# Air Methods LLC: FAA repair station 2A6D933B

- Type: FAA-certificated repair station (14 CFR Part 145)
- Certificate number: 2A6D933B
- Designator: 2A6D
- Name on the FAA list: AIR METHODS LLC
- Trade names: United Rotorcraft
- Address: 6355 SOUTH SOSSAMAN ROAD, MESA, AZ 85212
- Phone: (412) 466-2500
- Accountable manager: BRYCK, JEREMY, jeremy.bryck@airmethods.com
- Liaison: BRYCK, JEREMY, (970) 765-1909, jeremy.bryck@airmethods.com
- On the FAA list: On the list of October 26, 2026; listed since October 26, 2026 or earlier (OpenAirDocs’ first copy)
- Service difficulty reports filed: 195
- Source: FAA Find a Facility dashboard, https://www.faa.gov/av-info/facility-dashboard
- Page: https://openairdocs.org/faa-repair-station/2A6D933B/air-methods-llc

The FAA writes names in capitals; the mixed case here is OpenAirDocs'. The dashboard has no certificate dates, and nothing on it shows whether a certificate is in good standing.

## Ratings

- Airframe: Limited
- Powerplant: Limited
- Radio: Limited
- Instrument: Limited
- Accessory: Limited

A Limited class covers only the makes and models in the station's operations specifications (14 CFR 145.61), which the FAA doesn't publish.

## Service difficulty reports (195, newest 50)

Filed under designator 2A6D by a repair station (submitter type B).

