JASC 2700
Service difficulty reports · 1,743
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 J7SA2025082600452Fce · faultedPTRIM BACKUP FAIL CAS ILLUMINATED IN FLIGHT. REPLACED FCE #1 IAW PHENOM 300 AMM 27-03-01.SDR 21GA20250724016Power Supply · faultedAT FL 390 BEGAN TO EXPERIENCE DUTCH ROLLS WITH AUTO PILOT AND AUTO THROTTLES ENGAGED.DISCONNECTD AP BUT HAD TO HOLD THE YOKE TO THE RIGHT TO MAINTAIN CONTROL. DELCARED EMERGENCY AND DIVERTED TO ST. LOUIS. MAINTENANCE PERSONNEL REPLACED RIGHT CSEU POWER SUPPLY.SDR J7SA2025082600451Fce · faultedGND SPLR FAIL CAS ILLUMINATED ON TOUCHDOWN. REPLACED FCE 2. RIGGING AND OPS CHECK GOOD. ALL WORK COMPLETED IAW EMBRAER PHENOM 300 AMM 27-03-01.SDR 3EJA2025091801925Switch · out of adjustSTAB MIS COMPARE AT AROUND 215-230KTS. RE-ADJUSTED CONTROL SWITCHSDR MASA2025060930046Unknown · faultedAIRCRAFT RETURNED TO FIELD DUE TO PITCH TIME UNRESPONSIVE FROM CA, FO AND BACK UP SWITCHES. TECHNICIANS TROUBLESHOT THE DISCREPANCY PER THE FIM AND REPLACED THE HS-ACE. OPS CHECKS WERE GOOD, ALL 3 SWITCHES FUNCTIONED NORMALLY.SDR CALA2025060605330Pressure Switch · faultedSTAB TRIM LIGHT ON O/H PANEL AND EICAS ILLUM AFTER T/O. ACCOMPLI SHED NON NORMAL. REMOVED AND REPLACED RIGHT BRAKE PRESSURE SWITCH IN REF AMM 27-41-07. LEAK CHECK GOOD. PERFORMED THE STABILIZER TRIM MODULE TEST IN REF 27-09-00-712-037 UP TO AND INCLUDING (4)(SDR CALA2025060405271Unknown · vibrationMODERATE LATERAL VIBRATION. STARTED AT 17000-F230. SPEED WAS APP ROX 300 KTS CI 40..SLOWED TO FOUND YELLOW AN GREEN HYD QTY LOW, SERVICED BOTH SYS TO FULL IAW AMM 12-12-29-611-001-A, PREFORMED VISUAL INSP OF ACFT FOR HYD LEAKS NONE FOUND, VERIFIED NO OSCILLATISDR IPXA2025060568347Warning Message · illuminatedEMERGENCY DECLARED, NO LAND 3 FLT CONTROL SYS FAULT CODE 27570 27470 27183 27180,REF FIM27-09-00-810-884 FIM27-09-00-810-880 FIM27-09-00-810-834 FIM27-09-00-810-835,ALL FIM LINK TO ZFW, SUSPECT THE ZFW ERROR, DO THE CMC LCE L AND R & YSM L AND R,ALL TEST PASSSDR J7SA2025060600447Fce · faultedCREW RECEIVED FLAP FAIL CAS AFTER SELECTING FLAPS 1 FROM 0 IN FLIGHT BEFORE LANDING. REPLACED THE FCE #1 IAW EMB 505 AMM 27-03-01. PERFORMED FLAP RIGGING PROCEDURE AND ALL REQUIRED OPS CHECKS.SDR DXTA2025050903399Stick Pusher · faultedSTALL CHECK: DURING PREFLIGHT SPS SYSTEM CHECK, WITH LEFT AND RIGHT TEST SWITCHES IN TEST, STICK SHAKER ACTIVATED BUT WE HEARD, AND CO-PILOT FELT, A TAPPING/BANGING UNDER HIS RIGHT FOOT. ADDITIONALLY, THE PUSHER FAILED TO ACTIVATE. WE TESTED A SECOND TIME SDR DXTA2025043003254Yoke · multiple failCAPTAIN CONTROL YOKE