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 2016FA0000276Spring · missingDURING AN UNSCHEDULED INSPECTION OF THE FLIGHT CONTROL GUST LOCK SYSTEM, IT WAS NOTED THAT THE LT AILERON STOP ARM SPRING WAS MISSING. AN INSPECTION OF THE RELEVANT ZONE DID NOT FIND THE SPRING IN THE AREA. IT APPEARS THAT THE SPRING HAS BEEN MISSING SINCE TMay 13, 2016 · N95NB · Cessna 560XLSDR ASAA2016051216711Control Cable · out of adjustWHILE PERFORMING LAND VERIFY TEST NR 49, FCC-S FAILS 49.35 BITE TEST W/AIL POS SENSOR-1 FAULT. MESSAGE NR 22-11145. ACFT GROUNDED. REF FIM 22-12, TASK 813, PERFORMED AILERON RIGGING TEST REF 22-11-00, AILERON POSITION SENSOR ADJUSTED REF 22-11-29 TO COMPLETE May 12, 2016 · N584AS · Boeing 737890SDR 2016FA0000243Power Supply · shortedON PREFLIGHT THE UNINTERRUPTABLE POWER SUPPLY, FOR THE FLY-BY-WIRE SYSTEM WOULD NOT TEST. SUBSEQUENT INVESTIGATION RELEVELED THAT WIGGLING THE CIRCUIT BREAKER ON THE FRONT OF THE UNIT WOULD CAUSE THE UNIT TO INTERMITTENTLY START AND FAIL. UNIT HAD RECENTLY BMay 9, 2016 · N6D · Gulstm GVISDR QXEA2016050300289Flt Controls · malfunctionedTAKEOFF ABORTED DUE TO TAKEOFF WARNING AT 105 KNOTS. REPLACED CONDITION QUADRANT. OPS CHECK GOOD. C/W INSPECTION AFTER EXCESSIVE BREAKING. NO DEFECTS NOTED. FUNCTIONAL CHECK OF BRAKES GOOD.May 3, 2016 · N444QX · Bombdr DHC8402SDR GTIA2016042901440Computer · failedWHILE CRUISING AT FL 320, IN ALT CRUISE, THE ACFT WHILE ON AUTOPILOT, WOULD CLIMB AND OR DESCEND IN AN ABRUPT MANNER RESULTING ALTITUDE DEVIATIONS AT UP TO 50 FT AND VERTICAL SPEEDS AS HIGH AS 500 FPM, THIS OCCURRED APPROXIMATELY 12 TIMES DURING THE FLIGHT. TApr 29, 2016 · N619NK · Airbus A320232SDR 2016FA0000179Trim System · malfunctionedPILOT REPORTED A VERIFIED PITCH TRIM RUNAWAY DURING DESCENT WITH AUTOPILOT OFF AND NOT USING MANUAL TRIMS.Apr 14, 2016 · N824SA · Pilats PC1247ESDR A6WA201643702Not Reported · unknownBOTH ELEVATOR & AILERON CONTROLS FEEL HEAVY IN FLIGHT ON BOTH SIDES, AUTOPILOT OFF.Mar 14, 2016 · N410AW · Cndair CL6002B19SDR AALA201603089043Computer · defectiveAIRCRAFT WAS GNDED. CREW RECEIVED ON TAKEOFF A FLIGHT CONTROL ELAC 2 PITCH FAULT & ABORTED THE TAKEOFF. REPLACED THE ELAC 2 & LT INBD SERVO VLV IAW AMM 27-93-34 & AMM 27-34-51. SEE AALA201603099014 FOR ADDITIONAL PART INFORMATION.Mar 7, 2016 · N828AW · Airbus A319132SDR LR7A2016030100769Pulley Bracket · corrodedDURING FS93, BULKHEAD REPAIRS, FOUND THE FLIGHT CONTROL RT PULLEY BRACKET CORRODED, RBL19-RBL24, WL186-WL195. REPAIR BY REPLACEMENT ACCOMPLSIHED IAW LM DWG 350247, REV G AND SMP 581, CH 91-00.Mar 1, 2016 · N401LC · Lkheed 382GSDR LR7A2016030100768Pulley Bracket · corrodedDURING FS 93 BULKHEAD REPAIRS, FOUND THE FLIGHT CONTROL LT PULLEY BRACKET CORRODED, LBL19-LBL24, WL186-WL195. REPAIR BY REPLACEMENT ACCOMPLSIHED IAW LM DWG 350247, REV G AND SMP581 CH 91-00.Mar 1, 2016 · N401LC · Lkheed 382GSDR AALA201602279002Computer · faultedAIRCRAFT WAS GNDED. FLIGHT CONTROL ELAC 2 PITCH FAULT ON TAKEOFF. POWER UP DISCONTINUED TAKEOFF AT 5-10 KNOTS. PERFORMED BITE TEST OF EFCS SYS. OPERATIONS CHECK OF SIDE STICK ASSEMBLY IAW TSM 27-30-00-810-817. OPERATIONAL CHECKED GOOD, NO FAULT FOUND.Feb 26, 2016 · N709UW · Airbus A319112SDR CA160223006Unknown · unknown(CAN) AFTER COMPLETING DE-ICING THE ACFT, TAXIED TO RUNWAY FOR DEPARTURE. DURING THE BEFORE T/O CHECK RUDDER TRAVEL CHECK NORMAL, HOWEVER AILERON IMMOVABLE AND ELEVATORS ONLY MOVABLE VERY SLIGHTLY. ACFT TAXIED BACK TO GATE WHERE MAINTENANCE MET FLIGHT AND WERFeb 18, 2016 · Boeing 777333ERSDR FDEA201602110502Unknown · vibrationCLIMBING THRU FL 320, NOTICEABLE VIB BEGAN LEVELED AT 340, VIBS CONTINUED, SLOWED & EVENTUALLY DESCENDED BACK TO 320, VIBS CONTINUED. NO SECONDARY’S INDICATED, ENG VIBS NORMAL. NO OTHER INDICATIONS, NO FLIGHT CLT INDICATIONS. VIBS INCREASED SIGNIFICANTLY WFeb 11, 2016 · N664FE · Airbus A300F4605RSDR DJFA20160109001malfunctionedPILOT REPORTED THAT DURING APPROACH TWO CAS MSGS, SWPS FAULT & SPOILER FAULT, WERE PRESENT. FLAP POSITION & PITCH TRIM INDICATION WERE INOPERATIVE, RED X'D. FLAPS DID NOT MOVE. AN EMER WAS DECLARED. THE ACFT LANDED WITH NO FURTHER INCIDENT. REPLACED BOTH Jan 9, 2016 · N365FX · Emb EMB505SDR AALA201512289003Computer · defectiveRETURNED & ACFT WAS GNDED. ACFT RETURNED AFTER RECEIVING A FLIGHT CONTROL ALTERNATE IAW ECAM MSG. FLIGHT CREW DECLARED AN EMER & LANDED WITH NO INCIDENTS REPORTED. REPLACED THE NR 1 ELAC IAW AMM 27-93-00. PERFORMED CAT III LAND TEST IAW AMM 27-97-00. TESTDec 27, 2015 · N558UW · Airbus A321231SDR CA151130024Insulation · unsecure(CAN) SOUND DAMPENING INSULATION IN THE PILOTS SIDE FOOT WELL CAME DETACHED AND WAS INTERFERING WITH ELEVATOR OPERATION ON THE ELEVATOR TORQUE TUBE DURING CERTAIN PHASES OF FLIGHT. INSULATION WAS REINSTALLED AND RE SECURED. ELEVATOR OPS CHECKS SATISFACTORY.Nov 26, 2015 · Emb EMB505SDR AALA20151104004Computer · faultyECAM WARNING, FLIGHT CONTROL ALTN LAW, PROT LOST. THE FLIGHT DECLARED AN EMER INBOUND, THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. TROUBLE SHOT IAW TSM 27-93-00. FOUND FAULT ON ELAC 1 COMPUTER. RESET & TEST OF ELAC 1 COMPUTENov 4, 2015 · N141NN · Airbus A321231SDR 