BY ORDER OF THE COMMANDER AIR COMBAT COMMAND
AIR FORCE INSTRUCTION 21103_ACCSUP_ADDENDUM_F 2 FEBRUARY 2015 Maintenance EQUIPMENT INVENTORY, STATUS, AND UTILIZATION REPORTING SYSTEM/ EC130H MINIMUM ESSENTIAL SUBSYSTEM LIST (MESL)
COMPLIANCE WITH THIS PUBLICATION IS MANDATORY ACCESSIBILITY: Publications and forms are available on the e-Publishing website at www.e-Publishing.af.mil for downloading or ordering. RELEASABILITY: There are no releasability restrictions on this publication. OPR: HQ ACC/A4CA-EC130H Supersedes:
AFI 21103_ACCSUP_ADD_F, 6 AUGUST 2013
Certified by: HQ ACC/A4C (Col Charles D. Johnson) Pages: 16
This MESL complements AFI 21-103, Equipment Inventory, Status, and Utilization Reporting. It applies to all EC-130H ACC units. This Addendum does not apply to Air National Guard (ANG) or Air Force Reserve Command (AFRC) units and members. Ensure that all records created as a result of processes prescribed in this publication are maintained IAW Air Force Manual (AFMAN) 33-363, Management of Records, and disposed of IAW the Air Force Records Information Management System (AFRIMS) Records Disposition Schedule (RDS). Contact supporting records managers as required. Send recommended changes or comments on AF Form 847, Recommendation for Change of Publication, to HQ ACC/A4CA-EC130H, 219 Dodd Blvd, Langley AF VA 23665, and send information copies to the applicable Office of Collateral Responsibility (OCR). OCR: HQ ACC/A4Q. This publication may not be supplemented or further implemented/extended. The authorities to waive wing/unit level requirements in this publication are identified as T-2. See AFI 33-360, Publications and Forms Management, for a description of the authorities associated with the Tier numbers. SUMMARY OF CHANGES Revised to reflect restructure of prime mission equipment work unit codes. Included Baseline-2, Large Aircraft Infrared Countermeasures (LAIRCM) system, Modern Comms Receive (MCR) subsystem, Intelligence Broadcast Receiver (IBR), Counter Radar Subsystem (CRS), and new
2
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
Special Systems Air Conditioning (SSAC) subsystems. configuration. Corrected minor errors and omissions.
Removed references to Baseline-0
1. General. The MESL is the basis of status reporting IAW AFI 21-103. MESLs lay the ground work for reporting the status of aircraft capability. They list the minimum essential systems and subsystems that must work on an aircraft for it to perform specifically assigned unit wartime, training, test or other missions. Mission Ready Available (MRA) is used in readiness Status of Resources and Training System (SORTS) reporting only and denotes Mission Capable (MC) aircraft capable of being configured for a contingency mission in accordance with COMACC OMNIBUS Plan. 1.1. Notes. Qualifying notes are used to define aircraft exceptions and help explain complex degraded mission systems such as prime mission equipment (PME). 1.2. Status. Aircraft status for generation and deployment: The goal is to generate or deploy Fully Mission Capable (FMC) aircraft, recognizing status actually achieved may be less than FMC. A Not Mission Capable (NMC) aircraft may be deployed provided it is safe for flight and can be configured and generated to MRA status at an employment site. 1.3. Generation. All ACC units will generate, or deploy and regenerate, using ACC MESLs. Major Command differences in MESLs are acknowledged. Upon actual deployment to another MAJCOM theater, the gaining MAJCOM has the responsibility to resource and specify the unit's requirements and resource the differences in support/mission equipment. 1.4. Reading the MESL. A MESL is read by comparing the systems stated by work unit code (WUC) against the Full Systems List (FSL) and all applicable Basic Systems List (BSL) across the page. Each unit's Design Operational Capability (DOC) statement determines applicability of BSL columns in Table 1., EC-130H MESL. The aircraft MESLs incorporate all ACC assigned aircraft; therefore, it is important to compare only those columns listed in the MESL that are applicable to the unit's assigned aircraft. For example, units with CC (wartime) coded aircraft would determine and report status using only the FSL and BSL columns related to their DOC statement. Units with TF (training) coded aircraft would determine and report status using only the FSL and TNG columns, and units with CB (test) coded aircraft would determine and report status using only the FSL and TST columns. Units with multiple coded aircraft will ensure status is reported using the MESL columns appropriate to the individual aircraft assignment code. 1.4.1. EC-130H Unique Mission Codes: 1.4.1.1. EAC—Electronic Attack, Counter Communications Systems 1.4.1.2. EAN—Electronic Attack, Counter Navigational Systems 1.4.1.3. EAR—Electronic Attack, Counter Radar Systems
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
3
Table 1. EC-130H MESL BSL NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
X1
X1
X1
X1
11 - AIRFRAME 1.
