JASC 2730
Service difficulty reports · 2,649
Reports filed under 2730 · Elevator 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 = '2730' 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 = '2730' 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 HALA2017032000073Sensor · unknownELEVATOR SPLIT MESSAGE WAS DISPLAYED ON APPROACH TO LAND, SPEED 160KTS, FLAPS 18 GEAR DOWN. MESSAGE EXTINGUISHED AT 145KTS. ACCOMPLISHED FIM 27-30-804, R & R THE LEFT ELEVATOR POSITION SENSOR IAW AMM 27-34-01.SDR 2017FA0000085Control Cable · damagedCUSTOMER REQUEST, LOOK INTO A HYDRAULIC LEAK IN MAINTENANCE BAY. UPON ENTERING MAINTENANCE BAY FOUND BOTH ELEVATOR AND RUDDER SERVO CABLES DAMAGED, BOTH REQUIRING REPLACEMENT.SDR SWAA2017020611689Control Rod · corrodedLT INBOARD ELEVATOR CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.SDR SWAA2017020611688Control Rod · corrodedLT OUTBOARD ELEVATOR CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.SDR SWAA2017020611687Control Rod · corrodedRT OUTBOARD ELEVATOR TAB CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.SDR SWAA2017020611686Control Rod · corrodedRT INBOARD ELEVATOR CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.SDR F35R011220173Control Cable · frayedUP ELEVATOR CABLE PART NUMBER 3-1072 HAD MULTIPLE BROKEN/FRAYED WIRE STRANDS AT AFT MOST PULLEY LOCATION (APPROX FUSELAGE STATION 167.50, JUST AFT OF THE FRONT STABILIZER ATTACH POINT) AND MID PULLEY (APPROX LOCATION UNDER REAR SEAT). DOWN ELEVATOR CABLE PART SDR F35R201701122Control Cable · frayedUP ELEVATOR CABLE PART NUMBER 3-1072 HAD MULTIPLE BROKEN/FRAYED WIRE STRANDS AT AFT MOST PULLEY LOCATION (APPROX FUSELAGE STATION 167.50, JUST AFT OF THE FRONT STABILIZER ATTACH POINT) AND MID PULLEY (APPROX LOCATION UNDER REAR SEAT). DOWN ELEVATOR CABLE PART SDR SIMA20170104001Actuator · failedAT FL 30.3, RECEIVED A PTRIM MAIN INOPERATIVE, NON EICAS. USED BACKUP PITCH TRIM TO DIVERTED. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR IAW AMM 27-40-02. OPS CHECKED GOOD IAW AMM TASK 27-40-02-700-801-A/500.SDR YENA201612311127Servo Valve · failedFLT 368, PUJ-JFK, DIVERTED TO SJU. EMERGENCY DECLARED. CLIMBING THROUGH 310 AT MACH .76 VERY STRONG VIBRATIONS WERE FELT THROUGHOUT THE AIRCRAFT. SLOWED DOWN TO MACH .72 AND VIBRATION DISAPPEARED. ACCOMPLISHED TSM 05-50-00-810-801 (VIBES). R & R RT B ELEV SERVSDR YENA201612311126Fitting · failedFLT 368, PUJ-JFK, DIVERTED TO SJU. EMERGENCY DECLARED. CLIMBING THROUGH 310 AT MACH .76 VERY STRONG VIBRATIONS WERE FELT THROUGHOUT THE AIRCRAFT. SLOWED DOWN TO MACH .72 AND