- [SDR 2A6D20260814](https://openairdocs.org/sdr/2A6D20260814), Aug 14, 2026: Urocop EC130T2. FRAME. CORRODED. CORROSION ON THE COLLECTIVE SPLIT FRAME ON FWD AND AFT SIDE OF OPENING. (N741AC)
- [SDR 2A6D20260813002](https://openairdocs.org/sdr/2A6D20260813002), Aug 13, 2026: Urocop EC130T2. RIB. CHAFED. CHAFE DAMAGE ON BL 1263 RIB ON RH SIDE OF HORIZONTAL STABILIZER. (N741AC)
- [SDR 2A6D20260813001](https://openairdocs.org/sdr/2A6D20260813001), Aug 13, 2026: Urocop EC130T2. CROSSBEAM. CHAFED. GOUGE/CHAFE DAMAGE TO THE AFT LANDING GEAR ATTACHMENT FWD CROSSBEAM AND SUPPORT ANGLE. (N741AC)
- [SDR 2A6D20260728001](https://openairdocs.org/sdr/2A6D20260728001), Jun 16, 2026: Snias AS350B3. SUPPORT ANGLE. CRACKED. CRACK FOUND ON SUPPORT ANGLE OF UPPER LEFT FUSELAGE TO TAILBOOM ATTACHMENT (N350MV)
- [SDR 2A6D20260305001](https://openairdocs.org/sdr/2A6D20260305001), Mar 3, 2026: Urocop EC130T2. FUEL LINE. BENT. WHILE HOVER TAXIING THE AIRCRAFT DURING CHECK FLIGHTS, THE PILOT REPORTED A FUEL P LIGHT AND TURNED THE AIRCRAFT AROUND  (N11KQ)
- [SDR 2A6D20251125001](https://openairdocs.org/sdr/2A6D20251125001), Nov 25, 2025: Urocop EC130B4. CROSSBEAM. CHAFED. VARIOUS DAMAGES AT THE AFT LANDING GEAR LOCATION, THE FIRST DAMAGE (#1) IS AT THE AFT LANDING GEAR CROSS BEAM SHIM (P/N: (N92OU)
- [SDR 2A6D20251106001](https://openairdocs.org/sdr/2A6D20251106001), Nov 6, 2025: Snias AS350B3. BULKHEAD. CHAFED. CHAFING DAMAGE ON THE LT LONGITUDINAL BULKHEAD (X-FRAME) ON THE UPPER INBD FACE MEASURING APPROXIMATELY 0.017" IN DEPTH, (N629AM)
- [SDR 2A6D20251105001](https://openairdocs.org/sdr/2A6D20251105001), Nov 5, 2025: Snias AS350B3. BEAM. CHAFED. DAMAGE TO THE RH Y398.5 BEAM (P/N: 350A211351.22) AND STOP DOUBLER (P/N: 350A211363.25) IN THE FORM OF A CHAFE. THE CHAF (N629AM)
- [SDR 2A6D20251006001](https://openairdocs.org/sdr/2A6D20251006001), Oct 6, 2025: Snias AS350B3. KEELBEAM. DAMAGED. A MIS-DRILLED HOLE WAS FOUND ON THE FORWARD LH KEEL BEAM (PN: 350A21-1350-20), AFT LH KEEL BEAM (PN: 350A21-1056- 20) AN (N814SM)
- [SDR 2A6D20250818001](https://openairdocs.org/sdr/2A6D20250818001), Aug 18, 2025: Snias AS350B3. MOUNT FLANGE. GOUGED. DAMAGE TO THE LANDING GEAR LH OTBD AFT BEARING IN THE FORM OF GOUGE. THE GOUGE DAMAGE IS AT LOWER FLANGE OF THE BEARING  (N109LN)
- [SDR 2A6D20250602002](https://openairdocs.org/sdr/2A6D20250602002), Jun 2, 2025: Snias AS350B3. FLOOR SUPPORT. CHAFED. CHAFE DAMAGE WAS DISCOVERED ON THE R/H CABIN FLOOR EDGE P/N: 350A21-1359-21 (N267AM)
- [SDR 2A6D20250602001](https://openairdocs.org/sdr/2A6D20250602001), Jun 2, 2025: Snias AS350B3. DOUBLER. CHAFED. CHAFING DAMAGE WAS DISCOVERED ON T/R SERVO GUIDE DOUBLER P/N: 355A23-2000-20 (N267AM)
- [SDR 2A6D20250502001](https://openairdocs.org/sdr/2A6D20250502001), Jun 2, 2025: Urocop EC130T2. XMSN DECK. CHAFED. GOUGING- TOOL DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE TRANSMISSION DECK. THE DEPTH IS APPROXIMATELY 0.026". THE MAXI (N11UQ)
- [SDR 2A6D20250130001](https://openairdocs.org/sdr/2A6D20250130001), Jan 30, 2025: Snias AS350B3. BEAM. DAMAGED. FASTENER HOLE DAMAGE (ELONGATION) WAS DISCOVERED ON THE LH MAINTENANCE FOOTSTEP BEAM (P/N 350A21124520) IN THE FUSELAGE  (N354CF)
