TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 1 of 8
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TYPE-CERTIFICATE
DATA SHEET
No. IM.E.035
for
PW307 series engine
Type Certificate Holder
Pratt & Whitney Canada Corp.
1000 Marie-Victorin Blvd.
Longueuil, Quebec
Canada J4G 1A1
For Models:
PW307A
PW307D
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 2 of 8
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
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Intentionally left blank
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 3 of 8
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
TABLE OF CONTENTS
I. General ..................................................................................................................................... 4
1. Type/ Model ......................................................................................................................... 4
2. Type Certificate Holder ......................................................................................................... 4
3. Manufacturer ....................................................................................................................... 4
4. Date of Application ............................................................................................................... 4
5. EASA Type Certification Reference Date ................................................................................ 4
6. EASA Certification Date ......................................................................................................... 4
II. Certification Basis ..................................................................................................................... 4
1. State of Design Authority Certification Basis .......................................................................... 4
2. EASA Certification Basis ........................................................................................................ 4
2.1 Certification Specifications: ............................................................................................. 4
2.2 Special Conditions:.......................................................................................................... 4
2.3. Environmental Protection Requirements: ....................................................................... 5
III. Technical Characteristics .......................................................................................................... 5
1. Type Design Definition .......................................................................................................... 5
2. Description ........................................................................................................................... 5
3. Equipment ............................................................................................................................ 5
4. Dimensions .......................................................................................................................... 5
5. Dry Weight ........................................................................................................................... 5
6. Ratings ................................................................................................................................. 5
7. Control System ..................................................................................................................... 5
8. Fluids (Fuel, Oil, Coolant, Additives) ...................................................................................... 5
IV. Operating Limitations .............................................................................................................. 6
1. Temperature Limits .............................................................................................................. 6
2. Speed Limits ......................................................................................................................... 6
3. Pressure Limits ..................................................................................................................... 6
3.1 Fuel Pressure .................................................................................................................. 6
3.2 Oil Pressure .................................................................................................................... 6
4. Bleed Air: ............................................................................................................................. 6
5. Oil capacity limit ................................................................................................................... 6
V. Operating and Service Instructions ........................................................................................... 6
VI. Notes ...................................................................................................................................... 7
SECTION: ADMINISTRATIVE .......................................................................................................... 8
I. Acronyms and Abbreviations ................................................................................................. 8
II. Type Certificate Holder Record.............................................................................................. 8
III. Change Record .................................................................................................................... 8
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 4 of 8
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
I. General
1. Type/ Model
Type: PW307 / Models: PW307A, PW307D
2. Type Certificate Holder
Pratt & Whitney Canada Corp.
1000 Marie-Victorin Blvd.
Longueuil, Quebec
Canada J4G 1A1
3. Manufacturer
Pratt & Whitney Canada Corp.
1000 Marie-Victorin Blvd.
Longueuil, Quebec
Canada J4G 1A1
4. Date of Application
PW307A: 27 May 2002
PW307D: 30 October 2014
5. EASA Type Certification Reference Date
see also Canadian TCDS No. E-33
30 January 2002
6. EASA Certification Date
23 Feb 2007 – PW 307A
27 April 2016 – PW 307D
II. Certification Basis
1. State of Design Authority Certification Basis
1.1. Airworthiness Manual Chapter 533, change 533-5, dated 1 December 1999 as amended by
NPA-2000-265, adopted 5 March 2001.
1.2. Airworthiness Manual, Chapter 516, Change 516-06, subchapter B “Aircraft Engine
Emissions” plus ICAO Annex 16 Volume II, amendment 4.
see Canadian TCDS E-33
2. EASA Certification Basis
2.1 Certification Specifications:
JAR-E Amendment 11
E570 – Oil System of JAR-E Amendment 12
E850 of CS-E initial issue – Compressor, Fan and Turbine Shafts
E890 of CS-E initial issue – Thrust Reverser Tests
2.2 Special Conditions:
Certification of Programmable Logic Devices (PLDs)
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
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2.3. Environmental Protection Requirements:
CS-34 Amendment 4 as implemented by ED Decision 2021/011/R (applicable 25 July 2021),
ICAO Annex 16 Volume II, Amendment 10 applicable 1 January 2021 as implemented into EU
legislation 27 April 2021 . NOx standard in accordance with ICAO Annex 16 Volume II, Part III,
Chapter 2, § 2.3.2 e) (CAEP/8). Maximum nvPM mass concentration levels in compliance with
Part III, Chapter 4, paragraph 4.2.2.1. nvPM mass and number emissions in compliance with
Part III, Chapter 4, paragraph 4.2.2.2 a) 1) and 4.2.2.2 b) 1) (CAEP/11 In-Production standard).
III. Technical Characteristics
1. Type Design Definition
The Engine Type Design is defined in Engine Assembly Parts List No. A30P0100-01 (PW307A) and
A30P3300-01 (PW307D).
