JASC 2797
Service difficulty reports · 920
Reports filed under 2797 · Flight Control System Wiring, 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 = '2797' 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 = '2797' 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 8343720Wire · brokenYAW DAMP RUDDER BOOST, ENGAGED ON ITS OWN. REPAIRED WIRE AT NR W13 AT PIN A ON LT ENGINE P5 CONNECTOR AND REPLACED YR5-65 SENSOR.SDR GAIA04078OPWire · brokenFLT 2715 - ELP-DFW-FWA - DURING CLIMB, THE UPPER RUDDER INDICATOR WAS SWINGING BETWEEN MINOR INDICIES. AT 10,000 AGL THE LOWER RUDDER SWUNG HARD LEFT AND THEN ANOTHER LEFT NOT AS HARD. CREW FOLLOWED FLIGHT CONTROL EMERGENCY PROCEDURE AND RETURNED TO ELP. ANSDR RAIA00406005Wire · brokenMAIN PITCH TRIM INOP. MAINTENANCE REPAIRED BROKEN WIRE TO CAPTAIN'S TRIM SWITCH.SDR QXEA200400376Wire · brokenSEA - FLIGHT 2296 - WHILE EN ROUTE TO SEA, THE FLIGHT SPOILER 1 PUSH OFF ILLUMINATED. THE NUMBER 1 HYDRAULIC PRESSURE WAS NORMAL AND THE CHECKLIST WAS RUN. THE CREW PUSHED OFF THE FLIGHT SPOILER AND THE MASTER CAUTION ROLL SPOILER INBOARD HYDRAULIC ILLUMINATSDR PCAA0405204Wire · brokenFLIGHT NR 3828 LGA REPORTED THEIR STANDBY ELEVATOR TRIM AS BEING INOPERATIVE. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE FOUND THE GROUND AT TERMINAL BLOCK 2211 GS1 BROKEN. GROUND WAS REPAIRED AND ALL SYSTEMS OPERATIONAL CHECK GOOD. AIRCRASDR AUS20040389Terminal · faulty(AUS) STANDBY RUDDER SHUTOFF VALVE WILL NOT CLOSE ON SELECTION. INVESTIGATION FOUND WIRES W2212-0521-20 AND W5170-0505-20 TOTB262-XA3 NOT LOCKED INTO POSITION CAUSING OPEN CIRCUIT.SDR AUS20040374Wire · broken(AUS) FLAP CONTROL SYSTEM WIRE BROKEN. FAULT TRACE TO BROKEN WIRE A157B-A25799200 TO FLAP UP CONTROL SWITCH.SDR P5CA0401081Wire · brokenON ENGINE START, ELEVATOR FEELS LIGHT. DID NOT COME ON WITH HYD SYST NR 2 PRESSURIZED AND SYST 3 UNPRESSURIZED. FOUND BROKEN WIRE AT MISOI, REPAIRED IAW 20-10-13. PERFORMED SYST CHECK PER 27-31-00, SYST OPS NORMALLY.SDR SWIA200413189Wire · brokenFIRST OFFICER'S STALL WARNING SHAKER INOP. REPAIRED BROKEN WIRE NEAR SHAKER CONNECTOR ON CONTROL COLUMN OF FIRST OFFICER'S SIDE. OPS CHECKS GOOD.SDR SWIA200413132Wire · brokenFLAPS FAILED AT 17 DEGREES AFTER TAKEOFF AT SLC. RETURNED TO SLC. FOUND WIRE BROKEN AT PIN -K- ON CANNON PLUG 2P2CE TO RT BPSU AND CANNON PLUG SOCKETS CORRODED. REPLACED CANNON PLUG 2P2CE WITH A SERVICEABLE UNIT IAW CRJ WM 20-17-80. FLAPS SYSTEM OPERATES NSDR RAIA00403028Wire · faultyTAKE OFF CONFIGURATION WARNING FAULT DURING TAXI. MAINTENANCE REPAIRED BROKEN WIRE AT STICK SHAKER, RESET POWER AND OPS CK OK.SDR CA040405001Wire · malfunctioned(CAN) FLAP JAM OCCURRED AFTER TAKE OFF. AIRCRAFT RETURNED TO THE STATION FOR RECTIFICATION. FLAP SFCC COMPUTER WAS RESET BY MAINTENANCE. FLAP SYSTEM WAS INSPECTED AND OPERATED SEVERAL TIMES WITH NO