SOW_DC8_Heavy_Mx_2020_07.01.19.pdf

RFI #

STATEMENT OF WORK

NASA ARMSTRONG FLIGHT RESEARCH CENTER (AFRC) DC-8 HEAVY

MAINTENANCE

Date 07/01/2019 Rev1: 07/29/2019

National Aeronautics and Space Administration Armstrong Flight Research Center Edwards, California

DC-8-72 Heavy Maintenance and Landing Gear Replacement

Table of Contents

1.0 Background

2.0 Objectives and Scope

3.0 Tasks

4.0 Period of Performance

5.0 Other Requirements

6.0 Government-Furnished Property (GFP)

7.0 Data Requirements

8.0 Quality Assurance Requirements

ATTACHMENT 1 - AIRCRAFT DESCRIPTION

ATTACHMENT 2 - MSG-3 WORKCARDS

1.0 Background

The National Aeronautics and Space Administration (NASA) operates a McDonnell Douglas (Boeing) DC-8-72 aircraft as an Airborne Science flying laboratory. This aircraft N817NA S/N 46082 currently managed by NASA Armstrong Flight Research Center (AFRC) and is based at Bldg. 703 located in Palmdale, CA.

The aircraft was originally produced for Alitalia in 1969 and later leased to Braniff International as a commercial airliner. NASA bought the aircraft in 1986 to be used as airborne science laboratory for weather and environmental science. For the life of the aircraft, it has been maintained to aircraft manufacturers’ recommendations for maintenance and in accordance with Federal Aviation Administration directives for airworthiness. In 2013, NASA contracted with Boeing to develop a Low Utilization Maintenance Program (LUMP) specific for this aircraft, based upon similar programs developed by Boeing using the Maintenance Steering Group (MSG-3) logic for Reliability Centered Maintenance (RCM).

The aircraft has been modified with numerous NADIR and Zenith ports for science instruments as well as modified window configurations. A detailed description of the aircraft special modifications and its expected condition upon delivery to the maintenance facility is described in Attachment 1. Since the aircraft has been modified, NASA provides self-certification of the aircraft due to its unique configuration and capability.

Aircraft Information

Type Aircraft DC8-72

Engine Type CFM56-2C1

Tail Number N817NA

Line Number 458

Construction Number 46082

Date Built April 16, 1969

Aircraft Flight Hours, Total 54,994 (4/1/2019)

Aircraft Cycles, Total 19,132 (4/1/2019)

2.0 Objectives and Scope:

Provide scheduled maintenance checks (1C/2C).

3.0 Optional Objectives and Scope

a. Provide schedule maintenance checks (3C)

b. Perform full landing gear removal and replacement. The Government shall provide overhauled ready for issue replacement landing gear for removal and replacement.

c. Perform other various maintenance and repair activities described in Section 6.0 below.

4.0 Task for 1C and 2C

a. Scheduled Maintenance Checks. For all required inspections, the contractor shall perform inspections and maintenance strictly in accordance with MSG-3 Work Cards listed in the attached spreadsheet (Attachment 2). The effort shall include any and all labor, tooloing and materials necessary to complete all inspections, repairs, stripping, cleaning, and painting, and return the aircraft to service in accordance with applicable FAA certification standards. This maintenance cycle shall NOT include any engine maintenance to be performed by the contractor.

5.0 Optional Tasks

a. Scheduled Maintenance Checks (3C). For all required inspections, the contractor shall perform inspections and maintenance strictly in accordance with MSG-3 Work Cards listed in the attached spreadsheet (Attachment 2). The effort shall include any and all labor, tooloing and materials necessary to complete all inspections, repairs, stripping, cleaning, and painting, and return the aircraft to service in accordance with applicable FAA certification standards. This maintenance cycle shall NOT include any engine maintenance to be performed by the contractor.

b. Landing Gear Replacement. The contractor shall remove and replace the Left Main

Gear, Right Main Gear, and Nose Landing Gear with landing gears provided by the government. Contractor shall perform appropriate maintenance and repairs to the airframe as agreed by the government as preparation to install the replacement landing gear. The contractor, with government oversight, will perform the removal and installation of the following replacement parts on the inspected landing gear:

Lines, hoses, Anti-skid valves, brake limiters, actuators.

c. Aircraft Interior Modifications:

1) Remove and replace interior cabin floor carpet. The government will provide carpet materials.

6.0 Over and Above Cost.

NASA will authorize what is commonly termed "over and above" inspections and repairs as necessary. The NASA Contracting Officer will designate NASA personnel “on-site” as the Contracting Officer’s Representative (COR) to determine what “over and above” maintenance is to be performed.

7.0 Terminology

The following are provided to clarify terminology used in the C-Check cards and all other work requirements.

a. Clean: A cleaned area is an area that is free from dirt, oil and fluid spills. If the corrosion inhibiting compounds are in good condition, no further action is required.

However, if the corrosion inhibiting compounds are in poor condition or has heavily pooled areas which prohibit visual inspection, these areas shall be further cleaned to perform the visual inspection and/or the re-application of corrosion inhibiting compounds.

b. Verifying proper corrosion protection coatings: This step is called out in numerous places on the inspection cards. If the proper corrosion protection coatings, such as alodine, FR primer, topcoat, inhibitors, or sealants are not present or inadequate they must be replaced. Refer to General Corrosion Control Handbook (Optional), August 1990, Appendix B, Section 3.2 Para. 3.2.1.

8.0 Period of Performance. All work described above shall be completed within 120 calendar days. The desired aircraft induction date is on/about 01 December 2019. The contractor shall propose an aircraft induction date and submit a delivery schedule in the quote, indicating the expected start and end dates for Tasks 3.a-d above. Prior to contract award, the government and contractor will negotiate a final aircraft induction date.

9.0 Other Requirements

a. Tooling. The government will not provide any standard tooling or support equipment for work described above. Due to the unique configuration of NASA 817, the government will provide special tooling as available and requested.

b. Facilities.

1) Strip and paint work may be performed at a facility separate from the inspection/maintenance facility. NASA shall provide a maintenance crew to pre-flight/post flight the aircraft and a flight crew to move the aircraft between facilities for this purpose.

2) All inspection/maintenance work (with the exception of aircraft paint) shall be performed at the same location. Other than towing of the aircraft from one facility to another at the same location, the aircraft shall not be moved or ferried to another facility for any part of the maintenance or inspection.

c. Reference Material. The contractor shall possess all relevance DC-8 technical reference material, including but nit limited to: DC-8 Maintenance Manuals, Service Repair Manuals, Service Bulletins, and Airworthiness Directives. Contractor shall have an arrangement with Boeing/Douglas to access any required DC-8 production prints. NASA DC-8 specific reference material will be provided as available and requested.

d. Security. The Contractor shall provide reasonable security for the aircraft to ensure that only authorized contractor and Government personnel have access to the aircraft.

