# TCDS E00087EN: International Aero Engines LLC - Type: Type certificate data sheet - Status: Current - Holder: International Aero Engines LLC - Revision: 13 - Revised: July 10, 2026 - Product: Engine - Certification basis: Part 33, Part 34 - Registered aircraft: 440, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/81/70/8170fc021cd5c52fcb3e05ed02b6fcfc4f357663f8f52b0bf68aca544a9592c3 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115578277120260713164318.0001 - Page: https://openairdocs.org/tcds/E00087EN ## Models (41) As the data sheet lists them. - PW1431G-JM - PW1133GA-JM - PW1127G1-JM - PW1129G-JM - PW1127G-JM - PW1428GH-JM - PW1127GA-JM - PW1428GA-JM - PW1431GH-JM - PW1124G-JM - PW1124G1-JM - PW1133G-JM - PW1431GA-JM - PW1130G-JM - PW1428G-JM - PW1127G1A-JM - PW1127G1B-JM - PW1133GR/2-JM - PW1133GAR/2-JM - PW1133G1R/2-JM - PW1133GH/2-JM - PW1134GA/2-JM - PW1134G1/2-JM - PW1133G/2-JM - PW1133GA/2-JM - PW1133G1/2-JM - PW1130G/2-JM - PW1129G/2-JM - PW1127G/2-JM - PW1127GA/2-JM - PW1127G1/2-JM - PW1127G1A/2-JM - PW1127G1B/2-JM - PW1127GH/2-JM - PW1124G/2-JM - PW1124G1/2-JM - PW1130GS-JM - PW1133GS-JM - PW1133GAS-JM - PW1133G1S-JM - PW1122G-JM ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" NOT APPLICABLE NOTE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN PAGE 1 2 3 4 5 6 7 8 9 10 11 12 REV. 13 13 13 13 13 13 11 13 13 13 12 13 TCDS NUMBER E00087EN Revision 13 U. S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E00087EN International Aero Engines, LLC MODELS: PW1133G-JM, PW1133G1-JM, PW1133G1R-JM, PW1133GA-JM, PW1133GAR-JM, PW1133GR-JM, PW1133GS-JM, PW1133GAS-JM, PW1133G1S-JM, PW1130G-JM, PW1130GS-JM, PW1129G-JM, PW1127G-JM, PW1127G1-JM, PW1127G1A-JM, PW1127G1B-JM, PW1127GA-JM, PW1124G-JM, PW1124G1-JM, PW1134G1/2-JM, PW1134GA/2-JM, PW1133G/2-JM, PW1133G1/2-JM, PW1133G1R/2-JM, PW1133GA/2-JM, PW1133GAR/2-JM, PW1133GH/2-JM, PW1133GR/2-JM, PW1133GS/2-JM, PW1133GAS/2-JM, PW1133G1S/2-JM, PW1130G/2-JM, PW1130GS/2-JM, PW1129G/2-JM, PW1127G/2-JM, PW1127G1/2-JM, PW1127G1A/2-JM, PW1127G1B/2-JM, PW1127GA/2-JM, PW1127GH/2-JM, PW1124G/2-JM, PW1124G1/2-JM, PW1431G-JM, PW1431GA-JM, PW1431GH-JM, PW1428G- JM, PW1428GA-JM, and PW1428GH-JM Date: 07/10/2026 Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E00087EN ) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft i n accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations, provided t hey are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE (TC) HOLDER: International Aero Engines, LLC 400 Main Street East Hartford, CT 06118 High bypass ratio, axial-airflow, dual-spool, turbofan engine controlled by a Full Authority Digital Electronic Control (FADEC). The low pressure spool consists of a three-stage low pressure turbine that directly drives a three-stage low pressure compressor, and a single stage high bypass ratio fan through a fan drive gear speed reduction system. The high pressure compressor has eight axial stages driven by a two-stage cooled high-pressure turbine. MODELS: PW1133G-JM PW1133GA-JM PW1133G1-JM PW1130G-JM PW1130GS-JM PW1133G/2-JM PW1133GA/2-JM PW1133G1/2-JM PW1130G/2-JM PW1130GS/2-JM PW1431G-JM PW1431GA-JM PW1431GH-JM PW1428G-JM PW1428GA-JM PW1428GH-JM PW1129G-JM PW1129G/2-JM RATINGS (See NOTE 1) SEA LEVEL STATIC THRUST (lb.) Takeoff (5 minutes) Maximum Continuous 33,110 32,780 30,410 (PW1130G-JM & PW1130G/2-JM) 21,400 (PW1130GS- JM, PW1130GS/2-JM) 31,572 31,068 29,761 28,450 29,245 26,345 FLAT RATING AMBIENT TEMPERATURE Takeoff Maximum Continuous 30°C / 86°F 25°C / 77°F 55°C / 131°F (PW1130GS-JM, PW1130GS/2-JM) 30°C / 86°F 25°C / 77°F 30°C / 86°F 30°C / 86°F 44°C / 111°F 25°C / 77°F Data Storage Unit (DSU) PN (Ratings Plug) Service Bulletin PW30K-A-73-00-0066-00A-930A-D provides a listing of DSU Part Numbers. TCDS E00087EN Page 2 of 12 COMPONENTS/CONFIGURATION For information regarding components and engine configuration, refer to: PW1100G-JM Installation Drawing 5320001 PW1400G-JM Installation Drawing 5330001 PW1100G/2-JM Installation Drawing 5360001 MODELS: PW1127G-JM PW1127GA-JM PW1127G/2-JM PW1127GA/2-JM PW1124G-JM PW1124G1-JM PW1124G/2-JM PW1124G1/2-JM PW1127G1-JM PW1127G1A-JM PW1127G1B-JM PW1127G1/2-JM PW1127G1A/2-JM PW1127G1B/2-JM PW1127GH/2-JM PW1133GR-JM PW1133GAR-JM PW1133G1R-JM PW1133GS-JM PW1133GAS-JM PW1133G1S-JM PW1133GR/2-JM PW1133GAR/2-JM PW1133G1R/2-JM PW1133GS/2-JM PW1133GAS/2-JM PW1133G1S/2-JM PW1133GH/2-JM PW1134GA/2-JM PW1134G1/2-JM RATINGS (See NOTE 1) SEA LEVEL STATIC THRUST (lb.) Takeoff (5 minutes) Maximum