Attchmnt_J-1_SOW_R.081621.docx

SIR: 6973GH-20-R-00067

Attachment J-1 (Rev. 08/16/2021)

ATTACHMENT J-1 - STATEMENT OF WORK (SOW)

General Introduction This FAA has a requirement for the acquisition of used Bombardier Challenger 605 and/or 650 aircraft. The FAA will procure a total of four (4) aircraft. Each aircraft will be procured on a separate contract. The government does not have a preference between Challenger 605 aircraft or Challenger 650 aircraft. Aircraft must meet the FAA’s minimum requirements defined in C.2.1. C.2.1 also provides FAA preferences regarding age, flight hours/landings, avionics, maintenance records, basing, recommended service bulletins and programs. The FAA will acquire aircraft on an “as-is, where-is” basis.

“Aircraft” means the Airframe, the Engines, the Parts, the Ancillary Items, and the Aircraft Documents.

“Airframe” means that certain ___________________________ (year, make, model) aircraft, bearing manufacturer's serial number ______, and Federal Aviation Administration registration number N_______ , together with any and all Parts incorporated or installed in or attached thereto or otherwise in Seller's possession or control.

“Engines” means two (2) ______________________ series engines bearing manufacturer's serial numbers __________ and ____________ (described on the International Registry as ___________ bearing manufacturer’s serial numbers _________ and __________) together with any and all Parts incorporated or installed in or attached thereto or otherwise in Seller's possession and control.

“Title agent” means a person or entity holding documents in a transfer of real property, acting for both parties pursuant to instructions.

“Parts” means all appliances, components, parts, avionics, instruments, appurtenances, accessories, furnishings or other equipment of whatever nature (other than complete Engines or engines) incorporated or installed in or attached to the Airframe or any Engine, and all spare parts in Seller's possession or control.

“Ancillary Items” means all tool kits, spare parts, rotables (including life rafts) support equipment, engine covers, loose equipment and other equipment of whatever nature that is associated with the Airframe and the Engines.

“Aircraft Documents” means a valid United States Standard Airworthiness Certificate, and all logbooks, Airworthiness Directive compliance documents, major repair/major alternation documents, Airplane Fight Manual (AFM), AFM supplements, manuals for installed equipment, maintenance and inspection records, parts catalogs, yellow tags, wiring diagrams, completion/refurbishment records, 8130-3s or equivalent for all life limited components, burn certifications, or required STCs and other technical documentation pertaining to the Airframe or Engine that are in Seller's possession or control.

“International Registry” means the International Registry of Mobile Assets established pursuant to the Cape Town Treaty.

Scope of Work This SOW defines requirements to provide a Challenger 605 or 650 Aircraft.

Aircraft The Seller must provide a Challenger aircraft that meets the following minimum requirements. Aircraft that do not meet minimum requirements will not be accepted. The FAA will purchase aircraft meeting minimum requirements on an “as-is, where-is” basis. Aircraft meeting some or all of the FAA preferred requirements will be considered favorable.

Aircraft General Requirements

8 – 12 seats 10 – seat standard interior

Avionics/Comm/Nav/Instrumentation

Aircraft Ownership, Operations & Basing

Maintenance Documentation, Records and Programs

The Seller must complete Exhibit A, Aircraft Description and provide the specific Aircraft defined herein.

Warranty The seller must transfer all remaining assignable manufacturer’s warranties (express or implied) which are still in effect with respect to the aircraft, engines and all avionics to the FAA upon final acceptance of the aircraft.

Damage History The aircraft must have no damage history beyond minor, non-structural damage. “Damage History” shall mean damage, the repair of which would constitute a “major repair” as such term is defined in 14 C.F.R. Part 43, Appendix A, Paragraph (b).

Aicraft Inspection Pre-Purchase Inspection The FAA shall conduct a pre-purchase inspection of the aircraft. The inspection will be conducted at the Original Equipment Manufacturer (OEM) or OEM Authorized Service Facility. The scope of the pre-purchase inspection may include, but is not limited to, a visual inspection, aircraft document review, avionics, APU and other system checks, engine runs and engine borescope inspections. The inspection shall be used to determine that the aircraft is in the Delivery Condition, as defined hereunder. Solely as a condition precedent to the FAA’s obligation to complete the Closing and not as a representation or warranty of Seller that survives Closing in any way, Seller agrees that the FAA will not be obligated to purchase and accept delivery and conveyance of title to the aircraft from Seller at Closing until the following conditions have been met, which will be referred to collectively as the “Delivery Condition”:

(1) Aircraft in compliance with minimum and proposed preferred requirements as described in Exhibit A with all inspection discrepancies resolved;

(2) being airworthy, fully serviceable with all systems and parts working normally within their required limits;

(3) being free from any corrosion;

(4) complying with all airworthiness directives affecting the aircraft issued by the FAA and all alert service bulletins with a compliance date not less than 180 days after the delivery date;

(5) having all calendar, hourly and cycle inspections as recommended by the manufacturer's maintenance program current and complied with and all hourly, calendar and cycle limited components shall be within the limits in accordance with the manufacturer's maintenance program;

(6) being free and clear of any mortgage, charge, pledge, lien or other encumbrance;

(7) with all complete and continuous original aircraft documents in English;

(8) with no loaner or rental equipment installed thereon or thereto; and

(9) U.S. certificate of airworthiness or with an export certificate of airworthiness in favor of the United States of America (if deemed reasonably necessary by the FAA).

At the expense of the FAA, the FAA may conduct pre-purchase inspection flight(s) of not more than three (3) hours duration for the purpose of demonstrating that the aircraft is in the Delivery Condition. The Seller’s pilot, or a pilot designated by the Seller, shall serve as pilot in command and maintain command and control of the Aircraft at all times during the pre-purchase inspection flight. An FAA pilot will serve as second in command during the pre-purchase inspection flight. The FAA may also have one (1) additional observer on the pre-purchase inspection flight. Upon request, the FAA pilot will provide the documentation required by the Seller to add the pilot to Seller’s insurance for the pre-purchase inspection flight. Pre-purchase inspection flights will be conducted during the pre-purchase inspection and may be conducted at final acceptance at the discretion of the FAA. When conducting pre-purchase inspection flights, the FAA will use Exhibit E, Pre-Purchase Aircraft Flight Profile Checklist to conduct system checks to verify all systems are operational and function within the aircraft manufacturers design limits.

As soon as reasonably practicable after completion of the Inspection, Seller will, at Seller’s sole cost and expense, cause all Airworthiness Discrepancies to be corrected in accordance with the Aircraft's maintenance manual, as determined by the Inspection Facility.

The Seller must deliver the aircraft to the FAA designated inspection facility in accordance with the delivery schedule in Section F. The FAA shall pay all costs and expenses associated with the inspection. FAA shall pay or reimburse Seller the costs incurred in connection with the repositioning cost of the aircraft to and from the FAA’s designated inspection facility and conducting pre-purchase inspection flights, which shall include the cost of fuel, crew time and incidental expenses.

Aircraft Delivery and Acceptance Aircraft Acceptance Within three (3) business days after completion of the pre-purchase inspection, FAA shall notify Seller of FAA's acceptance or rejection of the aircraft in the form of the Pre-Purchase Inspection Report (Exhibit B).

The FAA's Pre-Purchase Inspection Report may include a list of inspection discrepancies which Seller must correct, at Seller's expense, in order for the Aircraft to comply with the Delivery Conditions. The Seller must correct all discrepancies within 10 business days, unless otherwise agreed to by the FAA Contracting Officer. The FAA reserves the right to reinspect the aircraft and conduct a post inspection flight to verify discrepancies have been properly rectified.

For the avoidance of doubt, failure or refusal by Seller to correct the inspection discrepancies identified by FAA in the Pre-Purchase Inspection Report, lacking a certificate of airworthiness or an export certificate of airworthiness in favor of the United States of America (if deemed reasonably necessary by the FAA), shall be considered an Event of Default of Seller, subject to Section H.8.

Delivery and Closing Date and Time of Closing. The Closing shall occur within three (3) business days after the inspection discrepancies have been rectified (such date being the “Closing Date”) and shall take place at a delivery location within the continental United States, designated by the Seller. Delivery shall be confirmed by the parties in writing by use of Exhibit C, Aircraft Delivery Receipt.

