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 01FDEA00415Fairlead · brokenMAIN DECK CONTROL CABLE FAIRLEAD FOUND BROKEN AT BS 575, RBL 30 BELOW FLOOR PANEL.SDR SIMA200115601Pin · corrodedSBP - RIGHT ELEVATOR OUTBOARD ATTACH SPIGOT CORRODED. REMOVED AND REPLACED ATTACH SPIGOT IAW SAAB AMM 55-10-20. (M)SDR BJNA010507Hydraulic LineLOST BOTH A/B HYDRAULIC SYSTEM PRESSURE. INSPECTED A/C FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC LINE FAILURE AT PRESSURE MODULE. A/C IS SAFE FOR ITS INTENDED FERRY FLIGHT WITH THE NR 1 ENGINE 'A' PUMP IN THE OFF POSITION. INSTALLED APPROVED RATED TEMPORARY FLSDR VNAA0106006Rudder · failedTHIS IS A CONTINUATION ODR FOR ODR VNAA0105018. MAINTENANCE INSPECTED AND REPLACED THE RUDDER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL TESTS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR MASA01043Transmitter · defectiveFLT 5778 - DURING APPROACH TO LANDING AT CLT DECLARED AN EMERGENCY BECAUSE OF WHAT THE CAPT THOUGHT WAS A FLAP FAIL PROBLEM. MAINTENANCE WAS CALLED AFTER UNEVENTFUL LANDING. MAINTENANCE TROUBLE SHOT THE SYSTEM AND FOUND OUT IT WAS AN INDICATION PROBLEM. THESDR 2001FA0000075Bearing · failedDURING RECEIVING INSPECTION FLAT NUT IS TESTED ON HOUSING. WILL SPIN FREELY ON BUT THEN LOCKS UP 50 TO 80 PER CENT FAIL RATE.SDR ABXA010124Arm · corrodedTHE LONGITUDINAL TRIM ARM WAS PITTED ON THE UPPER SIDE AT THE CABLE ATTACH BOLT, AFT OF FUSELAGE STATION 218, RBL 40. MAINTENANCE INSPECTED AND REPLACED THE SECTOR ARM.SDR LS1R072190Cable Drum · stretchedCABLE DRUM STRETCHED.SDR 20010413CW012Control Rod · separatedMETAL END OF CONTROL ROD IS SEPARATING FROM CARBON FIBER. A MOVEMENT OF .003 IN WAS OBSERVED DURING OPERATION OF SYSTEM DURING C INSPECTION PART SENT FOR EVALUATION.SDR DL73K010488Torque Tube · stuckELVEATOR JAMMED AND STUCK IN FLIGHT CONTINUED STICKING AND RELEASING THROUGH REST OF FLIGHT DIVERTED TO ATL TRIED ISOLATED A AND B DID NOT HELP. REPLACED ELEVATOR INPUT TORQUE TUBESDR USAASB0108Connector · damagedLGA-PBI - FLT 2693 - DURING A DESCENDING TURN THE CONTROL COLUMN SEIZED. NEITHER THE CAPT NOR THE F O COULD MOVE THE CONTROL COLUMN FOR SEVERAL SECONDS. AFTER A GO-AROUND THE AIRCRAFT LANDED W/O INCIDENT. MX REPLACED THE A/B AILERON PCUS, AUTOPILOT MODE CONSDR COMA0160313Warning System · activatedCONFIG AILERON AND CONFIG SPOILER DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECKS NORMAL.SDR 0100599909Control Cable · restrictedDURING DESCENT, THE AILERON TRIM LOCKED UP COMPLETELY. AILERONS WERE FUNCTIONAL BUT FELT HEAVY IN FLIGHT. AIRCRAFT ROLLED TO THE RIGHT WHEN SPEED BRAKES APPLIED. SPOILERS DEPLOYED ASYMMETRICALLY WITH SPEED BRAKE HANDLE OUT OF STOWED POSITION. FOLLOWED COM SDR S01427003Flap · damagedB18275 AFT LANDING FOUND LH INBD FORE FLAP DAMAGED.C/A:1.LH INBD FORE FLAP, MIDFLAP, LINK, SEQUENCE CARRIAGE, FITTING AND FIX PANEL DAMAGED WERE FOUND. 