# TCDS E-297: Rolls-Royce Deutschland Ltd & Co KG

- Type: Type certificate data sheet
- Status: Current
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Revision: 27
- Revised: March 23, 2007
- Product: Engine
- Certification basis: Part 13, CAR 10
- Registered aircraft: 5, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/00/e9/00e9fdb32a77324aaf5aa0818e4ca4a6d25e1dee15a8bccb97ebe7f2c4a002e0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ACE13266FD058359862572A50074E1B8.0001
- Page: https://openairdocs.org/tcds/E-297

## Models (31)

As the data sheet lists them.

- Dart 532-7R
- Dart 529D-8H
- Dart 529-8X
- Dart 535-7R
- Dart 552-2
- Dart 529-7H
- Dart 531
- Dart 529-8H
- Dart 551-7
- Dart 529D-8Z
- Dart 529-8E
- Dart 528-7E
- Dart 529D-8Y
- Dart 532-7N
- Dart 535-2
- Dart 532-7
- Dart 532-7L
- Dart 529-7E
- Dart 528D-7E
- Dart 551-7R
- Dart 552-7R
- Dart 529D-7E
- Dart 532-7P
- Dart 529-8Z
- Dart 529D-7H
- Dart 532-2L
- Dart 529D-8E
- Dart 552-7
- Dart 529D-8X
- Dart 525
- Dart 529-8Y

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No 1 2 3 4 5 6 7 8 9 
Revision No 27 26 25 27 25 26 26 26 27 
 
LEGEND:   "- -"  INDICATES "SAME AS PRECEDING MODEL" 
                    "---"  INDICATES "NOT APPLICABLE" 
NOTE:  SIGNIFICANT CHANGES ARE BLACK-LINED IN THE 
LEFT MARGIN. 
 
 
 
DEPARTMENT OF TRANSPORTATION 
 
FEDERAL AVIATION ADMINISTRAITON 
 
TYPE CERTIFICATE DATA SHEET 
 
E 297 
 
 
 
TCDS  E 297 
REVISION:  27 
DATE:  March 23, 2007 
Rolls-Royce Deutschland Ltd & Co KG 
 
Model:  Dart 
525, 528-7E, 528D-7E, 529-7E, 529D-7E, 529-7H 
529D-7H, 529-8E, 529D-8E, 529-8H, 529D-8H, 529-8X, 
529D-8X, 529-8Y, 529D-8Y, 529-8Z, 529D-8Z, 531 
532-7, 532-2L, 532-7L, 532-7N, 532-7P, 532-7R, 535-2 
535-7R, 551-7, 551-7R, 552-2, 552-7, 552-7R 
 
TYPE CERTIFICATE DATA SHEET NO. E 297 
 
Engines of models described herein conforming with this data sheet (which is part of Type Certificate No. E 297) and other approved 
data on file with the Federal Aviation Administration meet the minimum standards for use in certificated aircraft in accordance with 
pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated, and 
maintained as prescribed by the approved manufacturer's manuals and other approved instructions. 
 
Type Certificate Holder: Rolls-R oyce Deutschland  Ltd & Co KG 
 Postfach 1536 
 D-15827 Dahlewitz 
 Germany (formerly Rolls-Roy ce, Ltd., Derby, England) 
 
 
Model:   Dart 525  528-7E, 
528D-7E, 531 
529-7E, 529D-7E, 529-7H, 529D-
7H, 529-8E, 529D-8E 
529-8H, 529D-8H, 529-8X, 
529D-8X, 529-8Y, 529D-8Y, 
529-8Z, 529D-8Z 
Type:   Turboprop 2-stage centrifugal 
compressor; 3-stage turbine; 
7 combustion chambers; 
0.093 to 1 reduction gearing 
- - - - 
Rating    
Max. Continuous at sea level, 
equivalent shaft hp., shaft 
hp., jet thrust (lb.) rpm 
1755-1585-424-14500 2027-1835-479-15000 2103-1910-482-15000 
2152-1955-493-15000 
(Mod 1860) 
Takeoff (5 min.) at sea level,  
equivalent shaft hp., shaft 
hp., jet thrust (lb.), rpm 
1920-1730-474-15000 2027-1835-479-15000 2103-1910-482-15000 
2152-1955-493-15000 
(Mod 1860)