MAKES GRINDING NOISE WHEN ROLLED LT & RT. CAN ALSO FEEL BINDING/GRINDING. RIGHT SIDE IS SMOOTH BUT CAN STILL HEAR THE GRINDING. REMOVED DAMAGED SHAFT & INSTALLED NEW SHAFT IAW AMM 27-10 04 WITH NO DEFECTS NOTED. REMOVED DAMAGED DRUM ASSESDR J7SA2025050700445Fce · faultedPTRIM NML FAIL CAS WITH X OVER TRIM INDICATION FOLLOWING STAB TRIM MOVEMENT ANOMALY AFTER DE-ICE PROCEDURE. TRIM INITIALLY MOVED TO 0.0 DURING DE-ICE AND RETURNED TO T/O POSITION AFTERWARD, TRIGGERING THE CAS MESSAGE. CREW PERFORMED AN ELECTRICAL RESET, BUT THSDR AALA202504087746Computer · malfunctionedAIRCRAFT IN BASE MAINTENANCE: DURING POST MANTENANCE BASE VISIT FUNCTIONAL CHECK FLIGHT, THE FIGHT CREW REPORTED THAT WHEN SPEED BRAKE IS DEPLOYED AIRCRAFT ROLLS LEFT 2 TO 3 DEGREES. MAINTENANCE REPLACED RIGHT HAND AILERON SERVO CONTROLS 33CE2 (AALA20250408627SDR AALA202504080906Control Servo · malfunctionedAIRCRAFT IN BASE MAINTENANCE: DURING POST MANTENANCE BASE VISIT FUNCTIONAL CHECK FLIGHT, THE FIGHT CREW REPORTED THAT WHEN SPEED BRAKE IS DEPLOYED AIRCRAFT ROLLS LEFT 2 TO 3 DEGREES. MAINTENANCE REPLACED RIGHT HAND AILERON SERVO CONTROLS 33CE2 (AALA20250408627SDR AALA202504086274Control Servo · malfunctionedAIRCRAFT IN BASE MAINTENANCE: DURING POST MANTENANCE BASE VISIT FUNCTIONAL CHECK FLIGHT, THE FIGHT CREW REPORTED THAT WHEN SPEED BRAKE IS DEPLOYED AIRCRAFT ROLLS LEFT 2 TO 3 DEGREES. MAINTENANCE REPLACED RIGHT HAND AILERON SERVO CONTROLS 33CE2 (AALA20250408627SDR J7SA2025040200441Fce · faultedCREW RECEIVED GND SPOILER FAIL CAS MESSAGE DURING DESCENT. ATC INSTRUCTED THE CREW TO REDUCE SPEED TO 190 KNOTS; THE CREW ATTEMPTED TO DEPLOY SPEED BRAKES AT APPROXIMATELY 225 KNOTS. A GND SPOILER FAIL CAS MESSAGE APPEARED, AND THE SPOILER BOX INDICATED A FAILSDR DALA2025032802300Controller · faultedATB - DUE TO LATERAL OSCILLATION FELT DURING CLIMB OUT. CORRECTIVE ACTION: R/R AILERON SERVOCONTROL 9CS1 GREEN, R/R SERVOCONTROL BOLTS, R/R ADIRU, ADJUSTED SYSTEMS PER A330 AMM 27-14. OK FOR SERVICE.SDR J7SA2025040200442Fce · faultedON TAXI OUT, CREW RECEIVED PITCH TRIM BACKUP FAIL CAS. CREW PERFORMED MULTIPLE SOFT RESETS USING CIRCUIT BREAKERS WITH NO SUCCESS. AFTER RETURNING TO THE FBO, A FULL ELECTRICAL RESET WAS PERFORMED, BUT THE BACKUP PITCH TRIM FAIL CAS MESSAGE REMAINED. REPLACED SDR DXTA2025032602790Seal · missingAIRFRAME VIBRATION: NOISE AND VIBRATION BETWEEN SEATS ONE AND TWO. FOUND SPOTS ALONG THE FWD WTF SEAL TO BE MISSING RTV. APPLIED RTV AS NECESSARY IAW EMB PHENOM 300 AMM 51-21-02SDR DXTA2025032502788Control Cable · out of adjustHIGH VIBE IN YOKE AND PEDALS STARTING AT 250KTS. INCREASED INTENSITY AS SPEED INCREASED. CHECKED ELEVATOR AFT CONTROL CABLE TENSIONS, TENSIONS WERE WITHIN LIMITS IAW MM 27-31-00. CHECKED RUDDER CABLE TENSIONS, ALL TENSIONS WERE WITHIN LIMIT IAW MM 27-20-00. SDR ABXA20250319061Elevator · unknownDURING TAXI OUT, RIGHT ELEVATOR ONLY SHOWS ~ 80% TRAVEL UP AND DOWN. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED IAW MEL AMM 27-38-00. RETURNED A/C TO SERVICE. AMENDED: MTX DEFERRED IAW MEL AMM 27-38-00, AMENDED TO: MTX DEFERRED IAW MEL-SDR SWAA2025031806526Flap System · false indicationTRAILING EDGE FLAPS DISAGREE; INDICATOR SHOWED FLAPS 25 WITH FLAP HANDLE SELECTED AT FLAPS 30 <[01]. PERFORMED TRAILING EDGE FLAP SYSTEM OPS CK PER AMM 27-51-00. FLAPS OPERATE NORMALLY. PERFORMED FLAP OVERSPEED PHASE 1 CONDITIONAL INSPECTION AS A PRECAUTION ISDR R61A2025031700142Warning Message · illuminatedPITCH TRIM INDICATION AMBER. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED RETURN TO SERVICE TEST.SDR UIEA2025030800240Control Module · leakingHORIZONTAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAKAGE STAB TRIM CONTROL MODULE RH.(<P>LEAKAGE CHECK IN STAB TRIM CONTROL MODULE RH WAS PERFORMED IAW AMM 29-11-00-796-053 REV.144 DATE: 22DEC24. NO LEAK FOUND.</P>)SDR ABXA20250315058Valve · malfunctionedAFTER PUSHBACK DURING TAXI & ENGINE START WE HAD A RUDDER RATIO EICAS MSG WITH DISCREAT LIGHT/A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C MTX TROUBLESHOT AND T/S AS PER FIM 27-09 FT 814 PCA FAULT IN VIEW ON BOTH RRCM AFTER L AND R ENG START. REMOVED ASDR CALA2025031702874Computer · faultyELAC 1 PITCH FAULT ON TAKEOFF ROLL. ACP LOW SPEED ABORT R&R'D ELAC 1, OPS NML, REF AMM 27-93-34/401.SDR CALA2025031702867Module · faultedCREW REPORTED FLIGHT CONTROL B SYS HYD OVERHEAD LIGHT ON FOLLOWED QRH TURNED ON STDBY RUDDER ADDING WHAT CREW SENT IN ON E-MAIL ,ON DEPARTURE MASTER CAUTION ILLUMINATED WITH FLT CONT LIGHT AND LOW PRESSURE LIGHT ON OVERHEAD PANEL ON FLT CONT B SIDE. FLYING PILSDR J7SA2025040200443Fce · faultedPITCH TRIM BACKUP FAIL CAS MESSAGE DURING SYSTEM TEST. REPLACED FCE1 IAW AMM 27-03-01. RIGGING AND OPS CHECK GOOD.SDR R61A2025030700135Module · faultedON TAKEOFF HAD YAW DAMPER OFF THEN IMMEDIATELY GOT AVNX MAU 3B FAIL, NAV COMM 1 FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. ON LANDING FCND, LGND, AP WOULD NOT ENGAGE. R&R NIC 1 PROX MOD 6.SDR J7SA2025030400437Fce · faultedREPLACED FCE #1 DUE TO PITCH TRIM BACKUP FAIL CAS POSTED DURING FLIGHT. WORK COMPLETED IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD. RIG CHECKS