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.

SDR 01FDEA00415Fairlead · brokenMAIN DECK CONTROL CABLE FAIRLEAD FOUND BROKEN AT BS 575, RBL 30 BELOW FLOOR PANEL.Jun 7, 2001 · N583FE · Doug MD11SDR SIMA200115601Pin · corrodedSBP - RIGHT ELEVATOR OUTBOARD ATTACH SPIGOT CORRODED. REMOVED AND REPLACED ATTACH SPIGOT IAW SAAB AMM 55-10-20. (M)Jun 5, 2001 · N335AE · Saab 340BSDR 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 FLMay 27, 2001 · N457TM · Boeing 737214SDR 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.May 26, 2001 · N461PS · Dorner DO328100SDR 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. THEMay 22, 2001 · N37208 · Cndair CL6002B19SDR 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.May 9, 2001 · Emb EMB145SDR 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.Apr 11, 2001 · N968AX · Doug DC941SDR LS1R072190Cable Drum · stretchedCABLE DRUM STRETCHED.Apr 10, 2001 · N51AG · Bell UH1HSDR 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.Mar 26, 2001 · N375SC · Amd FALCON2000SDR 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 TUBEMar 25, 2001 · N321DL · Boeing 737232SDR 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 CONMar 18, 2001 · N248US · Boeing 737201SDR COMA0160313Warning System · activatedCONFIG AILERON AND CONFIG SPOILER DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECKS NORMAL.Mar 4, 2001 · N977CA · Cndair CL6002B19SDR 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 Feb 16, 2001 · N959N · Doug DC931SDR 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, Jan 31, 2001 · Boeing 747400SDR 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 LANDINGJan 4, 2001 · N916PG · Boeing 727287SDR SWIA972198Switch · looseCAPTS TRIM SWITCH ON YOKE LOOSE, CAUSING CIRCUIT BREAKER TO POP. RETURNED TO FIELD. RESECURED SWITCH. OPS CHECK GOOD.Dec 12, 2000 · N271YV · Emb EMB120ERSDR 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 SERVICENov 30, 2000 · N631AW · Airbus A320231SDR 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 BONov 24, 2000 · Airtrc AT802SDR 20001017SH011Control Cable · frayedRIGHT HAND BALANCE CABLE FRAYED. (X)Sep 28, 2000 · N4128X · Piper PA34220TSDR 20001018SH008Control Cable · frayedREAR TRIM CABLE FRAYED AT REAR DRUM. (X)Sep 15, 2000 · N9299E · Piper PA34220TSDR 20001017SH021Control Cable · frayedREAR TRIM CABLE FRAYED. (X)Sep 14, 2000 · N4142N · Piper PA34220TSDR 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 DISCONSep 8, 2000 · N820SC · Airbus A300B4203SDR AU000701Control Cable · broken(AUS) CABLE BROKEN. (X)Sep 1, 2000 · Cessna 404CESSNASDR 20000911SH032Control Cable · frayedTRIM CABLE FRAYED AT REAR DRUM. (X)Aug 21, 2000 · N4144P · Piper PA28181SDR 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 REAug 20, 2000 · Dhav DHC3SDR 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 THAug 17, 2000 · Dhav DHC3SDR 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 AIRCAug 17, 2000 · Dhav DHC3SDR 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 Aug 17, 2000 · Dhav DHC3SDR 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.Aug 3, 2000 · Dhav DHC8102SDR 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 EXTERNAJun 26, 2000 · N6910T · Piper PA46310PSDR 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 625Jun 25, 2000 · Dhav DHC3SDR 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.Jun 11, 2000 · N109ML · Fokker F28MK0100SDR 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.Jun 9, 2000 · N496US · Fokker F28MK4000SDR 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)May 31, 2000 · N755AS · Boeing 7374Q8SDR 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 UNTILMay 19, 2000 · N41676 · Piper PA46350PSDR 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 IMay 12, 2000 · N360AX · Doug DC1010SDR 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 GFeb 20, 2000 · N116ZX · Cessna 182SSDR CA000218008Switch · damaged(CAN) RUDDER BOOST SYSTEM - INOPERATIVE ON RIGHT SIDE.Feb 8, 2000 · Beech 200BEECHSDR DL72L000197Rib · crackedSLAT RIB NR 11 WAS CRACKED AT THE UPPER FWD END. INSTALLED A REPAIR DOUBLER PER 57-54-0 FIG 804.Jan 26, 2000 · N507DA · Boeing 727232SDR TWRA0006Nut · missingDURING C-CHECK, FOUND R/W INBOARD AILERON OUTBOARD HINGE BOLT NUT MISSING. REPLACED NUT PER MM 27-11-04. (M)Jan 10, 2000 · N603FF · Boeing 747130SDR DL73E992535damagedRT WING OUTBOARD FLAP JACKSCREW DAMAGED. REPLACED NR 8 JACKSCREW TRANSMISSION ASSY.Nov 16, 1999 · N369DL · Boeing 7372S3SDR 99ZZZM632Elac · failedELAC NR 1 FAILED IN FLIGHT. REF MEL 27-93-01 C NR 1146 ELAC INDICATION PER MAINTENANCE CONTROL. (M)Aug 24, 1999 · N304ML · Airbus A320231SDR 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 PANELJul 12, 1999 · Beech 200BEECHSDR 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 FLOORBOARApr 29, 1999 · N39471 · Piper PA44180SDR 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 SECTIONFeb 10, 1999 · N803DH · Doug DC873FSDR 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.Nov 1, 1998 · N639AW · Airbus A320232SDR 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 Oct 21, 1998 · N581FE · Doug MD11FSDR AU981330Control Cable · worn(AUS) NUMEROUS CONTROL CABLES FRAYED WITH BROKEN WIRES AND STRANDS.Oct 8, 1998 · Sctaiv PIONEERSER3SDR 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.Aug 17, 1998 · Cessna 172MSDR 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. Aug 8, 1998 · N857AW · Bag ATP
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