Continuous 27,075 26,345 24,240 24,035 27,075 24,070 33,110 23,250 FLAT RATING AMBIENT TEMPERATURE Takeoff Maximum Continuous 47°C / 117°F 25°C / 77°F 51°C / 123°F 25°C / 77°F 47°C / 117°F 30°C / 86°F 30°C / 86°F 55°C / 131°F Data Storage Unit (DSU) PN (Ratings Plug) Service Bulletin PW30K-A-73-00-0066-00A-930A-D provides a listing of DSU Part Numbers. TCDS E00087EN Page 3 of 12 MODELS: (cont.) PW1133G-JM PW1133GA-JM PW1133G1-JM PW1130G-JM PW1130GS-JM PW1133G/2-JM PW1133GA/2-JM PW1133G1/2-JM PW1130G/2-JM PW1130GS/2-JM PW1431G-JM PW1431GA-JM PW1431GH-JM PW1428G-JM PW1428GA-JM PW1428GH-JM PW1129G-JM PW1129G/2-JM PRINCIPAL DIMENSIONS (Room temperature) Length (flange to flange, in.) Length (fan spinner face to #6 bearing heatshield, in.) Nominal diameter (fan case, in.) Maximum radial projection (in.) (at oil tank) CENTER OF GRAVITY (in.) Axial engine station, relative to A-flange: Vertical, relative to engine centerline: Lateral, relative to centerline: 129.285 in +/- 0.051 134.350 in 87.566 in 50.150 in 63.510 in 63.688 in (PW1100G/2-JM models) - 1.420 in - 1.250 in (PW1100G/2-JM models) 0.820 in 0.290 in (PW1100G/2-JM models) -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- WEIGHT * (DRY) Basic engine (lbs.) 6,300 6,300 6,300 6,300 *The PW1100G-JM & PW1100G/2-JM engine weight is defined as the dry weight of the basic engine with IAE, LLC supplied engine build-up component (EBU1). EBU1 components include: Low Oil Pressure Switch; Core Nacelle Temperature Sensor; GBX Breather Tube; Engine Air Turbine Starter; starter attachment hardware and seals to gearbox; duct from starter to Starter Air Valve; Starter Air Valve; electrical harnesses; Mass Fuel Flow Meter; environmental control system Intermediate Pressure Check Valve. The PW1400G-JM engine weight is defined as the dry weight of the basic engine with standard equipment only FUEL Service Bulletin PW1000G-D-73-00-0002-00A-930A-D defines the fuels requirements and provides a listing of approved fuels and fuel additives for use in the PW1100G-JM & PW1100G/2-JM series turbofan engines. Service Bulletin PW1000G-C-73-00-0001-00B-930A-D defines the fuels requirements and provides a listing of approved fuels and fuel additives for use in the series turbofan engines. PW1400G-JM series turbofan engines. LUBRICATING OILS Service Bulletin PW1000G-D-79-00-0002-00A-930A-D provides a listing of approved turbine oils for use in the PW1100G-JM & PW1100G/2-JM series turbofan engines. Service Bulletin PW1000G-C-79-00-0001-00B-930A-D provides a listing of approved turbine oils for use in the PW1400G-JM series turbofan engines. TCDS E00087EN Page 4 of 12 MODELS: (cont. ) PW1127G-JM PW1127GA-JM PW1127G/2-JM PW1127GA/2-JM PW1124G-JM PW1124G1-JM PW1124G/2-JM PW1124G1/2-JM PW1127G1-JM PW1127G1A-JM PW1127G1B-JM PW1127G1/2-JM PW1127G1A/2-JM PW1127G1B/2-JM PW1127GH/2-JM PW1133GR-JM PW1133GAR-JM PW1133G1R-JM PW1133GS-JM PW1133GAS-JM PW1133G1S-JM PW1133GR/2-JM PW1133GAR/2-JM PW1133G1R/2-JM PW1133GS/2-JM PW1133GAS/2-JM PW1133G1S/2-JM PW1133GH/2-JM PW1134GA/2-JM PW1134G1/2-JM PRINCIPAL DIMENSIONS (Room temperature) Length (flange to flange, in.) Length (fan spinner face to #6 bearing heatshield, in.) Nominal diameter (fan case, in.) Maximum radial projection (in.) (at oil tank) CENTER OF GRAVITY (in.) Axial engine station, relative to A-flange: Vertical, relative to engine centerline: Lateral, relative to centerline: 129.285 in +/- 0.051 134.350 in 87.566 in 50.150 in 63.510 in 63.688 in (PW1100G/2-JM models) - 1.420 in - 1.250 in (PW1100G/2-JM models) 0.820 in 0.290 in (PW1100G/2-JM models) -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- WEIGHT * (DRY) Basic engine (lbs.) 6,300 6,300 6,300 6,300 *The PW1100G-JM & PW1100G/2-JM engine weight is defined as the dry weight of the basic engine with IAE, LLC supplied engine build-up component (EBU1). EBU1 components include: Low Oil Pressure Switch; Core Nacelle Temperature Sensor; GBX Breather Tube; Engine Air Turbine Starter; starter attachment hardware and seals to gearbox; duct from starter to Starter Air Valve; Starter Air Valve; electrical harnesses; Mass Fuel Flow Meter; environmental control system Intermediate Pressure Check Valve. The PW1400G-JM engine weight is defined as the dry weight of the basic engine with standard equipment only FUEL Service Bulletin PW1000G-D-73-00-0002-00A-930A-D defines the fuels requirements and provides a listing of approved fuels and fuel additives for use in the PW1100G-JM & PW1100G/2- JM series turbofan engines. Service