FAULT FOUND. AIRCRAFT WAS DISPATCH WITH NO FURTHER PROBLEM. AISDR GLBA20030598Wire · brokenLOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOODSDR SWIA200413095Wire · damagedFIRST OFFICER'S STAB TRIM SWITCH WILL NOT TRIM NOSE UP. TAXI BACK TO GATE. REPAIRED WIRE IAW WM 20-00-00. OPS CHECK GOOD IAW MM 27-40-00.SDR COMA0460223Wire Harness · malfunctionedFLIGHT 5020 FLAPS FAILED CAUTION MESSAGE. REPLACED PDU WIRE HARNESS.SDR GAIA04052OPConnector · dirtyON TAKEOFF ROLL, AFTER FLAP RETRACTION THE NR 4 LEADING EDGE DEVICE INDICATED IN TRANSIT. NO ROLL WAS NOTED, THE AIRCARFT CONTINUED FLIGHT. CLEANED THE NR 4 LEADING EDGE FLAP SWITCH. RAN FLAPS SYSTEM OPS CHECKED NORMAL, THE AIRCRAFT WAS RETURNED TO SERVICE.SDR GAIA04050OPConnector · dirtyAFTER TAKEOFF, THE NR 3 LEADING EDGE DEVICE DID NOT RETRACT ON FLAP RETRACTION. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. CLEANED CONNECTOR ON NR 3 LEADING EDGE DEVICE ACTUATOR. RAN FLAPS SYSTEM, OPS CHECKED NORMAL. THE AIRCRAFT WAS SDR GTIA040151Wire · brokenFLL - FLT 262 - AFTER TAKEOFF RETRACTED SLATS, GOT DISAGREE LIGHT. CONFIRMED SLATS DEPLOYED AT 280 KTS OVERSPEED WARNING. ALSO AT LANDING, INDICATIONS WERE 40/40 AND TAKEOFF, GPWS WENT OFF. FOUND FLAP BUSS TO ELEVATOR SERVO FORCE LIMITER CABLE BROKEN. REMOSDR CALA0400165Wire · shortedMACH TRIM INOP LIGHT ILLUMINATED AND AIRCRAFT BEGAN TO DUTCH ROLL AT 31,000 FEET EN ROUTE. QRH PROCEDURE COMPLETED, BUT NO CHANGE RESULTED. THERE WAS MINIMUM CONTROL WITH THE RUDDER. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTESDR UPS04841946Cable · brokenAILERON BINDING ON RIGHT TURN. LEFT AILERON BUSSING CABLE BROKEN AT I/B OF AILERON. INSTALLED LEFT .125 INCH BUSS CABLE PER MM 27-13-22 UP TO STEP (H) ACCOMPLISHED REMAINING STOPS AND ADJUSTED PER MM 27-10-17-5.SDR GAIA04025OPConnector · dirtyDURING CRUISE, THE NR 4 LEADING EDGE FLAP SHOWS EXTENDED WITH THE FLAPS RETRACTED. CLEANED AND RESEATED THE CONNECTOR ON THE NR 4 LEADING EDGE FLAP SWITCH. OPS CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)SDR SWIA200412775Wire · damagedON TAXI WITH FLAP SELECTOR SET TO 15 DEGREES AFTER 1-2 MINUTES, FLAP & ADV SWS ON MAP POSITION INDICATOR 0 DEGREES OUTBOARD LIGHT BAR 4 LIGHTS NACELLE, INBOARD AND COMD ONE LIGHT BAR. AFTER FIVE MINUTES SYSTEM CORRECTED ITSELF. INSTALLED NEW WIRES TO I/B, O/SDR MEX2003574Wire Harness · damagedFLT 605 - DFW-MEX - AIRCRAFT RETURNED TO PLATFORM, DURING THE TAXI THE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' DID NOT COME ON. THE SYSTEM WAS REVISED AND THE WIRE BUNDLE OF THE PROXIMITY SENSOR D1-33 WAS FOUND WITH DAMAGES. THE WIRE BUNDLE WAS REPAIRED IAW MMSDR C2XA03IA112Wire Harness · chafedPILOT REPORTED THAT DURING TAKEOFF THE SPOILERS DEPLOYED AND DID NOT RETRACT EVEN AFTER STOPPING THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LEFT SPOILER