What is AIRLOCK INC's OSHA violation history?

AIRLOCK INC has 1 OSHA inspection on record with 7 violations and $300 in total penalties.

Establishment profile

AIRLOCK INC

108 GULF ST, Milford, CT, 06460

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OSHA inspections

over 45 years

Violations

$300 in penalties

Penalties

$300

$43 avg

Summary

AIRLOCK INC has accumulated 7 OSHA violations across 1 inspection over 45 years of recorded history, with $300 in total assessed penalties.

The establishment sits in the 77th percentile for violations within its industry-state peer group of 25,052 employers. The most recent enforcement activity was recorded 45 years ago.

Federal records were found in 1 of 15 sources. Sources without matching records returned empty for this establishment.

Agency coverage

AIRLOCK INC appears in OSHA workplace safety record only. No matching records were found in WHD wage enforcement, MSHA mine safety, EPA environmental compliance, NLRB labor relations, OFLC visa and labor certification, FMCSA motor carrier registration, SAM.gov federal debarment, CMS nursing home enforcement, UVA Corporate Prosecution Registry, CPSC product recalls, or NHTSA vehicle recalls. Single-agency enforcement records typically indicate either a discrete incident-based inspection or a low-risk operational profile.

OSHA workplace safety

Inspections

0.0 / yr · last 45 yrs

Violations

0.2 / yr

Penalties

$300

$43 avg / violation

29% serious71% other

Inspection trigger · planned

1 of 1

100% of inspections at this establishment produced violations,

Peer comparison

77th

Above average violations. Peer group: 25,052 employers. This establishment has 7 OSHA violations; peer median is 2.

Fewer violationsMore violations

Penalty percentile

65th

peer median: $0

Inspection frequency

0th

peer median: 1

Safety self-report (OSHA 300A)

No self-reported injury rates filed with OSHA's Injury Tracking Application for AIRLOCK INC. Verify directly with OSHA Injury Tracking Application →

Inspection breakdown

Planned

Complaint- and accident-triggered inspections are stronger risk signals than routine planned inspections.

OSHA severe injury reports

No severe injury reports (hospitalization, amputation, or loss of an eye) on file under 29 CFR 1904.39 for AIRLOCK INC. Verify directly with Occupational Safety and Health Administration →

Activity timeline

Data refreshed

Weekly

First OSHA inspection

—

Most recent activity

45 years ago

No federal enforcement activity has been recorded against this establishment in 45+ years. Most recent activity: 45 years ago. Data on this page is refreshed weekly.

Wage & Hour Division (WHD)

No WHD wage, overtime, or child-labor enforcement cases on file for AIRLOCK INC. Verify directly with Wage and Hour Division →

Mine safety (MSHA)

No MSHA mine safety violations on file for AIRLOCK INC. Verify directly with Mine Safety and Health Administration →

Labor relations (NLRB)

No NLRB unfair labor practice charges or union representation cases on file for AIRLOCK INC. Verify directly with National Labor Relations Board →

Visa & labor certification (OFLC)

No H-1B, H-2A, or H-2B labor condition applications on file for AIRLOCK INC. Verify directly with Office of Foreign Labor Certification →

Environmental compliance (EPA)

No EPA inspections or formal enforcement actions on file for AIRLOCK INC. Verify directly with Environmental Protection Agency →

Federal criminal prosecution record

No federal criminal prosecutions, plea agreements, or deferred-prosecution agreements on file for AIRLOCK INC. Verify directly with UVA Corporate Prosecution Registry →

Federal contracts

This location

Obligated (5-yr)

$529K

Obligated (all-time)

$15.6M

Awards

275

Top agency

National Aeronautics and Space Administration

$11.5M

Company-wide — DAVID CLARK CO INC (across 5 entities)

Obligated (5-yr)

$86.8M

Obligated (all-time)

$420.1M

Awards (all-time)

3,377

Consolidated across all USAspending recipient entities under this corporate parent — not attributable to this single location.

