Attachment 02 - SOW N86 WO610423 23.03.21.pdf

N86 400/3200Hr MSG-3, 15000Hr AF, TLW Inspections

STATEMENT OF WORK

1.0 INTRODUCTION

Flight Program Operations (AJF) is responsible for all aspects of the FAA Flight Program to include: safety, policy/standards, operations, training, maintenance, administrative services, financial and business management, acquisition, reporting, regulatory compliance, and other internal/external requirements.

In accordance with Title 14 of the Code of Federal Regulations (14 CFR) 135.426(3)(c), AJF requires that each maintenance provider perform all covered work in accordance with Flight Program Operations’ FAA-accepted General Maintenance Manual (GMM) and FAA-approved Continuous Airworthiness Maintenance Program (CAMP). Any person contracted to perform maintenance, inspection, repair, or alteration on FAA Flight Program aircraft must be qualified, trained, certified, and authorized to perform the work.

2.0 SCOPE

The contractor must be an authorized Bombardier service center with a 14 CFR Part 145 Repair Station Certificate and associated Operations Specifications listing the appropriate ratings and limitations, have access to the original equipment manufacturer (OEM) engineering support, have the ability to provide Aircraft on Ground (AOG) support, and have approved tooling and equipment along with parts and material to adequately maintain all CL-600-2B16 aircraft systems. The contractor must have extensive Bombardier CL-600-2B16 type aircraft experience on both airframe and General Electric Engines (CF34-3A1) maintenance, as well as preventive maintenance, inspections and modifications. The contractor must provide technician labor and parts necessary to successfully accomplish the 15,000Hr, 400, 3200Hr MSG-3 Check, 400Hr Engine Check, and 12/36 month, as well as other requirements (listed below) for CL-600- 2B16 aircraft, registration number N86. Non-routine discrepancies discovered during these inspections must be corrected. The contractor must perform an airworthiness release in accordance with the Flight Program Operations’ FAA-approved CAMP.

The inspections required to comply with this requirement are as follows:

STATEMENT OF WORK

CL601-601-53EO-

01534

INSPECT LAIRCM

SLTA DOUBLER

CL601-FUNC-43AR-

01764

TVPS BORESIGHT

DATA

VERIFICATION

CL601-INSP-

15SCHED-00063

CL-600 - 8366

HORIZONTAL

STABILIZER FRONT

SPAR UPPER

CL601-INSP-

15SCHED-00089

CL-600 - 7394L-R

LOWER WING

PLANK VISUAL

INSP WS94.0,

STRINGER 23

CL601-INSP-

15SCHED-00156

CL-600 - 7353L-R

WING LOWER PLANK

WS163.0

CL601-INSP-15SCHED-

00160

CL-600 - 7364L-R WING

LOWER PLANK 242.0

STRNGR INSPECTION

CL601-INSP-

15SCHED-00169

CL-600 - 7337L-R

LOWER WING

PLANK REAR SPAR

CL601-INSP-

15SCHED-00214

CL-600 - 1337L-R

PYLON CANTED RIB

UPPER SPLICE - FS

672.2

CL601-INSP-

15SCHED-00215

CL-600 - 5350 CABIN

WINDOW

SURROUND

STRUCTURES

FS364.0 TO 529.0

STRINGERS

10 TO 13 VISUAL

CHECK

CL601-INSP-

15SCHED-01064

CL-600 - 8379

HORIZONTAL

STABILIZER

BATHTUB FITTING

VISUAL CHECK

CL601-INSP-

15SCHED-01113

CL-600 - 5342

PASSENGER DOOR

AND SURROUNDING

STRUCTURE VISUAL

CHECK

CL601-INSP-15SCHED-

01117

CL-600 15K/6KH AILERON

UPPER/LOWER SKIN

(7127,7386L/R,7627)

