JASC 2700
Service difficulty reports · 1,742
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 YENA2026101200942Control Servo · malfunctionedFLT#789, DTW-FLL. DURING CLIMB NOTICED A SMALL AMOUNT OF FWD STICK ABOUT 1/4" REQUIRED TO FOLLOW FLIGHT DIRECTORS(NOSE WANTED TO PITCH UP) CONTINUED FOR 30 MINS AFTER TOC & WENT AWAY UNTIL DESCENT, RETURNED & WAS PRESENT FOR DURATION OF FLT. ACFT COMPLETELY COSDR 2026FA0000824Trim Tab · faultedAILERON TRIM INDICATION, AILERON TRIM TAB POSITION INDICATION. INTERMITTENT ERRATIC FLICKERING OF THE AILERON TRIM INDICATION. SYMPTOM APPEARS RANDOMLY, UNRELATED TO TRIM POSITION OR FLIGHT PHASE, AND HAS PERSISTED ACROSS MULTIPLE COMPONENT REPLACEMENTS. ASDR VQMA20261008001Actuator · lack of lubeELEVATOR TRIM FROZE UP DURING CLIMB OUT, FREED WHEN DESCENDING BELOW FREEZING LEVEL. REMOVED LT & RT ELEVATOR TRIM TAB ACTUATOR ACCESS PANELS AND PERFORMED A DETAILED VISUAL INSPECTION OF THE TRIM TAB ACTUATORS AND ASSOCIATED CABLES. PORTIONS OF THE EXISTING SDR DALA2026100605512Computer · faultedATO - DUE TO "F/CTL PRIM 1 PITCH FAULT". SWAPPED FCPC1 AND FCPC3 AND PLACED FCPC3 ON MEL THEN REPLACED SERVO VALVE. OK FOR SERVICE. (8991859)SDR 2026FA0000813Arm · backed outNOTED UNUSUAL FEEL IN ELEVATOR CONTROL DURING INSP. PROBLEM DETERMINED TO BE A HEAVY RUB OF THE TORQUE TUBE USED BY THE PITCH SERVO AND THE LOWER ELEVATOR PRIMARY CONTROL CABLE. THE PITCH SERVO CONTROL ARM WAS FOUND TO HAVE ALL FOUR SCREWS THAT SECURE IT TO THSDR 4T1R00002Spigot · corrodedDURING THE BORESCOPE INSPECTION OF THE INBOARD FLAP INTERNAL STRUCTURE PER AMM 57-51-00-290-801, STEP F.(3), CORROSION WAS IDENTIFIED INSIDE THE AFT SPIGOT TUBE INNER BORE ON THE RIGHT-HAND INBD. FLAP. REFERENCE BOMBARDIER REPAIR ENGINEERING ORDER 700-57-51-53SDR 2026FA0000804Flt Controls · corrodedALL FLIGHT CONTROLS BORESCOPED. ALL FLIGHT CONTROLS EXHIBIT CORRISION THROUGHOUT, FLAPS, AILERON, & RUDDER. CORROSION FOUND THROUGHOUT ALONG THE SEAM LINES FROM INADEQUATE SURFACE PREP AND THROUGHOUT THE FLIGHT CONTROL STRUCTURE AND RIVET JOININGS. EXAMINED A SDR J7SA2026100200526Fce · unserviceableREPEAT FLAP FAIL. REPLACED FCE #1 IAW EMB 505 AMM 27-03-01. OPS AND RIGGING CHECK GOOD.SDR DALA2026092705364Computer · malfunctionedDURING DECENT FOR APPROACH, WITH SPEED BRAKES DEPLOYED. AIRCRAFT MADE AN UNCOMMANDED RIGHT ROLL WITH NOTICEABLE BANK. T/S IAW TSM 27-10-00-810-842A, PERFORMED OPS TEST OF BOTH ELACS 1 & 2. TESTED OK. PERFORMED ELAC TEST IAW AMM 27-93-00-710-001-A. PERFORMEDSDR