VIBRATION DISAPPEARED. ACCOMPLISHED TSM 05-50-00-810-801 (VIBES). R & R RT B ELEV SERVSDR YENA201612311125Control Servo · failedFLT 368, PUJ-JFK, DIVERTED TO SJU. EMERGENCY DECLARED. CLIMBING THROUGH 310 AT MACH .76 VERY STRONG VIBRATIONS WERE FELT THROUGHOUT THE AIRCRAFT. SLOWED DOWN TO MACH .72 AND VIBRATION DISAPPEARED ; ACCOMPLISHED TSM 05-50-00-810-801 (VIBES). R & R RT B ELEV SERSDR F35R201701121Control Cable · frayedUP ELEVATOR CABLE PART NUMBER 3-1072 HAD MULTIPLE BROKEN/FRAYED WIRE STRANDS AT AFT MOST PULLEY LOCATION (APPROX FUSELAGE STATION 167.50, JUST AFT OF THE FRONT STABILIZER ATTACH POINT) AND MID PULLEY (APPROX LOCATION UNDER REAR SEAT). DOWN ELEVATOR CABLE PART SDR COEA2016120501953Trim Switch · dirtyDURING CLIMB OUT, PITCH TRIM CLUTCH SWITCH DOES NOT RELEASE AFTER NOSE DOWN INPUT. RETURN TO DEPARTURE. SWITCH CLEANED. OPS CHECKED GOOD.SDR FDEA201612024310Feel Unit · wornF/O'S CONTROL COLUMN HAS RESISTANCE WHEN APPLYING FWD (NOSE DOWN) ELEVATOR. CAPT'S CONTROL COLUMN INTERMITTENTLY SHOWS SAME. REPLACED THE ELEVATOR FEEL UNIT.SDR GLBA2016112900619Duct · damagedPILOT REPORTED THAT THE CAPTAIN`S YOKE HAS ADNORMALY HIGHT AMOUNT OF RESISTANCE WHEN PRESSING FORWARD IN LEVEL FLIGHT, NO RESISTANCE WHEN MOVING YOKE AFT. MAINTENANCE FOUND DUCTING IN THE PATHWAY OF THE YOKE SPROKET ASSY AND CHAIN, SECURED DUCTING OUT OF THE WSDR HALA2016120700527Torque Tube · corrodedELEVATOR CONTROL TORQUE TUBE ON AFT SIDE OF STABILIZER CENTER BOX IS CORRODED. 12/03/16 REMOVED LOWER ELEVATOR CONTROL TORQUE TUBE FROM ELEVATOR FEEL UNIT IAW AMM 27-31-17 STEP 1 G (1) (D). INSTALLED LOWER ELEVATOR CONTROL TORQUE TUBE ON ELEVATOR FEEL UNIT ISDR DALA2016112109112Torque Tube · corrodedCORROSION ON RT AND LT ELEVATORS TORQUE TUBE ENDS. THE TORQUE TUBE ENDS WERE REPLACED IAW AMDS 2730-4234.SDR QXEA2016111700729Processor · malfunctionedIOP2 FAIL ED MESSAGE & AVIONICS CAUTION MESSAGE. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERAGATED CDS AND FOUND " NO DATA FROM IOP2". REMOVED & REPLACED NR 2 IOP IAW MTC 6314101 FLT. RETURNED TO SERVICE.SDR IPXA2016110410259Computer · failedDURING CRUISE AT FL220, PITCH FEEL 2 DISPLAYED ON LEFT ECAM. PITCH 2 FEEL FAULT LIGHT ON OVERHEAD. RESET AND FAILED AGAIN. R & R PITCH FEEL COMPUTER IAW MM 27-23-26-0401.SDR CALA2016101700759Actuator · failedHORIZONTAL STAB ACTUATOR FAILED WITH DISCOLORED WATER FROM BALL NUT. REMOVED AND REPLACED HSTA IAW AMM 27-41-81-400-801 AND EA 2740-01227 OPS 3 OPS 4.SDR AWKA201610130001Actuator · failedWHILE ON DEPARTURE FROM KLRD, FLIGHT CREW RECEIVED AN AMBER PITCH