THE ORIGINAL CABLE GUARD PIN HOLE. PRIOR MAINTENANCE INSTALSDR HNAA2023062600230Unknown · unknown00246 PROTRACTOR NUTPLATE MISSING ON TRAIL RUDDER LH SIDE REPLACE WITHIN 5000 FC PER SRM 55-40-01. REPAIRED RUDDER II LH SIDE IAW REPAIR #6 OF SRM 55-40-01,SDR COEA2023060710913Unknown · unknownWO 249025 FLIGHT 8783 ENROUTE FCA - GTF, DISCREPANCY: DURING APPROACH, THE CAPTAIN'S RUDDER PEDAL ADJUSTMENT FAILED ALLOWING THE PEDALS TO SLIDE FORWARD. PEDALS WERE SELF-ADJUSTING. THE AIRCRAFT LANDED WITHOUT FURTHER ISSUES. CORRECTIVE ACTION: MAINTENANCE ADSDR 4DPA2023051300002Pressure Switch · failedISSUE-CREW REPORTED SHORTLY AFTER TAKEOFF RUDDER OVERBOOST WAS PRESENTED ON THE EICAS, AFTER RUNNING THE QRH PUSHED OUT SYSTEM 2. MESSAGE DID NOT PERSIST. BELOW 135 PUSHED IN SYSTEM 2 MESSAGE DID PERSIST. CORR ACTION- MX TROUBLESHOT TO BAD RUDDER PRESSURE SWITSDR QXEA2023041700069Unknown · unknownINFLIGHT IT TOOK ONE HALF OF RIGHT RUDDER TRIM TO MAINTAIN COORDINATED FLIGHT. RUDDER PEDALS WERE PHYSICALLY SPLIT BY ABOUT 4 INCHES RIGHT DEFLECTION. REACCOMPLISHED AND VERIFIED RUDDER RIGGING IN REF TO EMB 175 FIM 27-20-00 AND AMM 27-20-00 COMPLTED FREEDOM OSDR UIEA2023040600322Actuator · unknownVERTICAL STABILIZER REAR SPAR, RUDDER RATIO CHANGER WITH EVIDENCE OF HYD LEAK(<P>R/R ACTUATOR ASSY - RUDDER RATIO CHANGER SERVO. OPS & LEAK CHECK GOOD IAW 27-20-00</P>)SDR J7SA2024060400404Torque Tube · crackedDURING MAINTENANCE, LEFT RUDDER TORQUE TUBE STABILIZER ROD FOUND CRACKED. REPLACED BOTH LEFT AND RIGHT RUDDER TORQUE TUBE STABILIZER RODS IAW PHENOM 300 AMM 27-21-01.SDR DU4R2023033100001Rudder · leakingDURING SCHEDULED MAINTENANCE AT HAECO, LAKE CITY, FLORIDA FOUND RUDDER R/H SURFACE SURROUNDING THE FWD LOWER HOIST POINT PRODUCED INDICATIONS OF POSSIBLE WATER INGRESS JUST FWD AND JUST AFT OF THE HOIST POINT (2 EA. INDICATIONS). S/O 339001 N/R 28021SDR VNAA202303311111Unknown · unknownRUD LIMITER FAULT CAUTION MSG IN FLIGHT. / REMOVED AND REPLACED L/H FADEC IAW CRJ 900 AMM 73-21-01-000/400-801-A01. OPS CHECKS GOOD. PERFORMED RUDDER TRAVEL LIMITER OPS CHECK IAW CRJ 900 AMM 27-25-00-710-801-A01. OPS CHECK GOOD AT THIS TIMESDR 2023FA0000163Mount · interferenceDURING ANNUAL INSPECTION ON ONE OF OUR TWO SEAT AIR TRACTORS, WHILE CLEANING INTERIOR OF AIRCRAFT, DAMAGE TO REAR SEAT MASTER CYLINDERS WAS DISCOVERED. UPON ACTUATION OF RUDDER PEDAL, THE MASTER CYLINDER ON EITHER REAR PEDAL CONTACTS THE SAME SIDE RUDDER PEDALSDR AALA202303308855Pcu · unserviceableAIRCRAFT WAS GROUNDED: UPON DEPARTURE IN RIGHT TURN, AIRCRAFT RUDDER VIBRATION FELT. EMERGENCY DECLARED; FLIGHT RETURNED TO SRQ LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202303278855: MAINTENANCE WAS UNABLE TO DUPLICATE ISSUE ON THE GROUND. SUSPECT FAULTY SDR AALA202303278855Unknown · unknownAIRCRAFT WAS GROUNDED: UPON DEPARTURE IN RIGHT TURN, AIRCRAFT RUDDER VIBRATION FELT, EMERGENCY DECLARED; FLIGHT RETURNED TO SRQ LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR 2023FA0000157Actuator · draggingNOTICEABLE YAWING WITH SMALL DISPLACEMENT BUMPS