GOOD. NO DEFECTS FOUND.SDR DXTA2025030302528Spoiler Sys · faultedHORIZONTAL STAB CONTROL: WE WERE AT FL400, 2 YELLOW AND 1 WHITE CAS MESSAGES POPPED UP ON THE PFD (GND SPLR FAIL, PTRIM NML FAIL, AND SPOILER FAULT). WE CONSULTED THE QRH, LANDED AT DESTINATION SAFELY. CORRECTIVE ACTION; AS INSTRUCTED BY MCC, SWAPPED FCE1 & FCSDR 2025FA0000118Lock Nut · looseDEFECTIVE LOCK NUT ON SCREW THAT CONNECTS THE YOLK ASSEMBLY TO THE AILERON ACTUATION BRACKET WAS LOOSE.SDR DALA2025021801204Relay · faultedSHIP 3915 -ATB- DUE TO STAB OUT OF TRIM LIGHT ILLUMINATED. CORRECTIVE ACTION: MAINTENANCE REPLACED RELAY R34 AND S145 STAB NOSE DOWN LIMIT SWITCH PER B737 WDM 20-13.SDR 2025FA0000119Lock Nut · defectiveDEFECTIVE LOCK NUT ON SCREW THAT CONNECTS THE YOLK ASSEMBLY TO THE AILERON ACTUATION BRACKET, CAME APART AFFECTING THE PILOT SIDE AILERON CONTROL.SDR J7SA2025020400430Switch · out of positionDIVERTED DUE TO MULTIPLE FLIGHT CONTROL FAULTS FOLLOWING TAKEOFF. AFTER GEAR RETRACTION, THE CREW RECEIVED FLTCTRL NO DISPATCH FOLLOWED BY FLTCTRL N-MODE FAIL, GROUND SPOILER FAIL, AND SPDBRK FAIL CAS MESSAGES, INDICATING INDIRECT MODE OPERATION. THE CREW LEVESDR DALA2025013000722Relay · faultedSHIP 3275 - FCNT - A/C EXPERIENCED AN UN-COMMANDED 400FT/MIN PITCH UP AT FL350, THEN RETURNED TO FL350. ELAC 2 PITCH FAULT THEN APPEARED. CORRECTIVE ACTION: REPLACED RELAYS 53CE, 36CE1 AND THS ACTUATOR. (LP: 6646470)SDR HNAA2025012700071Actuator · failedGUST LOCK WOULD NOT DISENGAGE UPON ENTERING RUNWAY. FACT 27JAN25 09:56 PHL RR RELAY K0848 IAW AMM 20-13-02. NO FIX, RR GUST LOCK ACTUATOR IAW AMM 27-71-01. OPS CK GOOD AT THIS TIME. AC OK FOR SERVICE AT THIS TIMESDR UIEA2025012000094Servo · leakingVERTICAL STABILIZER, REAR SPAR, YAW DAMPER SERVOS ASSY, LEAKING EVIDENCE.(<P>YAW DAMPER SERVOS LEFT AND RIGHT, WERE REPLACED, TEST WERE PERFORMED AND HYD LEAKAGE CHECK WAS PERFORMED AND TORQUE WAS APPLIED IAW AMM 22-21-02-414-016 REV 143. OPS CHECK GOOD. </P>)SDR DALA2025012100510Switch · failedSHIP 3276 - MISC/DE - DUE TO F/CTL SEC 3 FAULT. CORRECTIVE ACTION: SEC 3 PLACED ON MEL. R/R P/B SWITCH FOR SEC#3. OK FOR SERVICE. (LP: 6555042)SDR AALA202501185876Hinge Fitting · excess playAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING THAT AT FL 280 SPEED 310 STARTED GETTING SEVERE VIBRATION FROM TAIL SECTION OF AIRCRAFT. FLIGHT ATTENDANTS REPORTED FROM ROW 15 TO REAR OF AIRCRASDR A6WA202501098852Pcu · faultedAIRCRAFT FLUTTERS AT AIRSPEED ABOVE 280KIAS. EXPERIENCED FLUTTER IN AIRFRAME ON CLIMB THROUGH 10000FT. FLUTTER DISAPPEARED AFTER LEVELING OFF AND SLOWING