|
FAA AC 27-1 : 2008
|
CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
|
|
MIL-PRF-7958 Revision D:2013
|
PUSH-PULL CONTROLS, FLEXIBLE AND RIGID
|
|
NAS538 : 2003
|
BUSHING, FLANGED, PRESS FIT, UNDERSIZE INSIDE DIAMETER
|
|
MIL-F-8785 Revision C:1980
|
FLYING QUALITIES OF PILOTED AIRPLANES
|
|
AN665 Revision 6:2011
|
TERMINAL - THREADED CLEVIS TYPE TIE ROD
|
|
NAS1149:2014
|
WASHER, FLAT
|
|
NAS623:2012
|
SCREW, SHEAR, PAN HEAD, ALLOY STEEL, CRUCIFORM RECESS, SHORT THREAD, 95 KSI FSU
|
|
NAS620:2013
|
WASHER, FLAT, REDUCED OUTSIDE DIAMETER
|
|
MIL-DTL-83420 Revision P:2017
|
WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR
|
|
SAE AS 21152D : 2008
|
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, HOLLOW SHANK, SELF-ALIGNING, AIRFRAME, TYPE 3, -65 TO 300 DEGREES F
|
|
MIL-B-8584 Revision C:1970
|
BRAKE SYSTEMS, WHEEL, AIRCRAFT, DESIGN OF
|
|
MS21256 Revision G:2003
|
CLIP, LOCKING, TURNBUCKLE
|
|
MS21259 Revision K:2011
|
TERMINAL, WIRE ROPE, SWAGING, STUD, LONG THREAD
|
|
NAS1368:2014
|
GROMMET, PLASTIC FLIP TYPE
|
|
NASM21042:1998
|
NUT, SELF-LOCKING, 450 DEGREES F, REDUCED HEXAGON, REDUCED HEIGHT, RING BASE, NON-CORROSION RESISTANT STEEL
|
|
SAE AS 21151 : 2009
|
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, EXTERNAL THREAD, SELF-ALIGNING, AIRFRAME, TYPE 2, -65 TO 300 DEGREES F
|
|
SAE AS 21150 : 2009
|
BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, SOLID SHANK, SELF-ALIGNING, AIRFRAME, TYPE 1, -65 TO 300 DEGREES F
|
|
MIL-DTL-5541 Revision F:2006
|
Chemical Conversion Coatings on Aluminum and Aluminum Alloys
|
|
MIL-STD-464 Revision C:2010
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
|
|
MIL-DTL-6117 Revision L:2008
|
WIRE ROPE ASSEMBLIES, AVIATION, SWAGED TYPE
|
|
NAS537 : 2003
|
BUSHING, SLEEVE, PRESS FIT, UNDERSIZE INSIDE DIAMETER
|
|
NAS1193:2016
|
LOCKING DEVICE, POSITIVE INDEX
|
|
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
|
|
MIL-STD-203 Revision G:1991
|
AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT
|
|
FAA AC 23.1309-1 : 2011
|
SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
|
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
|
|
FAA AC 29-2 : 2008
|
CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
|
|
MIL-STD-1472 Revision G:2012
|
HUMAN ENGINEERING
|
|
FAA AC 25.1309-1 : 0
|
SYSTEM DESIGN AND ANALYSIS
|
|
MIL-DTL-5688 Revision E:2001
|
WIRE ROPE ASSEMBLIES; AIRCRAFT, PROOF TESTING AND PRESTRETCHING OF
|
|
MIL-PRF-16173 Revision E:1993
|
CORROSION PREVENTATIVE COMPOUND, SOLVENT CUTBACK, COLD-APPLICATION
|
|
NAS 559 : 2003
|
LOCK - ROD END (KEY TYPE)
|
|
NAS513:2015
|
WASHER, ROD END, LOCKING
|
|
JSSG-2006 Base Document:1998
|
JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
|
|
MS21251 Revision M:2002
|
TURNBUCKLE BODY, CLIP LOCKING
|
|
MIL-DTL-87218 Revision E:2012
|
Cable, Lockclad, for Aircraft Control
|
|
NAS428:2014
|
BOLT, MACHINE, CROWNED HEXAGON HEAD, ADJUSTING
|
|
NASM 21209 : 2003
|
INSERT, SCREW THREAD, COARSE AND FINE, SCREW LOCKING, HELICAL COIL, CRES
|
|
NAS509:2014
|
NUT, JAM, DRILLED AND UNDRILLED
|
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