CGTO 1C–130–1 FLIGHT MANUAL USCG SERIES

2-91 Changed text of warning in figure 2B-8. 2-98 Changed step 21.a. to a note and added text. 2-99, 2–100 Changed text in DMB paragraph. Changed all instances of ASRK–18 to ASRK–2, LRU–20/A six place to POD–8 eight place and ADR–6 to ADR–8. Changed maximum weight limitation for ADS– Can. Added section for Authorized Drill Equipment. 2-103 Deleted text from warning in figure 2C-4. 2-105 Added text to “30 seconds standby” in figure 2C-6. 2-106 Added text to introduction of figure 2C-7. 2-107 thru 2-116 Incorporated CGTO 1C–130–1S–052 (alternate restraint procedure for ADDS pack). 3-1, 3–2 Updated table of contents. 3-39 thru 3–46 Added CASPER Emergency Power Off Procedure and Electrical Isolation Procedure. Generated pages 3–40a and 3–40b to minimize number of pages affected by text rollover. Added cleanup proce- dures for Fuselage Fire/Smoke and Fume Elimination. Deleted Nose Radome from Overheat para- graph. Deleted Nose Wheel Well section from Overheat Chart. Deleted Nose Wheel Well/Nose Ra- dome section from Overheat Chart. 3-58 Added caution after step 8. concerning nose wheel steering. 3-63 Added picture of vertical torque shaft companion flange. 4-1, 4–2 Updated table of contents. Text rollback affected page 4–2. 4-3 Added step for EPOS in Loadmaster duties. 4-4 Added crew duties for Sensor System Operator and Tactical System Operator. Generated pages 4–4a and 4–4b to minimize number of pages affected by text rollover. 4-12 Added (LM) to line up checks. 4-18 Added step 33 (gunners belt) to LM/DM checklist. 4-22 Changed ARSK–18 to ARSK–24. 4-23 Changed ADR–6 to ADR–8. 4-29 Deleted step 13 (safety belt) and note from LM/DM Before Takeoff checklist. 4-30 Added note concerning fastening seatbelt. Added Line Up Checklist. 4-43 Added step to check FLIR/EO date and time. Added note concerning time–setting procedure. 4-45 Added (LM) to lineup checks. 4-48 Added (LM) to lineup checks. 5-2 Deleted -7 TIT indicator. CGTO 1C–130–1 C-130 FLIGHT MANUAL PAGE 4 HIGHLIGHTS 5-3 Changed frequency tolerance to 20 Hz. 5-28 Deleted Airdrop Limitations and Strake Limitations. FLIGHT MANUAL C–130 USCG SERIES AIRCRAFT CGTO 1C–130–1 RECORD OF REVISIONS PAGE 1/(2 BLANK)/(2 BLANK) RECORD OF REVISIONS REV NO. REV DATE INSERT DATE INSERT BY 1 JUNE 1/00 REV NO. REV DATE INSERT DATE INSERT BY This change incorporates Operational Supplements C.G.T.O. 1C–130–1S–043, C.G.T.O. 1C–130–1S–052 and C.G.T.O. 1C–130–1S–053. Operational Supplements C.G.T.O. 1C–130–1S–035, C.G.T.O. 1C–130–1S–042, C.G.T.O. 1C–130–1S–054 and C.G.T.O. 1C–130–1S–055 are not incorporated in this change and shall remain supplements until they are rescinded or incorporated. C.G.T.O. 1C–130–1S–049 (Electrical System Upgrade) has been incorporated, but will remain an active supplement until all planes have been modified. CGTO 1C–130–1 FLIGHT MANUAL USCG SERIES AIRCRAFT 15 DECEMBER 2000 C–130 COMMANDING OFFICERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTION OF ALL AFFECTED PERSONNEL. PUBLISHED UNDER THE AUTHORITY OF THE COMMANDANT, USCG. T.O. 1C–130(H)–1 PERFORMANCE DATA IS CONTAINED IN T.O. 1C–130H–1–1. CHANGE 1 – 1 JULY 2001 ERRATA CGTO 1C–130–1 USCG B CH–1 LIST OF EFFECTIVE PAGES INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. Dates of issue for original and changed pages are: Original 0 15 Dec 00 . . . . . . . . . . . . . . Change 1 1 01 Jul 01 . . . . . . . . . . . . . . Page No. Change No. . Title – D 1 . . . . . . . . . . . . . i – ii 1 . . . . . . . . . . . . . . . . . . . . . iii – viii blank 0 . . . . . . . . . . . . . 1-1 – 1-6 0 . . . . . . . . . . . . . . . . . . 1-7 – 1-11 1 . . . . . . . . . . . . . . . . . 1-12 – 1-13 0 . . . . . . . . . . . . . . . 1-14 – 1-15 1 . . . . . . . . . . . . . . . 1-16 0 . . . . . . . . . . . . . . . . . . . . . . 1-17 – 1-19 1 . . . . . . . . . . . . . . . 1-20 – 1-24 0 . . . . . . . . . . . . . . . 1-25 – 1-26 1 . . . . . . . . . . . . . . . 1-27 – 1-39 0 . . . . . . . . . . . . . . . 1-40 – 1-42 1 . . . . . . . . . . . . . . . 1-43 – 1-51 0 . . . . . . . . . . . . . . . 1-52 – 1-53 1 . . . . . . . . . . . . . . . 1-54 – 1-74 0 . . . . . . . . . . . . . . . 1-75 1 . . . . . . . . . . . . . . . . . . . . . . 1-76 – 1-97 0 . . . . . . . . . . . . . . . 1-98 1 . . . . . . . . . . . . . . . . . . . . . . 1-99 – 1-100 0 . . . . . . . . . . . . . . 1-101 1 . . . . . . . . . . . . . . . . . . . . . 1-102 0 . . . . . . . . . . . . . . . . . . . . . 1-103 1 . . . . . . . . . . . . . . . . . . . . . 1-104 0 . . . . . . . . . . . . . . . . . . . . . 1-105 1 . . . . . . . . . . . . . . . . . . . . . 1-106 – 1-126 0 . . . . . . . . . . . . . 1-127 – 1-131 1 . . . . . . . . . . . . . 1-132 – 1-133 0 . . . . . . . . . . . . . 1-134 1 . . . . . . . . . . . . . . . . . . . . . 1-135 – 1-145 0 . . . . . . . . . . . . . 1-146 1 . . . . . . . . . . . . . . . . . . . . . 1-147 – 1-149 0 . . . . . . . . . . . . . 1-150 1 . . . . . . . . . . . . . . . . . . . . . 1-151 – 1-153 0 . . . . . . . . . . . . . 1-154 1 . . . . . . . . . . . . . . . . . . . . . 1-155 – 1-162 0 . . . . . . . . . . . . . 1-163 1 . . . . . . . . . . . . . . . . . . . . . 1-164 0 . . . . . . . . . . . . . . . . . . . . . 1-165 – 1-171 1 . . . . . . . . . . . . . NOTE The portion of the text affected by changes is indicated by a vertical line in the outer margins of the page. Changes to illustrations are indicated by miniature pointing hands. Changes to wiring diagrams are indicated by shaded areas. *Zero in this column indicates an original page. * Page No. Change No. 1-172 – 1-173 0 . . . . . . . . . . . . . 1-174 1 . . . . . . . . . . . . . . . . . . . . . 1-175 – 1-177 0 . . . . . . . . . . . . . 