The aircraft shall not be accessible to the general public at any time. The Contractor shall specify how and where the aircraft will be secured.

e. Engineering. The Contractor shall utilize an FAA DER (designated engineering representative) to design and approve any deviations from manufacturer’s fabrication and repair specifications during the O&A portion of the maintenance.

f. NASA Access During Maintenance Activities. The Contractor shall permit NASA

Technical staff to have access to the aircraft, on a non-interference basis, during the maintenance. This requirement is to avoid removal or disabling of special research systems installed in the aircraft, and for the NASA technical staff to conduct necessary tests and inspections of research systems not normally accessible except during heavy maintenance.

g. Authorized Representative(s): A list of authorized onsite Government staff will be provided and updated by the Contracting Officer. The Contracting Officer will designate official representatives and alternates for any approvals or signoffs as required by this contract for each shift where work is performed under this contract.

These individuals will be designated Contracting Officer’s Representative (COR) and also have the authorization to approve over and above (O&A) work on the aircraft or aircraft systems/subsystems.

h. Mandatory Inspection Points (MIP): The Government will include provision for

MIPs concurrent with existing inspection points performed by Government inspectors prior to closeout of critical structures. This shall not relieve the Contractor of responsibility for all inspections including the “OK to Close” inspections. The Government will provide sufficient on site staff to ensure that the Contractor’s workflow is not disrupted by the MIP.

i. Verification by NASA: Because of the unique research nature of this aircraft, there are numerous non-standard systems that are not normally accessible to NASA except during major maintenance. NASA maintenance personnel shall be permitted to perform verification checks of research system wiring on a non-interference basis during all phases of the proposed effort. Also the verification of Service Bulletins, part numbers, serial numbers, etc.

j. Systems Checks: Because of the uniqueness of the systems in this airborne laboratory, NASA Technical staff will operate or oversee the operation of (at their discretion) all aircraft systems while at the Contractor’s facility. The Contractor shall not operate any of the aircraft systems without approval of the designated Government representative.

k. Reuse of Hardware: Reuse of existing fastener hardware is acceptable (referred to as “Serviceable Hardware”). However, fastener hardware is “Non-Serviceable Hardware” if there is evidence of corrosion, missing plating, bad threads, excessive tool wear, or stripped heads. In that event, the fastener shall be replaced with a new item.

l. Tools: All removable service or access panels shall be installed with hand tools such as “speed wrenches” or other approved torque limiting devices. The use of air or other power tools without torque limiting protection shall not be permitted for use on service or access panels.

10.0 Government-Furnished Property (GFP). The Government will provide reconditioned landing gear to the Contractor. These components will be ready for installation and no painting is required. The reconditioned landing gear will be shipped to the Contractor’s facility by the Government at the Government’s expense in appropriate shipping containers. These containers shall be reused by the vendor to package the existing landing gear. The landing gear removed from the A/C shall not require any maintenance action.

The Government will ship the removed landing gear from the Contractor’s facility at the Government’s expense. Government representatives will provide oversight and guidance for the landing gear change.

11.0 Data Requirements.

The Contractor shall submit the following status reports after receipt of aircraft to Contractor’s site (Contractor format acceptable):

a. DRD-1 Daily Status Reports: Verbal reports to the designated Government onsite representative, which shall include the status of all work performed in the previous 24 hours, plans for the next 24 hours, any deviations from the established schedule, problems encountered, and items requiring Government disposition. This report shall be given at a time agreed to by contractor and government team.

b. DRD-2 Weekly Status Reports: Written reports to the Contracting Officer, with copy to the designated Government onsite representative, which shall include the status of all work performed in the previous 7 day period, plans for the next 7 day period, any deviations from the established schedule, problems encountered, and items requiring Government disposition. This report shall be provided by close of NASA AFRC business (4:00 PM Pacific Time) on the second work day of the following work week. Electronic mail or FAX is acceptable transmission media.

c. Other Data Reporting Documents (the Contractor shall provide the following data/reports in accordance with the due date specified in the DRD)

1) DRD-3 Completed Work Card Package

2) DRD-4 Non-Standard Repair Report

3) DRD-5 Structural Alteration Report

4) DRD-6 Noted But Not Corrected (NBNC) Discrepancies Report

5) DRD-7 Maintenance History Summary Report

6) DRD-8 Non-Destructive Inspection (NDI) Report

7) DRD-9 Airworthiness Certificate

8) DRD-10 Mishap Report(s)

9) DRD-11 Safety & Health Plan

12.0 Quality Assurance Requirements.

The Contractor shall provide and maintain a quality assurance and inspection program.

The Contractor’s inspection program shall ensure compliance with technical guidance, engineering specifications, and FAA regulations applicable to depot level maintenance of commercial air carrier aircraft. Documentation shall be required for traceability, accountability, and a historical record of design, testing, inspection, qualification, and acceptance of all materials and components. The Government will evaluate and audit the Quality Assurance Program, to include an onsite evaluation, prior to contract signing.

a. Quality System: The Contractor shall possess current FAA Repair Station certification to 14 C.F.R. Part 145. It is strongly desired by the Government that the Contractor possess current AS9100D, AS9110 third-party certification OR demonstrate AS9100D, AS9110 compliance. The Contractor shall comply with the following minimum process controls as follows:

1) Suppliers: The Contractor shall be responsible for Quality Assurance of vendors, suppliers, and subcontractors providing services under this contract to verify compliance with accepted standards. For those vendors who provide DOD or FAA certified parts and services, a copy of the valid certification shall be made available for Government audit. For those vendors who are not providing certified parts and services, the Contractor shall perform a survey to verify compliance with accepted standards.

2) Non-conformance: The Contractor shall have in place a procedure for reporting of nonconforming articles, materials, and equipment. (“Non-conformance” is defined as a condition of any article, material, or service in which one or more characteristics do not conform to the specified requirements. This includes failures, discrepancies, deficiencies, defects, anomalies, and malfunctions).

3) Inspection: The C-Check and O&A work cards will provide for verification buyoff of tasks by mechanics and inspectors. The Contractor shall provide aircraft inspectors to verify that work is performed in accordance with technical specifications and that the workmanship is airworthy. The inspectors shall ensure that all inspection documentation is completed in accordance with the work cards.

4) Tool Control: The Government strongly encourages the Contractor to utilize a system of positive tool control, including (but not limited to) shadowing of tool boxes.

5) Metrology: The Contractor shall have an acceptable metrology recall system in-place to ensure that all tools requiring calibration are current and in good working condition.

6) Government Source Inspection: All work performed on this contract shall be subject to inspection by the Government, NASA, or NASA designated personnel at any time. Government designated inspectors will provide follow up inspections to work performed on the aircraft, as designated on the work cards. These NASA inspectors will be designated in writing by the Contracting Officer as the Contracting Officer’s Representative (COR).

7) Quality Manual: The Contractor shall utilize a Quality Manual for use on this contract.