Bulletin PW1000G-C-73-00-0001-00B-930A-D defines the fuels requirements and provides a listing of approved fuels and fuel additives for use in the and PW1400G-JM series turbofan engines. LUBRICATING OILS Service Bulletin PW1000G-D-79-00-0002-00A-930A-D provides a listing of approved turbine oils for use in the PW1100G-JM & PW1100G/2-JM series turbofan engines. Service Bulletin PW1000G-C-79-00-0001-00B-930A-D provides a listing of approved turbine oils for use in the PW1400G-JM series turbofan engines. TCDS E00087EN Page 5 of 12 CERTIFICATION BASIS PW1100G-JM & PW1400G-JM Engine Models • 14 CFR, Part 33, effective February 1, 1965, as amended by 33-1 through 33-32 • Equivalent Level of Safety findings: o 33.76, Bird Ingestion, par. (c)(7)(i) ELOS No. TC3289EN-E-P-8-R1 o 33.77, Foreign Object Ingestion-Ice, par. (c) ELOS No. TC3289EN-E-P-5-R1 o 33.78, Rain and Hail Ingestion, par. (a)(1) ELOS No. TC3289EN-E-P-6-R1 o 33.27, Rotor Overspeed, par. (c) & (e) ELOS No TC3289EN-E-P-9 • Exemptions: o 33.76, Bird Ingestion, par. (c)(6)(i) and (c)(7)(vii), Exemption No. 23174A. Applicable to engine models PW1133GR-JM, PW1133GAR-JM, PW1133G1R-JM, PW1130GS-JM, PW1133GS-JM, PW1133GAS-JM, and PW1133G1S-JM only. • 14 CFR, Part 34, Amendment 34-1 through 34-7A, effective May 24, 2024. See NOTE 23 for detailed summary of the certification basis for fuel venting and exhaust emissions. TYPE CERTIFICATE NUMBER: E00087EN MODEL APPLICATION ISSUED/AMENDED DELETED PW1133G-JM December 15, 2011 December 19, 2014 PW1133GA-JM June 12, 2015 October 23, 2015 PW1130G-JM December 15, 2011 October 23, 2015 PW1127G-JM December 15, 2011 October 23, 2015 PW1127GA-JM June 12, 2015 October 23, 2015 PW1127G1-JM December 15, 2011 August 16, 2023 PW1124G-JM December 15, 2011 October 23, 2015 PW1124G1-JM December 15, 2011 October 23, 2015 PW1122G-JM December 15, 2011 October 23, 2015 January 28, 2026 PW1431G-JM January 20, 2015 May 6, 2016 PW1129G-JM April 11, 2017 May 29, 2018 PW1431GA-JM October 3, 2017 May 29, 2018 PW1431GH-JM October 3, 2017 May 29, 2018 PW1428G-JM October 3, 2017 May 29, 2018 PW1428GA-JM October 3, 2017 May 29, 2018 PW1428GH-JM October 3, 2017 May 29, 2018 PW1127G1A-JM June 22, 2021 August 16, 2023 PW1127G1B-JM June 22, 2021 August 16, 2023 PW1133G1-JM December 11, 2023 December 12, 2024 PW1133GR-JM December 11, 2023 December 12, 2024 PW1133GAR-JM December 11, 2023 December 12, 2024 PW1133G1R-JM December 11, 2023 December 12, 2024 PW1130GS-JM April 23, 2025 June 26, 2026 PW1133GS-JM April 23, 2025 June 26, 2026 PW1133GAS-JM April 23, 2025 June 26, 2026 PW1133G1S-JM April 23, 2025 June 26, 2026 TCDS E00087EN Page 6 of 12 PW1100G/2-JM Engine Models • 14 CFR, Part 33, effective February 1, 1965, as amended by 33-1 through 33-32, §§33.68 & 33.77, Amendment 34 with the following • Equivalent Level of Safety findings: o 33.78, Rain and Hail Ingestion, par. (a)(1) ELOS No. TC3289EN-E-P-6-R1 o 33.27, Rotor Overspeed, par. (c) & (e) ELOS No TC3289EN-E-P-9 • Exemptions: o 33.76, Bird Ingestion, par. (c)(6)(i) and (c)(7)(vii), Exemption No. 23174A. Applicable to engine models: PW1133GH/2-JM, PW1134GA/2-JM, PW1134G1/2- JM, PW1133GR/2-JM, PW1133GAR/2-JM, PW1133G1R/2-JM, PW1130GS/2-JM, PW1133GS/2-JM, PW1133GAS/2-JM and PW1133G1S/2-JM only. • 14 CFR, Part 34, Amendment 34-1 through 34-7A, effective May 24, 2024. See NOTE 23 for detailed summary of the certification basis for fuel venting and exhaust emissions. TYPE CERTIFICATE NUMBER: E00087EN MODEL PW1133GR/2-JM PW1133GAR/2-JM PW1133G1R/2-JM PW1133GH/2-JM PW1134GA/2-JM PW1134G1/2-JM PW1133G/2-JM PW1133GA/2-JM PW1133G1/2-JM PW1130G/2-JM PW1129G/2-JM PW1127G/2-JM PW1127GA/2-JM PW1127G1/2-JM PW1127G1A/2-JM PW1127G1B/2-JM PW1127GH/2-JM PW1124G/2-JM PW1124G1/2-JM PW1122G/2-JM PW1130GS/2-JM PW1133GS/2-JM PW1133GAS/2-JM PW1133G1S/2-JM APPLICATION April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 03, 2019 April 23, 2025 April 23, 2025 April 23, 2025 April 23, 2025 ISSUE/AMENDED February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 February 26, 2025 June 26, 2026 June 26, 2026 June 26, 2026 June 26, 2026 DELETED January 28, 2026 PRODUCTION BASIS (ALL MODELS) Production Certificate No. 114 TCDS E00087EN Page 7 of 12 NOTES NOTE 1. ENGINE RATINGS Engine ratings are based on calibrated test stand performance under the following conditions: 1. Sea level static, standard pressure (14.696 psia), up to the flat rating ambient temperature °F 2. No customer bleed or customer horsepower extraction 3. Ideal inlet, 100% ram