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 J7SA2025010600428Fce · unserviceableFLAP FAIL AND PITCH TRIM BACKUP FAIL CAS MESSAGES RECEIVED ON POWER-UP. ATTEMPTED FULL RESET AND DISCOVERED FCE 1 CIRCUIT BREAKER (A13) WAS POPPED AND WOULD NOT RESET. REPLACED FCE 1 WITH REPAIRED UNIT IAW PHENOM 300 AMM 27-03-01. OPS CHECK GOOD WITH NO DEFECTSDR CALA2024120401400Computer · faultedF/CTL ELAC PITCH FAULT UPPER ECAM MESSAGE F/CTL ELAC 2 PITCH FAULT,POST FLIGHT REPORT FIN (9CE),FOLLOW TSM 27-93-00-810-836-A PERFORM (B) OPERATIONAL TEST OF THS-ACTUATOR ELECTRICAL CONTROL PER AMM 27-96-00-710-022,WITH THE ENGINE #2 RUNNING ALL TEST PASS.NO SDR CALA2024120201375Detector · faultedDUE TO RECENT HISTORY AND TO AVOID POSSIBLE SERVICE DISRUPTION OF MAINT MESSAGE 27-22321 SLATS DRIVE CAUTION OUTBOARD SLAT SKEW SENSOR 5 FAILED REPLACE THE LEFT LE OUTBOARD SLAT SKEW DETECTION MECHANISM ASSY PER AMM DMC-B787-A-27-89-03-00A-520A-A/DMC-B787-A-2SDR DXTA2024111401110Control Unit · faultedDURING APPROACH PRIM STAB TRIM FAIL APPEARED TWICE. DURING CLIMB AND DESCENT RECEIVED NOSE TRIM DOWN MESSAGES. FOLLOWED PROCEDURE AND THE STAB TRIM WAS AT 1.0 AND WOULD NOT MOVE. WE ARE UNABLE TO DESCEND FASTER THEN 270 KTS WITHOUT THE TRIM NOSE DOWN CAS MESDR J7SA2024120300421Controller · failedTHE #2 FCE FAILED DURING ENGINE RUNS. UNIT WAS SWAPPED AND FAULT FOLLOWED UNIT. REPLACED #2 FCE IAW PHENOM 300 AMM 27-03-01.SDR ANCF202411032024Transducer · faultedF/ CTL ALTN LAW (PROT LOST) IN ACCORDANCE WITH TSM 27-40-00-810-807-A FAILURE FOR THS ACTUATOR, ITEM 1 (B) OPERATIONAL TEST OF THS ACTUATOR ELECTRICAL CONTROL WAS PERFORMED, FAILURE ON STEP A 3.GROUND SETTING WITH ELAC 1 FAULT IN ACCORDANCE WITH AMM TASK 27-SDR CALA2024110400990Actuator · faultyREF ELAC 2 PITCH TRIM FAULTS. PFRS FAULTING THS ACTR POS ERROR 9CEOF ELAC2/IDEFCS 1. IF FAULT REPEATS, REPLACE THE "PITCH TRIM ACTUATOR" (AN LRU ON THE TRIMMABLE HORIZONTAL ACTUATOR) PER AMM 27-44-57. **REF TSM 27-93-00-810-836, PRE SB 27-1248. CARRIED BY ELSDR CALA2024102100883Flt Controls · unknownTO MAINTAIN STRAIGHT FLIGHT, PLANE IS IN APPRX3 DEGREE RIGHT BANK BELOK APPROX FL260 VISUALLY CHECKED ALL FLIGHT CONTROL SURFACES, NO ANOMALIES NOTED. PERFORMED BITE TESTS OF ALL FLIGHT CONTROL COMPUTERS AND ELEVATOR AND AILERON DAMPING TESTS PER MCDU. NO DISSDR DXTA2024101800871Roll Servo · defectiveDURING FLIGHT, THERE IS A SNAGGING, GRABBING FEEL IN THE FLIGHT CONTROLS WHEN THE YOKE IS TURNED ABOUT 10 DEGREES DEFLECTION TO THE LEFT. IT COULD NOT BE FELT DURING FLIGHT CONTROL CHECK ON THE GROUND. CORRECTIVE ACTION; PERFORMED AILERON SERVO TEST REF AMM 22SDR HYIA20241003001Unknown · faultedPILOT EXPERIENCED AN UNCONTROLLED ROLL TO THE RIGHT IN CRUISE WITH THE AUTOPILOT ENGAGED. TROUBLESHOOTING IN PROGRESS.SDR YENA2024092001287Unknown · abnormalFLT#816, JFK-SYR. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK) 'AFTER TAKE OFF ACCL THROUGH 250 TO 290 KTS DURING TURNS THE AIRCRAFT WOULD SKID BACK AND FORTH AT A RAPID RATE W/ AP AND WO AP ONLY IN TURNS ALT WAS 5000 CLIMB TO 15000; SDR ABXA20240916174Circuit Breaker · faultedDURING TAXIOUT BEFORE TAKE OFF RUDDER POS INDICATOR DID NOT MOVE DURING RUDDER CHECK.AC RETURNED TO THE GATE AND MTX GROUNDED AC . THEY RESET CIRCUIT BREAKER E16 AND E17 IAW B767 AMM 20-60-01 OPS TEST OK IAW B767 AMM 27-28-00 REMAINS ETOPS 180,AND MTX RETURNEDSDR CALA2024090600578Computer · faultySTAB TRIM UNCOMMANDED NOSE DOWN TRIM DURING LANDING ROLLOUT. MAI N ELEC TRIM NOT APPLIEDTALKED TO PILOTS. STAB ON LAND ROLLOUT WITH AUTO PILOT OFF TRIM STARTED TO GO FULL DOWN. PILOT MADE SURE HAND WAS OFF ELECTRIC TRIM. WHEN NOTICED WAS OFF THEY HOT TRIM CUT SDR CALA2024090500561Computer · faultedPER INBOUND CAPTAIN, AT ALTITUDE IN CRUISE, EXPERIENCED UN COMMANDED ROLL RIGHT. MAX ROLL AUTHORITY LIMIT STOP WAS REACHED. AIRCRAFT WAS AT FL 340, 255KTS ON ARRIVAL. THEY WERE APPROACHING A WAYPOINT THAT REQUIRED A SLIGHT RT TURN. AUTOPILOT STARTED THE RIGHSDR J7SA2024090300415Controller · unserviceableCREW RECEIVED SWPS FAULT, FLAP FAIL AND PTRIM BKP FAIL CAS IN FLIGHT. EXECUTED NO FLAP LANDING. REPLACED FCE #1 IAW PHENOM AMM 27-03-01. ALL FOLLOW-ON CHECK PASSED AND NO FURTHER CAS MESSAGES PRESENT.SDR CALA2024082700503Switch · faultyNOSE TRIM DOWN FAILED LEAVING 12000 FT 280KT BOTH SIDES SIMULATED 10000FT-25000FT 200KTS-300KTS WITH PITOT/STATIC TEST E QPT, AIR MODE, FLAPS UP/DOWN, ENGINES SIMULATED, IN ORDER TO ACT IVATE MACH TRIM, COULD NOT DUPLICATE SIMULATED 200KTS-300KTS TO ELEV PITOTSDR CALA2024082600494Indication Sys · indicationERRONEOUS MAX SPEED BARS ERONIOUS MAX SPEED BARBER POLE FROZE AT 270, BOTH PILOT AND COPILOT SIDE CREW REPORTS ON CLIMB BOTH CAPT'S AND F.O. 'S BARBER POLES STOPPED INCREASING AT 270 KNOTS WHEN THEY SHOULD HAVE INCREASED TO 300 OR MORE. CREW STOPPED INCREASINGSDR JR2R20240821817Fitting · crackedRH MLG WHEEL WELL LOWER FITTING FOR AILERON QUADRANT ASSY, LOWER SIDE OF WING SPAR 2 IS CRACKED. REPLACED.SDR SWIA202408210001Switch · faultedAFTER TAKE OFF ON DEPARTURE WE RECEIVED A MACH TRIM, STAB TRIM, AND STALL FAIL MESSAGE. QRH DID NOT RESOLVE, MOVING AND PULLING ON CAPTAIN SIDE STAB TRIM DISCONNECT SWITCH ALLOWED STAB/MACH TRIM TO BE REENGAGED. (FLIGHT 4735 - FILED CLOSED) REMOVED AND SDR YENA2024081901128Computer · faultedFLT#8644, MLB-JFK. (AIRCRAFT PERFORMED AN AIR TURN BACK TO MLB). 