11
Airframe
12 – COCKPIT AND FUSELAGE 2.
12C
Special Systems Crew Seating
X2
X2
X2
X2
3.
122
Flight Deck Crew Seating
X
X
X
X
4.
125
Aft Cargo
X3
X3
X3
X3
X
X
X
X
X
X4
X4
X4
X
X5
X5
X5
X
X
X
X7
X7
X7
X7
13 – LANDING GEAR 5.
13
Landing Gear
14 – FLIGHT CONTROL 6.
140
Flight Controls
22 – TURBO PROP POWER PLANT 7.
220
Turboprop Power Plant
24 – AUXILIARY POWER PLANT 8.
241
Gas Turbine Compressor (GTC)
X
9.
242
Air Turbine Motor (ATM)
X
10.
243
Cooling Fan Assembly
X
32 – HYDRAULIC PROPELLER 11.
320
Hydraulic Propeller
41 – AIR COND & SURFACE ICE CNTRL 12.
41Y
Special Systems AC
X
X8
X8
X8
13.
411
AC-Flight Deck
X
X9
X9
X9
14.
412
AC-Cargo Compartment
X
X9
X9
X9
15.
413
Pressurization
X
X 10
X 10
X 10
16.
414
Bleed Air System
X
X
X
X
17.
415
Anti-Ice/De-Ice Systems
X
X 11
X 11
X 11
18.
418
Air Cond, Press, & Surface Ice Control Instruments
X
X
X
X
19.
419
Under Floor Heat
X X 12
X 12
X 12
42 – ELECTRICAL POWER SUPPLY 20.
420
Electrical Power Supply
X 12
44 – LIGHTING SYSTEMS 21.
44A
Special Systems Interior Lighting
X
22.
4411
Navigation Lights
X 13
X 13
X 13
X 13
23.
4412
Landing Lights
X
X 14
X 14
X 14
24.
4414
Taxi Lights
X
X 15
X 15
X 15
25.
4415
Leading Edge Lights
X
4
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
26.
4418
Strobe Light System
X
X
X
X
27.
4427
Panel Lighting (Primary Instrument Lighting)
X 17
X 17
X 17
X 17
28.
4428
Warning Lights
X
X
X
X
29.
443
Emergency Exit Lights (Impact)
X
X
X
X
X 18
X 18
X 18
X 18
45 – HYD & PNEUMATIC PWR SUPPLY 30.
450
Hyd & Pneumatic Power Supply
46 – FUEL SYSTEM 31.
46W
UARRSI
X
32.
461
Fuel System – Fuel Tanks
X
X 19
X 19
X 19
33.
462
Fuel System – Distribution
X
X 20
X 20
X 20
34.
463
Fuel System – Single Pt Refueling
X 21
35.
464
Fuel System – Vent System
X
X
X
X
36.
466
Fuel System – Instruments
X
X 22
X 22
X 22
X2
X2
X2
X2
47 – OXYGEN SYSTEM 37.
470
Oxygen System
49 – MISCELLANEOUS UTILITIES 38.