Top agencies by obligation (this location)

National Aeronautics and Space Administration$11.5M

Department of Defense$4.1M

Largest awards (top 50 of 275)

National Aeronautics and Space Administration
HELMET, NECK RING AND EXTRAVEHICULAR VISOR ASSEMBLY (EVVA)
contract · Last action 2024-06-27
$2,746,014
National Aeronautics and Space Administration
LARGE HUT ASSEMBLY
contract · Last action 2022-12-12
$1,665,203
National Aeronautics and Space Administration
OCSS SUIT HARDGOODS
contract · Last action 2021-11-16
$862,110
National Aeronautics and Space Administration
OCSS SUIT HARDGOODS
contract · Last action 2022-07-28
$737,130
National Aeronautics and Space Administration
FABRICATION FOR XLCVG CONNECTORS
contract · Last action 2020-02-10
$692,934
National Aeronautics and Space Administration
IGF::OT::IGF AIR-LOCK'S PHASE I EFFORT TESTED THE EFFECTS OF BALL INDUCED CONTACT STRESSES ON TITANIUM BEARING RACES. THE CONTACT STRESS DESIGN LIMIT THAT WOULD ACHIEVE A PLANETARY EXPLORATION SUITS REQUIRED CYCLE LIFE WAS DETERMINED. THESE TESTS WERE PERFORMED ON UNIFORMLY LOADED FLAT THRUST BEARING STYLE TEST PLATES. THE PHASE II EFFORT WILL TAKE THIS INFORMATION AND USE IT IN A REAL WORLD APPLICATION, EXISTING ADVANCED PLANETARY EXPLORATION SUITS BEARINGS. SPECIFICALLY FOCUSING ON THE Z-1 SERIES SUITS HIP AND WAIST, AND ALSO THE Z-2 SERIES HIP BEARINGS. THESE ARE AREAS THAT ARE KNOWN TO HAVE LARGE CONTACT STRESSES DUE TO NON-UNIFORM LOADING THROUGH AXIAL RESTRAINT LINES. THIS LOADING YIELDS INCREASED STRESSES IN DIFFERENT AREAS OF THE RACE. WITH AN UNDERSTANDING OF THE MAX EXPECTED STRESS, THE BEARING DESIGN CAN BE MADE TO ACCOMMODATE ALL CONTACT STRESSES APPLIED TO THE RACE. THE PHASE II EFFORT WILL CONSIST OF FINDING THE MAXIMUM EXPECTED CONTACT STRESSES IN THESE BEARINGS THROUGH BOTH TEST AND FEA SIMULATION. THE BEARING DESIGNS CAN THEN BE OPTIMIZED TO REDUCE THE CONTACT STRESSES IN THESE AREAS. AIR-LOCK WILL MANUFACTURE DVT UNITS IN ORDER TO CYCLE TEST THE OPTIMIZED BEARINGS. THE TASK WILL BE FINALIZED WITH THE DELIVERY OF OPTIMIZED BEARINGS CAPABLE OF BEING USED ON THE Z-1 SERIES AND Z-2 SERIES SUITS.
contract · Last action 2019-09-20
$675,004
National Aeronautics and Space Administration
FABRICATION FOR DVT WEDGE AND HUT VENTS OF THE EXPLORATION EXTRAVEHICULAR MOBILITY UNIT ASSEMBLY COMPONENTS
contract · Last action 2019-09-05
$578,140
National Aeronautics and Space Administration
Z 2.5 HARD UPPER TORSO (HUT) ASSEMBLY
contract · Last action 2018-11-15
$425,500
National Aeronautics and Space Administration
HARD UPPER TORSO (HUT) ASSEMBLY
contract · Last action 2020-03-12
$400,240
National Aeronautics and Space Administration
UMBILICAL INTERFACE CONNECTORS
contract · Last action 2021-12-14
$349,770
National Aeronautics and Space Administration
XEMU AUXILIARY THERMAL LOOP CONNECTOR (ATLC) MULTIPLE WATER CONNECTOR (MWC)
contract · Last action 2018-12-13
$249,980
National Aeronautics and Space Administration
XEMU EXPLORATION LIQUID COOLING AND VENTILATION GARMENT XLCVG CONNECTORS
contract · Last action 2021-06-21
$201,040
