Engine model · Turbo-fan · registry code 54005

Manufacturer (registry)
ROLLS DEUT
Model
BR700-710C411
Registry code
54005
Type
Turbo-fan
Power
15,385 lb thrust
Data sheet
TCDSE00057EN
Holder
Rolls-Royce Deutschland Ltd & Co KG

Model codes come from the FAA registry’s reference file.

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Airworthiness directives that may apply · 8

ADs whose products match this engine model. Each AD’s applicability may narrow it by serial number, part number or configuration.

2011In forceSuperseded2026
ADs by the year they took effect: 10 ADs
20112
20132
20161
20181
20211
20232
20251
Superseded and historical ADs · 2
Query with SQL
duckdb -csv -c "SELECT d.ad_number, d.status, d.subject, d.effective_date
  FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
  WHERE d.ad_id IN (SELECT ad_id FROM 'https://openairdocs.org/data/latest/faa_engine_model_directive.parquet' WHERE engine_model_code IN ('54005'))
  ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESC"

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Registered aircraft · 292

See all 292 registered aircraft
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duckdb -csv -c "SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
  FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
  WHERE engine_model_code IN ('54005')
  ORDER BY n_number"

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NTSB investigations · 1

Aircraft matched to this engine model through the registry, by N-number and event date, checked against the reported serial number, make and model.

Query with SQL
duckdb -csv -c "SELECT c.\"ntsbNumber\", c.\"eventDate\", c.\"eventType\", c.\"eventCity\", c.\"eventStateOrRegion\", a.n_number, a.\"aircraftMake\", a.\"aircraftModel\", c.\"highestInjuryLevel\", c.\"totalFatal\", c.\"completionStatus\", c.report_url
  FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a JOIN 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c ON c.\"mKey\" = a.case_mkey
  WHERE a.engine_model_code IN ('54005')
  ORDER BY c.\"eventDate\" DESC, c.\"ntsbNumber\" DESC"

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FAA incident reports · 6

Matched to this engine model through the registry, by N-number and event date, checked against the reported make and model.

Incident 20251008018499IGulfstream Aerospace GV-SP (G550) · Opa Locka, FLUpon rollout after touchdown a stong microburst occurred with strong windshifts in direction dropping visability to none with visability returning after short distance down the runwayOct 8, 2025 · N768JJ · Minor damageIncident 20250321002769IGulfstream Aerospace GV-SP (G550) · Livermore, CAWhile taxiing from the runway to the hangar at lvk, the taxi included reversing direction by 180 degrees to a parallel taxiway. When on the connector between the taxiways, the aircraft was kept left of center to avoid other aircraft ahead on the ramp. In…Mar 21, 2025 · N333DS · Minor damageIncident 20240613005759IGulfstream Aerospace GV-SP (G550) · St. Petersberg, FLAircraft struck a bird on leading edge of the left wing while departing runway 36 and continued to destination landing without incident.Jun 13, 2024 · N126HR · Minor damageIncident 20181226021939IGulfstream Aerospace GV-SP (G550) · Saint Augustine, FLSt Augustine, FL (sgj): N550DX, G550, reported a bird strike on landing for runway 31. Aircraft taxied to the ramp. Damage: not reported. 12/26/2018 1415Z Occurred during gov't furlough.Dec 26, 2018 · N550DX · No damageIncident 20111010024149IGulfstream Aerospace GV-SP (G550) · Carlsbad, CA1.) Aircraft N273A was ramped on up-hill grade at a takeoff weight of 65,000 pds. 2.) The aircraft was positioned with exhaust tips pointed to the east with a 12 knot wind to the east, and the exhaust was essentially directed down a slope towards ga aircraft.…Oct 10, 2011 · N273A · Substantial damageIncident 20110214002129IGulfstream GV-SP (G550 · Appleton, WINearing the completion of a production test flight, the aircraft was established inside the final approach fix for runway 30. With flaps set to 20 degrees, the crew extended the landing gear. Shortly thereafter, the "left hydraulic quantity low" annunciator…Feb 14, 2011 · N535GA · Minor damage
Query with SQL
duckdb -csv -c "SELECT report_number, event_date, event_type, city, state, aircraft_make, aircraft_model, aircraft_damage, fatal_injuries, n_number
  FROM 'https://openairdocs.org/data/latest/faa_incident_report.parquet'
  WHERE engine_model_code IN ('54005')
  ORDER BY event_date DESC, report_number DESC"

