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FSC: 6610 - Flight Instruments

A-A-58055 - A-A-58055, COMMERCIAL ITEM DESCRIPTION: INDICATOR, ATTITUDE, THREE INCH, SOLID STATE SELF-CONTAINED (01-JAN-1996)
TR-74-116 - AFFDL TR-74-116, TECHNICAL REPORT: BACKGROUND INFORMATION AND USER GUIDE FOR MIL-F-9490D; FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR (JAN-1975)
TR-74-116 - AFFDL TR-74-116, TECHNICAL REPORT: BACKGROUND INFORMATION AND USER GUIDE FOR MIL-F-9490D - FLIGHT CONTROL SYSTEMS; DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR (JAN 1975)
AFGS-87242 A - AFGS-87242A (NOTICE 1), AIR FORCE GUIDE SPECIFICATION,: FLIGHT CONTROL SYSTEM GENERAL SPECIFICATION FOR (27 JUL 2001) [SUPERSEDING MIL-F-87242] [S/S b
AFGS-87211 A - AFGS-87211A (NOTICE-1), AIR FORCE GUIDE SPECIFICATION: AIR DATA SYSTEMS (31-DEC-1997) [NO S/S DOCUMENT]
AFGS-87213 A - AFGS-87213A, AIR FORCE GUIDE SPECIFICATION: DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED (30 NOV 1987) [S/S BY MIL-HDBK-87213]
AFGS-87213 B - AFGS-87213B (NOTICE 2), AIR FORCE GUIDE SPECIFICATION: DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED (27 FEB 1997) [S/S BY MIL-HDBK-87213]
AFGS-87213 B - AFGS-87213B (NOTICE 1), AIR FORCE GUIDE SPECIFICATION: DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED (05 APR 1996) [S/S BY MIL-HDBK-87213]
AFGS-87213 B - AFGS-87213B, AIR FORCE GUIDE SPECIFICATION: DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED (08-JAN-1993) [S/S BY MIL-HDBK-87213]
AFGS-87242 A - AFGS-87242A, AIR FORCE GUIDE SPECIFICATION: FLIGHT CONTROL SYSTEM GENERAL SPECIFICATION FOR (31-MAR-1986) [SUPERSEDING MIL-F-87242] [S/S by JSSG-2008]
AFGS-87242 A - AFGS-87242A (AMENDMENT 1), AIR FORCE GUIDE SPECIFICATION: FLIGHT CONTROL SYSTEM GENERAL SPECIFICATION FOR (25 OCT 1996) [SUPERSEDING MIL-F-87242] [S/S
AN5811 7 - AN5811 (REV. 7), AIR FORCE-NAVY AERONAUTICAL STANDARD: TUBE, PITOT, ELECTRICALLY HEATED, "L" SHAPED, INVERTED (13 MAY 1988)
AN5811 7 - AN5811 (REV. 7) (NOTICE 1), DETAIL SPECIFICATION SHEET: TUBE, PITOT, ELECTRICALLY HEATED, "L" SHAPED, INVERTED (13 MAY 1988)
AN5812 7 - AN5812 (REV. 7), AIR FORCE-NAVY AERONAUTICAL STANDARD: TUBE, PITOT, ELECTRICALLY HEATED, "L" SHAPED (30 MAR 1956)
AN5812 7 - AN5812 (REV. 7) (NOTICE 2), DETAIL SPECIFICATION SHEET: TUBE, PITOT, ELECTRICALLY HEATED, "L" SHAPED (13 JUL 2007)
AN5812 7 - AN5812 (REV. 7) (NOTICE 1), DETAIL SPECIFICATION SHEET: TUBE, PITOT, ELECTRICALLY HEATED, "L" SHAPED (03 JUN 1996)
MIL-A-5885 D - MIL-A-5885D, MILITARY SPECIFICATION: ACCELEROMETER, AIRCRAFT (09 FEB 1987)
MIL-A-5885 D - MIL-A-5885D (AMENDMENT 1), MILITARY SPECIFICATION: ACCELEROMETER, AIRCRAFT (15 APR 1994)
MIL-A-5885 D - MIL-A-5885D (NOTICE 2), MILITARY SPECIFICATION: ACCELEROMETER, AIRCRAFT (14 AUG 2008)
MIL-A-5885 D - MIL-A-5885D (NOTICE 1), MILITARY SPECIFICATION: ACCELEROMETER, AIRCRAFT (01 APR 1996).