8) Documentation: Documentation and records of all non-routine (O&A) repairs shall be included along with the completed work cards. Documentation shall include signature sign-off and inspection compliance.

9) Warranties: The Contractor shall submit, and recover whenever possible, warranty claims for the Government for parts and labor. The Contractor shall maintain internal records of the warranty program, which shall be available for review by Government personnel. The Contractor shall pass through to the Government any supplier warranties acquired by the Contractor as a result of work performed under this contract.

NASA AFRC DC-8 Heavy Maintenance

ATTACHMENT 1 – AIRCRAFT DESCRIPTION

The following describes the significant modifications and the status of the aircraft as it will be delivered to the Contractor by the Government.

1. Experimenter Ports

1.1. Five Zenith ports have been added to the fuselage. Drive motors for port shutters will be removed.

1.1.1. Three left side 62° ports at FS 470, 1090 and 1130, respectively

1.1.2. One right side 62° port at FS 1310

1.1.3. One centerline port at FS 330

1.2. Four Nadir ports have been added to the fuselage. Drive motors for port shutters will be removed.

1.2.1. One left side 62° port at FS 1130

1.2.2. One right side 62° port at FS 1310

1.2.3. Two large centerline ports at FS 420 and 1200, respectively

1.3. Ten modified window ports have been installed replacing standard window ports. There will be window blanks installed at these locations.

1.3.1. Six left side ports at FS 330, 450, 570, 890, 1010, and 1290, respectively

1.3.2. Four right side ports at FS 530, 570, 1010 and 1290, respectively

2. Wing Pylons. The outer wings have hard points to allow for the installation of wing probes.

Wiring and GN2 purge lines have been routed along the leading edge wing spar cap. No pylons will be installed when the aircraft is delivered for maintenance.

3. APU Installation. The aircraft has been modified with the installation of an Auxiliary

Power Unit (APU) in the aft portion of the forward cargo pit. The APU is transverse-mounted with the inlet located on the lower left fuselage, forward of the wing leading edge and the exhaust located at a similar position on the right side of the aircraft. The actual APU will be removed prior to aircraft delivery.

4. Cockpit Intercom.

4.1. The DC-8 cockpit has been modified to accommodate headset operations at the Pilot, Co-Pilot and Flight Engineer stations. Boom microphone jacks have been added at the three stations to accommodate civilian style headsets.

4.2. The radio control panel microphone switch selection at all three stations switches microphone operation between handheld and boom/mask. The flight engineer station also incorporates a foot switch for hands free operation. A second guarded switch has been added at the three stations to switch between boom and mask when the radio switch is in the boom/mask position. This switch is located outboard of the Pilot and Co-Pilot seats at the forward edge of the map case and at the lower right edge of the Flight Engineer’s panel.

5. Ground Proximity Warning System (GPWS) Modification. A GPWS flap warning inhibit switch has been installed to eliminate nuisance warnings during practice landings with flaps out of the landing position. The switch overrides the flap position warning in the GPWS logic. The top half of the switch is lighted, with intensity controlled by the Co-Pilot’s instrument integral lighting. It is labeled “GPWS FLP INHIBIT”. The switch is a push button type with the lower half of the switch displaying “OVRD” in amber to indicate the flap position function of the GPWS has been overridden. The switch is located under the Co- Pilot’s glare shield near the GPWS INOP light.

6. Landing Gear Warning Cutoff Button Relocation. The landing gear warning cutoff has been moved from under the glare shield to the throttle quadrant, left of the flap handle.

7. TCAS II Installation. The aircraft is equipped with a TCAS II system. TA/VSIs are powered on the left and right DC emergency buses, and the display lights are controlled by the Pilot's and Co-Pilot's instrument light rheostats.

8. AC Outlets in Cockpit. There are three outlets in the cockpit to provide 115V, 60Hz, AC power limited to 5 amps. One outlet is located near the Co-Pilot station next to the intercom headset connector. The other two are located near the FE station, one on the floor and one on the side near the utility radio. Power to the cockpit outlets is provided through the mission manager distribution panel.

9. Stormscope. A Stormscope system is installed.

10. Cabin Lighting. The original lighting system was replaced with the FAA approved fluorescent type lighting system, which has been installed in the cabin sidewall and ceiling.

11. Relocated Forward Lavatory Vent Outlet. The forward lavatory vent outlet was relocated from approximately FS270, mid-level, to the lower level of the same FS270, just aft of the air conditioning access panel.

12. Mission Director Console. The Mission Director console is the main power distribution center for all experimenter payloads. A bank of fifteen 3.5KVA, 115VAC, 60Hz power converters located in the forward cargo pit is the primary power source for experimenters.

400Hz, three phase power is also distributed throughout the cabin area as well as limited 220VAC power. The Flight Engineer panel has been modified to provide a means of isolating the ship’s system power from experimenter power distribution.

13. KT-19 IR Camera (Shutter). A KT-19 IR camera and shutter mechanism is located in the air conditioner compartment at STA 240. The camera will be removed for delivery.

14. VHF Radio Upgrade to 8.33 KHz Channel Spacing. The VHF radio transceivers and control heads have been replaced with a new system to allow 8.33 kHz resolution on the channel spacing currently required in some European countries.

15. Center Tank Sump Strip Heater Removal. The center tank strip heaters have been removed to eliminate the chance of short circuit failures in the area. The circuit breakers providing power to the heaters have been collared and labeled “deactivated”. The scavenge pump circuit breaker has been collared and labeled “Ground use only above freezing.” The scavenge pump switch located on the Flight Engineer panel has also been labeled “Ground use only above freezing.”

16. Dual Power For Landing Gear Warning and Interlock. If power is lost to DC-bus 1, a relay will switch power from the dead bus to DC-bus 4. A circuit breaker from DC-bus 4 has been added at the circuit breaker panel adjacent to the existing landing gear warning and interlock circuit breaker on DC-bus 1.

