Manufacturer Serial Number | *** | *** | |||||||||
*** | *** | *** | *** |
Manufacturer Serial Number | *** | |||||||
*** | *** | *** |
THE BOEING COMPANY | UNITED AIRLINES, INC. | |||||||
/s/ Irma L. Krueger | /s/ Gerald Laderman | |||||||
Signature | Signature | |||||||
Irma L. Krueger | Gerald Laderman | |||||||
Printed Name | Printed Name | |||||||
Attorney-in-Fact | Executive Vice-President and Chief Financial Officer | |||||||
Title | Title |
ARTICLES | SA NUMBER | |||||||||||||
Article 1. | Quantity, Model and Description | |||||||||||||
Article 2. | Delivery Schedule | |||||||||||||
Article 3. | Price | |||||||||||||
Article 4. | Payment | |||||||||||||
Article 5. | Additional Terms | |||||||||||||
TABLE | ||||||||||||||
1. | 737-*** Aircraft Delivery, Description, Price and *** | SA-6 & SA-8§4.1 | ||||||||||||
1. | *** 737-*** Aircraft Delivery, Description, Price and *** | SA-9 | ||||||||||||
1 | *** 737-*** Aircraft Delivery, Description, Price and *** | SA-7 & SA-8§4.1 | ||||||||||||
1. | 737-*** Aircraft Delivery, Description, Price and *** | SA-7 & SA-8§4.1 | ||||||||||||
1. | 737-*** Aircraft Delivery, Description, Price and *** | SA-5 & SA-8§4.1 | ||||||||||||
1. | *** 737-*** Aircraft Delivery, Description, Price and *** | SA-8 | ||||||||||||
1. | 737-*** Aircraft Delivery, Description, Price and *** | SA-5 & SA-8§4.1 | ||||||||||||
1. | *** 737-*** Aircraft Delivery, Description, Price and *** | SA-6 & SA-8§4.1 | ||||||||||||
1. | *** 737-*** Aircraft Delivery, Description, Price and *** | SA-6 & SA-8§4.1 | ||||||||||||
2. | 737-*** Aircraft Delivery, Description, Price and *** | SA-9 | ||||||||||||
TABLE OF CONTENTS, CONTINUED | ||||||||||||||
EXHIBITS | SA NUMBER |
A | 737-8 Aircraft Configuration | SA-7 | ||||||||||||
A | 737-9 Aircraft Configuration | SA-1 | ||||||||||||
A | 737-10 *** Aircraft Configuration | SA-5 | ||||||||||||
A | 737-10 Aircraft Configuration | SA-6 | ||||||||||||
B. | Aircraft Delivery Requirements and Responsibilities |
SUPPLEMENTAL EXHIBITS | SA NUMBER | |||||||
AE1. | ***/Airframe and *** Features for the 737MAX Aircraft | |||||||
BFE1. | BFE Variables 737-8 Aircraft | SA-2 | ||||||
BFE1. | BFE Variables 737-9 Aircraft | SA-1 | ||||||
BFE1. | BFE Variables 737-10 Aircraft | SA-2 | ||||||
EE1. | Engine Warranty and *** | |||||||
SLP1. | Service Life Policy Components |
TABLE OF CONTENTS, CONTINUED | ||||||||
LETTER AGREEMENTS | SA NUMBER | |||||||
UAL-PA-04761-LA-1801463R3 | *** Matters | SA-6 | ||||||
UAL-PA-04761-LA-1801464 | Demonstration Flight Waiver | |||||||
UAL-PA-04761-LA-1801465R2 | Open Matters 737-9 and 737-10 Aircraft | SA-5 | ||||||
UAL-PA-04761-LA-1801466 | Seller Purchased Equipment | SA-5 | ||||||
UAL-PA-04761-LA-1801467R5 | Special Matters – 737 MAX Aircraft | SA-9 | ||||||
UAL-PA-04761-LA-1801468 | *** | |||||||
UAL-PA-04761-LA-1801469R3 | *** | SA-8 | ||||||
UAL-PA-04761-LA-1801470 | Privileged and Confidential Matters | |||||||
UAL-PA-04761-LA-1801471 | AGTA Matters | |||||||
UAL-PA-04761-LA-1801472 | Assignment Matters | |||||||
UAL-PA-04761-LA-1801473 | 737-10 Aircraft *** | |||||||
UAL-PA-04761-LA-1801474R1 | *** for the 737-10 Aircraft | SA-7 | ||||||
UAL-PA-04761-LA-1801475 | Loading of Customer Software | |||||||
UAL-PA-04761-LA-1801476 | Installation of Cabin Systems Equipment | |||||||
UAL-PA-04761-LA-1801477 | Special Customer Support Matters | |||||||
UAL-PA-04761-LA-1801478R1 | Delivery *** Matters | SA-6 | ||||||
UAL-PA-04761-LA-1807022R5 | *** Aircraft – 737-*** | SA-6 & SA-8§4.1 | ||||||
UAL-PA-04761-LA-1807420R1 | 737-*** and 737-*** Aircraft Model *** | SA-6 & SA-8§4.1 | ||||||
UAL-PA-04761-LA-1807490R1 | 737-*** Aircraft and 737-*** Aircraft *** | SA-2 |
UAL-PA-04761-LA-1900347 | 737-8 *** | SA-6 | ||||||
UAL-PA-04761-LA-2001831R1 | Certain Special Matters | SA-4 | ||||||
TABLE OF CONTENTS, CONTINUED | ||||||||
LETTER AGREEMENTS | SA NUMBER | |||||||
