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.

SDR UALA2013012300402Actuator · failedON TAKE OFF ROLL, LEFT ENGINE HIGH STAGE BLEED INDICATION ILLUMINATED. ABORTED TAKE OFF. TROUBLESHOT PER FIM 27-31-00-10 1 FIG 108. FOUND RIGHT SYSTEM OUTBOARD PCA ON LT ELEVATOR BAD. REPLACED PCA PER MM, OPS CHECKED GOOD.Jan 22, 2013 · N560UA · Boeing 757222SDR 9JLA2013020104423Actuator · leakingTHE CREW REPORTED AFTER TAKEOFF, DURING THE CLIMBOUT, RECEIVED A LT LOW HYD QTY CAS MESSAGE. THE CREW STATED THAT THEY COMPLETED THE CHECKLIST IN THE POH AND SHORTLY AFTER THAT THE LT HYD PRESSURE BEGAN TO FLUCTUATE BETWEEN ZERO AND 2800 PSI. THE CREW DIVERTJan 17, 2013 · N2HL · Gulstm 200SDR DJFA20130116001Control Cable · chafedDURING A SCHEDULED INSPECTION, MX FOUND THE ELEVATOR CABLES TO HAVE CHAFE MARKS, PN: 505-15041-403 & 505-15042-403. LOCATION OF CHAFE MARKS WERE IN THE VERTICAL STAB AT THE FITTING FORWARD OF THE RUDDER TRIM ACTUATOR. BOTH CABLES WERE REPLACED.Jan 16, 2013 · N311FL · Emb EMB505SDR USAA2013011800002Bearing · wornFLT 1967, EN ROUTE. DURING APPROACH, ELEVATOR REQUIRED AN ABNORMALLY HIGH AMOUNT OF FORCE TO KEEP THE NOSE OF THE AIRCRAFT UP. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO VISUAL FAULTS. THE AIRCRAFT WAS MAINTJan 16, 2013 · N200UU · Boeing 7572B7SDR CALA2013011600041Pcu · leakingHYDRAULIC PRESSURE LOW, COMPLIED WITH UNABLE TO EXTEND T/E FLAPS BEYOND 5. L/E SLAT DISAGREE T/E FLAP DISAGREE, R & R LT, INBD (CTR HYD SYS) ELEVATOR ACTUATOR, L/E SLAT INBD MOTOR & T/E FLAP PDU ELECTRIC MOTOR, OPS CHECKED GOOD.Jan 16, 2013 · N66057 · Boeing 767424ERSDR UALA2013011600263Computer · faultyPILOT REPORTS RT BLUE ELEVATOR SERVO BOXED WITH ELEV SERVO FAULT. REPLACED SEC 1 FOR FAULT "SEC 1 OR WIRING FROM R Y ELEVATOR MODE TRANSDUCER 34CE2", OPS CHECKED GOOD.Jan 13, 2013 · N802UA · Airbus A319131SDR DJX2013F00001Rivet · looseRIVETS LOOSE, HOLDING INBD ATTACH BELLCRANK LEVER TO TORQUE TUBE. BELLCRANK LEVER HAS PLAY TO TORQUE TUBE.Jan 11, 2013 · N948CE · Beech B200SDR UALA2013010900162Pcu · failedLEFT STAB I/B ELEVATOR PCU FAILED DURING FREEPLAY CHECK. PCU WAS INTERNALLY BYPASSING DURING FREEPLAY CHECK. REMOVED & REPLACED LEFT ELEV INBD PCU PER MM 27-31-05. PERFORMED WEAR CHECK OF ATTACH POINTS - NO DEFECTS NOTED. PERFOMRED OPS & FREEPLAY CHECK - CJan 7, 2013 · N520UA · Boeing 757222SDR HNAA2013010401147Unknown · malfunctionedCREW REPORTS AFTER LEVELING, AFTER DESCENT, ACFT RAN OUT OF NOSE DOWN TRIM. CHECKED LT AND RT ELEVATOR SPRING TABS AND TRIM TABS FOR TRAVELS. ALL TRAVELS ARE WITHIN LIMITS FOR AMM 27-00-00.Jan 4, 2013 · N937HA · Dhav DHC8102SDR HNAA2013010401142Control Cable · out of adjustELEVATOR CONTROLS VERY SLOPPY AND DIFFICULT TO MAINTAIN PITCH ATTITUDE ON APPROACH AND LANDING. ADJUSTED ELEVATOR CABLE TENSIONS IAW MM 27-00-00. COMPLETED RII OF ELEVATOR CABLE TENSION.Jan 4, 2013 · N914HA · Dhav DHC8102SDR