491
Fire Extinguisher System
X
X
X
X
39.
495
Windshield Wipers
X
X 23
X 23
X 23
40.
496
Personnel Warning Bell
X
X
X
X
51 – INSTRUMENTS 41.
51J
Ground Collision Avoid Sys
X
X
X
X
42.
51Z
Rosemont Pitot Static System
X
X
X
X
43.
51Y
Air Data Computer
X
X
X
X
44.
5112
Turn And Slip Indicating System
X
X 64
X 64
X 64
45.
5113
Attitude Indicating System
X
X
X
X
46.
5114
Navigation Instruments
X
X 25
X 25
X 25
47.
518
AF Standard Flt Director System
X
X
X
X
48.
519
Stand By Compass
X
X
X
X
X 26
X 26
X 26
52 – AUTOPILOT 49.
523
C-12 Compass System
X 26
50.
527
Digital Autopilot (AN/AYW-1(V)-1)
X
56 – ACCIDENT INVESTIGATION 51.
56A
Cockpit Voice Recorder
X 27
X
X
X
52.
56B
Flight Data Recorder
X 27
X
X
X
X
X 28, 29
X 28, 29
X 28, 29
61 – HF COMMUNICATIONS 53.
614
Antenna System – HF Long Wire
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
5 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
54.
615
HF Communications (AN/ARC-190)
X
X 28, 29
X 28, 29
X 28, 29
55.
616
ANDVT (KYV-5)
X
X 30
X 30
X 30
X
X 31
X 31
X 31
X
X 32
X 32
X 32
Interphone System
X
X 2, 33
X 2, 33
X 2, 33
62 – VHF COMMUNICATIONS 56.
62B
VHF Comm (AN/ARC-186)
63 – UHF COMMUNICATIONS 57.
630
UHF Comm (AN/ARC-164)
64 – INTERPHONE 58.
64 65 – IFF
59.
652
IFF/SIF (APX-119)
X
X
X
X
60.
65L
E-TCAS
X
X
X
X
66 – EMERGENCY COMMUNICATIONS 61.
6617
Emergency Locator Transmitter
X 34
X
X
X
62.
663
Underwater Acoustic Locator Sys
X6
X6
X6
X6
X 28
X 28
X 28
X
X 30
X 30
X 30
68 – SATELLITE COMMUNICATIONS 63.
68L
JTIDS (URC-107) (BL1 acft only)
X 36
64.
68N
AITG (ARC-234)
X
65.
682
Intel Broadcast Receiver (IBR)
X 68
66.
683
LINK 16 (JTRS) (BL2 acft only)
X
67.
684
Ku Band Satellite System (KuSS) (BL2 acft only)
X
69 – MISC COMM EQUIPMENT 68.
69YC
KY-58 Secure Voice
71 – RADIO NAVIGATION 69.
71C
VOR/ILS/MB (AN/ARN-147)
X
X 28
X 28
X 28
70.
71E
GPS (AN/ARN-151)
X
X 37
X 37
X 37
71.
71Z
TACAN System (AN/ARN-118)
X
X 28
X 28
X 28
72 – RADAR NAVIGATION 72.
72Z
Inertial Navigation Set
X
X 37
X 37
X 37
73.
72Z
Computer-Aided Nav Sys (CANS)
X
X 38
X 38
X 38
74.
721
Doppler Nav System (APN-218)
X
75.
722
CARA Altimeter (AN/APN-232)
X
76.
7232
Wave Guide Pressurization System
X 26
77.
727A
Search Radar (AN/APN-59F)
X 26
76 – ELECTRONIC COUNTERMEASURE 78.
76F
LAIRCM (AN/AAQ-24A(V)13)
X 69
X
X
X
79.
76N
CMDS (AN/ALE-47)
X 69
X
X
X
80.
761
MWS (AN/AAR-54)
X 69
X
X
X
6
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
X
X
X
X
X 61 X 61
X 61 X 61
X 61 X 61
X 62
X 62
X 62
78 – SYSTEM CONTROL, PME 78A – CONSOLE RACK POWER (CRP) 81.