17. Equipment Removals Prior to Delivery

17.1. Navigator’s Station

17.2. Support benches in aft “pit” area will be removed for delivery.

17.3. Converters in forward “pit” will be removed for delivery.

17.4. APU will be removed for delivery.

17.5. Mission Directors Console will be covered to prevent damage.

NASA AFRC DC-8 Heavy Maintenance

ATTACHMENT 2 – MSG WORKCARDS

Interval MPD ITEM

NUMBER TASK DESCRIPTION

1C 20-010-10-01 Lower Fuselage - Engine to Pylon Feeder Cables

1C 20-010-10-02 Lower Fuselage - Engine to Pylon Feeder Cables

1C 20-010-10-03 Lower Fuselage - Engine to Pylon Feeder Cables

1C 20-010-10-04 Lower Fuselage - Engine to Pylon Feeder Cables

1C 20-010-14-01 Lower Fuselage - EWIS Main Landing Gear Wheel Wells

1C 20-010-14-02 Lower Fuselage - EWIS Main Landing Gear Wheel Wells

1C 20-020-12-01 Upper Fuselage - EWIS Power Plant

1C 20-020-12-02 Upper Fuselage - EWIS Power Plant

1C 20-020-12-03 Upper Fuselage - EWIS Power Plant

1C 20-020-12-04 Upper Fuselage - EWIS Power Plant

1C 20-020-13-01 Upper Fuselage - EWIS Landing Gear and Gear Doors

1C 20-020-13-02 Upper Fuselage - EWIS Landing Gear and Gear Doors

1C 20-020-13-03 Upper Fuselage - EWIS Landing Gear and Gear Doors

1C 20-050-03-01 Left Wing - EWIS Left Wing Trailing Edge

NUMBER TASK DESCRIPTION

1C 20-060-03-01 Right Wing - EWIS Right Wing Trailing Edge

1C 21-022-06-01 Air Condition Distribution - Recirculation Fan Filter

1C 21-031-01-01 Aircraft Pressurization - Cabin Pressure Valves

1C 21-031-02-01 Aircraft Pressurization - Cabin Pressure Valves

1C 21-061-02-01 Cockpit/Cabin Temperature Control - Temperature Sensing Element

1C 23-070-01-01 Voice Recorder

1C 24-110-02-01 Constant Speed Drive - QAD Safety Wire

1C 24-110-02-02 Constant Speed Drive - QAD Safety Wire

1C 24-110-02-03 Constant Speed Drive - QAD Safety Wire

1C 24-110-02-04 Constant Speed Drive - QAD Safety Wire

1C 24-130-01-01 AC Generation and Control - Engine Generator Field Disconnect

1C 25-011-01-01 Flight Compartment Seats - Lubrication

1C 25-011-02-01 Flight Compartment Seats - Seat Belt Connecting Links

1C 25-011-03-01 Flight Compartment Seats - Shoulder Harness Reel Assembly

1C 25-011-04-01 Flight Compartment Seats - Seat Restraints

1C 25-011-05-01 Flight Compartment Seats - Seat Attachments

1C 25-011-06-01 Flight Compartment Seats - Seat Belt Attach Bolt

1C 25-023-02-01 Passenger/Attendant Seats - Attendant Shoulder Harness

1C 25-023-05-01 Passenger/Attendant Seats - Attendant Shoulder Harness

1C 25-023-07-01 Passenger/Attendant Seats - Seat Belt Attachment Bolt

1C 25-061-03-01 Emergency Equipment - Door Deployment System

1C 25-061-29-01 Emergency Equipment - Passenger Seat Cushions

1C 27-002-00-01 Horizontal Stabilizer Primary Control - Jackscrew

NUMBER TASK DESCRIPTION

1C 27-110-01-01 Aileron Mechanical Control - Load Feel Trim Assembly

1C 27-110-01-02 Aileron Mechanical Control - Load Feel Trim Assembly

1C 27-110-02-01 Aileron Mechanical Control - Aileron Control and Trim Cables

1C 27-110-02-02 Aileron Mechanical Control - Aileron Control and Trim Cables

1C 27-110-04-01 Aileron Mechanical Control - Aileron Bus Cable

1C 27-110-04-02 Aileron Mechanical Control - Aileron Bus Cable

1C 27-110-04-03 Aileron Mechanical Control - Aileron Bus Cable

1C 27-110-05-01 Aileron Mechanical Control - Aileron Lubrication

1C 27-110-05-02 Aileron Mechanical Control - Aileron Lubrication

1C 27-130-02-01 Aileron Hydraulic Actuation - Aileron Damper

1C 27-130-02-02 Aileron Hydraulic Actuation - Aileron Damper

1C 27-130-03-01 Aileron Hydraulic Actuation - Aileron Hydraulic Filter

1C 27-130-03-02 Aileron Hydraulic Actuation - Aileron Hydraulic Filter

1C 27-130-04-01 Aileron Hydraulic Actuation - Aileron Control Manual Reversion

1C 27-210-03-01 Rudder Controls/Indication and Trim - Rudder Trim and Load Feel Mechanism

1C 27-210-04-01 Rudder Controls/Indication and Trim - Rudder Trim and Load Feel Mechanism

1C 27-230-02-01 Rudder Hydraulic Actuation - Rudder Actuators

1C 27-230-03-01 Rudder Hydraulic Actuation - Filters

1C 27-230-03-02 Rudder Hydraulic Actuation - Filters

1C 27-230-03-03 Rudder Hydraulic Actuation - Filters

1C 27-410-01-01 Horizontal Stabilizer Primary Control - Electrical Control

1C 27-410-02-01 Horizontal Stabilizer Primary Control - Mechanical Control

NUMBER TASK DESCRIPTION

1C 27-410-04-01 Horizontal Stabilizer Primary Control - Jackscrew and Aft Bearings

1C 27-410-06-01 Horizontal Stabilizer Primary Control - Drive Chain

1C 27-510-01-01 Flap Mechanical Control - Flap Control Cables (Exposed)

1C 27-510-01-02 Flap Mechanical Control - Flap Control Cables (Exposed)

1C 27-510-01-03 Flap Mechanical Control - Flap Control Cables (Exposed)

1C 27-510-01-04 Flap Mechanical Control - Flap Control Cables (Exposed)

1C 27-510-03-01 Flap Mechanical Control - Flap Follow - up Cables (Exposed)

1C 27-510-03-02 Flap Mechanical Control - Flap Follow - up Cables (Exposed)

1C 27-510-06-01 Flap Mechanical Control - Flap Bus Cables (Exposed)

1C 27-510-06-02 Flap Mechanical Control - Flap Bus Cables (Exposed)

1C 27-510-07-01 Flap Mechanical Control - Flaps

1C 27-510-07-02 Flap Mechanical Control - Flaps

1C 27-510-08-01 Flap Mechanical Control - Flap Bridle Cables (Exposed)

1C 27-510-08-02 Flap Mechanical Control - Flap Bridle Cables (Exposed)

1C 27-510-08-03 Flap Mechanical Control - Flap Bridle Cables (Exposed)

1C 27-510-08-04 Flap Mechanical Control - Flap Bridle Cables (Exposed)

1C 27-610-03-01 Spoiler Mechanical Actuating System - Spoiler Cables (Exposed)

1C 27-610-03-02 Spoiler Mechanical Actuating System - Spoiler Cables (Exposed)

1C 27-610-03-03 Spoiler Mechanical Actuating System - Spoiler Cables (Exposed)

1C 27-610-03-04 Spoiler Mechanical Actuating System - Spoiler Cables (Exposed)

1C 27-800-04-01 Slot Mechanical Control and Indication - Doors and Latching Mechanism

1C 27-800-04-02 Slot Mechanical Control and Indication - Doors and Latching Mechanism

NUMBER TASK DESCRIPTION

1C 28-220-01-01 Engine Fuel Supply - Suction Feed System

1C 28-310-02-01 Fuel Dump System - Cables (Exposed)