Department of Defense
8509984486!VALVE,PNEUMATIC INF
contract · Last action 2023-06-30
$193,806
National Aeronautics and Space Administration
XEMU HELMET FABRICATION
contract · Last action 2022-10-06
$184,800
Department of Defense
8507755248!VALVE,PNEUMATIC INF
contract · Last action 2021-12-07
$182,400
National Aeronautics and Space Administration
MK-III PROTOTYPE SPACE SUIT HARDWARE AND SPARES
contract · Last action 2011-12-06
$178,409
National Aeronautics and Space Administration
XEXTRAVEHICULAR MOBILITY UNIT (EMU) EXTRAVEHICULAR VISOR ASSEMBLY (EVVA)
contract · Last action 2018-01-19
$163,500
Department of Defense
4518332519!VALVE,PNEUMATIC INF
contract · Last action 2011-07-06
$149,500
Department of Defense
8501462424!VALVE,PNEUMATIC INF
contract · Last action 2014-10-24
$145,452
Department of Defense
4523844387!PV IRAQ
contract · Last action 2013-03-01
$143,900
Department of Defense
4521355322!BOA
contract · Last action 2012-05-21
$138,500
Department of Defense
4520539460!BOA
contract · Last action 2012-02-28
$138,500
Department of Defense
4520138891!BOA
contract · Last action 2012-01-17
$138,500
National Aeronautics and Space Administration
IGF::OT::IGF AS HUMAN SPACEFLIGHT ONCE AGAIN MOVES TOWARD PLANETARY EXPLORATION, SPACE SUIT HARDWARE MUST BE READY TO FACE THE HARSH ENVIRONMENTAL CONDITIONS OF THESE SURFACES. THIS IS ESPECIALLY TRUE FOR HIGH PRESSURE OXYGEN QUICK DISCONNECTS. THESE SYSTEMS ARE CRITICAL LIFE SUPPORT ITEMS THAT ENABLE THE FLOW OF BREATHING GAS, WATER, AND ELECTRICAL&COMMUNICATION SIGNALS FROM THE SUIT TO THE VEHICLE OR HABITAT. LUNAR AND MARTIAN DUST AND REGOLITH CAN HAVE A DETRIMENTAL EFFECT RANGING FROM AN ANNOYANCE DURING MATE&DEMATE, TO A SEVERE HAZARD THROUGH CONTAMINATION OF THE BREATHING GAS LINES. THE WORK PROPOSED IN THIS EFFORT WILL FOCUS ON DUST MITIGATION STRATEGIES THAT CAN BE USED IN A VARIETY OF HIGH PRESSURE OXYGEN QUICK DISCONNECTS. AS A TEST BED FOR THIS EFFORT, AIR-LOCK WILL FOCUS ON THE EXISTING CONNECTOR DESIGNS OF THE EMU SCU/DCM MULTIPLE CONNECTORS, AND THE CSSS T-HANDLE MULTIPLE CONNECTOR. HOWEVER, THE TASK WILL DETERMINE DUST MITIGATION STRATEGIES THAT WILL BE EXTENSIBLE TO ANY EXISTING OR FUTURE CONNECTOR DESIGN. THE FIRST STEP IN THIS PROCESS IS IDENTIFYING THE EFFECTS THAT DUST AND REGOLITH WILL HAVE. THE NEXT STEP WILL BE A MULTIFACETED APPROACH, WE WILL LOOK TO MITIGATE DUST THROUGH 1) MATERIAL AND COATING TECHNOLOGIES 2) MECHANICAL DESIGN FEATURES SUCH AS PURGES, WIPERS, AND DUST SEALS 3) CONNECTOR COVERING AND SHIELDING. AFTER A VARIETY OF DUST MITIGATION OPTIONS ARE DEVELOPED, THE THIRD STEP IN THIS PROCESS WILL BE IMPLEMENTATION OF THE STRATEGIES INTO THE CONNECTOR DESIGNS. THE FINAL STEP IN THIS PROCESS WILL BE TESTING OF THE STRATEGIES THROUGH SAMPLES AND MOCK-UPS IN A SIMULATED DIRTY ENVIRONMENT.
contract · Last action 2016-06-07
$124,821
National Aeronautics and Space Administration
