# N852HK: 2000 Embraer EMB-145LR, registration cancelled 2019-09-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 6, 2019
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145353
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 16, 2000
- Certificate issued: May 30, 2013
- Last registry action: February 10, 2016
- Mode S code: ABAF7F
- Owner when cancelled: [Aerovision Aircraft Services LLC](https://openairdocs.org/faa-owner/AEROVISION%20AIRCRAFT%20SERVICES%20LLC)
- Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon)
- Owner type: LLC
- Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N852HK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=852HK
- Page: https://openairdocs.org/deregistered/N852HK-2019-09-06

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md

## Service difficulty reports (63, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR RAIA201009110002](https://openairdocs.org/sdr/RAIA201009110002), Sep 11, 2010: LIGHT. INOPERATIVE. DURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE FWD EMERGENCY LIGHT INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LIGHT BULB. SYSTEM OPS CH
- [SDR RAIA201008270002](https://openairdocs.org/sdr/RAIA201008270002), Aug 27, 2010: SEAL. DIRTY. DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND CLEANED THE PASSENGER DOOR SEAL. DOOR OPS CHEC
- [SDR RAIA201008250001](https://openairdocs.org/sdr/RAIA201008250001), Aug 25, 2010: CONNECTOR. LOOSE. DURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY LIGHT AT ROW 11 WAS INOP. MAINTENANCE INSPECTED AND FOUND A LOOSE CONNECTION. MAINTENANCE RES
- [SDR RAIA201008110001](https://openairdocs.org/sdr/RAIA201008110001), Aug 11, 2010: SEAL. DIRTY. FLIGHT CREW REPORTED THE PASSENGER DOOR AS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND CLEANED THE PASSENGER DOOR SEAL. OPS CHECKED GOOD.
- [SDR V0XR201007290002](https://openairdocs.org/sdr/V0XR201007290002), Jul 29, 2010: SEAT TRACK. CORRODED. SEAT TRACK AT CTR FUSELAGE III FR 36-47 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2094
- [SDR V0XR201007290001](https://openairdocs.org/sdr/V0XR201007290001), Jul 29, 2010: SEAT TRACK. CORRODED. SEAT TRACK AT CENTER FUSELAGE FR 30 - 35 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2093
- [SDR V0XR201007280012](https://openairdocs.org/sdr/V0XR201007280012), Jul 28, 2010: ANGLE. CRACKED. (V0XR) RT WING BODY FAIRING TOP ATTACHMENT BRACKET AT FR 48 IS CRACKED BEYOND LIMITS. R & R RT WING BODY FAIRING ANGLE. W/C 6009
- [SDR V0XR201007280011](https://openairdocs.org/sdr/V0XR201007280011), Jul 28, 2010: ATTACH BRACKET. CRACKED. (V0XR) RT WING BODY FAIRING TOP ATTACHMENT BRACKET AT FR 49 IS CRACKED BEYOND LIMITS. R & R RT WING BODY FAIRING ANGLE. W/C 6008
- [SDR V0XR201007280010](https://openairdocs.org/sdr/V0XR201007280010), Jul 28, 2010: ANGLE. CRACKED. (V0XR) LT WING BODY FAIRING BOTTOM ATTACHMENT BRACKET AT FR 47 IS CRACKED BEYOND LIMITS. R & R LT WING BODY FAIRING ANGLE. W/C 5066
- [SDR V0XR201007280009](https://openairdocs.org/sdr/V0XR201007280009), Jul 28, 2010: SEAT TRACK. CORRODED. (V0XR) LT OTBD SEAT TRACK AT FR 36-47 IS CORRODED BEYOND LIMITS. R & R LT OTBD SEAT TRACK. W/C 2161
- [SDR V0XR201007280008](https://openairdocs.org/sdr/V0XR201007280008), Jul 28, 2010: SEAT TRACK. CORRODED. (V0XR) SEAT TRACK AT FR 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2159.
