JASC 2730
Service difficulty reports · 2,650
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 SWAA012659Torque Tube · wornDURING SCHEDULED C4 CHECK, BOTH ELEVATORS FAILED FREE PLAY CHECK. R&R ELEVATOR CONTROL BUS TORQUE TUBE PER MM.SDR MALA010737Control Cable · chafedDURING 4K-CHECK IN CWA, LT OUTBOARD FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FWD ELEVATOR CABLE P/N 7227105-712, IAW SF3 AMM 27-31-15.SDR MALA010735Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSELAGE ELEVATOR CABLE PN7227705-644 IAW SF3 AMM 27-31-15.SDR SWIA200110199Proximity Sensor · failedABORTED TAKEOFF WHEN WE BROUGHT THE POWER UP DUE TO TAKEOFF TRIM WARNING. TRIM CONFIRMED SET AT 4 IN THE GREEN BAND.REMOVED AND REPLACED LEFT TRIM PROXIMITY SENSOR. OPS CHECK GOOD. P/N: ATG120TRSDR MALA010718Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED LT O/B ELEVATOR FWD FUSELAGE CABLE P/N 7227105-712.SDR MALA010717Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED LT I/B FWD ELEVATOR CABLE P/N 7227705-644 IAW SF340 AMM 27-31-15.SDR MALA010707Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B FWD ELEVATOR FUSELAGE CABLE IS CHAFED. MX REPLACED RT I/B FWD FUSELAGE CABLE IAW SF340 AMM 27-31-15-4. P/N 7227705-644.SDR MALA010706Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MX REPLACED RT O/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-712.SDR DL72S011522Module · damagedON LANDING ROLLOUT HYD SYS -A- PRESS AND QTY WENT TO ZERO. FOUND -A- SYS ELEV CONTROL MODULE DAMAGED. SOLENOID BLEW OUT OF THE TOP OF MODULE. REPLACED MODULE.SDR MALA010694Control Cable · chafedDURING 4K-CHECK IN CWA, LT I/B ELEVATOR FUSELAGE CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT I/B ELEVATOR FUSELAGE CABLE P/N 7227705-643 IAW SF340 AMM 27-31-15.SDR MALA010693Control Cable · chafedDURING 4K-CHECK IN CWA, RT I/B ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RT I/B ELEVATOR FUSELAGE CABLE P/N 7227705-643 IAW SF340AMM 27-31-15.SDR MALA010689Control Cable · chafedDURING 4K-CHECK IN CWA, RT O/B FWD ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REPLACED RT O/B FWD ELEVATOR FUSELAGE CABLE P/N 7227105-712 IAW SF340 AMM 27-31-15.SDR QXEA0101487Pushrod · excess playPDX - RIGHT-HAND ELEVATOR TRIM PUSH ROD HAS APPROXIMATELY .020 INCH RADIAL PLAY ON ROD BEARING AT IDLER ARM END. REPAIRED IAW DASH-8 MM 27-36-00.SDR 2001F00402Indicator · wornFLT 9389 - MIA/FLL - DURING FLIGHT, ELEVATOR TRIM WHEEL POSITION INDEX MARKER DOES NOT CORRESPOND TO TRIM SETTINGS. REMOVED AND REPLACED ELEVATOR TRIM DIAL INDICATOR ASSEMBLY AND INDEXED. OPERATIONAL CHECK NORMAL. (M)SDR SIM2001F00000Bushing · wornBUSHINGS ARE MIGRATING CAUSING EXCESSIVE WEAR TO ELEVATOR CONTROL QUADRANT SUPPORT FITTINGS.SDR MALA010685Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B FWD ELEVATOR FUSELAGE CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B FWD ELEVATOR FUSELAGE CABLE P/N 7227105-711 IAW SF340 AMM 27-31-15.SDR ABXA010449Computer · faultyCREW REPORTED ELEVATOR CONTROL SURFACE PRESSURE MUCH HIGHER THAN NORMAL. AIRCRAFT WAS DIFFICULT TO ROTATE ON TAKEOFF. A VIBRATION WAS ALSO FELT IN THE CONTROL YOKE THREE TIMES ON APPROACH TO ILN. REPLACED THE ELEVATOR FEEL COMPUTER IAW B767 AMM 27-31-19-4. SDR 