SOW_ATTACHMENT_D_Operational_and_Flight_Check_Requirements.pdf
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- Attached to
- A-10 Thunderbolt Advanced-Wing Continuation Kit (ATTACK) Federal contract opportunity
- Solicitation number
- FA8202-18-R-1001
About this file
This statement of work attachment defines operational ground checks and functional check flight procedures for the A-10 Thunderbolt Advanced-Wing Continuation Kitting contract opportunity. Key requirements include conducting continuity checks, leak checks, system checkouts for components like the data transfer system, countermeasures dispense system, electronic warfare systems, external and internal armament systems, lighting, fuel and hydraulic systems, and flight control systems. Acceptable flight parameters and performance specifications are also defined by aircraft manuals.
The related solicitation seeks to award a contract for A-10 Thunderbolt Advanced-Wing Continuation Kitting to add structural components that extend the service life of A-10 aircraft. Interested offerors must be registered and certified to handle export-controlled technical data. The Department of the Air Force Materiel Command Lifecycle Management Center at Hill Air Force Base is the contracting agency.
SOW Attachment D - Operational and Flight Check Requirements
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Text version
STATEMENT OF WORK
ATTACHMENT D
OPERATIONAL AND FLIGHT CHECK
REQUIREMENTS
FOR
A-10 THUNDERBOLT ADVANCED-WING
CONTINUATION KITTING
(ATTACK)
22 Jan 2018
Prepared by:
AFLCMC/WWAP
Fighter/Bomber Directorate
Hill AFB, Utah 84056
REVISION CONTROL
Note: The portion of the text affected by the current revision is indicated by vertical black lines in the outer left hand margin.
Revision Date Description Pages Changed
Initial 22 JAN 2018 Initial Release
1. PURPOSE
This attachment to the Statement of Work (SOW) defines the Operational Ground Checks (Ops
Checks) and Functional Check Flight (FCF) procedures used by the government during and after
ATTACK Wing Assembly installation on a functional A-10 aircraft. This list may not be all inclusive and is included for contractor reference only. For additional procedures and checks performed during installation of the ATTACK Wing Assembly, reference TCTO 1A-10C-520.
Ops Checks:
Continuity check (TO 1A-10C-2-110-1).
Reinstall Protective Caps for Connectors 9361J3, 9361J4 and 9461J34 on Pylon Station 1
(TO 1-1A-14)
Reinstall Protective Caps for Connectors 9362J3, 9362J4 and 9462J34 on Pylon Station
11 (TO 1-1A-14)
Operational checkout of DC power system (TO 1A-10C-2-24JG-2).
Operational checkout of emergency power system (TO 1A-10C-2-24JG-3).
Operational checkout of master caution system (TO 1A-10C-2-24JG-6).
Leak Check of Aerial and Ground Refueling Manifold Assemblies (TO 1A-10C-2-28JG-
3).
Anti-Skid System Checkout (TO 1A-10C-2-32JG-4).
Operational Checkout of Data Transfer System (TO 1A-10C-2-34JG-9).
Countermeasures Dispense System Checkout (TO 1A-10C-2-93JG-5-1).
o Operational Checkout of Countermeasures Dispense System using TSS-
4485/ALM-288.
o Operational Checkout, Dispense System Station #1 thru #4.
o Operational Checkout, General.
o Operational Checkout, Initialization.
Electronic Warfare ALQ System Checkout (TO 1A-10C-2-93JG-2-1).
o ALQ-184 and ALQ-131 Test Using Test Set AN/USM-670.
o Cockpit-to-Pod Wiring Checkout with ECM Pod Wiring Tester and ALQ-213
Cockpit Adapter (CMS Aircraft).
o ECM Pod Operational Checkout, Countermeasures Set (CMS) AN/ALQ-213(V)2
System ECM POD, Operational Checkout.
External Armament System Checkout (TO 1A-10C-2-94JG-7).
o CICU LRU IBIT for HOTAS.
o Operational Check of CICU.
o Operational Check of AIM-9 Missile Control System.
o Operational Check of Integrated Data and Weapons Management System
(IDWMS).
o Operational Check TGM-65 B/D/E/G/G2 or CATM-65 K.
Operational Checkout of External Fuel Feed System with Alternate External Fuel Tank
Preinstallation Tester (TO 1A-10C-2-28JG-4).
Operational Checkout of Exterior Lighting and NVIS Lighting System (TO 1A-10C-2-
24JG-5).
o Position Lights Check.
o Formation Lights Check.
o Anti-collision Lights Check.
o Landing and Taxi Light Check.
Fuel Feed/Vent System Checkout (TO 1A-10C-2-28JG-1).
o Operational Check of Fuel System (Without external Fuel Tanks).
Fuel Quantity Indicating and Warning System Checkout (TO 1A-10C-2-28JG-5).
o Operational Checkout of Fuel Quantity Indicating System (Full Tanks).
o Operational Checkout of Fuel Quantity Indicating System (Empty Tanks).
o Aircraft Capacitance and Resistance Check of Fuel Probes and Harness (With
Test Sets P/N 361-022-002 and P/N 361-015-001) or Aircraft Capacitance and
Resistance Check of Fuel Probes and Harness (With Test Sets P/N 361-022-002 and P/N PSD60-1AF).
o Calibration of Fuel Quantity Indicating System.
Fuel System Leak Check During Ground Refueling (TO 1A-10C-2-12JG-1).
Hydraulic System Service and Bleed (TO 1A-10C-2-12JG-1).
Operational Checkout of AN/ARN-108(V) Instrument Landing System (ILS), Using
972Q4 Test Set or Operational Checkout of AN/ARN-108(V) Instrument Landing
System (ILS), Using AN/ARM-201 Radio Test Set or Operational Checkout of
AN/ARN-108(V) Instrument Landing System (ILS), Using IFR-4000 Test Set (TO 1A-
10C-2-34JG-6).