- [SDR V0XR201007280007](https://openairdocs.org/sdr/V0XR201007280007), Jul 28, 2010: FLOOR SUPPORT. CRACKED. (V0XR) RT FWD OMEGA BEAM Y479.0 IS CRACKED BEYOND LIMITS. R & R FWD OMEGA BEAM. W/C 2130
- [SDR V0XR201007280006](https://openairdocs.org/sdr/V0XR201007280006), Jul 28, 2010: SEAT TRACK. CORRODED. (V0XR) CO-PILOTS SEAT TRACK IS CORRODED BEYOND LIMITS. R & R CO-PILOTS SEAT TRACK. W/C 2113
- [SDR V0XR201007280005](https://openairdocs.org/sdr/V0XR201007280005), Jul 28, 2010: SEAT TRACK. CORRODED. (V0XR) SEAT TRACK AT CENTER FUSELAGE STA 4154.5 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2102
- [SDR V0XR201007280004](https://openairdocs.org/sdr/V0XR201007280004), Jul 28, 2010: SEAT TRACK. CORRODED. (V0XR) SEAT TRACK BEAM Y0.0 AT FR 40-46 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK BEAM. W/C 1087
- [SDR V0XR201007280003](https://openairdocs.org/sdr/V0XR201007280003), Jul 28, 2010: CHANNEL. CRACKED. (V0XR) SERVICE DOOR FRAME CHANNEL FR 21-16R IS CORRODED BEYOND LIMITS. R & R SERVICE DOOR FRAME CHANNEL. W/C 1058
- [SDR V0XR201007280002](https://openairdocs.org/sdr/V0XR201007280002), Jul 28, 2010: STRUCTURE. CRACKED. (V0XR) RT COLUMN FR 24 IS CRACKED. R & R RT COLUMN. W/C 1083
- [SDR V0XR201007280001](https://openairdocs.org/sdr/V0XR201007280001), Jul 28, 2010: GUSSET. CORRODED. (V0XR) CENTER BEAM GUSSET Y0.0 FR 20-23 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1060
- [SDR V0XR20100726014](https://openairdocs.org/sdr/V0XR20100726014), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS AT STA 7131.0. REPLACED SEAT TRACK AT STA 7131.0 IAW AMM 53-01-06. W/C 2101.
- [SDR V0XR20100726013](https://openairdocs.org/sdr/V0XR20100726013), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS, CENTER FUSELAGE IV. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. W/C 2100.
- [SDR V0XR20100726012](https://openairdocs.org/sdr/V0XR20100726012), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS, CENTER FUSELAGE III, FRAMES 47-52. REPLACED SEAT TRACK RT AT FRAMES 47-52 IAW EMB145 AMM 53-01-06. W/C 2098.
- [SDR V0XR20100726011](https://openairdocs.org/sdr/V0XR20100726011), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS, CENTER FUSELAGE III, FRAME 47-52. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. W/C 2097.
- [SDR V0XR20100726010](https://openairdocs.org/sdr/V0XR20100726010), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS AT CENTER FUSELAGE III, FRAMES 36-49. REMOVED OLD SEAT TRACK AND INSTALLED NEW AT CENTER FUSELAGE III, FROM FRAMES 36-47, IAW 
- [SDR V0XR20100726009](https://openairdocs.org/sdr/V0XR20100726009), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS AT CENTER SECTION II, FRAMES 30-35. REMOVED AND REPLACED LT UPPER SEAT TRACK IN CENTER FUSELAGE II IAW AMM 53-01-06. W/C 2092.
- [SDR V0XR20100726008](https://openairdocs.org/sdr/V0XR20100726008), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS AT CENTER FUSELAGE II BETWEEN FRAMES 30 TO 35. REMOVED AND REPLACED SEAT TRACK IAW EMB145 AMM 53-01-06. W/C 2091.
- [SDR V0XR20100726007](https://openairdocs.org/sdr/V0XR20100726007), Jul 26, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS AT CENTER FUSELAGE II, BETWEEN FRAMES 24-30. REMOVED AND REPLACED CORRODED SEAT TRACK AT CENTER FUSELAGE II, LOWER LT BETWEEN 
- [SDR V0XR20100726006](https://openairdocs.org/sdr/V0XR20100726006), Jul 26, 2010: ANGLE. CORRODED. ANGLE AT FRAME 23 AND RY780.0 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED ANGLE AT FRAME 23 AND RY780.0 IAW SRM 51-40-02. W/C 1085.