2001UALA01777Computer · failedLANDING FLARE CONTROL PRESSURE TWICE THE NORMAL EFFORT (PITCH PRESSURE EXTREMELY HIGH). FAILURE OF THE ELEVATOR FEEL COMPUTER CAUSED THE EXTRA FORCE REQUIRED TO OPERATE THE CONTROL COLUMN. REPLACED THE ELEVATOR FEEL COMPUTER.SDR MALA010669Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, RT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD ELEVATOR CABLE P/N 7227105-712 IAW SF340 AMM 27-31-15.SDR MALA010668Control Cable · chafedDURING 4K-CHECK IN CWA, FOUND RT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT I/B FWD FUSELAGE CABLE P/N 7227705-643, IAW SF340 AMM 27-31-15.SDR MALA010664Control Cable · chafedDURING 4K-CHECK, FOUND LT ELEVATOR FWD I/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B FWD 7227705-643 P/N 7227705-643 IAW SF340 MM 27-31-15.SDR MALA010662Control Cable · chafedDURING 4K-CHECK IN CWA, LT ELEVATOR FWD O/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT ELEVATOR FWD FUSELAGE CABLE REPLACED IAW SF340 AMM 27-31-15.SDR AUS20010907Control Cable · frayed(AUS) ELEVATOR DOWN CONTROL CABLE FRAYED.SDR CA010828023Torque Tube · cracked(CAN) UPON PERFORMING THE SB2145 ON THE COMPONENT.FIRST INSPECTION FROM FACTORY, WE DO IT UPON ARRIVAL FOR QUALITY REASONS. A CRACK WAS FOUND DURING THE LPI PROCESS.THE CRACK TRAVELS FROM INSIDE THE HOLE TO APROX. 4MM OUTSIDE THE HOLE RUNNING AXIAL ALONG THE SDR 2001FA0000365Screw · looseEXCESS FRICTION IN PITCH, (ELEVATOR) CONTROL. DISASSEMBLY OF CONTROL, REVEALED RETAINING SCREW HAD BACKED OUT OF NYLON SLIDE. UNCONTAINED PARTS OCCASSIONALLY POSITIONED THEMSELVES THROUGH OUT NORMAL MOTION OF THE CONTROL SO AS TO CREATE EXCESS FRICTION. (M)SDR AUS20010918Actuator · leaking(AUS) RT ELEVATOR CENTRE ACTUATOR LEAKING.SDR COMA0160586DamperYAW DAMPER #2 WOULD NOT ENGAGE DURING TAXI-OUT, AIRCRAFT RETURNED TO THE GATE.CLEANED THE ELECTRICAL CONNECTOR FOR #2 YAW DAMPER.SDR 2001UALA01661Servo · defectiveELEVATOR AILERON COMPUTER WARNING FAULT. A/C HAD HISTORY OF ELAC 1 PITCH FAULT AND ELAC 2 -RELATED PROBLEMS. IT WAS DETERMINED THAT THE LEFT GREEN ELEVATOR SERVO CONTROL 34CE1 NEEDED TO BE REPLACED. OPS TEST WAS ACCOMPLISHED.SDR CA010727023Bushing · loose(CAN) BUFFETING FELT THROUGH THE FLIGHT AND INCREASE IN FREQUENCY DURING CLIMB OUT. THE LEFT ELEVATOR WAS INDICATING LOWER THAN THE RIGHT AND WOULD FLUCTUATE UPWARD. INVESTIGATION REVEALED LEFT END OUTBOARD POWER ACTUATOR (P.C.A.) EYE END BUSHING LOOSE AND SUPSDR UPS01536406Computer · faultyINSPECTION TYPE:N/A PILOT REPORT, YOKE STIFF IN PITCH MODE. ACCOMPLISHED FIM 27-31-00 FIG 105 ELEV CTRLS BINDING. REMOVED AND REPLACED ELEV FEEL COMPUTER PER MM 27-31-19; ELEVATOR SYS PASSED THE ELEV FEEL SYS FORCES TEST ACFT OK FOR SERVICE.SDR 2001FA0000277Housing · corrodedHOUSING ASSEMBLY IS CORRODED ON THE SEAL PLATE SURFACE, IN THE CHECK VALVE PORTS AND BOLT HOLES. HOUSING ASSEMBLY IS MADE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS.SDR SWAA012054Bearing · wornDURING SCHEDULED C4 CHECK, BOTH ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BEARINGS AT ELEVATOR TORQUE TUBE PER MM.SDR LS1R074928Bellcrank · wornPART IS WORN EXCESSIVELY.SDR MALA010632Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, RT