2.SENT AOG TEAM TO BKK, DAMAGED PARTS WERE REPAIRED OR REPLD. A/C RETURNED TO TPE ON 2001/02/03. 3.MIDFLAP, SDR GAIA01003OPControl Unit · malfunctionedFLT 1735 - BNA-FWA - THE CREW REPORTED THAT THE AIRPLANE VIBRATES AND TE CONTROL WHEEL HARD TO TURN AS IF MAYBE A FLIGHT CONTROL IS OUT OF ADJUSTMENT. IT TAKES TWO UNITS OF RUDDER TRIM TO STRAIGHTEN THE PLANE IN LEVEL FLIGHT. THE AIRCRAFT MADE A SAFE LANDINGSDR SWIA972198Switch · looseCAPTS TRIM SWITCH ON YOKE LOOSE, CAUSING CIRCUIT BREAKER TO POP. RETURNED TO FIELD. RESECURED SWITCH. OPS CHECK GOOD.SDR AWXA0000999Computer · inoperativePHX - DURING CLIMBOUT AFTER TAKEOFF, ECAM F/CTL ELAC2 PITCH FAULT IDENTIFIED; RESET ELAC2 BUT FAILED AGAIN APPROX 1 MIN LATER; PERFORMED AIR TURNBACK TO PHX, UNEVENTFUL LANDING.R/R NO.2 ELAC COMPUTER IAW AMM 27-93-34, TEST OK; A/C RETURNED TO SERVICESDR CA001201021Control Cable · damaged(CAN) WHILE REMOVING PANELS FOR ANNUAL INSP, CABLE FOR ELEV - FLAP INTERCONNECT HAD POPPED OFF FWD LOWER PULLEY ASSY AND WAS TRAPPED BETWEEN PULLEY AND PULLEY GUARD. CABLE P/N 70810-1 HAD BEEN BENT SHARPLY AND WAS SPIKED. INTERCONNECT PUSH ROD WAS BENT AT BOSDR 20001017SH011Control Cable · frayedRIGHT HAND BALANCE CABLE FRAYED. (X)SDR 20001018SH008Control Cable · frayedREAR TRIM CABLE FRAYED AT REAR DRUM. (X)SDR 20001017SH021Control Cable · frayedREAR TRIM CABLE FRAYED. (X)SDR 20010116SG002Aileron · inoperativeAFTER TAKEOFF, LEFT LOW SPEED AILERON WOULD NOT DISCONNECT IN AUTO OR MANUAL MODE AND POPPED CB 7AG. CREW ACCOMPLISHED PROCEDURE A29 AND RETURNED TO LAX AT A SPEED OF LESS THAN 250 KNOTS. NO FUEL WAS DUMPED. LANDING NORMAL. L/N LOW SPEED AILERON WAS DISCONSDR AU000701Control Cable · broken(AUS) CABLE BROKEN. (X)SDR 20000911SH032Control Cable · frayedTRIM CABLE FRAYED AT REAR DRUM. (X)SDR CA000829018Screw · loose(CAN) NOT AN SDR - WHILST CARRYING OUT A 100 HOUR INSPECTION, THE ENGINEER NOTICED THAT THE SCREWS ATTACHING THE COUNTERWEIGHT ARM TO THE SERVO TAB WERE LOOSE. THE TRIM TAB WAS OPENED UP, THE SCREWS WERE TIGHTENED, THE TAB WAS CLOSED UP AND THE AIRCRAFT WAS RESDR CA000829017Control Cable · frayed(CAN) WHILST CARRYING OUT AN 800 HOUR INSPECTION OF THE AIRCRAFT, SEVERAL CABLES WERE FOUND WHICH HAD A QUANTITY OF BROKEN STRANDS BEYOND THE ALLOWABLE LIMITS. THIS IS ONE OF THE CABLES THAT WAS FOUND. IT SHOULD BE NOTED THAT THE AIRCRAFT MANUAL STATES THAT THSDR CA000829016Control Cable · frayed(CAN) WHILST P/N C3CF195-7 AND P/N C3CF199-5. WHILST CARRYING OUT AN 800 HOUR INSPECTION OF