TCDS  E 297   2
 
Model:  Dart (Continued) 525  528-7E, 
528D-7E, 531 
529-7E, 529D-7E, 529-7H, 529D-7H, 529-
8E, 529D-8E 
529-8H, 529D-8H, 529-8X, 
529D-8X, 529-8Y, 529D-8Y, 
529-8Z, 529D-8Z 
Takeoff (5 min.) at sea level, 
with w/m injection:  
equivalent shaft hp. shaft hp., 
jet thrust (lb.) rpm 
(529-8K, 529D-8K, 529-8Y, 
529D-8Y, 529-8Z, 529D-8Z) 
(532-7, 532-7N, 532-7P) 
(532-2L, 532-7L, 535-2) 
(532-7R, 535-7R) 
1955-1765-474-15000 2062-1870-479-15000 2143-1950-482-15000 
(For Models above except 529-8X, 529D-
8X, 529-8Y, 529D-8Y, 529-8Z, 529D-8Z)  
 
*2183-1990-482-15000 (See NOTE 13) 
*2196-1990-514-15000 (See NOTE 13) 
*2250-2040-524-15000 (See NOTE 13) 
*2293-2080-532-15000 (See NOTE 13) 
2297-2085-529-15000 (535-7R Mod 1860) 
(*Applies only to models listed at left side 
of page). 
Propeller Shaft Type SBAC No. 4 - - - - 
Fuel Control Lucas CCU 39/30AM Lucas CCU 36/27 AS 
for 531 
Lucas CCU 39/38 AY 
for 528 series 
 
Lucas CCU 69/55 AY for 529-8 series 
Lucas CCU 39/38 AY for 529-7 series 
Water Methanol Control 
Unit 
RK 39831  
RK 40195 for 528 
series;  
RK 39831 for 531. 
RK 40196 for 529-8 series;  
RK 40195 for 529-7 series. 
Fuel See NOTE 6 - - - - 
Oil Types See relevant Rolls-
Royce Operating 
Instructions Manual 
(NOTE 14) 
- - - - 
Oil Capacity 4 U.S. gal. integral tank - - - - 
Principal Dimensions    
Length overall (in.) 97.6 - - - - 
Diameter (in.) 37.9 - - - - 
C.G. Location    
Aft of mounting feet (in.) 2.4 - - - - 
Weight (dry), (lb.)    
Includes all controls, 
exhaust unit, igniters, 
thermocouples, oil tank 
and fuel pump 
1260 1270 for 528 series 
1270 for 531 
1260 
1273 (Mod 1860) 
Ignition System Alternatives   
High energy type with 
transformers 
LUCAS NB34, NB38, 
NB2503, NB5707, 
NB5706, NB5714. 
- - - - 
HE units LUCAS C10/TS, 
C63/TS, C65/TS, 
C67/TS, C69/TS 
- - - - 
HE igniters SMITHS LR 104series 
SMITHS KR 104 
series 
Champion CR 104 
series (Champion FHE-
19-6H)  
AC Type YA20 1 
through 12 
- - 
 