I/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE INSTALLED RT I/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-644, S/N PEG2SFEX IAW SF3 AMM 27-31-15.SDR MALA010631Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, RT O/B FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE INSTALLED RT O/B FWD ELEVATOR CABLE P/N 7227105-712, IAW SF3 AMM 27-31-15.SDR MALA010630Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, LT I/B ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LT I/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-644, S/N PEG2SFEX, IAW SAAB AMM 27-31-15-4.SDR MALA010629Control Cable · chafedDURING 4K-CHECK IN CWA, LT O/B ELEVATOR CABLE IS CHAFED. MAINTENANCE REMOVED AND REPLACED LT O/B FWD FUSELAGE ELEVATOR CABLE P/N 7227105-712/711, SN/PEG2SFEX.SDR SWAA012039Bearing · wornDURING SCHEDULED C4 CHECK, SWA SI 11052-55, LT & RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT& RT UPPER ELEVATOR PUSH ROD BEARINGS PER MM.SDR 2001FA0000278Housing · corrodedHOUSING ASSEMBLY IS CORRODED ON THE SEAL PLATE SURFACE, IN THE CHECK VALVE PORTS AND BOLT HOLES. HOUSING ASSEMBLY IS MADE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS.SDR MASA01068Computer · malfunctionedFLT 5869 - DCA-CHS - RETURNED TO DCA DUE TO MAIN PITCH TRIM SYSTEM INOPERATIVE AFTER TAKEOFF. MAINTENANCE RESET IC6001 COMPUTER SYSTEM. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR N3X2001F00000Bellcrank · looseBEARING HOUSING IS LOOSE IN BELLCRANK.SDR 2001FA0000128Rod · corrodedELEVATOR PUSH PULL CONTROL ROD VERY RUSTY AND PITTED. LOCATED IN TAIL SECTION WHERE MOISTURE AND CONTAMINATION ACCUMULATE.SDR MALA010585Control Cable · wornDURING 4K-CHECK IN CWA, RHOB ELEVATOR CABLE WORN FWD FUSELAGE. MAINTENANCE REMOVED AND REPLACED RHOB FWD FUSELAGE ELEVATOR CABLE P/N 7227105-712 IAW SF3 AMM 27-31.SDR SWAA012087Bearing · wornDURING SCHEDULED D CHECK AT DALFORT, FOUND BOTH LH & RH ELEVATOR TORQUE TUBE PUSH ROD ATTACH BEARINGS WORN. R&R PUSH ROD BEARINGS PER OHM.SDR SWAA011985Bearing · wornDURING SCHEDULED D-CHECK, FOUND RT ELEVATOR PUSH ROD ATTACH BEARING WORN. REMOVED AND REPLACED BEARING AND SLEEVE PER MM.SDR SWAA011966Bushing · wornDURING SCHEDULED SERVICE CHECK, SI 11052-55, FOUND RH ELEVATOR TAB # 3 HINGE BUSHING WORN. R&R HINGE BUSHING PER MM.SDR VNAA0107011Warning System · activatedAFTER APPLYING POWER FOR TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION CAS AND ELEVATOR TRIM CAS MESSAGE. THE CREW ABORTED TAKEOFF AND EXITED THE RUNWAY. THE CREW MOVED THE ELEVATOR TRIM TO A POSITION FURTHER IN THE GREEN BAND SETTING AND THE MESSAGE CLSDR EVA001Balance Weight · detached1. DURING C10 CHECK FOUND R/H HORIZONTAL STABLIZER PANEL BROKEN.2. AFTER INSPECTION FOUND R/H OUTBOARD ELEVATOR SUPPORT RIBS OF BALANCE WEIGHT FALLING DOWN AND DAMAGED TO THE ELVATOR PANEL.3. REPLACE THE R/H OUTBOARD ELEVATOR PER BOEING AMM 27-31-01.CONDITION SDR MALA010560Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED I/B CABLE P/N 7227705-644 IAW SF340A MM 27-31-15.SDR MALA010559Control Cable · chafedFOUND DURING 4K-CHECK IN CWA, RHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RHOB CABLE P/N 7227105-712 IAW SF340A MM 27-31-15.
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