1C 28-310-02-02 Fuel Dump System - Cables (Exposed)

1C 29-230-01-01 Electrically Driven Pumping, Auxiliary Hydraulic System - Emergency Reservoir

1C 29-310-01-01 Hydraulic Indication System

1C 30-300-01-01 Air Data Sensor and Drain Mast Heater System - Static Port Heaters

1C 31-310-01-01 Flight Recording System - Flight Recorder

1C 31-510-01-01 Aural Warning - Landing Gear

1C 32-240-01-01 Nose Gear Ground Sensing Mechanism - Cables (Exposed)

1C 32-310-02-01 Landing Gear Control - Cables (Exposed)

1C 32-310-02-02 Landing Gear Control - Cables (Exposed)

1C 32-310-02-03 Landing Gear Control - Cables (Exposed)

1C 32-310-04-01 Landing Gear Control - Anti - Retract Mechanism

1C 32-310-05-01 Landing Gear Control - Alternate Landing Gear Control

1C 32-440-04-01 Main Brake Control - Brake System Cables (Exposed)

1C 32-440-04-02 Main Brake Control - Brake System Cables (Exposed)

1C 32-440-07-01 Main Brake Control - Emergency Air Brake

1C 32-440-07-02 Main Brake Control - Emergency Air Brake

1C 32-440-08-01 Main Brake Control - Emergency Air Brake System Cables (Exposed)

1C 32-440-08-02 Main Brake Control - Emergency Air Brake System Cables (Exposed)

1C 32-450-02-01 Anti Skid System - Parking Brake

1C 32-510-01-01 Nosewheel Steering Mechanical Control - Steering Wheel, Follow - up Differential, Override

NUMBER TASK DESCRIPTION

1C 32-510-01-02 Nosewheel Steering Mechanical Control - Steering Wheel, Follow - up Differential, Override

1C 32-510-02-01 Nosewheel Steering Mechanical Control - Steering Wheel Cables (Exposed)