CL601-INSP-

15SCHED-01118

CL-600 - 7349L-R

WING LOWER

PLANK 45.0

STRNGR

CL601-INSP-

15SCHED-01122

CL-600 - 5334

FUSELAGE TO

WING LATCH

FRAME VISUAL

INSPECTION

CL601-INSP-

15SCHED-01123

CL-600 - 5336 R

PRESSURE

BLUKHEAD FLOOR

BEAMS VISUAL

INSPECTION

CL601-INSP-

15SCHED-02021

CL-600 - 8360L-R

VERTICAL

STABILIZER -

FUSELAGE FRAME

REFERENCE VS

55.625%, STRINGER 5

VISUAL CHECK

15SCHED-02022

CL-600 - 8361L-R

EXTERNAL SKIN AND

DRAG ANGLES

FRAMES 55.62% AND

67.5%

VERTICAL

STABILIZER CHORD

NDT

CL601-INSP-15SCHED-

02051

CL-600 - 8371 VERTICAL

STABILIZER FRONT SPAR

AND CAP - VISUAL CHECK

CL601-INSP-

15SCHED-02053

CL-600 - 5354

FUSELAGE

STRINGER,

STRINGER SPLICE

FS 718.0

STRINGERS 0,1

VISUAL CHECK

CL601-INSP-

15SCHED-02068

CL-600 - 7348L-R

WING LOWER

CENTER PLANK

WS45.0

CL601-INSP-

15SCHED-02069

CL-600 - 7366L-R

WING LOWER

PLANK 264.0

STRNGR

CL601-INSP-

15SCHED-02084

CL-600 - 7352L-R

WING LOWER

PLANK WS86.0

CL601-INSP-

15SCHED-02087

CL-600 - 4307

LONGITUDINAL

FLOOR BEAM

INSPECTION

CL601-INSP-15SCHED-

02130

CL-600 - 7321L-R FLIGHT

SPOILER - UPPER AND

LOWER SKIN - VISUAL

INSPECTION

CL601-INSP-

15SCHED-02995

CL-600 - 5353

STRINGER SPLICE

FS 473.0 STRINGER

3, SKIN SPLICE,

STRINGER 0 FS

439 VISUAL CHECK

CL601-INSP-

15SCHED-03007

CL-600 - 7335L-R

LOWER WING

PLANK REAR SPAR

WS 242.0 NDT

VISUAL CHECK

CL601-INSP-

15SCHED-03008

CL-600 - 7355L-R

WING LOWER

PLANK VISUAL

CHECK

CL601-INSP-

15SCHED-03020

CL-600 - 7376L-R

WING LOWER

PLANK - WS 242.0

STRINGER 7

VISUAL CHECK

CL601-INSP-

15SCHED-03027

CL-600 - 7338L-R

LOWER WING PLANK

REAR SPAR

CL601-INSP-15SCHED-

03029

CL-600 - 5340 FLOOR

STRUCTURE/UNDERFLOOR

LONGERONS VISUAL

CHECK FS513.0

BL 45.0

CL601-INSP-

15SCHED-03570

CL-601 - 36 M

CHECK

CL601-INSP-

15SCHED-03961

CL-600 - 8372 15000

HR VERTICAL

STABILIZER VISUAL

INSPECTION

CL601-INSP-

15SCHED-03967

CL-600 - 8362

ENGINE SUPPORT

BEAM UPPER CAP

CL601-INSP-

15SCHED-03980

CL-600 - 4306

VISUAL

INSPECTION

FLOOR BEAM ATCH

CL601-INSP-

15SCHED-03982

CL-600 - 5351

FUSELAGE SKIN

PANEL/STRINGER

VISUAL INSPECTION

CL601-INSP-15SCHED-

04586

CL-601 - 12 M CHECK

CL601-INSP-

15SCHED-04937

CL-600 - 7361L-R

WING LOWER

PLANK 45.0

STRNGR

CL601-INSP-

15SCHED-04938

CL-600 - 7363L-R

WING LOWER AFT

PLANK MLG

CL601-INSP-

15SCHED-04952

CL-600 - 3308

PILOTS/COPILOTS

FLOOR WEB AT

PRESS BULKHEAD

FS 203.0 BL 16.0

VISUAL CHECK

CL601-INSP-

15SCHED-04956

CL-600 - 1342L-R

THRUST

REVERSER MAIN

UPPER PYLON

TRACKS

CL601-INSP-

15SCHED-04957

CL-600 15K/3KH

FRONT WING SPAR

WEB

(7104,7332L/R,7604)

CL601-INSP-15SCHED-

04958

CL-600 - 8363 HORIZONTAL

STABILIZER REAR SPAR

CENTER

CL601-INSP-

15SCHED-04959

CL-600 - 7339L-R

WING REAR SPAR

LOWER PLANK

CL601-INSP-

15SCHED-05323

CL-601 - 3200 H

MSG-3 CHECK

CL601-INSP-

15SCHED-05854

CL-600 - 8369

ELEVATOR - VISUAL

CHECK

CL601-INSP-

15SCHED-05863

CL-600 - 1335L-R

PYLON UPPER

SKIN FS682.0

CL601-INSP-

15SCHED-05908

CL-600 - 7367L-R

WING LOWER PLANK

C/SPLICE

CL601-INSP-15SCHED-

05913

CL-600 - 3307 FUSELAGE

BULKHEAD FRAME/

UPPER CAP ANGLE FS

235.0 BL

8.0COCKPIT FLOOR CLIPS

FS202.75 BL 6.0 TO BL

30.0VISUAL CHECK

STATEMENT OF WORK

CL601-INSP-

15SCHED-06142

CL-600 - 4326 VCS

CONDENSER

COOLING

INSTALLATION

INSPECTION.

CL601-INSP-

15SCHED-06825

CL-600 - 8377

RUDDER VISUAL

CHECK OF SKINS,

FRONT SPAR AND

HINGE BOLTS

CL601-INSP-

15SCHED-06829

CL-600 - 8367

HORIZONTAL

STABILIZER

COUNTER LINE RIB,

UPPER STRINGER 1

BL 6.0

VISUAL CHECK

CL601-INSP-

15SCHED-06854

CL-600 - 8370

VERTICAL

STABILIZER MID

SPAR CAP @ RIB 1

VISUAL CHECK

CL601-INSP-15SCHED-

06878

CL-600 - 8365

HORIZONTAL

STABILIZER REAR

SPAR UPPER

CL601-INSP-

15SCHED-06879

CL-600 - 7333L-R

FRONT SPAR SPLICE

LOWER WING

CL601-INSP-

15SCHED-06881

CL-600 - 7351L-R

WING LOWER PLANK

AFT EDGE

CL601-INSP-

15SCHED-06886

CL-600 - 5348

FUSELAGE SKIN

PANEL VISUAL

INSPECTION

CL601-INSP-

15SCHED-06890

CL-600 - 7330L-R

LOWER

PLANK/REAR SPAR

CL601-INSP-

53SCHED-00506

NASA MSBLS DATA

BUS CONNECTOR

FEEDS - FORWARD

PRESSURE

BULKHEAD

CL601-INSP-55SCHED-

03957

CL-600 - 8378

VERTICAL/HORIZONTAL

STABILIZER PIVOT

LUGS AND FITTINGS

INSPECTION

(AIRWORTHINESS

LIMITATION)

57SCHED-04941

CL-600 - 7365L-R

WING LOWER PLANK

242.0 STRNGR

INSPECTION

(AIRWORTHINESS

LIMITATION)

CL601-INSP-

57SCHED-06874

WING/FUSELAGE

ATTACHMENT

FITTING LUGS 57-40-

00-182*.