- - 
 
- - 
- - 
 
- - 
- - 
 
- - 
 
- - 
- - 
 
- -

TCDS  E 297   3
 
Model:   Dart (Cont'd) 532-2L, 532-7, 532-7L 
532-7N, 532-7P, 532-7R 
535-2, 535-7R 
551-7, 551-7R 552-2, 552-7, 552-7R 
Type:   Turboprop 2-stage centrifugal 
compressor; 3-stage turbine; 7 
combustion chambers; 0.093 
to 1 reduction gearing 
- - - - 
Rating  
Max. Continuous at sea level, 
equivalent shaft hp., shaft hp., 
jet thrust (lb.) rpm 
2075-1880-488-15000 (for 
models above except 535-2 & 
535-7R) 
2225-2030-487-15000 (for 
models 535-2 & 535-7R only) 
2346-2164-455-15000 2370-2167-508-15000 
Takeoff (5 min.) at sea level 
equivalent shaft hp., shaft hp., 
jet thrust (lb.) rpm 
2260-2060-500-15000 
(535-7R Mod 1860) 
2027-1835-479-15000 
2346-2164-455-15000 2370-2167-508-15000 
Takeoff (5 min.) at sea level, 
with w/m injection: equivalent 
shaft hp. Shaft hp, jet thrust 
(lb.) rpm 
- - 2417-2225-479-15000 
(For Model 551-7) 
2319-2136-457-15000 
(For Model 551-7R) 
2390-2185-512-15000 
2433-2225-519-15000 
2343-2140-508-15000 
Propeller Shaft Type SBAC No. 4 - - SBAC No. 4 
Fuel Control Lucas CCU 82/67AS or 
36/27AS 
Lucas CCU509-110-CA Mk552-2  Lucas CCU520-
/113CB or CCU519/112CB 
Mk552-7, -7R Lucas 
CCU509/110CA 
or CCU504/108CA 
Water Methanol Control 
Unit 
RK 40195 for 532-7, 537-7L, 
532-7R, 532-7P, 535-7R; RK 
42153 for 532-7N; RK 39831 
for 532-2L and 535-2. 
RK 44317A Mk552-2  Rolls-Royce 
RK48264A 
Mk552-7, -7R Rolls-Royce 
RK30403A 
Fuel See NOTE 6 - - - - 
Oil Types See relevant Rolls-Royce 
Operating Instructions Manual 
(NOTE 14) 
- - - - 
Oil Capacity 4 U.S. gal. integral tank - - - - 
Principal Dimensions    
Length overall (in.) 97.6 - - - - 
Diameter (in.) 37.9 - - 38.0 
C.G. Location    
Aft of mounting feet (in.) 2.4 1.7 Mk552-2  +1.4 
Mk552-7, -7R + 1.6 
Weight (dry), (lb.)    
Includes all controls, exhaust 
unit, igniters, thermocouples, 
oil tank and fuel pump 
1270 
1273 
(535-7R Mod 1860) 
1264 1273 
Ignition System Alternatives   
High energy type with 
transformers 
LUCAS NB34, NB38, 
NB2503, NB5707, NB5706, 
NB5714. 
- - - - 
HE units LUCAS C10/TS, C63/TS, 
C65/TS, C67/TS, C69/TS 
- - - - 
HE igniters SMITHS LR 104 series 
SMITHS KR 104 series 
Champion CR 104 series 
(Champion FHE-19-6H) 
AC Type YA20 
- - 
- - 
- - 
 
- - 
- - 
- - 
- - 
 
- - 
NOTES: 1 through 12 - - - -

TCDS  E 297   4
Certification Basis 1. For Dart 525 series, 528 series, 529-7E, 529D-7 E, 529-8E, 529D-8E, and 531:  CAR Part 10 and 
British Civil Airworthiness Requirements Section C Issue 4. 
 
  Section C Issue 4 is equivalent to the applicab le parts of CAR 13 effective June 15, 1956.  Special 
Conditions equivalent to PART 13 Amendment 13-1 and 13-2 were applied in addition to Section C 
issue 4. 
 
 2. For Dart 529-7H, 529D-7H, 529-8H, 529D-8 H, 529-8X, 529D-8X, 529-8Y, 529D-8Y, 529-8Z, 
529D-8Z, 532-2L, 532-7, 532-7L, 532-7N, 532-7P, 532-7R, 535-2, 535-7R CAR Part 10 and British 
Civil Airworthiness Requirement Section C issue 5, dated July 1, 1962. 
 
  Section C Issue 5 is equivalent to the applicab le parts of CAR Part 13 effective June 15, 1956, and 
Amendments 13-1 through 13-5. 
 
 3. For Dart 551-7, 551-7R, 552-2, 552-7, 552-7R  CAR Part 10 and British Civil Airworthiness 
Requirement Section C Issue 6, dated June 15, 1966. 
 
  Section C Issue 6 contains all the requirements of I ssue 5 and is therefore equivalent to the applicable 
parts of CAR Part 13 effective June 15, 1956 and Amendments 13-1 through 13-5. 
 
 Date of Application for Type Certificate May 17, 1956.  Engine Type Certificate No. 297 issued 
December 2, 1957.  For subsequent additions see NOTE 12. 
The aviation authority for Germany, Luftfahrt-Bundesamt, originally type certificated this engine. 
The FAA validated this product under U.S. Type Certificate Number E-297. Effective September 28, 
2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of 
Germany. 
 
 
Import Requirements:      To be considered eligible for installation on U.S.  registered aircraft, each new engine to be exported    
                                                       to the United States with Luftfahrt-Bundesamt (Germany) or EASA airworthiness approval shall  
                                                       have a Joint Aviation Authorities (JAA) or EASA Form 1, Authorized Relea se Certificate.  The JAA  
                                                       or EASA Form 1 should state that the engine conforms to the type design approved under the U.S.  
                                                       Type Certificate E-297, is in a condition for safe operation and has und ergone a final operational    
                                                       check. 
 
      Additional guidance is contained in FAA Adviso ry Circular 21.23, Airworthiness Certification of   
                                                       Civil Aircraft, Engines, Propellers and Related Products, Imported into the United States. 
 