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Service difficulty reports · 14

SDR 2023F00051Hydraulic Line · leakingTHE CREW RECEIVED A HYDRAULIC CAS MESSAGE WHILE IN FLIGHT. AIRCRAFT DIVERTED TO THE NEAREST AIRPORT. INSPECTION BY MAINTENANCE REVEALED A HYDRAULIC LINE.TO HAVE SEPARATED AT PERMASWAGED AREA ON T-FITTING ABOVE FWD RH SIDE OF MLG TORQUE BOX.Feb 10, 2023 · N588TN · Gulstm GVSPG550 · Hydraulic System, MainSDR 2023F00052Hydraulic Line · leakingTHE CREW RECEIVED A HYDRAULIC CAS MESSAGE WHILE IN FLIGHT. AIRCRAFT DIVERTED TO THE NEAREST AIRPORT. INSPECTION BY MAINTENANCE REVEALED A HYDRAULIC LINE TO HAVE SEPARATED AT PERMASWAGED AREA ON T-FITTING ABOVE FWD RH SIDE OF MLG TORQUE BOX.Dec 10, 2022 · N588TN · Gulstm GVSPG550 · Hydraulic System, MainSDR 2023F00054Hydraulic Line · leakingCREW RECEIVED A HYDRAULIC CAS MESSAGE WHILE IN CRUISE. AIRCRAFT DIVERTED TI NEAREST AIRPORT. INSPECTION BY MAINTENANCE PERSONNEL REVEALED A HYDRAULIC LINE TO HAVE SEPARATED AT A PERASWAGED AREA FROM T-FITTING ABOVE FWD RH SIDE OF MLG TORQUE BOX.Dec 10, 2022 · N588TN · Gulstm GVSPG550 · Hydraulic System, MainSDR 2023FA0000084Hydraulic Line · leakingCREW RECEIVED A HYRAULIC CAS MESSAGE WHILE IN CURISE. AIRCRAFT DIVERTED TO NEAREST AIRPORT. INSPECTION BY MAINTENANCE PESONNEL REVEALED A HYDRAULIC LINE TO HAEVE AT A PERASWAGED T-FITTING LOCATED ABOVE FWD RH SIDE OF MLG TORQUE BOX, RT. WING.Dec 10, 2022 · N588TN · Gulstm GVSPG550 · Hydraulic System, MainSDR 2022F00402Landing Gear · failedLANDING GEAR FAILED TO RETRACT AFTER TAKE OFF.Sep 29, 2022 · N1759C · Gulstm GVSP · Landing Gear SystemSDR W6JA20210216043Engine · unknownKJAX-AT 1531Z, 16 FEB EXECUTED A REJECTED TAKEOFF AT JACKSONVILLE INTL AIRPORT. THE LEG WAS KJAX - KHND . START UP AND TAXI WERE NORMAL ALTHOUGH INITIALLY, BOTH ENGINES WERE IN ALT CTL (AMBER) ON THE EICAS AT PRE-START AND APU START. CLEARED ALL MSGS VIA THFeb 16, 2021 · N97FT · Gulstm GVSPG550 · Engine (Turbine/Turboprop)SDR 3SRA20200722001Terminal · failed2 MINUTES AFTER DEPARTURE, CREW WAS LEVEL AT 3,000 FEET, 250KTS , HEADING 150. DURING CLIMB, THE CREW HEARD A HIGH PITCH ELECTRICAL SQUEAL FOLLOWED IMMEDIATELY BY A POP, AND A PUFF OF SMOKE ABOUT THE SIZE OF A SOFTBALL, FROM WHERE THE CO-PILOT'S WINDSHIELD MEJul 17, 2020 · Gulstm GVSP · Ice/Rain Protection System WiringSDR 2PSA20190217001Brake Assy · cracked# 1 LEFT OUTBOARD BRAKE OUTBOARD DISK CRACK IN NUMEROUS PLACES.FOUND WHILE PERFORMING ITEM # 21.19 CMP 321003.P/N 1159SCL504-5 S/N 5231EP.INSTALLED NEW BRAKE ASSEMBLY P/N 1159SCL504-5, S/N 5050LA IAW CMP 324105.Feb 17, 2019 · N671LE · Gulstm GVSP · Landing Gear Brake