Standard
Alloy Sheet and Strip, Corrosion and Heat Resistant Cobalt Base 25.5cr 20ni 4mo 2w 2(Cb+Ta)
2002-12-16
CURRENT
AMS5535
Search Results
Standard
Magnesium Alloy Sheet Aluminum Zinc (Hard)
2002-12-16
CURRENT
AMS4381
Standard
STEEL, NITRIDING .65 Ni 1 Cr 1 Mo
1946-04-01
HISTORICAL
AMS6480
Standard
STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)
1942-06-01
HISTORICAL
AMS6510
Standard
STEEL Nickel Molybdenum
1939-12-04
HISTORICAL
AMS6315
Standard
STEEL Nickel Molybdenum
1942-03-01
HISTORICAL
AMS6315A
Standard
STEEL 1.8 Ni - .25 Mo (.38 - .43C) Heat Treated (105,000 TS)
1945-07-01
HISTORICAL
AMS6315B
Standard
Alloy, Corrosion and Heat Resistant 37ni 20co 18cr 3mo 2.9ti
1949-01-01
CURRENT
AMS5760
Parts, such as bolts, turbine wheels, discs, buckets, and blades, for high strength and oxidation resistance up to 1500 F when suitably heat treated.
Standard
STEEL COTTER PINS, GALVANIZED Low Carbon
1942-12-01
CURRENT
AMS7212
Standard
BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
1973-05-15
HISTORICAL
AMS7461B
This specification covers premium quality bolts and screws made of 6Al - 4V titanium alloy.
Standard
BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
1970-11-01
HISTORICAL
AMS7461A
Standard
BOLTS AND SCREWS, TITANIUM ALLOY 6Al - 4V Upset Headed, Heat Treated, Roll Threaded
1964-06-30
HISTORICAL
AMS7461
Standard
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
1994-09-01
MAM2203B
Standard
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
1994-04-01
MAM2203A
This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard
TOLERANCES, METRIC Aluminum Alloy Drawn Tubing
2002-07-23
MAM2203
This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
Standard
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
2000-05-01
HISTORICAL
MAM5598B
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.
Standard
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
1993-07-01
HISTORICAL
MAM5598A
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.
Standard
ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
1991-10-01
HISTORICAL
MAM5598
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5598 is the equivalent, specified in inch/pound units, of this MAM.
Standard
FIBER OPTIC TRAINING REQUIREMENTS
2019-01-10
CURRENT
ARINC807-4
This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education. ARINC Report 807: Fiber Optic Training Requirements is a subset of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics.
Standard
Training Program Guidelines for Deicing/Anti-Icing of Aircraft on Ground-Digital Annex
2019-09-11
CURRENT
ARP5149CDA
This Digital Annex (DA) contains the current, full-PDF version of ARP5149B, Training Program Guidelines for Deicing/Anti-Icing of Aircraft on Ground, as well as .jpeg format files of Appendix D, Application Guidelines Configuration, Critical Component, and Spray Area Diagrams for Aircraft. The .jpeg diagram files may be used by purchasers in accordance with the terms of the included license agreement.
