OpenAP engine properties
OpenAP / Junzi Sun · Retrieved 2026-09-05
LGPL-3.0; source dataset includedPRATT & WHITNEY
PW2040
Turbofan
ENGINE13 documented fields
OpenAP reference record 4PW073. Values describe the source configuration and test conditions. Fuel-flow modes are reference test points, not an in-flight fuel prediction. Dimensions and certified operating limits are not supplied by this dataset.
Reference thrust182020 N
Bypass ratio5.54 :1
Pressure ratio29.4 :1
Takeoff fuel flow1.752 kg/s
REFERENCE COVERAGELoading coverage…
PROVENANCE1 linked source
LAST RETRIEVED2026-09-05
View missing fields and source dates
Source editions
OpenAP engine properties ↗Edition / snapshot: Reference snapshot, September 2026Retrieved: 2026-09-05
Retrieval dates record when Owl obtained the data; they are not publication dates or proof that a specification is current. Where the edition contains only a snapshot date, the original publication date is not recorded.
01
Output
- Reference maximum thrustOpenAP engine dataset · 4PW073 · max_thrust
- 182,020 N
02
Architecture
- Bypass ratioOpenAP engine dataset · 4PW073 · bpr
- 5.54 :1
- Overall pressure ratioOpenAP engine dataset · 4PW073 · pr
- 29.4 :1
03
Fuel flow
- Approach fuel flowOpenAP engine dataset · 4PW073 · ff_app
- 0.496 kg/s
- Climb-out fuel flowOpenAP engine dataset · 4PW073 · ff_co
- 1.445 kg/s
- Idle fuel flowOpenAP engine dataset · 4PW073 · ff_idl
- 0.159 kg/s
- Reference LTO fuelOpenAP engine dataset · 4PW073 · fuel_lto
- 631 kg
- Takeoff fuel flowOpenAP engine dataset · 4PW073 · ff_to
- 1.752 kg/s
04
Cruise reference
- Reference cruise MachOpenAP engine dataset · 4PW073 · cruise_mach
- 0.85
- Reference cruise SFCOpenAP engine dataset · 4PW073 · cruise_sfc
- 0.0165 kg/(kN·s)
- Reference cruise altitudeOpenAP engine dataset · 4PW073 · cruise_alt
- 35,000 ft
- Reference cruise thrustOpenAP engine dataset · 4PW073 · cruise_thrust
- 28,913 N
05
Provenance
- Source manufacturer nameHistorical source label retained.
- Pratt & Whitney
Aircraft connections
Exact engine-name matches in the aircraft catalogue. This is not a complete installation or certification list.
No exact aircraft connection documented in this dataset.
Dimensions, dry weight, shaft-power ratings and certified limits are not documented in this engine dataset.
Sources & context
Reference values vary with model, rating and conditions. Consult the relevant manufacturer documentation for certified specifications.