BMW Rolls BR700-710A110

Service difficulty reports · 188

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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 engine_model_key = 'BR700710A110'
  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 AT0500005Shutoff Valve · inoperativePILOT GOT A RIGHT ANTI-ICE DISAGREE LIGHT ON THE EAD. REMOVED AND REPLACED THE RIGHT ENGINE ANTI-ICE VALVE.Jan 26, 2005 · N977AT · Boeing 717200 · Air Intake Anti/De-Ice SystemSDR UG82005F00002Squat Switch · contaminatedGROUND SPOILER RED LIGHT CAME ON DURING TAKEOFF. ALSO HAD AMBER WOW FAULT. BLOW DRIED AND CLEANED LT AND RT MLG WEIGHT ON WHEEL SWITCHES AND CONNECTORS. FAULTS CLEARED AND AIRCRAFT RETURNED TO SERVICE. (GM05003) (K)Jan 21, 2005 · N5101 · Gulstm GULFSTREAMGV · Landing Gear Position and WarningSDR UG82005F00001Door · bindingWHEN LANDING GEAR WAS RETRACTED AFTER TAKEOFF, THE LT MLG DOOR REMAINED OPEN. LANDING GEAR WAS CYCLED IAW AFM. THE DOOR WOULD CLOSE WITH THE GEAR SELECTED DOWN BUT WOULD REMAIN OPEN WITH IT SELECTED UP. LT WHEEL WELL, DOOR, UPLOCK, LINKAGE AND PLUMBING WEREJan 12, 2005 · N5102 · Gulstm GULFSTREAMGV · Landing Gear Door Retract SectionSDR 623456Actuator · failedAFTER LANDING, SELECTED FLAPS TO UP BUT DID NOT MOVE. FLAP / STAB FAIL MESSAGE, FLAP / STAB IND INOP MESSAGE.Nov 30, 2004 · N506QS · Gulstm GULFSTREAMGV · Stabilizer ActuatorSDR UG8APA04005Fastener · corrodedCORROSION FOUND ON FASTENERS UNDER MAIN ENTRANCE DOOR SEAL AT THE HINGE AREA. DISSIMILAR MATERIAL CORROSION BETWEEN THE HUCK FASTENERS AND THE SURROUNDING COMPOSITE STRUCTURE. REPLACED HUCK FASTENERS WITH RECOMMENDED FASTENERS FROM THE MANUFACTURE. AIRCRAFTNov 18, 2004 · N920DC · Gulstm GULFSTREAMGV · FastenersSDR AT0400023Engine · failedENGINE FAILURE ON CLIMBOUT, LOUD BANG. ENGINE RPM LOW, RUNAWAY TGT, STARBOARD ENGINE. REMOVED AND REPLACED NR 2 ENGINE.Nov 10, 2004 · N945AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR AMCR200400005Roller · out of positionAFTER LANDING, THE PILOT WAS NOT ABLE TO RAISE THE FLAPS FROM THE 39 DEGREE POSITION AND HAD ASSOCIATED CAS MESSAGES CONCERNING THE FLAP SYSTEM. VISUAL INSPECTION REVEALED THE FLAPS TO BE OVER-EXTENDED WHICH CAUSED EACH OB ROLLER TO BE OUT BEYOND THE FLAP TRANov 3, 2004 · N524AC · Gulstm GULFSTREAMGV · Trailing Edge Flap Control SystemSDR 63710292004Control Unit · defectiveUNCOMMANDED STAB, FLAP/STAB SYS FAIL CH B, FLAP STAB MX REQ CAS MESSAGES.Oct 29, 2004 · N509QS · Gulstm GULFSTREAMGV · Trailing Edge Flap Control SystemSDR 637102404Resolver · defectiveAT FL410 AFTER 3.1 HRS OF FLIGHT, RECEIVED AN AMBER (UNCMDED STAB) MSG ALONG WITH (FLAP STAB SYS FAIL) AND (FLAP STAB MAINT REQ) MSG. HORIZONTAL STABILIZER SYSTEM AND RESOLVER. VERIFIED RESOLVER (SATB) WIRING TO THE FCU. REMOVED AND REPLACED