Condition of Aircraft at Closing. Seller shall deliver the aircraft to FAA at closing:

(1) meets all delivery condition requirements stated in Section C2.2.1;

(2) airworthy with a valid FAA Certificate of Airworthiness and any and all discrepancies identified in inspection rectified;

(3) with no Damage History in accordance with C2.1.3 as attested by the Sellers Representations and Warranties (Section K);

(4) if the FAA elects to transfer maintenance program, the Seller must be current on applicable subscriptions or maintenance programs, provided, however, that the responsibility and cost for the transfer of programs shall be borne solely by FAA;

(5) with an undated, executed Exhibit D, Warranty Bill of Sale, in duplicate;

(6) with an undated, executed FAA Bill of Sale, in duplicate;

(7) with an export certificate of airworthiness in favor of the United States of America (if deemed reasonably necessary by the FAA); and

(8) with all original and complete, correct, continuous and up-to-date Aircraft Documents printed or published in English, and maintained in accordance with industry standards and the Federal Aviation Regulation (FAR).

Additional Seller Covenants. Seller covenants and agrees as follows:

Sellers Service Program Contracts. Effective as of the Closing and if requested by the FAA, Seller shall cooperate with FAA to cause to be transferred and assigned to FAA any of its rights with respect to any other repair or maintenance agreements or programs relating to the aircraft, and/or engines that are in effect and transferrable or assignable, including without limitation, any subscriptions maintained by Seller to any computerized maintenance programs and any maintenance service programs for the engines, avionics or other similar agreements (collectively, the “Service Program Contracts”). Upon request, the Seller must provide the Service Program Contracts to the FAA for review as part of the pre-purchase inspection. Seller shall be responsible for and shall have paid any and all sums owing to providers of Service Program Contracts with respect to all periods prior to the Closing. If the rights to any maintenance agreements or programs are transferred to the FAA, payment of any and all associated sums owing to providers of Service Program Contracts with respect to all periods after the Closing will be the responsibility of the FAA. FAA, at its election, may terminate any Service Program Contracts after transfer or, by notice to Seller at least five business days before the Closing choose not to have any Service Program Contract transferred or assigned. Seller shall cooperate with FAA to obtain acceptance and acknowledgement by the provider of any Service Program Contract of the transfer or assignment or termination of each such Service Program Contract, and any obligation to make any payment in connection therewith shall be the responsibility of FAA. The obligations of Seller in this section shall survive Closing.

Warranties. To the extent that any warranties from manufacturers, prior owners of the aircraft, service providers or suppliers with respect to the aircraft are still in effect and are assignable, all rights under such warranties are hereby assigned and transferred to FAA effective upon completion of the Closing; provided that FAA shall pay any transfer fees.

FPFM SOW Exhibit A

AIRCRAFT DESCRIPTION

Aircraft _____________________________ Manufacture date: _____________________ Serial Number ________________________ Registration Number: __________________ Engines on __________ Engine Program Damage History ____________________

Airframe Total Time (as of ________) _______ Hours _______ Landings

Engine Total Time (as of _________) Engine #1 ______ Hours / _______ Cycles Engine S/N ___________

Engine #2 ______ Hours / _______ Cycles Engine S/N ___________

APU Total Time (as of___________) APU ______ Hours

APU S/N ___________

APU on __________ Program

Avionics:

Maintenance & Inspections:

Interior:

Exterior:

FPFM SOW Exhibit B

PRE-PURCHASE INSPECTION REPORT

Re: Completion of Inspection

Dear Sir/Madam:

Pursuant to FAA contract #_________ (the “Agreement”) dated as of the ___ day of _________, 202_, by and between _______________ (“Seller”) and _______________ (“Purchaser”), pertaining to that certain ______________________ (year, make, model) aircraft, bearing manufacturer's serial number ____, and registration number _____ (the “Aircraft”), this letter confirms that the FAA has completed its Inspection of the Aircraft.

CHECK ONE:

____ Subject to correction or repair by Seller, at Seller's sole cost and expense, of all Inspection Discrepancies, the Aircraft is satisfactory and is hereby accepted in accordance with the terms of the Agreement. The list of the Inspection Discrepancies which must be repaired by Seller is attached hereto as Schedule 1.