1-178 1 . . . . . . . . . . . . . . . . . . . . . 1-179 – 1-183 0 . . . . . . . . . . . . . 1-184 1 . . . . . . . . . . . . . . . . . . . . . 1-185 – 1-190 0 . . . . . . . . . . . . . 1-191 1 . . . . . . . . . . . . . . . . . . . . . 1-192 – 1-202 0 . . . . . . . . . . . . . 1-203 – 1-208 blank 1 . . . . . . . . 1-209 – 1-238 blank 1 . . . . . . . . 2-1 – 2-16 0 . . . . . . . . . . . . . . . . . 2-17 1 . . . . . . . . . . . . . . . . . . . . . . 2-18 – 2-22 0 . . . . . . . . . . . . . . . 2-23 1 . . . . . . . . . . . . . . . . . . . . . . 2-24 – 2-38 0 . . . . . . . . . . . . . . . 2-39 1 . . . . . . . . . . . . . . . . . . . . . . 2-40 – 2-43 0 . . . . . . . . . . . . . . . 2-44 1 . . . . . . . . . . . . . . . . . . . . . . 2-45 0 . . . . . . . . . . . . . . . . . . . . . . 2-46 1 . . . . . . . . . . . . . . . . . . . . . . 2-47 – 2-49 0 . . . . . . . . . . . . . . . 2-50 1 . . . . . . . . . . . . . . . . . . . . . . 2-51 – 2-52 0 . . . . . . . . . . . . . . . 2-53 1 . . . . . . . . . . . . . . . . . . . . . . 2-54 – 2-59 0 . . . . . . . . . . . . . . . 2-60 – 2-61 1 . . . . . . . . . . . . . . . 2-62 – 2-74 0 . . . . . . . . . . . . . . . 2-75 1 . . . . . . . . . . . . . . . . . . . . . . 2-76 – 2-78 0 . . . . . . . . . . . . . . . 2-79 – 2-80 1 . . . . . . . . . . . . . . . 2-81 – 2-84 0 . . . . . . . . . . . . . . . 2-85 1 . . . . . . . . . . . . . . . . . . . . . . 2-86 0 . . . . . . . . . . . . . . . . . . . . . . 2-87 1 . . . . . . . . . . . . . . . . . . . . . . 2-88 0 . . . . . . . . . . . . . . . . . . . . . . 2-89 1 . . . . . . . . . . . . . . . . . . . . . . 2-90 0 . . . . . . . . . . . . . . . . . . . . . . 2-91 1 . . . . . . . . . . . . . . . . . . . . . . * Page No. Change No. 2-92 – 2-97 0 . . . . . . . . . . . . . . . 2-98 – 2-100 1 . . . . . . . . . . . . . . 2-101 – 2-102 0 . . . . . . . . . . . . . 2-103 1 . . . . . . . . . . . . . . . . . . . . . 2-104 0 . . . . . . . . . . . . . . . . . . . . . 2-105 – 2-116 1 . . . . . . . . . . . . . . 3-1 – 3-2 1 . . . . . . . . . . . . . . . . . . 3-3 – 3-38 0 . . . . . . . . . . . . . . . . . 3-39 – 3-46 1 . . . . . . . . . . . . . . . 3-47 – 3-57 0 . . . . . . . . . . . . . . . 3-58 1 . . . . . . . . . . . . . . . . . . . . . . 3-59 – 3-62 0 . . . . . . . . . . . . . . . 3-63 1 . . . . . . . . . . . . . . . . . . . . . . 3-64 – 3-96 0 . . . . . . . . . . . . . . 4-1 – 4-4b 1 . . . . . . . . . . . . . . . . . 4-5 – 4-11 0 . . . . . . . . . . . . . . . . . 4-12 1 . . . . . . . . . . . . . . . . . . . . . . 4-13 – 4-17 0 . . . . . . . . . . . . . . . 4-18 1 . . . . . . . . . . . . . . . . . . . . . . 4-19 – 4-21 0 . . . . . . . . . . . . . . . 4-22 – 4-23 1 . . . . . . . . . . . . . . . 4-24 – 4-28 0 . . . . . . . . . . . . . . . 4-29 – 4-30 1 . . . . . . . . . . . . . . . 4-31 – 4-42 0 . . . . . . . . . . . . . . . 4-43 1 . . . . . . . . . . . . . . . . . . . . . . 4-44 0 . . . . . . . . . . . . . . . . . . . . . . 4-45 1 . . . . . . . . . . . . . . . . . . . . . . 4-46 – 4-47 0 . . . . . . . . . . . . . . . 4-48 1 . . . . . . . . . . . . . . . . . . . . . . 4-49 – 4-50 0 . . . . . . . . . . . . . . . 5-1 0 . . . . . . . . . . . . . . . . . . . . . . . 5-2 – 5-3 1 . . . . . . . . . . . . . . . . . . 5-4 – 5-27 0 . . . . . . . . . . . . . . . . . 5-28 1 . . . . . . . . . . . . . . . . . . . . . . 5-29 – 5-34 0 . . . . . . . . . . . . . . . 6-1 – 6-12 blank 0 . . . . . . . . . . . 7-1 – 7-10 blank 0 . . . . . . . . . . . Index 1 – Index 20 1 . . . . . . . . . * P 141813Z FEB 02 FM COMDT COGARD WASHINGTON DC//G-OCA/G-SEA// TO COGARD AIRSTA BARBERS PT HI//OPS/ENG// COGARD AIRSTA CLEARWATER FL//OPS/ENG// COGARD AIRSTA ELIZABETH CITY NC//OPS/ENG/C130 STAN TEAM// COGARD AIRSTA KODIAK AK//OPS/ENG// COGARD AIRSTA SACRAMENTO CA//OPS/ENG// COGARD ATC MOBILE AL//C130 STAN TEAM// COGARD AR SC ELIZABETH CITY NC//C130 PLM// BT UNCLAS //N13221// SUBJ: INTERIM CHANGE 2 TO FLIGHT MANUAL C-130 USCG SERIES AIRCRAFT A. FLIGHT MANUAL C-130 USCG SERIES AIRCRAFT, CGTO 1C-130-1 1. DUE TO A CHANGE 1 PRINTING ERROR, TWO STEPS WERE LEFT OFF OF THE FLIGHT ENGINEER'S PORTION OF THE OPERATIONAL STOP CHECKLIST. 2. MAKE THE FOLLOWING PEN AND INK CHANGES IN REF A. A. ON PAGE 2-60, FLIGHT ENGINEER STEP 8, OPERATIONAL STOP CHECKLIST ADD STEPS "C. ENGINE ANTI-ICING - ON" AND "D. PROP ANTI/DEICING - ON". 3. COMMANDING OFFICERS SHALL MAKE A COPY OF THIS MESSAGE AVAILABLE TO ALL C-130 PILOTS AND AIRCREW. ENSURE THE CHANGE IS ENTERED IN ALL UNIT COPIES OF REF A. C-130 STAN TEAM POC IS LCDR JOHN BORIS (252) 335-6320. BT NNNN P 142056Z FEB 02 FM COMDT COGARD WASHINGTON DC//G-OCA/G-SEA// TO COGARD AIRSTA BARBERS PT HI//OPS/ENG// COGARD AIRSTA CLEARWATER FL//OPS/ENG// COGARD AIRSTA ELIZABETH CITY NC//OPS/ENG/C130 STAN TEAM// COGARD AIRSTA KODIAK AK//OPS/ENG// COGARD AIRSTA SACRAMENTO CA//OPS/ENG// COGARD ATC MOBILE AL//C130 STAN TEAM// COGARD AR SC ELIZABETH CITY NC//C130 PLM// BT UNCLAS //N13221// SUBJ: ADDENDUM TO INTERIM CHANGE 1 TO FLIGHT MANUAL C-130 USCG SERIES AIRCRAFT A. MY 282102Z JAN 02 B. FLIGHT MANUAL C-130 USCG SERIES AIRCRAFT, CGTO 1C-130-1 C. CHECKLIST C-130 USCG SERIES AIRCRAFT, CGTO 1C-130-1CL-1 1. REF A OUTLINED PROCEDURAL CHANGES TO REF B FOR AIRCRAFT EQUIPPED WITH DUAL LN-100 INS UNITS. ASSOCIATED CHANGES TO REF C ARE CONTAINED HEREIN. 