# Rolls-Royce DART-511

- Type: Engine model (FAA registry)
- Registry code: 54074
- Manufacturer (registry): ROLLS-ROYC
- Model: DART 511
- Engine type: Turbo-prop
- Power: 1,677 hp
- Data sheet: [TCDS E-283](https://openairdocs.org/tcds/E-283) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-dart-511

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

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2000-12-18](https://openairdocs.org/ad/2000-12-18): Reduction Gearbox · Rolls-Royce Deutschland Dart 511, Dart 511-7E, Dart 514-7 and 10 more. Effective Jul 31, 2000
- [AD 99-27-04](https://openairdocs.org/ad/99-27-04): Low Torque Switches · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 38 more. Effective Feb 28, 2000
- [AD 98-04-13](https://openairdocs.org/ad/98-04-13): Propeller Low Torque Switch · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 43 more. Effective Mar 24, 1998
- [AD 93-15-09](https://openairdocs.org/ad/93-15-09): Servo Fuel Pipe · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 40 more. Effective Sep 7, 1993
- [AD 88-21-06](https://openairdocs.org/ad/88-21-06): High Pressure Impellers · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 35 more. Effective Nov 6, 1988
- [AD 86-20-10](https://openairdocs.org/ad/86-20-10): High Pressure Turbine Disks · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 3 more. Effective Nov 4, 1986
- [AD 85-03-03 R1](https://openairdocs.org/ad/85-03-03-R1): Low Pressure Impeller · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 38 more. Effective Jan 6, 1986
- [AD 82-09-02 R1](https://openairdocs.org/ad/82-09-02-R1): Engine Fuel Manifold Assembly Connection Flexible Hose · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 33 more. Effective May 12, 1983
- [AD 78-24-01 R1](https://openairdocs.org/ad/78-24-01-R1): Control Box Mounting Bolt Failure · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 34 more. Effective May 12, 1983
- [AD 77-20-05 R1](https://openairdocs.org/ad/77-20-05-R1): Fuel Burner Feed And Manifold Pipes · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 27 more. Effective May 12, 1983
- [AD 72-18-02 R1](https://openairdocs.org/ad/72-18-02-R1): Fuel Burner Shroud Nuts · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 31 more. Effective May 12, 1983
- [AD 80-23-01](https://openairdocs.org/ad/80-23-01): Low Pressure Impellers · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 38 more. Effective Oct 30, 1980
- [AD 72-16-05](https://openairdocs.org/ad/72-16-05): Impellers · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 35 more. Effective Dec 4, 1972
- [AD 71-06-05](https://openairdocs.org/ad/71-06-05): Turbine Disc Retaining Bolt · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 3 more. Effective Apr 12, 1971
- [AD 70-15-13](https://openairdocs.org/ad/70-15-13): Fuel Washed Burners · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 28 more. Effective Aug 20, 1970
- [AD 63-07-04](https://openairdocs.org/ad/63-07-04): Air Casing · Rolls-Royce Deutschland Dart 506, Dart 510, Dart 511 and 43 more. Effective May 2, 1963

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## STCs that may be installed (OpenAirDocs) (5)

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

- [STC SE905EA](https://openairdocs.org/stc/SE905EA): Repair and modification of compresor outlet and interstage cases. Airwork Corporation
- [STC SE13WE](https://openairdocs.org/stc/SE13WE): Flexible hose fuel manifold assembly. Resistoflex Corporation
- [STC SE203SO](https://openairdocs.org/stc/SE203SO): Variations in Rolls-Royce modification 636. Piedmont Aviation Inc
- [STC SE20WE](https://openairdocs.org/stc/SE20WE): Flexible hose assemblies. Resistoflex Corporation
- [STC SE748EA](https://openairdocs.org/stc/SE748EA): Installation of GLA ignition exciter. General Laboratory Association Inc

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