DALA2026092805368Computer · faultyON THE ARRIVAL TO DTW, THE ACFT HAD A NOSE DOWN PITCH. THE ECAM FOR FLT CONTROL ELAC 2 PITCH FAULT COMPLIED WITH ECAM & QRH. IAW AMM 27 93 34, TSM 27-93-00 810 867 710-001, REPLACED ELAC 2. OPS TESTED GOOD. PERFORMED EFCS AND SIDESTICK TESTING, NO FAULTS. ASDR J7SA2026092900524Fce · malfunctionedCREW REPORTS FCE1 CB POPS WITH BATTERIES ON. REPLACED FCE # 1 IAW EMB-505 CH 27-03-01. OPS CHECK GOOD.SDR IPXA2026092379070Accelerometer · oscillatesDURING CLIMB EXPERIENCED NOTICABLE OSCILLATIONS COMING FROM THE TAIL THAT DISSIPATED AT CRUISE. ALL ENG INDICATIONS NORMAL VERTICAL STABILIZER ACCESS PANELS AND RH ELEVATOR PCU PANLES CLOSED IAW AMM 27-31-05 REV149. FOUND FAULT DURING YAW DAMPER SYSTEM BITE PRSDR J7SA2026092900523Fce · malfunctionedCREW RECEIVED GND SPOILER FAIL ON DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AT CRE. REPLACED #2 FCE IAW EMB 505 AMM 27-03-01. OPS CHECKS GOOD.SDR J7SA2026092900522Fce · unserviceableAFTER ENGINE START "SWPS FAULT", "GND SPLR FAIL", "PTRIM NML FAIL", "SPOILER FAULT" CAS MESSAGES ILLUMINATED. CAS MESSAGES WOULD NOT CLEAR AFTER SHUTDOWN AND POWER RESETS. REPLACED # 2 FCE IAW EMB-505 300 AMM 27-03-01.SDR ASAA2026091066874Flt Controls · faultedAIRCRAFT HAD HARD ROLL TO THE RIGHT, 10 DEGREES AT GEAR EXTENSION, FLAPS 18 UNIT, 170KTS 2100FT. ASA1074 HNL LDG RWY 26L ON AS1074 ON 9/9/2026. GROUNDED - YES. COMPLIED WITH TSI-000725, ALL ITEMS HAD BEEN COMPLETED AND SUBMITTED. THE SIGNIFICANT EVENT RESPONSSDR J7SA2026090300519Fce · faultedCREW RECEIVED SPOILER FAIL AND GND SPOILER FAIL CAS UPON TOUCHDOWN. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS TESTED GOOD.SDR ASAA2026082966644Flt Controls · faultedUNCONTROLLED ROLL ON SHORT FINAL. REPEAT WRITE UP, FLAPS 40, VAPP 143, 400 FEET, AUTOPILOT/AUTO THROTTLES OFF. GROUNDED - YES. COMPLIED WITH TSI-00723 ITEM 1, ALL ITEMS HAD BEEN COMPLETED AND SUBMITTED. THE SIGNIFICANT EVENT RESPONSE PROCESS HAS BEEN COMPLETESDR J7SA2026090100514Fce · faultedFLAP FAIL CAS ILLUMINATED AFTER MOVING FLAP LEVER TO NR 1 POSITION. REPLACED FCE NR 1 IAW AMM 27-03-01. REPLACED FLAP SELECTED LEVER AND FLAP POWER DRIVE UNIT IAW AMM 27-53-01 AND 27-51-07. COMPLIED WITH FLAP RIGGING IAW 27-50-00. OPS CHECKS GOOD.SDR J7SA2026090100515Fce · faultedCONTINUOUS FLAP FAIL UPON BATTERY POWER UP. REPLACED FCE # 1 IAW EMB 505 AMM 27-03-01.SDR AALA202608145189Computer · defectiveAIRCRAFT WAS GROUNDED: THE FLT CREW REPORTED THAT THE ACFT DID NOT TRIM ITSELF