RESOLVER IAW GVOct 23, 2004 · N509QS · Gulstm GULFSTREAMGV · Stabilizer Control SystemSDR 63710112004Control System · malfunctionedON TAKEOFF WHEN FLAPS WERE SELECTED UP THE STOPPED AT APPROX 7 DEGREES. FLAPS WERE CYCLED BUT THEY WOULD NOT MOVE (UP AND DOWN). ON TAXI IN, HOWEVER THE FLAPS WERE SELECTED TO 10 DEGREES THEN UP. THEY WENT UP AND ARE WORKING NORMAL. TECH DISPATCHED PERFORMOct 11, 2004 · N509QS · Gulstm GULFSTREAMGV · Trailing Edge Flap Control SystemSDR HALA0400829Engine · fireCREW REPORTED TO TAXI OUT, NR 2 ENGINE WENT TO 997C. ALOHA OBSERVED FLAMES COMING FROM NR 2 EXHAUST. ALSO, ACARS MESSAGE ENGINE SURGE. ENGINE CHANGE IN PROCESS. (M)Aug 22, 2004 · N478HA · Boeing 717200 · Engine (Turbine/Turboprop)SDR MWEA04124Skin · damagedUPPER FORWARD CORNER OF PASSENGER DOOR SKIN EDGE IS BENT 1.00 INCH X 2.00 INCH. REMOVED DAMAGE AND INSTALLED DOUBLER.Jul 23, 2004 · N904ME · Boeing 717200 · Passenger/Crew DoorsSDR MWEA040123Skin · bentLOWER CORNER OF PASSENGER DOOR SKIN IS BENT AT EDGE 1.00 INCH X 4.00 INCH. REMOVED DAMAGE, INSTALLED EXTERNAL DOUBLER.Jul 23, 2004 · N904ME · Boeing 717200 · Passenger/Crew DoorsSDR 2004FA0000608Line · looseAT FL 410 RECEIVED A CABIN PRESSURE LOW (RED) MESSAGE ON YTHE CAS. AIRCRAFT INITIATED EDM APPROX. FL 380 CAS MESSAGE EXTINGUISHED LEVELED OFF AT FL 200. UNDECLARED AN EMERGENCY. APPROX. 10 MIN LATER RECEIVED ANOTHER CABIN PRESSURE LOW MESSAGE, DECLARED AN EMEJun 25, 2004 · N300K · Gulstm GV · Hoses and TubesSDR YNO2004F00001Windshield · crackedAC WAS ENROUTE, ON A 91 LEG, PILOTS NOTICED THE RT WINDSHIELD OUTER LAYER CRACKED. THE AC DIVERTED AND LANDED WITH NO PROBLEM. MFG SERVICE CENTER REPLACED THE WINDSHIELD AND AIRCRAFT IS RETURNED TO SERVICE.Jun 10, 2004 · N917R · Bombdr BD7001A10 · Flight Compartment WindowsSDR CA040427010Screw · galled(CAN) DURING INCORPORATION OF SERVICE BULLETIN THE SERVICE CENTER TECHNICIAN FOUND GALLING ON THE ACME SCREW AND A SMALL PIECE OF THE SCREW THREAD WAS MISSING. THE PITCH TRIM ACTUATOR WAS REMOVED FROM THE AIRCRAFT AND SHIPPED TO THE VENDOR FOR INVESTIGATION. NApr 6, 2004 · Bombdr BD7001A10 · FastenersSDR 3M57931704Resolver · inaccurateFLAP STAB MISCOMPARE CAS MESSAGE. STAB ACTUATOR HAS BAD RESOLVER.Mar 17, 2004 · N23M · Gulstm GULFSTREAMGV · Stabilizer ActuatorSDR UG8A235JAEec · faultyRT ENGINE ROLLED BACK AFTER TAKEOFF, ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CHANNEL B AND ENGINE OK. TROUBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICE EEC IAW MFG MM AND PERFORMED ENGINE OPERATIONAL CHECKS. ALL Mar 5, 2004 · N920DC · Gulstm GULFSTREAMGV · Fuel Controlling SystemSDR UG82004F00000Eec · faultyRT ENGINE ROLLED BACK AFTER TAKE OF ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CH B AND ENGINE, OK. TROUBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICEABLE EEC IAW MDG MM AND PERFORMED ENGINE OPERATIONAL CHECKS. ALL PMar 5, 2004 · N920DC · Gulstm GULFSTREAMGV · Fuel Controlling SystemSDR PA04001Eec · inoperativeRT ENGINE ROLLED BACK AFTER TAKE OFF ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CH. B AND ENGINE OK.Mar 5, 2004 · N920DC · Gulstm GULFSTREAMGV · Fuel Controlling SystemSDR UG82004F00003Eec · faultyDURING CLIMB, RT ENGINE ROLLED BACK AFTER TAKE OFF ABOUT 20 DEGREES. SWITCHED DAU NR 1 TO CHANNEL B AND ENGINE OK. TROUBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICEABLE EEC IAW MFG MM AND PERFORMED ENGINE OPERATIMar 5, 2004 · N920DC · Gulstm GULFSTREAMGV · Fuel Controlling SystemSDR HALA0400286Eec · failedLT FADEC FAIL CAME ON INFLIGHT. LT ENGINE FAILED ON FINAL VFR CONDITIONS JUST OUTSIDE EWABE NORMAL LANDING. HAL3392 FIM/MRM CODE: 732145. CURRENT FAULTS/ 732115, 732116, AND 732145 REPLACED NR 1 EEC IAW MM. GROUND RUN CHECK, OK. HAL580/4884 PN OFF 114E611Feb 28, 2004 · N485HA · Boeing 717200 · Fuel Controlling SystemSDR HALA0400278Bulkhead · crackedDURING 2A CHECK, TWO CRACKS MEASURING 2.0 INCHES AND 1.5 INCHES WERE FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD AT STA 1178.225 AT LONGERON 17L, IN THE CAPS FORWARD FLANGE. REPAIR IN WORK.Feb 26, 2004 · N484HA · Boeing 717200 · Fuselage Main, BulkheadSDR AT0400003Valve · leakingWHILE RETRACTING GEAR, HAD A NOSE WHEEL RED LIGHT STAY ON. REMOVED AND REPLACED NOSE GEAR SCHRADER VALVE AND SERVICED NOSE STRUT IAW 32-21-01, PERFORMED NOSE GEAR RETRACTION SEVERAL TIMES. OPS CHECK GOOD IAW MM 32-00.Feb 18, 2004 · N604AT · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR MWEA040006Eec · failedRIGHT AND LEFT ENGINE FAIL ALERT CAME ON. REMOVED AND REPLACED ENGINE ELECTRONIC CONTROLLER.Jan 7, 2004 · N907ME · Boeing 717200 · Fuel Control/Turbine EnginesSDR QRX2004F00000Switch · failedSWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BDec 5, 2003 · N84GV · Gulstm GULFSTREAMGV · Engine Thrust ReverserSDR QRX2004F00001Switch · failedSWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BDec 5, 2003 · N84GV · Gulstm GULFSTREAMGV · Engine Thrust ReverserSDR QRX2004F00002Switch · failedSWITCH FAILED. FOUND THE SWITCH HOUSING FULL OF WATER. THIS SWITCH IS LOCATED ON THE TOP SIDE OF THE ENGINE NACELLE. IT APPEARS TO HAVE WATER MIGRATING THROUGH THE SWITCH PLUNGER INTO THE HOUSING. THIS COULD COME FROM BEING PARKED IN THE RAIN OR AIRCRAFT BOct 29, 2003 · N130GV · Gulstm GV · Engine Thrust ReverserSDR 3M5940903Metering Valve · intermittentBRAKES ARE VERY GRABBY WILL NOT APPLY EVENLY.Sep 30, 2003 · N33M · Gulstm GULFSTREAMGV · BrakeSDR 3M59409031Metering Valve · intermittentMETERING VALVES CAUSING GRABBY BRAKES UNABLE TO APPLY EVENLYSep 30, 2003 · N33M · Gulstm GULFSTREAMGV · BrakeSDR AT0300027Engine · failedNR 1 ENGINE FAILURE, ENGINE AUTO SHUTDOWN, TGT NOT EXCEEDED, ENGINE RELIGHT ATTEMPTED, ENGINE SURGING, MANUAL ENGINE SHUTDOWN. ENGINE NOT SHUTDOWN FOR MORE THAN 30 MINUTES. REMOVED AND REPLACED NR 1 ENGINE.Sep 23, 2003 · N924AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR 2003F00589Probe · wornCREW REPORTED ON CLIMB THROUGH 29,000 FT, 'ALT' COMPARISON MONITOR ILLUMINATED. CREW FOUND THE NR 1 MADC IN ERROR. NR 3 SELECTED, AND CLIMB CONTINUED TO FL400. 'ALT' COMPARISON LIGHT ILLUMINATED AGAIN, & NONE OF MADC'S AGREED. ON DESCENT, ALL MADC'S AGAINSep 14, 2003 · N910DC · Gulstm GULFSTREAMGV · Pitot/Static SystemSDR 2003FA0001043Shuttle Valve · leakingOXYGEN ACCESS PANEL ON RIGHT SIDE OF FUSELAGE HAD A NOTICEABLE AMOUNT OF SKYDROL-500 ACCUMALATED INSIDE THE ACCESS DOOR OF THE O-2 SERVICE PANEL. IT WAS DETERMINED THAT THE FLUID WAS COMING FROM THE EMERGENCY LANDING GEAR AIR RELEASE VALVE VENT PORT DUE TO A Sep 3, 2003 · N130GV · Gulstm GULFSTREAMGV · Hydraulic System, MainSDR 2003FA0001174Line · rupturedOXYGEN LINE CONNECTING NR 3 CYL TO AC OXYGEN PRESS PLUMBING RUPTURED AT SWEDGE WHILE OTHER MAINT WAS BEING PERFORMED. ALL 4 OXYGEN CYL WERE SELECTED TO OFF BEFORE COMPLETE DEPLETION OCCURRED. AS PRECAUTION ALL REMAINING ORIGINAL PRESSURIZED OXYGEN SUPPLY LINEJul 24, 2003 · N324SM · Bombdr BD7001A10 · Crew Oxygen SystemSDR HALA0300648Eec · malfunctionedRT ENGINE FADAC ALTN WILL NOT RESET. REPLACED NR 2 EEC IAW MM 73-21-01. RETURN TO SERVICE TEST OK. GROUND RUN OK.Jul 22, 2003 · N481HA · Boeing 717200 · Fuel Controlling SystemSDR MG3478109Brake Assy · brokenDURING INSPECTION OF THE MAIN LANDING GEAR BRAKES, DRIVE ROTOR CLIPS FOUND THE NR 3 AND NR 4 BRAKE ASSEMBLIES TO HAVE FOUR CLIPS EACH BROKEN OFF. REPLACED BOTH BRAKE ASSEMBLIES WITH OVERHAULED UNITS. THIS IS A KNOWN CONDITION AND TROUBLESHOOTING IS ON GOING.Jun 18, 2003 · N910DC · Gulstm GULFSTREAMGV · BrakeSDR 349811Block · separatedTUNGSTEN BLOCK (BALLAST WEIGHT) AT OUTBOARD END OF LT AILERON FOUND SEPARATED FROM MAIN COUNTER WEIGHT. BLOCK SLID FORWARD AGAINST WING REAR BEAM AND WAS RESTRICTING AILERON DOWNWARD MOVEMENT. PROBABLE CAUSE: LOOSE AND MISSING HARDWARE. ONE SCREW AND TWO NJun 2, 2003 · N50KC · Gulstm GULFSTREAMGV · AileronsSDR 3M25603Clamp · out of positionCLAMP ON RIGHT HAND MAIN GEAR SIDE BRACE ACTUATOR IS CONTACTING GEAR ACTUATION FLEX LINE. REPOSITIONED CLAMP TO CLEAR LINE.May 6, 2003 · N23M · Gulstm GULFSTREAMGV · Landing Gear ActuatorSDR 3M35603Clamp · out of positionCLAMP ON RIGHT HAND MAIN LANDING GEAR SIDE BRACE ACTUATOR IS CONTACTING ACTUATOR FLEX LINE. REPOSITION CLAMP TO CLEAR LINE.May 6, 2003 · N33M · Gulstm GULFSTREAMGV · Landing Gear ActuatorSDR E7J2003F00000Compressor Wheel · damagedWHILE PERFORMING AD 203-07-11, ENGINE FAN DISK ULTRASONIC