UALA2012122407374Pcu · leakingLEFT OUTBD ELEVATOR PCA LEAKING AT 90 DROPS PER MINUTE AFTER PRESSURIZING RIGHT HYDRAULICS. REMOVED OLD AND INSTALLED NEW UNIT PER 27 31 05. INSTALLATION TORQUE AND PART VERIFICATION COVERED UNDER PTT 8302020.Dec 22, 2012 · N555UA · Boeing 757222SDR UALA2012121907283Computer · malfunctionedCREW REPORTS FLT CONTROL ELEVATOR SERVO FAULT: FOR NR 2 ELAC RESET. RESET ELACS CB'S AND PERFORMED EFCS TEST, ALL SYSTEMS NORMAL.Dec 19, 2012 · N826UA · Airbus A319131SDR MTNA121120120001Elevator · obstructedDURING INITIAL CLIMBOUT OF REPOSITION FLIGHT 7559 MSN-CID, MADE A PRECAUTIONARY AIR TURNBACK INTO MSN DUE TO ABNORMAL PITCH FORCES. INSPECTION OF AIRCRAFT FOUND ICE ON THE RIGHT ELEVATOR. REMOVED ICE AND PERFORMED VISUAL INSPECTION OF ELEVATOR TRIM IAW ATR72Dec 11, 2012 · N800FX · Aerosp ATR72212SDR UALA2012121207181Module · faultyELEV ASYM EICAS MSG ON TAXI IN. REPLACED LEFT SAM M524 REF MM27-09-00 AND FIM 27-09-00, ACCOMPLISHED CAT III TEST, NO FAULTS.Dec 8, 2012 · N587UA · Boeing 757222SDR CA121210006Housing · separated(CAN) DISPATCH WAS NOTIFIED BY CREW THAT DURING TAXI FOR TAKEOFF, THE, A-SYSTEM HYDRAULIC PRESSURE WAS DROPPING AND THE QTY HAD DROPPED TO ZERO. THE CREW REQUESTED A TOW TO RETURN THE ACFT TO THE RAMP, NO NOSE WHEEL STEERING AVAILABLE. MAINTENANCE TOWED THEDec 7, 2012 · Boeing 727225SDR UALA2012121207180Actuator · faultyELEV ASYM STATUS MESSAGE ON CLIMBOUT. CONTROLS FEEL NORMAL AND ELEV INDICATORS APPEAR NORMAL. REMOVED AND REPLACED ASYMMETRY LIMITER ACTUATOR IAW AMM, OPS CHECKS GOOD.Dec 7, 2012 · N587UA · Boeing 757222SDR CA121211009Control Cable · frayed(CAN) FWD ELEVATOR TRIM CABLE FRAYED SEVERAL PLACES AT TRIM SERVO PULLEY.Dec 4, 2012 · Piper PA31SDR COZR20121130002Guard · out of positionDURING AN UNDERFLOOR INSPECTION, FOUND THE CABLES FOR THE AILERON AUTOPILOT SERVO RUBBING ON THE CABLE DRUM GUARDS. FURTHER INVESTIGATION FOUND THE CABLE GUARDS CAN BE LOCATED IN DIFFERENT POSITIONS ON THE SERVO. THIS IS TO ALLOW FOR DIFFERENT CABLE ANGLES DNov 29, 2012 · N118K · Cessna 501SDR 2012FA0000783Turnbuckle · brokenAFT FUSELAGE ELEVATOR CABLE TURNBUCKLE END, CRACKED AND BROKE OFF AT THE BARREL SIDE IN THE SHANK PART, .6250" BACK FROM THE THREADED PORTION OF THE TURNBUCKLE END, JUST AT THE THICKER PART WHERE THE SAFETY WIRE HOLE IS, OPPOSITE THE SWEDGED END. THERE WAS ENov 29, 2012 · N41EK · Piper PA32RT300SDR CA120316001Control Cable · out of alignment(CAN) DURING THE 12 MONTH AND 48 MONTH DETAILED INSPECTION OF THE RUDDER AND ELEVATOR CABLES IN THE AFT EQUIPMENT AREA, WEAR WAS FOUND ON THE ELEVATOR AND RUDDER FLIGHT CONTROL CABLES. THE WEAR EXCEEDED THE AMM CABLE TOLERANCE INSPECTION. THE CABLE WEAR IS FNov 22, 2012 · Cndair CL6002B16SDR HNAA2012111401047Cable · corrodedSECOND CABLE, INBD CORRODED IN BAG BAY CABIN UNDER FLOOR. CLEANED CABLE ON RT SIDE OF BAG BAY UNDER FLOOR AS NEEDED IAW