IGF::OT::IGF IN RESPONSE TO NASA 2015 SBIR TOPIC H4.02, AIR-LOCK PROPOSES TO DEFINE THE MAXIMUM ALLOWABLE CONTACT STRESS FOR TITANIUM BEARINGS. THE MODULUS OF TITANIUM IS LOWER THAN LEGACY SPACESUIT BEARING MATERIALS (STAINLESS STEEL). DUE TO THIS, TITANIUM BEARINGS ARE MORE SUSCEPTIBLE TO DEFLECTION UNDER MAN AND PLUG LOAD SCENARIOS. BEARING DEFLECTION CAUSES A LIMITED NUMBER OF BALLS TO ABSORB THE FULL LOAD AND RESULTS IN HIGHER, LOCALIZED, CONTACT STRESSES. LOCALIZED CONTACT STRESS IS BELIEVED TO BE THE MAIN CONTRIBUTOR TO THE BEARING RACE DEGRADATION OBSERVED DURING NASA'S 2014 OXYGEN COMPATIBILITY TESTING. IN PHASE 1, WE WILL CORRELATE ANALYTICAL CONTACT STRESS DATA WITH SAMPLE BEARING TEST DATA. THIS CORRELATION WILL CHARACTERIZE BEARING WEAR AND DEGRADATION RELATIVE TO BALL CONTACT STRESS. MULTIPLE TEST ITERATIONS WILL BE PERFORMED TO CLEARLY IDENTIFY THE CONTACT STRESS THAT DEGRADES A TITANIUM RACE. WE WILL ALSO DETERMINE IF THERE ARE COMMERCIAL SURFACE TREATMENTS (COATINGS) THAT MAY ENHANCE TITANIUM WEAR RESISTANCE. AT THE CONCLUSION OF PHASE 1, WE SHALL HAVE IDENTIFIED THE MAXIMUM ALLOWABLE BEARING CONTACT STRESS. THIS DATA POINT WILL SERVE AS A VALUABLE DESIGN GUIDELINE FOR FUTURE BEARING DESIGNS AND SHOULD YIELD REDUCED CERTIFICATION AND DEVELOPMENT COSTS.
contract · Last action 2015-06-09
$124,085
National Aeronautics and Space Administration
NRE NON-RECURRING ENGINEERING CHARGES FOR MOBILE LTA ADAPTER ASSEMBLY
contract · Last action 2019-10-21
$122,620
National Aeronautics and Space Administration
OT - HUT, HATCH AND TEST SAMPLES
contract · Last action 2018-03-22
$119,060
National Aeronautics and Space Administration
IGF::OT::IGF THE CURRENT NASA SPACESUIT COMMUNITY IS FOCUSING ON UTILIZING A 13" HEMISPHERICAL HELMET FOR THE NEXT GENERATION OF EXTRAVEHICULAR ACTIVITY SPACESUITS. THIS HELMET ARCHITECTURE PRESENTS THE END USER WITH A MYRIAD OF POSITIVE ATTRIBUTES, INCLUDING A LARGE FIELD OF VIEW, ENHANCED CO2 WASHOUT AND IMPROVED COMPONENT DURABILITY/OPERATIONAL LIFE. THE 13" DOME HELMET ARCHITECTURE HAS PROVEN THESE ATTRIBUTES VIA THE NASA MK-III AND Z-1 ADVANCED EVA SPACESUIT TEST BEDS. AIR-LOCK'S 2012 SBIR PROPOSAL ADVANCES THE 13" DOME HELMET FROM NASA PROTOTYPE/TEST BED TO EVA ACCEPTABILITY FOR USE BY ENHANCING THE DESIGN WITH A FULLY FUNCTIONAL EXTRAVEHICULAR VISOR ASSEMBLY (EVVA). PHASE I WILL SEE AIR-LOCK ENGINEERS LEVERAGE CURRENT HELMET/EVVA TECHNOLOGIES, INFUSE THE DESIGN WITH LESSONS LEARNED FROM THE EMU PROGRAM AND IMPLEMENT THE RESULTANT DESIGN INTO A 13" HEMISPHERICAL HELMET ARCHITECTURE; HERETOFORE REFERRED TO AS THE ADVANCED EXTRAVEHICULAR HELMET ASSEMBLY (AEHA). IN ADDITION TO THE DESIGN FACET OF THE PHASE I TASK, AIR-LOCK ENGINEERS WILL DEVELOP A VERIFICATION AND VALIDATION TEST PLAN (V&V) BASED ON CURRENT EMU S/AD AND CARD REQUIREMENTS ALONG WITH HIGHER ADVANCED EVA OPERATING PRESSURES (8.0 PSI). THIS TEST PLAN WILL LAY THE FOUNDATION FOR PHASE 2 ACCEPTABILITY FOR USE TESTING TO FACILITATE THE USE OF THE AEHA ABOARD THE INTERNATIONAL SPACE STATION IN SUPPORT OF NASA'S PLANNED 2017 ISS ADVANCED SPACESUIT DEMONSTRATION TEST.
contract · Last action 2013-05-17
$117,809
Department of Defense
8511014111!VALVE,PNEUMATIC INF
contract · Last action 2024-11-20