THE AIRCRAFT, SEVERAL CABLES WERE FOUND THAT HAD A QUANTITY OF BROKEN STRANDS BEYOND THE ALLOWABLE LIMITS. THESE ARE TWO OF THE CABLES. IT SHOULD BE NOTED THAT THE AIRCSDR CA000829015Control Cable · frayed(CAN) WHILST CARRYING OUT AN 800 HOUR INSPECTION OF THE AIRCRAFT, SEVERAL CABLES WERE FOUND THAT HAD A QUANTITY OF BROKEN STRANDS BEYOND THE ALLOWABLE LIMITS. THIS IS ONE OF TH CABLES THAT WAS FOUND. IT SHOULD BE NOTED THAT THE AIRCRAFT MANUAL STATES THAT THE SDR CA000804007Pseu · failed(CAN) ROLL SPOILER INBOARD / OUTBOARD GROUND CAUTION LIGHTS ILLUMINATED WHEN POWER LEVERS ADVANCE. DURING GROUND RUNS. FAULT PERSISTED WITH AUTO-FEATHER ON OR OFF. DRIVER FAULT ON PSEU. PSEU REPLACED, MICRO SWITCHES CLEANED AND AIRCRAFT RETURNED TO SERVICE.SDR 20000802SH017Rod End · corrodedDURING ANNUAL INSPECTION, TUBE WAS FOUND WITH EXTERIOR CORROSION ON BOTTOM AFT SURFACE. FLAKED OFF LOOSE PAINT FOUND A DEEP PIT. ABLE TO PASS THIS TUBE WITH AN AWL. WAS ABLE TO PUSH THROUGH A SECOND AREA OF TUBE THAT DID NOT HAVE SIGNS OF CORROSION EXTERNASDR CA000921002Cable · corroded(CAN) AIRCRAFT SUNK IN SALT WATER ON A MOORING IN NAIN LABRADOR. AIRCRAFT SALVAGED AND FLOATED. AIRCRAFT FLUSHED WITH FRESH WATER, INSTRUMENTS CHANGED, ENGINE COMPONENTS CHANGED, AIRCRAFT READIED FOR FERRY FLIGHT USING PROCEDURES IN ACCORDANCE WITH CARS 625SDR JBXA0000181Transducer · failedLIFTDUMP FAULTED ON TAKEOFF AT 90 KTS. ABORTED TAKEOFF. REMOVED AND REPLACED LT INBOARD WHEEL SPEED TRANSDUCER. OPS CHECK GOOD IAW F-100 AMM 32-42-02.SDR QXEA0001693Pulley · damagedPDX- THREE FLIGHT CONTROL GUIDE PULLEY''S ABOVE NOSE LANDING GEAR TOP BAY COVER HAS IMPACT DAMAGE. REPAIRED IAW HORIZON AIR EA 4-27-110.SDR ASAA0040075Plate · brokenSEA - DURING SCHEDULED C-CHECK, THE STABILIZER TRIM CABLE GUIDE PLATE WAS FOUND TO BE BROKEN AT STATION 1024 RIGHT SIDE. REPAIRED PER EA 2740-01047. (M)SDR 20000609SH015Control Cable · bindingPILOT NOTICED FLIGHT CONTROLS GETTING STIFF IN ROLL DIRECTION. INSPECTED ENTIRE SYSTEM FOR PROPER ROUTING OF CABLES AND CORRECT TENSION ON PRIMARILY AND AUTOPILOT CABLES. NO DISCREPANCY NOTED. WENT THROUGH ENTIRE SYSTEM AND LUBED ALL ROTATIONAL POINTS UNTILSDR 20001011AP008Pivot · brokenDURING ROUTINE ''A'' CHECK, A LUBE CARD WAS ISSUED FOR THE HORIZ STAB, WHICH INCLUDED THE HINGE FITTING PIVOT SHAFT. DURING THIS TASK, IT WAS NOTED THAT THE HINGE PIVOT SHAFT AND SLEEVE HAD MIGRATED APPROXIMATELY .125 INCH OUT OF THE HINGE FITTING. FURTHER ISDR 20000407SH010Servo · wornWHILE PERFORMING A SERVICE BULLETIN ON A PRIMARY SERVO (SB KS271C-5 ALERT) NOTED THE SERVO GEAR TEETH TO HAVE EXCESSIVE WEAR. GEAR BEARING APPEARS TO BE MAKING METAL. MEAL POWDER RESIN VISIBLE UNDER THE GEAR. GEAR