recovery 4. Production aircraft flight cowling corrected to ideal conditions 5. Production instrumentation 6. Fuel lower heating value of 18,400 BTU/lb. 7. The normal 5 minute takeoff rating may be extended to 10 minutes for engine out contingency. NOTE 2. TEMPERATURES Maximum permissible Indicated Turbine Temperatures (ITT) are as follows: Condition Inter-Turbine Temperature (PW1100G-JM) Inter-Turbine Temperature (PW1100G/2-JM) 2 Takeoff (5 Minutes) 1 Actual Redline 1,083 degC / 1,982 degF 1,093 degC / 1,999 degF Cockpit Indicated 1,083 degC / 1,982 degF 1,083 degC / 1,982 degF Maximum Continuous Actual Redline 1,043 degC / 1,909 degF 1,051 degC / 1,923 degF Cockpit Indicated 1,043 degC / 1,909 degF 1,043 degC / 1,909 degF Start-up Ground Actual Redline 1,083 degC / 1,982 degF 1,093 degC / 1,999 degF Cockpit Indicated 1,083 degC / 1,982 degF 1,083 degC / 1,982 degF Start-up In-flight Actual Redline 1,083 degC / 1,982 degF 1,093 degC / 1,999 degF Cockpit Indicated 1,083 degC / 1,982 degF 1,083 degC / 1,982 degF 1. May be extended to 10 minutes for One Engine Inoperative (O.E.I.) contingency. 2. The cockpit and aircraft flight manuals will reflect temperature limits consistent with PW1100G-JM, but the EEC Software allows Actual Redline limits shown above. Oil outlet temperature: Continuous operation: Engine main oil temperature maximum limit varies with engine power level. The limit decreases from 152 degC /305 degF at idle power; to 146 degC /295 degF at cruise power; to 141 degC /285 deg F at high power. See PW1100G-JM & PW1100G/2-JM Installation and Operating Manual, PWA-9851 or PW1400G-JM Installation and Operating Manual, PWA-9914 for details. Minimum oil temperature at idle, before takeoff power operation: For PW1100G-JM & PW1100G/2-JM series turbofan engines: 51.7 degC / 125 degF For PW1400G-JM series turbofan engines: 37.7 degC / 100 degF Fuel Temperatures: See PW1100G-JM & PW1100G/2-JM Installation and Operating Manual, PWA-9851 or PW1400G-JM Installation and Operating Manual, PWA-9914 for details Component Temperatures: See PW1100G-JM & PW1100G/2-JM Installation and Operating Manual, PWA-9851 or PW1400G-JM Installation and Operating Manual, PWA-9914 for details NOTE 3. PRESSURES Fuel pressure limits: Fuel pressure at the engine fuel pump inlet during operation shall be maintained at not less than 5.0 psi above the true vapor pressure of the fuel but not greater than 60 psig with a vapor/liquid ratio of zero. The maximum allowable pressure at the fuel pump inlet after shutdown is 151 psig. Oil pressure limits: Minimum: 63 psig at idle. Variable by N2 Speed off idle. See PW1100G-JM & PW1100G/2-JM Installation and Operating Manual, PWA- 9851 or PW1400G-JM Installation and Operating Manual, PWA-9914 for details. Maximum: 270 psig Oil supply pressure is measured relative to ambient pressure: Temporary interruption associated with negative “g” operation is limited to 10 seconds maximum. Normal oil pressure will be restored rapidly once the negative “g” effect has been eliminated. TCDS E00087EN Page 8 of 12 NOTE 4. ACCESSORY DRIVE PROVISIONS PW1100G-JM & PW1100G/2-JM ACCESSORY DRIVES Drive Pad Rotation Speed Ratio to N2 Torque (lb.-in.) Overhung Moment (lb.-in.) Continuous Overload Static Hydraulic Pump Integrated Drive Generator (IDG) Air Turbine Starter CCW CCW CCW 0.1768 : 1 0.3932 : 1 0.407 : 1 1300 1990* --- 1800 4475* 10692 4250 9400 9084 400 900 280 CCW = Counterclockwise (facing the drive pad) * Maximum allowable continuous torque values are at any engine speed unless otherwise specified provided no destructive forces resulting from accessory torsional vibration are present. PW1400G-JM ACCESSORY DRIVES Drive Pad Rotation Speed Ratio to N2 Torque (lb.-in.) Overhung Moment (lb.-in.) Continuous Overload Static Hydraulic Pump Variable Frequency Generator (VFG) Air Turbine Starter CCW CCW CCW 0.1763 : 1 0.9611 : 1 0.407 : 1 1300 1000* --- 1800 1300* 10692 4250 7655 9084 400 1275 280 CCW = Counterclockwise (facing the drive pad) * Maximum allowable continuous torque values are at any engine speed unless otherwise specified provided no destructive forces resulting from accessory torsional vibration are present. NOTE 5. MODEL DESCRIPTION The PW1100G-JM engine series consists of the following engine models: PW1100G-JM Engine Models Associated A/C Model Description PW1124G-JM A319-171N Basic Model PW1124G1-JM A320-272N Alternate Climb Thrust Model PW1127G-JM A320-271N Basic Model PW1127GA-JM A320-271N Alternate Climb Thrust Model