2. MAKE THE FOLLOWING PEN AND INK CHANGES TO REF C. A. ON PAGE N-27, STEP 17 (BEFORE STARTING AND PUSH-BACK CHECKLIST) REPLACE "SET, STATE SETTING", WITH "OFF". B. ON PAGE N-28, ADD STEP 36A, TO READ, "INS "SET, STATE SETTING" N/E/CP. 3. COMMANDING OFFICERS SHALL MAKE A COPY OF THIS MESSAGE AVAILABLE TO ALL C-130 PILOTS AND AIRCREW. ENSURE THE CHANGE IS ENTERED IN ALL UNIT COPIES OF REF C. C-130 STAN TEAM POC IS LCDR JOHN BORIS (252) 335-6320. BT NNNN CGTO 1C–130–1 USCG C CH–1 ERRATA STATUS PAGE This page provides a listing of the active Safety and Operational Supplements for the Flight Manual. Safety supplements are numbered as follows: C.G.T.O. 1C–130–SS–1, C.G.T.O. 1C–130–SS–2, etc. Op- erational supplements continue in sequence and are numbered as follows: C.G.T.O. 1C–130–1S–1, C.G.T.O. 1C–130–1S–2, etc. Supplement numbers should follow in sequence and will never be used more than once. If your manual is missing any supplements listed on this page, see your Quality Assurance De- partment. AIRCREW FLIGHT MANUAL BASIC DATE CHANGE NO. / DATE 1C-130-1 15 Dec 00 1/01 Jul 01 FLIGHT CREW CHECKLIST BASIC DATE CHANGE NO. / DATE C.G.T.O. 1C-130-1CL-1 15 Dec 00 1/01 Jul 01 C.G.T.O. 1C-130-1CL-2 15 Dec 00 1/01 Jul 01 C.G.T.O. 1C-130-1CL-3 15 Dec 00 1/01 Jul 01 C.G.T.O. 1C-130-1CL-4 15 Dec 00 1/01 Jul 01 C.G.T.O. 1C-130-1CL-5 15 Dec 00 1/01 Jul 01 C.G.T.O. 1C-130-1CL-6 15 Dec 00 1/01 Jul 01 C.G.T.O. 1C-130-1CL-7 15 Dec 00 1/01 Jul 01 The supplements listed below were not incorporated into the latest Flight Manual change and shall remain supplements until they are rescinded or incorporated. SAFETY AND OPERATIONAL SUPPLEMENTS DATE SHORT TITLE C.G.T.O. 1C–130–1S–035 1 Apr 96 Garmin GPS 55 Global Positioning System C.G.T.O. 1C–130–1S–042 1 Oct 99 Emergency Procedures for Aircraft with a For- ward Escape Hatch Mounted MILSATCOM Antenna Installed C.G.T.O. 1C–130–1S–048 Reserved C.G.T.O. 1C–130–1S–049 1 Jan 01 Electrical System Upgrade (Incorporated, but remains active, with restricted distribution) C.G.T.O. 1C–130–1S–054 1 Apr 01 Single LN–100 System C.G.T.O. 1C–130–1S–055 1 May 01 Chip Detector System INCORPORATED, RESCINDED, OR DELETED SUPPLEMENTS C.G.T.O. 1C–130–1S–031 16 Jan 97 Control Display Navigation Unit (CDNU) C.G.T.O. 1C–130–1S–036 RESCINDED C.G.T.O. 1C–130–1S–040 30 Oct 98 406 MHz ELT C.G.T.O. 1C–130–1S–041 1 Apr 99 Corrections to Critical and Emergency Proce- dures C.G.T.O. 1C–130–1S–043 1 Jun 00 CASPER System C.G.T.O. 1C–130–1S–044 15 Jan 00 Dual LN–100 Systems C.G.T.O. 1C–130–1S–045 15 Jan 00 Single LN–100 with CNMS (Superseded) C.G.T.O. 1C–130–1S–046 1 Aug 00 Single LN–100 without CNMS (Superseded) C.G.T.O. 1C–130–1S–047 1 Oct 99 Standby Attitude Indicator (SAI) C.G.T.O. 1C–130–1S–050 1 Mar 00 HC–130 Navigator and Radio Operator Syllabi CGTO 1C–130–1 USCG ERRATA CH–1 D C.G.T.O. 1C–130–1S–051 1 Dec 00 Single LN–100 w/o CNMS/GPS (Superseded) C.G.T.O. 1C–130–1S–052 1 Dec 00 Alternate Restraint Procedure for ADDS Pack C.G.T.O. 1C–130–1S–053 1 Apr 01 Dual LN–100 Systems CGTO 1C–130–1 i CH–1 TABLE OF CONTENTS PAGE SECTION I DESCRIPTION Part A Systems 1–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Part B Avionics 1–209 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION II OPERATION Part A Normal Procedures 2–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Part B Instrument Procedures 2–81 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Part C SAR Procedures 2–93 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Part D Aerial Dispersant Delivery System 2–107 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Part E System Operation 2–117 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION III EMERGENCY PROCEDURES 3–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION IV CREW DUTIES 4–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION V OPERATING LIMITATIONS 5–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION VI FLIGHT CHARACTERISTICS 6–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECTION VII ALL–WEATHER OPERATIONS 7–1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALPHABETICAL INDEX Index 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CGTO 1C–130–1 ii CH–1 SCOPE This manual contains the necessary information for safe and efficient operation of the C–130. These instructions provide you with a general knowledge of the airplane, its characteristics and specific normal and emergency operating procedures. Your flying experience is recognized; therefore, basic flight principles are avoided. When information in the manual pertains to a particular airplane, the following code symbols are used: HC–130 COAST GUARD TO AIR FORCE TO LOCKHEED NUMBER CROSS REFERENCE USCG USAF LOCKHEED USCG USAF LOCKHEED 1500 72–01300 4501 1705 83–0007 4993 1501 72–01301 4507 1706 83–0505 4996 1502 72–01302 4513 1707 83–0506 4999 1503 73–00844 4528 1708 83–0507 5002 1504 73–00845 4529 1709 83–0508 5005 1710 84–0479 5028 1601 77–0318 4760 1711 84–0480 5031 1602 77–0319 4762 1712 84–0481 5033 1603 77–0320 4764 1713 84–0482 5034 1714 84–0051 5035 1790 81–0999 4931 1715 85–0052 5037 1700 82–0081 4947 1716 85–1360 5023 1701 82–0082 4958 1717 86–0420 5104 1702 82–0083 4966 1718 86–0421 5106 1703 82–0084 4967 1719 86–0422 5107 1704 82–0085 4969 1720 87–0156 5120 SOUND JUDGMENT Instructions in this manual are for a crew inexperienced in the operation of this airplane. This manual provides the best possible operating instructions under most circumstances, but it is not a substitute for sound judgment. Multiple emergencies, adverse weather, terrain, etc., may require modification of the procedures. PERMISSIBLE OPERATIONS The Flight Manual takes a “positive approach” and normally states only what you can do. Unusual operations or configurations (such as asymmetrical loading) are prohibited unless specifically covered herein. Clearance must be obtained from the Commandant (G–OCA–2) before any questionable operation is attempted which is not specifically permitted in this manual. HOW TO BE ASSURED OF HAVING LATEST DATA Refer to COMDTINST M13005 series, its monthly supplement, and the