 
N O T E S 
 
 
NOTE  1. 
Maximum permissible 
temperatures: Turbine 
gas temperature, (°C) 
525 528-7E 
528D-7E 
529-7E, 529D-7E, 529-8E, 
529D-8E, 529-7H, 529D-7H, 
529-8H, 529D-8H 
529-8X 
529D-8X 
529-8Y 
529D-8Y 
529-8Z 
529D-8Z 
Takeoff (wet) 810 860 860 - - - - - - 
Takeoff (dry) 780 810 825 - - - - - - 
Maximum  Continuous 760 850 850 870 910 920 
Maximum Transient for  
  starts 
930 - - - - - - - - - - 
Max. Overtemperature  
  (5 sec. limit) 
950 - - - - - - 1000 - - 
Oil inlet temperature 
range,  
  °C 
minus 15 
to + 115 
minus 15 
to + 120 
- - - - - - - - 
Min. start minus 30 - - - - - - - - - - 
Min. wet takeoff       
- aircraft static 40 - - - - - - - - - - 
- aircraft rolling 40 - - - - - - - - - -

TCDS  E 297   5
 
NOTE  1 (Continued) 
Maximum permissible 
temperatures:Turbine gas 
temperature, (°C) 
531 532-7 532-7L 
532-7R 
532-7N 532-2L 535-2 
Takeoff (wet) 875 860 905 - - - - 920 
Takeoff (dry) 810 - - - - - - - - - - 
Maximum Continuous 850 - - 885 - - - - 920 
Maximum Transient for starts 930 - - - - - - - - - - 
Max. Overtemperature (5 sec. limit) 950 - - 1000 - - - - - - 
Oil inlet temperature range, °C minus 15 - - - - - - - - - - 
 to + 120      
Min. start minus 30 - - - - - - - - - - 
Min. wet takeoff       
- aircraft static 50 40 50 40 60 - - 
- aircraft rolling 40 - - 50 40 - - - - 
       
 
Maximum permissible 
temperatures:Turbine gas 
temperature, (°C) 
532-7P 535-7R 551-7 551-7R 552-2, 552-7, 552-7R 
Takeoff (wet) 925 920 940 - - 930 
Takeoff (dry) - - - - 910 - - 900 
Maximum Continuous 910 920 930 - - 920 
Maximum Transient for starts - - - - - - - - 930 
Max. Overtemperature (5 sec. limit) - - - - - - - - 1000 
Oil inlet temperature range, °C - - - - - - - - - - 
Min. start - - - - - - - - - - 
Min. wet takeoff     552-2  552-7  552-7R  
- aircraft static 40 50 65 50 60 65 50 
- aircraft rolling 40 50 65 50 40 65 50 
        
 
 
NOTE  2. Fuel & Oil Pressure Limits: 
 
 Fuel supply pressure at engine fuel inlet varies with flow per latest approved issue of RR curve HK 23643. 
 
 Oil pressure varies with oil inlet temp erature.  Normal for 525 series, 13 to 35 psig; for all other models, 12 to 35 psig.  9 
psig is minimum in-flight for all models. 
 
NOTE  3. The engine ratings are based on standard conditions with no ai r bleed or aircraft accessory power extraction, 60°F, 29.92 in. 
Hg., and PW/PO=.01 at sea level within limiting gas temperatures.  On dry air, T.O. power is increased less than .5% and 
M.C. power by 1.3%.  Jet thrust is converted to equivalent shaft hp by dividing the thrust value by a factor of 2.5.  The 
output values are the minimum acceptable and are based on the use of Rolls-Royce exhaust cone RK 21556, RK 25226 or 
approved equivalent and with 12 thermocouples located in the intermediate turbine guide vanes. 
 
 
NOTE  4. Water/methanol injection is optional and is utilized through auto matically varied flow to provide a constant level of power 
output for take-off.  The w/m fluid should be a 63/37 mixture of water and methyl alcohol for all models, (Rolls-Royce 
MSRR 9359 latest approved issue).  The water used is distilled or contains a maximum of 10 ppm solids, and the methyl 
alcohol is British D.Eng.RD.2491 or equivalent.  The w/m flow varies up to a maximum for the different models as 
follows: 
 
 525 series:  493 gph (U.S.); 529-8X, 529D-8X, 529-8Y, 529D -8Y, 529-8Z, 529D-8Z, 532-2L, 532-7, 532-7N, 532-7P,:  
660 gph (U.S.); 532-7L, 532-7R, 535-7R:  673 gph (U.S.); 535-2:  696 gph (U.S.); 551-7, 551-7R, 552-2, 552-7, 552-7R:  
627 gph (U.S.); Remaining models:  564.5 gph (U.S.) 
 