1C 32-700-02-01 Landing Gear and Landing Gear Doors

1C 32-700-02-02 Landing Gear and Landing Gear Doors

1C 32-700-02-03 Landing Gear and Landing Gear Doors

1C 33-140-01-01 Flood and Thunderstorm Lights - Emergency Power

1C 33-140-02-01 Flood and Thunderstorm Lights - Cockpit Flood Lights

1C 34-100-02-01 Air Data System - Pitot and Static Ports

1C 34-100-04-01 Air Data System - Static Selector System

1C 34-100-06-01 Air Data System - Standby Altimeter and Airspeed

1C 34-100-08-01 Air Data System - Altitude Alert

1C 34-190-01-01 Stall Warning

1C 34-190-02-01 Stall Warning - Lift Transducer

1C 34-190-03-01 Stall Warning - Stick Shaker

1C 34-230-02-01 Attitude - Attitude Switching

1C 34-290-02-01 Standby Compass

1C 35-200-02-01 Passenger Oxygen Supply and Distribution - Manual Eject Switch

1C 35-200-03-01 Passenger Oxygen Supply and Distribution - Pressure Regulators

1C 38-100-02-01 Potable Water System - Fill Cap Seal

1C 38-310-01-01 Lavatory Waste System - Drain and Fill Cap

1C 38-310-02-01 Lavatory Waste System - Drain Plumbing

1C 52-110-01-01 Forward Passenger Door - Mechanism

NUMBER TASK DESCRIPTION

1C 52-110-06-01 Forward Passenger Door - Pressure Seal

1C 52-120-01-01 Aft Passenger Door - Mechanism

1C 52-120-06-01 Aft Passenger Door - Pressure Seal

1C 52-200-01-01 Overwing Emergency Exit Door - Mechanism

1C 52-200-04-01 Overwing Emergency Exit Door - Pressure Seal Depressor

1C 52-200-05-01 Overwing Emergency Exit Door - Pressure Seal

1C 52-200-06-01 Overwing Emergency Exit Door - Mechanism

1C 52-300-01-01 Lower Cargo Doors (54 x 63) - Mechanism

1C 52-300-03-01 Lower Cargo Doors (54 x 63) - Pressure Seal Depressor

1C 52-300-04-01 Lower Cargo Doors (54 x 63) - Pressure Seal

1C 52-310-01-01 Lower Cargo Doors (36 x 44) - Mechanism

1C 52-310-01-02 Lower Cargo Doors (36 x 44) - Mechanism

1C 52-310-03-01 Lower Cargo Doors (36 x 44) - Pressure Seal Depressor

1C 52-310-03-02 Lower Cargo Doors (36 x 44) - Pressure Seal Depressor

1C 52-310-04-01 Lower Cargo Doors (36 x 44) - Pressure Seal

1C 52-310-04-02 Lower Cargo Doors (36 x 44) - Pressure Seal

1C 52-410-01-01 Forward Galley Service Door - Mechanism

1C 52-410-06-01 Forward Galley Service Door - Pressure Seal

1C 52-420-01-01 Aft Galley Service Door - Mechanism

1C 52-420-06-01 Aft Galley Service Door - Pressure Seal

1C 52-450-01-01 Air Conditioning and Accessory Compartment Door - Mechanism

1C 52-450-02-01 Air Conditioning and Accessory Compartment Door - Pressure Seal

NUMBER TASK DESCRIPTION

1C 52-710-01-01 Door Warning System

1C 52-800-02-01 Lower Cargo Doors and Surrounding Jambs

1C 52-800-02-02 Lower Cargo Doors and Surrounding Jambs

1C 52-800-03-01 Passenger Doors and Surrounding Jambs

1C 52-800-03-02 Passenger Doors and Surrounding Jambs

1C 52-800-03-03 Passenger Doors and Surrounding Jambs

1C 52-800-03-04 Passenger Doors and Surrounding Jambs

1C 52-800-03-05 Passenger Doors and Surrounding Jambs

1C 53-100-09-01 Nose Gear Wheel Well and Unpressurized Sidewalls

1C 53-100-12-01 Forward Cargo Compartment Bilge Area

1C 53-100-17-01 Midship Accessory Compartment, Forward Side of Center Wing

1C 53-100-19-01 L/H and R/H Main Gear Wheel Wells and Aft of Center Wing

1C 53-100-22-01 Aft Cargo Compartment Bilge Area

1C 53-107-04-01 Fuselage Interior - Cusp Extrusion and Fittings

1C 53-108-03-01 Forward Lower Cargo Compartment - Cusp Extrusion and Bilge

1C 53-108-03-02 Forward Lower Cargo Compartment - Cusp Extrusion and Bilge

1C 53-110-03-01 Aft Lower Cargo Compartment - Cusp Extrusion and Bilge

1C 53-110-03-02 Aft Lower Cargo Compartment - Cusp Extrusion and Bilge

1C 53-111-02-01 Main Landing Gear Wheel Wells - Wheel Well and Keel Beam

1C 53-111-02-02 Main Landing Gear Wheel Wells - Wheel Well and Keel Beam

1C 53-300-02-01 Aft Fuselage and Empennage

1C 53-300-03-01 Aft Fuselage

1C 56-120-01-01 Sliding Clearview Windows

1C 56-120-02-01 Sliding Clearview Windows

1C 56-120-03-01 Sliding Clearview Windows - Pressure Seal

1C 57-500-02-01 Left Wing Upper and Lower Surface

1C 57-500-06-01 Left Wing Fixed Trailing Edge Compartment

1C 57-600-02-01 Right Wing Upper and Lower Surface

1C 57-600-06-01 Right Wing Fixed Trailing Edge Compartment

Interval MPD ITEM NUMBER TASK DESCRIPTION

2C 20-020-07-01 Upper Fuselage - Pressure Panel and Frame Aft of Center Wing

2C 21-022-02-01 Air Condition Distribution - Cabin Air Exhaust Baffles

2C 21-022-03-01 Air Condition Distribution - Hot Air Check Valves

2C 21-022-05-01 Air Condition Distribution - Cabin Air Emergency Shut Off

2C 21-022-07-01 Air Condition Distribution - Ram Air Ventilation

2C 21-022-08-01 Air Condition Distribution - Ozone Converter

2C 21-031-06-01 Aircraft Pressurization - Outflow Drive

2C 21-033-01-01 Cabin Pressure Indication - Low Pressure Warning

2C 21-034-01-01 Cabin Pressure Relief - Cabin Positive Pressure Relief Valve

2C 21-034-02-01 Cabin Pressure Relief - Cabin Positive Pressure Relief Valve Filter

2C 21-034-03-01 Cabin Pressure Relief - Cargo Compartment Pressure Relief Valve

2C 21-034-03-02 Cabin Pressure Relief - Cargo Compartment Pressure Relief Valve

2C 21-053-02-01 Refrigeration Package - Heat Exchangers

2C 21-056-01-01 Auto Pack Shutdown

2C 25-061-07-01 Emergency Equipment - Cockpit Escape Lines

2C 26-210-02-01 Engine Fire Extinguishing - Firex Bottle

2C 26-210-03-01 Engine Fire Extinguishing - Agent Discharge System

2C 27-410-07-01 Horizontal Stabilizer Primary Control - Jackscrew

2C 28-220-03-01 Engine Fuel Supply - Fuel Low Level System

2C 29-120-01-01 Main Hydraulic Distribution and Control - Aspirator/Regulator Reservoir Valve and Relief Valve

2C 32-440-03-01 Main Brake Control - Despin System and Dual Brake Control Valves (SFAR 88)

2C 32-450-01-01 Anti Skid System - Antiskid Control Valves

2C 35-200-04-01 Passenger Oxygen Supply and Distribution - Aneroid Switch

2C 35-200-06-01 Passenger Oxygen Supply and Distribution - Manifold

2C 52-101-01-01 Forward Passenger Door - Exterior Surface

2C 52-101-02-01 Forward Passenger Door and Jamb - Interior

2C 52-102-01-01 Aft Passenger Door - Exterior Surface

2C 52-102-02-01 Aft Passenger Door and Jamb - Interior

2C 52-103-01-01 Forward Service Door - Exterior Surface

2C 52-103-02-01 Forward Service Door and Jamb - Interior

2C 52-104-01-01 Aft Service Door - Exterior Surface

2C 52-104-02-01 Aft Service Door and Jamb - Interior

2C 52-105-01-01 Left Overwing Exit Doors - Exterior Surface

2C 52-105-02-01 Left Overwing Exit Doors and Jambs - Interior

2C 52-106-01-01 Right Overwing Exit Doors - Exterior Surface

2C 52-106-02-01 Right Overwing Exit Doors and Jambs - Interior

2C 52-107-01-01 Left Forward Type 1 Emergency Exit Doors - Exterior Surface

2C 52-108-01-01 Right Forward Type 1 Emergency Exit Doors - Exterior Surface

2C 52-109-01-01 Left Aft Type 1 Emergency Exit Doors - Exterior Surface

2C 52-110-05-01 Forward Passenger Door - Pressure Seal Depressor

2C 52-110-11-01 Right Aft Type 1 Emergency Exit Doors - Exterior Surface

2C 52-110-12-01 Right Aft Type 1 Emergency Exit Door and Jamb - Interior

2C 52-111-01-01 Forward Lower Cargo, Forward Door - Exterior Surface

2C 52-111-02-01 Forward Lower Cargo, Forward Door and Jamb - Interior

2C 52-112-01-01 Forward Lower Cargo, Aft Door - Exterior Surface

2C 52-112-02-01 Forward Lower Cargo, Aft Door and Jamb - Interior

2C 52-113-01-01 AFt Lower Cargo, Forward Door - Exterior Surface

2C 52-113-02-01 Aft Lower Cargo, Forward Door and Jamb - Interior

2C 52-114-01-01 Aft Lower Cargo, Aft Door - Exterior Surface

2C 52-114-02-01 Aft Lower Cargo, Aft Door and Jamb - Interior

2C 52-117-01-01 Air Conditioning Compartment Access Door and Jamb - Exterior Surface

2C 52-117-02-01 Air Conditioning Compartment Access Door and Jamb - Interior

2C 52-118-01-01 Midship Accessory Compartment Door - Exterior Surface

2C 52-118-02-01 Midship Accessory Compartment Door and Jamb - Interior

2C 52-120-05-01 Aft Passenger Door - Pressure Seal Depressor

2C 52-300-05-01 Lower Cargo Doors (54 x 63) - Latching Pin and Jamb Fitting

2C 52-410-05-01 Forward Galley Service Door - Pressure Seal Depressor

2C 52-420-05-01 Aft Galley Service Door - Pressure Seal Depressor

2C 52-540-01-01 Flight Compartment Door - Blowout Panels

2C 53-101-01-01 Fuselage Exterior - Exterior Surface, Nose and Main Fuselage

2C 53-102-02-01 Radome Compartment Interior - Interior Structure

2C 53-103-02-01 Turbo Compressor and Doppler Antenna Compartments - Interior Structure