Internal Armament System Checkout (TO 1A-10C-2-94JG-6).
o Operational Checkout of 30MM Gun System..
Operational Checkout/Maintenance BIT Check of LASTE System (TO 1A-10C-2-94JG-
10).
Leading Edge Slat System Checkout (TO 1A-10C-2-27JG-1).
o Alpha Mach and Audio Stall Warning System Checkout.
o Slat Extension and Retraction Check.
o Slat Operating Time Check.
o Slat Seal Check.
MLG Brake System Checkout (TO 1A-10C-2-32JG-4).
o Anti-Skid Operational Checks.
o Bleed of Main Landing Gear Brakes.
o Normal Operation Check.
o Emergency Operation Check.
MLG Shock Strut Servicing (TO 1A-10C-2-12JG-1)
MLG System Checkout.
o Rig MLG Aft Door and Mechanism (TO 1A-10C-2-32JG-1).
o Bleed MLG Drag Strut Actuator (TO 1A-10C-2-32JG-1).
o Rig MLG Strut Fairing Assembly (TO 1A-10C-2-32JG-1).
o Rig MLG Torque Arm Fairing (TO 1A-10C-2-32JG-1).
o Adjust MLG Uplock Cylinder and Upstop Pad Assembly (TO 1A-10C-2-32JG-1).
o Landing Gear System Leak Check (TO 1A-10C-2-32JG-1).
o Landing Gear Auxiliary Extension Check (TO 1A-10C-2-32JG-2).
o Landing Gear Retraction for Control System Check (TO 1A-10C-2-32JG-2).
o Landing Gear Retraction for Flight Safety Circuit Check (TO 1A-10C-2-32JG-2).
o Landing Gear Warning Horn Check (TO 1A-10C-2-32JG-2).
o Adjust MLG Uplock Switch (TO 1A-10C-2-32JG-2).
o Adjust Weight On Wheels Switch (TO 1A-10C-2-32JG-2).
Operational Check of Electrical and Avionics Compartment Cooling Blowers and
Interlock Switches (TO 1A-10C-2-21JG-3).
Bleed Air Leak Detection System Operational Test (TO 1A-10C-2-21JG-2, Chapter 2
Step 2).
Multifunction Color Display System (TO 1A-10C-2-94JG-3).
o Operational Checkout of Multifunction Color Display (MFCD) System.
o Video and Wiring Check of Multifunction Color Display (MFCD) and Electro-
Optical (EO) Munition Check.
Nose Wheel Steering Engagement Test (TO 1A-10C-2-32JG-3).
Pitot-Static System Checkout (TO 1A-10C-2-34JG-2).
o Purge Pitot Pressure Line.
o Pitot-Static Tube Heater Check.
o Pitot-Static Leak Check.
o Purge Static Pressure Line.
Roll Flight Control System Checkout (TO 1A-10C-2-27JG-5).
o Rigging Aileron Actuator.
o Aileron Actuator Piston Rod End Alignment (Chapter 14, Para 14-1-2, Steps 8 through 25).
o Aileron Actuator Stability Check.
o Checking Aileron and Aileron Servo Tab Neutral.
o Aileron Fine Trim Rigging.
o Aileron Hydraulic Leakage Check.
o Aileron Travel Check.
o Aileron Trim Check.
o Control Cable Tension Adjustment.
o Rigging Feel and Trim Device.
o Leading Edge Aileron Neutral Set Check.
o Lubricate Aileron Actuator (TO 1A-10C-6WC-2).
o Manual Reversion Check.
o Rigging Mechanical Subsystem.
o Roll Feel Device Check.
o Rigging Servo Tab Shifter and Servo Tab.
Simultaneous Localizer and Glide Slope Checkout (TO 1A-10C-2-34JG-6).
Checkout and Adjustment of Speed Brake Position LVDT (TO 1A-10C-2-27JG-3).
Speed Brake System Checkout (TO 1A-10C-2-27JG-2).
o Deceleron Camber Rigging.
o Emergency Retraction Check.
o In-Flight Limitation Check.
o Speed Brake Pinch Check.
o Rigging Speed Brakes.
o Speed Brake Travel Check.
o Synchronization Check.
Control Stick Shaker Check (TO 1A-10C-2-34JG-2).
Trailing Edge Flap System Checkout (TO 1A-10C-2-27JG-1).
o Automatic Electrical Blowback Operational Check.
o Emergency Retract Check.
o Flap Indicating System Operational Check/Calibration.
o Ground Safety Check.
o Normal Flap Extension and Retraction Check.
o Rigging Trailing Edge Flap System.
Weapons Station Check (TO 1A-10C-2-40MS-1 PATS-35 or 1A-10C-2-15JG-3 PATS-
70).
o TGP Station Checkout.
o 1760 Weapons Station Check.
Functional Check Flight Procedures:
Check that the following systems work properly, IAW TO 1A-10C-6CF-1:
Fuel system/gauges
Landing gear
Flaps
Primary flight controls o Pitch and roll trim o Speed brake o Speed brake warning system
Slats
Primary flight controls in manual reversion
Ensure the following are within limits IAW TO 1A-10C-1:
Stores/carriage limits
Load factors
Stall speeds, stall performance
Manual reversion stick forces
Aileron disconnect
Ensure the following are within limits IAW TO 1A-10C-1-1:
Takeoff speed, takeoff ground run
Climb (max thrust, single engine)
Cruise and service ceiling
Specific range
Max endurance
Level flight max speed
Turn performance, turn rate/radius
Final approach speed
Landing roll distance
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