LEFT & RIGHT WITH AUTOPILOT ON OR OFF. INSPECTION FOUND RUDDER BIAS ACTUATORS DRAGGING AND SEALS NEEDED CLEANED AND LUBRICATED.SDR 8G9R20230317001Taper Pin · looseRUDDER TOURQE TUBE INPUT ARM UPPER TAPER PIN FOUND LOOSE. COTTER PIN MISSING.SDR IPXA2023040392542Doubler · damagedINSPECTION TYPE:SEGRUDDER R/H SIDE UPPER T/E HAS LIGHTENING STRIKEFABRICATED DOUBLER IAW SRM-44-11SDR N6WA2023031501Control Unit · brokenRUDDER HAS NO TENSION. INSPECTED AND FOUND SHAFT TO PRIMARY RUDDER FEEL UNIT MECHANISM CAM BROKEN, R&R PRIMARY RUDDER FEEL UNIT MECHANISM IAW CRJ 550-AMM 27-21-05. OPS CHECK GOOD, COMPLIED WITH EO # C550/700-27AD-002-OSDR IPXA2023032192096Rudder · corrodedINSPECTION TYPE:C3AFT LWR RUDDER INTERNAL UPPER SIDE HAS CORROSION.REMOVED AND REPLACED AFT LWR RUDDER IAW AMM 27-20-20 (MINOR)SDR KW7R2023011228002Clevis Bolt · wornDURING SCHEDULED INSPECTION OF RUDDER PEDAL TORQUE TUBE AND ATTACHING ARMS PER CESSNA INSPECTION OPERATION 73 USING SUPPLEMENTAL INSPECTION NUMBER 27-20-05 INSPECTION PROCEDURES: UPON REMOVAL OF THE RUDDER PEDAL ASSEMBLY, THE CLEVIS BOLTS (ITEM #90 IN IPC) SECSDR 2023F00066Arm · gougedCOPILOTS RUDDER PEDAL ADJUSTMENT ARM GOUGED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ38345M1 DATED FEBRUARY 22, 2023; 700-0073 COPILOTS RUDDER PEDAL ADJUSTMENT ARM GOUGE.SDR KCQA20221221Cable · brokenON 11/10/22 WORLDWIDE AIRCRAFT SERVICES, INC. R&R LIB & LOB RUDDER CABLES (AFT SECTION) PNS 120-27649-021 & 120-27649-023 IAW EMB120 AMM 27-00-01. PULLEY UNDER FLOOR PANEL, 263AF, WILL NEED SAFETIED. TENSIONED CABLES AND SAFETIED PULLEY. OPS CHECKS GOOD. *SDR QXEA2023022100025Actuator · malfunctionedRUDDER TRIM MIGRATING LEFT AND RIGHT BELLOW 230 KIAS. NO MISBEHAVIOR ABOVE 230. NO EICAS MESSAGES OR OTHER FAULT. REMOVED FROM SERVICE. INTERROGATED CMC FOUND NO FAULT CODES, PERFORMED GVI OF RUDDER AND TRIM, FOUND NO DEFECTS, PERFORMED RUDDER TRIM ACTUATOR FUSDR ABXA2023021323Unknown · unknownON TAXI OUT RUDDER RATIO EICAS WITH ASSOCIATED OVERHEAD LIGHT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED T/S AND TEST IAW B767-300 FIM 27-09 FT 814, AMM 27-21-00. REMOVED AND REINSTALLED RRCMS PER AMM. NO FAULTS FOUND AT THIS TISDR YENA2023020900141None · noneDURING HEAVY MAINTENANCE: CRACK ON RUDDER HINGE FITTING #3; RUDDER ASSY P/ N 190-09910-401 S/N 0000765010 WAS REPLACED WITH A SERVICEABLE UNIT P/N 190-09910-431 S/N 0000491972 PER EMB 190 AMM 27-21-05-400-801-A & WILL BE INSTALLED PER TASK CARD NO: E190-27-21-SDR AALA202301064403Relay · defectiveAIRCRAFT WAS GROUNDED: AIRCRAFT HAD UNCOMMANDED RUDDER TRIM INPUT. HEADING CHANGE OF AROUND 2, TRIM CHANGE FROM NORMAL OF L 0.3 TO L 1.4 UNITS. HAPPENED WITH BOTH AUTOPILOTS YAW INPUT FELT WORSE ON AUTOPITOT 2 CONTINUED TO NEXT. IN BETWEEN UNCOMMANDED RUDDER TSDR AALA202301062548Actuator · defectiveAIRCRAFT WAS GROUNDED, ACFT HAD UNCOMMANDED RUDDER TRIM INPUT. HEADING CHANGE OF 2, TRIM CHANGE FROM NORMAL L 0.3 TO L 1.4 UNITS. WITH BOTH AUTOPILOTS YAW INPUT, WORSE ON AUTOPITOT 2. BETWEEN UNCOMMANDED RUDDER TRIM, HAD STATUS MESSAGE