2C 53-104-02-01 Nose Landing Gear Well, Tunnels and Doors - Interior Structure

2C 53-105-02-01 Air Conditioning Accessory Compartment - Interior Structure

2C 53-106-02-01 Flight Deck - Interior Structure

2C 53-107-02-01 Fuselage Interior - Interior Structure

2C 53-107-02-02 Fuselage Interior - Interior Structure

2C 53-108-02-01 Forward Lower Cargo Compartment - Tunnels - Interior

2C 53-108-04-01 Forward Lower Cargo Compartment - Tunnels - Interior

2C 53-109-02-01 Midship Accessory Compartment - Interior

2C 53-110-02-01 Aft Lower Cargo Compartment - Interior Structures

2C 53-112-02-01 Aft Fuselage and Tail Section - Interior Structure

2C 53-200-15-01 Pressure Panel and Frame Area

2C 54-101-05-01 Engine Pylon - Upper Spar Reinforcement

2C 54-101-05-02 Engine Pylon - Upper Spar Reinforcement

2C 54-101-05-03 Engine Pylon - Upper Spar Reinforcement

2C 54-101-05-04 Engine Pylon - Upper Spar Reinforcement

2C 55-101-02-01 Horizontal Stabilizer - Interior Structure

2C 55-101-02-02 Horizontal Stabilizer - Interior Structure

2C 55-103-01-01 Elevator and Tabs - Interior Structure

2C 55-103-01-02 Elevator and Tabs - Interior Structure

2C 55-103-02-01 Elevator and Tabs - Interior Structure

2C 55-103-02-02 Elevator and Tabs - Interior Structure

2C 55-104-02-01 Horizontal Stabilizer Outer Section and Elevator - Exterior Surface

2C 55-104-02-02 Horizontal Stabilizer Outer Section and Elevator - Exterior Surface

2C 55-201-02-01 Vertical Stabilizer and Tip - Interior Structure

2C 55-202-01-01 Rudder - Interior Structure

2C 55-202-02-01 Rudder - Interior Structure

2C 55-300-06-01 Horizontal Stabilizer Center Box Section

2C 56-010-01-01 Windshield

2C 56-NAS-01-01 NASA Unique Viewports

2C 56-NAS-01-02 NASA Unique Viewports

2C 56-NAS-01-03 NASA Unique Viewports

2C 56-NAS-01-04 NASA Unique Viewports

2C 56-NAS-01-05 NASA Unique Viewports

2C 56-NAS-01-06 NASA Unique Viewports

2C 56-NAS-01-07 NASA Unique Viewports

2C 56-NAS-01-08 NASA Unique Viewports

2C 56-NAS-01-09 NASA Unique Viewports

2C 56-NAS-01-10 NASA Unique Viewports

2C 56-NAS-01-11 NASA Unique Viewports

2C 56-NAS-01-12 NASA Unique Viewports

2C 56-NAS-01-13 NASA Unique Viewports

2C 56-NAS-01-14 NASA Unique Viewports

2C 56-NAS-01-15 NASA Unique Viewports

2C 56-NAS-01-16 NASA Unique Viewports

2C 56-NAS-01-17 NASA Unique Viewports

2C 56-NAS-01-18 NASA Unique Viewports

2C 56-NAS-01-19 NASA Unique Viewports

2C 57-101-02-01 Center Wing - Interior Structure

2C 57-201-02-01 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-02 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-03 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-04 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-05 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-06 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-07 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-201-02-08 Wing Box (XCW=69.5 to XCW=761.695 - Interior Structure

2C 57-202-01-01 Wing Exterior, Upper and Lower - Exterior Structure

2C 57-202-01-02 Wing Exterior, Upper and Lower - Exterior Structure

2C 57-202-01-03 Wing Exterior, Upper and Lower - Exterior Structure

2C 57-202-01-04 Wing Exterior, Upper and Lower - Exterior Structure

2C 57-202-01-05 Wing Exterior, Upper and Lower - Exterior Structure

2C 57-202-01-06 Wing Exterior, Upper and Lower - Exterior Structure

2C 57-203-02-01 Wing Leading Edge - Interior

2C 57-203-02-02 Wing Leading Edge - Interior

2C 57-204-02-01 Trailing Edge and Flight Controls - LH and RH Flap and Exhaust Gate, Interior

2C 57-204-02-02 Trailing Edge and Flight Controls - LH and RH Flap and Exhaust Gate, Interior

2C 57-204-03-01 Trailing Edge and Flight Controls - LH and RH Trailing Edge, Flapwell

2C 57-204-03-02 Trailing Edge and Flight Controls - LH and RH Trailing Edge, Flapwell

2C 57-204-05-01 Trailing Edge and Flight Controls - LH and RH Aileron, Interior

2C 57-204-05-02 Trailing Edge and Flight Controls - LH and RH Aileron, Interior

2C 71-400-05-01 Pylons

2C 71-400-05-02 Pylons

2C 71-400-05-03 Pylons

2C 71-400-05-04 Pylons

NUMBER TASK DESCRIPTION

3C 20-010-01-01 Lower Fuselage - Air Conditioning Accessory Compartment

3C 20-010-02-01 Lower Fuselage - Forward Cargo Compartment

3C 20-010-03-01 Lower Fuselage - Between Cabin Floor and Center Wing

3C 20-010-04-01 Lower Fuselage - Center Wing Vapor Barrier

3C 20-010-05-01 Lower Fuselage - Center Wing Fuel Tank Wiring

3C 20-010-06-01 Lower Fuselage - Midship Accessory Compartment

3C 20-010-07-01 Lower Fuselage - Aft Cargo Compartment

3C 20-010-08-01 Lower Fuselage - Aft Accessory Compartment

3C 20-010-09-01 Lower Fuselage - Electrical Main Feeder Cables

3C 20-010-11-01 Lower Fuselage - EWIS Forward Lower Cargo Compartment

3C 20-010-12-01 Lower Fuselage - EWIS Midship Accessory Compartment

3C 20-010-13-01 Lower Fuselage - EWIS Aft Cargo Compartment

3C 20-020-01-01 Upper Fuselage - Cockpit

3C 20-020-02-01 Upper Fuselage - Main Cabin, F.S. 25 TO F.S. 80

3C 20-020-03-01 Upper Fuselage - Main Cabin, F.S. 80 TO F.S. 620

3C 20-020-04-01 Upper Fuselage - Main Cabin, F.S. 620 TO F.S. 1020

3C 20-020-05-01 Upper Fuselage - Main Cabin, F.S. 1020 TO F.S. 1620

3C 20-020-06-01 Upper Fuselage - Main Cabin, F.S. 1620 TO F.S. 1766

3C 20-020-08-01 Upper Fuselage - EWIS Center Fuel Tank

3C 20-020-09-01 Upper Fuselage - EWIS Center Wing Exterior

3C 20-020-09-02 Upper Fuselage - EWIS Center Wing Exterior

NUMBER TASK DESCRIPTION

3C 20-020-10-01 Upper Fuselage - EWIS Cockpit

3C 20-020-11-01 Upper Fuselage - EWIS Main Cabin

3C 20-020-14-01 Upper Fuselage - EWIS Air Conditioning Accessory Compartment

3C 20-050-01-01 Left Wing - Fuel Tank Wiring

3C 20-050-02-01 Left Wing - EWIS Left Wing Center Section

3C 20-050-04-01 Left Wing - EWIS Left Wing Forward Auxiliary Fuel Tank

3C 20-060-01-01 Right Wing - Fuel Tank Wiring

3C 20-060-02-01 Right Wing - EWIS Right Wing Center Section

3C 20-060-04-01 Right Wing - EWIS Right Wing Forward Auxiliary Fuel Tank

3C 23-060-01-01 Static Dischargers

3C 23-060-01-02 Static Dischargers

3C 23-060-01-03 Static Dischargers

3C 23-060-01-04 Static Dischargers

3C 23-060-01-05 Static Dischargers

3C 27-110-03-01 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-03-02 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-03-03 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-03-04 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-03-05 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-03-06 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-03-07 Aileron Mechanical Control - Aileron Control and Trim Cables