UAL-PA-04761-LA-2100095 | *** Matters for the 737-8 *** Aircraft | SA-5 | ||||||
UAL-PA-04761-LA-2100096R1 | Certain Special Matters for the 737-*** Aircraft and for the *** 737-*** Aircraft | SA-7 | ||||||
UAL-PA-04761-LA-2100136 | Open Matters Relating to *** Model 737-8 Aircraft | SA-5 | ||||||
UAL-PA-04761-LA-2100718R1 | Special Matters Relating to *** 737-9 Aircraft | SA-6 | ||||||
UAL-PA-04761-LA-2103100 | Airline Operational Efficacy Matters | SA-6 | ||||||
UAL-PA-04761-LA-2103236 | *** | SA-6 | ||||||
UAL-PA-04761-LA-2104314 | *** for Certain 737-*** Aircraft | SA-9 | ||||||
UAL-PA-04761-LA-2104366 | *** for 737-*** Aircraft *** | SA-9 | ||||||
UAL-PA-04761-LA-2104367 | *** for 737-*** Aircraft *** | SA-9 | ||||||
UAL-PA-04761-LA-2105142 | Certain Special Matters for the 737-*** Aircraft | SA-9 | ||||||
UAL-PA-04761-LA-2105143 | Open Matters Relating to *** Model 737-*** Aircraft | SA-9 |
SUPPLEMENTAL AGREEMENTS | DATED AS OF | ||||
Supplemental Agreement No. 1 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . September 25, 2018 | ||||
Supplemental Agreement No. 2 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . December 12, 2018 | ||||
Supplemental Agreement No. 3 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . March 20, 2020 | ||||
Supplemental Agreement No. 4 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . June 30, 2020 | ||||
Supplemental Agreement No. 5 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . February 26, 2021 | ||||
Supplemental Agreement No. 6 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . June 27, 2021 | ||||
Supplemental Agreement No. 7 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . August 12, 2021 | ||||
Supplemental Agreement No. 8 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . September 8, 2021 | ||||
Supplemental Agreement No. 9 . . . . . . . . . . . . . | . . . . . . . . . . . . . . . . November 30, 2021 |
Airframe Model/MTOW: | 737-*** | *** pounds | ^ | Detail Specification: | *** | ||||||||||||||||||||||||||||||
Engine Model/Thrust: | *** | *** pounds | + | Airframe Price Base Year/*** Formula: | *** | *** | |||||||||||||||||||||||||||||
Airframe Price: | *** | Engine Price Base Year/*** Formula: | *** | *** | |||||||||||||||||||||||||||||||
*** Features: | *** | ||||||||||||||||||||||||||||||||||
Sub-Total of Airframe and Features: | *** | Airframe *** Data: | |||||||||||||||||||||||||||||||||
Engine Price (Per Aircraft): | *** | Base Year Index (ECI): | *** | ||||||||||||||||||||||||||||||||
Aircraft Basic Price (Excluding BFE/SPE): | *** | Base Year Index (CPI): | *** | ||||||||||||||||||||||||||||||||
Buyer Furnished Equipment (BFE) Estimate: | *** | ||||||||||||||||||||||||||||||||||
Seller Purchased Equipment (SPE) Estimate: | *** | ||||||||||||||||||||||||||||||||||
Deposit per Aircraft: | *** | ||||||||||||||||||||||||||||||||||
# of Aircraft | *** Delivery Month | *** | Manufacturer Serial Number | *** Forecast | Actual or Nominal Delivery **** | *** Estimate | *** Per Aircraft (Amts. Due/*** Prior to Delivery): | ||||||||||||||||||||||||||||
Number of | Factor | *** Base | *** | *** | *** | *** | |||||||||||||||||||||||||||||
Aircraft | (Airframe) | Price Per A/P | *** | *** | *** | *** | |||||||||||||||||||||||||||||
*** | *** | *** | *** | *** | *** | *** | *** | *** | *** | *** | *** | ||||||||||||||||||||||||
Total: | *** | ||||||||||||||||||||||||||||||||||
* Nominal delivery *** pursuant to Letter Agreement number UAL-PA-04761-LA-1801465R2 entitled "Open Matters 737-*** Aircraft", as may be subsequently amended. | |||||||||||||||||||||||||||||||||||
Note: Serial Numbers above, if any are included, are provided as guidance only and are subject to change until delivery. | |||||||||||||||||||||||||||||||||||
^ -*** | |||||||||||||||||||||||||||||||||||
+ -*** |
UAL-PA-04761 APR: 117225.TXT | Boeing / United Airlines, Inc. Proprietary | *** 737-*** Aircraft | |||||||||
Table 1, SA-9, Page, | 1 |
