# Rolls-Royce DART-532-7R

- Type: Engine model (FAA registry)
- Registry code: 54100
- Manufacturer (registry): ROLLS-ROYC
- Model: DART 532-7R
- Engine type: Turbo-prop
- Power: 2,260 hp
- Data sheet: [TCDS E-297](https://openairdocs.org/tcds/E-297) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-dart-532-7r

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 2008-16-05](https://openairdocs.org/ad/2008-16-05): Intermediate pressure turbine (IPT) disk · Rolls-Royce Deutschland Dart 528-7E, Dart 528D-7E, Dart 529-7E and 29 more. Effective Sep 4, 2008
- [AD 2007-03-13](https://openairdocs.org/ad/2007-03-13): High pressure turbine (HPT) blade platforms and shrouds · Rolls-Royce Deutschland Dart 528-7E, Dart 528D-7E, Dart 529-7E and 27 more. Effective Mar 19, 2007
- [AD 2003-17-11](https://openairdocs.org/ad/2003-17-11): Sermetel coating (Omat 7/46) · Rolls-Royce Deutschland Dart 528-7E, Dart 529-7E, Dart 529-7H and 29 more. Effective Sep 30, 2003
- [AD 2001-19-06](https://openairdocs.org/ad/2001-19-06): High Pressure Turbine Discs · Rolls-Royce Deutschland Dart 525, Dart 525F, Dart 528-7E and 31 more. Effective Oct 15, 2001
- [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 99-04-09](https://openairdocs.org/ad/99-04-09): High Pressure Turbine Disk · Rolls-Royce Deutschland Dart 525, Dart 525F, Dart 526 and 35 more. Effective Feb 25, 1999
- [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 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 85-06-01](https://openairdocs.org/ad/85-06-01): Flame Tube Liners And Suspension Pins · Rolls-Royce Deutschland Dart 525, Dart 525F, Dart 526 and 29 more. Effective Apr 3, 1985
- [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 77-21-05](https://openairdocs.org/ad/77-21-05): High Pressure Turbine Discs · Rolls-Royce Deutschland Dart 527, Dart 528-7E, Dart 528D-7E and 28 more. Effective Nov 11, 1977
- [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 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 67-15-03](https://openairdocs.org/ad/67-15-03): Oil Filter · Rolls-Royce Deutschland Dart 525, Dart 525F, Dart 526 and 23 more. Effective May 14, 1967
- [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

Historical (superseded or no longer in force):

- [AD 2007-02-07](https://openairdocs.org/ad/2007-02-07) (historical): Intermediate pressure turbine (IPT) disk · Rolls-Royce Deutschland Dart 528-7E, Dart 528D-7E, Dart 529-7E and 29 more. Effective Feb 26, 2007

## 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.

## Service difficulty reports (25)

As reported by operators and repair stations, by the model named in the report.