2015FA0000522Electrical Box · faultyMECHANIC INSTALLED NEW STARTER, STARTER SOLENOID , MASTER SOLENOID. SYSTEM WORKED FOR MORE THAN 10 CYCLES BUT NOT MORE THAN 20 CYCLES WHEN, AFTER A MONTH OF NO USAGE, ACFT STARTER WOULD NOT RESPOND TO START EFFORT. TROUBLESHOOTING REVEALED THAT MASTER SOLENOIOct 12, 2015 · N9146V · Mooney M20CSDR 2015FA0000475Turnbuckle · crackedWHILE ACCOMPLISHING AD 3013-02-13 FOR STABILATOR CABLE TURNBUCKLE AND SWAGED FITTING CORROSION, DISCOVERED THAT THE BRASS TURNBUCKLE WAS BADLY CORRODED AND NEEDED TO BE REPLACED. WHILE INSPECTING THE STAINLESS STEEL SWAGED FITTINGS ATTACHED TO THIS TURNBUCKSep 15, 2015 · N77077 · Piper PA28235SDR 2015FA0000431Actuator · brokenUPON REACHING CRUISE FLIGHT WITH THE AUTOPILOT ENGAGED, THE CREW BEGAN TO TRIM OUT THE AIRPLANE FOR LEVEL FLIGHT AND AS THE TRIM WHEEL WAS TURNING THEY GOT A TRIM IN MOTION WARNING. IT REPEATED MULTIPLE TIMES AND EVENTUALLY SAID CHECK PITCH TRIM. THE CREW DISep 2, 2015 · N7276Z · Cessna 206HSDR HNAA2015090200271Unknown · unknownTROUBLESHOT UNCOMMANDED LT TURN WITH AUTOPILOT ENGAGED, NR 802 MESSAGE OR CAUTION LIGHTS NOTED. INSPECTED AILERON SERVO AND CABLE FOR PROPER INSTALLATION, NO DEFECT. PERFORMED OPS MAINTENANCE ST FOR 45 MINUTES. FLYING WITH LT AND RT AFCS MASTER AND FLYING WITSep 2, 2015 · N941HA · Dhav DHC8102SDR ASMF201507021Pressure Switch · failedDURING TRANSIT CHECK, DURING PREFLIGHT PROCEDURE THE FLIGHT CONTROL LOW PRESSURE LIGHT TURNED OFF IN THE CHANNEL B. PERFORMED FIM 27-21 TASK 814 PROCEDURE, DETECTING THE LOW PRESSURE WARNING SWITCH OF SYS B WITH FAILURE. THE LOW PRESSURE WARNING SWITCH WAS REJul 17, 2015 · N997AM · Boeing 73776QSDR ASOA20150706035Unknown · malfunctionedTHE CREW REPORTED ACFT ROLLED RT SUDDENLY WITH AUTOPILOT ON. ALSO FELT SOME BUFFETING. THE AUTIOPILOT WAS TURNED OFF AND ACFT FLEW WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS . NO FAULTS WERE FOUND. MAINTENANCE REPLACED THEJul 6, 2015 · N14902 · Emb EMB145LRSDR CALA2015070600554Computer · unserviceableSHORTLY AFTER TAKEOFF, METALLIC CLANKING NOISE WAS HEARD FROM THROTTLE QUADRANT. IT WAS STEADY CADENCE AT ABOUT 2 BEATS PER SECOND. THAT WAS ABOVE ABOUT 290 KIAS. ACCELERATING ABOVE 305 KIAS CLUNKING SOUND WAS ALSO HEARD, SAME CADENCE. CREW REPORTED VERBAL Jul 6, 2015 · N37018 · Boeing 777224SDR SIMA20150630001Warning System · false activationSPS 2 INOPERATIVE WARNING & SPS ADV MSG ON EICAS, DURING TAKEOFF ROLL OF APPROX 100 KTS. ABORTED THE TAKEOFF, MSGS DISAPPEARED. TROUBLE SHOT BY FIM 27-36-00. PERFORMED OPERATIONS CHECK IAW AMM 27-36-00. OPERATIONS CHECKED