CAT3 SINGLE ONLY INSDR ABXA20221221155Warning Message · false activationRUDDER RATIO EICAS MESSAGE IN VIEW WITH ASSOCIATED LIGHT ON OVERHEAD PANEL AFTER ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED FIM 27-09 FT 803 + FIM 27-09 FT 814 FOR RUDDER RATIO CHANGER BITE PROCEDURE. ALL TEST PASSESDR TIMA20221223014Control Cable · brokenCONTROL CHECK PRIOR TO FLIGHT NORMAL. FLIGHT KBIL - KGPI. NOTHING NOTICED UNTIL ON LAST 1/4 OF APPROACH, NO RESPONSE FROM RUDDER PEDALS. LANDED THE PLANE UNEVENTFUL.ONCE WEIGHT ON WHEELS NOSE STEERING OPERATED NORMALLY. TAXIED, PARKED AND NOTIFIED MOC. GLACSDR YENA2022120201197Actuator · failedFLT#798, MCO-LGA. AIRCRAFT DIVERTED TO JFK AND DECLARED AN EMERGENCY. SLAT FAULT, REMOVED AND REPLACED LT WING SLAT ACTUATOR IAW AMM 27-84-49. OPS CHECK GOOD.SDR DALA2022112807587Ratio Changer · warning messageSHIP 6803 - MISC/DE - DUE TO L HYD QUANTITY LOW INDICATION CORRECTIVE ACTION: MTC FOUND LEAK COMING FROM RUDDER RATIO. REPLACED RUDDER RATIO, EDP, PTU, ACMP, AND ALL REQUIRED FILTERS. REPLACED RELAYS K105 AND K123. C/W NO GO ODI PREVENTION.SDR ABXA20221121129Circuit Breaker · faultedEICAS MESSAGE RUDDER RATIO DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE CYCLED CB G10 RUDDER RATIO IAW AMM 20-60-01 AND CLEARED FAULT BALLS IAW FIM 27-09. MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE.SDR 2022FA0000770Control Cable · frayedRIGHT RUDDER CABLE FOUND FRAYED WITH REAR PULLEY IN GOOD WORKING CONDITION. BELIEVE THE STAINLESS STEEL CABLES WEAR DIFFERENTLY THAN THE STEEL CABLES AND REQUIRE A 10X MAGNIFYING GLASS TO IDENTIFY WEAR BEFORE THE STRANDS START TO BREAK. THIS TYPE OF WEAR ALLOWSDR YENA2022110101063None · noneDURING HEAVY MAINTENANCE: CRACK AND MIGRATED BUSHINGS IN HINGE FITTING #3 LOCATED IN FWD FRONT SPAR OF RUDDER SURFACE. TC NDT-55-40-00-211-801; REF TOMX WO 2047 NR-00305 RUDDER WAS REPLACED PER AIPC 27-21-05 ITEM 10, AMM 51-60-02-820-801-A ANDF JOB CARD 669 TASDR 1E1R2022102600419Hinge Arm · crackedTHE HINGE ARM BR1 AND ATTACH FORK FITTING OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK AT HOLES #5 AND #7 DURING INSPECTIONS. MAINTENANCE ATTEMPTED TO REMOVE THE CRACK DAMAGE BY OVERSIZING. THE CRACK STILL REMAINS AT EACH HOLE WITH A DIAMETER OF 0.279".SDR AALA202211154827Cap · corrodedAIRCRAFT IN BASE MAINTENANCE: RUDDER COUNTERWEIGHT CAP HAD CORROSION. LOCATED AT RUDDER STA 184.6 AND WATER LINE 153. REMOVED AND REPLACED RUDDER COUNTERWEIGHT CAP PER SRM 51-60-07-0G.SDR AALA202211034827Cap · corrodedAIRCRAFT IN BASE MAINTENANCE: RUDDER COUNTERWEIGHT CAP HAD CORROSION. LOCATED AT RUDDER STA 184.6 AND WATER LINE 153. REMOVED AND REPLACED RUDDER COUNTERWEIGHT CAP PER SRM 51-60-07-0G.SDR SWAA2022101459172None · erodedRUDDER COUNTERBALANCE WEIGHT IS ERODED; LOOSE AND SEALANT IS MISSING FROM THE SEAMS. RUDDER COUNTERBALANCE WEIGHT IS ERODED LOOSE AND MISSING SEALANT FROM THE SEAMS. / [01] REPLACED RUDDER COUNTERBALANCE WEIGHT PER CMM 55-40-09;[02] C/W INSPECTION PER CMM 55-4
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