latest safety or operational supplement flyleaf. STANDARDIZATION AND ARRANGEMENT Standardization assures that the scope and arrangement of all Flight Manuals are identical. The manual is divided into seven sections to simplify reading straight through or using it as a reference manual. CGTO 1C–130–1 iii SAFETY SUPPLEMENTS Information involving safety will be promptly forwarded to you by Safety Supplements. Supplements covering loss of life will get to you in 48 hours by message, and those concerning serious damage to equipment will arrive within 10 days by mail. The title page of the Flight Manual and the title block of each Safety Supplement should be checked to determine the effect they may have on existing supplements. You must remain constantly aware of the status of all supplements – current supplements must be complied with, but there is no point in restricting your operation by complying with a replaced or rescinded supplement. OPERATIONAL SUPPLEMENTS Information involving operations will be promptly forwarded to you by Operational Supplements. Supplements covering urgent operational information will get to you in 48 hours by message and those concerning essential information, but of a less urgent nature, will get to you within 21 days by mail. The title page of the Flight Manual and the title block of each Operational Supplement should be checked to determine the effect they may have on existing supplements. You must remain constantly aware of the status of all supplements – current supplements must be complied with, but there is no point in restricting your operation with a replaced or rescinded supplement. CHECKLISTS The Flight Manual contains amplified checklists. Abbreviated checklists have been issued as separate technical orders. Line items in the Flight Manual and checklists are identical with respect to arrangement and item numbers. Whenever a Safety Supplement affects the checklists, write in the applicable change on the affected checklist page. As soon as possible, a new checklist page incorporating the supplement will be issued. This will keep handwritten entries of Safety Supplement information in your checklist to a minimum. HOW TO GET PERSONAL COPIES Each flight crew member is entitled to a personal copy of the Flight Manual, Safety Supplements, Operational Supplements and Checklists. The required quantities should be ordered before you need them to assure their prompt receipt. Check with your quality assurance personnel. It is their job to fulfill your Technical Order requests. Basically, you must order the required quantities on the Publication Requirements Table (COMDTINST M13005 series). Make sure a system is established at your station to deliver these publications to the flight crew members immediately upon receipt. FLIGHT MANUAL AND CHECKLIST BINDERS Loose–leaf binders are available for use with your manual. These are obtained through local purchase procedures and are listed in the Federal Supply Schedule (FSC Group 75, Office Supplies, Part 1). Binders are also available for carrying your checklist. These binders contain plastic envelopes into which individual checklist pages are inserted. They are available in two capacities and are obtained through quality assurance. Check with your quality assurance personnel for assistance in securing these items. Sectionalized tabs may be special ordered through quality assurance. PERFORMANCE MANUALS For aircraft equipped with T–56–A–15 use T.O. 1C–130H–1–1. REFERENCE MANUALS The following manuals are to be used for reference as applicable. T.O. 1C–130A–9 AFJMAN 24–204 T.O. 1C–130–6CF–1 CFR 49, Parts 171,172, 173, 175 T.O. 1C–130E–5 T.O. 1–1B–40 T.O. 1–1B–50 COMDTINST M3710.1 (series) CGTO 1C–130–1 iv WARNINGS, CAUTIONS, AND NOTES The following definitions apply to “Warnings,” “Cautions,” and “Notes” found throughout the manual: WARNING – Operating procedures, techniques, etc., which will result in personal injury or loss of life if not carefully followed. CAUTION – Operating procedures, techniques, etc., which will result in damage to equipment if not carefully followed. NOTE – Operating procedures, techniques, etc., which are considered essential to emphasize. USE OF WORDS SHALL, WILL, AND MAY The following definitions apply to words “shall,” “will,” and “may” found throughout the manual: Shall and Will – Used to indicate a mandatory requirement. May – Indicates an acceptable or suggested means of accomplishment. USE OF CAPITAL LETTERS, QUOTATION MARKS, COMMAS AND VIRGULES, “IF INSTALLED,” “TYPICAL.” 1. In description information: a. Placarded name of switches, controls, fuses, circuit – CAPITALS breakers, illuminated annunciator lights, and illuminated pushbutton switch lights. b. Marked or unmarked switch/control positions. – CAPITALS IN QUOTATION MARKS c. The phrase “if installed” is used where equipment/switch locations could not accurately be determined before publication of this manual. If used with a checklist challenge, it means all series aircraft do not or will not have this item installed. If used with a checklist response, it means the item’s location varies with different series airplanes. 