ROTATION IS NOT SMOOTH AND MAKES A SLIGHT GSDR CA000218008Switch · damaged(CAN) RUDDER BOOST SYSTEM - INOPERATIVE ON RIGHT SIDE.SDR DL72L000197Rib · crackedSLAT RIB NR 11 WAS CRACKED AT THE UPPER FWD END. INSTALLED A REPAIR DOUBLER PER 57-54-0 FIG 804.SDR TWRA0006Nut · missingDURING C-CHECK, FOUND R/W INBOARD AILERON OUTBOARD HINGE BOLT NUT MISSING. REPLACED NUT PER MM 27-11-04. (M)SDR DL73E992535damagedRT WING OUTBOARD FLAP JACKSCREW DAMAGED. REPLACED NR 8 JACKSCREW TRANSMISSION ASSY.SDR 99ZZZM632Elac · failedELAC NR 1 FAILED IN FLIGHT. REF MEL 27-93-01 C NR 1146 ELAC INDICATION PER MAINTENANCE CONTROL. (M)SDR AU990713Control Cable · corroded(AUS) CONTROL CABLES, WIRING AND COAXIAL CABLES LOCATED BEHIND THE INSTRUMENT PANEL AND CENTER CONSOLE CORRODED. CORROSION AND SURFACE CORROSION ON MOST EXPOSED STEEL AND CADMIUM PLATED SURFACES. THE AIRCRAFT HAD BEEN TAXIED WITH THE NLG BAY AFT ACCESS PANELSDR 99ZZZX2096Flight Control · fodPRIOR TO TRAINING FLIGHT, AIRCRAFT PRE-FLIGHT INSPECTION REVEALED ELEVATOR CONTROLS WERE FOUND JAMMED NOSE DOWN WITH VERY LITTLE NOSE UP TRAVEL AVAILABLE. MAINTENANCE INSPECTION FOUND LARGE SCREWDRIVER WEDGED IN COCKPIT FLIGHT CONTROLS UNDER COCKPIT FLOORBOARSDR DHL99803003Controls · iced upEXCESSIVE AND RAPID REVERSAL OF TRIM, BUFFET AND PARTIAL LOSS OF CONTROL WITH A/P OFF, IAS 350 KTS AT FL 310. DECLARED EMERGENCY AND LANDED AT LHR. UPON INVESTIGATION, FOUND FLIGHT CONTROLS COVERED WITH ICE IN LAYERS, INCLUDING FLAPS, SLOTS, SPOILERS SECTIONSDR AWXA9800216Elac · malfunctionedDURING FLAP EXTENSION POS 1 TO POS 2 AND POS 2 TO POS 3 AIRCRAFT ROLLED SHARPLY L/R SHORT DURATION ROLL. REPLACED BOTH ELAC COMPUTERS PER 27-93 AND TESTED PER 27-93-00, OK FOR SERVICE.SDR 98FDEA00666Mixer Cable · fodON T/O LEG A/C REQ ALMOST FULL LT AILERON AND RUDDER TO HOLD HEAD. RETURNED TO AIRPORT. FOUND LATERAL CONT MIXER CABLE JAM WITH FOD CAUSING RT WING SPOILERS TO REMAIN IN UP POSITION. REMOVED FOD AND INSP MIXER AND FOUND NO DAMAGE. SPOILER RETRACT WHEN FOD SDR AU981330Control Cable · worn(AUS) NUMEROUS CONTROL CABLES FRAYED WITH BROKEN WIRES AND STRANDS.SDR AU981128Control Cable · corroded(AUS) FLIGHT CONTROL CABLES CORRODED AND WORN. SUBMITTER SUSPECTS CORROSION (RUST) IS A DIRECT RESULT OF THE RECENT STRIP AND RE-PAINT OF THE AIRCRAFT DUE TO CONTAMINATION BY THE PAINT STRIPPING CHEMICALS.SDR UF6A980804Controls · vibrationORD - FLT 5727 - HIGH PITCH HUM HEARD IN COCKPIT AFTER TAKEOFF WITH VIBRATION FELT IN FLIGHT CONTROLS, POWER LEVERS, TILLER, AND FLOOR. MAINTENANCE PERFORMED OPS CHECK OF ENTIRE SYSTEM WITH NO DEFECTS NOTED. TEST FLIGHT WAS PERFORMED AND FOUND SATISFACTORY.
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