$115,992
National Aeronautics and Space Administration
IGF::OT::IGF DESIGN&DEVELOP HELMET&EVA PROTOTYPE
contract · Last action 2017-06-02
$100,800
National Aeronautics and Space Administration
INTERCHANGEABLE BEARINGS FOR PROFILE AND WEIGHT TRADE STUDIES AIR-LOCK, INCORPORATED IS PROPOSING TO DESIGN FULLY SEALED SHOULDER AND ARM BEARINGS WITH INTERCHANGEABLE BEARING HOUSINGS. THE INTERCHANGEABLE HOUSINGS SHALL BE UTILIZED IN TRADE STUDIES TO DETERMINE THE OPTIMAL BEARING PROFILE AND WEIGHT RELATIVE TO THE SHOULDER AND ARM POSITION. IT IS ASSUMED THAT THE NEXT GENERATION OF NASA PRESSURE SUITS WILL REQUIRE THE CREWMEMBER TO UTILIZE THEIR SUIT IN BOTH THE PRESSURIZED AND UNPRESSURIZED MODE. HISTORIC, KEY DESIGN DRIVERS HAVE ALWAYS BEEN SUITED COMFORT IN THE UNPRESSURIZED MODE AND SUIT MOBILITY IN THE PRESSURIZED MODE. AS A MINIMUM, BEARINGS WILL BE NEEDED AT THE SHOULDER, BICEP, AND WRIST TO SATISFY PRESSURIZED MOBILITY REQUIREMENTS. TO PLACATE UNPRESSURIZED COMFORT, THE OPTIMAL BEARING DESIGN SHALL BE LIGHTWEIGHT AND LOW PROFILE; OFTEN CONFLICTING CHARACTERISTICS IN BEARING DESIGN. THIS SBIR PROPOSAL WILL PROVIDE NASA WITH A BEARING DESIGN THAT FACILITATES QUICK TRADE STUDIES TO DETERMINE THE OPTIMAL BEARING PROFILE AND WEIGHT.
contract · Last action 2009-01-15
$97,782
National Aeronautics and Space Administration
UNDER PHASE 1 OF SUBJECT SBIR, AIR-LOCK, INCORPORATED WILL DESIGN A SELF DONNING AND DOFFING REAR ENTRY HARD UPPER TORSO (REHUT) THAT INTERFACES WITH A SUIT PORT. THIS DESIGN WILL ALLOW SUITED, PRESSURIZED CREWMEMBERS TO MATE/DEMATE THEIR SUITS TO/FROM SUIT PORTS LOCATED ON LUNAR OR PLANETARY HABITATS, ROVERS, ETC. THIS IS A SIGNIFICANT ACTIVITY BECAUSE IT MINIMIZES CONCERNS OVER DUST ENTERING THE HABITAT DURING CREWMEMBER ENTRY/EXIT AND IT MAXIMIZES THE HABITAT'S WORKING VOLUME BY ELIMINATING THE NEED FOR AIRLOCKS. FOR THE PURPOSE OF THIS SBIR, THE BASELINE ARCHITECTURE BEING WILL FOCUS ON NASA JSC'S MK-III ADVANCED SPACESUIT AND THE SUIT PORT BEING UTILIZED BY THE LUNAR ELECTIRC ROVER (LER).
contract · Last action 2011-08-12
$97,633
National Aeronautics and Space Administration
ADVANCED CREW ESCAPE SUIT - ACES NECK RINGS AND WRIST DISCONNECTS
contract · Last action 2010-03-10
$95,800
Department of Defense
8503490942!VALVE,PNEUMATIC INF
contract · Last action 2016-08-02
$95,580
National Aeronautics and Space Administration
HARD UPPER TORSO SHOULDER JOINT DESIGN FOR CREW MEMBER SIZING ADJUSTMENT AND ENHANCED MOBILITY.
contract · Last action 2008-02-01
$93,703
Department of Defense
4523101204!VALVE,PNEUMATIC INF
contract · Last action 2012-12-04
$79,580
National Aeronautics and Space Administration