PW1127G1-JM+ A319-173N Hot and High Thrust Model, Reduced Go Around Thrust A320-271N Basic Model, Reduced Go Around Thrust PW1127G1A-JM+ A320-271N Alternate Climb Thrust Model, Reduced Go Around Thrust Alternate Climb C, Reduced Go Around Thrust PW1127G1B-JM+ A320-271N Alternate Climb Thrust Model, Reduced Go Around Thrust PW1129G-JM+ A320-273N High and Hot Airfield Thrust Model PW1130G-JM A321-272N A321-272NX Reduced Thrust Model PW1130GS-JM+ A321-272N A321-272NX Reduced Thrust Model, Reduced Go Around Thrust PW1133G-JM A321-271N A321-271NX Basic Model PW1133GA-JM A321-271N A321-271NX Alternate Climb Thrust Model Alternate Climb C Thrust Model PW1133G1-JM^ A321-271N A321-271NX Hot Day Take Off Boost PW1133GR-JM+ A321-271NY Basic Model, Reduced Go Around Thrust PW1133GS-JM+ A321-271N A321-271NX Basic Model, Reduced Go Around Thrust PW1133GAS-JM+ A321-271NX A321-271NX Alternate Climb A Thrust Model, Reduced Go Around Thrust PW1133G1S-JM+^ A321-271N A321-271NX Hot Day Take Off Boost, Reduced Go Around Thrust PW1133GAR-JM+ A321-271NY Alternate Climb Thrust Model, Reduced Go Around Thrust PW1133G1R-JM+^ A321-271NY Hot Day Take Off Boost, Alternate Climb Thrust Model, Reduced Go Around Thrust TCDS E00087EN Page 9 of 12 NOTE 5 – cont’d. The PW1100G/2-JM engine series consists of the following engine models: PW1100G/2-JM Engine Models Associated A/C Model Description PW1124G/2-JM A319-171N Basic Model PW1124G1/2-JM A320-272N Alternate Climb Thrust Model PW1127G/2-JM A320-271N Basic Model PW1127GA/2-JM A320-271N Alternate Climb Thrust Model PW1127G1/2-JM+ A319-173N Hot and High Thrust Model, Reduced Go Around Thrust A320-271N Basic Model, Reduced Go Around Thrust PW1127G1A/2-JM+ A320-271N Alternate Climb Thrust Model, Reduced Go Around Thrust PW1127G1B/2-JM+ A320-271N Alternate Climb Thrust Model, Reduced Go Around Thrust PW1127GH/2-JM+ A320-271N Hot and High Thrust Model PW1129G/2-JM+ A320-273N High and Hot Airfield Thrust Model PW1130G/2-JM A321-272N Reduced Thrust Model A321-272NX PW1130GS/2-JM+ A321-272N A321-272NX Reduced Thrust Model, Reduced Go Around Thrust PW1133G/2-JM A321-271N Basic Model A321-271NX PW1133GA/2-JM A321-271N Alternate Climb Thrust Model A321-271NX PW1133G1/2-JM^ A321-271N Hot Day Take Off Boost A321-271NX PW1133GR/2-JM+ A321-271NY Basic Model, Reduced Go Around Thrust PW1133GS/2-JM+ A321-271N A321-271NX Basic Model, Reduced Go Around Thrust PW1133GAS/2-JM+ A321-271N A321-271NX Alternate Climb A Thrust Model, Reduced Go Around Thrust PW1133G1S/2-JM+^ A321-271N A321-271NX Hot Day Take Off Boost, Reduced Go Around Thrust PW1133GAR/2-JM+ A321-271NY Alternate Climb Thrust Model, Reduced Go Around Thrust PW1133G1R/2-JM+^ A321-271NY Hot Day Take Off Boost, Alternate Climb Thrust Model, Reduced Go Around Thrust PW1133GH/2-JM+ A321-271NY Hot and High Thrust Model, Reduced Go Around Thrust A321-271N Hot and High Thrust Model, Reduced Go Around Thrust A321-271NX PW1134GA/2-JM+ A321-271NY 4% Take Off & Max Continuous Boost, Alternate Climb Thrust Model, Reduced Go Around Thrust PW1134G1/2-JM+ A321-271NY 4% Take Off & Max Continuous Boost, Reduced Go Around Thrust + These models include different thrust levels for Go-Around. The thrust is selected by the Electronic Engine Control (EEC) based on aircraft & engine inputs. The Go-Around thrust is less than the maximum rated takeoff thrust of the PW1100G-JM & PW1100G/2-JM engine, as agreed with the Aircraft Type Certificate Holder. See Installation and Operating Manual PWA-9851. ^ These models include a cockpit selectable thrust boost of 2% increased thrust. The 2% thrust boost is equal to or less than the maximum rated takeoff thrust of the PW1100G-JM & PW1100G/2-JM engine. The PW1400G-JM engine series consists of the following engine models: PW1400G-JM Engine Models Associated A/C Model Description PW1428G-JM Irkut MC21-200 Basic Model PW1428GA-JM Irkut MC21-200 Alternate Climb Thrust Model PW1428GH-JM Irkut MC21-200 High and Hot Airfield Thrust Model PW1431G-JM Irkut MC21-300 Basic Model PW1431GA-JM Irkut MC21-300 Alternate Climb Thrust Model PW1431GH-JM Irkut MC21-300 High and Hot Airfield Thrust Model TCDS E00087EN Page 10 of 12 NOTE 6. TYPICAL AIRCRAFT ACCESSORIES, COMPONENTS, OR SYSTEM ASSEMBLIES, WITH AIRCRAFT LEVEL REQUIREMENTS, PROVIDED AS PART OF ENGINE TYPE DESIGN For the PW1100G-JM & PW1100G/2-JM Engine Models: Air Turbine Starter; Starter Air Valve. NOTE 7. AIRCRAFT ACCESSORIES, COMPONENTS, OR SYSTEM ASSEMBLIES INSTALLED ON THE ENGINE BUT ARE NOT PROVIDED AS PART OF ENGINE