- [SDR 2A6D20241209001](https://openairdocs.org/sdr/2A6D20241209001), Dec 9, 2024: Urocop EC130B4. CROSSBEAM. CHAFED. THE FIRST DAMAGE IS ON THE AFT LANDING GEAR CROSS BEAM (P/N: 350A214311.20). THE AFT CROSS BEAM IS DAMAGED DUE TO MISSIN (N317AM)
- [SDR 2A6D20240828006](https://openairdocs.org/sdr/2A6D20240828006), Aug 28, 2024: Snias AS350B3. STRUCTURE. GOUGED. GOUGE AT THE OUTBOARD FLANGE RIVNUT LOCATION IN THE FORM OF SHEAR OUT. THE GOUGE WAS MEASURED TO BE APPROXIMATELY 0.1” X (N108LN)
- [SDR 2A6D20240828003](https://openairdocs.org/sdr/2A6D20240828003), Aug 28, 2024: Snias AS350B3. BULKHEAD WEB. CHAFED. DAMAGE TO THE 15° BULKHEAD LH WEB (PN: 350A21-1032.86) IN THE FORM OF SEVERAL CHAFES. THE CHAFES WERE REPORTED TO BE 0.2 (N108LN)
- [SDR 2A6D20240828002](https://openairdocs.org/sdr/2A6D20240828002), Aug 28, 2024: Snias AS350B3. STRUCTURE. GOUGED. DAMAGE TO THE LH UPPER CARGO EDGING (P/N: 350A211041.22) IN THE FORM OF A GOUGE CAUSED WHILE INSTALLING BLIND FASTENER.  (N108LN)
- [SDR 2A6D20240828001](https://openairdocs.org/sdr/2A6D20240828001), Aug 28, 2024: Snias AS350B3. FLOOR PANEL. CORRODED. THERE IS CORROSION DAMAGE TO THE CABIN FLOOR EDGING (PN: 350A21-1359-20/21). (N108LN)
- [SDR 2A6D20240614001](https://openairdocs.org/sdr/2A6D20240614001), Jun 14, 2024: Urocop EC130T2. ATTACH ANGLE. CRACKED. DAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DA (N11FQ)
- [SDR 2A6D20240528001](https://openairdocs.org/sdr/2A6D20240528001), May 28, 2024: Urocop EC130T2. FRAME. CORRODED. DAMAGE TO THE AFT UPPER FRAME (P/N: 350A21-1242.35) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS ON THE UPPER FLANG (N11FQ)
- [SDR 2A6D20240509003](https://openairdocs.org/sdr/2A6D20240509003), May 9, 2024: Urocop EC130T2. FLOORBEAM. CORRODED. DAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PL (N11FQ)
- [SDR 2A6D20240509002](https://openairdocs.org/sdr/2A6D20240509002), May 9, 2024: Urocop EC130T2. BONDING PLATE. CORRODED. DAMAGE IS ON THE TAIL BOOM VHF ANTENNA BASE PLATE (P/N: 350A65-1707.00) IN THE FORM OF CORROSION. THE BASE PLATE IS EXCE (N11FQ)
- [SDR 2A6D20240509001](https://openairdocs.org/sdr/2A6D20240509001), May 9, 2024: Urocop EC130T2. BULKHEAD. CORRODED. THE UPPER 7° BULKHEAD DOUBLER (PN: 350A21-0849.20) IS CORRODED AT THE LOCATION OF A PASS-THRU HOLE. THE DAMAGE AREA WAS  (N11FQ)
- [SDR 2A6D20240508003](https://openairdocs.org/sdr/2A6D20240508003), May 8, 2024: Urocop EC130T2. CROSSTUBE. CORRODED. THE AFT LANDING GEAR CROSSTUBE FITTING (PN: 350A21-0960.20) IS CORRODED IN MULTIPLE AREAS ON THE LOWER SURFACE. THE DEEP (N11FQ)
- [SDR 2A6D20240508002](https://openairdocs.org/sdr/2A6D20240508002), May 8, 2024: Urocop EC130T2. CROSSBEAM. CORRODED. THE RH X2244 CROSSBEAM (PN: 350A21-0861.20) IS CORRODED IN AN AREA ON THE LOWER OUTBOARD CORNER OF THE CROSSBEAM. THE DA (N11FQ)
- [SDR 2A6D20240508001](https://openairdocs.org/sdr/2A6D20240508001), May 8, 2024: Urocop EC130T2. CROSSBEAM. CORRODED. THE RH X1790 CROSSBEAM (PN: 350A21-0572.20) IS CORRODED IN AN AREA WHERE IT CONTACTS THE RH Y400 BEAM (PN: 350A21-0587.2 (N11FQ)