FEEL FAIL CAS MESSAGE, THE CHECK LIST WAS THEN ACCOMPLISHED WHICH STATES TO LAND AS SOON AS POSSIBLE. CREW ELECTED TO RETURN TO KLRD, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. DURING SDR DALA2016092906952Spring · failedAFTER A ROUTINE APPROACH, DURING THE FLARE MANEUVER, THE CONTROL COLUMN WAS REPORTED TO MAKE AN ABRUPT MOTION IN THE FO'S HANDS. ELEVATOR AUTHORITY APPEARED TO HAVE BEEN RESTRICTED PER THE PILOT WRITE-UP. MAINTENANCE DISCOVERED THE ELEVATOR LOAD FEEL & CENTERISDR ASOA20160926050RSwitch · stuckCREW REPORTED NOSE UP PITCH TRIM(UNCOMMANDED) RIGHT AFTER TAKEOFF. POSSIBLE PITCH TRIM RUNAWAY. AURAL WARNING"TRIM, TRIM" BUT NO EICASE MESSAGE. SMOOTH LANDING REPORTED ON AIR RETURN BACK TO EWR. MX REMOVED AND REPLACED THE F/O'S YOKE PITCH TRIM SWITCH WITH OPSDR SOKF20160902006Servo Control · faultyDURING CLIMB, THE ACFT RETURN TO DEPARTURE DUE TO ECAM WARNING FLIGHT CONTROL ELAC 2 PITCH FAULT, AT STATION, PERFORMED TSM 27-93-00-810-867-A. R & R ELEVATOR SERVO CONTROL LT SIDE, 34 CE1 IAW AMM 27-34-51-000-001-A AND 27-34-51-400-001-A. ADJUSTMENT TEST OFSDR FDEA201608102850Computer · malfunctionedDURING CLIMB OUT, ELEVATOR FLUTTER FROM 260 KTS UP TO 300 KTS. NO CHANGE WITH AUTO PILOT ON OR OFF. R & R THE ELEVATOR FEEL COMPUTER.SDR YENA20160802676Warning System · false activationEMERGENCY DECLARED, WHILE DESCENDING INTO DESTINATION AT ABOUT 16000 FT, CREW RECEIVED 2 EICAS MESSAGES. PITCH CONTROL DISC AND AUTO PILOT FAIL. AN EMERGENCY WAS DECLARED INTO DESTINATION. ACFT LANDED UNEVENTFULLY, NO FAULTS FOUND. TRANSITORY CONDITION.SDR HNAA201662000189Actuator · malfunctionedTRIM MAIN INOPERATIVE WARNING MESSAGE ILLUMINATED ON EICAS DURING CLIMB OUT 41500. R & R THE HSCU, NO FIX. CAN RESET P TRIM INDICATION WITH TRIM FULL DOWN. FAIL, WHEN TRIM GOES UP BEFORE FIRST CARROT. INSTALLED IAW AMM TASK 27-40-01-400-801-A.SDR VQIA201607290026Servo · failedREPORTED AN ABNORMAL VIBRATION IN THE AIRFRAME DURING THE FLIGHT CONTROL CHECK AFTER PUSH BACK AND RETURNED TO THE GATE. LOCAL MAINTENANCE CONTRACTOR EVALUATED AND THE CONFIRMED THE CONDITION, THE AIRCRAFT WAS REMOVED FROM SERVICE FOR TROUBLESHOOTING AND REPASDR DALA2016060204340Rod End · corrodedLT ELEVATOR OTBD. PCA PGO ROD END CORRODED. R & R LT ELEVATOR OTBD PCA POGO ROD IAW AMM 27-31-06, FUNCTIONALLY CHECK/ADJUSTMENT WILL BE ACCOMPLISHED ON N/RSDR AALA201605249009Elevator · out of adjustAIRCRAFT WAS GNDED. AIRFRAME VIBRATION DURING CLIMB FROM 3,000 FL - 18,000 FL. ACCOMPLISHED AN ADJUSTMENT OF THE ELEVATORS IAW AMM 27-34-00-820-003 & REPLACED 6 EACH RUDDER