PROXIMITY SWITCH HARNESS, OPERATIONALLY CHECKED THE SPOILER SYSTEM AND RETURNED THE AIRCRAFT TO SESDR SWIA200312682Wire · brokenWIRE LEADING TO STALL PUSHER MOTOR ON CAPTAIN'S YOKE IS BROKEN. REPAIRED WIRING TO NR 1 STICK SHAKER AS REQUIRED. OPS CHECK GOOD.SDR SIMA200333802Connector · looseBOS - FLT 4592 - FLAP FAIL/SPS ADVANCED FLAPS REMAINED AT ZERO REGARDLESS OF FLAP SELECTOR POSITION. RESECURED CONNECTOR ON FLAP VELOCITY SENSOR PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR P5CA0300994Connector · looseBOTH GREEN BAND & STAB TRIM GREEN BAND LIGHT CAME ON DURING TAXI BEFORE T/O. FOUND R586 LOOSE RESET R586, OPS CKS GOOD PER 27-48-00.SDR QXEA200301463Wire · brokenON FLIGHT 2246 SPOILER 2 PFCS SWITCH LIGHT ILLUMINATED IN FLIGHT. REPAIRED BROKEN WIRES ON LEFT WING SPOILER CLUTCH QUADRANT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD.SDR AUS20031204Wire · loose(AUS) PILOT REPORTED AILERONS JAMMING AFTER TAKE OFF. THE JAMMING CONTINUED INTERMITTENTLY AND AFTER LANDING THE PILOT WAS ABLE TO DUPLICATE THE PROBLEM. IT WAS SUSPECTED THAT A LOOSE WIRE MAY HAVE BEEN FOULING WITH THE PULLEY ON THE PILOTS CONTROL YOKE.SDR SWIA200312595Wire · looseCAPTAIN'S TRIM SWITCH WILL NOT TRIM DOWN. SOLDERED WIRE ON TRIM SWITCH. OPS CHECK GOOD.SDR EWG2003F00001Wire · chafedPILOT REPORTS (SPEED BRAKE) CIRCUIT BREAKER POPS EVERY TIME SPEED BRAKES EXTEND MANUALLY OR IN AUTO MODE PROBLEM WAS ISOLATED TO A CHAFED WIRE BETWEEN PIN 5 AND PIN X AT CONNECTORS JR004 AND PS003. THE WIRE WAS ARCING AGAINST THE RT ENGINE MOTIVE FLOW LINE PSDR MWEA030412Wire · brokenAFTER CONTROL CHECK, THE RUDDER TRAVEL UNRESTRICTED LIGHT WENT OUT, WHEN LEFT RUDDER IS MOVED 3 INCHES THE LIGHT ILLUMINATED AND WHEN THE RIGHT PEDAL IS MOVED FULL TRAVEL THE LIGHT STAYS OUT. REMOVED AND REPLACED SWITCH AND BROKEN WIRES.SDR MWEA030396Wire · brokenELEVATOR POWER ON WOULD NOT ILLUMINATE WHEN CHECKED DURING TAXI CHECKLIST, ELEVATOR PUSHED FORWARD TO0 EASY. REMOVED AND REPLACED CONNECTOR, ALSO FOUND BROKEN WIRES, SPLICED IN NEW WIRES.SDR MWEA030363Wire · brokenRUDDER TRAVEL UNRESTRICTED LIGHT NOT ON. FOUND WIRE BROKEN NEAR RUDDER, REPAIRED WIRE.SDR SWIA200312387Wire · broken(STALL FAIL) MESSAGE WHILE ENROUTE COMPLIED WITH THE APPROPRIATE QRH PROCEDURE. REPAIRED BROKEN WIRE AT CONNECTOR FOR CAPT STICK SHAKER.SDR MEX2003408Wire · looseAIRCRAFT ARRIVED WITH CAPTAIN REPORT OF (WARN ELEX/ SLAT FLAP ELEC STATUS) MESSAGE IN EICAS. DURING REVISION WAS DETECTED BCPU POPPED DUE TO LOOSE OF WIRE NUMBER 5 TB 5001. THE BCPU C/B 6-14 WAS RESETED AND FSEU POWER OPERATED IN A NORMAL WAY TEST PERFORMED SDR AUS20031155Wire · broken(AUS) FLAP UP MICROSWITCH WIRE BROKEN. SWITCH IS LOCATED BEHINDFLAP SELECTOR.SDR SWIA200312369Wire · looseCAPTAIN'S ELECTRIC TRIM SWITCH UP POSITION INOP. FOUND TERMINAL SOLDER JOINT LOOSE ON TRIM SWITCH. RESOLDERED