 Refer to appropriate Rolls-Royce Operations Instructions  for additional operating limits, characteristics and procedures 
when using W/M selection (NOTE 14).

TCDS  E 297   6
NOTE  5. Accessory provisions on engine (oil c ooler and air inlet are engine-mounted) 
 
Drive Rotation (facing drive) Speed Ratio Continuous Static  Maximum 
 (C-clockwise) 
(CC-counter clockwise) 
to turbine Torque*  
(in. lb.) 
Torque** 
(in. lb.) 
Overhang 
(in. lb.) 
Power takeoff (120hp) CC .345 1510 6300 101 
Propeller Governor      
CU 84 for 525 series 528 series 529-7E, 
529D-7E, 529-7H, 529D-7H, 532-2L, 
532-7 series, 535 series, 551 series, and 
552-7, 552-7R 
CC .192 138 1380 102 
      
      
CU 88 for 529-8 series and 529D-8 series, 
 
     
CU 91 for 531      
CU 99 for 552-2      
Starter (Rotax C5104) CC 2.0 272 1000 84 
Fuel pump (Lucas GB 222/3AU series) CC .192 108 780 34 
* Continuous torque values are based on takeoff power at sea level. 
**   Maximum torque of weak link without permanent set, or the clutch setting for the starter. 
 
 
NOTE  6. Approved fuels and fuel additives given in Rolls-Royce Operating Instructions.  (See NOTE 14). 
 
 
NOTE  7. These engines meet FAA requirements for ic ing protection, for adequate turbine disk integrity, for rotor blade containment, 
and do not require external armoring. 
 
 
NOTE  8. Propellers used with this engine must have functioning characteristics which are compatible with the engine and its control 
system. 
 
 
NOTE  9. Maximum air bleed for aircraft servi ces is 1.55% of the no-bleed mass flow. 
 
 
NOTE  10. Maximum overspeed limit is 17000 rpm for 20 seconds.  If these limits are exceeded, the engine will require inspection as 
detailed in the Rolls-Royce Maintenance Manual. 
 
 
NOTE  11. The maximum allowable horsepower cleared for the engine to  cover operation at low ambient air temperature and/or ram 
conditions is 3000 HP for the 529 series, 532 series, 535 series, 551 and 552 series and is 2075 HP for all other models. 
 
 
NOTE  12. The above models incorporate the following general characteristics. 
   
Model: Characteristics: 
 
 
1A Dart 525 Basic model for use in Viscount  800 Series aircraft.  10' 0" Propeller. 
 
Approved December 2, 1957 
B Dart 525F As 525 with improved turbine blading and higher TCT operating 
limitations. 
 
Added April 7, 1961 Cancelled 
December 9, 2002 (See note 15) 
C Dart 525D As 525F but with a modi fication to the nozzle box affecting 
interchangeability. 
 
Added February 7, 1962 Cancelled 
December 9, 2002 (See note 15) 
2 Dart 526 Variant for installation in Ar mstrong Whitworth Argosy aircraft.  Take-
off and Maximum continuous ratings are higher than 525.  11' 6" 
Propeller. 
 
Added November 23, 1959 
Cancelled December 9, 2002 (See 
note 15)

TCDS  E 297   7
NOTE  12. (Continued) 
Model: Characteristics:  
3 Dart 527 Variant for installation in Handley Page Herald aircraft.  Ratings as Dart 
526.  12' 6" Propeller 
Added September 17, 1956 
Cancelled December 9, 2002 (See 
note 15) 
4A Dart 528 Variant for installation in F okker & Fairchild F.27 Friendship aircraft.  
ISA rating same as Dart 526 but lower takeoff and max. continuous 
temperature limit as fitted with early standard of turbine blading 11' 6" 
Propeller. 
 
Added June 22, 1960 Canceled 
September 9, 1980 (See Note 15) 
B 528-7E As 528 with improved turbine blading and higher TGT operating 
limitations. 
 
Added June 22, 1960 
C 528D-7E As 528-7E but with nozzle box m odification affecting interchangeability. 
 
Added February 7, 1962 
D 532-7 AS 528-7E but with various mech anical improvements and with a higher 
wet rating. 
 
Added June 1, 1965 
E 532-7L As 532-7 but with improved turb ine blading and higher rating/operating 
limitations. 
 