MIL-A-27671 B - MIL-A-27671B, MILITARY SPECIFICATION: AMPLIFIER-INDICATOR GROUP, ALTITUDE-VERTICAL SPEED A/A24G-11 (16-AUG-1965)
MIL-A-27671 B - MIL-A-27671B (NOTICE-2), MILITARY SPECIFICATION: AMPLIFIER-INDICATOR GROUP, ALTITUDE-VERTICAL SPEED A/A24G-11 (05-NOV-2006)
MIL-A-27671 B - MIL-A-27671B (NOTICE-1), MILITARY SPECIFICATION: AMPLIFIER-INDICATOR GROUP, ALTITUDE-VERTICAL SPEED A/A24G-11 (01-JAN-1996)
MIL-A-27671 B - MIL-A-27671B (AMENDMENT-3), MILITARY SPECIFICATION: AMPLIFIER-INDICATOR GROUP, ALTITUDE-VERTICAL SPEED A/A24G-11 (06-AUG-1986)
MIL-A-83419 C - MIL-A-83419C, MILITARY SPECIFICATION: ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY (15-OCT-1979) [S/s by MIL-prf-83419D]
MIL-A-83419 C - MIL-A-83419C (AMENDEMENT-3), MILITARY SPECIFICATION: ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY (15-APR-1994) [S/S by MIL-PRF-83419D].
MIL-A-83419 C - MIL-A-83419C (NOTICE-1), MILITARY SPECIFICATION: ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY (01-AUG-1996) [S/S by MIL-PRF-83419D].
MIL-C-38286 A - MIL-C-38286A, MILITARY SPECIFICATION: COMPUTER, FLIGHT DIRECTOR CPU-65/A (15-DEC-1977)
MIL-C-38286 B - MIL-C-38286B, MILITARY SPECIFICATION: COMPUTER, FLIGHT DIRECTOR CPU-65/A (16-MAY-1990)
MIL-C-38286 B - MIL-C-38286B (NOTICE 2), MILITARY SPECIFICATION: COMPUTER, FLIGHT DIRECTOR CPU-65/A (01-FEB-2005)
MIL-C-38286 B - MIL-C-38286B (NOTICE 1), MILITARY SPECIFICATION: COMPUTER, FLIGHT DIRECTOR CPU-65/A (15-JAN-1996)
MIL-C-83321 A - MIL-C-83321A (NOTICE-1), CONTROL ASSEMBLY, GYROSCOPE, ATTITUDE-HEADING (19-JUN-1980) [NO S/S DOCUMENT]
MIL-D-81641 - MIL-D-81641, MILITARY SPECIFICATION: DISPLAY, HEAD-UP, GENERAL SPECIFICATION FOR (26-JUN-1972)
MIL-D-81641 - MIL-D-81641 (NOTICE 2), MILITARY SPECIFICATION: DISPLAY, HEAD-UP, GENERAL SPECIFICATION FOR (09-OCT-1996)
MIL-D-81641 - MIL-D-81641 (NOTICE 1), MILITARY SPECIFICATION: DISPLAY, HEAD-UP, GENERAL SPECIFICATION FOR (17-OCT-1991)
MIL-D-87213 - MIL-D-87213 (NOTICE 1), MILITARY SPECIFICATION: ELECTRONICALLY GENERATED AIRBORNE DISPLAYS (08 JUN 1988) [S/S BY AFGS-87213B (CONTROLLED DISTRIBUTION)]
MIL-DTL-5421 C - MIL-DTL-5421C, DETAIL SPECIFICATION: TUBES, PITOT, ELECTRICALLY HEATED, AIRCRAFT (13 JUL 2007) [SUPERSEDING MIL-T-5421B]
MIL-DTL-5421 D - MIL-DTL-5421D, DETAIL SPECIFICATION: TUBES, PITOT, ELECTRICALLY HEATED, AIRCRAFT (05 APR 2011) [SUPERSEDING MIL-T-5421B]
MIL-DTL-7627 G - MIL-DTL-7627G, DETAIL SPECIFICATION: INDICATOR, TURN AND SLIP, 28V DC (24 AUG 2010) [SUPERSEDING MIL-I-7627F]
MIL-DTL-9490 E - MIL-DTL-9490E, DETAIL SPECIFICATION: FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR (22 APR 200
MIL-F-9490 - MIL-F-9490D (NOTICE 1), MILITARY SPECIFICATION: FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT GENERAL SPECIFICATION FOR (05 OCT 1992) [S/S BY MIL-DTL-9490E]