Airframe Model/MTOW: | 737-*** | *** pounds | ^ | Detail Specification: | *** | |||||||||||||||||||||||||||
Engine Model/Thrust: | *** | *** pounds | + | Airframe Price Base Year/*** Formula: | *** | *** | ||||||||||||||||||||||||||
Airframe Price: | *** | Engine Price Base Year/*** Formula: | *** | *** | ||||||||||||||||||||||||||||
*** Features: *** | *** | |||||||||||||||||||||||||||||||
Sub-Total of Airframe and Features: | *** | Airframe *** Data: | ||||||||||||||||||||||||||||||
Engine Price (Per Aircraft): | *** | Base Year Index (ECI): | *** | |||||||||||||||||||||||||||||
Aircraft Basic Price (Excluding BFE/SPE): | *** | Base Year Index (CPI): | *** | |||||||||||||||||||||||||||||
Buyer Furnished Equipment (BFE) Estimate: | *** | |||||||||||||||||||||||||||||||
Seller Purchased Equipment (SPE) Estimate: | *** | |||||||||||||||||||||||||||||||
Non-Refundable Deposit per Aircraft: | *** | |||||||||||||||||||||||||||||||
^ -*** | ||||||||||||||||||||||||||||||||
+ -*** | ||||||||||||||||||||||||||||||||
Applicability pursuant to § 3.1 of Letter Agreement UAL-PA-04761-LA-2105143 entitled "Open Matters Relating to *** Model 737-*** Aircraft". | ||||||||||||||||||||||||||||||||
*** | *** Forecast | *** Estimate | *** Per Aircraft (Amts. Due/*** Prior to Delivery): | |||||||||||||||||||||||||||||
Delivery | Number of | Factor | *** Base | *** | *** | *** | *** | |||||||||||||||||||||||||
Date | Aircraft | (Airframe) | Price Per A/P | *** | *** | *** | *** | |||||||||||||||||||||||||
1 | *** | *** | *** | *** | *** | *** | *** | *** | *** | |||||||||||||||||||||||
1 |
UAL-PA-04761 APR: 117225; Sec.2.2 | Boeing / United Airlines, Inc. Proprietary | 737-*** Aircraft | |||||||||
SA-9, Table 2: 737-*** Aircraft, Page | 1 |
The Boeing Company P.O. Box 3707 Seattle, WA 98124-2207 |
Table Reference | Description | Quantity of Aircraft | ||||||
1 | 737-*** Aircraft Delivery, Description, Price and *** | *** | ||||||
1 | *** 737-*** Aircraft Delivery, Description, Price and *** | *** | ||||||
Total |
Aircraft Type | *** Number | Description | *** | *** | Quantity of 737-*** Aircraft | ||||||||||||
737-8 | *** | *** | *** | *** | *** |
THE BOEING COMPANY | |||||
By: | /s/ Irma L. Krueger | ||||
Its: | Attorney-in-Fact | ||||
ACCEPTED AND AGREED TO this | ||||||||
Date: | November 30, 2021 | |||||||
UNITED AIRLINES, INC. | ||||||||
By: | /s/ Gerald Laderman | |||||||
Its: | Executive Vice-President and Chief Financial Officer |
THE BOEING COMPANY | |||||
By: | /s/ Irma L. Krueger | ||||
Its: | Attorney-in-Fact |
The Boeing Company P.O. Box 3707 Seattle, WA 98124-2207 |
ACCEPTED AND AGREED TO this | |||||
Date: | November 30, 2021 | ||||
UNITED AIRLINES, INC. | |||||
By: | /s/ Gerald Laderman | ||||
Its: | Executive Vice President and Chief Financial Officer |
Manufacturer Serial Number | |||||
*** | *** |
The Boeing Company P.O. Box 3707 Seattle, WA 98124-2207 |
THE BOEING COMPANY | |||||
By: | /s/ Irma L. Krueger | ||||
Its: | Attorney-in-Fact | ||||
ACCEPTED AND AGREED TO this | ||||||||
Date: | November 30, 2021 | |||||||
UNITED AIRLINES, INC. | ||||||||
By: | /s/ Gerald Laderman | |||||||
Its: | Executive Vice-President and Chief Financial Officer |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
The runway slope is *** percent uphill. | |||||
The minimum level off height is *** feet. | |||||
The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: | |||||
Height Distance 1. *** feet *** feet 2. *** feet *** feet 3. *** feet *** feet 4. *** feet *** feet 5. *** feet *** feet 6. *** feet *** feet 7. *** feet *** feet | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. |
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at eastbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds |
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
` | The minimum level off height is *** feet. | ||||
The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: |