Added January 15, 1968 
F 532-7N As 532-7 but with modified wate r methanol unit, improved HP turbine 
blade material and higher T.G.T. limitations, to permit use of w/m up to 
15,000 ft. 
 
Added March 24, 1969 
G 532-7P As 532-7 but with improved turbine blading and higher wet takeoff and 
MC T.G.T. limits 
 
Added March 24, 1969 
H 532-2L As 532-7L but with installation features for Hawker Siddeley, HSA 748 
aircraft. 
 
Added April 7, 1972 
I 532-7R As 532-7L but with w/m unit set to provide higher wet takeoff rating. 
 
Added February 19, 1976 
J 535-2 As 532-2L but with improved turbine blading, higher T.G.T. limitations, 
and higher max. continuous rating. 
 
Added May 22, 1980 
K 535-7R As 532-7R but with improved turbine blading, higher T.G.T. limitations, 
and a higher maximum continuous rating. 
 
Added September 3, 1980 
5A Dart 529 Variant for installation in the Grumman Gulfstream aircraft.  As Dart 526 
but with higher takeoff and maximum continuous rating.  11 6" Propeller. 
Added September 17, 1958 
Cancelled September 9, 1980 (See 
Note 15) 
B 529D As 529 but with nozzle box mod. affecting interchangeablity. Added February 7, 1962 
Cancelled Sept 9, 1980 
(see Note 15) 
C 529-8E As 529 but with improved turbin e bladeing and higher T.G.T. operating 
limitations. 
 
Added February 7, 1962 
D 529D-8E As 529-8E but with nozzle box mod. affecting interchangeability. 
 
Added February 7, 1962 
E  529-8H As 529-8E but with various m echanical improvements and higher cruise 
T.C.T. limitations. 
 
Added June 1, 1965 
F 529D-8H As 529-8H but with nozzle box mod. affecting interchangeability. 
 
Added June 1, 1965 
G 529-7E As 529-8E but for installation in Fokker and Fairchild Executive 
Friendship aircraft.  11' 6" Propeller. 
 
Added February 7, 1962 
H 529-7E As 529-7E with nozzle box mod. affecting interchangeability. 
 
Added February 7, 1962 
I 529-7H As 529-7E but with various mech anical improvements and higher cruise 
T.G.T. limitations. 
 
Added June 1, 1965

TCDS  E 297   8
NOTE  12. (Continued) 
Models: 
(Cont'd) 
Characteristics:  
J 529D-7H As 529-7H with nozzle box mod. affecting interchangeability. 
 
Added June 1, 1965 
K 529-8X Variant for installation in Gru mman Gulfstream executive aircraft.  As 
529-8H but with higher wet take-off ratings. 
 
Added October 1, 1965 
L 529D-8X As 529-8X with nozzle box mod. affecting interchangeability. 
 
Added October 1, 1965 
M 529-8Y As 529-8X but with improved turbine blading and higher max 
continuous TGT limit. 
 
Added June 16, 1981 
N 529D-8Y As 529-8Y but with nozzle box mod affecting interchangeability 
 
Added June 16, 1981 
P 529-8Z As 529-8Y but with improved turbine blading and higher max 
continuous TGT limit 
 
Added June 16, 1981 
Q 529D-8Z As 529-8Z but with nozzle box mod affecting interchangeably. 
 
Added June 16, 1981 
6 Dart 531 Variant for installation in Avro 748 aircraft.  Ratings and limitations as 
Dart 526 but with increased wet TO TCT limit.  12' 0" dia. propeller. 
 
Added February 7, 1962 
7 Dart 530 Variant for installation in Viscount  aircraft.  Uprated 525F with increased 
wet and dry Takeoff and Maximum Continuous power ratings. 
 
Added December 28, 1982 
Cancelled December 9, 2002 (see 
note 15) 
8A Dart 551-7 Variant with new impellers and turbines for installation in Fokker F27 
aircraft.  Updated 535-7R with increased wet and dry takeoff and 
maximum continuous power ratings and improved specific fuel 
consumption. 
 
Added January 14, 1985 
B Dart 551-7R As 551-7 but with lower wet power rating. 
 
Added January 14, 1985 
9A Dart 552-2 Variant for installation in HSA 748 aircraft.  Uprated and improved s.f.c.  
Derivative of Mk536-2. 
 
Added August 30, 1985 
B Dart 552-7R Improved fuel burn derivative of Mk551-7R. 
 