WIRE TO TERMINAL. OPS CHECK OK.SDR SWIA200312299Wire · damagedCAPT'S FLIGHT DIRECTOR PITCH WANDERS IN FLIGHT. FIRST OFFICERS AUTOPILOT WAS ENGAGED AND THE AUTOPILOT FAIL ILLUMINATED ON MAP. REPAIRED WIRING TO NR 1 GO-AROUND SWITCH AND COPILOTS TRIM SWITCH WIRES ON YOKE. AP SYSTEM OPS CHECKED GOOD IAW MM 22-11-00.SDR SWIA200312309Wire · chafedSTAB TRIM CH 1 STATUS MSG ILLUMINATED INFLIGHT. COMPLIED WITH QRH PROCEDURE, WOULD NOT RESET. REPAIRED CHAFED WIRE CD75C22 AT P0268. STAB TRIM SYSTEM OPERATIONAL CHECKS GOOD IAW AMM 27-40-00.SDR CA030825007Wire · chafed(CAN) DURING REASSEMBLY CONTROL WHEEL, A TECHNICIAN DISCOVERED TWO BARE WIRES HIDDEN INSIDE THE CONTROL WHEEL ASSY. THE BARE WIRES COULD BE PARTIALLY SEEN FROM A SMALL OPENING IN THE FRONT SIDE OF THE CONTROL WHEEL PAD. AFTER DISMOUNTING THE CONTROL WHEEL ASSESDR 2003FA0000835Wire · frayedREPLACED W2094304, DUE TO 4 FRAYED WIRES. FOUND AT ANNUAL. LOCATION , BEHIND LEFT GEAR WELL COVER WHERE CABLE COMES INTO WING.SDR SWIA200312082Wire · brokenFLAPS CONTROL FAULTED INFLIGHT. OUTBOARD PAIR ON ANNUNCIATOR FLASHING. TROUBLESHOT FLAP SYSTEM. FOUND BROKEN WIRES IN HARNESS AT LEFT OUTBOARD FLAP ACTUATOR. REPAIRED BROKEN WIRES IAW WM 20-21-00. OPS CHECK GOOD.SDR CA030520003Wire · burned(CAN) FIVE WIRES DAMAGED FROM ARCING, AT WIRE CLAMP LOCATED OUTBOARD OF NR 2 SLAT OUTBOARD ATTACH ARM AT LT WING STATION 480. NO EVIDENCE OF RUBBING OR CHAFING.WIRE BUNDLE CLAMPS FOUND TO BE IN COMPLIANCE WI TH AD CF-84-08R2. SUSPECT BRITTLE WIRING DUE AGE OF SDR IXXA0300035OWire · chafedON CLIMB OUT FROM TOL TO ATL CREW REPORTED RUDDER MANUAL REVERSION LIGHT CAME ON. THE CREW REPORTED THAT THE RUDDER WAS POWERED BUT THE LIGHT WAS STAYING ON. CREW RETURNED TO TOL. MAINTENANCE VERIFIED HYDRAULIC PRESSURE AND QUANTITY ARE OKAY. MAINTENANCE FOUSDR AUS20030480Wire · chafed(AUS) FLAP WIRING CHAFED IN AREA BETWEEN CONNECTOR D11822 PINS 6 AND 7AND CONNECTOR D11824 PINS 1 AND 2.SDR RAIA00304112Wire · disconnected5540-STL- RUDDER TRIM CD POPPED. MAINTENANCE REPLACED WIRE VAD 5055VC, OPS CHECK GOOD.SDR SWIA200311856Wire · brokenAFTER LANDING UNABLE TO RE-CENTER RUDDER TRIM, TRIMS ONLY TO THE LEFT, RIGHT TRIM INOP. REPAIRED BROKEN WIRES ON SWITCH. OPS CHECK GOOD.SDR SWIA200311833Connector · damagedFLAP CONTROL FAULT INDICATED FOR INBOARD FLAPS. FLAPS WOULD NOT RETRACT ON THE GROUND. REMOVED AND REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR WITH A NEW PART. OPS CHECK OF FLAPS PERFORMED SATISFACTORY. P/N ON MS3476L12-10S.SDR CA030506006Wire · failed(CAN) THE AME INSTALLED THE COMPONENT (OVERHAULED JAN/02) DURING 2002-2003 WINTER MAINTENANCE. A FUNCTION CHECK OF THE UNIT REVEALED INTERMITTENT INDICATIONS. REMOVAL OF THE UNIT REVEALED THAT THERE WAS A BROKEN WIRE INTERNALLY. A PREVIOUSLY UNDISCOVERED CRACK
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