- [SDR 2A6D2024043002](https://openairdocs.org/sdr/2A6D2024043002), Apr 25, 2024: Snias AS350B3. BEAM. DAMAGED. DAMAGE TO THE LH BEAM UNDER THE ENGINE DECK (P/N: 355A21-2110.25) IN THE FORM OF AN ELONGATED HOLE IN THE LOWER FLANGE N (N350AM)
- [SDR 2A6D20240425009](https://openairdocs.org/sdr/2A6D20240425009), Apr 25, 2024: Urocop EC130T2. SKIN PANEL. CORRODED. CORROSION DAMAGE ON THE FWD UPPER SKIN MEASURED TO BE APPROXIMATELY 0.80” X 0.60” X 0.003” (N11FQ)
- [SDR 2A6D20240425008](https://openairdocs.org/sdr/2A6D20240425008), Apr 25, 2024: Urocop EC130T2. STIFFENER. CORRODED. DAMAGE TO THE TAIL BOOM LH FWD STIFFENER MEASURED TO BE APPROXIMATELY 0.85” X 0.85” X 0.0125” IN THE FORM OF CORROSION. (N11FQ)
- [SDR 2A6D20240425007](https://openairdocs.org/sdr/2A6D20240425007), Apr 25, 2024: Urocop EC130T2. ATTACH ANGLE. CORRODED. REAR LANDING GEAR ATTACHMENT LOWER ANGLE HAS DAMAGE IN THE FORM OF CORROSION. THE DAMAGE NEAR THE ANGLE OVERLAPS WITH MA (N11FQ)
- [SDR 2A6D20240425006](https://openairdocs.org/sdr/2A6D20240425006), Apr 25, 2024: Urocop EC130T2. CRADLE. CORRODED. RH AFT FUEL CRADLE REINFORCEMENTS HAS DAMAGE IN THE FORM OF CORROSION. THE RH AFT CORROSION DAMAGE MEASURED TO BE APPROX (N11FQ)
- [SDR 2A6D20240425005](https://openairdocs.org/sdr/2A6D20240425005), Apr 25, 2024: Urocop EC130T2. CRADLE. CORRODED. THE LH FWD FUEL CRADLE REINFORCEMENTS HAD DAMAGE IN THE FORM OF CORROSION. THE LH FWD CORROSION DAMAGE MEASURED TO BE AP (N11FQ)
- [SDR 2A6D20240425004](https://openairdocs.org/sdr/2A6D20240425004), Apr 25, 2024: Urocop EC130T2. SKIN PANEL. CORRODED. DAMAGE IS ON THE AFT FUSELAGE RH SIDE SKIN PANEL (P/N: 350A210046-21 IN THE FORM OF CORROSION. THE RH SIDE SKIN DAMAGE I (N11FQ)
- [SDR 2A6D20240425003](https://openairdocs.org/sdr/2A6D20240425003), Apr 25, 2024: Urocop EC130T2. SKIN PANEL. CORRODED. FIRST DAMAGE IS ON THE AFT FUSELAGE LH SIDE SKIN PANEL IN THE FORM OF CORROSION. THE LH SIDE SKIN DAMAGE IS NEAR TOP EDG (N11FQ)
- [SDR 2A6D20240425002](https://openairdocs.org/sdr/2A6D20240425002), Apr 25, 2024: Urocop EC130T2. BRACE. CORRODED. DAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CO (N11FQ)
- [SDR 2A6D20240425001](https://openairdocs.org/sdr/2A6D20240425001), Apr 25, 2024: Urocop EC130T2. WEB. CORRODED. DAMAGE TO THE LOWER CENTER WEB IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LI (N11FQ)
- [SDR 2A6D20240402001](https://openairdocs.org/sdr/2A6D20240402001), Apr 2, 2024: Snias AS350B3. XMSN DECK. CHAFED. CHAFING DAMAGE WAS DISCOVERED ON THE L/H SIDE TRANSMISSION DECK. (N629AM)
- [SDR 2A6D20240329001](https://openairdocs.org/sdr/2A6D20240329001), Mar 29, 2024: Snias AS350B3. XMSN DECK. CHAFED. CHAFING DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE MEASURES APPROXIMATELY 0.3” LONG, 0.1 WIDE WITH A MAX (N350AM)
- [SDR 2A6D20240321002](https://openairdocs.org/sdr/2A6D20240321002), Mar 21, 2024: Snias AS350B3. FLOOR SUPPORT. CORRODED. CORROSION DAMAGE DISCOVERED TO THE R/H CABIN FLOOR EDGING P/N: 350A21-1359-21. (N4497Y)
- [SDR 2A6D20240321001](https://openairdocs.org/sdr/2A6D20240321001), Mar 21, 2024: Snias AS350B3. FLOOR SUPPORT. CORRODED. CORROSION DAMAGE DISCOVERED TO THE L/H CABIN FLOOR EDGING P/N: 350A21-1359-20. (N4497Y)