TYPE DESIGN For the PW1400G-JM Engine Models: Environmental Control System Intermediate Pressure Check Valve NOTE 8. SPECIAL ANTI-ICING OR DE-ICING REQUIREMENTS Not Applicable NOTE 9. ENGINE MOUNT SYSTEM PROVISIONS PW1100G-JM Engine mount system provisions are specified in Installation Drawing 5320001 and Mount and Maneuver Load Drawing 5360003. PW1400G-JM Engine mount system provisions are specified in Installation Drawing 5330001 and Mount and Maneuver Load Drawing 5330003. PW1100G/2-JM Engine mount system provisions are specified in Installation Drawing 5360001 and Mount and Maneuver Load Drawing 5360003. NOTE 10. POWER BOOST, INJECTION OR AUGMENTATION SYSTEMS Not Applicable NOTE 11. SPECIAL INSTALLATION REQUIREMENTS 1) PW1100G-JM & PW1100G/2-JM Engine design and operating limitations are defined in the Installation and Operating Manual, PWA-9851. 2) PW1400G-JM Engine design and operating limitations are defined in the Installation and Operating Manual, PWA-9914 3) The PW1133G-JM, PW1133G1-JM, PW1133G1R-JM, PW1133GA-JM, PW1133GAR-JM, PW1133GR-JM, PW1133GS-JM, PW1133GAS-JM, PW1133G1S-JM, PW1130G-JM, PW1130GS-JM, PW1129G-JM, PW1127G-JM, PW1127G1-JM, PW1127G1A-JM, PW1127G1B-JM,PW1127GA-JM, PW1124G-JM, PW1124G1-JM, PW1134G1/2-JM, PW1134GA/2-JM, PW1133G/2-JM, PW1133G1/2-JM, PW1133G1R/2-JM, PW1133GA/2-JM, PW1133GAR/2-JM, PW1133GH/2-JM, PW1133GR/2-JM, PW1133GS/2-JM, PW1133GAS/2-JM, PW1133G1S/2-JM, PW1130G/2-JM, PW1130GS/2-JM, PW1129G/2-JM, PW1127G/2-JM, PW1127G1/2-JM, PW1127G1A/2-JM, PW1127G1B/2-JM, PW1127GA/2-JM, PW1127GH/2-JM, PW1124G/2-JM, and PW1124G1/2-JM engine models have complied with the requirements of §§ 33.4 (A33.3(c)), 33.71(c)(4) and 33.201, and are therefore eligible for installation on Extended Operations (ETOPS) and Early ETOPS approved airplanes. The demonstrated diversion time is 180 minutes at MCT plus 15 minutes at hold power. Note that ETOPS eligibility does not constitute airplane or operational level approvals necessary to conduct ETOPS flights. 4) The PW1400G-JM Engine Series are not eligible for Extended Operations (ETOPS). 5) The minimum N1 certified for in-flight operation in icing conditions is 1,801 rpm. The Electronic Engine Control will prevent rotor speeds below this value while in flight. 6) The PW1100G-JM engine is certified with Time Limited Dispatch. Criteria pertaining to the engine control systems’ dispatch and maintenance requirements for PW1100G-JM engine models installed on the Airbus A319/A320/A321 Aircraft are specified in the PW1100G-JM Airworthiness Limitations Manual PN 5316993 and PWA-10958 “PW1100G-JM Turbofan Engine Electronic Engine Control System Fault Message and Dispatch Category Cross-Reference”. The PW1100G/2-JM engine is certified with Time Limited Dispatch. Criteria pertaining to the engine control systems’ dispatch and maintenance requirements for PW1100G/2-JM engine models installed on the Airbus A319/A320/A321 Aircraft are specified in Airworthiness Limitations Manual PN5316993 and PWA-12798 “PW1100G-JM GTFA Engine Electronic Engine Control System Fault Message and Dispatch Category Cross-Reference”. 7) The PW1400G-JM engine is certified with Time Limited Dispatch. Criteria pertaining to the engine control systems’ dispatch and maintenance requirements for PW1400G-JM engine models installed on the Irkut MC-21 Aircraft are specified in the PW1400G-JM Airworthiness Limitations Manual PN 5321241 and PWA-10958 “PW1100G-JM Turbofan Engine Electronic Engine Control System Fault Message and Dispatch Category Cross- Reference” 8) The PW1100G-JM & PW1100G/2-JM electromagnetic compatibility (EMC) protection requirements and electromagnetic interference, (EMI) emitted by the electronic engine control system, including cables, are specified in the Installation and Operating Manual, PWA-9851. 9) The PW1400G-JM electromagnetic compatibility (EMC) protection requirements and electromagnetic interference (EMI) emitted by the electronic engine control system, including cables, are specified in the Installation and Operating Manual, PWA-9914. 