AMM 20-60-01. EVALUATED CABLE CONDITION AND DETERMINED IT WAS AIRWORTHY IAW BULLETIN 20-60-01.Nov 14, 2012 · N805EX · Dhav DHC8102SDR HNAA2012111401046Cable · corrodedFIRST AND SECOND CABLE SHOWS SIGNS OF CORROSION AT X564 ON OTBD CABLES. CLEANED CABLES IAW MM 20-60-01. EVALUATED CABLES AND DETERMINED AIRWORTHY IAW BULLETIN 20-60-01.Nov 14, 2012 · N805EX · Dhav DHC8102SDR UALA2012110506344Computer · faultyREPLACE ELEVATOR FEEL COMPUTER PER MM. REMOVED ELEVATOR FEEL COMPUTER PER MM. OFF UNIT MR27313-562. ITEM CREATED FOR MOUNT INSPECTION.Nov 2, 2012 · N572UA · Boeing 757222SDR UALA2012110506346Actuator · leakingHYD LEAK BELOW RT STAB (CHRONIC). OPENED ELEVATOR PCU ACCESS PANEL ON RIGHT SIDE OF STABILIZER AND RAN ALL THREE HYD SYSTEMS WHILE LOOKING FOR LEAKS AND FOUND CENTER ACTUATOR ROD END TO BE WEEPING 1 DROP EVERY 5 MINUTES, ACTUATOR 1 DROP WEEP IS WITHIN LINE LNov 1, 2012 · N590UA · Boeing 757222SDR SWAA2012103008979Computer · faultyAIR TURNBACK -- AFTER TAKEOFF, APPROX 220-250 KTS "DIFF PRESS" LIGHT CAME ON. LIGHT WENT OUT AGAIN ON LANDING AT 150KTS. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER M/M.Oct 29, 2012 · N555LV · Boeing 7377BDSDR UALA2012102906228Computer · faultyFLIGHT CONT ELAC 1 PITCH CONTROL FAULT. REPLACED 1 ELAC PER AMM. OPERATIONAL TEST GOOD PER AMM.Oct 27, 2012 · N468UA · Airbus A320232SDR UALA2012102506098Rod End · faultyFOUND LEFT ELEVATOR GREEN SERVO WITH CUMULATIVE PLAY OUT OF LIMITS. REF AMM MT 27-025 HAS PLAY OF 10 MM. SAMC TEXT: REF AMM 24-34-51, SERVO ROD END REPLACEMENT: GREEN TY-WRAP NO LONGER REQUIRED PER ECRA 2734-01006. REPLACED LEFT GREEN ELEV SERVO ROD END REFOct 23, 2012 · N489UA · Airbus A320232SDR QXEA2012102201337Warning Light · false activationELEVATOR ASSYMETRY CAUTION LIGHT ENROUTE RAN CHECK LIST LIGHT EXTINGUISHED ON LANDING. PERFORMED FIM TASK 27-30-00-810-801. NO FAULTS NOTED. OPS TEST GOOD. FAULT DID NOT RETURN. COULD NOT DUPLICATE. NO PARTS REPLACED. RETURNED TO SERVICE.Oct 22, 2012 · N405QX · Bombdr DHC8402SDR CA121022019Computer · failed(CAN) DURING TAKEOFF, THE FLIGHT CREW REPORTED THE ACFT REQUIRED MORE ELEVATOR FORCE THAN NORMAL TO ROTATE. ONCE AIRBORNE THE REQUIRED FORCE WAS TRIMMED OUT WITHOUT DIFFICULTY. ALL OTHER PHASES OF FLIGHT WERE REPORTED AS NORMAL. ON APPROACH, DUE TO THE POSSIBOct 21, 2012 · Boeing 737*SDR AALA20121013010Computer · malfunctionedJFK - INFLIGHT ORD-LHR. CREW REPORTED EICAS MESSAGE - ELEV FEEL- DISPLAYED, LEFT ENGINE SPAR VALVE LIGHT ON WITH ASSOCIATED EICAS MESSAGE AND STANDBY AIRSPEED INDICATOR PROBLEM. