JASC 2700
Service difficulty reports · 1,745
Reports filed under 2700 · Flight 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 = '2700' 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 = '2700' 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 AALA202207135088Accelerometer · defectiveAIRCRAFT WAS GROUNDED: WITH AUTO PILOT OFF, CONTINUOUS NOSE DOWN PRESSURE REQUIRED TO MAINTAIN LEVEL FLIGHT OR CORRECT CLIMB ANGLE. WITHOUT PRESSURE THE AIRCRAFT PITCHES NOSE UP CONTINUOUSLY. MAINTENANCE REPLACED #2 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-SDR VNAA202207111111Trim Panel · unserviceableFLIGHT RETURNED TO FIELD AFTER TAKEOFF. CREW DISCOVERED THAT AILERON AND RUDDER TRIM WERE DEFLECTING SEVERELY TO THE LEFT. CREW THEN CONTACTED ATC AND DECLARED AN EMERGENCY. FLIGHT LANDED SAFELY AND TAXIED BACK TO GATE. CREW REPORTS LANDING OVERWEIGHT. CABIN WSDR AALA202207086663None · noneAIRCRAFT WAS GROUNDED: AIRCRAFT MADE A LOUD NOISE WHEN ACCELERATING PASSED 250 KNOTS, SOUNDED LIKE WIND NOISE FROM A GEAR DOOR OPEN. AUTO PILOT ON OR OFF 2 DEGREES RIGHT WING DOWN ON CONTROL WHEEL. DIVERTED TO PHL EMERGENCY WAS DECLARED. **SUPPLEMENTAL REPORT SDR 2022FA0000308None · separatedUPON LANDING ON THE GRASS, THE FLIGHT CONTROL HANDLE ON THE STICK SEPARATED AND THE CONTROL STICK WENT FORWARD CAUSING THE AIRCRAFT TO FLIP NOSE OVER. THE RAY ALLEN G101 STICK GRIP IS MADE OF UV AND OIL RESISTENT FOAM AND NYLON. IT SLIDES DIRECTLY ONTO 1' DIAMSDR JJBA20220620009None · noneEXTERNAL FWD VENTRAL TANK DRAIN VENT SKIN CORRODED. REPAIR DOUBLER ON CENTER FUSE VENTRAL TANK RIB 1SDR 2022FA0000301None · noneWARNING ELEX MESSAGE DURING TAXI. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. TROUBLESHOT WARN ELEX MSG TO BROKEN WIRE AT FO'S STICK SHAKER CONNECTOR D1399 PIN A. ACCOMPLISHED SPLICE REPAIR PER SWPM 20-10-13 ALL CHECKS NORMAL IAW AMM 2732-00 AND WDM 27-32-21 ASDR CALA2022061501509None · failedFLT/CONTRL SPOILERFAULT ON DEPARTURERIGHT INBOARD 1 REMAINEDEXTE NDED..RTB COMPLIED WITH MEL, SPOILER 1 RIGHT SIDE LOCKED OUT, PER MEL. PK PER TOMC ADD EMP:U116706,U167027 DISPATCH DESK: 23 NAME: VS DATE: 13-JUN-22- 2764A APPROVED. TROUBLE SDR SWIA202266301None · chafedLH WING O/B GROUND SPOILER HAS CHAFES WHERE THE BUMP PADS MEET X2 (MARKED) (C-CHECK RO 8/15/2022) BLENDED OUT DAMAGE AND RESTORED FINISH TO LH WING O/B GROUND SPOILER WHERE THE BUMP PADS MEET X2 . COMPLIED WITH REO 601R-57-72-387 REV - A DATE 2022-06-27SDR SWIA202266300None · chafedRH WING FLIGHT SPOILER HAS CHAFES WERE THE BUMP PADS MEET X2 (MARKED) (C-CHECK RO 8/15/2022) REMOVED DAMAGE ON RH WING FLIGHT SPOILER WHERE BUMP PADS MEET REF. CRJ-200 SRM, 51-12-00. FOUND TO BE IN A NO DAMAGE ALLOWED AREA AND COMPLIED WITH REO 601R-57-SDR VNAA202206099913Slat Track · wornL/H SLAT TRACK 1-1 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKSSDR CALA2022060601440Skin · delaminatedLEFT SIDE ELEVATOR OUTBOARD UPPER SURFACE 1EA DELAMINATION REF HAECO NON-ROUTINE NO:9488657 - ORIGINATED BY EMP V902926, SUPPORT TASK. PERFORME BY EMP V902926,LEFT SIDE ELEVATOR OUTBOARD UPPER SURFAC E 1EA DELAMINATION REPAIRED AS PER SRM 55-20-01-2R-1 REPAIR SDR AJXA2022060600016Trim System · malfunctionedON TAKEOFF THE PILOT REPORTED THAT THEY HAD A PRIMARY TRIM FAILURE AND A MACH TRIM OFF INDICATION. THE PRIMARY TRIM FAILURE WAS DUE TO THE FACT THAT THE PILOT IN COMMAND DID NOT TURN ON THE MACH TRIM. WE PERFORMED A FUNCTIONAL CHECK OF THE SYSTEM AND FOUND THASDR CALA2022060201428Skin · delaminatedLEFT SIDE ELEVATOR OUTBOARD UPPER SURFACE 1EA DELAMINATION REF HAECO NON-ROUTINE NO:9488657 - ORIGINATED BY EMP V902926, SUPPORT TASK. PERFORME BY EMP V902926,LEFT SIDE ELEVATOR OUTBOARD UPPER SURFAC E 1EA DELAMINATION REPAIRED AS PER SRM 55-20-01-2R-1 REPAIR SDR F3LA2022053100048Servo · inoperativeDISCREPANCY: REFERENCE LP210393 ITEM 1 WRITEUP: FLT CONTROL CHECK FAILED. L AIL. OUT OF LIMITS.