2. Checklist: a. In checklist responses/actions, placarded names and unplacarded switch positions will be in capitals, and unplacarded names/actions will be in initial capitals. Challenges will be in initial capitals. Quotation marks are reserved for spoken responses. b. A comma between crew positions or responses indicates that both will be applicable. A virgule (/) between positions or responses indicates either one or the other will apply. c. Due to the varying configurations of aircraft the phrase “Typical” is used when a description or figure is representative of the majority of aircraft. CGTO 1C–130–1 v GENERAL DESCRIPTION OF SYSTEM, POWER SOURCE, BUS, AND CIRCUIT BREAKER LOCATION. All ac power is assumed to be three–phase unless otherwise stated. All circuit protection is assumed to be a circuit breaker unless otherwise specified, i.e., fuse or current limiter. Circuit protection information is presented in manual as follows: (Paragraph Heading) FUEL FLOW GAUGES. Type Power 115V AC Inst & P Side Single Eng Fuel Cont Circuit Protection Bus Power Panel Location (reference Source is to physical location of panel) Circuit Pro– FUEL FLOW – IND NO. tection Title Type Power 28V Ess DC CP Side Bus Power Source Circuit Pro– FUEL FLOW tection Title General Each of the four fuel flow gauges Description (figure 1A–30) indicates flow in pounds per hour. Flow is meas– ured at the point where it enters the manifold (between TD valve and nozzles) on the engine. YOUR RESPONSIBILITY – TO LET US KNOW Every effort is made to keep the Flight Manual current. Flight Manual review conferences with operating personnel and a constant review of accident and flight test reports assure inclusion of the latest data in the manual. However, we cannot correct an error unless we know of its existence. In this regard, it is essential that you do your part. Comments, corrections, and questions regarding this manual or any phase of the Flight Manual program are welcomed. These should be forwarded through your C–130 Standardization Officer to Commanding Officer, USCG Air Station, Elizabeth City, NC 27909, ATTN: C–130 Standardization Unit. CGTO 1C–130–1 vi RECOMMENDATION FOR CHANGE OF PUBLICATION (FLIGHT PUBLICATIONS) DATE UNIT NUMBER (Reserved) PUBLICATION NUMBER (1) PAGE NUMBER (4) SUB–PARAGRAPH TITLE (6) BASIC DATE (2) REVISION/CHANGE DATE (3) MAJOR PARAGRAPH TITLE (5) ITEM NUMBER (7) (8) CHANGE DELETE SO MUCH OF PARAGRAPH ITEM FIGURE AS READS TO READ AFTER PRESENT (9) SENTENCE ITEM AS READS TO READ ADD NEW (10) PARAGRAPH SENTENCE ITEM FIGURE REASON FOR RECOMMENDED CHANGE, ADDITION OR DELETION (Include Adverse operational effects) (11) ORGANIZATION TYPED NAME AND GRADE OF ORIGINATOR SIGNATURE AF 847FORM AUG 74 CGTO 1C–130–1 vii/(viii blank) ACTION 1ST ENDORSEMENT TO: FROM: CONCUR DO NOT CONCUR REMARKS DATE TYPED NAME, GRADE AND TITLE SIGNATURE 2ND ENDORSEMENT TO: FROM: CONCUR DO NOT CONCUR REMARKS DATE TYPED NAME, GRADE AND TITLE SIGNATURE 3RD ENDORSEMENT TO: FROM: CONCUR DO NOT CONCUR REMARKS DATE TYPED NAME, GRADE AND TITLE SIGNATURE 4TH ENDORSEMENT TO: FROM: CONCUR DO NOT CONCUR REMARKS DATE TYPED NAME, GRADE AND TITLE SIGNATURE CGTO 1C–130–1 1–1 SECTION ....... I DESCRIPTION PART A – SYSTEMS TABLE OF CONTENTS PAGE PAGE THE AIRPLANE 1–1 . . . . . . . . . . . . . . . . . . . . . . . . . . ENGINES 1–23 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OIL SYSTEMS 1–35 . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGINE INSTRUMENTS 1–35 . . . . . . . . . . . . . . . . . . PROPELLERS 1–38 . . . . . . . . . . . . . . . . . . . . . . . . . . . . GTC (GAS TURBINE COMPRESSOR) 1–45 . . . . . . . ATM (AIR TURBINE MOTOR) 1–48 . . . . . . . . . . . . . . APU (AUXILIARY POWER UNIT) 1–48 . . . . . . . . . . FUEL SYSTEM 1–51 . . . . . . . . . . . . . . . . . . . . . . . . . . . ELECTRICAL POWER SUPPLY SYSTEM 1–61 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BLEED AIR SYSTEM 1–98 . . . . . . . . . . . . . . . . . . . . . AIR CONDITIONING SYSTEMS 1–99 . . . . . . . . . . . . CABIN PRESSURIZATION SYSTEM 1–116 . . . . . . . . ANTI–ICING AND DEICING SYSTEMS 1–123 . . . . . . HYDRAULIC POWER SUPPLY SYSTEMS 1–130 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT CONTROLS 1–135 . . . . . . . . . . . . . . . . . . . . . . FLAP SYSTEM 1–141 . . . . . . . . . . . . . . . . . . . . . . . . . . . LANDING GEAR SYSTEM 1–143 . . . . . . . . . . . . . . . . . BRAKE SYSTEM 1–153 . . . . . . . . . . . . . . . . . . . . . . . . . CARGO DOOR AND RAMP SYSTEM 1–156 . . . . . . . FLARE LAUNCHER SYSTEM 1–161 . . . . . . . . . . . . . . INSTRUMENTS 1–165 . . . . . . . . . . . . . . . . . . . . . . . . . . PITOT–STATIC INSTRUMENTS (1500 AND 1600 SERIES) 1–165 . . . . . . . . . . . . . . . . . . PITOT–STATIC INSTRUMENTS (CG 1700–1716 AND 1790) 1–167 . . . . . . . . . . . . . . . . . ROSEMOUNT PITOT STATIC SYSTEM (CG 1717 AND UP) 1–170 . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY EQUIPMENT 1–170 . . . . . . . . . . . . . . . LIGHTING SYSTEM 1–178 . . . . . . . . . . . . . . . . . . . . . . OXYGEN SYSTEM 1–190 . . . . . . . . . . . . . . . . . . . . . . . MISCELLANEOUS EQUIPMENT 1–194 . . . . . . . . . . . A/A32H–4A CARGO HANDLING SYSTEM 1–198 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SINGLE POINT REFUELING AND DEFUELING SYSTEM 1–204 . . . . . . . . . . . . . . . . . . . . THE AIRPLANE The Lockheed C-130 is an all-metal, high-wing, long-range, land-based monoplane. The fuselage is divided into the cargo compartment and the flight station. It can be fully pressurized and air conditioned, both in flight and on the ground. The mis- sion of the airplane is to provide rapid transportation of per- sonnel or cargo for delivery by parachute or by landing. The airplane can be used as a tactical transport carrying 86 ground troops or 58 paratroops and equipment, and can be readily converted for ambulance or aerial delivery missions. When used as an ambulance, the airplane can carry up to 66 litters. There are provisions for normal life raft storage to accommo- date 80 persons for overwater flights. The C-130 can land and takeoff on short runways, and it can be used on landing strips such as those usually found in advance base operations. CGTO 