MIL-F-9490 D - MIL-F-9490D, MILITARY SPECIFICATION: FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT GENERAL SPECIFICATION FOR (06 JUN 1975
MIL-F-9490 D - MIL-F-9490D (NOTICE 2), MILITARY SPECIFICATION: FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT GENERAL SPECIFICATION FOR (05 SEP 2007) [S/S BY MIL-DTL-9490E]
MIL-F-87242 - MIL-F-87242 (NOTICE 1), MILITARY SPECIFICATION: FLIGHT CONTROL SYSTEM GENERAL SPECIFICATION FOR (30 AUG 1991) [S/S BY AFGS-87242]
MIL-HDBK-2084 - MIL-HDBK-2084, DEPARTMENT OF DEFENSE HANDBOOK: MAINTAINABILITY OF AVIONICS AND ELECTRONIC SYSTEMS AND EQUIPMENT (31-JUL-1995) [SUPERSEDES MIL-STD-2084]
MIL-I-5133 C - MIL-I-5133C, MILITARY SPECIFICATION: INDICATOR, ATTITUDE, TYPE J-8 (05-AUG-1968) [NO S/S DOCUMENT]
MIL-I-5133 C - MIL-I-5133C (NOTICE-1), MILITARY SPECIFICATION: INDICATOR, ATTITUDE, TYPE J-8 (10-MAR-1993) [NO S/S DOCUMENT]
MIL-I-5356 A - MIL-I-5356A, MILITARY SPECIFICATION: INDICATOR, AIRSPEED, PITOT STATIC, TYPE L-7A (06-JUN-1950) [NO S/S DOCUMENT]
MIL-I-5356 A - MIL-I-5356A (NOTICE-1), MILITARY SPECIFICATION: INDICATOR, AIRSPEED, PITOT STATIC, TYPE L-7A (19-AUG-1988) [NO S/S DOCUMENT]
MIL-I-5356 A - MIL-I-5356A (AMENDMENT-1), MILITARY SPECIFICATION: INDICATOR, AIRSPEED, PITOT STATIC, TYPE L-7A (29-JUN-1983) [NO S/S DOCUMENT]
MIL-I-5392 A - MIL-I-5392A, MILITARY SPECIFICATION: INDICATOR, AIRSPEED, PITOT STATIC, TYPE K-3 (14-DEC-1956) [NO S/S DOCUMENT]
MIL-I-5392 A - MIL-I-5392A (AMENDMENT-3), MILITARY SPECIFICATION: INDICATOR, AIRSPEED, PITOT STATIC, TYPE K-3 (09-FEB-1984) [NO S/S DOCUMENT]
MIL-I-5419 B - MIL-I-5419B, MILITARY SPECIFICATION: INDICATOR, INDICATED AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED, 50-650 KNOTS (27-FEB-1969)
MIL-I-5419 B - MIL-I-5419B (NOTICE-2), MILITARY SPECIFICATION: INDICATOR, INDICATED AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED, 50-650 KNOTS (04-SEP-1996)
MIL-I-5419 B - MIL-I-5419B (NOTICE-1), MILITARY SPECIFICATION: INDICATOR, INDICATED AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED, 50-650 KNOTS (07-DEC-1987)
MIL-I-6115 A - MIL-I-6115A, MILITARY SPECIFICATION: INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF (29-MAR-1951)
MIL-I-6115 A - MIL-I-6115A (AMENDMENT-4), MILITARY SPECIFICATION: INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF(15-DEC-1999)
MIL-I-6115 A - MIL-I-6115A (NOTICE-1), MILITARY SPECIFICATION: INSTRUMENT SYSTEMS, PITOT TUBE AND FLUSH STATIC PORT OPERATED, INSTALLATION OF (01-JUN-2016)
MIL-I-7028 - MIL-I-7028, MILITARY SPECIFICATION: INSTRUMENT AND INSTRUMENT BOARDS, AIRCRAFT, INSTALLATION OF (11-OCT-1950) [NO S/S DOCUMENT]
MIL-I-7028 - MIL-I-7028 (AMENDMENT 1), MILITARY SPECIFICATION: INSTRUMENT AND INSTRUMENT BOARDS, AIRCRAFT, INSTALLATION OF (08-NOV-1951) [NO S/S DOCUMENT]