CORRECTIVE ACTION: LP210393 ITEM 1 SIGN OFF: REF TSM 27-10-00-810-836-A FOUND LH AILERON SERVO CONTROL (BLUE SYSTEM) TO BE OUT OF LIMITS. REMOVED AND REPLACED OUTSDR ABXA202252658None · noneUNSCHED STAB TRIM EICAS MESSAGE ON TAKEOFF ROLL AT APPROX 65 KTS. ABORTED TAKEOFF. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLESHOT SYSTEM. NO FAULT ON SAM L/H OR R/H FOUND R/H STCM FAULT RESET AND MAINTENANCE PROCEDURE 27-91-2 PERFORSDR CALA2022052301323Panel · missingSMALL 2 INCH ROUND ACCESS PANEL MISSING FROMINBOARD SIDE OF OUTER MOST FLP/TRK FRNG RT SIDE REQUESTING CDL 27A. APPLIED SPEED TAPE TO HOLE. COMPLIED WITH CDL 27AD. ADD EMP:U113818 DISPATCH DESK: 06 NAME: AN DATE: 18-MAY-22- OK TO CDL UPDATED NR WITH PICTURESDR ABXA202252257None · faultedDURING PUSHBACK, SPOILERS EICAS ADVISORY MESSAGE ILLUMINATED. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL MODULE ASSY 3 LEFT IAW AMM 27-09-00. OP CHECK GOOD. AICRAFT RETURNED TO SERVICE.SDR IXXA2022051901Skin Panel · corrodedAREA OF BULGING SKIN ON LEFT HAND WING I/B FLAP LOWER SURFACE AROUND MID FLAP.SDR DALA2022052003459None · noneSHIP 3121 - ABORT T/O DUE TO F/CTL ELAC 1 PITCH FAULT. CORRECTIVE ACTION: REMOVED LOB ELEVATOR HYD ACTUATOR. INSTALLED L OB ELV HYD SERVO CONTROL REF A319 AMM 27-34. R/R ELAC #1 COMPUTER. OPS CHECK GOOD REF A319 AMM 27-93.(2239143)SDR QXEA2022051700200Flap Track · wornRH OUTBD FLAP INBD FLAP CARRIAGE INBD UPPER FLAP ROLLER SURFACE WORN AND CORRODED. BLENDED RH OUTBD FLAP INBD FLAP CARRIAGE INBD UPPER FLAP ROLLER SURFACE IAW SRM 53-10-03.SDR AALA202205199855Servo · defectiveAIRCRAFT WAS NOT GROUNDED: DURING CRUISE FLIGHT CONTROL AILERON SERVO FAULT WITH ELAC 1 PITCH FAULT AMBER BOX AROUND G ON RIGHT AILERON AND MODERATE ROLL PRIOR TO FAULT. **SUPPLEMENTAL REPORT FOR AALA202205179855: REPLACED RIGHT WING GREEN AILERON SERVO AND ASDR AALA202205179855None · noneAIRCRAFT WAS NOT GROUNDED: DURING CRUISE FLIGHT CONTROL AILERON SERVO FAULT WITH ELAC 1 PITCH FAULT AMBER BOX AROUND G ON RIGHT AILERON AND MODERATE ROLL PRIOR TO FAULT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)SDR SIMA20220514002None · noneMECHANICAL / DUAL SPS FAIL. EMERGENCY DECLARED. AT 16000 MSL SPS 2 INOP WARNING MSG.IN QRH WHEN SPS 2 CUT OUT WAS PRESSED,SPS 1 INOP WARNING MSG ON EICAS ASSICIATED EICAS MSG OF SPS ADVANCED AND STICK PUSHER FAIL.AOA CAUTION ON FO PFD. "TRANSFERRED TO NRWC 610SDR DALA2022051703415None · noneSHIP 3121 - ATO - DUE TO ELAC 1 PITCH FAULT AT THROTTLE UP FOR TAKE-OFF. CORRECTIVE ACTION: REMOVED AND REPLACED SERVOVALVE OF ELEVATOR SERVOVONTROL ACTUATOR 34CE3 IAW A319 AMM 27-34-51.