1C–130–1 1-2 Aircraft Dimensions (Typical) Figure 1A–1 52 FT 8 IN. 3 FT. 1 IN. 30 FT 1 IN. 132 FT 7 IN. 13 FT 6 IN. DIA 5 FT 10 IN. 6 FT 7 IN. 7 FT 6 IN. 1 FT 10 IN. 14 FT 3 IN. 2 30’ DIHEDRAL FLIGHT REFERENCE LINE 15 FT 3 IN. 11 FT 6 IN. 29 FT 6 IN. 5 FT 99 FT 7 IN. 38 FT 8 IN. NOTE 1. DIMENSIONS SHOWN AIRPLANE EQUIPPED AND EMPTY. CGTO 1C–130–1 1–3 Figure 1A–2 Cargo Compartment Loading (Typical) 108 IN. 492 IN. NOTE DO NOT USE FOR CARGO LOADING INFORMATION. FOR LOADING INFORMATION USE T.O. 1C–130A–9 123 IN. 123 IN. CGTO 1C–130–1 1-4 Figure 1A–3 OUTER WING STATION 0 CENTER WING STATION 220 OWS 576 OWS 224 OWS 182 WS 196 WS 84.3 C/L 0.0 OWS 82 JACK POINT HYPOTHETICAL CENTER OF GRAVITY JACK POINT 0 30 93 165 380 535 597.58 737 941 1079 FS523 FS583 FUSELAGE STATIONS 0 100 200 300 400 500 600 700 800 900 1000 1100 245 CGTO 1C–130–1 1–5 Figure 1A–4 (Sheet 1 of 2) General Arrangement and Servicing Diagram 1 2 2 1 35 37 36 3 3 16 15 15 16 17 1 34 33 31 32 30 29 28 27 26 25 24 23 22 21 20 19 18 16 15 SPECIFICATIONS RECOMMENDED FUEL OIL HYDRAULIC FLUID MIL–T–5624 JP–4 ENGINE MOBIL OIL 254 APU/GTC STARTER MIL–H–83282 F–40 H–537 NATO SYMBOL 1 SPECIFICATIONS EXTINGUISHER FLUID OXYGEN PROPELLER FLUID MIL–H–83282 MIL–O–27210 TYPE II H–537 ENGINE AND APU ALTERNATE HAND EXTINGUISHERS MIL–D–4540 MIL–B–4394 HALON 1211 NATO SYMBOL CGTO 1C–130–1 1-6 Figure 1A–4 (Sheet 2 of 2) 1. FUEL FILLER POINTS (6 PLACES) 2. MAIN FUEL TANKS (4 PLACES) 3. AUXILIARY FUEL TANKS (2 PLACES) 4. GROUND AIR CONDITIONING ADAPTERS 5. WATER BOTTLES (LH–5, RH–5) 6. RAMP 7. FLARE STOWAGE 8. FLARE LAUNCHER 9. FLARE STOWAGE COMPARTMENTS 10. CARGO DOOR 11. ENGINE TAILPIPE SHIELDS 12. AUXILIARY HYDRAULIC SYSTEM RESERVOIR 13. TOILET 14. PARATROOP DOORS (LH SHOWN – RH OPPOSITE) 15. ENGINE OIL AND STARTER OIL (4 PLACES) 16. PROPELLER OIL RESERVOIR 17. EXTERNAL FUEL TANKS (2 PLACES)(IF INSTALLED) 18. FIRE EXTINGUISHER AGENT BOTTLES 19. APU/GTC RESERVOIR 20. APU/GTC 21. UTILITY HYDRAULIC RESERVOIR 22. ENGINE AIR INTAKE SHIELDS 23. SCANNER’S SEAT (LH SHOWN – RH OPPOSITE) 24. STOWAGE CABINET 25. GALLEY 26. EXTERNAL ELECTRICAL POWER RECEPTACLE 27. BATTERY 28. EXTERNAL INTERPHONE CONNECTION 29. PILOT’S AND COPILOT’S SEATS 30. FLIGHT ENGINEER’S SEAT 31. NAVIGATOR’S SEAT 32. CURTAIN 33. RADIO OPERATOR’S SEAT 34. BOOSTER HYDRAULIC SYSTEM RESERVOIR 35. TOILET SERVICING ADAPTER 36. SINGLE POINT REFUELING ADAPTER 37. OXYGEN FILLER 4 5 6 7 8 9 10 11 12 13 14 2 1 1 2 17 16 15 1 BENDIX STARTERS ARE PERMANENTLY LUBRICATED NOTE 1 CGTO 1C–130–1 1–7 CH–1 Figure 1A–5 Overhead Control Panel (Typical) 3 4 5 8 18 17 12 13 14 15 16 11 10 6 7 1 2 19 1. FUEL GOVERNING CHECK PANEL 10. OVERHEAD ELECTRICAL CONTROL PANEL 2. ANTI–SKID PANEL 11. FUEL CONTROL PANEL 3. FLIGHT ENGINEER’S INTERCOM MONITOR PANEL 12. FIRE EMERGENCY CONTROL PANEL 4. FLIGHT ENGINEER’S INTERCOM CONTROL PANEL 13. OIL COOLER FLAP CONTROL PANEL 5. OXYGEN REGULATOR PANEL 14. CONTROL BOOST SWITCH PANEL 6. AIR CONDITIONING AND PRESSURIZATION 15. ICE DETECTION PANEL CONTROL PANEL 16. ENGINE STARTING CONTROL PANEL 7. APU CONTROL PANEL 17. ANTI–ICE OVERHEAT PANEL (1500 SERIES) 8. ANTI–ICING SYSTEMS CONTROL PANEL 18. FLARE LAUNCH PANEL 9. DELETED 19. ICS CONNECTOR DEPENDING ON AIRCRAFT SERIES, THIS DEPICTION MAY VARY FROM ACTUAL EQUIPMENT INSTALLATION 1 NOTE 1 1 1 1 CGTO 1C–130–1 1-8 CH–1 Figure 1A–6 (Sheet 1 of 2) Instrument Panel (CGNR 1503, 1504) 1. MAGNETIC COMPASS 16. MARKER BEACON CONTROL PANEL 2. ACCELEROMETER 17. WEATHER RADAR INDICATOR 3. DOOR OPEN WARNING LIGHT 18. ELEVATOR TAB POSITION INDICATOR 4. INS WAYPOINT ALERT INDICATOR 19. AILERON TAB POSITION INDICATOR 5. INS ATTITUDE SELECTOR SWITCH 20. RUDDER TAB POSITION INDICATOR 6. ATTITUDE DIRECTOR INDICATOR 21. ELECTRONIC FUEL CORRECTION PANEL 7. HORIZONTAL SITUATION INDICATOR 22. AIR DIVERTER HANDLE 8. ALTITUDE LOW WARNING LIGHT 23. DELETED 9. BEAM COUPLER OFF LIGHT 24. AIRSPEED LIMITATION PLACARD 10. INS NAV SELECT SWITCH 25. AUTOPILOT OFF LIGHT 11. ALTIMETER-ENCODER 26. MAGNETIC COMPASS CORRECTION CARD HOLDER 12. MASTER FIRE WARNING LIGHT 27. BEARING-DISTANCE-HEADING INDICATOR 13. NAVIGATION SELECTOR PANEL 28. RADIO MAGNETIC INDICATOR 14. VSI – TA/RA DISPLAY 29. CLOCK 15. RADAR ALTIMETER 30. AIRSPEED INDICATOR 1 2 3 4 5 6 7 8 10 11 12 13 14 15 16 17 19 20 26 27 28 29 30 24 22 21 18 25 9 CGTO 1C–130–1 1–9 CH–1 Figure 1A–6 (Sheet 2 of 2) 1 26 2 3 4 5 6 7 8 9 10 11 12 14 15 16 17 18 19 20 21 27 22 23 24 25 1. CABIN ALTIMETER 14. VSI–TA/RA DISPLAY 2. FREE AIR TEMPERATURE INDICATOR 15. CLOCK 3. NACELLE OVERHEAT WARNING 16. BEARING-DISTANCE-HEADING INDICATOR 4. AIRSPEED INDICATOR 17. HOMING SYSTEM SLAVE INDICATOR 5. SELECTED NAV SYSTEM OFF LIGHT 18. SLAVE INDICATOR BRIGHT/DIM SWITCH 6. ATTITUDE DIRECTOR INDICATOR 19. AIR DIVERTER HANDLE 7. HORIZONTAL SITUATION INDICATOR 20. HYDRAULIC CONTROL PANEL 8. ALTITUDE LOW WARNING LIGHT 21. PROP LOW OIL QUANTITY MASTER WARNING LIGHT 9. COPILOT’S ADI REPEAT LIGHT 22. LANDING AND TAXI LIGHTS CONTROL PANEL 10. INS NAV SELECT SWITCH 23. LANDING GEAR CONTROL PANEL 11. ALTIMETER 24. RADIO MAGNETIC INDICATOR 12. NAVIGATION SELECTOR PANEL 25. WING FLAP POSITION INDICATOR 13. SCROLL CHECKLIST 26. CABIN LOW PRESSURE WARNING LIGHT 27. ENG LOW OIL QUANTITY MASTER WARNING LIGHT 13 CGTO 1C–130–1 1-10 CH–1 Instrument Panel (Typical) Figure 1A–7 (Sheet 1 of 2) 1. MAGNETIC COMPASS 2. CLOCK 3. DOOR OPEN WARN LIGHT 4. GPWS INOP ANN 5. GPWS PULL UP ANN 6. ATT SEL SW AND IND LIGHT 7. ATT DIRECTOR INDICATOR 8. HORIZONTAL SITUATION IND 9. GPWS OVERRIDE ANN 10. GPWS BELOW GS ANN 11. FCS MODE ANN LIGHT PANEL 12. FCS WARN OR ADVISORY ANN LIGHT PANEL 13. ALTIMETER–ENCODER 14. MASTER FIRE WARN LIGHT 15. NAV SEL CONTROL PANEL 16. VERTICAL