78A
Console Rack Power (CRP)
78B – SYS CMPTR & MGMNT (SCM) 82. 83. 84.
78BA 78BB 78BC
CCU Controller (CCU A & CCU B) CCU MASS Storage System Local Bypass Unit
X X X
85.
78BD
RS422/TTL Converter (422TTL)
X
86.
78BE
RS422/RS232 Converter (422CFC)
X
87.
78BF
Pwr Supply Module (AW20S/12-A)
X
88.
78BG
Time Freq Std Interface (TFSI)
X
X 52
89.
78BH
Disciplined Frequency Std
X
X
X
X
90.
78BJ
System Timing (TBUs)
X
X
X
X
91.
78BK
Ethernet Switch
X
X
X
X
92.
78BL
Media Converter
X
X 39
X 39
X 39
93.
78BM
Ethernet Patch Panel
X
X
X
X
94.
78BN
Remote Status Ind (B38432012-103)
X
95.
78BP
Remote Status Ind (B38432012-107)
X
96.
78BR
Tech Station Subsystem Antenna
X
97.
78BS
Auto Ant Switch (B38432044-133)
X
X
X
X
98.
78BT
Auto Ant Switch (B38432044-145)
X
X
X
X
99.
78BU
RF/IF Switch Unit (B38432036-101)
X
X
100.
78BV
Low/Mid Band Sw Unit (LMBSU)
X
X
101.
78BW
TSS Patch Panel (B38622004-101)
X
X
X
X
102.
78BX
Spectrum Analyzer
X
103.
78BY
TSS Controller
X
104.
78BZ
TSC/TNA Mass Storage System
X
105.
78B1
TNA Controller
X
106.
78B2
Blanking Unit
X
X
X
X
107.
78B4
Server PC
X
X
X
X
108.
78B5
Proterm Handheld Local Controller
X
109.
78B6
Coax Switch Assembly (CSA) (BL2 acft only)
X
X
X
X
X
X 65
X 65
X 65
X
X
X
78C – HMI SUBSYSTEM 110.
78C
HMI Subsystem
86 – RF RECEIVE, PME 86A – RF RECEIVE SUBSYSTEM 111.
86AA
Low Band Receive Antenna
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
7 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
112.
86AB
Antennas – Receive
X
X
X
113.
86AD
LMH – RFD
X
X
X
114.
86AE
DF Antenna Retract Panel
X
X
115.
86AL
Phase Shifter Box Assy
X
X
116.
86AM
Multicoupler
X
X
117.
86AP
Wingtip Radome Assy
X
X
X
118.
86AT
EHB – RFDN
X
X
X
X
X
X
87 – SIGNAL PROCESSING, PME 87A – LMB ACQUISITION (ACQ) 119.
87AA
ACQ Controller
X
X
120.
87AB
Digital ACQ Receiver
X
X 50
121.
87AC
PAN Display
X
87B – LMB ANALYSIS (ANA) 122.
87BA
ANA Controller
X
X
123.
87BB
ANA Receiver
X
X 51
124.
87BC
WB Dual Signal Analyzer (WBDSA)
X
X 51
125.
87BD
Analysis Assembly
X
X 57
87C – LMB DIRECTION FINDING (DF) 126.
87CA
DF Controller
X
X
127.
87CB
Phase Shifters
X
X
128.
87CC
DF Receiver RFD
X
X
129.
87CD
DF Receiver (8 Channel)
X
X
87E – LMB EXCITER (EXC) 130.
87EA
EXC Controller
X
X
131.
87EB
RF Generator
X
X
132.
87EC
EXC Assembly
X
X
87F – ENHANCED HIGH BAND (EHB) 133.
87FA
EHB ACQ Tuner 1, 2
X
X 53
X 53
134.
87FB
EHB ACQ Processor Unit 1, 2
X
X 54
X 54
135.