INSPECTION, THREE FAN BLADE TRAILING EDGES WERE FOUND WITH UNACCEPTABLE DAMAGE. THE FAN DISK RING SHOWED GOUGING IN THE AREAS CORRESPONDING WITH THE DAMAGED BLADES. (REPORT NR: 625-01-03) (PTRS: NE0May 5, 2003 · N507QS · Gulstm GULFSTREAMGV · Turbine Engine Compressor SectionSDR 3M24031Rotor · crackedBRAKE ROTOR SPLINTERING AT KEYWAY CLIPS.Apr 11, 2003 · N23M · Gulstm GULFSTREAMGV · Landing Gear Brake SystemSDR 3M24032Rotor · chippedROTOR IS CHIPPED AT BRAKE KEYWAY CLIP.Apr 11, 2003 · N23M · Gulstm GULFSTREAMGV · Landing Gear Brake SystemSDR 3M24033Rotor · crackedROTOR IS SPLINTERING AT KEYWAY CLIPS.Apr 11, 2003 · N23M · Gulstm GULFSTREAMGV · Landing Gear Brake SystemSDR 3M2Contactor · failedCONTACTOR INTERMITTENLY FAILS TO CONNECT TO THE BUS. REPLACED CONTACTOR.Mar 18, 2003 · N33M · Gulstm GULFSTREAMGV · Electrical Power System WiringSDR 3M1Contactor · sticksCONTACTOR STICKS INTERMITTENLY. REPLACED CONTACTOR OPERATIONAL CHECKS NORMAL.Mar 11, 2003 · N33M · Gulstm GULFSTREAMGV · Electrical Power System WiringSDR 6370103Compressor Wheel · crackedDISCOVERED DURING SCHEDULED MAINTENANCE. RT ENGINE FAN DISK FOUND CRACKED WHILE PERFORMING SCHEDULED NON DISTRUCTIVE TESTING IAW AD AND MFG SB. FAN DISK PN BRR20791, SN CTDK 7185 ENGINE TYPE BR700-710A1-10, SN 11386. REMOVED LP FAN MODULE 31, PN M31-113, SNMar 11, 2003 · N509QS · Gulstm GULFSTREAMGV · Turbine Engine Compressor SectionSDR LD22003F00000Brake Assy · crackedCRACKS WERE FOUND IN THE NR ROTOR DRIVE CLIPS. A NEW BRAKE UNIT WAS INSTALLED. MFG ARE WORKING ON NEW DESIGNS TO CORRECT THESE PROBLEMS.Mar 6, 2003 · N23M · Gulstm GULFSTREAMGV · BrakeSDR LD22003F00001Brake Assy · damagedDURING POST FLIGHT INSPECTION, A BRAKE TEMPERATURE OF 980 WAS NOTED ON THE NR 4 BRAKE. THE WHEEL WAS REMOVED AND THE NR 1 ROTOR HAS SEVERAL DRIVE CLIPS COMING OFF. THE BRAKE WAS REPLACED WITH A NEW UNIT. THE NR 4 MAIN WHEEL WAS REMOVED AND SENT OUT FOR INSPMar 6, 2003 · N23M · Gulstm GULFSTREAMGV · Landing Gear Brake SystemSDR BZP2003F00001Contactor · arcedTERMINAL C2 OF CONTACTOR KPB101 WAS NOT TORQUED PROPERLY. THIS TERMINAL IS SUBJECTED TO HIGH ELECTRICAL LOADING AND AS SUCH EXPERIENCED ARCING DUE TO ITS BEING LOOSE. ARCING CAUSED CONTACTOR TERMINAL COVER, (PN MS272436), TO MELT NEAR TERMINAL C2. PLASTIC PFeb 15, 2003 · N949GP · Bombdr BD7001A10 · Electrical Power System WiringSDR 2003F00213Compressor Wheel · out of balanceDURING CLIMB, OUT OF KDTW, THE LEFT ENGINE AMBER 'VIBRATION EXCEEDANCE' CAS MESSAGE WAS RECEIVED. POWER ON THE LT ENGINE WAS REDUCED, IAW THE AFM, AND THE MESSAGE EXTINGUISHED. THERE FORE, THE TRIP CONTINUED TO DESTINATION AND AACI MX PROVIDER AT KDTW WAS COFeb 11, 2003 · N5102 · Gulstm GULFSTREAMGV · Turbine Engine Compressor Section
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