CL601-NDT-

15SCHED-00057

CL-600 - 2318 NLG

SUPPORT

STRUCTURE - NDT

VISUAL CHECK

CL601-NDT-

15SCHED-00058

CL-600 - 2320

FORWARD

PRESSURE

BULKHEAD

VERTICAL MEMBER

AND WEB BL13.7 +

22.0, WL 79.5 TO 93.0

NDT VISUAL

INSPECTION

CL601-NDT-

15SCHED-00104

CL-600 - 8375

VERTICAL

STABILIZER FRONT

SPAR CAP SPLICE

STRAP NDT CHECK

CL601-NDT-15SCHED-

00332

CL-600 - 8358 REAR

PRESSURE BULKHEAD

FS 621.0 FRAME CAP

NDT VISUAL CHECK

CL601-NDT-

15SCHED-01031

CL-600 - 1357L-R

THRUST REVERSER

MAIN TRACKS

LOWER FLANGE,

SERVICE PYLON

UPPER TRACK

SUPPORT BED

VISUAL-NDT CHECK

CL601-NDT-

15SCHED-01116

CL-600 15K/1.2KH

LOWER WING PLANK

NDT CHECK

(7354L/R, 7122,7622)

CL601-NDT-

15SCHED-02003

CL-600 - 8374

VERTICAL

STABILIZER FRONT

SPAR CAP AT RIB 1

NDT CHECK

CL601-NDT-

15SCHED-02120

CL-600 - 1338 AFT

ENGINE MOUNT

THRUST FITTING-

VISUAL AND EDDY

CURRENT

CL601-NDT-

15SCHED-02960

CL-600 - 8356

STRINGER SPLICES

AND FUSELAGE -

NDT - VISUAL

CHECK

CL601-NDT-15SCHED-

02976

CL-600 - 8355 OUTER

FLANGE CAP SPLICE

ANGLE - FS 625.3 NDT

CHECK EDDY

CURRENT

CL601-NDT-

15SCHED-03019

CL-600 - 7329L-R

WING ATTACHMENT

FRAME, LUGS AND

LINKS - EDDY

CURRENT AND

VISUAL CHECK

CL601-NDT-

15SCHED-03035

CL-600 - 5338 FS625

VERTICLE ANGLE

NDT VISUAL

INSPECTION

CL601-NDT-

15SCHED-03064

CL-600 - 4328

OVERWING

EMERGENCY EXIT

AND SURROUND

STRUCTURE NDT

CHECK

CL601-NDT-

15SCHED-03164

CL-600 - 8357 REAR

PRESSURE

BULKHEAD, FS 621.0

BL 9.5 AND 27.0 WL

73.0 AND 96.0

NDT VISUAL

INSPECTION

CL601-NDT-

15SCHED-03900

CL-600 - 1339L-R

FORWARD NACELL

STRUCTURE AT

ENGINE NACELL

JOINT VISUALNDT

CHECK

CL601-NDT-15SCHED-

03901

CL-600 - 1340L-R

ENGINE MOUNT YOKE-

LOWER LUG VISUAL-

NDT CHECK

CL601-NDT-

15SCHED-03958

CL-600 - 8381 PYLON

UPPER SPAR CAP AT

FS 625.3 - NDT

CHECK

CL601-NDT-

15SCHED-03970

CL-600 - 8354

FUSELAGE FRAME

CAP ANGLE FS 755.0

NDT VISUAL CHECK

CL601-NDT-

15SCHED-03983

CL-600 - 5345

PASSENGER DOOR

FRAMES - FS 310.0

AND FS 349.1 NDT

VISUAL CHECK

CL601-NDT-

15SCHED-03984

CL-600 - 5355

PRESSURE

SKIN/FLOOR ANGLE

AT WL 73.0 FS 409.0

TO 559.0NDT

CHECK/EDDY

CURRENT

15SCHED-03997

CL-600 - 7331L-R

LOWER WING

PLANK/REAR SPAR

NDT EDDY CURRENT

CL601-NDT-15SCHED-

04029

CL-600 - 5332 KEEL

LONGERON NDT

VISUAL INSPECTION

AND EDDY CURRENT

CL601-NDT-

15SCHED-04964

CL-600 - 5347 LIGHT

FUSELAGE FRAMES

NDT VISUAL

CL601-NDT-

15SCHED-05857

CL-600 - 8373

VERTICAL

STABILIZER REAR

SPAR NDT CHECK

CL601-NDT-

15SCHED-05884

CL-600 - 5344

OVERWING

EMERGENCY EXIT

STOPS/FITTINGS

/ATTACHMENTS NDT

VISUAL CHECK

CL601-NDT-

15SCHED-06787

CL-600 - 1344L-R

FORWARD ENGINE

MOUNT UPPER LINK

AND BOLTS-NDT

CHECK

CL601-NDT-

15SCHED-06827

CL-600 - 8359

BAGGAGE DOOR

AND SURROUNDING

STRUCTURE - NDT

EDDY

CURRENT

CL601-NDT-15SCHED-

06873

CL-600 - 7340L-R WING

LOWER PLANK - WS-

314.5 /315.0 AND BUTT

STRAP SPAR NDT

CHECK

CL601-NDT-

15SCHED-06915

CL-600 - 7305L-R

INTEGRAL FRAME

ATTACHMENT LUGS

FS 424.0 BL45 NDT

STATEMENT OF WORK

CL601-NDT-

15SCHED-06916

CL-600 - 7308L-R

INTEGRAL FRAME

ATTACHMENT BOLTS

FS 424.0 BL45 NDT

CHECK

CL601-NDT-

15SCHED-06925

CL-600 - 5352 WING

TO FUSELAGE

ATTACHMENT

FRAME FS513.0

VISUAL AND NDT

CHECK

CL601-NDT-

53SCHED-01182

CL-600 - 5320

GPS/GLONASS

ANTENNA NDI

INSPECTION

(AIRWORTHINESS

LIMITATION)

CL601-NDT-

53SCHED-07124

CL-600 - 5313

SATCOM ANTENNA

INSTALLATION NDT

INSPECTION

(AIRWORTHINESS

LIMITATION)

53SCHED-07125

CL-600 - 5314 TVPS

CAMERA

INSTALLATION NDT

INSPECTION

(AIRWORTHINESS

LIMITATION)