HINGE ARM FITTINGS, 1, 2, 3, 4, 5 & 7, DUE TO EXCESSIVE PLAY IAW AMM 55-36-211-00400-SDR 2016FA0000211Control Cable · brokenELEVATOR CONTROL CABLE BROKE DUE TO CORROSION AT THE CABLE CONNECTOR FOR THE TURNBUCKLE. RECOMMEND AN INSPECTION WITH A 10 POWER MAGNIFYING GLASS TO DETECT ANY CRACKS AT THE CABLE TURNBUCKLES ATTACHMENTS.SDR A6WA201643815Elevator · jammedELEVATOR JAMMED ON APPROACH WITH AUTO PILOT OFF. BROKE LOOSE WITH ADDITIONAL FORCE.SDR DALA2016042103256Rod End · corrodedLT ELEVATOR INBD PCA. POGO ROD END IS WORN AND RUSTED. REPLACED INPUT RODS, 2 EA AND POGO ROD, REF AMM 27-31-06.SDR O2GA2016042550701Proximity Switch · out of adjustNO TAKEOFF WARNING HORN & MASTER CAUTION ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED ELEVATOR TRIM POINTER & PROXIMITY SWITCH. TAKEOFF WARNING SYS OPERATIONAL CHECKED GOOD DURING ENG RUNS & HIGH SPEED TAXI. ACFT WAS RETURNED TO SERVICE.SDR DXTA2016041306231Torque Tube · corrodedLEFT ELEVATOR TORQUE TUBE CORRODED OUT OF LIMITS. FOUND DURING COMPLETE PAINT PROCESS. REMOVED TORQUE TUBE, PN UNKNOWN, FROM LT ELEVATOR PN 6634200-9, SN 0000106 DUE TO LEVEL 2 CORROSION. INSTALLED NEW TORQUE TUBE PN 6634002-15 IAW SRM 51-40-03, 51-40-04, 5SDR DXTA2016041306230Torque Tube · corrodedRIGHT ELEVATOR TORQUE TUBE CORRODED OUT OF LIMITS. FOUND DURING COMPLETE PAINT PROCESS. REMOVED TORQUE TUBE DUE TO LEVEL 2 CORROSION. INSTALLED NEW TORQUE TUBE PN 6634002-16 IAW SRM 51-40-03, 51-40-04, 51-40-05, 51-40-06, 55-20-01 & MM 20-32-00. THIS IS COSDR AALA201603099014Control Servo · defectiveAIRCRAFT WAS GNDED. CREW RECEIVED ON TAKEOFF A FLIGHT CONTROL ELAC 2 PITCH FAULT & ABORTED THE TAKEOFF. REPLACED THE ELAC 2 & LT INBD SERVO VLV IAW AMM 27-93-34 & AMM 27-34-51. SEE AALA201603089043 FOR ADDITIONAL PART INFORMATION.SDR IPXA2016040901857Coupler · chafedINSPECTION TYPE:3C, ELEVATOR LOAD FEEL MOMENT ARM CHANGER COUPLER ARM CHAFE DAMAGE. REPAIRED CHAFE DAMAGE TO NOTED ARM IAW EA 011-2730-01-A6181, REV IR AND EO MD11-2730-60303-A.SDR 2016FA0000108Servo · intermittentPILOT REPORTS THAT IMMEDIATELY AFTER ROTATION, THE ELEVATORS BOUND IN THE MOSTLY UP POSITION. AILERONS FUNCTIONED NORMALLY. ELEVATOR TRIM WAS MOVABLE. POWER WAS REDUCED, AIRSPEED KEPT AT 135 KTS, AND THE ACFT RETURNED TO DEPARTURE. ELEVATOR CONTROL WAS RESTSDR QXEA2016030200169Switch · faultedPITCH TRIM CAUTION ABOUT 40-50 KNOTS. ABORTED TAKEOFF AT 100 KNOTS. NO EXCESSIVE BRAKING. INTERROGATED CDS IAW AMM 45-00-27-742-801 FOUND FAULT PILTRIM SW. ERASED FAULT CODED IN CDS. PERFORMED OPS TEST OF THE PITCH TRIM SYSTEM IAW AMM TASK 