GOOD. DETERMINED TO BE TRANSITORYJun 30, 2015 · N827AE · Emb EMB135KLSDR CA150612009Turnbuckle · cracked(CAN) DURING INSPECTION, FOUR TURNBUCKLES FROM A FLIGHT CONTROL TRIM SYSTEM WERE FOUND CRACKED. ONE MS21251B-5L, TWO MS21251B-2L, & ONE MS21251-B2L. CRACKS ARE LONGITUDINAL IN AREA OF LOCKING GROOVE. REMINDER THERE MAY STILL BE TURNBUCKLES IN SERVICE FROM TJun 12, 2015 · Dhav DHC6300SDR QMLA2015060915046Solenoid · malfunctionedPILOT LEFT THE PAD TO PICK UP MEDICAL CREW. ON HIS WAY OVER, THE PEDAL STOP WARNING INDICATOR ON THE CAUTION WARNING PANEL ILLUMINATED, SO PILOT SLOWED HIS AIRSPEED BELOW 55 KNOTS & IMMEDIATELY RETURNED TO BASE. LESS THAN A MILE FROM THE BASE. RETURNING TO Jun 9, 2015 · N193AM · Bell 407SDR AALA201506019008Unknown · malfunctionedFLIGHT 1897, EN-ROUTE, ON TAKEOFF WITH FLAPS 2, FLEX 54,151,000 POUNDS, HAD PITCH AXIS OSCILLATION & PORPOISING. IT WAS VERY NOTICEABLE AT FIRST, BUT DAMPENED TO NOTHING ABOUT 90 - 120 SECONDS AFTER FLAP RETRACTION. AN OPERATIONAL DECISION WAS MADE TO RETURNMay 30, 2015 · N524UW · Airbus A321231SDR HNAA2015052700172Unknown · unknownRUDDER TRAVEL TO LEFT INDICATION IS 8 DEGREES AT O FLAPS AND 11 DEGREES AT 5 DEGREES OF FLAPS. INSPECTED RUDDER TRAVEL IAW MM 27-05-16 AND INSPECTED PSEU OUTPUT VOLTAGE TO FDAU. FOUND NO FAULTS WITH RUDDER OPERATION O INDICATION IAW AMM BULLETIN NR 27-28.May 27, 2015 · N940HA · Dhav DHC8102SDR 2015FA0000428Control Cable · damagedPROBLEM FOUND ON ANOTHER ACFT. FOUND THE SAME DISCREPANCIES OF WIRE ROPES BOWED AWAY FROM THE CABLE IN THE LOWER AFT STABILATOR CONTROL CABLE, PN 62701-12 AND THE UPPER AFT STABILATOR CONTROL CABLE PN 62701-13 AS IN OTHER ACFT. THE AC43.13 IS NOT CLEAR AS TOMay 23, 2015 · N8115Y · Piper PA28161SDR SIMA20150515003Flt Controls · vibrationUNUSUAL AMOUNT OF VIBRATION FELT ON THE FLIGHT CONTROLS. DIVERTED DUE HI FREQ VIBE IN FLIGHT CONTROLS. FLIGHT CONTROLS CLIMBING THRU FL280 ALL THE WAY UP TO 360. INTERMITTENT LEVEL OFF & POWER CHANGES DID NOT CHANGE THE CONDITION. VIBRATION PERSISTED TO THMay 15, 2015 · N645AE · Emb EMB145LRSDR VQI2015F00017Computer · malfunctionedDURING TAKEOFF, BELOW 80 KNOTS, ACFT HAD REJECTED TAKEOFF. AIRCRAFT CAME BACK TO THE GATE. FLIGHT CONTROL ELAC 2 PITCH FAULT ECAM REJECTED TAKEOFF AND RETURNED TO GATE. IAW PFR, PERFORMED TSM 27-93-00-810-880-A. BITE TEST EFCS 1 AND 2 REPORTED NO FAULTS. May 3, 2015 · N522VA · Airbus A319112SDR AALA201504209023Warning Message · activatedFLIGHT 874 EN-ROUTE, AFTER TAKEOFF, THE ACFT EXPERIENCED UNDUE ACTIVATION OF ALPHA PROTECTION. OVER-SPEED WARNING ACTIVATED AT 170 