- [SDR COEA0802703](https://openairdocs.org/sdr/COEA0802703), Mar 19, 2008: ALTERNATOR. FAILED. RETURN TO BLOCKS. FLT NR7276, DURING TAXI TO THE RUNWAY, THE LT ALTERNATOR FAILED. THE AC RETURNED TO THE RAMP (BLOCKS) WITHOUT ANY FURTHUR INCIDENT. LT ALTERNA
- [SDR COEA0801702](https://openairdocs.org/sdr/COEA0801702), Mar 14, 2008: GYRO. FAILED. RETURN TO BLOCKS. FLIGHT NR 7276 ITC TO AFW. WHILE PREPAIRING FOR DEPARTURE THE CREW DISCOVERED THE CAPT HEADING AND SITUATION INDICATOR (HSI) COMPASS CARD WAS 
- [SDR COE2005F00002](https://openairdocs.org/sdr/COE2005F00002), Oct 3, 2005: INVERTER. INOPERATIVE. DEPARTURE, ENROUTE, NR 1 INVERTER WENT OFF LINE AND WOULD NOT COME BACK ON. CREW REPORTED A STRONG BURNING ODOR BUT NO SMOKE. AIRCRAFT DIVERTED. THE NR 1 INVERT
- [SDR COE2005F00000](https://openairdocs.org/sdr/COE2005F00000), Jan 20, 2005: WIRE HARNESS. INOPERATIVE. NR 2 TGT FLUCUTATED BETWEEN 0 AND 600 DEGREES IN FLIGHT. AIRCRAFT RETURNED TO AIRPORT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND
- [SDR COE2004F00001](https://openairdocs.org/sdr/COE2004F00001), Nov 3, 2004: ALTERNATOR. FAILED. ON CLIMB OUT, RT ALTERNATOR FAIL LIGHT CAME ON. AIRCRAFT RETURNED TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACE
- [SDR COE2004F00000](https://openairdocs.org/sdr/COE2004F00000), Mar 4, 2004: CONTROL PANEL. FAILED. AFTER TAKEOFF, LEFT ENGINE GENERATOR WOULD NOT CARRY A LOAD. CREW TURNED BACK WHERE MAINTNANCE WAS AVAILABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMO
- [SDR MTNA20032](https://openairdocs.org/sdr/MTNA20032), Apr 2, 2003: PROPELLER. MALFUNCTIONED. IN FLIGHT FROM CRW TO LCK THE LEFT ENGINE AUTO-FEATHERED. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED UNEVENTFULLY AT LCK. THE CAUSE IS UNKNOWN AT THIS TIME.
- [SDR AU000155](https://openairdocs.org/sdr/AU000155), Mar 23, 2000: COMPRESSOR. FAILED. (AUS) LH ENGINE DRIVEN PNEUMATIC COMPRESSOR FAILED. OIL LINE FOUNDBROKEN AT BRAZED FITTING.
- [SDR 99ZZZX2119](https://openairdocs.org/sdr/99ZZZX2119), Mar 25, 1999: SKIN. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR SKIN STA 1050 - STA 1070, STR 29R.
- [SDR AU990148](https://openairdocs.org/sdr/AU990148), Feb 11, 1999: SEAL. FAILED. (AUS) NR 2 ENGINE AUXILIARY GEARBOX OUTPUT SHAFT SEAL LEAKING. ENGINE HAD SUFFERED A PREVIOUS AUXILIARY GEARBOX DRIVESHAFT FAILURE WHICH MAY HAVE CONTRIBUTED TO
- [SDR COEA9901701](https://openairdocs.org/sdr/COEA9901701), Jan 14, 1999: ENGINE. FAILED. EN ROUTE TO OAK FOM YVR FLT 7525, PILOTS REPORTED HAVING A LOW TORQUE INDICATION ON NR 1 ENGINE. MAINTENANCE WAS ADVISED UPON ARRIVAL IN OAK. WHEN THE MECHANIC 
- [SDR AU980886](https://openairdocs.org/sdr/AU980886), Jul 23, 1998: DRIVESHAFT. FAILED. (AUS) RIGHT ENGINE GEARBOX DRIVESHAFT FAILED AT THE FORWARD UNIVERSAL JOINT DAMAGING THE ENGINE `W' STRUT AND NR 1 AND NR 2 COMBUSTION CHAMBERS.
- [SDR 98ZZZM565](https://openairdocs.org/sdr/98ZZZM565), Jul 10, 1998: LINE. LOOSE. DURING CRUISE, LEFT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. (M)
- [SDR AU981017](https://openairdocs.org/sdr/AU981017), Jul 1, 1998: SWITCH. LEAKING. (AUS) NR 2 ENGINE PROPELLER CONTROL UNIT PRESSURE SWITCH LEAKING OIL.
- [SDR 98ZZZX2571](https://openairdocs.org/sdr/98ZZZX2571), Jun 21, 1998: COMBUSTION CAN. CRACKED. DURING A SCHEUDLED INSPECTION, THE NR 1 COMBUSTION CAN ASSY ON THE LEFT ENGINE WAS REJECTED DUE TO AN OUTER CASING BURN-THROUGH NEAR THE AFT END. UPON CAN REMOV
- [SDR AU971553](https://openairdocs.org/sdr/AU971553), Dec 10, 1997: TRANSCEIVER. FAILED. (AUS) RADAR TRANSMITTER/RECEIVER FAILED.
- [SDR COEA9701701](https://openairdocs.org/sdr/COEA9701701), Dec 1, 1997: ENGINE. FAILED. UPON START OF THE NR 2 ENGINE (S/N 14211), FLIGHT CREW EXPERIENCED MODERATE VIBRATION EMANATING FROM THE ENGINE. CREW SHUT DOWN ENGINE AFTER LOW IDLE WAS ATTAIN
- [SDR 97ZZZM1065](https://openairdocs.org/sdr/97ZZZM1065), Sep 10, 1997: TURBINE BLADE. BROKEN. THE FLIGHT CREW NOTED THAT THE NR 2 ENGINE WAS RUNNING ABOVE THE NORMAL EGT AT TAKEOFF POWER. VISUAL INSPECTION OF THE ENGINES TURBINE SECTION REVEALED IMPACT D
- [SDR COEA9702740](https://openairdocs.org/sdr/COEA9702740), Jul 17, 1997: OIL SEAL. WORN. AFTER DEPARTURE FROM LBB, CAPTAIN REPORTS RT ENGINE GEARBOX OIL PRESSURE LIGHT ILLUMINATED. PILOT FEATHERED ENGINE AND RETURNED TO LBB. MX DISPATCHED . UPON INS
- [SDR COEA9701740](https://openairdocs.org/sdr/COEA9701740), Jul 16, 1997: B NUT. LOOSE. AFTER DEPARTURE FROM LBB, PILOT REPORTED LOW PRESSURE LIGHT FOR RIGHT GEARBOX ILLUMINATED. THE CAPTAIN OBTAINED CLEARANCE AND ELECTED TO SHUT DOWN RIGHT ENGINE 
- [SDR 97ZZZX2093](https://openairdocs.org/sdr/97ZZZX2093), Apr 29, 1997: FUEL PUMP. SHAFT SHEARED. ON CLIMB-OUT OF LCK, THE LEFT ENGINE AUTOFEATHERED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LCK WITH NO FURTHER PROBLEMS. THE MECHANIC FOUND A SHEARED SH
- [SDR 97ZZZX2094](https://openairdocs.org/sdr/97ZZZX2094), Feb 6, 1997: ENGINE. DAMAGED. EWR/YMX - EN ROUTE, THE LEFT ENGINE STARTED TO AUTOFEATHER. THE LEFT ENGINE TEMP STARTED TO RISE, THE FLIGHT CREW THEN MANUALLY FEATHERED THE PROP. THE CREW DEC
- [SDR 96ZZZX5461](https://openairdocs.org/sdr/96ZZZX5461), Apr 17, 1996: DRIVE SHAFT. SHEARED. GRR - ON DEPARTING REACHING 5,000 FEET ALTITUDE, THE RIGHT GEARBOX OIL PRESSURE LIGHT, ALTERNATOR LIGHT, GENERATOR FAIL LIGHT CAME ON AT THE SAME TIME. THE FLIG
- [SDR 96ZZZX458](https://openairdocs.org/sdr/96ZZZX458), Jan 12, 1996: GEARBOX. FAILED. RIC - ON CLIMB-OUT, THE LEFT ENGINE INDICATED A POWER LOSS (RPM DROPPED TO 13,800 AT MAX). THE CREW DECLARED AN EMERGENCY AND RETURNED TO RIC. DURING DESCENT, L
- [SDR 96ZZZX185](https://openairdocs.org/sdr/96ZZZX185), Oct 9, 1995: BEARING. FAILED. CREW NOTED REDUCED TORQUE INDICATED ON TAKEOFF. CLIMB TORQUE INDICATED NORMAL. PCU AND FCU WERE CHANGED WITH NO EFFECT. WET TAKEOFF POWER NORMAL. ENGINE WAS REM