- [SDR V0XR20100726005](https://openairdocs.org/sdr/V0XR20100726005), Jul 26, 2010: ANGLE. CORRODED. FORWARD RIGHT ANGLE BETWEEN FRAMES 23 AND 24 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANGLE BETWEEN FRAMES 23 AND 24 IAW EMB145 SRM 51-40-02. W/C 1082.
- [SDR V0XR20100726004](https://openairdocs.org/sdr/V0XR20100726004), Jul 26, 2010: FLOORBEAM. CORRODED. DIGITAL PLATE AT FRAME 15, LY780.0 TO RY780.0 CORRODED OUT OF LIMITS. REPLACED DIGITAL PLATE AT FRAME 15 FROM LY780.0 TO RY 780.0 IAW SRM 21-20-02, 51-10-02, 51
- [SDR V0XR20100726003](https://openairdocs.org/sdr/V0XR20100726003), Jul 26, 2010: ANGLE. CORRODED. SCALLOPED ANGLE AT FRAME 18 AND LY479.0 TO Y780.0 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SCALLOPED ANGLE WITH NEW ANGLE IAW SRM 51-40-02. W/C 1059.
- [SDR V0XR20100726002](https://openairdocs.org/sdr/V0XR20100726002), Jul 26, 2010: FRAME. CORRODED. DOUBLERS AT FRAME 20 AND 22 AT RY479.0 ARE CORRODED OUT OF LIMITS. DRILLED OFF OLD DOUBLERS, MATCH DRILLED TWO EACH NEW DOUBLERS AND INSTALLED IAW SRM 51-20-03 
- [SDR V0XR20100726001](https://openairdocs.org/sdr/V0XR20100726001), Jul 26, 2010: GUSSET. CORRODED. GUSSET AT FRAME 17-18 LY478.0 - Y 0.0 CORRODED OUT OF LIMITS. REPLACED GUSSET AT FRAME 17-18, LY 478.0 - Y 0.0 IAW EMB145 SRM 51-20-01, 51-10-02, 51-40-02, 51-4
- [SDR V0XR20100723012](https://openairdocs.org/sdr/V0XR20100723012), Jul 23, 2010: PROFILE. CORRODED. PROFILE AT FRAME 18, LT SIDE IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE AT FRAME 18, I/B SIDE OF LT OMEGA BEAM IAW EMB145 SRM 51-10-02 AND 51-40-02
- [SDR V0XR20100723011](https://openairdocs.org/sdr/V0XR20100723011), Jul 23, 2010: DOUBLER. CORRODED. PREVIOUS REPAIR ON OMEGA BEAM LT AT FRAME 19 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED NEW PATCH REPAIR WITH 2024T3 0.050 MATERIAL ON OMEGA B
- [SDR V0XR20100723010](https://openairdocs.org/sdr/V0XR20100723010), Jul 23, 2010: SILL. CORRODED. RIGHT SILL AT FRAMES 48-52 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED RIGHT SILL AT FRAMES 48-52 IAW EMB145 SRM 51-40-02, 51-20-01, AND 51-10-02. W/C 2104.
- [SDR V0XR20100723009](https://openairdocs.org/sdr/V0XR20100723009), Jul 23, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS AT CENTER FUSELAGE II. REMOVED AND REPLACED SEAT TRACK AT UPPER LT CENTER FUSELAGE II IAW EMB145 AMM 53-01-06. W/C 2089.
- [SDR V0XR20100723008](https://openairdocs.org/sdr/V0XR20100723008), Jul 23, 2010: SILL. CORRODED. AFT MAIN SERVICE DOOR SILL AT FRAMES 22-23, Y780.0 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED MAIN SERVICE DOOR SILL AT FRAMES 22-23, Y780.0 IAW EMB145 SRM
- [SDR V0XR20100723007](https://openairdocs.org/sdr/V0XR20100723007), Jul 23, 2010: SILL. CORRODED. RIGHT SILL BETWEEN FRAMES 52-59 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED RIGHT SILL FR52-59 IAW EMB145 SRM 51-40-02. W/C 2105.