Added August 30, 1985 
C Dart 552-7 Improved fuel burn derivativ e of Mk551-7, mechanically similar to 
Mk552-7R but with a higher water-methanol power rating. 
 
Added August 30, 1985 
 
 
NOTE  13.          Ratings shown give HP at the propeller shaft conditions per NOTE 3.  Corresponding ratings at the turbine shaft with 
                             40 HP gearbox offtake for these models are: 
 
 
529-8X, 529D-8X, 529-8Y, 
529D-8Y, 529-8Z, 529D-8Z 
 
 
532-7, -7N, -7P 
 
 
532-2L, -7L, 535-2 
 
 
532-7R, 535-7R 
 
2239-2030-522-15000 2239-2030-522-15000 2293-2080-532-15000 2336-2120-539-15000

TCDS  E 297   9
 
NOTE  14. ENGINE MARK NO. AIRCRAFT MAINTENANCE  
MANUAL 
OPERATING  
INSTRUCTIONS 
525 Vickers Viscount M-Da7-V F-Da7-V 
    
    
528-7E, 528D-7E Friendship 
Fairchild and Fokker 
M-Da7-F F-Da7-FaF 
F-Da7-FoF 
529-7E, 529D-7E, 
529-7H, 529D-7H 
Fairchild 
Friendship 
M-Da7-F F-Da7-FaF 
529-8E, 529D-8E Grumman Gulf stream M-Da7-G F-Da7-G 
529-8H, 529D-8H    
529-8X, 529D-8X    
529-8Y, 529D-8Y    
529-8Z, 529D-8Z    
531, 532-2L, 535-2, 
552-2 
H.S.A. 748 M-Da7-Av F-Da7-Av 
532-7, 532-7L, 532-7N Friendship 
Fairchild and Fokker 
M-Da7-F F-Da7-FaF 
F-Da7-FoF 
532-7P, 532-7R, 
535-7R, 551-7, 551-7R, 
552-7, 552-7R 
Fokker Friendship M-Da7-F F-Da7-FoF 
OVERHAUL MANUAL: 
 
ALL MARK NOS.  0-Da7-AC  
 
 
NOTE  15. The 528, 529, and 529D are no longer in service and were  deleted from this TCDS on September 9, 1980. The 525D, 
525F,526, 527 and 530 are no longer in service and were deleted from this TCDS on December 9, 2002. 
 
 
NOTE  16. Life limits, established for critical rotating components, ar e published in Chapter 5 of the maintenance and overhaul 
manuals. 
 
NOTE 17.. Each of the documents listed below must state that it is a pproved by the European Aviation Safety Agency (EASA) or, for 
approvals made before September 28, 2003 by Luftfahrt-Bundesamt (Germany) or CAA (UK). Any such documents 
including those approved under a delegated authority, are accepted by the FAA and are considered FAA approved.  
• Service bulletins,  
• Structural repair manuals,  
• Vendor manuals,  
• Aircraft flight manuals, and  
• Overhaul and maintenance manuals.  
• Technical Variances    
These approvals pertain to the type design only. 
  