10) For the PW1100G-JM & PW1100G/2-JM, the Collins Aerospace (formerly UT Aerospace System- Aerostructures) Thrust Reverser Unit as specified in the Installation and Operating Manual, PWA-9851, is acceptable for use on the engine. The thrust reverser is not part of the engine type design and is certified as part of the aircraft. TCDS E00087EN Page 11 of 12 NOTE 11 – cont’d. SPECIAL INSTALLATION REQUIREMENTS 11) For the PW1400G-JM, the Spirit AeroSystems (formerly Shorts Brother’s) Thrust Reverser Unit as specified in the Installation and Operating Manual, PWA-9914, is acceptable for use on the engine. The thrust reverser is not part of the engine type design and is certified as part of the aircraft. NOTE 12. MANUFACTURER’S SERVICE BULLETINS OR OTHER INSTRUCTIONS COVERING MATTERS OF INTEREST Not Applicable NOTE 13. SPECIAL OPERATING PROCEDURES Requirements and limitations for ground operation in icing conditions are specified in the PW1100G-JM & PW1100G/2-JM Installation and Operating Manual, PWA-9851 and the PW1400G-JM Installation and Operating Manual, PWA-9914. NOTE 14. SPECIAL REPAIR OR OVERHAUL LIMITATIONS Not Applicable NOTE 15. APPLICABLE INSTALLATION, MAINTENANCE & OVERHAUL MANUALS 1) PW1100G-JM & PW1100G/2-JM Installation and Operating Manual, PWA-9851 2) PW1400G-JM Installation and Operating Manual, PWA-9914 3) The following PW1100G-JM & PW1100G/2-JM Engine Instructions for Continued Airworthiness (ICA’s) have been accepted by the FAA Engine Certification Office: a. PW1100G-JM & PW1100G/2-JM Airworthiness Limitations Manual PN 5316993, b. PW1100G-JM & PW1100G/2-JM Engine Maintenance Manual PN 5316994, c. PW1100G-JM & PW1100G/2-JM Engine Manual PN 5316992, d. PW1100G-JM & PW1100G/2-JM Clean, Inspect and Repair Manual PN 5315653, e. PW1100G-JM & PW1100G/2-JM Series Troubleshooting Manual PN 5323704, 4) Standard Practices Manual PN 585005 5) The following PW1400G-JM Engine Instructions for Continued Airworthiness (ICA’s) have been accepted by the FAA Engine Certification Office: a. PW1400G-JM Airworthiness Limitations Manual PN 5321241, b. PW1400G-JM Engine Maintenance Manual PN 5321242, c. PW1400G-JM Engine Manual PN 5321240, d. PW1400G-JM Clean, Inspect and Repair Manual PN 5321246, e. PW1400G-JM Series Troubleshooting Manual PN 5323215, f. Standard Practices Manual PN 585005 NOTE 16. IMPORT REQUIREMENTS Not Applicable NOTE 17. LIFE LIMITED PART INFORMATION 1) PW1100G-JM & PW1100G/2-JM Life limits for critical components and mandatory inspection requirements are specified in the PW1100G-JM & PW1100G/2-JM Airworthiness Limitation Manual PN 5316993. 2) PW1400G-JM Life limits for critical components and mandatory inspection requirements are specified in the PW1400G-JM Airworthiness Limitations Manual PN 5321241. NOTE 18. MILITARY MODEL INFORMATION Not Applicable NOTE 19. ROTOR SPEEDS Maximum permissible Low Pressure Rotor (N1): 10,047 rpm Maximum permissible High Pressure Rotor (N2): 22,300 rpm Power setting, power checks, and control of engine thrust output in all operations are based on Low Rotor Speed (N1). Fan Speed, (NFAN) is directly proportional to Low Rotor Speed (N1) by a gear ratio of 1:3.0625. Minimum Rotor Speeds: Rotor PW1100G-JM/PW1400G-JM PW1100G/2-JM Ground Flight Ground Flight N1 (rpm) 1,750 1,801 1,750 1,801 N2 (rpm) 12,400 12,400 12,823 12,823 TCDS E00087EN Page 12 of 12 NOTE 20. OUTPUT/PROPELLER SHAFT TORQUE LIMITS Not Applicable. NOTE 21. BLEED AIR EXTRACTION PROVISIONS PW1100G-JM & PW1100G/2-JM Maximum Permissible Bleed Extraction limits are specified in PW1100G-JM & PW1100G/2-JM Installation and Operating Manual PWA-9851 PW1400G-JM Maximum Permissible Bleed Extraction limits are specified in PW1400G-JM Installation and Operating Manual PWA-9914 NOTE 22. ROTOR DISK INTEGRITY AND ROTOR BLADE CONTAINMENT (where special requirements apply) Not Applicable. NOTE 23. EXHAUST EMISSIONS AND FUEL VENTING The following emissions standards promulgated in 14 CFR Part 34, Amendment 7A, effective May 24, 2024, and 40 CFR part 1031, effective December 23, 2022, have been complied with for the PW1133G-JM, PW1133G1-JM, PW1133G1R-JM, PW1133GA-JM, PW1133GAR-JM, PW1133GR-JM, PW1133GS-JM, PW1133GAS-JM, PW1133G1S-JM, PW1130G-JM, PW1130GS-JM, PW1129G-JM, PW1127G-JM, PW1127G1-JM, PW1127G1A-JM, PW1127G1B-JM, PW1127GA-JM, PW1124G-JM, PW1124G1-JM, PW1134G1/2-JM, PW1134GA/2-JM, PW1133G/2-JM, PW1133G1/2-JM, PW1133G1R/2-JM, PW1133GA/2-JM, PW1133GAR/2-JM, PW1133GH/2-JM, PW1133GR/2-JM, PW1133GS/2-JM, PW1133GAS/2-JM, PW1133G1S/2-JM, PW1130G/2-JM, PW1130GS/2-JM, PW1129G/2-JM, PW1127G/2-JM, PW1127G1/2-JM, PW1127G1A/2-JM, PW1127G1B/2-JM, PW1127GA/2-JM, PW1127GH/2-JM, PW1124G/2-JM, PW1124G1/2-JM, PW1431G-JM, PW1431GA-JM, PW1431GH-JM, PW1428G-JM, PW1428GA-JM, and PW1428GH-JM engine models: Fuel Venting Emission Standards: 14 CFR §§ 34.10(a) and 34.11; in addition, in addition, 40 CFR § 1031.30(b)(2). Carbon Monoxide (CO) Emission Standards: 14 CFR § 34.21(d)(l)(ii); in addition, in addition, 40 CFR § 