27-40-00-710-802SDR FDEA201603020757Regulator · damagedFLIGHT CONTROLS, DURING BUY BACK, FOUND ELEVATOR TENSION REGULATOR SPRING GUIDE BROKEN. LT SIDE ELEVATOR TENSION REGULATOR R & R IAW AMM 27-31-12 REV 115. CONTROL CABLE FOR ELEVATOR TENSION REGULATOR REMOVED & INSTALLED AFTER MX IAW AMM 27-31-12 REV 115. ADSDR QXEA2016022500158Control Unit · malfunctionedFCS ECU 1 CIRCUIT BREAKER POPPED DURING CLIMBOUT. RETURNED TO FIELD. LANDING UNEVENTFUL. ROLL SPOILER INBD GROUND, PITCH TRIM ELEVATOR FEEL CAUTIONS ILLUMINATED ELEVATOR ASYMMETRY CAUTION ILLUMINATED ON LANDING ROLL OUT. R & R FLIGHT CONTROL ELECTRONIC CONTSDR AALA20160525002Bearing · wornCLIMBING THROUGH 18,000 FEET, AT 280 KNOTS WITH THE NR 1 AUTOPILOT ENGAGED, A DISTINCT & PRONOUNCED BOUNCE & VIBRATION SET UP IN THE LONGITUDINAL AXIS OF THE ACFT. VIBRATION REDUCED WHEN SPEED DECREASED. THE FLIGHT DECLARED AN EMER & DIVERTED WITHOUT FURTHERSDR AALA20160525001Bearing · wornCLIMBING THROUGH 18,000 FEET, AT 280 KNOTS WITH THE NR 1 AUTOPILOT ENGAGED, A DISTINCT & PRONOUNCED BOUNCE & VIBRATION SET UP IN THE LONGITUDINAL AXIS OF THE ACFT. VIBRATION REDUCED WHEN SPEED DECREASED. THE FLIGHT DECLARED AN EMER & DIVERTED WITHOUT FURTHERSDR DALA2016022501431Control Rod · corrodedCORROSION ON RT ELEVATOR CONTROL ROD WHICH ATTACHES ELEVATOR CONTROL MECHANISM IN AFT EQUIPMENT ACCESS TO INBD CONNECTING LINK AT INBD END OF RT HORIZONTAL STABILIZER ACCESS NR 345AB. ROD END. R & R RT ELEVATOR CONTROL ROD IAW AMM-27-31-15/20-11-00, ASSET 00SDR 2016FA0000075Pulley · failedPILOT REPORTED ELEVATOR TRIM VERY STIFF AND STICKING. UPON INSPECTION OF ELEVATOR TRIM CONTROL CABLES, FOUND PULLEY, PN MS24566-1B AT BS 244 HAD BEEN APPROXIMATELY 90 PERCENT DESTROYED BY ELEVATOR TRIM CABLE TURNBUCKLE. WHEN ELEVATOR TRIM OPERATED, TURNBUCKLSDR CA160209010Pcu · leaking(CAN) LANDING GEAR DID NOT RETRACT, AFTER GEAR UP SELECTION ALL GEARS DID NOT RETRACT FOR APPROX 3 MINS. ALL GEAR THEN RETRACTED. ONCE GEAR UP AND LOCKED A NR 2 HYD PUMP CAUTION AND A PTU FAIL LIGHT ILLUMINATED. THESE THEN RESET WITHOUT INTERACTION. PILOT DECISDR A6WA201643528Unknown · malfunctionedELEVATOR INPUT VIA YOKE SEEMS HEAVY, ALL PHASES OF FLIGHT & ON GND, CAPTAINS & FIRST OFFICERS SIDE.SDR AWKA7500127Bearing · corrodedDURING CLIMB OUT, THE FLIGHT CREW NOTED AT SEVERAL ALTITUDE CHANGES. WHILE PULLING THE CONTROL YOKE BACK TO CLIMB & ALSO MOVING THE YOKE FWD TO CAPTURE THE ASSIGNED ALTITUDE THAT THERE WAS CONSIDERABLE ROUGHNESS FELT IN THE CONTROL YOKE. ALSO, THEY OBSERVED
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