3C 27-110-06-01 Aileron Mechanical Control - Aileron Torque and Override Assembly

NUMBER TASK DESCRIPTION

3C 27-210-01-01 Rudder Controls/Indication and Trim - Cables

3C 27-210-01-02 Rudder Controls/Indication and Trim - Cables

3C 27-210-01-03 Rudder Controls/Indication and Trim - Cables

3C 27-210-01-04 Rudder Controls/Indication and Trim - Cables

3C 27-210-01-05 Rudder Controls/Indication and Trim - Cables

3C 27-210-01-06 Rudder Controls/Indication and Trim - Cables

3C 27-210-01-07 Rudder Controls/Indication and Trim - Cables

3C 27-300-01-01 Elevator Mechanical Control - Cables

3C 27-300-01-02 Elevator Mechanical Control - Cables

3C 27-300-01-03 Elevator Mechanical Control - Cables

3C 27-300-01-04 Elevator Mechanical Control - Cables

3C 27-300-01-05 Elevator Mechanical Control - Cables

3C 27-300-01-06 Elevator Mechanical Control - Cables

3C 27-300-01-07 Elevator Mechanical Control - Cables

3C 27-410-03-01 Horizontal Stabilizer Primary Control - Cables

3C 27-410-03-02 Horizontal Stabilizer Primary Control - Cables

3C 27-410-03-03 Horizontal Stabilizer Primary Control - Cables

3C 27-410-03-04 Horizontal Stabilizer Primary Control - Cables

3C 27-410-03-05 Horizontal Stabilizer Primary Control - Cables

3C 27-410-03-06 Horizontal Stabilizer Primary Control - Cables

3C 27-410-03-07 Horizontal Stabilizer Primary Control - Cables

3C 27-450-01-01 Horizontal Stabilizer Position Indication and Warning - Cables

NUMBER TASK DESCRIPTION

3C 27-450-01-02 Horizontal Stabilizer Position Indication and Warning - Cables

3C 27-450-01-03 Horizontal Stabilizer Position Indication and Warning - Cables

3C 27-450-01-04 Horizontal Stabilizer Position Indication and Warning - Cables

3C 27-450-01-05 Horizontal Stabilizer Position Indication and Warning - Cables

3C 27-450-01-06 Horizontal Stabilizer Position Indication and Warning - Cables

3C 27-450-01-07 Horizontal Stabilizer Position Indication and Warning - Cables

3C 27-510-02-01 Flap Mechanical Control - Flap Control Cables (Unexposed)

3C 27-510-02-02 Flap Mechanical Control - Flap Control Cables (Unexposed)

3C 27-610-02-01 Spoiler Mechanical Actuating System - Spoiler Cables (Unexposed)

3C 27-610-02-02 Spoiler Mechanical Actuating System - Spoiler Cables (Unexposed)

3C 27-610-02-03 Spoiler Mechanical Actuating System - Spoiler Cables (Unexposed)

3C 27-610-02-04 Spoiler Mechanical Actuating System - Spoiler Cables (Unexposed)

3C 28-310-03-01 Fuel Dump System - Cables (Unexposed)

3C 30-100-01-01 Airfoil Anti - Icing - Tail Duct Pressure/Differential Switch

3C 32-240-02-01 Nose Gear Ground Sensing Mechanism - Cables (Unexposed)

3C 32-310-03-01 Landing Gear Control - Cables (Unexposed)

3C 32-310-03-02 Landing Gear Control - Cables (Unexposed)

3C 32-310-03-03 Landing Gear Control - Cables (Unexposed)

3C 32-310-03-04 Landing Gear Control - Cables (Unexposed)

3C 32-310-03-05 Landing Gear Control - Cables (Unexposed)

3C 32-440-05-01 Main Brake Control - Brake System Cables (Unexposed)

3C 32-440-05-02 Main Brake Control - Brake System Cables (Unexposed)

NUMBER TASK DESCRIPTION

3C 32-440-05-03 Main Brake Control - Brake System Cables (Unexposed)

3C 32-440-05-04 Main Brake Control - Brake System Cables (Unexposed)

3C 32-440-09-01 Main Brake Control - Emergency Air Brake System Cables (Unexposed)

3C 32-440-09-02 Main Brake Control - Emergency Air Brake System Cables (Unexposed)

3C 32-440-09-03 Main Brake Control - Emergency Air Brake System Cables (Unexposed)

3C 32-440-09-04 Main Brake Control - Emergency Air Brake System Cables (Unexposed)

3C 32-440-09-05 Main Brake Control - Emergency Air Brake System Cables (Unexposed)

3C 32-440-09-06 Main Brake Control - Emergency Air Brake System Cables (Unexposed)

3C 32-440-11-01 Main Brake Control - Emergency Air Brake

3C 32-510-03-01 Nosewheel Steering Mechanical Control - Steering Cables (Unexposed)

3C 32-510-03-02 Nosewheel Steering Mechanical Control - Steering Cables (Unexposed)

3C 52-110-02-01 Forward Passenger Door - Mechanism

3C 52-120-02-01 Aft Passenger Door - Mechanism

3C 52-200-02-01 Overwing Emergency Exit Door - Mechanism

3C 52-300-02-01 Lower Cargo Doors (54 x 63) - Mechanism

3C 52-310-02-01 Lower Cargo Doors (36 x 44) - Mechanism

3C 52-310-02-02 Lower Cargo Doors (36 x 44) - Mechanism

3C 52-310-05-01 Lower Cargo Doors (36 x 44) - Door Stops

3C 52-310-05-02 Lower Cargo Doors (36 x 44) - Door Stops

3C 52-410-02-01 Forward Galley Service Door - Mechanism

3C 52-420-02-01 Aft Galley Service Door - Mechanism

3C 52-450-03-01 Air Conditioning and Accessory Compartment Door - Latch Mechanism and Track

NUMBER TASK DESCRIPTION

3C 52-800-01-01 Doors (Passenger and Cargo)

3C 53-100-02-01 Lower Fuselage including Radome and Upper and Lower Wing to Fuselage Fillets

3C 53-100-03-01 Radome, including Forward Face of Turbo Compressor Compartment Bulkhead

3C 53-100-04-01 Antenna Compartment

3C 53-100-05-01 Turbo Compressor Compartment Bulkhead

3C 53-100-06-01 Air Conditioning Accessory Compartment

3C…