- [SDR 2A6D20240320001](https://openairdocs.org/sdr/2A6D20240320001), Mar 20, 2024: Urocop EC130T2. SUPPORT ANGLE. CORRODED. EXFOLIATION CORROSION LOCATED ON FWD. L/H SIDE STIFFENER OF MASTER ELECTRICAL BOX. (N11FQ)
- [SDR 2A6D20240229001](https://openairdocs.org/sdr/2A6D20240229001), Feb 29, 2024: Urocop EC130B4. BULKHEAD. CRACKED. A CRACK WAS DISCOVERED ON THE AFT BULKHEAD CENTER STRUCTURE. THE CRACK MEASURES APPROXIMATELY 1.0 INCH LONG (N344AM)
- [SDR 2A6D20240201002](https://openairdocs.org/sdr/2A6D20240201002), Feb 1, 2024: Urocop EC130B4. WEB. CORRODED. DAMAGE TO THE LOWER CENTER WEB (P/N: 350A21-4300.20) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT S (N11FQ)
- [SDR 2A6D20240201001](https://openairdocs.org/sdr/2A6D20240201001), Feb 1, 2024: Urocop EC130B4. ANGLE. CORRODED. DAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CO (N11FQ)
- [SDR 2A6D20231102001](https://openairdocs.org/sdr/2A6D20231102001), Nov 2, 2023: Snias AS350B3. FLOOR SUPPORT. CORRODED. CORROSION WAS FOUND ON THE CABIN FLOOR EDGING ON THE LH AND RH SIDE (P/N: 350A21-1359-20/21) (N574AM)
- [SDR 2A6D20230825001](https://openairdocs.org/sdr/2A6D20230825001), Aug 25, 2023: Urocop EC130T2. BULKHEAD. CHAFED. DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE 15 DEGREE BULKHEAD ON THE AFT FACE. THE CHAFE CORRESPONDS TO AN ANGLE CLIP O (N790K)
- [SDR 2A6D20230824003](https://openairdocs.org/sdr/2A6D20230824003), Aug 24, 2023: Snias AS350B3. XMSN DECK. CHAFED. CHAFING DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE TRANSMISSION DECK. THE FIRST CHAFE AREA MEASURES APPROXIMATELY: 0.01 (N544AM)
- [SDR 2A6D20230807002](https://openairdocs.org/sdr/2A6D20230807002), Aug 7, 2023: Urocop EC130T2. BULKHEAD. CHAFED. DAMAGE TO THE AFT BULKHEAD PANEL (P/N: 350A21-1570.20) IN THE FORM OF MULTIPLE CHAFED AREAS IN THE PART, MOST OF WHICH A (N223SH)
- [SDR 2A6D20230807001](https://openairdocs.org/sdr/2A6D20230807001), Aug 7, 2023: Urocop EC130T2. FLANGE. CRACKED. DAMAGE TO THE LH SIDE OF THE 7 DEG BULKHEAD FLANGE (P/N: 350A21-0980.22) IN THE FORM OF A CRACK AND A DENT AT THE FASTEN (N223SH)

All 195: https://openairdocs.org/faa-repair-station/2A6D933B/air-methods-llc/reports.md

## Other certificates of this company (1)

- [QMLR253U](https://openairdocs.org/faa-repair-station/QMLR253U/air-methods-llc): Air Methods LLC, Englewood, CO

## STCs held under this name

STC holders whose name matches the station's, matched by OpenAirDocs; a shared name can be another company.

- Air Methods Corporation (OpenAirDocs): 138 STCs, https://openairdocs.org/search?q=Air%20Methods%20Corporation&type=stc
- Air Methods LLC (OpenAirDocs): 32 STCs, https://openairdocs.org/search?q=Air%20Methods%20LLC&type=stc
- Air Methods Inc. (OpenAirDocs): 3 STCs, https://openairdocs.org/search?q=Air%20Methods%20Inc.&type=stc
- Air Methods Corp. (OpenAirDocs): 2 STCs, https://openairdocs.org/search?q=Air%20Methods%20Corp.&type=stc

## Aircraft registered to this name

Registry owners whose name matches the station's, matched by OpenAirDocs; a shared name can be another company.

- [AIR METHODS LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC.md) (OpenAirDocs): 342 registered aircraft

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