Height Distance 1. *** feet *** feet 2. *** feet *** feet 3. *** feet *** feet 4. *** feet *** feet 5. *** feet *** feet 6. *** feet *** feet | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. | ||||
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at westbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. |
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
The runway slope is *** percent downhill. | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. | ||||
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at westbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. |
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
The headwind is *** knots. | |||||
The runway slope is *** percent downhill. | |||||
The minimum level off height is *** feet. | |||||
The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: | |||||
Height Distance 1. *** feet *** feet | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. | ||||
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. |
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at eastbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds |
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Block Fuel: | The block fuel is defined as the sum of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise, descent, approach and landing maneuver, and taxi-in. | ||||
Takeoff: | The airport altitude is sea level. | ||||
The takeoff gross weight is not limited by the airport conditions. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. |
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is standard day during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at westbound ICAO RVSM cruise altitudes. | |||||
The temperature is standard day during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is standard day during descent. | |||||
Minimum flight idle thrust is used during descent. |
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is sea level. |
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
2.5.7 737-8 Weight Summary - United Airlines, Inc. | |||||||||||||||||
pounds | |||||||||||||||||
Standard Model Specification Manufacturer's Empty Weight (MEW) | *** | ||||||||||||||||
Configuration Specification *** | |||||||||||||||||
*** Tourist Class Passengers | |||||||||||||||||
*** Engines | |||||||||||||||||
*** | |||||||||||||||||
United Airlines, Inc. MEW | *** | ||||||||||||||||
Standard and Operational Items Allowance | *** | ||||||||||||||||
(Paragraph 2.5.8) | |||||||||||||||||
United Airlines, Inc. OEW | *** | ||||||||||||||||
quantity | pounds | pounds | |||||||||||||||
***: | *** | ||||||||||||||||
*** | *** | *** |
quantity | pounds | pounds | pounds | |||||||||||
Standard Items Allowance | *** | |||||||||||||
Unusable Fuel | *** | |||||||||||||
Oil | *** | |||||||||||||
Oxygen Equipment | *** | |||||||||||||
Miscellaneous Equipment | *** | |||||||||||||
Galley Structure & Fixed Inserts | *** | |||||||||||||
Operational Items Allowance | *** | |||||||||||||
Crew and Crew Baggage | *** | |||||||||||||
Flight Crew | *** | *** | ||||||||||||
Cabin Crew | *** | *** | ||||||||||||
Crew Baggage | *** | *** | ||||||||||||
Catering Allowance & Removable Inserts | *** | |||||||||||||
First Class | *** | *** | ||||||||||||
Economy Class | *** | *** | ||||||||||||
Passenger Service Equipment | *** | *** | ||||||||||||
Potable Water - *** USG | *** | |||||||||||||
Waste Tank Disinfectant | *** | |||||||||||||
Emergency Equipment (Including Overwater Equipment) | *** | |||||||||||||
Total Standard and Operational Items Allowance | *** |
The Boeing Company P.O. Box 3707 Seattle, WA 98124-2207 |
THE BOEING COMPANY | |||||
By: | /s/ Irma L. Krueger | ||||
Its: | Attorney-in-Fact | ||||
ACCEPTED AND AGREED TO this | ||||||||
Date: | November 30, 2021 | |||||||
UNITED AIRLINES, INC. | ||||||||
By: | /s/ Gerald Laderman | |||||||
Its: | Executive Vice-President and Chief Financial Officer |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