ADG UPLOCK

ACTUATOR SQUIB

REPLACEMENT

R/H ENGINE FIRE

EXTINGUISHER

HYDRO

SB 601-0613 R2

PASSENGER DOOR

EPOXY RAMP

REMOVAL

SB 1104 PART A

TORQUE BOX,

TRACK & SLIDERS

SB 1104 PART B

TORQUE BOX,

TRACK & SLIDERS

SB 1106

THRUST REVERSER

BLOCKER DOOR &

LINK ARM

ASSEMBLIES

TSO MC10-15-157

OXYGEN MASK

REPLACEMENT

P/N-APUINSP-

49SCHED

CL-600 - APU

IGNITION SYSTEM

INSPECTION, 1200

APU HOURS

P/N-FUNC-15SCHED-

06404

FUNCTIONAL TEST

OF THE ENGINE

THROTTLE GEARBOX

P/N 2100140-010 AT

5000 HOURS. L/H

P/N-FUNC-76SCHED-

05662

FUNCTIONAL TEST

OF THE ENGINE

THROTTLE GEARBOX

P/N 2100140-

003/005/007 AT

1000 HOURS R/H

SB 601-0633

MODIFICATION - NO.

1 AND NO. 2 MAIN

SYSTEMS -

RELOCATION OF THE

HYDRAULIC SYSTEM

NO. 1 AND NO. 2

ACCUMULATORS

BASIC ISSUE DATED

10/8/2015 REQUIRED

BY AD 2019-08-08

SB 601-0637

MODIFICATION - NO.

3 MAIN SYSTEM -

RELOCATION OF THE

HYDRAULIC

SYSTEM NO. 3

ACCUMULATOR

REQUIRED BY AD

2019-08-08

STATEMENT OF WORK

At the completion of each maintenance event, scheduled inspection, or repair; the contractor must clean the inside and outside of the aircraft. This includes washing and polishing to maintain the appearance and condition equal to the condition of the aircraft when first delivered to the contractor for services.

The contractor must ensure that airframe and engine logbooks are properly completed in accordance with the Flight Program Operations’ FAA-approved CAMP and/or FAA-accepted GMM, as applicable, following any maintenance completed by the contractor or subcontractor.

3.0 OBJECTIVES/CONTRACTOR RESPONSIBILITIES

3.1 Scheduled Maintenance / Inspections

Scheduled maintenance and inspections on the CL-600-2B16 aircraft will include preventive maintenance, scheduled inspections, special inspections required by the manufacturer, corrosion control, overhaul and/or replacement of components, and modifications to aircraft system(s). Scheduled items include Service Bulletins issued by the manufacturer, Airworthiness Directives (AD) issued by the FAA, as well as Maintenance Alert Directives (MAD) issued by Flight Program Operations. All scheduled work to be performed will be preceded with a budgetary quote/proposal for the known items of work to be completed. Scheduled work will not commence until the work package has been approved in writing by the FAA Contracting Officer (CO) or the Contracting Officer Representative (COR), as the designated representative of the CO. The scope of the work to be performed as part of this effort is specified in Section 2 of this Statement of Work (SOW).

3.2 Replacement Asset / Equipment Condition and Documentation

Any parts required to accomplish scheduled inspections or to correct discrepancies discovered during the performance of scheduled inspection may be procured or purchased by the contractor with prior authorization from the FAA CO or COR. Time change items will be provided by the FAA.

Any asset(s) required to replace existing component(s) necessary for the accomplishment of the contracted work must meet the following requirements:

Reasonable Parts Handling surcharge fees will be negotiated by Federal Aviation Administration and Contractor prior to contract being awarded.

Components offered as “New” must:

• Have zero (0) hours and zero (0) cycles in service since time of manufacture, and the internal components must have (0) hours and zero (0) cycles in service since time of manufacture.

• Have documentation that provides full traceability of parts and assemblies, if applicable, and a copy of the original shipping invoice from the Production Approval Holder (PAH) to the supplier providing evidence that the origin of the part is from a FAA PAH or that the original acquisition was from a FAA-approved source.

STATEMENT OF WORK

• Have documentation that identifies assembly internal components that are required to be tracked for traceability in accordance with the OEM manuals. Documents must identify part number and serial number.

Components offered as “Repaired/Overhauled/Serviceable” must:

• Be restored by an FAA-approved 14 CFR Part 145 Repair Station in accordance with the OEM manual requirements.

• Be restored after January 1, 2011, and have zero (0) time and zero (0) cycles in service since time of restoration.

• Have documentation that identifies all assemblies and assembly components meet the OEM 120-month restoration requirement.

• Have documentation that identifies assembly internal components that are required to be tracked for traceability in accordance with the OEM manuals. Documents must identify part number, serial number, and times/cycles/landings since new or overhaul.

All components must:

• Be properly identified as an approved aeronautical part in accordance with 14 CFR Part 21 and 14 CFR Part 45.

• Have a shipping invoice from the contractor to the FAA identifying part numbers and serial numbers.

3.3 Contractor Over and Above (O&A) Support

The FAA will have a need for the contractor to provide additional maintenance, parts, and support tasks that are not covered under the cost for maintenance and inspections. Additional maintenance services, parts, and support tasks will be considered as Over and Above (O&A) actions and are described in Section 7.0 of this SOW. O&A actions must be billed on a separate Contract Line Item Number (CLIN). The contractor must receive prior authorization from the FAA CO or COR before providing O&A maintenance, parts, or support tasks.

3.4 Contractor Personnel

The contractor must employ personnel who possess the required qualifications under 14 CFR, as well as the necessary skills to effectively accomplish the requirements of this SOW. The skills must include technical support for all applicable aircraft maintenance tasks, engine and airframe troubleshooting, parts support required for airframe and engine maintenance/inspection, field support for airframe and engine repairs, engine change, and accounting support for invoicing as described in this SOW.

