MS33588 Revision E:1984
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Nuts, Self-Locking, Aircraft, Reliability and Maintainability Usage Requirements for (S/Sby NASM33588)
Available format(s)
PDF
Published date
28-12-1984
Publisher
Superseded date
04-11-1999
$31.16
Including GST where applicable
| DevelopmentNote |
Supersedes AND10068 (10/2001)
|
| DocumentType |
Standard
|
| Pages |
4
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| Supersedes |
| JSGS-87231 Revision A:1995 | Engines, Aircraft, Turbine (S/S by JSSG-2007) |
| MIL-S-38399 Revision A:1975 | Starter, Pneumatic, Aircraft Engine General Specification For (No S/S Document) |
| MIL-C-8605 Revision B:1990 | Cap; Pressure Fuel Servicing |
| MIL-V-81356 Revision B:1992 | Valve, Fuel System Pressurization And Vent |
| MS21077 Revision H:1994 | NUT, SELF-LOCKING, PLATE, TWO LUG, FLOATING, NON-METALLIC INSERT, STEEL, 125 KSI FTU, 250 DEG. F (S/S BY NASM21077) |
| MIL-C-19179 Revision B:1963 | Coupling Assembly, Quick-Disconnect, Fuel (S/S by MIL-C-24788) |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-N-85730 Base Document:1988 | NUT, SELF-LOCKING, SPLINE DRIVE, ASSEMBLED WASHER, NICKEL ALLOY 718, 220 KSI FTU, 900 DEGREES F, GENERAL SPECIFICATION FOR |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-V-25023 Revision B:1967 | Valve, Fuel Drain, Self-Locking |
| MIL-A-19736 Revision A:1960 | Air Refueling Systems, General Specification for |
| MIL-I-23870 Base Document:1963 | Indicator, Fuel Rate of Flow, 0 to 15 GPM (No S/S Document) |
| MIL-C-38373 Revision B:1975 | Cap, Fluid Tank Filler (No S/S Document) |
| MIL-S-8710 Revision B:1969 | Strainer, Airframe Fuel System, General Specification for |
| MIL-A-6425 Revision B:1959 | Adapter, Pressure Fuel Servicing, Aircraft, General Specification for (S/S by MIL-A-25896) |
| MIL-V-8610 Revision B:1984 | Valve, Fuel Shutoff Solenoid Operated, 28 Volt DC |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| MIL-A-25896 Revision E:1983 | Adapter, Pressure Fuel Servicing, Nominal 2.5-Inch Diameter |
| MIL-D-8181 Revision B:1965 | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification for (S/S by SAE-AS8181) |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL-N-85729 Base Document:1988 | NUT, SELF-LOCKING, A-286, 160 KSI FTU, 450 DEGREES F, GENERAL SPECIFICATION FOR |
| MIL-S-21277 Revision A:1958 | SWITCHES, LIQUID LEVEL, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-S-7470 Revision A:1975 | Shaft, Power Transmission, Aircraft Accessory, General Specification For |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
Summarise
$31.16
Including GST where applicable
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.