MIL-I-7028 - MIL-I-7028 (NOTICE 2), MILITARY SPECIFICATION: INSTRUMENT AND INSTRUMENT BOARDS, AIRCRAFT, INSTALLATION OF (18-SEP-1996) [NO S/S DOCUMENT]
MIL-I-7627 E - MIL-I-7627E, MILITARY SPECIFICATION: INDICATOR, TURN AND SLIP, 28V DC (04 APR 1974) [S/S BY MIL-DTL-7627G]
MIL-I-7627 E - MIL-I-7627E (AMENDMENT 1), MILITARY SPECIFICATION: INDICATOR, TURN AND SLIP, 28V DC (06 OCT 1986) [S/S BY MIL-DTL-7627G]
MIL-I-7627 F - MIL-I-7627F, MILITARY SPECIFICATION: INDICATOR, TURN AND SLIP, 28V DC (15 NOV 1994) [S/S BY MIL-DTL-7627G]
MIL-I-7627 F - MIL-I-7627F (NOTICE 1), MILITARY SPECIFICATION: INDICATOR, TURN AND SLIP, 28V DC (01 APR 1996) [S/S BY MIL-DTL-7627G]
MIL-I-18804 B - MIL-I-18804B, MILITARY SPECIFICATION: INDICATOR, VERTICAL SPEED, 0-6000 FPM, 2-INCH (22-JUN-1964)
MIL-I-18804 B - MIL-I-18804B (AMENDMENT-1), MILITARY SPECIFICATION: INDICATOR, VERTICAL SPEED, 0-6000 FPM, 2-INCH (14-JUN-1967)
MIL-I-18856 B - MIL-I-18856B (AMENDMENT-1), MILITARY SPECIFICATION: INDICATOR, ANGLE OF ATTACK, 28VDC MS28062 AND MS28067 (04-DEC-1987)
MIL-I-18856 B - MIL-I-18856B (NOTICE-1), MILITARY SPECIFICATION: INDICATOR, ANGLE OF ATTACK, 28VDC MS28062 AND MS28067 (30-AUG-1999)
MIL-I-18856 B - MIL-I-18856B, MILITARY SPECIFICATION: INDICATOR, ANGLE OF ATTACK, 28VDC MS28062 AND MS28067 (27-OCT-1969)
MIL-I-25355 B - MIL-I-25355B, MILITARY SPECIFICATION: INDICATOR, INSTRUMENT LANDING, AIRPORT RUNWAY (01-JUN-1993)
MIL-I-25355 B - MIL-I-25355B (NOTICE-3), MILITARY SPECIFICATION: INDICATOR, INSTRUMENT LANDING, AIRPORT RUNWAY (01-MAY-2014)
MIL-I-25355 B - MIL-I-25355B (NOTICE-2), MILITARY SPECIFICATION: INDICATOR, INSTRUMENT LANDING, AIRPORT RUNWAY (05-NOV-2008)
MIL-I-25355 B - MIL-I-25355B (NOTICE-1), MILITARY SPECIFICATION: INDICATOR, INSTRUMENT LANDING, AIRPORT RUNWAY (01-JAN-1996)
MIL-I-27197 C - MIL-I-27197C, MILITARY SPECIFICATION: INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED (31-DEC-1985) [S/S BY MIL-PRF-27197D]
MIL-I-27197 C - MIL-I-27197C (AMENDMENT-2), MILITARY SPECIFICATION: INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED (15-OCT-1994) [S/S BY MIL-PRF-27197D]
MIL-M-6756 - MIL-M-6756 (NOTICE-1), MILITARY SPECIFICATION: MEASURING AND LEVELING PROVISIONS (FOR AIRCRAFT) (15-JUL-1980) [S/S BY MIL-W-25140B]. Cancelled and superseded by MIL-W-25140]
MIL-O-87243 - MIL-O-87243, MILITARY SPECIFICATION: OFFENSIVE AVIONICS (30 MAY 1986) [NO S/S DOCUMENT]
MIL-O-87243 - MIL-O-87243 (NOTICE 1), MILITARY SPECIFICATION: OFFENSIVE AVIONICS (30 MAY 1986) [NO S/S DOCUMENT]
MIL-O-87243 - MIL-O-87243 (NOTICE 2), MILITARY SPECIFICATION: OFFENSIVE AVIONICS (31 JUL 1996) [NO S/S DOCUMENT]
MIL-I-5133 C - MIL-I-5133C (AMENDMENT-2), MILITARY SPECIFICATION: INDICATOR, ATTITUDE, TYPE J-8 (06-JUN-1986) [NO S/S DOCUMENT]