BELOW 250KIAS AT 14,000FT. NO FLUTTER ON DECENT OR APPROACH. AIRCRAFT REMOVED FROM SERVICE. R & R ELESDR SCNA20250108004Flt Controls · stiffDEFECT 796540: FLIGHT CONTROLS ARE ABNORMALLY STIFF. RESOLUTION: LUBED AILERON MIXER REF AMM 27-11-81 OPS TEST GOOD.SDR DALA2025010800157Stab System · out of adjustWHILE PERFORMING W/C 2740-01114-07, THE JACKSCREW DID NOT STOP AUTOMATICALLY AND CONTACTED THE UPPER STOP. HORIZ STAB ADJ REQUIRED PER B717 AMM 27-40-00 820-801 & INSPECTION OF THE JACK SCREW REQUIRED PER B717 AMM 27-41-04 220-802. C/W INSPECTION OF JACKSCREW SDR J7SA2025010600424Flt Controls · unserviceablePTRM NML FAIL CAS MESSAGE RECEIVED DURING AIRCRAFT SETUP. RESET ATTEMPTED WITH NO SUCCESS. REPLACED #2 FLIGHT CONTROL ELECTRONIC IAW EMBRAER 505 AMM 27-03-01. PERFORMED OPS AND RIGGING CHECKS; ALL CHECKS GOOD WITH NO DEFECTS NOTED.SDR 2025FA0000005Control Cable · damagedUPON VISUAL INSPECTION OF PITCH SERVO AREA IT WAS NOTED THAT THERE APPEARS TO BE ELEVATOR CABLE DAMAGE ON THE CAPSTAN COVER OF THE PITCH SERVO. DAMAGE ON ONE OF THE SCREWS THAT ATTACH THE COVER INDICATE THE ELEVATOR CABLE WAS CAPTURED BY THE SCREW CAUSING THE SDR J7SA2025010600425Flt Controls · unserviceablePTRIM BKP FAIL OBSERVED DURING TESTING. REPLACED FCE #1 IAW EMBRAER 505 AMM 27-03-01. PERFORMED RIGGING AND OPS CHECKS; ALL CHECKS GOOD.SDR J7SA2025010600426Fce · unserviceableSWPS FAULT, PITCH TRIM BACKUP FAULT, AND FLAP FAIL CAS MESSAGES RECEIVED DURING GROUND OPERATIONS. REPLACED FCE #1 IAW PHENOM 300 AMM 27-03-01. PERFORMED FLAP RIGGING IAW PHENOM 300 AMM 27-50-00. OPS TEST OF FCE #1 SYSTEMS GOODSDR J7SA2025010600427Fce · unserviceableFLAP FAIL CAS RECEIVED UPON SELECTING FLAP FULL DURING APPROACH. CREW PERFORMED QRH PROCEDURE, REVERTED TO FLAPS 3, AND LANDED SAFELY. ON THE GROUND, THREE ATTEMPTS TO SELECT FLAP FULL TRIGGERED THE FLAP FAIL CAS, AND SELECTING FLAPS 0 INITIALLY FAILED TO RETRSDR J7SA2024121200422Fce · faultedAIR TURN BACK DUE TO PTRIM NML FAIL CAS MESSAGE AFTER MANUAL PITCH TRIM ACTIVATION RESULTED IN NO TRIM INPUT NEAR THE INITIAL LEVEL-OFF ALTITUDE. BACKUP MODE PITCH TRIM WAS USED FOR THE REMAINDER OF THE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT AT KMDW. REPLACESDR ABXA20241210249Warning Message · false activationABORTED TAKE-OFF AT ~75KTS DUE TO WARNING HORNING, RED FLAPS EICAS MESSAGE. AC ABORTED T/O DURING ABORT AFTER EXPENDING, SPOILERS, NOTED REF SPOILER EICAS MESSAGE AFTER ABORT WHILE TAXING NOTED FLAP/SLAT ELEC STATUS MTX GROUNDED AC . UPON INSPECTION FOUND NO A
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