87FC
EHB DF Tuner
X
X 53
X 53
136.
87FD
EHB DF Acquisition Unit 1, 2
X
X 54
X 54
137.
87FE
EHB Data Processor
X
X 55
X 55
138.
87FF
EHB Exciter Controller Unit 1, 2
X
X 56
X 56
139.
87FG
EHB Exciter Synthesizer 1, 2
X
X 56
X 56
X 59
X 59
87G – COMMON SIGNAL GENERATORS 140.
87GA
Common Signal Generator (E4433B)
X
141.
87GB
Common Signal Generator (N5182A)
X
X 59
8
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
87J – COUNTER RADAR SUBSYSTEM 142.
87JA
CRS RF Chassis
X
X
143.
87JB
CRS Power Supply
X
X
87S – INTEGRATED NOVA 144.
87SA
AXE Controller
X
X 66 X 67
87T – NCCT 145.
87TA
Blade Server Chassis Assy-3 (Con 2)
X
146.
87TB
Blade Server Chassis Assy-2 (Con 3)
X
147.
87TC
Blade Server Chassis Assy-1 (ER 2)
X
148.
87TD
RAID Chassis
X
149.
87TE
Accelerator
X
150.
87TF
Converter
X
151.
87TH
STE RI (ISDN/PSTN)
X
152.
87TJ
AMT-3800 SATCOM System
X
X 52
153.
87TK
High Spd Data Terminal (HSD-400)
X
X 52
154.
87TM
Encryptor (KG-175D)
X
155.
87TQ
INMARSAT Power Panel
X
X 52
156.
87TR
ECPC2
X
X 67
87V – IRIDIUM & KVM 157.
87VA
KVM Splitter Assembly
X
X 67
158.
87VB
Power Distribution Assembly
X
X 67
159.
87VC
Sectera Wireline Terminal BDI
X
160.
87VD
Interface Module, Beam Iridium Data
X
161.
87VE
Converter, DC – DC
X
162.
87VF
Switch, Switchview SC 8 Port
X
163.
87VG
Antenna
X
87W – SIGNAL DISTRIBUTION 164.
87WA
Dual Purpose Combiner Module
X
X
X 58
X 58
X
X
X
X
87Y – MODERN COMMS RECEIVE (MCR) 165.
87Y
MCR
88 – RF TRANSMIT, PME 88A – RF TRANSMIT (RFT) 166.
88AA
Fault Indicator Panel
X
167.
88AB
RF Patch Panel (BL1 acft only)
X
X
168.
88AC
Low Band Transmit Subsystem
X 58
X 58
169.
88AD
Low Band Transmit Antenna
X 58
X 58
170.
88AG
Mid Band Transmit Subsystem
X
X 28
X 28,67
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
9 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
171.
88AH
Mid Band Transmit Antenna Assy
X
X
172.
88AJ
High Band Switch Unit Controller
X 60
X 60
X 60
173.
88AK
High Band Switch RF Unit
X 60
X 60
X 60
174.
88AL
SB1 Amplifier Assy
X 60
X 60
X 60
175.
88AM
SB1 Power Supply Assy
X 60
X 60
X 60
176.
88AN
HB L/R Load Switch
X 60
X 60
X 60
177.
88AP
HB RF Load Resistor Assy
X
178.
88AQ
HB1/SB1-H Transmit Antenna Assy
X 60
X 60
X 60
179.
88AR
HB2 T3/SB1-V Transmit Ant Assy
X 60
X 60
X 60
180.
88AS
HB2 T2 Transmit Antenna Assy
X 60
X 60
181.
88AT
HB3 Transmit Antenna Assy
X 60
X 60
182.
88AU
Antenna Polarization Switch (L/R)
X
X
X
X
88B – SPEAR SUBSYSTEM 183.
88BA
Pod Antenna Array (LH/RH)
X 60
X 60
X 60
X 60
184.
88BB
Pylon Assembly
X 60
X 60
X 60
X 60
185.