____ The Aircraft is unsatisfactory and is hereby rejected.

FPFM SOW EXHIBIT C

AIRCRAFT DELIVERY RECEIPT

Pursuant to FAA contract #_________ dated as of the ___ day of ____, 202_, by and between_________ (“Seller” ) and the FAA, pertaining to that certain ___________________ (year, make, model) aircraft, bearing manufacturer's serial number ____, and registration number _____ (the “Aircraft”), The FAA hereby acknowledges acceptance of the Aircraft from Seller, at _______ o'clock (am / pm) on the ____ day of ___________, 202_, at _____________ Airport, in the State of _______. The times on the Aircraft at the time of delivery are as follows:

TOTAL TIME ENGINES:

TOTAL ENGINE CYCLES:

FAA ACKNOWLEDGED BY SELLER:

Company Name

FPFM SOW EXHIBIT D

WARRANTY BILL OF SALE

_____________________ (“Seller”), is the lawful owner of the beneficial title to the Airframe, the Engines, the Parts, the Ancillary Items, and the Aircraft Documents described and referred to herein (all of the foregoing collectively the “Aircraft”):

“Aircraft Documents” means a current and validly issued United States Standard Airworthiness Certificate, and all logbooks, Airworthiness Directive compliance records, FAA Form 337s, Pilot Operating Handbooks (POH), POH supplements, manuals for installed equipment, maintenance and inspection records, parts catalogs, yellow tags, wiring diagrams, completion/refurbishment records, 8130-3s or equivalent for all life limited components, burn certifications, or required STC’s and other technical documentation pertaining to the Airframe or Engine that are in Seller's possession or control.

“Airframe” means that certain _________________________(year, make, model) aircraft, bearing manufacturer's serial number ____, and Federal Aviation Administration registration number_____ together with any and all Parts incorporated or installed in or attached thereto or otherwise in Seller's possession and control.

“Ancillary Items” means all tool kits, spare parts, rotables (including life rafts) support equipment, engine covers, loose equipment and other equipment of whatever nature that is associated with the Airframe and the Engines.

“Engines” means two (2) _______ model _________ series engines bearing manufacturer's serial numbers __________ and _________ (described on the International Registry as __________ bearing manufacturer’s serial numbers ________ and ________) together with any and all Parts incorporated or installed in or attached thereto or otherwise in Seller's possession and control.

“Parts” means all appliances, components, parts, avionics, instruments, appurtenances, accessories, furnishings or other equipment of whatever nature (other than complete Engines or engines) incorporated or installed in or attached to the Airframe or any Engine, and all spare parts in Seller's possession and control.

THAT, for good and valuable consideration, receipt and adequacy of which is hereby acknowledged, Seller does as of the date provided below, grant, convey, transfer, deliver and set over all right, title and interest in and to the Aircraft unto the FAA, and unto the FAA’s successors and assigns.

THAT, Seller hereby represents that there is hereby conveyed to the FAA on the date hereof, good and marketable title to the Aircraft free and clear of any and all liens, claims, and encumbrances, provided that Seller will be solely responsible to warrant and defend such title forever against all claims and demands whatsoever.

IN WITNESS WHEREOF, Seller has caused this instrument to be executed and delivered by its duly authorized signatory as of this ___ day of _______________, 202_.

FPFM SOW EXHIBIT E

PRE-PURCHASE AIRCRAFT FLIGHT PROFILE CHECKLIST

CL-605/650

N ________ Date(s): ________________

PIC __________________ SIC ___________________

Other Persons on Board

Note: The purpose of this flight profile is to verify aircraft systems and operational functions.

Review maintenance records of recently accomplished work performed. Note any additional required or recommended checks as requested/briefed by maintenance.

· PIC determines WX requirements. Day VMC is recommended for initial takeoff.

Aircraft Preflight Exterior and Interior

· Conduct a thorough examination of Aircraft Logbook.

· Conduct thorough detailed exterior inspection.

· Conduct thorough detailed interior inspection.

· Review/locate on board required emergency equipment. Lifejackets, oxygen masks, fire extinguishers, first aid kit, flashlights.

Normal Power-up (additional items)

· At APU start, note the following:

Check transmit and receive capability on all radios (ensure personnel are clear of the aircraft prior to transmitting on HF, or check during flight)

· Check Pilot and Copilot O2 masks and radio communications

· Complete VOR Check and document the results

· Check NDB operation

· Check FMS database currency

· Check function of all reversion switches

· Manually run stab, rudder, and aileron fully in both directions and return to neutral

· Check interior cockpit and cabin lighting if possible

· Check Exterior Lighting with Second Crewmember (LDG, TAXI, BEACON, RECOG, ICE, NAV)

· Flight Control Disconnect Check

· Hydraulic Pumps - 1B, 2B, 3A, 3B - ON with normal pressure in all three systems

· Pitch Disconnect - Pull

· Move each control column in turn

· Confirm each column moves only the same side elevator and does not move the other column

· Pitch Disconnect - Reconnect

· Roll Disconnect - Pull

· Move each control wheel in turn

· Confirm each column moves only the same side aileron and does not move the other control wheel

· Roll Disconnect - Reconnect

· Hydraulic Pumps - 1B, 2B, 3B – OFF, 3A – ON

· Flight Control Check

· Visually verify normal operation of all flight controls

After Start (additional items)

Record engine parameters after start.