3.5 Quality Control Inspection

The contractor must provide adequate quality control during the performance of all maintenance on FAA Flight Program aircraft. Quality control will be strictly exercised while the aircraft is being maintained and repaired. This includes:

• Continuous monitoring of technicians and work in progress to ensure technical data is being followed, and ensuring all work is completed in accordance with the Flight Program Operations’ 14 CFR Part 135 FAA-approved CAMP, applicable 14 CFR parts, and in a safe and thorough manner.

STATEMENT OF WORK

• Competently performing complete records research of Airworthiness Directives and Service Bulletins, as well as preparing proper documentation of compliance in permanent aircraft logbook.

• Approve aircraft for return to service in accordance with Flight Program Operations’ 14 CFR Part 135 FAA-approved CAMP.

• No work shall start on aircraft prior to FAA Representative’s arrival on site. (Due to COVID-19 a Quality inspection will be in contact with you and provide a plan for oversight)

• The FAA will have a COR(s) on site to oversee scheduled and non-routine maintenance tasks. All maintenance will be performed in accordance with Bombardier CL-600-2B16 series aircraft maintenance manuals and FAA-accepted and/or approved aircraft maintenance manuals. (Due to COVID-19 a Quality inspection will be in contact with you and provide a plan for oversight)

• FAA will provide the contractor with technical manuals and custom Work Content Documents, the FAA GMM, and the FAA-approved CAMP. The Quality Control Inspector/COR will be given access to the aircraft, throughout the maintenance visit, for oversight purposes.

3.6 Aircraft Inspection

Upon the arrival of the aircraft, the contractor and the FAA COR shall inspect the aircraft exterior and interior to confirm the configuration and condition of the aircraft. Any irregularities should be documented and a copy will be provided to the COR.

All routine and non-routine maintenance tasks will be completed, prior to release of aircraft for flight. After completion of the scheduled maintenance visit, a post-maintenance inspection will be performed to ensure airworthiness, to inspect for damage, and verify completeness.

3.7 Communication / Reporting Requirements

At induction, Contractor will provide to the FAA representative for review, a Gantt chart of the proposed check flow with milestones noted such as inspection redline date, major planned events and completion dates

The Daily Status Report (DSR) is to be completed by the MRO project manager and submitted to the FAA representative for review on a daily basis at any time in the morning but prior to 9am CST, so the live aircraft status can be briefed at the 0930 Briefing.

The FAA rep will review the DSR and either approve it, or request changes that reflect the actual aircraft status.

4.0 COMPONENT WARRANTY

STATEMENT OF WORK

The contractor shall provide a written statement of warranty for the work performed for the FAA.

The warranty statement must identify what is covered under warranty and the warranty duration.

5.0 GOVERNMENT RESPONSIBILITIES

The FAA shall ferry the aircraft at the Government’s expense, to and from any location, for all scheduled and unscheduled maintenance operations. The Government will assume all costs (including pilots, fuel, and travel expenses) for ferrying the aircraft to and from a place of disablement, to a service center for repairs.

The FAA may elect to perform any repair or inspection to the aircraft at home base or grounded location site using FAA maintenance personnel and equipment.

6.0 GOVERNMENT PROPERTY

An inventory of loose equipment will be performed and the property will be stored as Government Property (GP) and returned with the aircraft upon completion of the maintenance.

GP will be stored in a secure location.

7.0 OVER & ABOVE (O&A) PROCEDURES

All non-routine discrepancies will be routed through the COR for approval prior to any work starting. The CO must approve all obligations.

1. Either the FAA or the contractor may initiate the O&A action.

2. If the FAA determines an O&A action is required, the FAA CO or COR will request a price quote for the O&A action. Upon approval of the price quote, the FAA COR will ensure sufficient funding is available on the O&A CLIN. The CO or COR will provide approval to the contractor by issuing a Purchase Approval in FAA format or written notification by electronic mail.

3. If the contractor determines an O&A action is required, they must submit to the FAA CO and COR a description of the action and an explanation of why it is considered an O&A action as soon as practical (but no later than one calendar day after discovery of the O&A action) via electronic mail. The CO will review the contractor O&A request with the appropriate FAA personnel and provide approval or disapproval. If approved, the CO and COR will ensure sufficient funding is available on the O&A CLIN. The CO or COR will provide approval to the contractor by issuing a Purchase Approval in FAA format or notification by electronic mail.

4. Upon approval and completion of the O&A task, the contractor must submit an invoice within thirty (30) days of receipt of goods or completion of services.

At a minimum, O&A actions or quote must identify the requested maintenance or support action and specify the aircraft system, engine serial number, part number(s), tool, rental fee, etc. with supporting pricing documentation. The contractor must provide a Firm-Fixed-Price (FFP).

Failure to agree on a reasonable price must be considered a question of fact subject to the DISPUTES clause of the contract.

STATEMENT OF WORK

8.0 PERIOD OF PERFORMANCE / DELIVERY TIMES

Period of performance: not to exceed 60 days from the Induction Date.

N86 will arrive at the contractor’s Repair Station facility on or around March 31, 2023 The Induction Date (day 1) is the later of the date when the aircraft is delivered to the contractor and/or the date the work order is signed. If the aircraft arrives before 1200 local time that is considered to be Day 1, if after 1200 Local, the following day is considered to be day one of the check.

All paperwork should be cleared in TRAX as it is closed in process. The ETR is defined as the time when the aircraft is released and ready for flight, all paperwork is completed, cleared in the system and accounted for prior to the release

9.0 PLACE OF PERFORMANCE

The place of performance is the contractor’s facility, which must be an FAA-approved Repair Station. The place of performance should be the same address as listed on the contractor’s Air Agency Certificate.