88BF
High Voltage Power Supply
X 60
X 60
X 60
X 60
186.
88BG
RF Distribution
X 60
X 60
X 60
X 60
187.
88BK
Timing Buffer Unit (TBU)
X 60
X 60
X 60
X 60
188.
88BL
Crypto Timing Interface Assy
X
189.
88BM
SPEAR System Controller (NCR)
X 60
X 60
X 60
X 60
88D – SUBSYSTEM 1 & SUBSYSTEM 2 190.
88DA
Transmit/Receive Assembly
X 58
X 58
191.
88DB
Dual Band Simulator
X 58
X 58
192.
88DC
SS1 Digital VME
X 58
X 58
193.
88DD
SS1 Oscillator
X 58
X 58
194.
88DE
SS1 Downconverter
X 58
X 58
195.
88DF
SS1 Upconverter
X 58
X 58
196.
88DG
SS2 Digital VME
X 58
X 58
197.
88DH
SS2 Oscillator
X 58
X 58
198.
88DJ
SS2 Downconverter Filter Sw Matrix
X 58
X 58
199.
88DK
SS2 Downconverter
X 58
X 58
200.
88DL
SS2 Upconverter
X 58
X 58
201.
88DM
SS2 Upconverter Filter Sw Matrix
X 58
X 58
202.
88DN
RF Switch / SS2
X 58
X 58
203.
88DP
SS1 / SS2 Ballast Plates
X 58
X 58
91 – EVACUATION & EMERGENCY 204.
91113
Escape Rope
X
X
X
X
10
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
205.
91213
Life Raft (Type F-2)
X 24, 35
X 35
X 35
X 35
X2
X2
X2
X2
96 – PERSONNEL AND MISC EQUIPMENT 206.
963
AERP System
97 – EXPLOSIVE DEVICES AND CMPNTS 207.
97A
Squib, Fire Extinguisher
X
X
X
X
208.
97Y
LBT Antenna Cutter Assembly
X
X 40
X 40
X 40
QUALIFYING NOTES: Notes 1 through 49 are primarily for aircraft subsystems. Notes 41 through 49 have been intentionally left blank to accommodate future modifications. Notes 50 and above are primarily for special mission subsystems (WUCs 78, 86, 87 and 88). 1.
One air deflector door may be inoperative
2.
One required at each operational position
3.
Urinal / Toilet facilities required; urinal may be inop provided toilet is properly serviced
4.
WUC 14511 Flap Indicator may be inoperative
5.
WUC 22DBF - Datum Amplifier, 22EBD-Temp Datum Amplifier, 22EBH-Low Speed Idle Solenoid, may be inoperative. WUC 22GF0 - Oil Cooler Door Position Indication, and one 22GG0-Oil Quantity Indication may be inoperative if low oil light is operational and oil level is verified prior to flight. WUC 22GGD - Low oil quantity light may be inoperative if all four engine oil gauges are operational. WUC 22140 - Oil cooler flap may be inoperative if the flap can be manually positioned to open & fixed.
6.
Required for Over Water Missions
7.
System operational with a feather override failure where the override button fails to pop out at the full feather, and the malfunction has been isolated to a faulty pressure switch and no other system is affected.
8.
For Baseline-1 aircraft: Report aircraft as PMC provided one special air conditioner & recirculation fan are operational on the same side. For Baseline-2 aircraft: Report aircraft as PMC provided one special air conditioner and condenser fan on the same side, and the main recirculation fan are operational
9.
Automatic system may be inoperative provide manual temperature control is operable. Manual system may be inoperative provided automatic temperature control is operable.
10.
Automatic controller may be inoperative provide manual pressure control is operative.
11.
If inoperative, report aircraft as PMC. System required for flights into known or forecasted icing conditions.
12.
If an engine-driven generator or one Essential TR fails, it may be disconnected or the failed generator will be removed and the mount padded to fly to repair facility; provided no other electrical malfunction exists.