KIAS. ALPHA MAX STRIP MOMENTARILY VARIED +/ - 20 KTS AT ABOUT 170 KTS. THE FLIGHT DECLARED AN EMERGENCY & DIVERTED. LANDED WApr 18, 2015 · N119US · Airbus A320214SDR SIMA20150407004Unknown · malfunctionedON APPROACH, STALL & RUDDER LIMITER FAILED, ADC FAILED. DECLARED EMERGENCY . LANDED NO INCIDENT. AHRS SYS OPERATIONS CHECKED GOOD IAW AMMM 34-21-01. ADC SYS OPERATIONS CHECKED GOOD IAW AMM 34-13-01 & AMM 34-11-00.Apr 7, 2015 · N517AE · Cndair CL6002C10SDR AALA201504089017Computer · faultyWITH AP ON, OPEN DESCENT, SPEED BRAKES FULL, GOT 5' LT BANK GOING FROM FLAPS UP TO FLAPS 2 RT AT THE END OF FLAP MOVEMENT. R & R BOTH ELAC COMPUTERS IAW AMM 27-93-34-000-001A & 400-001-A. OPERATIONAL CHECK OF ELAC'S IAW AMM 27-93-00-710-001-A IS GOOD.Apr 7, 2015 · N114UW · Airbus A320214SDR AALA201504089002Computer · malfunctionedWITH AP ON, OPEN DESCENT, SPEED BRAKES FULL, GOT 5' LT BANK GOING FROM FLAPS UP TO FLAPS 2 RT AT THE END OF FLAP MOVEMENT. R & R BOTH ELAC COMPUTERS IAW AMM 27-93-34-000-001A & 400-001-A. OPERATIONAL CHECK OF ELAC'S IAW AMM 27-93-00-710-001-A IS GOOD. SEE AApr 7, 2015 · N114UW · Airbus A320214SDR NYFG2015FA0000157Nut · damagedTHE AN365-428 NUT CAME OFF THE AN45-13A ATTACHMENT BOLT. THIS ACTION RESULTED IN THE ELEVATOR CONTROL TORQUE TUBE BECOMING UNATTACHED AND FALLING INTO THE FUSELAGE LEAVING THE ELEVATORS UNRESPONSIVE AND INEFFECTIVE. CHEMICALS DETERIORATING THE FIBER LOCKING Apr 4, 2015 · N623LA · Airtrc AT402ASDR ASOA20150327021Actuator · faultyTHE CREW REPORTED YAW TRIM SELF ACTUATES BOTH RT AND LT AT RANDOM. MAINTENANCE REPLACED YAW TRIM ACTUATOR. OPS CHECKS WERE GOOD.Mar 27, 2015 · N16919 · Emb EMB145LRSDR ANCF2015032401Pressure Switch · faultyAFTER ENG 1 START ELAC 1 PITCH FAULT WAS PRESENTED ON ECAM. IAW AMM 27-92-17 PB 401 PRESS SWITCH HYD FLIGHT CONTROL, 10CE1, WAS REPLACED, TESTED SATISFACTORY. IAW AMM 27-94-34 PB 401 THE SECOND ONE WAS REPLACED, TESTED OK.Mar 24, 2015 · N821AV · Airbus A320214SDR ANCF2015032001Warning System · false activationBEFORE TAKEOFF ELAC 1 PITCH CONTROL FAULT MSG APPEARS. IAW AMM TASK 27-93-00-810-947 FALSE ELAC WARNING WAS PERFORMED & NO HELP. TRANSFER TO DMI 257 MEL 27-93-01 CAT B. IAW AMM 27-93-00-040-001A TEST WAS PERFORMED SATISFACTORY & IAW MEL 27-93-01.L THE PROCMar 20, 2015 · N821AV · Airbus A320214SDR CA150320002Bolt · corroded(CAN) WHILE CHECKING COMMUNIQUE 2015-01-ATA27, IT WAS NOTICED THAT THE BOLT WAS BADLY CORRODED. A NEW BOLT WAS INSTALLED.Mar 18, 2015 · Beech B200SDR ANCF2015030806Warning System · activatedAFTER ENG START ELAC 1 FAULT WAS PRESENTED, RESET WAS