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 TIA-222
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A-A-53825/2 1989 Edition, June 15, 1989
FORCEPS, TOOTH EXTRACTING, NO. 222
Includes all amendments and changes through Cancellation Notice 1, October 1, 2008

A-A-53825/2

1989 Edition, June 15, 1989

Complete Document
 
FORCEPS, TOOTH EXTRACTING, NO. 222
Includes all amendments and changes through Cancellation Notice 1, October 1, 2008
Additional Comments:
CNCL NO S/S
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AASHTO T 222 81st Edition, 1981
Standard Method of Test for Nonrepetitive Static Plate Load Test of Soils and Flexible Pavement Components for Use in Evaluation and Design of Airport and Highway Pavements
Includes all amendments and changes through Reapproval Notice , 2017

AASHTO T 222

81st Edition, 1981

Complete Document
 
Standard Method of Test for Nonrepetitive Static Plate Load Test of Soils and Flexible Pavement Components for Use in Evaluation and Design of Airport and Highway Pavements
Includes all amendments and changes through Reapproval Notice , 2017
Additional Comments:
ONLY AVAILABLE IN ELECTRONIC FORMAT
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AASHTO TIA 16 1st Edition, 2002
Transportation Invest in America; Tea-21 Reauthorization Recommendations

AASHTO TIA 16

1st Edition, 2002

Complete Document
 
Transportation Invest in America; Tea-21 Reauthorization Recommendations
Additional Comments:
AVAILABLE ELECTRONIC FORMAT ONLY
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ABMA STD 22.2 88th Edition, 2010
Spherical Plain Radial Bearings, Joint Type Inch Design
Includes all amendments and changes through Stabilization Notice (No longer revised / updated) , 2010

ABMA STD 22.2

88th Edition, 2010

Complete Document
 
Spherical Plain Radial Bearings, Joint Type Inch Design
Includes all amendments and changes through Stabilization Notice (No longer revised / updated) , 2010
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ACI 222.1 1996 Edition, 1996
Provisional Standard Test Method for Water-Soluble Chloride Available for Corrosion of Embedded Steel in Mortar and Concrete Using the Soxhlet Extractor

ACI 222.1

1996 Edition, 1996

Complete Document
 
Provisional Standard Test Method for Water-Soluble Chloride Available for Corrosion of Embedded Steel in Mortar and Concrete Using the Soxhlet Extractor
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EN
Additional Comments:
W/D NO S/S
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ACI 222.2R 2014 Edition, October 2014
Report on Corrosion of Prestressing Steels

ACI 222.2R

2014 Edition, October 2014

Complete Document
 
Report on Corrosion of Prestressing Steels
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EN
Additional Comments:
AVAILABLE ELECTRONICALLY ONLY
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ACI 222.3R 2011 Edition, April 2011
Guide to Design and Construction Practices to Mitigate Corrosion of Reinforcement in Concrete Structures

ACI 222.3R

2011 Edition, April 2011

Complete Document
 
Guide to Design and Construction Practices to Mitigate Corrosion of Reinforcement in Concrete Structures
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ACI 222R 2001 Edition, 2001
Protection of Metals in Concrete Against Corrosion
Includes all amendments and changes through Reapproval Notice , 2010

ACI 222R

2001 Edition, 2001

Complete Document
 
Protection of Metals in Concrete Against Corrosion
Includes all amendments and changes through Reapproval Notice , 2010
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EN
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AVAILABLE ELECTRONICALLY ONLY
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ACI SP-222 2004 Edition, May 2004
Recent Advances in Concrete Technology

ACI SP-222

2004 Edition, May 2004

Complete Document
 
Recent Advances in Concrete Technology
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ACI SP-291 CD 2013 Edition, 2013
Corrosion of Reinforcing Steel in Concrete - Future Direction: Proceedings-Hope & Schupack Corrosion Symposium CD

ACI SP-291 CD

2013 Edition, 2013

Complete Document
 
Corrosion of Reinforcing Steel in Concrete - Future Direction: Proceedings-Hope & Schupack Corrosion Symposium CD
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ACI SP-308 2016 Edition, June 2016
Chloride Thresholds and Limits for New Construction

ACI SP-308

2016 Edition, June 2016

Complete Document
 
Chloride Thresholds and Limits for New Construction
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EN
Additional Comments:
AVAILABLE IN PDF ONLY - SEND CUSTOMER DIRECT
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AD 00-04-15 March 14, 2000
PREVENT FATIGUE FAILURE OF A DRIVE PIN\BELL HELICPTR TEXTRON\222B\222U\222\230