## STCs that may be installed (OpenAirDocs) (1)

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 SE12WE](https://openairdocs.org/stc/SE12WE): Flexible hose fuel manifold assembly. Crane Resistoflex. Lists Dart 532 Series

## PMA parts (OpenAirDocs) (14)

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.

- [AS112](https://drs.faa.gov/browse/excelExternalWindow/C9558B7A8E61E26D86257AD7006CF06B.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112 · Dec 9, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/8DADE792DAB865F186257AD7006CF070.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118 · Dec 9, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/617664DAA8C4485F86257AD7006CF084.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118, RTV 118 · Dec 9, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/4AB87B0DC36E248F86257AD7006CF081.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116, RTV 116 · Dec 9, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/2B43C6B50D22E12F86257AD7006CF06C.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116 · Dec 9, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/17A2F94467E39E9F86257AD7006CF07F.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112, RTV112 · Dec 9, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/8F5FF0B2D52B579E86257AAD006A7831.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118, RTV 118 · Oct 23, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/8E518499870C01D686257AAD006A77CD.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112 · Oct 23, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/699A146AEFCCFD7786257AAD006A77D0.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116 · Oct 23, 2012
- [AS112](https://drs.faa.gov/browse/excelExternalWindow/5FFDD126D3F3D3E886257AAD006A780B.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 112, RTV 112 · Oct 23, 2012
- [AS118](https://drs.faa.gov/browse/excelExternalWindow/5EBDAB2435C52CB486257AAD006A77E9.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 118 · Oct 23, 2012
- [AS116](https://drs.faa.gov/browse/excelExternalWindow/06F9202F2290B40986257AAD006A7819.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces GE 116, RTV 116 · Oct 23, 2012
- [NSL870 B2](https://drs.faa.gov/browse/excelExternalWindow/14C5EEADE7A73689862578650062C79A.0001): Sealant. Aerospace Sealants LLC · PMA PQ3886CE · Replaces PEC-DeSoto Sealant Pro Seal 870 B2 · Mar 22, 2011
- [FHE19-6L](https://drs.faa.gov/browse/excelExternalWindow/C68D9F6831BC14378525703F004A6178.0001): Igniter. Champion Aerospace LLC · Replaces Rolls Royce CR104-2 · Dec 6, 1988

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