10.0 WORK CARDS / DELIVERABLES

List Tasks: All work cards included in the bid proposal are included in the scope of work as an initial proposal requirement. The aircraft will be inducted with no expected pilot-reported logbook entries. Any pilot-reported logbook entry upon induction would be considered non-routine and billed as O&A. Flight crewmembers do not have the authority to approve any financial obligations.

All maintenance must be conducted in accordance with the Flight Program Operations’ FAA-approved CAMP, FAA-accepted manuals, and applicable 14 CFR parts.

STATEMENT OF WORK

APPENDIX 1

WORK CARDS

A/C

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CL601-601-53EO-01534

INSPECT LAIRCM SLTA DOUBLER.

CL601-FUNC-43AR-01764

TVPS BORESIGHT DATA VERIFICATION

CL601-INSP-15SCHED-00063

CL-600 - 8366 HORIZONTAL STABILIZER FRONT SPAR UPPER

CL601-INSP-15SCHED-00089

CL-600 - 7394L-R LOWER WING PLANK VISUAL INSP WS94.0, STRINGER 23

CL601-INSP-15SCHED-00156

CL-600 - 7353L-R WING LOWER PLANK WS163.0

CL601-INSP-15SCHED-00160

CL-600 - 7364L-R WING LOWER PLANK 242.0 STRNGR INSPECTION

CL601-INSP-15SCHED-00169

CL-600 - 7337L-R LOWER WING PLANK REAR SPAR

CL601-INSP-15SCHED-00214

CL-600 - 1337L-R PYLON CANTED RIB UPPER SPLICE - FS 672.2

CL601-INSP-15SCHED-00215

CL-600 - 5350 CABIN WINDOW SURROUND STRUCTURES FS364.0 TO 529.0 STRINGERS

10 TO 13 VISUAL CHECK

DUPLICATE

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CL601-INSP-15SCHED-01064

CL-600 - 8379 HORIZONTAL STABILIZER BATHTUB FITTING VISUAL CHECK

CL601-INSP-15SCHED-01113

CL-600 - 5342 PASSENGER DOOR AND SURROUNDING STRUCTURE VISUAL CHECK

CL601-INSP-15SCHED-01117

CL-600 15K/6KH AILERON UPPER/LOWER SKIN (7127,7386L/R,7627)

CL601-INSP-15SCHED-01118

CL-600 - 7349L-R WING LOWER PLANK 45.0 STRNGR

CL601-INSP-15SCHED-01122

CL-600 - 5334 FUSELAGE TO WING LATCH FRAME VISUAL INSPECTION

CL601-INSP-15SCHED-01123

CL-600 - 5336 R PRESSURE BLUKHEAD FLOOR BEAMS VISUAL INSPECTION

CL601-INSP-15SCHED-02021

CL-600 - 8360L-R VERTICAL STABILIZER - FUSELAGE FRAME REFERENCE VS 55.625%,

STRINGER 5 VISUAL CHECK

CL601-INSP-15SCHED-02022

CL-600 - 8361L-R EXTERNAL SKIN AND DRAG ANGLES FRAMES 55.62% AND 67.5%

VERTICAL STABILIZER CHORD NDT

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CL601-INSP-15SCHED-02051

CL-600 - 8371 VERTICAL STABILIZER FRONT SPAR AND CAP - VISUAL CHECK

CL601-INSP-15SCHED-02053

CL-600 - 5354 FUSELAGE STRINGER, STRINGER SPLICE FS 718.0 STRINGERS 0,1

VISUAL CHECK

CL601-INSP-15SCHED-02068

CL-600 - 7348L-R WING LOWER CENTER PLANK WS45.0

CL601-INSP-15SCHED-02069

CL-600 - 7366L-R WING LOWER PLANK 264.0 STRNGR

CL601-INSP-15SCHED-02084

CL-600 - 7352L-R WING LOWER PLANK WS86.0

CL601-INSP-15SCHED-02087

CL-600 - 4307 LONGITUDINAL FLOOR BEAM INSPECTION

CL601-INSP-15SCHED-02130

CL-600 - 7321L-R FLIGHT SPOILER - UPPER AND LOWER SKIN - VISUAL INSPECTION

CL601-INSP-15SCHED-02995

CL-600 - 5353 STRINGER SPLICE FS 473.0 STRINGER 3, SKIN SPLICE, STRINGER 0 FS

439 VISUAL CHECK

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-INSP-15SCHED-03007

CL-600 - 7335L-R LOWER WING PLANK REAR SPAR WS 242.0 NDT VISUAL CHECK

CL601-INSP-15SCHED-03008

CL-600 - 7355L-R WING LOWER PLANK VISUAL CHECK

CL601-INSP-15SCHED-03020

CL-600 - 7376L-R WING LOWER PLANK - WS 242.0 STRINGER 7 VISUAL CHECK

CL601-INSP-15SCHED-03027

CL-600 - 7338L-R LOWER WING PLANK REAR SPAR

CL601-INSP-15SCHED-03029

CL-600 - 5340 FLOOR STRUCTURE/UNDERFLOOR LONGERONS VISUAL CHECK FS513.0

BL 45.0

CL601-INSP-15SCHED-03570

CL-601 - 36 M CHECK

CL601-INSP-15SCHED-03961

CL-600 - 8372 15000 HR VERTICAL STABILIZER VISUAL INSPECTION

CL601-INSP-15SCHED-03967

CL-600 - 8362 ENGINE SUPPORT BEAM UPPER CAP

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CL601-INSP-15SCHED-03980

CL-600 - 4306 VISUAL INSPECTION FLOOR BEAM ATCH

CL601-INSP-15SCHED-03982

CL-600 - 5351 FUSELAGE SKIN PANEL/STRINGER VISUAL INSPECTION

CL601-INSP-15SCHED-04586

CL-601 - 12 M CHECK

CL601-INSP-15SCHED-04937

CL-600 - 7361L-R WING LOWER PLANK 45.0 STRNGR

CL601-INSP-15SCHED-04938

CL-600 - 7363L-R WING LOWER AFT PLANK MLG

CL601-INSP-15SCHED-04952

CL-600 - 3308 PILOTS/COPILOTS FLOOR WEB AT PRESS BULKHEAD FS 203.0 BL 16.0

VISUAL CHECK

CL601-INSP-15SCHED-04956

CL-600 - 1342L-R THRUST REVERSER MAIN UPPER PYLON TRACKS

CL601-INSP-15SCHED-04957

CL-600 15K/3KH FRONT WING SPAR WEB (7104,7332L/R,7604)