'F/CTL ELAC 1 PITCH FAULT ON CLIMB OUT; REPLACED ELAC 1 COMPUTER & ELEVATOR SERVO OB STS WO# 3521 NR 25.'SDR K11A2024081300277Sensor · out of limitsDURING CLIMB SOON AFTER REACHING 1000 FT CLIMB AGL FEEL DIFF PRESS AND SPEED TRIM FAIL ANNUNCIATOR LIGHTS ILLUMINATED, ELEVATOR CONTROL WAS MARGINALLY HEAVY, AND AUTO PILOT WOULD NOT MAINTAIN PITCH CONTROL. : R&R ELEVATOR FEEL COMPUTER IAW B737 AMM 22-31-37 PASDR CALA2024081302203Probe · obstructedFEEL DIFF PRESS LIGHT LIGHT ON FEEL DIFF PRESS LIGHT BURNED OUT AS WELL RELAMPED ELEV FEEL LIGHT. OPS CHKS NORMAL. FOUND BLOCKAGE IN RT ELEV PROBE. CLEARED BLOCKAGE AND PERFORMED LEAK CHK PER AMM 27-31-37. READINGS NORMAL, INDICATIONS NORMAL. NO LKS NOTED.SDR DALA2024081308065Servo Valve · faultedSHIP 3273 - ATO - AT 20KTS DUE TO F/CTL ELAC 1 PITCH FAULT. CORRECTIVE ACTION: R/R SERVO VALVE AT LEFT BLUE ELEVATOR SERVOCONTROL (34CE3). OPS CHECK GOOD. (LP:5718676)SDR 4DPA2024081100001Computer · failedCREW REPORTED EICAS MSG SPS 2 INOP & STICK PUSHER FAIL APPEARED CLIMBING THROUGH FL270ISH. RAN QRH AFTER FOLLOWING QRH STEP TO PUSH OUT THE STALL PROTECTION 2 WE GOT ANOTHER MASTER CAUTION FOR SPS1-2 INOP. CONSULTED WITH MAINTENANCE AND RETURNED TO DAL. CORR ASDR YENA2024082101135Elect Module · failedFLT#603, JFK- . (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'MULTIPLE ELAC 2 PITCH FAULT; PERFORMED TSM 27-93-00-810-845-A FOUND ELECTRONIC MODULE #2 AT FAULT. REMOVED AND REPLACED ELECTRONIC MODULE IAW AMM 27-44-57 OPS CHK GOOD NO FAULTS AT THIS TIME.'SDR 2024F00187Flt Controls · trippedF/CTL FAULT IN CRUISE, AUTO FLT AP OFF IN CRUISE. IAW TSM 27-51-00-810-836-A STEP A (1) (2) (3) A-B & C OF SOLENOIDE WERE CHECKED WITHIN LIMITS. IAW AMM 27-51-00-710-001-A WTB TEST ON SFCC1 WAS PERFORMED TEST OK. ADDITIONAL ACTION SEE WO 18376426SDR UIEA2024071900697Skin · delaminatedLHW T/E I/B AFT FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)SDR YENA2024073001059Computer · faultedDURING HEAVY MAINTENANCE: FLIGHT CONTROLS - ELEVATOR AILERON COMPUTER SYSTEM (ELAC) - INSTALL SOFTWARE STANDARD L104 ON ELAC B WITH DATA LOADING CAPABILITY ON CEO, SUPPORTING SAFETY BEYOND STANDARD FUNCTIONS; REFERENCES
/1/ AIRBUS SB A320-27-1305
/2/ AIRBUS SDR YENA2024073001058Computer · faultedDURING HEAVY MAINTENANCE: FLIGHT CONTROLS - ELEVATOR AILERON COMPUTER SYSTEM (ELAC) - INSTALL SOFTWARE STANDARD L104 ON ELAC B WITH DATA LOADING CAPABILITY ON CEO, SUPPORTING SAFETY BEYOND STANDARD FUNCTIONS; REFERENCES /1/ AIRBUS SB A320-27-1305 /2/ AIRBUS RISDR SWAA2024072214617Cable · out of adjustDURING LANDING AT ABOUT 100 FEET AN UNCOMMANDED ROCKING OF THE WINGS FROM LEFT TO RIGHT HAPPENED ALL THE WAY DOWN TO TOUCHDOWN.<[01] INTERROGATED FSEU; FOUND F/C 27-51351; T/E FLAP UCM.