VELOCITY INDICATOR 17. RADIO ALTIMETER 18. MARKER BEACON INDICATOR 19. WEATHER RADAR INDICATOR 20. ELECTRONIC FUEL CORRECTION PANEL 21. ELEV TAB POSITION INDICATOR 22. RUD TAB POSITION INDICATOR 23. AILERON TAB POSITION INDICATOR 24. AIR DIVERTER HANDLE 25. AIRSPEED LIMITATION PLACARD 26. BEARING–DISTANCE–HEADING INDICATOR 27. ACCELEROMETER 28. WAY POINT ALERT INDICATOR 29. RADIO MAGNETIC INDICATOR 30. AIRSPEED INDICATOR 31. GPS MODE ANNUNCIATOR PANEL 32. PITOT HEAT OFF LIGHT (1717 AND UP) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 31 18 19 20 21 22 23 24 25 26 27 28 29 30 32 CGTO 1C–130–1 1–11 CH–1 Figure 1A–7 (Sheet 2 of 2) 1. CABIN ALTIMETER 2. NACELLE OVERHEAT WARN 3. AIRSPEED INDICATOR 4. ATT DIRECTOR INDICATOR 5. GPWS OVERRIDE ANN 6. HORIZONTAL SITUATION IND 7. FCS MODE ANN LIGHT PANEL 8. ATT SEL SW AND IND LIGHT 9. GPWS BELOW GS ANN 10. GPWS PULL UP ANN 11. ALTIMETER 12. FCS WARN OR ADVISORY ANN LIGHT PANEL 13. SCROLL CHECKLIST HOLDER 14. NAV SEL CONTROL PANEL 15. VERTICAL VELOCITY INDICATOR 16. NAV REPEAT LIGHT 17. BEARING–DISTANCE–HEADING INDICATOR 18. CLOCK 19. HOMING SYSTEM SLAVE INDICATOR 20. SLAVE INDICATOR BRIGHT/DIM SWITCH 21. AIR DIVERTER HANDLE 22. HYDRAULIC CONTROL PANEL 23. PROP LOW OIL QTY MASTER WARN LIGHT 24. ENG LOW OIL QTY WARN LIGHT 25. LANDING AND TAXI LIGHTS CONTROL PANEL 26. RADIO MAGNETIC INDICATOR 27. LANDING GEAR CONTROL PANEL 28. WAYPOINT ALERT INDICATOR 29. WING FLAP POSITION INDICATOR 30. STANDBY ATTITUDE INDICATOR 31. CABIN LOW PRESSURE LIGHT 32. PITOT HEAT OFF LIGHT (1717 AND UP) TAC 2 TAC 1 VOR/ ILS 1 VOR/ ILS 2 SELECTOR POINTER VOR 2 CDNU INS 1 INS 2 AIR 0 3 6 13 18 21 24 27 30 ADF 1 ADF 2/UHF/VHF/DF MILES E 12 15 S 21 24 W 30 33 N 3 6 COURSE O77 HEADING 350 300 250 200 180 160 140 120 100 80 1 2 3 4 5 6 7 8 9 5 4 0 0 1 0 1 3 9 , 9 2 2 100 FEET MILLIBARS IN HG ADF 1 TAC 1/ADF 2 0 33 30 27 24 21 18 12 6 3 60 12 55 50 45 40 35 30 25 20 15 10 5 11 10 9 8 7 6 5 4 3 2 1 INS1 ATT INS2 ATT 1 2 3 4 W PT ALERT CABIN LOW PRESSURE NAV REPEAT CAUTION NACELLE OVERHEAT TEST NORM DOWN UP 20 40 60 80 FLAPS PERCENT EXTENDED HANDLE LIGHT TEST LEFT NOSE RIGHT LOCK RELEASE UP DOWN HORN SILENCE TO RIGHT LEFT FROM BRT DIM 0 1 2 3 4 HYD PRESS PSI X 1000 0 1 2 3 4 HYD PRESS PSI X 1000 0 1 2 3 4 HYD PRESS PSI X 1000 0 1 2 3 4 HYD PRESS PSI X 1000 0 1 2 3 4 HYD PRESS PSI X 1000 0 1 2 3 4 HYD PRESS PSI X 1000 0 1 2 3 4 HYD PRESS PSI X 1000 RUDDER BOOST PRESS UTILITY BOOSTER BOOSTER UTILITY OFF OFF OFF OFF OFF ON ON ON ON ON SUCTION BOOST PUMP ENGINE PUMP PRESSURE WARNING ENGINE PUMP PRESS OFF BRAKES AUXILIARY NORMAL AUX PUMP ON OFF ANTI-SKID INOPERATIVE EMERGENCY A N T I S K I D LANDING LIGHTS TAXI LIGHTS AP DISENG ELEV TRIM AP FAIL TRIM FAIL AP CPLD COMPTR FAIL HDG NAV ARM NAV CAPT ALT HOLD GS ARM GS CAPT BACK LOC G/A BRAKE SELECT ENG OIL LOW PROP OIL LOW LEFT MOTOR RIGHT MOTOR EXTEND HOLD RETRACT ON OFF LEFT LIGHT RIGHT LIGHT ON OFF 10 20 30 40 50 CABIN PRESSURE ALTITUDE KNOTS NAV SEL VOR 1 GPWS TEST PULL UP GPWS OVRD BELOW G/S OFF CLI MB DI VE PUL L CAGE TO 4 +12 -03 +05 1 2 .5 6 4 2 1 .5 0 TCAS VSI RNG 5 ABOVE FL- - VERTICAL SPEED 1000 FPM BRT TA SEL 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 PITOT HEAT OFF 32 CGTO 1C–130–1 1-12 Figure 1A–8 Flight Control Pedestal (1500 Series without CDNU Modification) 1. TACAN NO. 1 CONTROL PANEL 2. PILOT’S INTERCOMMUNICATION SYSTEM CONTROL PANEL 3. COPILOT’S INTERCOMMUNICATION SYSTEM CONTROL PANEL 4. TACAN NO. 2 CONTROL PANEL 5. VHF NAV NO. 2 CONTROL PANEL 6. ADF NO. 2 CONTROL PANEL 7. COPILOT’S INTERCOMMUNICATION SYSTEM MONITOR PANEL 8. VHF-DF SELECTOR PANEL 9. UHF ANTENNA SELECTOR PANEL 10. LOW SPEED GROUND IDLE PANEL 11. AUTOPILOT CONTROLLER 12. ASSISTED TAKEOFF CONTROL PANEL 13. ADS CONTROL PANEL 14. UHF COMM CONTROL PANEL 15. VHF COMM CONTROL PANEL 16. VHF DF SELECTOR SWITCH 17. IFF ANTENNA SWITCH AND CAUTION LIGHT PANEL 18. FLAP CONTROL QUADRANT 19. MODE S CONTROL PANEL 20. INS AUTOPILOT ENGAGE AND AUTOPILOT HOLD SWITCH PANEL 21. AUTOPILOT CONTROL PANEL 22. TRIM TAB CONTROL PANEL 23. ELEVATOR TRIM TAB POWER SWITCH 25. CRASH POSITION INDICATOR CONTROL PANEL 26. PILOT’S INTERCOMMUNICATION MONITOR PANEL 27. VHF-FM CONTROL PANEL 28. VHF NAV NO. 1 CONTROL PANEL 1 2 28 27 3 26 25 23 22 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 116.40 1 1 1 X TEST NAV VOL T C N CHANNEL CHARGE RELEASE BEACON TEST VHF–FM NORMAL TURN PRESS FOR LOW SPEED ASSISTED TAKE–OFF ARMED SAFE R E A D Y F I R E 1 2 3 LOW SPEED IDLE 310.600 C H U T E R E L OPEN OFF CLOSE OPEN ADS IFF CAUTION IFF ANT SW TOP BOT BOTH VHF DF OFF VHF DF ON PWR TEST OFF VOL 1 1 3 .8 0 U H F GUARD MANUAL RESET READ ADF BOTH MAIN OFF PRESET SQUELCH OFF ON TONE VOLUME DIR TEST 01 02 03 04 05 06 07 08 09 10 11 12 13 14 15 16 17 18 19 20 D E P L O Y C P I C P I XMT OFF REC T/R AM REC AM T/R OFF OFF VOL RUD ELEV ENGAGE ALL A U T O P I L O T S E R V O DISENGAGE AFF RANGE LOC GYRO PILOT BLUE LEFT LOC PRESS FOR BLUE LEFT RESET A/P INS ENGAGE INS A/P HOLD FL TCAS RANGE 510 3040 ALT SOURCE 1 2 OFF ATC IDENT ATC FAIL ABOVE BELOW NORM ATC 2 ON STBY TEST STBY TEST ATC 1 ON CAL VOL HOT MIC TALK LSPKR V/U-2 HF-2 FM RT V/U-1 HF-1 VHF I N T E R CAL VOL HOT MIC TALK LSPKR V/U–2 HF–2 FM RT V/U–1 HF–1 VHF I N T E R 4 3 2 1 1 2 3 4 FEATHER TAKE OFF MOVEMENT SHALL NOT BE MADE IN LESS THAN ONE SECOND T H R O T T L E E N G I N E C O N D I T I O N GROUND STOP FLIGHT IDLE FLIGHT IDLE GROUND IDLE TRIM FLAPS TEMP DATUM CONTROL VALVE PA ADF–1 VOR–1 TACAN 1 BCN ADF–2 VOR–2 TACAN 2 PA ADF–1 VOR–1 TACAN 1 BCN ADF–2 VOR–2 TACAN 2 1 6 3 9 8 2 4 116.40 1 1 1 X TEST NAV VOL T C N CHANNEL OFF REC T/R AM REC AM T/R OFF OFF VOL CGTO 1C–130–1 1–13 Flight Control Pedestal (Typical) Figure 1A–9 