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-INSP-15SCHED-04958

CL-600 - 8363 HORIZONTAL STABILIZER REAR SPAR CENTER

CL601-INSP-15SCHED-04959

CL-600 - 7339L-R WING REAR SPAR LOWER PLANK

CL601-INSP-15SCHED-05323

CL-601 - 3200 H MSG-3 CHECK

CL601-INSP-15SCHED-05854

CL-600 - 8369 ELEVATOR - VISUAL CHECK

CL601-INSP-15SCHED-05863

CL-600 - 1335L-R PYLON UPPER SKIN FS682.0

CL601-INSP-15SCHED-05908

CL-600 - 7367L-R WING LOWER PLANK C/SPLICE

CL601-INSP-15SCHED-05913

CL-600 - 3307 FUSELAGE BULKHEAD FRAME/UPPER CAP ANGLE FS 235.0 BL

8.0COCKPIT FLOOR CLIPS FS202.75 BL 6.0 TO BL 30.0VISUAL CHECK

CL601-INSP-15SCHED-06142

CL-600 - 4326 VCS CONDENSER COOLING INSTALLATION INSPECTION.

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-INSP-15SCHED-06825

CL-600 - 8377 RUDDER VISUAL CHECK OF SKINS, FRONT SPAR AND HINGE BOLTS

CL601-INSP-15SCHED-06829

CL-600 - 8367 HORIZONTAL STABILIZER COUNTER LINE RIB, UPPER STRINGER 1 BL 6.0

VISUAL CHECK

CL601-INSP-15SCHED-06854

CL-600 - 8370 VERTICAL STABILIZER MID SPAR CAP @ RIB 1 VISUAL CHECK

CL601-INSP-15SCHED-06878

CL-600 - 8365 HORIZONTAL STABILIZER REAR SPAR UPPER

CL601-INSP-15SCHED-06879

CL-600 - 7333L-R FRONT SPAR SPLICE LOWER WING

CL601-INSP-15SCHED-06881

CL-600 - 7351L-R WING LOWER PLANK AFT EDGE

CL601-INSP-15SCHED-06886

CL-600 - 5348 FUSELAGE SKIN PANEL VISUAL INSPECTION

CL601-INSP-15SCHED-06890

CL-600 - 7330L-R LOWER PLANK/REAR SPAR

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-INSP-53SCHED-00506

NASA MSBLS DATA BUS CONNECTOR FEEDS - FORWARD PRESSURE BULKHEAD

CL601-INSP-55SCHED-03957

CL-600 - 8378 VERTICAL/HORIZONTAL STABILIZER PIVOT LUGS AND FITTINGS

INSPECTION (AIRWORTHINESS LIMITATION)

CL601-INSP-57SCHED-04941

CL-600 - 7365L-R WING LOWER PLANK 242.0 STRNGR INSPECTION (AIRWORTHINESS

LIMITATION)

CL601-INSP-57SCHED-06874

WING/FUSELAGE ATTACHMENT FITTING LUGS 57-40-00-182*.

CL601-NDT-15SCHED-00057

CL-600 - 2318 NLG SUPPORT STRUCTURE - NDT VISUAL CHECK

CL601-NDT-15SCHED-00058

CL-600 - 2320 FORWARD PRESSURE BULKHEAD VERTICAL MEMBER AND WEB BL13.7 +

22.0, WL 79.5 TO 93.0 NDT VISUAL INSPECTION

CL601-NDT-15SCHED-00104

CL-600 - 8375 VERTICAL STABILIZER FRONT SPAR CAP SPLICE STRAP NDT CHECK

CL601-NDT-15SCHED-00332

CL-600 - 8358 REAR PRESSURE BULKHEAD FS 621.0 FRAME CAP NDT VISUAL CHECK

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-NDT-15SCHED-01031

CL-600 - 1357L-R THRUST REVERSER MAIN TRACKS LOWER FLANGE, SERVICE PYLON

UPPER TRACK SUPPORT BED VISUAL-NDT CHECK

CL601-NDT-15SCHED-01116

CL-600 15K/1.2KH LOWER WING PLANK NDT CHECK (7354L/R, 7122,7622)