1031.60(d). Hydrocarbons (HC) Emission Standards: 14 CFR § 34.21(d)(1)(i); in addition, 40 CFR § 1031.60(c) Oxides of Nitrogen (NOx) Emission Standards: 14 CFR § 34.23(b)(l); in addition, in addition, 40 CFR § 1031.60(e)(5). Non-volatile particulate nvPM mass concentration (nvPMMC): 14 CFR § 34.25(a)(1); in addition, 40 CFR § 1031.60(a)(6). Non-volatile particulate nvPM mass (nvPMmass) & nvPM number (nvPMnum): 14 CFR § 34.25(a)(2); in addition, 40 CFR § 1031.60(b)(2). In addition to the FAA’s finding of compliance based on the certification requirements defined in this TCDS, the engine manufacturer has declared that the ICAO emissions standards identified in Annex 16, Volume II, Fourth Edition, Amendment 10, effective July 20, 2020, have also been demonstrated for the following: • Part II, Chapter 2 for Fuel Venting • Part III, Chapter 2, Section 2.2.2 for Smoke Number • Part III, Chapter 2, Section 2.3.2 for Carbon Monoxide and Hydrocarbons • Part III, Chapter 2, Section 2.3.2 for Oxides of Nitrogen (also known as CAEP/8), and • Part III, Chapter 4, Section 4.2.2 for non-volatile Particulate Matter (also known as CAEP/10 & CAEP/11). ---END--- ``` ## ADs (18, in force first) - [AD 2025-26-04](https://openairdocs.org/ad/2025-26-04): Miscellaneous Hardware · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 15 more. Effective Feb 17, 2026 - [AD 2024-14-04](https://openairdocs.org/ad/2024-14-04): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G1-JM, PW1124G-JM and 9 more. Effective Aug 20, 2024 - [AD 2024-06-14](https://openairdocs.org/ad/2024-06-14): Turbine Engine Compressor Section · International Aero Engines PW1124G1-JM, PW1127G-JM, PW1127GA-JM and 4 more. Effective Jun 3, 2024 - [AD 2024-05-11](https://openairdocs.org/ad/2024-05-11): Turbine Engine Compressor Section; Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 15 more. Effective Apr 11, 2024 - [AD 2023-20-11](https://openairdocs.org/ad/2023-20-11): Turbine Engine Compressor Section · International Aero Engines PW1124G1-JM, PW1127G-JM, PW1127GA-JM and 4 more. Effective Nov 1, 2023 - [AD 2023-16-07](https://openairdocs.org/ad/2023-16-07): Turbine Section · International Aero Engines PW1122G-JM, PW1124G1-JM, PW1124G-JM and 13 more. Effective Aug 28, 2023 - [AD 2021-19-10](https://openairdocs.org/ad/2021-19-10): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Sep 27, 2021 - [AD 2020-08-04](https://openairdocs.org/ad/2020-08-04): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective May 21, 2020 - [AD 2020-05-28](https://openairdocs.org/ad/2020-05-28): Turbine Engine Accessory Drive · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Apr 21, 2020 - [AD 2020-06-02](https://openairdocs.org/ad/2020-06-02): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Apr 6, 2020 - [AD 2019-25-01](https://openairdocs.org/ad/2019-25-01): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Dec 16, 2019 - [AD 2019-06-01](https://openairdocs.org/ad/2019-06-01): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Apr 10, 2019 - [AD 2018-21-10](https://openairdocs.org/ad/2018-21-10): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Dec 12, 2018 - [AD 2018-22-02](https://openairdocs.org/ad/2018-22-02): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Dec 12, 2018 - [AD 2018-13-03](https://openairdocs.org/ad/2018-13-03): Turbine Engine Compressor Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Jul 11, 2018 - [AD 2022-19-15](https://openairdocs.org/ad/2022-19-15) (historical): Turbine Section · International Aero Engines PW1122G-JM, PW1124G1-JM, PW1124G-JM and 7 more. Effective Nov 7, 2022 - [AD 2019-11-08](https://openairdocs.org/ad/2019-11-08) (historical): Turbine Engine Accessory Drive · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 7 more. Effective Jun 28, 2019 - [AD 2018-24-01](https://openairdocs.org/ad/2018-24-01) (historical): Turbine Section · International Aero Engines PW1122G-JM, PW1124G-JM, PW1124G1-JM and 6 more. Effective Mar 15, 2019 ## Registered aircraft by registry model (OpenAirDocs) - [IAE PW1133GA-JM](https://openairdocs.org/engine/iae-pw1133ga-jm): 168 aircraft (registry code 34598) - [IAE PW1133G-JM](https://openairdocs.org/engine/iae-pw1133g-jm): 162 aircraft (registry code 34600) - [IAE PW1127G-JM](https://openairdocs.org/engine/iae-pw1127g-jm): 79 aircraft (registry code 34550) - [IAE PW1127GA-JM](https://openairdocs.org/engine/iae-pw1127ga-jm): 31 aircraft (registry code 34551) --- 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.