Left Right

Hyd. Qty 1 ______ 2. _________ 3.________

Hyd. Press 1A______ 3A_______ 3B______ 2B________

Takeoff Configuration Warning Check

· With throttles greater than 70% N1 lever position, check that takeoff warning does not occur with:

· Spoilers stowed

· Flaps 20

· Stab trim in the green (check full range of green)

· With throttles greater than 70% N1 lever position, check that takeoff warning occurs with (check each condition individually):

NOTE: 605- Warning includes: 1. Flashing Master Caution; 2. EICAS Message; and, 3. Voice warning.

· Flight/Ground spoilers deployed – “Config Spoilers”

· Flaps 0, 30, and 45 – “Config Flaps”

· Stab trim not in T/O range – “Config Trim”

· Parking brake set- “Config Brakes”

· Autopilot on – “Config Autopilot”

Lineup Checklist (additional items) Perform static takeoff and thoroughly check all engine indications and APR

· Record engine parameters (T/O)

After Takeoff (additional items)

· Gear up, note time ________ (max 14 sec.)

· Verify autothrottle

· After Radar Contact, verify operation of all transponders.

· During the climb, check each flying control and trim system for proper feel and operation

· Elevator

· Aileron

· Rudder

· Pitch Trim

· Roll Trim

· Rudder Trim

During the climb and/or cruise, check each Autopilot and Flight Director for proper operation. Confirm each Flight Director mode operates properly

Cruise Checklist (additional items)

· Cabin Pressurization Check- climb to altitude with min PSID of 6.0 (usually between 15,000-20,000 feet)

· Passenger O2 supply (“rubber jungle”) O2 - OFF

· Crew O2 masks DON or in-hand for quick-donning if cabin goes over 10,000 feet

· Left and Right Cowl Anti-Ice - ON

· Left 10th STAGE - CLOSED

· Right Thrust Lever - IDLE for 1 MINUTE

· Note Any Cabin Climb Rate __________ FPM Note: Record results >500 FPM in the ALB and follow the following troubleshooting procedure: For climb rates >500 FPM, add power above idle on the Right Thrust Lever to stabilize the rate change to zero.

Note power setting: ___ N1.

· Right Thrust Lever - CRUISE

· Left 10th Stage - OPEN

· Right 10th Stage - CLOSED

· Left Thrust Lever – IDLE for 1 MINUTE

· Note Any Cabin Climb Rate __________ FPM Note: Record results >500 FPM in the ALB and follow the following troubleshooting procedure: For climb rates >500 FPM, add power above idle on the Left Thrust Lever to stabilize the rate change to zero.

Note power setting: ___ N1.

· Left Thrust Lever - CRUISE

· Right 10th Stage – OPEN

· Both Packs – OFF

· Record Leak after 30 seconds __________ FPM Note: Record Leak Rate Readings > 2,500 FPM in the ALB.

· Both Packs – ON

· Left and Right Cowl Anti-Ice - As Required

· Manual pressurization check PRESS CONT. - Push in . “Manual” light illuminated, white.

MAN ALT Select DOWN.

MAN RATE Select MAX.. note increasing cabin pressure diff. (If 9.1 reached, DIFF PRESS posted (red)) MAN RATE Select MIN.

PRESS CONT. – Push out “Manual” light extinguished.

· Cabin Pressure Low and Emer. Press check – if requested by maintenance. See Appdx.

Cruise Checklist (additional items) During descent, @ 280 kts, Thrust levers symmetrical, record fuel load.

Left tank ______ Aux _____ Right tank _____ Tail _____ Total _____ Trim LWD/RWD ____________ Surface position L ______ R ______ Elev Trim _______ units Rudder trim _______ units

Record engine parameters Left Right

· Descend to 10,000 feet at 185 KIAS, level flight, and accomplish the following:

· Check flight inst. Pilot/Co-pilot/Stby

· Gear transit time

· GEAR-DOWN ___ sec (14 SEC MAX)

· Flap operation transit time (gear down):

· Record flap indication at each flap setting. Verify no buzzing.