PROPERLY DURING PREVIOUS TWO FLTS, BOTH CAPTAIN AND FIRST OFFICER EXPERIENCED UNUSUAL PITCH UP TENDENCIES DURING CLIMB OUT & APPROACH TO LANDING WHILE HAND FLYING ACFT. FLT CREW SDR J7SA2026081700512Fce · faultedCREW REPORTS FCE2 CIRCUIT BREAKER POPS UPON POWERING ON AIRCRAFT. REPLACED FCE 2 WITH IAW AMM 27-05-01. SPOILER RIG AND OPS TEST SATISFACTORY IAW 27-60-00.SDR CALA2026080418250Control Unit · faultedSTABILIZER R2 ADVISORY THIS MESSAGE IS SET WHEN THE R2 CONTROL CHANNEL NOT AVAILABLE FOR TRIM OR WHEN 1ST OFFICER'S TRIM SWITCH HAS BEEN DISAB LED BY COLUMN CUTOUT. R2 REFERS TO ELECTRICAL BUS. DB 27 FCM OPS (RIGHT) DB 27 FCM OPS (CENTER) DB 27 FCM OPS (LT) DESDR HNAA2026080400645Elect Module · faultedON TAKE OFF ROLL AT V1 FLIGHT CONTROL DID NOT RESPOND TO YOKE MOVEMENT. C/W HORIZONTAL STABILIZER ELECTRICAL/ELECTRONIC OPS CHECK IAW AMM 27-40-00-700-802-A. C/W AURAL WARNING OPS CHECK IAW AMM TASK 31-51-00-700-801-A. C/W ELEVATOR CONTROL CABLE TENSION CHECKSDR SIMA20260727001Mau · failedAVNX MAU 1B FAIL IN FLIGHT. ASSOCIATED MESSAGES SPOILER FAULT AND SPDBRK FAIL. EMERGENCY DECLARED. PERFORM POWER DOWN POWER UP RESET PER QRH 7.2.1 AND 7.2.2. MESSAGE EXTINGUISH A/C OK FOR SERVICE. AND PERFORM QRH 7.3.22 AND AMM 27-00-00. OPS CHECK GOODSDR DXTA2026072709024Trim System · failedAT CRUISE FL380 BOTH STAB TRIM FAILED AT 2.2 FOLLOWED BY MACH TRIM. RAN CHECKLIST AND DID NOT CLEAR.SDR DXTA2026072708997Warning Message · illuminatedAT CRUISE FL380 BOTH STAB TRIM FAILED AT 2.2 FOLLOWED BY MACH TRIM. RAN CHECKLIST AND DID NOT CLEAR.SDR J7SA2026080400507Fce · faultedP-TRIM NML FAIL DURING TRIM TESTS. REPLACED FCE 2 AND PERFORMED SUCCESSFUL RIGGING AND OPS CHECK. WORK COMPLETED IAW EMB 505 AMM 27-03-01 AND 27-60-00.SDR J7SA2026080400508Fce · faultedON SHORT FINAL TO LAND, CREW RECEIVED AUTO PTRIM FAIL, GND SPLR FAIL, SWPS FAULT, AND SPOILER FAULT CAS. AIRCRAFT LANDED WITHOUT INCIDENT AT KTRI. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS CHECKED GOOD.SDR FDEA202607170941Fcu · failedDURING CLIMB OUT PASSING 5000 ATS LEVER TRIPPED OFF AND WE LOST POWER TO THE ENTIRE FCP. NO FLIGHT DIRECTORS, NO FMAS. TRIED RESETTING ATS LEVER AND PITCH TRIM AND YD LEVERS. NO LUCK. AIR TURN BACK. MANUALLY FLOWN AND NO AUTO THROTTLES. AMM: 22-15-12-04SDR YENA2026071700583Fcu · failedFLT 1408, CDG-JFK. (ETOPS) SPD/MARH BUTTON MISSING. R & R FCU (2CA) IAW AMM 22-81-12. OPS CHECK OK. CAT III LAND TEST REQUIRED.SDR J7SA2026072200487Flt Controls · multiple failDIVERTED DUE TO SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT MESSAGES AT FL410. THE CREW RAN THE QRH AND DIVERTED TO KSFB. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED FCE #1 IAW AMM 27-03-01.SDR J7SA2026080400509Fce · faultedDESCENDING THROUGH FL340 RECEIVED GND SPLR FAIL, PTRIM NML FAIL, AND SPOILER FAULT. CREW RAN QRH AND LANDED WITHOUT INCIDENT. REPLACED FCE #2. ALL OPS CHECKS GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01.SDR DALA2026062403743Secu · faultedDIV TO BOS DUE TO F/CTL SEC 3 FAULT. REPLACED SEC 3 AND RELAY 41CE3. (LP: 8320072, AIRCRAFT WAS GROUNDED)SDR DALA2026062203695Control Stick · faultedATO - DUE TO PRIM 1 FAULT AT TAKE-OFF. REPLACED CAPTAINS AND F/O SIDESTICKS. (8318232) AIRCRAFT WAS GROUNDED.SDR DALA2026061503564Computer · faultedBOTH ENGINES RUNNING, REJECTED TAKEOFF DUE TO ELAC 1 PITCH FAULT MESSAGE AT 10 KNOTS. DUE TO HISTORY - APPLING ELAC 1 TO MEL & PLAC PER A319/320/321 MEL 27-93-01. M PROC C/W, MCC NOTIFIED. (LP: 8778668, AIRCRAFT WAS GROUNDED)SDR DALA2026061203551Memory Device · shortedDURING PREFLIGHT IN CVG THE F/O THUMBWHEEL ON LEFT SIDE OF YOKE BEGAN TO SMOKE FOR APPROX 30 SECONDS. FOUND F/O CONTROL WHEEL MEMORY DEVICE INTERNAL SHORT. RPLD MEMORY DEVICE PER B737 AMM 33-11. OP CKS GOOD. NO EVIDENCE OF SMOKE. (LOG 8327226 - AIRCRAFT WAS GRSDR VNAA2026051117801Pcu · faultedIB SPOILERONS / IB FLT SPLRS CAUTION IN FLIGHT. REMOVED & REPLACED LH IB MULTI-FUNCTION SPOILER PCU(MPE33) IAW AMM 27-62-01-000/400-801-A02, PERFORMED BLEEDING OF HYD SYSTEM #1 IAW AMM 29-10-00-870-801-A01, LEAK TEST OF THE MULTI-FUNCTION SPOILER DONE IAWSDR DALA2026050102766Computer · faultedATO - AT APPROXIMATELY 10KTS DUE TO F/CTL ELAC 1 PITCH FAULT. ELAC 1 PLACED ON MEL AND CONTINUED. LATER REPLACED ELAC 1. (LP 8038066 - AIRCRAFT WAS GROUNDED)SDR 2026FA0000310Torque Tube · excess playPERFORMED INSPECTION OF THE RUDDER HINGES INSTALLATION DUE TO THE CUSTOMER REQUEST. ALL FOUND SATISFACTORY. DURING THE INSPECTION TECHNICIAN TOUCH THE ELEVATORS LH & RH SIDE AND FEELS FREE PLAY. WITH THE INSPECTION MIRROR AND TORCH PERFORMED QUICK CHECK AND RESDR IPXA2026050990937Torque Box · damagedTHE R/H LWR FWD TORQUE BOX PANEL HAS A DELAMINATED / DISBONDED AREA (1EA) NEAR THE BOTTOM OF THE PANEL. ALL DAMAGE MARKED IN RED.ACCOMPLISH REPAIR IAW SRM REV 124 CHAPTER 51-70-10-2R-2, SRM 51-70-10-2R-0 REPAIR GENERAL PER SRM 55-30-01-2R-5 TO ACCOMPLISH REPASDR DALA2026042002475Unknown · unknownATB - DUE TO AIRCRAFT PITCHING UP WITH A/P