UNSUCCESSFUL. IAW AMM 27-93-00-710-001-A, OPERATIONAL TEST OF ELAC 1 WAS PERFORMED WITH SATISFACTORY RESULTS.Mar 9, 2015 · N451AV · Airbus A320214SDR HALA2015030700031Computer · malfunctionedETOPS SIGNIFICANT ITEM, ECAM PRIM 1 FAULT, PRIM 1 SWAPPED TO PRIM 3 POSITION. OK TO CONTINUE IAW MEL 27-93-1B, DMI 50574. NO HISTORY 14 LEGS, FAULT TRANSFERRED FROM 1 TO 3. PRIM IN POSITION 3 IS FAULTY. PERFORMED BITE TEST OF EFCS. CHECK OK IAW AMM 27-96-0Mar 7, 2015 · N392HA · Airbus A330243SDR CA150309006Bearing · seized(CAN) WHILE CHECKING COMMUNIQUE 2015-01-ATA27 IT WAS NOTICED THAT THE BOLT WAS BADLY CORRODED AND THE BEARING WAS SEIZED. A NEW BOLT AND BEARING WAS INSTALLED.Mar 4, 2015 · Beech B200SDR ANCF2015021901Unknown · vibrationSTRONG VIBRATION ON TAIL SECTION DURING CLIMB. IAW AMM TASK 27-34-00-200001A WAS PERFORMED CHECK OF THE ELEVATOR SERVO CONTROL & HINGE BEARING FOR TOO MUCH PLAY & CONDITION. TESTED SATISFACTORY. LT ELEV GREEN SYS 4.90MM, LT ELEV B SYS 5.0 MM, RT ELEV YELLOFeb 19, 2015 · N992TA · Airbus A319112SDR Y2PA2015021900004Unknown · unknownCLIMBING THRU 28,000, APU GENERATOR AND NR 2 GENERATOR REPEATEDLY BOUNCED BETWEEN APU & NR 2 GEN UNTIL THE LT APU AC BUSS WAS SWITCHED OFF. AT THE SAME TIME, ACFT BEGAN TO OSCILLATE VIOLENTLY. DISCONNECTED AUTOPILOT, DECLARED AN EMERGENCY AND DIVERTED. RAFeb 15, 2015 · N831US · Doug DC983SDR JJBA20150122010Flt Controls · stiffFLIGHT CONTROLS ARE ABNORMALLY STIFF & RESISTANT TO PITCH & ROLL IN FLIGHT. PERFORMED CABLE TENSION CHECKS, NO DEFAULT FOUND. OPERATIONS CHECK FLIGHT IS REQUIRED.Jan 22, 2015 · N876CA · Dhav DHC8311SDR SIMA20150111004Relay · malfunctionedON DESCENT IN ICING CONDITIONS CREW RECEIVED STAB ANTI-ICE FAIL MSG. CREW COMPLIED WITH AOM VOL 1 PROCEDURES. DECLARED AN EMER & LANDED WITHOUT INCIDENT. R & R RELAY K0537 IAW AMM 30-11-00. OPS CHECKED GOOD IAW AMM 30-00-00.Jan 11, 2015 · N813AE · Emb EMB135KLSDR USAA2015010900007Computer · faultyUNCOMMANDED NOSE DOWN ON APPROACH LEVEL FLIGHT. THEN SE THRUST NON-RESPONSIVE. DISCONNECT AUTO PILOT 1 & AUTO THRUST, MANUALLY FLOWN, NO ECAMS & NORMAL LANDING. REPLACED NR 1 ELAC IAW AMM 27-93-34-000-001 400-001-A.Jan 8, 2015 · N770UW · Airbus A319112SDR WX0A2014121672301Unknown · malfunctionedON APPROACH WITH FLAPS 40 CONFIGURED FOR LANDING AT 134 KTS WING DOWN TRIM REQUIRED 4 UNIT OF RT TRIM & ACFT STILL ROLLED TO LT WING DOWN. PERFORMED GVI OF AILERON & SPOILER SYSTEMS, NO DEFECTS NOTED. PERFORMED AILERON CHECK IAW AMM 27-10-00. SYS OPERATIONSDec 9, 2014 · N415NV · Doug DC983
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