Engine model · Turbo-prop · 2,103 hp · registry code 54081

Manufacturer (registry)
ROLLS-ROYC
Model
DART 529-7E
Registry code
54081
Installed in
0 registered aircraft
Type
Turbo-prop
Power
2,103 hp
Data sheet
TCDSE-297
Holder
Rolls-Royce Deutschland Ltd & Co KG

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

On this page

Airworthiness directives that may apply · 22

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

1963In forceSuperseded2026
ADs by the year they took effect: 23 ADs
19631
19671
19701
19721
19771
19801
19834
19851
19861
19881
19931
19981
19991
20002
20011
20031
20072
20081
See all 23 ADs
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 ('54081'))
  ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number 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.

Registered aircraft · 0

No aircraft currently registered with this engine model

NTSB investigations

No NTSB investigations matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older cases aren’t counted.

FAA incident reports

No reports matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older reports aren’t counted.

Service difficulty reports · 14

SDR CA040519003Tire · separated(CAN) UPON LANDING, THE LT IB TIRE RE-TREAD SEPARATED FROM THE TIRE.May 4, 2004 · Frchld F27F · TireSDR CA010411004Skin · cracked(CAN) CRACK FOUND AT TOP REAR CORNER OF FRONT CARGO DOOR FRAME (FUSELAGE). THE PROBLEM IS ONE BAD FLUSH RIVET CRACK FROM RIVET TO SKIN EDGE. CRACK FOUND ON DAILY INSPECTION.REPAIR DONE AT STATION 181.102 AND 14 INCH ABOVE W.L. 0 LINE.Mar 12, 2001 · Frchld F27F · Fuselage Structure (General)SDR CA001102005Skin · cracked(CAN) A 1.5 INCH CRACK WAS FOUND AT FS 33.662 AND WL +50 APPROX. THE CRACK WAS FOUND BY X-RAY AND CONFRIMED BY EDDY CURRENT DURING A SPECIAL INSPECTION.Oct 10, 2000 · Frchld F27F · Fuselage Main, Plate/SkinSDR CA000110096Compressor · separated(CAN) STAGE 2 CYLINDER FOUND SEPARATED FROM PNEUMATIC COMPRESSOR CAUSING CASING CAUSING GEAR BOX OIL LOSS.Dec 17, 1999 · Frchld F27F · Pneumatic SystemSDR CA991231004Angle · cracked(CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RIB AT W.L. 201.575Dec 1, 1999 · Frchld F27F · Vertical StabilizerSDR CA990907080Transmitter · malfunctioned(CAN) OIL PRESSURE FLUCTUATIONS INDICATING. TRANSMITTER REPLACED.Aug 22, 1999 · Frchld F27F · Engine Oil PressureSDR CA990707063Cylinder · failed(CAN) DURING FLIGHT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING. CREW SECURED ENGINE. INVESTIGATION REVEALED THAT THE CYLINDER CAP ON THE AIR COMPRESSOR ON NR 2 ACCESSORY GEARBOX WAS LEAKING. PUMP REPLACED.Jun 3, 1999 · Frchld F27F · Accessory GearboxesSDR CA990119005Transformer · failed(CAN) RESISTANCE ON WINDSHIELD HAD INCREASED. NEW WINDOW ORDERED. NEXT APPLICATION OF WINDSHIELD HEAT, THE TRANSFORMER OVERHEATED AND FILLED THE COCKPIT WITH SMOKE. REPLACED.Jan 19, 1999 · Frchld F27F · Windshield/Door Rain/Ice RemovalSDR CA981230043Wheel · ruptured(CAN) AFTER LANDING AND DURING TAXI, THE LEFT OUTBOARD WHEEL HALF SEPARATED ALONG THE CIRCUMFERENCE. THE WHEEL HAD BEEN INSPECTED AT THE LAST TIRE CHANGE AND WAS OK. NO DAMAGE TO LANDING GEAR AS A RESULT OF SEPARATION. INVESTIGATION AFTER THE INCIDENT REVEADec 9, 1998 · Frchld F27F · Wheel/Ski/FloatSDR CA980317052Fuel Control · damaged(CAN) FUEL CONTROL UNIT WAS LEAKING. INLET SIDE FROM FUEL PUMP WAS ENLARGED CAUSING O RING ON TUBE TO ALLOW FUEL TO ESCAPE. FCU WAS REPLACED WITH ONE OFH IGHER MOD STATUS. ROLLS ROYCE SUGGESTED THAT THE FCU WAS MOVING ON ITS THREE MOUNTS. NEW UNIT HAD BUSHINGSJan 15, 1998 · Frchld F27F · Fuel Control/Reciprocating EnginesSDR CA970530010Actuator · failed(CAN) A JUST OVERHAULED MAIN LANDING GEAR ACTUATOR HAD BEEN INSTALLED. DURING GROUND RETRACTION TEST, WHEN WHEELS WERE LOWERED, THE ACTUATOR DID NOT HAVE ANY DAMPENING, WHICH RESULTED IN A NOT-CONTROLLED DESCENT OF GEAR AND THE BREAKAGE OF THE WHEEL DOWNLOCK SMay 15, 1997 · Frchld F27F · Landing Gear ActuatorSDR COEA9622201Engine · failedOAK/YVR - WHILE EN ROUTE WITH MODERATE TURBULENCE AND MODERATE ICING CONDITIONS, LT ENGINE AUTOFEATHERED IN CRUISE. CREW INITIATED AIRSTART PROCEDURES. ENGINE WAS BACK ON-LINE WITH NO PROBLEMS. ENGINE PERFORMED THROUGH THE REMAINDER OF THE FLIGHT WITH NO REOct 18, 1996 · N222DG · Frchld F27F · Engine (Turbine/Turboprop)SDR CA960103534Pipe Fuel Servo · blistered(CAN)DURING FIFTY HOUR ROUTINE (SERVICE BULLETIN) INSPECTION OF THE SERVO FUEL PIPE, WHICH RUNS FROM THE HIGH PRESSURE FUEL PUMP TO THE FUEL CONTROL UNIT, WAS FOUND BLISTERED. THE PART WAS REMOVED AND A NEW PIPE P/N 1021106 WAS INSTALLED.Nov 29, 1995 · Frchld F27F · Engine Fuel DistributionSDR COEA9572901Vent Line · crackedDURING CRUISE OF FLIGHT 729, NR 2 GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEARBOX AND FOUND LEAK AT VENT LINE. REPAIRED LINE IAW AC 43.13 STANDARD PRACTICES. SERVICED GEARBOX, LEAOct 28, 1995 · N729FE · Fokker F27MK600 · Turbine Engine Accessory Drive
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 = 'DART5297E'
  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.

STCs that may be installed · 5

Approved for this engine model: the STC’s model list names it on its data sheet, or a series that includes it. The registry doesn’t record which STCs an aircraft has.

Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
  FROM (
    SELECT stc_number, min(matched_model) AS matched_model
    FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet'
    WHERE engine_model_code IN ('54081')
    GROUP BY stc_number
  ) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
  ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number"

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.

PMA parts · 17

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 17 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 ('E-297')
    AND len(list_intersect(tcds_models, ['Dart 529-7E'])) > 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.