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVEOct 13, 2012 · N389AA · Boeing 767323SDR UALA2012101205820Computer · malfunctionedAIRCRAFT CONTINUES TO NOSE UP PITCH AFTER RELEASING SIDE STICK .5DG PER SECOND. REPLACED ELAC 2 PCN 482-9572 PRECAUTIONARY. ACP TSM 27-30-810-853-A. WIRING CHECKS OK, REPLACED NR 2 ELAC PER MM.Oct 10, 2012 · N452UA · Airbus A320232SDR UALA2012100305620Pcu · leakingLEFT OUTBOARD ELEVATOR PCA BAD. LEAKING AT ACTUATOR ROD END. REPLACED LEFT OUTBOARD ELEVATOR PCU, OPS CHECK GOOD.Oct 2, 2012 · N556UA · Boeing 757222SDR UALA2012091205144Computer · malfunctionedELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS: ATTEMPTED RESET ECAM MESSAGE RETURNED SAMC TEXT: CFDS SHOWS "27-44-00 THS ACTR POS ERROR 9CE OF ELAC 2" AT FLT PHASE 5. OPBLM SEE TSM 27-93-00-810-836A. REPLACED ELAC 2 & TESTED PER MM Sep 10, 2012 · N411UA · Airbus A320232SDR UALA2012091005086Pca · faultySTATUS MSG L ELEV PCU AFTER LANDING. COMPLIED WITH SINGLE SYSTEM HYD TEST PER MEL 2721D. ACP BREAKOUT OF EACH PCA, FOUND LEFT INBOARD PCA BAD. NO PCA IN STOCK DEN. REPLACED LEFT INBOARD ELEVATOR PCA, OPS CHECK, LEAK OKAY.Sep 8, 2012 · N548UA · Boeing 757222SDR SIMA20120907007Unknown · malfunctionedDURING MAINTENANCE INSPECTION FOR FLIGHT 4304, TROUBLESHOT ELEVATOR IT WOULD NOT PUSH FORWARD DURING LANDING. PERFORM CHECK OF GUST LOCK SYSTEM. PERFORMED GENERAL VISUAL INSPECTION AND OPERATIONAL CHECK OF ELEVATOR GUST LOCKS. NO DEFECTS NOTED AT THIS TIME Sep 7, 2012 · N668HH · Emb EMB145LRSDR UALA2012090705054Computer · faultyELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. FLT CONTROL ELAC 1 FAULT. REMOVED AND REPLACED ELAC NR 1, CHECKS NORMAL PER AMM. FLT CONTROL ELAC 1 FAULT. CHECKS NORMAL PER AMM.Sep 6, 2012 · N498UA · Airbus A320232SDR UALA2012090404933Rod · faultyAIRFRAME VIBRATION, RTFL. PER CAPT FELT STRONG CYCLICAL VIBRATION IN THE VERTICAL ONLY WENT AWAY WITH DECREASE IN SPEED. FELT THROUGHOUT CABIN. ALT 200FL-320FL, SPEED 320KTS. STRONGEST CAPT EVER FELT WITH AUDIBLE NOISE FACTOR. REPLACED THE LEFT GREEN AN RSep 1, 2012 · N449UA · Airbus A320232SDR ASAA2012091592902Sensor · failedDURING ACCOMPLISHING LWMP UPGRADE, FOUND FAULT IN BITE GRP 49.32. ELEV POS FAIL- POS SENS -1 MSG 22-11125. R & R ELEVATOR POSITION SENSOR REF MM 22-11-30-400-801. ELEVATOR POSITION SENSOR ADJUSTMENT AND TEST PASSED REF MM 22-11-30-820-801. OPS NORMAL.Sep 1, 2012 · N506AS · Boeing 737890SDR UALA2012082204696Computer · leakingLEAK IN RIGHT AUX PITOT SYSTEM. CONFIRMED RIGHT AUX PITOT LEAK COMING FROM ELEVATOR FEEL COMPUTER. NO LEAKS FOUND ON RIGHT AUX LINE WHEN REMOVED AND CAPPED FROM FEEL COMPUTER. REPLACED ELEVATOR FEEL COMPUTER IAW AMM. REPLACED ELEVATOR FEEL COMPUTER. ACP OAug 22, 2012 · N668UA · Boeing 767322SDR UALA2012082104668Actuator · faultyELAC 1 FAULT, CFDS SHOWS "THS ACTR SERVO MOTOR 2 9CE OF ELAC 1". WITH ELAC 1 PITCH FAULT DISPLAYED ON UPPER ECAM. -WORK WITH TSM 27-93-00-810-845A. SEE IPC 27-92-08-3C ITEM 32. REPLACED PITCH TRIM ACTUATOR MOTOR 2 SPLY RELAY (36-CE-2) PER TSM 27-93-00-810-84Aug 20, 2012 · N456UA · Airbus A320232SDR CA120817002Actuator · sticking(CAN) ON ROTATION, THE F/O NOTED THAT THE ELEVATOR CONTROL WAS STICKY. IT WAS HARDER THAN NORMAL AND