13.
For night operations, all wing tip Nav lights and at least one tail cone white light must be operational.
14.
One may be inoperative provided the taxi light on the same side is operational.
15.
One may be inoperative provided the landing light on the same side is operational.
16.
Not Used
17.
Report aircraft as PMC if inoperative. For night operations sufficient edge lighting or backlit lighting must be operational for airspeed, altimeters, VVI/VSI, ADI and HSI.
18.
Aux Hyd Press Indicator direct reading gauge in cargo compartment may be inoperative.
19.
WUC 46120 – When leaking, tanks may be kept empty.
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
11 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
EAN
EAR
20.
WUC 46212 – Auxiliary tank boost pumps may be inoperative provided tank is empty.
21.
WUC 46321 – SPR drain pump required for air refueling.
22.
Fuel tank fuel quantity indication allowed to be inop provided fuel quantity is verified prior to flight: both auxiliary tanks, two non-symmetrical main tanks. Report aircraft as PMC; aircraft should not be scheduled for AR missions where fuel transfer is expected.
23.
Pilot's Side Must Be Operational
24.
Not required for PDM input.
25.
BDHIs and RMIs May Be Inoperative.
26.
Report aircraft as PMC if APN-59 Radar, ASQ-14 Waveguide Pressurization, and/or Number 2 C-12 Compass System is/are inoperative. Required for over-water missions.
27.
Either CVR or DFDR must be operational for training missions, and to continue en-route to next repair facility. Both required prior to deployment.
28.
One Operational System Required.
29.
HF #2 needed for UST-105. Report as PMC if unable to support UST-105.
30.
One Secure Voice Sys Required For Each Band.
31.
May Be Inoperative If Either AITG Is Operational
32.
Two UHF Radios required. One must be the Nbr 1 UHF system. One operational AITG may substitute for inop Nbr 2 or Nbr 3 UHF radio.
33.
AIC-13 PA System Not Required
34.
If en-route, must be repaired at next capable repair facility.
35.
Two Life Rafts required For Over Water Missions.
36.
Flight Deck JTIDS display not required
37.
Minimum Is Two of The Three Nav Systems (INS & GPS) for PMC condition 1. If Both INUs Operational, GPS May Be Inop. 2. If Only one INU Operational, GPS Required.
38.
Navigator’s CDU must be operational
39.
Two Operational Systems Required
40.
Required if Low Band Transmit Antenna is Installed (Notes 41 – 49 Intentionally Left Blank for Future Use)
50.
Acquisition Receiver must have at least 5 good channels/tuners.
51.
Eight channels required
52.
Required for aircraft with MCR installed
53.
One ACQ and DF Tuner Required
54.
ACQ Unit 1 and DF ACQ Unit 1 Required for Operational ACQ Tuner 1 OR ACQ Unit 2 and DF ACQ Unit 2 Required for Operational ACQ Tuner 2.
55.
DPU Must Have Methods, Comm & Jam CPUs For Minimal Performance
56.
EHBS Exciter Channel 1 or Channel 2 Required for Minimal Performance. If exciter controller 1 is inoperative, SB-1 must be controlled manually.
57.
Minimum of 1 unit / 6 channels required for PMC condition.
12
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 BSL
NO.
WUC
SYSTEM/SUBSYSTEM
FSL
EAC
58.
Alternate Mission Equipment for Baseline 1 aircraft / Must Be Operational If Installed
59.
BL-2 aircraft: 5 CSGs required for PMC condition
60.
Alternate Mission Equipment / Must Be Operational If Installed
61.
Either CCU A and MSS A, Or CCU B and MSS B Must Be Operational
62.
Report aircraft as PMC with degraded FDDI wrap.
63.
Required if TSC is functional
64.
Pilot or Co-Pilot Side Must be Operational
65.
Two Operator Workstations Required. Two ORUs Required.
66.
Must have at least 4 transmit channels
67.
Mid-Band 1 required when CRS installed
68.