- [SDR V0XR20100723006](https://openairdocs.org/sdr/V0XR20100723006), Jul 23, 2010: SILL. CORRODED. SILL AT RY780.0 BETWEEN FRAMES 18-20 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SILL AT RY780.0 FR 18-20 IAW EMB145 SRM 51-10-02, 51-40-02, AND 51-20-03. W
- [SDR V0XR20100723005](https://openairdocs.org/sdr/V0XR20100723005), Jul 23, 2010: PROFILE. CORRODED. PROFILE AT YL479, FR 63 HAS A PUNCTURE HOLE. REMOVED AND REPLACED WITH NEW PART. W/C 1067.
- [SDR V0XR20100723004](https://openairdocs.org/sdr/V0XR20100723004), Jul 23, 2010: SILL. CORRODED. RIGHT SILL BETWEEN FRAME 59-61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL BETWEEN FRAME 59-61 IAW EMB145 SRM 51-10-02, 51-40-02, AND 51-20-03. W/C 210
- [SDR V0XR20100723003](https://openairdocs.org/sdr/V0XR20100723003), Jul 23, 2010: SILL. CORRODED. RIGHT SILL FRAME 61-65 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED RIGHT SILL FRAME IAW EMB145 SRM 51-10-02, 51-40-02, AND 51-20-03. W/C 2107.
- [SDR V0XR20100723002](https://openairdocs.org/sdr/V0XR20100723002), Jul 23, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS, CENTER FUSELAGE IV. REMOVED AND REPLACED SEAT TRACK ON FUSELAGE IV CENTER LT TRACK A IAW EMB 145 AMM 53-01-06.
- [SDR V0XR20100723001](https://openairdocs.org/sdr/V0XR20100723001), Jul 23, 2010: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BEYOND LIMITS, CENTER FUSELAGE III, FRAME 47-52. REMOVED AND REPLACED SEAT TRACK IN CENTER FUSELAGE III, FRAME 47-52 IAW EMB 145 AMM 53-01-0
- [SDR V0XR201007200002](https://openairdocs.org/sdr/V0XR201007200002), Jul 20, 2010: GUSSET. CORRODED. (V0XR) GUSSET YO.O, FRM 59 - 61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2108
- [SDR V0XR201007200001](https://openairdocs.org/sdr/V0XR201007200001), Jul 20, 2010: GUSSET. CORRODED. (V0XR) RT GUSSET 479.0, FRM 59 - 61 IS CORRODED BEYOND LIMITS. R & R RT GUSSET. W/C 2106
- [SDR RAIA201007080001](https://openairdocs.org/sdr/RAIA201007080001), Jul 8, 2010: MECHANISM. LOOSE. DURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR HARD TO OPEN. MAINTENANCE INSPECTED AND FOUND THE ACTUATING MECHANISM LOOSE. RE-SECURE
- [SDR RAIA201007070002](https://openairdocs.org/sdr/RAIA201007070002), Jul 7, 2010: LINKAGE. BINDING. FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED, CLEANED, AND LUBED THE PASSENGER DOOR LINKAGES. DOOR OPS CHECKED GOOD.
- [SDR RAIA2010042800001](https://openairdocs.org/sdr/RAIA2010042800001), Apr 28, 2010: CONNECTOR. LOOSE. DURING THE PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT SIGN AS BEING INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND 
- [SDR RAIA2010030700002](https://openairdocs.org/sdr/RAIA2010030700002), Mar 7, 2010: DUCT. BROKEN. DURING CRUISE, THE CREW REPORTED RECEIVING A PACK NR 1 FAIL MESSAGE ON THE EICAS. THE NR 2 PACK WAS ON DEFERRAL. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED 

All 63: https://openairdocs.org/deregistered/N852HK-2019-09-06/reports.md

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