The runway slope is *** percent uphill. | |||||
The minimum level off height is *** feet. | |||||
The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: | |||||
Height Distance 1. *** feet *** feet 2. *** feet *** feet 3. *** feet *** feet 4. *** feet *** feet 5. *** feet *** feet 6. *** feet *** feet 7. *** feet *** feet | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. |
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at eastbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds |
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
` | The minimum level off height is *** feet. | ||||
The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: |
Height Distance 1. *** feet *** feet 2. *** feet *** feet 3. *** feet *** feet 4. *** feet *** feet 5. *** feet *** feet 6. *** feet *** feet | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. | ||||
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at westbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. |
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
The runway slope is *** percent downhill. | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. | ||||
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at westbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. |
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Takeoff: | The airport altitude is *** feet. | ||||
The airport temperature is ***°F. | |||||
The runway length is *** feet. | |||||
The headwind is *** knots. | |||||
The runway slope is *** percent downhill. | |||||
The minimum level off height is *** feet. | |||||
The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: | |||||
Height Distance 1. *** feet *** feet | |||||
Takeoff performance is based on an alternate forward center of gravity limit of *** percent of the mean aerodynamic chord. | |||||
Maximum takeoff thrust is used for the takeoff. | |||||
The takeoff gross weight will conform to FAA Regulations. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. | ||||
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. |
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is ***°C during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at eastbound ICAO RVSM cruise altitudes. | |||||
The temperature is ***°C during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is ***°C during descent. | |||||
Minimum flight idle thrust is used during descent. | |||||
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is *** feet. | |||||
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds |
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
Stage Length: | The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. | ||||
Block Fuel: | The block fuel is defined as the sum of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise, descent, approach and landing maneuver, and taxi-in. | ||||
Takeoff: | The airport altitude is sea level. | ||||
The takeoff gross weight is not limited by the airport conditions. | |||||
Climbout Maneuver: | Following the takeoff to *** feet, the Aircraft retracts landing gear, climbs to *** feet above the departure airport altitude and accelerates to the recommended speed while retracting flaps. |
Climb: | The Aircraft climbs from the initial climb altitude to *** feet altitude at the recommended speed. | ||||
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. | |||||
The climb continues at the recommended climb speed for minimum block fuel to the final climb altitude. | |||||
The temperature is standard day during climb. | |||||
Maximum climb thrust is used during climb. | |||||
Cruise: | The Aircraft cruises at *** Mach number. | ||||
The Aircraft cruises at westbound ICAO RVSM cruise altitudes. | |||||
The temperature is standard day during cruise. | |||||
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used. | |||||
Descent: | The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination airport altitude. | ||||