· Flaps – UP

· Gear transit time

· GEAR-UP ___ sec (14 SEC MAX)

· Landing Gear Manual Extension (if requested by maintenance)

· Altitude 10,000 feet, 190 KIAS, Flaps 20 degrees, HYD 2B - ON

· Landing Gear Manual Release - PULL *Exercise care not to let go of the handle prematurely*

· 3 Green / Nose Door Open – CHECK

· Gear Lever Down - DOWN

· Landing Gear Manual Release - STOW *Exercise care not to let go of the handle prematurely*

· 3 Green- CHECK/ Nose Door Open Light– Extinguished

· Anti skid inop (amber)

· Parking Brake SOV (amber)

· Gear Lever – UP

· Flaps – UP (if not previously accomplished)

· Hydraulic B Pumps – As Required

Cruise Checklist additional items (Continued)

· Check ability to couple both autopilots to VOR course ___________

· Check both ADF receivers for proper operation __________

· Check radar, all modes ___________ Descent Checklist additional items

· Ensure proper operation of flight spoilers ___________ Before Landing Checklist additional items and approaches ( 2 required)

· Check ability to couple both autopilots to ILS. Check nav to nav transfer

· Check ability to couple both autopilots to RNAV approach. LNAV/VNAV appr.

· Confirm all GPWS callouts. GA/AP disconnect function

· Confirm all normal indications on approaches.

· Brief the use of full reverse thrust.

ADG check. If requested by maintenance. See checklist After landing, ensure normal operation of ground and flight spoilers.

Less than 16 kts and 40 sec. WOW and flt spoilers retracted.

Shutdown Checklist Supplement

· Verify Hyd Quantities 1. __________ 3. __________ 2. ___________

· Verify IRS accuracy Flt time ___________ Select POS SUMMARY LSK. Check position difference relative to FMS is less than 2.5 nm per hour flown

IRS #1 _____/___nm IRS #2 _____/____nm, IRS #3 ______/_____nm

Select LRN STATUS LSK. While stationary 9within 2 mins) check ground speed. Less than 15 kts.

IRS #1 _____/____, IRS #2. _____/____ KTS. IRS #3 ____/____ KTS.

· Perform Post Flight Exterior Inspection.

Debrief

· Complete all logbook entries

· Review/discuss with maintenance personnel.

Logbook Entries and Noteworthy Items

· Aircraft logbook entries:

Appendix 1- Cabin Pressure Low Warning Check (Includes Emerg. Depress)

· Cabin Pressure Low Warning Check (if required)

· Maintain Level Flight of 15,000 – 20,000 feet

· Left and Right ACU’s – ON

· Cabin Pressurization Mode – AUTO

· Cabin Altitude Selector

· 9,000 feet

· Cabin Pressurization Rate – SET to INDEX POSITION

· O2 Masks – DON

· Verify O2 mask comms NOTE: The follow readings come very quickly and are therefore difficult to read/interpret. Make best effort to ensure that the events occur in order shown, at approximately the target values.

· Emergency Depress Switch – PRESS IN (Light On)

· Amber CABIN ALT EICAS msg and aural “Cabin Pressure” ON at __________ FT (cabin altitude) NOTE: This should occur when cabin altitude reaches 8,500.

· Red CABIN ALT EICAS msg and aural “Cabin Pressure” ON at __________ FT (cabin altitude) NOTE: This should occur when cabin altitude reaches 10,000.

· Outflow Valves Close at __________ FT (cabin altitude) NOTE: Cabin altitude limiters close the outflow valves to maintain a cabin altitude of 14,500 ± 500 feet. This will be indicated when cabin alt readout on ED2 and Standby Cabin Altimeter stops climbing.

· Emergency Depress Switch – PRESS OUT(Light Off)

· Red CABIN ALT EICAS msg OUT at __________ FT (cabin altitude) NOTE: This should occur at approximately 10,000 feet.

· Amber CABIN ALT EICAS msg OUT at __________ FT (cabin altitude) NOTE: This should occur at approximately 8,500 feet.

· Cabin Pressurization Controls – RESET TO NORMAL

· Passenger O2 Supply (“rubber jungle”)- O2- ON

Section C: FFSP PWS - i

August 16, 2021 1