(8667912)SDR AALA202205149645Computer · faultyAIRCRAFT WAS GROUNDED: SEVERE AIRFRAME VIBRATION ON TAKE OFF, AUTO PILOT STEERED HARD RIGHT WHEN ENGAGED, FLIGHT CONTROL PAGE INDICATED LEFT SPOILERS EXTENDED. NO ECAM MESSAGES. EMERGENCY DECLARED, RETURNED TO PHX LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALASDR IXXA20220051107Torque Tube · damagedR/W T/E I/B FLAP OUTER TORQUE TUBE PITTEDSDR IXXA20220051106Torque Tube · damagedR/W T/E I/B INNER TORQUE TUBE PITTEDSDR IXXA20220051104Torque Tube · damagedLEFT WING INBD FLAP TORQUE TUBE DAMAGEDSDR IXXA20220051103Torque Tube · chafedLW IB TE TORQUE TUBE HAS BARE METAL/WEAR MARKSSDR CALA2022051101205None · failedFLAPS WOULD NOT EXTEND WHEN 5 WAS SELECTED. RAN TE FLAP AYSEMITR Y CHECKLIST AND LANDED 27-51 TASK 801 PROCEDURE 2. PERFORMED PROCEDURE 11 CONNECTOR D229 28 VAC PRESENT. CAT REQUIRED DUE TO DISCONNECT RECONNECT. LOCKING DUE TO EMERGENCY DECLARED ON LANDING UNLSDR AALA202205109781None · faultyAIRCRAFT WAS GROUNDED: DURING DESCENT INTO CLT, AUTOPILOT #2 DISCONNECTED; SOON AFTER, BOTH ELAC'S FAILED. DECLARED AN EMERGENCY AND LANDED SAFELY. TROUBLESHOT PER TSM 27-40-00-810-802-A. REPLACED #2 ELEVATOR AILERON COMPUTER (ELAC) PER AMM 27-93-34 (AALA20220SDR CALA2022050901194Flap · none*EMERGENCY*LE FLAP TRANSIT CAUTION LIGHT LEFT OUTBOARD SLAT RAN FLAPS #1 SLAT NO AMBER LIGHT AND NO GREEN LIGHT AT 15. ACCOMPLISHED FIM 27-81 TASK 809 THRU STEP D NO ACTIVE FAULTS INDICATED. ACCOMPLISHED FIM 27-51 TASK 801 HAVE FAULT HISTORY FLIGHT LEG 1-- SLSDR JIKA2022050601Sensor · defectiveFOUND A DEFECTIVE PROX SENSOR. REMOVED AND REPLACED SENSOR. ISSUE REMAINED. REMOVED AND REPLACED WARNING COMPUTER WITH NO CHANGE NOTED. FOUND SIGNAL WIRE SHORTING WITH SHIELDING GROUND, REPAIRED WIRE. ALL OPS CHECKS GOOD.SDR J7SA2022060200321Spoiler · fault messageREPLACED FCE #2 DUE TO GND SPLR FAIL AND SPOILER FAULT ON LANDING. OPS CHECK GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01.SDR 2022F00279None · noneAFTER COMPLETING A LEG FROM NAPLES, FL WE MADE A SUCCESSFUL LANDING AT KMKE WITH NO ABNORMALITIES. THE PASSENGERS WERE DEPLANED AND THE AIRCRAFT WAS REFUELED. WITHIN 30 MINUTES WE BEGAN OUR TAXI FOR A REPOSITIONING FLIGHT (NO PASSENGERS) TO CHICAGO EXECUTIVE ASDR IXXA2022042114None · gougedFLAP MITIGATION INSPECTION RIGHT FLAP 6 - 9 DRIVE BEAM ON THE # 8 FLAP SUPPORT HAS TOOLING MARKS/GOUGES.SDR MTNA20220419001None · nonePITCH TRIM ASYMMETRY IN FLIGHT. PITCH, ROLL, AND RUDDER TRIM INDICATOR INOP. TRIPPED CIRCUIT BREAKER. REMOVED AND RECONNECTED LEFT AND RIGHT ELECTRIC PITCH TRIM ACTUATOR CONNECTORS AFTER CLEANING WITH CONTACT CLEANING. REMOVED AND REPLACED CREW ALERTING COMPUTSDR ABXA2022041843None · noneDURING TAXI AILERON LOCK OUT MESSAGE AND SELECTED FLAPS 5 AND TE DISAGREE EICAS AND FLAPS DID NOT EXTEND PAST FLAPS 5. AIRCRAFT RETURNED TO BLOCK AND WAS GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF AILERON LOCKOUT SYSTEM IAW B767 AMM 27-11-44. SDR CALA2022041801012Annunciator · warning lightLEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 2 LOCKING FOR POSITIVE FIX UNLOCK TO SIGN OFF OVERHEAD ANNUNCIATOR PANEL IS FINAL FIX. PLEASE REFER TO LOG PAGE 8384678 FOR ALL MX ACTIONS TAKEN. OPS CHECK GOOD.SDR J7SA2022050200315Circuit Breaker · poppedREPLACED FCE 1 DUE TO CIRCUIT BREAKER POPS ON POWER UP. WORK COMPLETED IAW AMM 27-03-01. ALL OPS AND RIG CHECKS GOOD.SDR 2022F00182None · noneVIRGIN AUSTRALIA AIRCRAFT BOEING B737 REGISTRATION VH-VUY IS UNDERGOING MAINTENANCE AT ETIHAD AIRWAYS ENGINEERING (EYENG) FACILITY. (FAA APPROVAL NUMBER 2GUY107C). DURING REPLACEMENT OF NEW SERVICEABLE RATIO CHANGER ASSY, THE FOLLOWING DEFECTS WERE IDENTIFIED:SDR J7SA2022050200314Fcu · failedREPLACED #2 FCE DUE TO PTRIM NML FAIL AT FL390. WORK COMPLETE IAW EMBRAER PHENOM 300 AMM 27-03-01. OPS CHECK AND RIGGING SATISFACTORY.SDR JJBA20220406008None · noneLT WING FLAP FLEX SHAFTS #1, #2, #4 DAMAGED FERRULES. REMOVED AND REPLACED LEFT WING FLAP FLEX SHAFTS SECTIONS 1, 2, AND 4.SDR JJBA20220404006None · noneRT WING AILERON ON AILERON DAMPER HINGE GOUGED. REMOVED AND REPLACED RT WING AILERON DAMPER HINGE.SDR CALA2022040400877Bolt · sheared*EMERGENCY DECLARED* GREEN HYDRAULIC SYSTEMQUANTITY IS VERY LOW. OPENED PANEL 325BL ON LEFT SIDE OF VERT STAB. FOUND 1 OF 3 BOLTS R&R LH SERVOACTUATOR YAW DAMPER IAW AMM 27-26-51. OPS CHECK LEAK INSPECTED ACTUATOR PER GMM 09-10-05 .MARCHAND U098190 . SHEARD FRSDR CALA2022040600896None · noneTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022040600896 SUBMITTED ON 04/06/22. NEAR NO. 3 SLAT ON LOWER EDGE HAS A MISSING PANEL. REPLACED MISSING SLAT PANEL PER EA 00-0592-3-4149. FUNCTION TESTED SLATS ALL FUNCTION TESTED UP AND DOWN OK ATSDR JJBA20220402005None · noneREMOVED ELEVATOR LH TO EVALUATE DAMAGE. REMOVED LH ELEVATOR AND REPAIRED ONE ELEVATOR FITTING. RE-INSTALLED ORIGINAL ELEVATOR FITTING. ELEVATOR RE-INSTALLED.SDR HNAA2022040400133None · nonePDIS 657 27-36 2473701 02APR22 ORD CLOSE
RTO DUE TO EICAS MSG SPS 2 INOP AND SPS ADVANCE. FO PFD SHOWS AMBER AOA
FACT 02APR22 22:19 ORD
UPON ARRIVAL TO AIRCRAFT FOUND AOA VANES 1 AND 2 SPLIT. ALIGNED AOA PERFORMED STEP 1 OF FIM 27-36-00-810-80SDR AALA202204044795None · faultyAIRCRAFT WAS GROUNDED: MACH TRIM LIGHT ILLUMINATED DURING CLIMB. AIRCRAFT EXCEEDED ALTITUDE WHEN LEVELING. TURNED OFF AUTOPILOT AND HAD A LARGE NOSE DOWN TRIM RECOVERY. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO ORD LANDING SAFELY. ACCOMPLISHED FIM 22-13-00.SDR CALA2022032800797Control Module · faultedRTO AT 95KTS DUE TO UNSCHED STAB TRIM MSG REMOVED AND REPLACED LEFT STAB TRIM CONTROL MODULE I.A.W FIM 27-09 FAULT TREE 813. OPS CHECK NORMAL AS PER AMM 27-09-00-422-008. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1785251 SN OFF 1997 IPC REFERENCE # 27-09-00
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