ON IT`S OWN, WOULD NOT RETURN TO THE NEUTRAL POSITION. CREW ELECTED TO RETURN. MAINTENANCE PERSONNEL FOUND THAT THE CAPTAIN AND SERVO ACTUATOR AT FAULT. BOTAug 14, 2012 · Cndair CL6002B19SDR SIMA20120812004Control Unit · inoperativeFLT 4038, CREW REPORTED PITCH TRIM BACKUP INOPERATIVE MASTER WARNING AND EICAS MESSAGE PRESENTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.Aug 13, 2012 · N905JH · Emb EMB145LRSDR CVGA20120904001Warning System · activatedSTAB MISCOMPARE ANNUNCIATOR ILLUMINATES AFTER FLAPS INDICATE RETRACTED.Aug 12, 2012 · N178BR · Cessna 560XLSDR CA120814006Pushrod · undertorqued(CAN) DURING THE 36 MONTH CHECK THE AREA OF THE ELEVATOR CONTROL SYS SECTOR AND HORN WAS ACCESSED FOR THE FIRST TIME SINCE THE ACFT WAS NEW AND IT WAS FOUND THE BOLTS WERE NOT TORQUED CORRECTLY AND THAT BOTH THE BOLTS COULD BE SLID BACK AND FORTH IN THE ROD ANAug 10, 2012 · Cessna 510SDR UALA2012081304399Bellcrank · damagedELEVATOR PCA BELLCRANK FUNCTIONALLY CHECK RIG OF ELEVATORS TO IDENTIFY ANY OUT OF RIG CONDITION CAUSED BY SHEARED OR PARTIALLY SHEARED RIVETS IN THE ELEVATOR POWER CONTROL ACTUATOR INPUT LINKAGE ASSEMBLIES. REFERENCE AMM 27-31-98 PAGE SERIES 601. MANDATED BYAug 7, 2012 · N662UA · Boeing 767322SDR UALA2012073004096Elevator · flutterVERY STRONG FLUTTER IN CLIMB FL230M.77 WITH -.4PITCH TRIM AND IN CLEAR SLOWED IN CLIMB AND DSPTD. CW VIBRATION REPORTING CL, PROCESS FOR ID OF VIBRATION SOURCE, DECISION TREE, DECISION TABLE, IAW DECISION TABLE WAS A TYPE 1, CW FAULT ISOLATION TYPE 1 IAW 27-3Jul 28, 2012 · N831UA · Airbus A319131SDR UALA2012073004097Control Rod · out of adjustDURING CONTROL CHECK, ELEVATORS SPLIT AND NOT NEUTRAL. FOUND RT ELEVATOR RIG PIN ES T9 UNABLE TO FREELY PUT IN MIDDLE PCA AND RT ELEVATOR TRAILING EDGE .25 INCH FROM LOCATING HOLE ON INDEX PLATE. ADJUSTED RT ELEVATOR PCA INPUT CONTROL ROD AND POWER CONTROL AJul 28, 2012 · N547UA · Boeing 757222SDR HNAA2012072700882Control Unit · failedECU POWER UPTRIM LIGHT ILLUMINATED ON TAKE-OFF ROLL. R & R NR 1 TSCU IAW AMM 61-26-00. OPS CHECKED IAW SRT, SECTION 5. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.Jul 27, 2012 · N805EX · Dhav DHC8102SDR 2012FA0000485Control Cable · frayedWHILE COMPLYING WITH MANDATORY SB 75, R3, "FLIGHT CONTROL CABLES", ONE OF THE 2 FWD STABILATOR CABLES WAS FOUND FRAYED. THE FRAYED CABLE WAS FOUND ONLY BY SLACKENING THE CABLE AND BENDING IT AT A SHARP RADIUS AS CALLED FOR IN SB 75. THIS ACFT HAS BEEN MODIFIJul 16, 2012 · N856H · Parten P68CSDR DXTA2012071305048Elevator System · frozenAFTER PLANE SAT IN HEAVY RAIN, DEPARTED AND STARTED CLIMB TO ALTITUDE. CLIMBING THROUGH MID 20000, NOTICED ELEVATOR STARTING TO BECOME STIFF. ADJUSTED TRIM AND TRIM WHEEL MOVED FINE. DECIDED TO LEVEL OFF AT FL360 AND ASSESS SITUATION. ACCELERATED ELEVATORJul 12, 2012 · N665QS · Cessna 560XL
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