1. CONTROL DISPLAY NAVIGATION UNIT (CDNU) (PILOT’S) 2. PILOT’S INTERCOMMUNICATION CONTROL PANEL 3. COPILOT’S INTERCOMMUNICATION CONTROL PANEL 4. TCAS/MODE S CONTROL PANEL 5. EMERGENCY RADIO SELECT PANEL 6. RADIO MASTER VOLUME CONTROL PANEL 7. COPILOT’S INTERCOMMUNICATION MONITOR PANEL 8. NO. 2 U/V ANTENNA SELECT CONTROL PANEL 9. VHF/DF SELECTOR CONTROL PANEL 10. LOW SPEED GROUND IDLE AND ADS CONTROL PANEL 11. FCS ANNUNCIATOR LIGHTS CONTROL PANEL 12. AUTOPILOT CONTROLLER 13. FCS NO. 2 REMOTE HEADING AND COURSE SELECTOR 14. FCS NO. 2 MODE SELECTOR PANEL 15. ADF NO. 2 CONTROL PANEL 16. VHF-FM RADIO CONTROL PANEL 17. FLAP CONTROL QUADRANT 18. IFF TRANSPONDER CONTROL PANEL 19. INS SEARCH HOLD AND CAUTION IFF PANEL 20. FCS NO. 1 MODE SELECTOR PANEL 21. FCS NO. 1 REMOTE HEADING AND COURSE SELECTOR 22. TRIM TAB CONTROL PANEL 23. ELEVATOR TRIM TAB POWER SELECTOR PANEL 24. VHF/DF SELECTOR CONTROL PANEL 25. NO. 1 U/V ANTENNA SELECT CONTROL PANEL 26. PILOT’S INTERCOMMUNICATION MONITOR PANEL 1 2 3 26 25 24 23 22 21 20 19 18 17 16 15 14 13 12 11 10 9 8 7 6 5 4 1 2 3 A B C D E F L R X K Q W J P V I O U H N T G M S 6 9 5 8 0 4 7 F4 F3 F2 F1 F5 F6 F7 Z Y MENU STAT CLR PROG DIR FPLN RNAV MARK 1DX BRT OFF ON HF 1 HF 2 VHFFM RT VU 1 VU2 CAL VOL HOT MIC TALK LSPKR V/U–2 HF–2 FM RT V/U–1 HF–1 VHF I N T E R HF1 HF 2 VHF FM RT VU 1 VU2 CAL VOL HOT MIC TALK LSPKR V/U–2 HF–2 FM RT V/U–1 HF–1 VHF I N T E R RADIO MASTER VOLUME CONTROL VHF V/U–1 V/U–2 4 3 2 1 1 2 3 4 FEATHER TAKE OFF MOVEMENT SHALL NOT BE MADE IN LESS THAN ONE SECOND T H R O T T L E E N G I N E C O N D I T I O N GROUND STOP FLIGHT IDLE FLIGHT IDLE GROUND IDLE U/V ANTENNA SELECT U/V ANTENNA SELECT TRIM OPEN AERIAL DELIVERY SYSTEM SEARCH HOLD CAUTION IFF TOP AUTO BOT AP CP ID ATT SEL ATT HDG NAV IOC APPR VS IAS AP CP ID ATT HDG NAV IOC APPR 1 6 3 9 8 2 4 1 2 3 4 2 3 1 0 2 7 FLAPS TEMP DATUM CONTROL VALVE CGTO 1C–130–1 1-14 CH–1 Figure 1A–10 Navigator’s Station (Typical) 1. ELECTRICAL SPARES STORAGE 2. INSTRUMENT PANEL 3. CONSOLE 4. CONTROL PANEL 5. RADAR INDICATOR 6. FREE AIR TEMPERATURE INDICATOR 7. BLEED AIR MANFOLD PRESSURE INDICATOR 8. REMOTE COMPENSATORS (SINGLE LN–100 ONLY) BLEED MANIFOLD PRESS PSI 50 0 100 C 40 30 0 -20 -40 -60 1 2 3 4 5 6 7 8 CGTO 1C–130–1 1–15 CH–1 Figure 1A–11 Navigator’s Instrument Panel 1. ALTIMETER–ENCODER 2. BEARING–DISTANCE–HEADING INDICATOR (BDHI) 3. POINTER SELECTOR SWITCH 4. CLOCK 5. BLANK 6. COMPASS MODE SELECTOR 7. TRUE AIRSPEED INDICATOR 8. FREE AIR TEMPERATURE INDICATOR 9. NAVIGATOR’S INSTRUMENT LIGHTS CONTROL 1 2 3 4 5 6 7 9 8 2 A ON SINGLE LN–100 INSTALLATIONS THIS SPACE IS OCCUPIED BY THE C–12 DIGITAL CONTROLLER NOTE 1 B CGTO 1C–130–1 1-16 Figure 1A–12 Navigator’s Control Panel (1500 Series without CDNU Modification) A 1. SEA SEARCH RADAR (INDICATOR) 2. AIRBORNE VIDEO CASSETTE TAPE RECORDER 3. INS NO. 1 MODE SELECTOR UNIT 4. RADAR FAN WARNING LIGHT 5. INS RAPID/UPDATE/FAN WARNING PANEL 6. ANS–4 RECEIVER/CONTROL 7. ADF NO. 1 CONTROL PANEL 8. OXYGEN REGULATOR 9. REMOTE SEA SEARCH RADAR CONTROL 10. SEA SEARCH RADAR B–SCAN DISPLAY 11. SEA SEARCH RADAR CONTROL INDICATOR 12. INS NO. 1 CONTROL DISPLAY UNIT 2 1 3 4 5 6 7 8 9 10 11 12 A CGTO 1C–130–1 1–17 CH–1 Figure 1A–13 Navigator’s Control Panel (Typical) 1. SEA SEARCH RADAR (INDICATOR) 2. AIRBORNE VIDEO CASSETTE TAPE RECORDER 3. INS NO. 1 MODE SELECTOR UNIT 4. RADAR FAN WARNING LIGHT 5. INS NO. 2 MODE SELECTOR UNIT 6. CONTROL DISPLAY NAVIGATION UNIT (CDNU) A 7. ANS–4 RECEIVER/CONTROL 8. OXYGEN REGULATOR 9. REMOTE SEA SEARCH RADAR CONTROL 10. SEA SEARCH RADAR B–SCAN DISPLAY 11. SEA SEARCH RADAR CONTROL INDICATOR 12. INS NO. 1 CONTROL DISPLAY UNIT 13. INS NO. 2 CONTROL DISPLAY UNIT A 2 1 3 4 5 6 7 8 9 10 11 13 12 CGTO 1C–130–1 1-18 CH–1 Figure 1A–14 Navigator’s Console (CGNR 1503, 1504) 1. C–12 COMPASS NO. 1 REMOTE COMPENSATOR 2. C–12 COMPASS NO. 2 REMOTE COMPENSATOR 3. CFA OVERRIDE PANEL 4. SEA SEARCH RADAR COOLING FAN CONTROL PANEL 5. VHF WFS–210 RECEIVER CONTROL 6. NAVIGATOR’S ICS MONITOR PANEL 7. NAVIGATOR’S ICS CONTROL PANEL 8. PUBLIC ADDRESS SYSTEM CONTROL PANEL 9. NAVIGATOR’S LIGHTING CONTROL 10. ICS DISCONNECT RECEPTACLE 11. COMPASS CORRECTION CARD HOLDER 12. TEST EQUIPMENT CONNECTOR 13. SEA SEARCH RADAR VIDEO CONVERTER 14. NAVIGATOR’S FUNCTION CONTROL PANEL 15. BOTTOM STROBE LIGHT TEST SWITCH 15 1 2 3 4 5 6 7 8 9 10 11 13 14 A A 12 A A CGTO 1C–130–1 1–19 CH–1 Figure 1A–15 Navigator’s Console (Typical) 1. C–12 COMPASS NO. 1 REMOTE COMPENSATOR 2. C–12 COMPASS NO. 2 REMOTE COMPENSATOR 3. PUBLIC ADDRESS SYSTEM CONTROL PANEL 4. DIGITAL TRANSFER DEVICE 5. GPS FILL PANEL 6. SEA SEARCH RADAR COOLING FAN CONTROL PANEL 7. CFA OVERRIDE PANEL 8. NAVIGATOR’S ICS MONITOR PANEL 9. NAVIGATOR’S ICS CONTROL PANEL 10. ADF NO. 1 CONTROL PANEL 11. NAVIGATOR’S LIGHTING CONTROL 12. ICS DISCONNECT RECEPTACLE 13. COMPASS CORRECTION CARD HOLDER 14. TEST EQUIPMENT CONNECTOR 15. SEA SEARCH RADAR VIDEO CONVERTER 16. NAVIGATOR’S FUNCTION CONTROL PANEL 17. COCKPIT VOICE RECORDER CONTROL UNIT 18 COCKPIT VOICE RECORDER TEST SWITCH 19. BOTTOM STROBE LIGHT TEST SWITCH A 14 3 4 5 6 7 1 2 17 16 8 9 10 11 12 15 A 18 19 13 CGTO 1C–130–1 1-20 Figure 1A–16 Radio Operator’s Station (1500 Series) 1. BOOM LIGHT 2. LIGHTING CONTROL PANEL 3. ICS DISCONNECT RECEPTACLE 4. OXYGEN REGULATOR 5. INTERCOMMUNICATION CONTROL PANEL 6. INTERCOMMUNICATION MONITOR PANEL 7. HF SECURE SQUELCH PANEL 8. HF COMMUNICATION NO. 2 CONTROL PANEL 9. HF COMMUNICATION NO. 1 CONTROL PANEL 10. SECURE VOICE NO. 2 REMOTE CONTROL UNIT IIB 11. SECURE VOICE NO. 1 REMOTE CONTROL UNIT IIB 12. SECURE VOICE NO. 2 REMOTE CONTROL UNIT IIA 13. SECURE VOICE NO. 1 REMOTE CONTROL UNIT IIA 14. BOOM LIGHT CONTROL A 1 2 3 5 4 6 7 8 9 10 11 12 13 14 A