AD 00-04-15

March 14, 2000

Complete Document
 
PREVENT FATIGUE FAILURE OF A DRIVE PIN\BELL HELICPTR TEXTRON\222B\222U\222\230
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AD 00-10-14 June 26, 2000
PREVENT THE FRACTURE OF A FLAPPING BEARING TO YOKE ATTACHMENT BOLT (BOLT), FAILURE OF THE BEARING AND YOKE INTERFACE, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON\222B\222U\222\230

AD 00-10-14

June 26, 2000

Complete Document
 
PREVENT THE FRACTURE OF A FLAPPING BEARING TO YOKE ATTACHMENT BOLT (BOLT), FAILURE OF THE BEARING AND YOKE INTERFACE, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON\222B\222U\222\230
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AD 00-NM-104 June 12, 2000
PREVENT A SUDDEN CHANGE IN PITCH DUE TO AN OUT-OF-TRIM CONDITION COMBINED WITH AN AUTOPILOT DISCONNECT\AIRBUS INDUSTRIE\A300-B2-203\A300-B4-203\A300-600\A300-600R\A310-200\A310-200ADV\A310-221\A310-22 2\A310-300\A310-322\A310-324\A310-325

AD 00-NM-104

June 12, 2000

Complete Document
 
PREVENT A SUDDEN CHANGE IN PITCH DUE TO AN OUT-OF-TRIM CONDITION COMBINED WITH AN AUTOPILOT DISCONNECT\AIRBUS INDUSTRIE\A300-B2-203\A300-B4-203\A300-600\A300-600R\A310-200\A310-200ADV\A 310-221\A310-222\A310-300\A310-322\A310-324\A310-325
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AD 00-NM-214 October 25, 2000
PREVENT REDUCED STRUCTURAL INTEGRITY OF THE AIRPLANE DUE TO FATIGUE DAMAGE AND CONSEQUENT CRACKING OF THE PICK-UP ANGLES AT FRAME 40\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325

AD 00-NM-214

October 25, 2000

Complete Document
 
PREVENT REDUCED STRUCTURAL INTEGRITY OF THE AIRPLANE DUE TO FATIGUE DAMAGE AND CONSEQUENT CRACKING OF THE PICK-UP ANGLES AT FRAME 40\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324 \A310-325
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AD 00-NM-222 December 21, 2000
PREVENT LOSS OF THE NOSE WHEEL STEERING AND REDUCED CONTROLLABILITY OF THE AIRPLANE ON THE GROUND\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES

AD 00-NM-222

December 21, 2000

Complete Document
 
PREVENT LOSS OF THE NOSE WHEEL STEERING AND REDUCED CONTROLLABILITY OF THE AIRPLANE ON THE GROUND\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES
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AD 00-NM-223 January 9, 2001
DETECT AND CORRECT FATIGUE CRACKING OF FUSELAGE FRAME 07 IN THE UPPER FRAME SECTION ASSEMBLY OF THE LATERAL COCKPIT WINDOWS\AIRBUS INDUSTRIE\A300-B4-620\A310-203\A310-221\A310-222

AD 00-NM-223

January 9, 2001

Complete Document
 
DETECT AND CORRECT FATIGUE CRACKING OF FUSELAGE FRAME 07 IN THE UPPER FRAME SECTION ASSEMBLY OF THE LATERAL COCKPIT WINDOWS\AIRBUS INDUSTRIE\A300-B4-620\A310-203\A310-221\A310-222
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AD 00-NM-48 August 2, 2000
PREVENT THE FIRE WARNING FROM TERMINATING PREMATURELY\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300- 600

AD 00-NM-48

August 2, 2000

Complete Document
 
PREVENT THE FIRE WARNING FROM TERMINATING PREMATURELY\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324 \A310-325\A300-600
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AD 00-NM-77 April 19, 2000
PREVENT FRACTURE OF THE LEAD SCREW OF THE POSITION 1 FLAP SCREW JACK\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325

AD 00-NM-77

April 19, 2000

Complete Document
 
PREVENT FRACTURE OF THE LEAD SCREW OF THE POSITION 1 FLAP SCREW JACK\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324 \A310-325
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AD 01-01-51-E January 5, 2001
LETTER AD 2001-01-51 PREVENT FAILURE OF THE SUPPORT AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON\222\222B\222U\230\430

AD 01-01-51-E

January 5, 2001

Complete Document
 
LETTER AD 2001-01-51 PREVENT FAILURE OF THE SUPPORT AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON\222\222B\222U\230\430
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