SystemSDR 2015FA0000290Hydromech Unit · shearedAMBER CAS MESSAGE FOR LT HYDRAULIC SYSTEM FAIL, DURING FLIGHT. THERE WAS A LOSS OF PRESSURE BUT NOT QUANITY. THE AUTOMATIC BACKUP PTU HYDRAULIC SYSTEM CAME ON AS DESIGNED. THERE WERE NO ADVERSE AFFECTS TO THE AIRCAFT WITH THE LOSS OF THE LEFT SYSTEM AS THE BACJun 25, 2015 · N585DW · Gulstm GVSPG550 · Hydraulic System, MainSDR PB8R201408280001Strut · crackedDURING ROUTINE EDDY CURRENT INSPECTION OF ENGINE STRUT, FOUND A CRACK IN THE ATTACH LUG.Aug 27, 2014 · N529Q · Gulstm GVSPG550 · Engine Mount SectionSDR 2012FA0000514Plunger · meltedCREW REPORTED THAT THE FORWARD EMERGENCY EXIT WINDOW WAS ICING UP IN FLIGHT. TECH FOUND THAT THE SPRING HOLDING THE PLUNGER FOR THE CABIN WINDOW HEAT HAD MELTED THE BACK PLATE OF THE PLUNGER ASSY AND THAT THE PLUNGER AND CONNECTOR ASSY HAD BOTH BEEN ARCING. Jul 13, 2012 · N4PG · Gulstm GVSPG550 · Emergency ExitsSDR DXTA2010121104362Heater · smokeELECTRICAL SMOKE IN FWD LAV AFTER LANDING IN CHOCKS. SMOKE DISSIPATED AFTER 2 MIN COULD NOT FIND SOURCE. ISOLATED SOURCE OF SMOKE AND ODOR TO THE FWD LAV WATER HEATER. REMOVED FAULTY WATER HEATER . INSTALLED NEW WATER HEATER, OPS CHECKED GOOD. LEAK CHECKEDDec 10, 2010 · N531QS · Gulstm GVSPG550 · Wash Water SystemSDR DXTA2010120304346Unknown · odorCREW REPORTED SMOKE/BURN ODOR IN BAGGAGE COMPARTMENT AFTER FINDING THE RT CREW CIRCUIT BREAKER POPPED. INSPECTED 60HZ CB PANEL. RAN ALL CABIN SYS, AND DREW POWER FROM GALLEY AND CREW REST 60HZ OUTLETS FOR EXTENDED PERIODS OF TIME WITH NO DISCRPANCIES FOUND, Dec 1, 2010 · N546QS · Gulstm GVSPG550 · Air Distribution SystemSDR 2009FA0001027Tube · reversedDURING THE DISASSEMBLY FOR ACCESS TO ACCOMPLISH A SB, AN INCORRECT INSTALLATION OF ONE OF THE LPC INTERNAL GEARBOX AIR DISTRIBUTION TUBES WAS DISCOVERED. THE SPECIFIC AIR TUBE IS PN FW34112 AND WAS INSTALLED IN THE UPPER LT LOCATION. THE AIR TUBE WAS INSTALLEDec 8, 2009 · Turbine Engine Compressor Section
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 engine_model_key = 'BR700710C411'
  ORDER BY difficulty_date DESC"

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PMA parts · 99

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

See all 99 PMA parts
Query with SQL
duckdb -csv -c "SELECT drs_guid, part_number, part_name, holder, pma_number, replaces_part, supplement_date, tcds_models
  FROM 'https://openairdocs.org/data/latest/faa_type_certificate_pma.parquet'
  WHERE tcds_number IN ('E00057EN')
    AND len(list_intersect(tcds_models, ['BR700-710C4-11'])) > 0
  ORDER BY supplement_date DESC, drs_guid 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.