Applicable to BL-1 aircraft after CCOS 4.4 and IBR-S upgrade Applicable to BL-2 aircraft
69.
Not required for Home Station Training Missions
EAN
JOHN B. COOPER, Major General, USAF Director of Logistics, Air Combat Command
EAR
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 Attachment 1 GLOSSARY OF REFERENCES AND SUPPORTING INFORMATION References AFI 11-2EC-130H Vol 3, EC-130H—Operations Procedures, 24 February 2010 AFI 21-103, Equipment Inventory, Status, and Utilization Reporting, 30 January 2012 Prescribed Forms This addendum does not prescribe any forms. Adopted Forms AF Form 847, Recommendation for Change of Publication Abbreviations and Acronyms AAS—Automatic Antenna Switch AC—Air Conditioner /Air Conditioning ACC—Air Combat Command ACQ—Acquisition AERP—Aircrew Eye Respiratory Protection AF—Air Force AFRC—Air Force Reserve Command AITG—Airborne Integrated Terminal Group AME—Alternate Mission Equipment ANA—Analysis ANDVT—Advanced Narrowband Digital Voice Terminal ATM—Air Turbine Motor BDHI—Bearing Distance Heading Indicator BL—Base Line BSL—Basic Systems List CANS—Computer-Aided Navigation System CARA—Combined Altitude Radar Altimeter CCU—Common Controller Unit CDU—Control Display Unit CMDS—Countermeasures Dispensing System CPU—Computer Processing Unit CRS—Counter Radar Subsystem
13
14
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
CSG—Common Signal Generator CVR—Cockpit Voice Recorder DC—Direct Current DF—Direction Finding DFDR—Digital Flight Data Recorder DOC—Design Operational Capability DPU—Data Processing Unit DSA—Dual Signal Analyzer EC—External Communications ELT—Emergency Locator Transmitter EHB—Enhance High Band E-TCAS—Enhanced Traffic Collision Avoidance System EXC—Exciter FMC—Full Mission Capability / Fully Mission Capable FSL—Full Systems List GPS—Global Positioning System GTC—Gas Turbine Compressor HB—High Band HF—High Frequency HQ—Head Quarters IAW—In Accordance With IBR—Intelligence Broadcast Receiver IFF/SIF—Identify Friend or Foe / Selective Identity Function ILS—Instrument Landing System JTIDS—Joint Tactical Information Distribution System LAIRCM—Large Aircraft Infrared Countermeasures LBT—Low-Band Transmit LH—Left Hand LMB—Low-Mid Band LMH—Low-Mid-High KVM—Kernel-based Virtual Machine MAJCOM—Major Command
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015 MB—Marker Beacon MC—Mission Capable MCR—Modern Communications Receive MRA—Mission Ready Aircraft MSS—Mass Storage System MWS—Missile Warning System NCCT—Network-Centric Collaborative Targeting NGB—National Guard Bureau NMC—Non Mission Capable PA—Public Address PAN—Panoramic PDM—Programmed Depot Maintenance PMC—Partially Mission Capable / Partial Mission Capability PME—Prime Mission Equipment RF—Radio Frequency RFD—Radio Frequency Distribution RFDN—Radio Frequency Distribution Network RFR—Radio Frequency Receive RFT—Radio Frequency Transmit RH—Right Hand RMI—Radio Magnetic Indicator SATCOM—Satellite Communications SB—Special Band SORTS—Status of Resources & Training System SS—Special System SSAC—Special Systems Air Conditioning / Conditioner TACAN—Tactical Air Navigation TBU—Timing Buffer Unit TIBS—Tactical Information Broadcast System TSS—Tech Station Subsystem UARRSI—Universal Air Refueling Receptacle Slipway Installation UHF—Ultra High Frequency
15
16 VHF—Very High Frequency VOR—Visual Omni Range WB—Wide Band WUC—Work Unit Code
AFI21-103_ACCSUP_ADD_F 2 FEBRUARY 2015