MIL-P-26292 C - MIL-P-26292C, MILITARY SPECIFICATION: PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (03-DEC-1969) [NO S/S DOCUMENT]
MIL-P-26292 C - MIL-P-26292C (AMENDMENT-3), MILITARY SPECIFICATION: PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (15-JUN-1972) [NO S/S DOCUMENT]
MIL-P-26292 C - MIL-P-26292C (NOTICE-1), MILITARY SPECIFICATION: PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (04-MAY-1998) [NO S/S DOCUMENT]
MIL-P-26292 C - MIL-P-26292C (NOTICE-2), MILITARY SPECIFICATION: PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (04-MAY-1998) [NO S/S DOCUMENT]
MIL-P-83207B (NOTICE-1), MILITARY SPECIFICATION: B - MIL-P-83207B (NOTICE-1), MILITARY SPECIFICATION: PITOT- STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR (28-AUG-1987) [CANCELLED W/ NO S/S DOCUMENT]
MIL-PRF-27197 D - MIL-PRF-27197D, PERFORMANCE SPECIFICATION: INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED (24-NOV-1997) [SUPERSEDING MIL-I-27197C]
MIL-PRF-27197 D - MIL-PRF-27197D (AMENDMENT-1), PERFORMANCE SPECIFICATION: INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED (17-DEC-1998) [SUPERSEDING MIL-I-27197C]
MIL-PRF-27197 E - MIL-PRF-27197E, PERFORMANCE SPECIFICATION: INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED (11-JUN-2012)
MIL-PRF-83419 D - MIL-PRF-83419D, PERFORMANCE SPECIFICATION" ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY (12-MAR-2008) [SUPERSEDING MIL-A-83419C]
MIL-PRF-83419 E - MIL-PRF-83419E, PERFORMANCE SPECIFICATION" ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY (12-MAR-2008)
MIL-S-23535 - MIL-S-23535, MILITARY SPECIFICATION, SYSTEM, INTEGRATED FLIGHT INSTRUMENTATION (01-APR-1963)
MIL-S-23535 - MIL-S-23535 (NOTICE-1), MILITARY SPECIFICATION, SYSTEM, INTEGRATED FLIGHT INSTRUMENTATION (09-OCT-1996)
MIL-STD-843 - MIL-STD-843, MILITARY STANDARD: ALTIMETER, PRESSURE, GENERAL TEST REQUIREMENT FOR (01 APR 1965) [NO S/S DOCUMENT]
MIL-STD-843 - MIL-STD-843 (NOTICE 4), MILITARY STANDARD: ALTIMETER, PRESSURE, GENERAL TEST REQUIREMENT FOR (12 NOV 1987) [NO S/S DOCUMENT]
MIL-STD-884 C - MIL-STD-884C (NOTICE 2), MILITARY STANDARD: ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (01 DEC 1993) [NO S/S DOCUMENT]
MIL-STD-884 C - MIL-STD-884C, MILITARY STANDARD: ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (25 APR 1975) [NO S/S DOCUMENT]
MIL-STD-884 C - MIL-STD-884C (NOTICE 1), MILITARY STANDARD: ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (05 NOV 1988) [NO S/S DOCUMENT]
MIL-STD-1293 - MIL-STD-1293 (NOTICE 1), MILITARY STANDARD: ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT (16 APR 1986) [NO S/S DOCUMENT]
MIL-STD-1293 - MIL-STD-1293 (NOTICE 2), MILITARY STANDARD: ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT (05 DEC 1995) [NO S/S DOCUMENT]
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