Throughout the descent, the cabin pressure is controlled to a maximum rate of descent equivalent to *** feet per minute at sea level. | |||||
The temperature is standard day during descent. | |||||
Minimum flight idle thrust is used during descent. |
Approach and Landing Maneuver: | The Aircraft decelerates to the final approach speed while extending flaps and landing gear, then descends and lands. | ||||
The destination airport altitude is sea level. |
Fixed Allowances: | For the purpose of this *** and for the purpose of establishing compliance with this ***, the following will be used as fixed quantities and allowances: | ||||
Taxi-Out: Fuel *** pounds | |||||
Takeoff and Climbout Maneuver: Fuel *** pounds Distance *** nautical miles | |||||
Approach and Landing Maneuver: Fuel *** pounds | |||||
Taxi-In (will be consumed from the reserve fuel): Fuel *** pounds | |||||
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** pounds | |||||
For information purposes, the reserve fuel is based on a hold equivalent to *** minutes at *** feet above sea level on a standard day at the Maximum Landing Weight. |
2.5.7 737-8 Weight Summary - United Airlines, Inc. | |||||||||||||||||
pounds | |||||||||||||||||
Standard Model Specification Manufacturer's Empty Weight (MEW) | *** | ||||||||||||||||
Configuration Specification *** | |||||||||||||||||
*** Tourist Class Passengers | |||||||||||||||||
*** Engines | |||||||||||||||||
*** | |||||||||||||||||
*** | *** | ||||||||||||||||
United Airlines, Inc. MEW | *** | ||||||||||||||||
Standard and Operational Items Allowance | *** | ||||||||||||||||
(Paragraph 2.5.8) | |||||||||||||||||
United Airlines, Inc. OEW | *** | ||||||||||||||||
quantity | pounds | pounds | |||||||||||||||
*** | *** | ||||||||||||||||
*** | *** | *** |
quantity | pounds | pounds | pounds | |||||||||||
Standard Items Allowance | *** | |||||||||||||
Unusable Fuel | *** | |||||||||||||
Oil | *** | |||||||||||||
Oxygen Equipment | *** | |||||||||||||
Miscellaneous Equipment | *** | |||||||||||||
Galley Structure & Fixed Inserts | *** | |||||||||||||
Operational Items Allowance | *** | |||||||||||||
Crew and Crew Baggage | *** | |||||||||||||
Flight Crew | *** | *** | ||||||||||||
Cabin Crew | *** | *** | ||||||||||||
Crew Baggage | *** | *** | ||||||||||||
Catering Allowance & Removable Inserts | *** | |||||||||||||
First Class | *** | *** | ||||||||||||
Economy Class | *** | *** | ||||||||||||
Passenger Service Equipment | *** | *** | ||||||||||||
Potable Water - *** USG | *** | |||||||||||||
Waste Tank Disinfectant | *** | |||||||||||||
Emergency Equipment (Including Overwater Equipment) | *** | |||||||||||||
Total Standard and Operational Items Allowance | *** |
The Boeing Company P.O. Box 3707 Seattle, WA 98124-2207 |
*** | *** | ||||
1.1737-8 Aircraft ***. At the time of delivery of each *** Aircraft, Boeing *** to Customer *** (737-8 Aircraft ***). | *** | ||||
1.2737-8 ***. At the time of delivery of each *** Aircraft, Boeing *** to Customer *** (737-8 ***). Boeing represents that the *** of this 737-8 *** is consistent with the terms of Letter Agreement 6-1162-KKT-080, as amended. | *** | ||||
1.3*** 737-8 ***. *** | *** | ||||
1.4 *** | *** | ||||
1.5*** | *** |
THE BOEING COMPANY | |||||
By: | /s/ Irma L. Krueger | ||||
Its: | Attorney-in-Fact | ||||
ACCEPTED AND AGREED TO this | ||||||||
Date: | November 30, 2021 | |||||||
UNITED AIRLINES, INC. | ||||||||
By: | /s/ Gerald Laderman | |||||||
Its: | Executive Vice-President and Chief Financial Officer |
The Boeing Company P.O. Box 3707 Seattle, WA 98124-2207 |
*** | *** | *** | ||||||
*** | *** | *** |
THE BOEING COMPANY | |||||
By: | /s/ Irma L. Krueger | ||||
Its: | Attorney-in-Fact | ||||
ACCEPTED AND AGREED TO this | ||||||||
Date: | November 30, 2021 | |||||||
UNITED AIRLINES, INC. | ||||||||
By: | /s/ Gerald Laderman | |||||||
Its: | Executive Vice-President and Chief Financial Officer |