2. Description
Two Spool Turbofan Engine consisting of a single front fan driven by a three stage fan turbine, 4
stage axial and one stage centrifugal high pressure compressor driven by a two stage high
pressure turbine; annular combustion chamber; accessory gearbox and dual channel Full
Authority Digital Electronic Control System (FADEC).
3. Equipment
see Installation Manual
4. Dimensions
The maximum diameter of the engine is about 1170 mm.
Engine length is about 2185 mm.
5. Dry Weight
(PW307A/PW307D): 551 kg (dry weight including standard equipment)
6. Ratings
Take-off: PW307A: 2849 daN PW307D: 2991 daN
Max. Continuous: PW307A: 2849 daN PW307D: 2991 daN
7. Control System
The engines are equipped with a dual channel FADEC system EEC P/N 30P0608-04 or later
approved standard.
8. Fluids (Fuel, Oil, Coolant, Additives)
Approved fuel and oil types are listed in the Maintenance Manual.
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 6 of 8
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
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IV. Operating Limitations
1. Temperature Limits
Interturbine Temperature [°C]:
PW307A PW307D
Take-off 920 920
Max. Cont. 920 920
Starting 950 950
Transient (20sec.) 930 945
Fuel Temperatures: Min.: -40°C (Kerosene Type) Max.: +57°C (starting and normal
operation up to 20,000ft) - for details
refer to chapter 2.4 of the relevant
Installation Manual
Oil Temperatures: Engine Operation: 25°C to 141°C
Starting: -40 °C for details refer to Table 2-1 of the
relevant Installation Manual
2. Speed Limits
Permissible Rotational Speeds [min
-1
] for PW307A/PW307D:
N1 11110 (101%)
N2 28500 (100%)
Min. N2
Flight Idle 17100 (60%)
3. Pressure Limits
3.1 Fuel Pressure
Max. at pump inlet: 241 kPa
Min: 34,5 kPa above true vapour pressure (normal operation) For details refer to relevant
Installation Manual,
Section 6.
3.2 Oil Pressure
Engine Operation: 241 to 1000 kPa for details refer to relevant Installation Manual,
Table 2-1.
4. Bleed Air:
Refer to relevant Installation Manual, Section 2.
5. Oil capacity limit
total oil capacity: 7,1 l
usable oil capacity: 2,19 l
V. Operating and Service Instructions
1. Maintenance Manual: P/N 30P0422 (PW307A) P/N 30P3242 (PW307D)
2. Overhaul Manual: P/N 30P0423 (PW307A) P/N 30P3243 (PW307D)
3. Installation Manual: ER5598 (PW307A) P/N 30P3400 (PW307D)
4. FADEC Interface Control Document : ER5220 (PW307A) ER8652 (PW307D)
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 7 of 8
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
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VI. Notes
1. The Critical Parts Life Limits are included in the Airworthiness Limitations Section of the Maintenance
Manual.
2. The engine ratings are based on dry sea level static ICAO standard atmospheric conditions, no external
accessory loads and no airbleed. The quoted ratings are obtainable on a test stand with the specified
fuel and oil, and using the exhaust duct and intake bellmouth specified in the Installation Manual.
3. The PW307A and PW307D Engines are approved for multiple engine installation only.
4. HIRF and Lightning conformance and installation requirements are provided in the Installation
Manual.
5. The software contained in the Electronic Engine Control has been designed, developed, tested and
documented in accordance with the provisions of the Critical Category, Level A of RTCA/DO178B /
EUROCAE ED-12B.
6. The engines are approved for operation with a Thrust Reverser P/N F7XC782140020 which is not part
of the engine Type Design.
7. The PW307A and PW307D engines are approved with Time Limited Dispatch (TLD) Limitations. The
dispatch criteria are contained in the Airworthiness Limitations section of relevant Maintenance
Manuals.
TCDS No.: IM.E.035
PW307 series engine
Issue: 06
10 January 2023
TE.CERT.00052-001 © European Union Aviation Safety Agency, 2023. All rights reserved. ISO9001 Certified. Page 8 of 8
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
SECTION: ADMINISTRATIVE
I. Acronyms and Abbreviations
n/a
II. Type Certificate Holder Record
n/a
III. Change Record
Issue
Date
Changes
TC issue
Issue 01
23 Feb 2007
Initial Issue
Initial Issue,
23 Feb 2007
Issue 02
05 June 2007
Introduction of FADEC Interface Control
Document ER 5220
Issue 03
03 Jan 2013
Emissions requirements according to ICAO annex
16
Issue 04
27 April 2016
Model PW307D added
27 April 2016
Issue 05
12 December
2019
Introduction of CAEP/10 for nvPM compliance
(EASA Major Change approval 10072018)
Issue 06
10 January 2023
Introduction of CAEP/11 for nvPM compliance
(EASA Major Change approval 10080993)
-END-