THE OBJECTIVES OF PHASE III ARE: 1. DESIGN, ANALYZE, MANUFACTURE, AND DELIVER A PAIR EACH OF MOBILITY BEARINGS FOR THE SCYE JOINT (SHOULDER) AND ARM JOINT (ELBOW) OF THE EXPLORATION EXTRAVEHICULAR MOBILITY UNIT (XEMU) ADVANCED SPACE SUIT. 2. EVALUATION OF THESE BEARINGS IN A RELEVANT TEST ENVIRONMENT (DUST MITIGATION). TO MEET THE STATED OBJECTIVES, AIR-LOCK WILL PERFORM THE FOLLOWING TASKS: 1. HOLD A KICK OFF MEETING WITH A REQUIREMENT DECOMPOSITION OF THE XEMU SCYE JOINT AND ARM JOINT TO GAIN A FULL UNDERSTANDING OF THE BEARING S NEEDS RELATIVE TO DIAMETER, HEIGHT, HOLE PATTERN, LOADING, RESTRAINT LINE ATTACHMENT, CYCLE LIFE, DUST MITIGATION, SOFT GOODS ATTACHMENT AND SEALING. 2. CREATE CAD MODELS OF BOTH BEARING ASSEMBLIES. 3. PERFORM FINITE ELEMENT ANALYSIS (FEA) USING THE PHASE II DEVELOPED METHODS TO EVALUATE CONTACT STRESSES AND ENSURE PROPER MARGIN OF DURABILITY; UPDATE CAD MODELS AS REQUIRED. 4. ADAPT AND INTEGRATE NASA S DUST MITIGATION TECHNOLOGIES INTO THE CAD MODELS (SEE FIGURE 2). 5. CREATE DETAILED DRAWING PACKAGES FOR THE XEMU ARM AND SCYE BEARING ASSEMBLIES. 6. CREATE A VERIFICATION TEST PLAN FOR THE XEMU ARM AND SCYE BEARING ASSEMBLIES. 7. HOLD A MANUFACTURING READINESS REVIEW (MRR) WITH NASA PRIOR TO BUILD 8. FABRICATE (2) EACH XEMU SCYE BEARING ASSEMBLY 9. FABRICATE (2) EACH XEMU ARM BEARING ASSEMBLY 10. PERFORM NON-DESTRUCTIVE TESTING ON BEARING ASSEMBLIES INCLUDING DUST TESTING. WITHIN THE SCOPE OF THIS EFFORT, VARIOUS DUST SEAL MATERIALS WILL BE EVALUATED. 11. PERFORM MAINTENANCE AND CLEANING OF THE BEARINGS PRIOR TO DELIVERY. 12. DELIVERY OF ALL DATA AND HARD GOOD PRODUCTS TO THE ADVANCED EVA SPACE SUIT PROJECT GROUP.
contract · Last action 2019-09-20
$75,410
Department of Defense
4510408556!STRAP,WEBBING
contract · Last action 2009-04-02
$72,480
Department of Defense
8505383907!WYE,QUICK DISCONNEC
contract · Last action 2018-04-09
$67,314
National Aeronautics and Space Administration
EXTRAVEHICULAR MOBILITY UNIT SPACE SUIT WRIST BEARINGS
contract · Last action 2012-08-10
$64,500
Department of Defense
4516370773!STRAP,WEBBING
contract · Last action 2010-12-09
$57,870
National Aeronautics and Space Administration
ECCENTRIC SHOULDER BEARINGS
contract · Last action 2011-11-18
$52,546
Department of Defense
8508138585!STRAP,WEBBING
contract · Last action 2021-04-15
$51,820
Department of Defense
4517647405!CONNECTOR,BAYONET,O
contract · Last action 2011-04-25
$51,660
Department of Defense
4508565774!COUPLING
contract · Last action 2008-09-06
$50,915
Department of Defense
8500562083!STRAP WEBBING
contract · Last action 2016-03-29
$50,311
Department of Defense
8509896021!WYE,QUICK DISCONNEC
contract · Last action 2023-05-16
$45,227
Department of Defense
8511396570!CONNECTOR,BAYONET,O
contract · Last action 2025-05-22
$44,395
Department of Defense
8506093109!BODY,VALVE,PNEUMATI
contract · Last action 2018-11-29
$41,385
Department of Defense
8510392910!COUPLING HALF,QUICK
contract · Last action 2024-01-25
$40,019

Federal contract dollars to this establishment. Primary NAICS: 332510 - HARDWARE MANUFACTURING. Last action: 2026-04-23. Source: USAspending.gov, net obligations. Recipient address is the SAM registration / HQ address, not necessarily the worksite.

Inspection history

Date	Trigger	Violations	Serious	Penalty
1981-05-18	Planned	7	2	$300

Source: OSHA IMIS. Citation amounts reflect initially assessed penalties; final amounts after appeal may differ.

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