<BR>PERFORMED FIM TASK FLAP LOAD RELIEF TEST 27-51-830. NO FAULTS;[02] SUSPSDR J7SA2024080500412Controller · faultedON TOUCHDOWN, RECEIVED GND SPLR FAIL AND SPOILER FAULT CAS. REPLACED #1 FCE. PERFORMED SUCCESSFUL RIGGING AND OPS CHECK. WORK COMPLETED IAW AMM 27-03-01.SDR J7SA2024080500413Controller · faultedON LANDING, GND SPLR FAIL AND SPOILER FAULT CAS MESSAGES POSTED. SPOILER INDICATION ON MFD SHOWED FAIL IN YELLOW. REPLACED #2 FCE IAW EMB505 AMM 27-03-01. ACCOMPLISHED MFS RIGGING PER EMB505 AMM 27-50-00. SPOILER SYSTEM OPS CHECK GOOD AND NO CAS ILLUMINATED.SDR DALA2024071307093Flt Controls · abnormalSHIP 3254 DISC: ON APPROACH TO MSP, SPEED BRAKE EXTENSION CAUSED LEFT WING TO DROP BEFORE AP CORRECTED TO WINGS LEVEL. C/A: INSPECTED SPOILERS DEPLOYED - THEY ARE EQUAL. PERFORMED CAT III AUTOLAND TEST PER A320 AMM 22-97. OPS CK GOOD. NO 30 DAY HISTORY. OK FORSDR YENA2024071100988Module · failedFLT#909, BOS-NAS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS). 'CB Q16 TRIPPED IN FLT C/B TRIPPED R ELEC BAY ECAM; SEE ITEM-2 9SLAVED IN ELAC-2 PER AMM 27-93-34, NO HELP. FOLLOWED TSM 27-93-00-810-836-A & R/R PITCH TRIM ACTUATOR ELECTRONIC MODULE-1 PER AMM 27SDR HALA20240708182Control System · faultedATB - F/CTL PRIM 1 PITCH FAULT, PRIM 2 PITCH FAULT, PRIM 3 PITCH FAULT; F/CTL ALTN LAW. PERFORMED OPS CHECK OF PITCH TRIM ACTR PER AMM 27-44-00-710-805-A, OPS CHECK GOOD. PERFORMED EFCS 1/2 SYS TEST, EFCS1 TEST FAIL. DURING BITE TEST OF EFCS 1, TEST FAILED 3 SDR YENA2024070100925Computer · failedFLT#2065, BOS-RSW. (AIRCRAFT DIVERTED TO RIC). 'ELAC 2 FAULT IN FLT ALONG WITH BURNING ODOR . DID NOT RESET AND BURNING ODOR STAYED; REMOVED AND REPLACED ELAC 2 COMPUTER PER AMM 27-93-34. OPS CHECK GOOD AT THIS TIME REF LP 4048103-1 9PER TSM 05-50-00-810-831-ASDR QMLA2024070120080Flt Controls · malfunctionedAIRCRAFT WAS APPROX 10NM OF KDOV, AT AN ALTITUDE OF 1000-1100 MSL, AIRSPEED WAS ABOUT 130KIAS. CRUISE TORQUE WAS SET TO APPROXIMATELY 65%. PILOT HEARD A CHANGE IN BLADE NOISE FOLLOWED IMMEDIATELY BY AN UN-COMMANDED NOSE UP PITCH. THE ACFT WAS GREATER THAN 3SDR CALA2024061901863Motor · faultedTRIM SWITCH DOES NOT OPERATE CORRECTLY ELEC TRIM INOP BOTH LEFT AND RIGT YOKE. UP AND DOWN INOP. REMOVED AND REPLACED STAB TRIM MOTOR IAW AMM 27-41-71 OP CHECK GOOD IAW AMM 27-41-71, 27-41-00, AND 22-11-81.SDR CALA2024061700010Module · faultedERRONEOUS OVERSPEEDWARNING DURING FLAPRETRACTIONVMO WARNING AFTE R THAT PER CREW VERBAL WAS BELOW OVERSPEED BY 6 KNOTS ON CLIMB AND DECENT, GROUND TEST RESULTS, FOUND ADM 19FP3 DISCONNECTED FROM PITOT LINE.,SDR AALA202406132006Flaperon · failedAIRCRAFT WAS GROUNDED: AIRCRAFT 7BC CLT-DUB DIVERTED TO JFK ON ACCOUNT OF LOSS OF FLAPERON. THE CREW DECLARED AN EMERGENCY, AND THE AIRCRAFT LANDED OVERWEIGHT, WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTEDSDR DALA2024060305737Jackscrew · corroded-AD- FOUND CORROSION ON LOWER JACKSCREW THREADS APPROX 6"ABOVE LOWER STOP. SUMMARY SEE NRC 006-0001:2740-01114-05 /002 00007: REPLACED JACK SCREW PER AMDS 2740-01114-05. CLOSING REQUIREMENTS RII: INSPECTOR 00260220. (LP #0373180)SDR QMLA2024052820055Computer · unserviceableON CLIMB-OUT FROM BASE, PASSING THROUGH ABOUT 600FT MSL, THE ROLL SAS CAUTION LIGHT ILLUMINATED ON THE COCKPIT DASH. THIS WAS ACCOMPANIED BY A WOBBLE IN THE ROLL AXIS, AND A CHANGE OF CONTROL/TRIM FORCE FEEL IN THE CYCLIC. THERE WAS ALSO A VERY STRONG SMELL OFSDR VNAA2024052911102Connector · dirtyRUDDER LIMITER CAUTION AFTER TAKEOFF / REMOVED SSCU 1, CLEANED CONNECTORS AND LUBRICATED SEALS OF ELECTRICAL CONNECTORS ON MOUNTING TRAY THEN REINSTALLED SSCU 1 IAW CRJ 900 AMM 27-61-05-000/400-801-A01, PERFORMED SPOST IAW CRJ 900 AMM 27-61-05-740-801-A03 OPS SDR AWKA202405290003Control System · multiple fail(DECLARED EMER.) (DIVERTED) CREW REPORTED DURING CLIMB AS GEAR MADE THE UPLOCKS MULTIPLE CAS MESSAGES POSTED, PITCH TRIM, YAW DAMP, MACH TRIM. MESSAGES BEGAN TO EXTINGUISH, STAB. TRIM REMAINED INOP. PERFORMED AFCS FAULTS PER TECH SUPPORT, OPS CHECKS GOOD ON GSDR DALA2024052905608Computer · faultedDUE TO APPEARANCE OF F/CTL ALT LAW MESSAGE CAUSED BY AN ELAC 2 FAULT DURING THE APPROACH. ELAC 1 ALREADY ON MEL. CORRECTIVE ACTION: REPLACED NBR 2 ELAC.SDR QXEA2024052300130Aileron Sys · unknownRT AILERON DROOP WITH HYDRAULICS OFF. NORMAL OPERATION WITH HYDRAULICS ON. REMOVED FROM SERVICE. NO ASSOCIATED FAULT CODES FOUND IN CMC. GAINED ACCESS TO THE RIGHT WING AILERON PCU'S IAW AMM 29-10-00-790-801-A, NO LEAKS NOTED. COMPLIED WITH PCU COMPENSATOR POSSDR DALA2024052305442Computer · faultedSHIP 3141 - MISC/DE - DUE TO APPEARANCE OF F/CTL ALT LAW MESSAGE CAUSED BY AN ELAC 2 FAULT DURING THE APPROACH. ELAC 1 ALREADY ON MEL. CORRECTIVE ACTION: REPLACED NBR 2 ELAC. (LP 5471064)SDR DALA2024051705293Computer · burned outSHIP 3079 - ATB - DUE TO ELECTRICAL SMELL IN THE COCKPIT. CORRECTIVE ACTION: FOUND ELAC 1 BURNED OUT. CORRECTIVE ACTION: REPLACED NBR 1 ELAC, RECIRCULATION FILTERS, AND AVIONICS FILTER. (LP 0343125)SDR J7SA2024070100407Control Unit · unserviceableCREW RECEIVED PTRIM NML FAIL, GND SPLR FAIL, SWPS FAULT, AND SPOILER FAULT AFTER STARTUP. REPLACED FCE # 1. REPLACED FCE # 2. RIG COMPLETED WITH NO DEFECTS NOTED. OPS CHECK GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01/SB505-27-0022.SDR YENA2024051600749Secu · failedFLT#1294, MCO-HPN. (AIRCRAFT DIVERTED TO JFK) 'ECAM SEC 2 FAULT- ECAM/QRH COMPLETE WITH NO IMPROVEMENT; REMOVED AND REPLACED SEC 2 COMPUTER IAW AMM 27-94-34. OPS CHECK GOOD. A/C OK TO CON'T SVC.'
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