CL601-NDT-15SCHED-02003

CL-600 - 8374 VERTICAL STABILIZER FRONT SPAR CAP AT RIB 1 NDT CHECK

CL601-NDT-15SCHED-02120

CL-600 - 1338 AFT ENGINE MOUNT THRUST FITTING-VISUAL AND EDDY CURRENT

CL601-NDT-15SCHED-02960

CL-600 - 8356 STRINGER SPLICES AND FUSELAGE - NDT - VISUAL CHECK

CL601-NDT-15SCHED-02976

CL-600 - 8355 OUTER FLANGE CAP SPLICE ANGLE - FS 625.3 NDT CHECK EDDY

CURRENT

CL601-NDT-15SCHED-03019

CL-600 - 7329L-R WING ATTACHMENT FRAME, LUGS AND LINKS - EDDY CURRENT AND

VISUAL CHECK

CL601-NDT-15SCHED-03035

CL-600 - 5338 FS625 VERTICLE ANGLE NDT VISUAL INSPECTION

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-NDT-15SCHED-03064

CL-600 - 4328 OVERWING EMERGENCY EXIT AND SURROUND STRUCTURE NDT CHECK

CL601-NDT-15SCHED-03164

CL-600 - 8357 REAR PRESSURE BULKHEAD, FS 621.0 BL 9.5 AND 27.0 WL 73.0 AND 96.0

NDT VISUAL INSPECTION

CL601-NDT-15SCHED-03900

CL-600 - 1339L-R FORWARD NACELL STRUCTURE AT ENGINE NACELL JOINT VISUAL-

NDT CHECK

CL601-NDT-15SCHED-03901

CL-600 - 1340L-R ENGINE MOUNT YOKE-LOWER LUG VISUAL-NDT CHECK

CL601-NDT-15SCHED-03958

CL-600 - 8381 PYLON UPPER SPAR CAP AT FS 625.3 - NDT CHECK

CL601-NDT-15SCHED-03970

CL-600 - 8354 FUSELAGE FRAME CAP ANGLE FS 755.0 NDT VISUAL CHECK

CL601-NDT-15SCHED-03983

CL-600 - 5345 PASSENGER DOOR FRAMES - FS 310.0 AND FS 349.1 NDT VISUAL CHECK

CL601-NDT-15SCHED-03984

CL-600 - 5355 PRESSURE SKIN/FLOOR ANGLE AT WL 73.0 FS 409.0 TO 559.0NDT

CHECK/EDDY CURRENT

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CL601-NDT-15SCHED-03997

CL-600 - 7331L-R LOWER WING PLANK/REAR SPAR NDT EDDY CURRENT

CL601-NDT-15SCHED-04029

CL-600 - 5332 KEEL LONGERON NDT VISUAL INSPECTION AND EDDY CURRENT

CL601-NDT-15SCHED-04964

CL-600 - 5347 LIGHT FUSELAGE FRAMES NDT VISUAL

CL601-NDT-15SCHED-05857

CL-600 - 8373 VERTICAL STABILIZER REAR SPAR NDT CHECK

CL601-NDT-15SCHED-05884

CL-600 - 5344 OVERWING EMERGENCY EXIT STOPS/FITTINGS/ATTACHMENTS NDT

VISUAL CHECK

CL601-NDT-15SCHED-06787

CL-600 - 1344L-R FORWARD ENGINE MOUNT UPPER LINK AND BOLTS-NDT CHECK

CL601-NDT-15SCHED-06827

CL-600 - 8359 BAGGAGE DOOR AND SURROUNDING STRUCTURE - NDT EDDY

CURRENT

CL601-NDT-15SCHED-06873

CL-600 - 7340L-R WING LOWER PLANK - WS-314.5 /315.0 AND BUTT STRAP SPAR NDT

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135 15000 Hr AF FINANCE GO-LIVE OKC

CL601-NDT-15SCHED-06915

CL-600 - 7305L-R INTEGRAL FRAME ATTACHMENT LUGS FS 424.0 BL45 NDT CHECK

CL601-NDT-15SCHED-06916

CL-600 - 7308L-R INTEGRAL FRAME ATTACHMENT BOLTS FS 424.0 BL45 NDT CHECK

CL601-NDT-15SCHED-06925

CL-600 - 5352 WING TO FUSELAGE ATTACHMENT FRAME FS513.0 VISUAL AND NDT

CHECK

CL601-NDT-53SCHED-01182

CL-600 - 5320 GPS/GLONASS ANTENNA NDI INSPECTION (AIRWORTHINESS LIMITATION)

CL601-NDT-53SCHED-07124

CL-600 - 5313 SATCOM ANTENNA INSTALLATION NDT INSPECTION (AIRWORTHINESS

LIMITATION)

CL601-NDT-53SCHED-07125

CL-600 - 5314 TVPS CAMERA INSTALLATION NDT INSPECTION (AIRWORTHINESS

LIMITATION)

DISCARD 055046B 5484 ADG

HYDRO 899074-1 5687U RIGHT

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P/N-APUINSP-49SCHED- 3800488-3 P-321C

CL-600 - APU IGNITION SYSTEM INSPECTION, 1200 APU HOURS.

APU

P/N-FUNC-15SCHED-06404 2100140-010 2254

FUNCTIONAL TEST OF THE ENGINE THROTTLE GEARBOX P/N 2100140-010 AT 5000

HOURS.

LEFT

P/N-FUNC-76SCHED-05662 2100140-003 721

FUNCTIONAL TEST OF THE ENGINE THROTTLE GEARBOX P/N 2100140-003/005/007 AT

1000 HOURS.

RIGHT

SB 601-0633

SB 601-0633 MODIFICATION - NO. 1 AND NO. 2 MAIN SYSTEMS - RELOCATION OF THE

HYDRAULIC SYSTEM NO. 1 AND NO. 2 ACCUMULATORS

BASIC ISSUE DATED 10/8/2015 REQUIRED BY AD 2019-08-08

SB 601-0637

SB 601-0637 MODIFICATION - NO. 3 MAIN SYSTEM - RELOCATION OF THE HYDRAULIC

SYSTEM NO. 3 ACCUMULATOR

REQUIRED BY AD 2019-08-08

SB 601-1104 PART A

SB 601-1104 PART A MODIFICATION – TORQUE BOX, TRACK AND SLIDERS –

INTRODUCTION OF NEW BOLTS TO THE TORQUE BOX STOP ASSEMBLIES AND HINGE

ASSEMBLIES

COMPLY WITH SHORT SERVICE BULLETIN NO. CF34-NAC-78-037

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SB 601-1104 PART B

SB 601-1104 PART B MODIFICATION – TORQUE BOX, TRACK AND SLIDERS –

INTRODUCTION OF NEW BOLTS TO THE TORQUE BOX STOP ASSEMBLIES AND HINGE

ASSEMBLIES

COMPLY WITH SHORT SERVICE BULLETIN NO. CF34-NAC-78-037

SB 601-1106

601-1106 MODIFICATION THRUST REVERSER BLOCKER DOOR AND LINK ARM

ASSEMBLIES INTRODUCTION OF HARDENED BUSHINGS

TSO MC10-15-157 60267 L351007