OFF. REPLACED ACCELEROMETER UNIT 12CE4, THS ZERO ADJUSTMENT CHECK, AND ELEVATOR FREE PLAY CHECK. NTF, AND ALL OPS CHECK GOOD. (LP: 7729382). AIRCRAFT WAS GROUNDED.SDR DALA2026041602405Computer · faultyATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. ENG 1 G HYD MON C/B WAS FOUND POPPED. REPLACED ELAC 2.SDR QXEA2026041500087Pace · malfunctionedURING CRUISE AT FL370, GOT AN AMBER ELEVATOR FAULT. RAN CHKLIST IN QRH. ON PUSHING FCM ELEVATORS BUTTON IN AND OUT, THE MESSAGE WENT AWAY. UPON LANDING, WE GOT FLT CTRL NO DISPATCH. AFTER PARKING, GOT ANOTHER ELEVATOR FAULT, WHICH WENT AWAY ON ITS OWN AFTER ABSDR 2026FA0000308Control Cable · twistedDURING THE REPLACEMENT OF THE PITCH TRIM ACTUATOR, WE ENCOUNTERED DIFFICULTY RIGGING AND PERFORMING THE OPERATIONAL CHECK OF THE ACTUATOR. UPON FURTHER INSPECTION, THE TECHNICIAN FOUND THAT THE ELECTRIC TRIM AND MANUAL TRIM CABLES WERE INTERTWINED INBOARD OF SDR CALA2026041415351Module · faultedSLAT DRIVE FAIL EICAS MESSAGE CHRONIC ISSUE, PERFORMED WIRE CHECK FROM CONNECTOR DE2702003P03B PIN 26,27 & 28 TO DM2789061P01 4,5,3 ON SLAT SKEW SENSOR. WIRE CHECK GOOD. CHECKED WIRE FROM ACE PIN F16 AND F15 ALSO CHECKS GOOD. SLAT SKEW SENSOR & ACE NEED TOSDR JJBA20260413010Control Unit · inoperativeDURING INITIAL CLIMBOUT, PITCH TRIM BACK UP INOPERATIVE AND PITCH TRIM MAIN INOPERATIVE. REMOVED AND REPLACED HSCU. REMOVED AND REPLACED FO'S YOKE TRIM SWITCH. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.SDR DALA2026040902256Computer · faultyATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. REPLACED ELAC 2. (LP: 8410558) AIRCRAFT WAS GROUNDEDSDR CALA2026041315324Unknown · oscillatesSMALL PITCH OCCILATIONS DURING CLIMBOUT. PRONOUN CED BELOW FL210 . NOT FEL T THROUGH FLT CONTROLS FLT CREW STATES AIRCRAFT PORPOISING OCCURRED THROUGH ALL PHASES OF FLIGHT WITH NO AUTOPILOT ENGAGED, BUT WAS MOST NOTICEABLE IN CLIMB CONFIGURATION AND BECAME MORSDR CALA2026033014895Control Unit · damagedON TAKEOFF, AIRCAFT REQUI RED 5-6 UNITS LT AILERON TO MAINTAIN LE VEL FLIGHT INSPECTED AILERON CABLES ABSB AT B SYSTEM DRUM ASSY. FOUND SHEAR RIVETS SHEARED ON ABSB DRUM. EMERGENCY DECLARED. AILERON POWER CONTROL UNIT REMOVAL AND INSTALATION COMPLETED. ALL OSDR R61A2026031100060Torque Tube · faultedFLAP FAIL EICAS MSG ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. TRANSITORY CONDITION OF FLAP CONTROL SYSTEM. INSTALLED CORBAN, TORQUED, AND COTTER PINNED LT TORQUE TUBE BOLTS.
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