---E N D---
```

## ADs (23, in force first)

- [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 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 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 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 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 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
- [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 by registry model (OpenAirDocs)

- [Rolls-Royce DART-529](https://openairdocs.org/engine/rolls-royce-dart-529-series): 4 aircraft (registry code 54507)
- [Rolls-Royce DART-535-7R](https://openairdocs.org/engine/rolls-royce-dart-535-7r): 1 aircraft (registry code 54102)
- [Rolls-Royce DART-525](https://openairdocs.org/engine/rolls-royce-dart-525): 0 aircraft (registry code 54505)
- [Rolls-Royce DART-528-7E](https://openairdocs.org/engine/rolls-royce-dart-528-7e): 0 aircraft (registry code 54078)
- [Rolls-Royce DART-528D-7E](https://openairdocs.org/engine/rolls-royce-dart-528d-7e): 0 aircraft (registry code 54079)
- [Rolls-Royce DART-529-7E](https://openairdocs.org/engine/rolls-royce-dart-529-7e): 0 aircraft (registry code 54081)
- [Rolls-Royce DART-529-7H](https://openairdocs.org/engine/rolls-royce-dart-529-7h): 0 aircraft (registry code 54083)
- [Rolls-Royce DART-529-8E](https://openairdocs.org/engine/rolls-royce-dart-529-8e): 0 aircraft (registry code 54085)
- [Rolls-Royce DART-529-8H](https://openairdocs.org/engine/rolls-royce-dart-529-8h): 0 aircraft (registry code 54087)
- [Rolls-Royce DART-529-8X](https://openairdocs.org/engine/rolls-royce-dart-529-8x): 0 aircraft (registry code 54089)
- [Rolls-Royce DART-529-8Y](https://openairdocs.org/engine/rolls-royce-dart-529-8y): 0 aircraft (registry code 54091)
- [Rolls-Royce DART-529-8Z](https://openairdocs.org/engine/rolls-royce-dart-529-8z): 0 aircraft (registry code 54093)
- [Rolls-Royce DART-529D-7E](https://openairdocs.org/engine/rolls-royce-dart-529d-7e): 0 aircraft (registry code 54082)
- [Rolls-Royce DART-529D-7H](https://openairdocs.org/engine/rolls-royce-dart-529d-7h): 0 aircraft (registry code 54084)
- [Rolls-Royce DART-529D-8E](https://openairdocs.org/engine/rolls-royce-dart-529d-8e): 0 aircraft (registry code 54086)
- [Rolls-Royce DART-529D-8H](https://openairdocs.org/engine/rolls-royce-dart-529d-8h): 0 aircraft (registry code 54088)
- [Rolls-Royce DART-529D-8X](https://openairdocs.org/engine/rolls-royce-dart-529d-8x): 0 aircraft (registry code 54090)
- [Rolls-Royce DART-529D-8Y](https://openairdocs.org/engine/rolls-royce-dart-529d-8y): 0 aircraft (registry code 54092)
- [Rolls-Royce DART-529D-8Z](https://openairdocs.org/engine/rolls-royce-dart-529d-8z): 0 aircraft (registry code 54094)
- [Rolls-Royce DART-531](https://openairdocs.org/engine/rolls-royce-dart-531): 0 aircraft (registry code 54080)
- [Rolls-Royce DART-532-2L](https://openairdocs.org/engine/rolls-royce-dart-532-2l): 0 aircraft (registry code 54095)
- [Rolls-Royce DART-532-7](https://openairdocs.org/engine/rolls-royce-dart-532-7): 0 aircraft (registry code 54096)
- [Rolls-Royce DART-532-7L](https://openairdocs.org/engine/rolls-royce-dart-532-7l): 0 aircraft (registry code 54097)
- [Rolls-Royce DART-532-7N](https://openairdocs.org/engine/rolls-royce-dart-532-7n): 0 aircraft (registry code 54098)
- [Rolls-Royce DART-532-7P](https://openairdocs.org/engine/rolls-royce-dart-532-7p): 0 aircraft (registry code 54099)
- [Rolls-Royce DART-532-7R](https://openairdocs.org/engine/rolls-royce-dart-532-7r): 0 aircraft (registry code 54100)
- [Rolls-Royce DART-535-2](https://openairdocs.org/engine/rolls-royce-dart-535-2): 0 aircraft (registry code 54101)
- [Rolls-Royce DART-551-7](https://openairdocs.org/engine/rolls-royce-dart-551-7): 0 aircraft (registry code 54103)
- [Rolls-Royce DART-551-7R](https://openairdocs.org/engine/rolls-royce-dart-551-7r): 0 aircraft (registry code 54104)
- [Rolls-Royce DART-552-2](https://openairdocs.org/engine/rolls-royce-dart-552-2): 0 aircraft (registry code 54105)
- [Rolls-Royce DART-552-7](https://openairdocs.org/engine/rolls-royce-dart-552-7): 0 aircraft (registry code 54106)
- [Rolls-Royce DART-552-7R](https://openairdocs.org/engine/rolls-royce-dart-552-7r): 0 aircraft (registry code 54107)
- [Rolls-Royce DART532](https://openairdocs.org/engine/rolls-royce-dart532-series): 0 aircraft (registry code 54509)

## STCs approved under this data sheet (5)

- [STC SE12WE](https://openairdocs.org/stc/SE12WE): Flexible hose fuel manifold assembly.. Crane Resistoflex
- [STC SE905EA](https://openairdocs.org/stc/SE905EA): Repair and modification of compresor outlet and interstage cases.. Airwork Corporation
- [STC SE19WE](https://openairdocs.org/stc/SE19WE): Flexible hose assemblies.. Resistoflex Corporation
- [STC SE206SO](https://openairdocs.org/stc/SE206SO): Replacement of accessory gear box oil pressure warning switch.. Piedmont Aviation Inc
- [STC SE748EA](https://openairdocs.org/stc/SE748EA): Installation of GLA ignition exciter.. General Laboratory Association Inc.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.