# N636AR: 1987 Boeing / Dehavilland DHC-8-103, registration cancelled 2018-05-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 22, 2018
- Status when cancelled: Valid registration
- Airframe: [Boeing / Dehavilland DHC-8-103](https://openairdocs.org/model/boeing-dehavilland-dhc-8-103) (registry code 1386005)
- Engine: [Pratt & Whitney Canada PW121](https://openairdocs.org/engine/pratt-whitney-canada-pw121) (registry code 52124)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 086
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 26, 2006
- Certificate issued: September 3, 2008
- Last registry action: March 15, 2018
- Mode S code: A85416
- Owner when cancelled: [Ep Aviation LLC](https://openairdocs.org/faa-owner/EP%20AVIATION%20LLC)
- Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale)
- Owner type: Corporation
- Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N636AR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=636AR
- Page: https://openairdocs.org/deregistered/N636AR-2018-05-22

From the FAA registry file of October 29, 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 Boeing / Dehavilland DHC-8-103: https://openairdocs.org/model/boeing-dehavilland-dhc-8-103.md

## Service difficulty reports (13)

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

- [SDR 39LA2014071481](https://openairdocs.org/sdr/39LA2014071481), Jul 14, 2014: FRAME. CRACKED. FUSELAGE FRAME AT STATION X354.25 CRACKED BETWEEN STRINGER 21L & 22L. R & R FUSELAGE FRAME AT STATION X354.25 IAW RD8-53-2995 & RD8-53-13705.
- [SDR 39LA2014008290077](https://openairdocs.org/sdr/39LA2014008290077), Jul 7, 2014: WEB. DEFECTIVE. FLOOR WEB HAS A DOUBLE DRILLED HOLE AT X580.500, JUST INBD OF CARGO DOOR OPENING. REPAIRED FLOOR WEB AT X580.500, IAW RD 8-53-13681.
- [SDR 39LA2014070780](https://openairdocs.org/sdr/39LA2014070780), Jul 7, 2014: SKIN. CRACKED. RIGHT NACELLE OUTER SKIN CRACKED AT LOWER CORNER FWD OF MLG. REPAIRED RT NACELLE OUTER SKIN CRACK AT LOWER CORNER FWD OF MLG IAW RD8-54-874.
- [SDR 39LA2014070779](https://openairdocs.org/sdr/39LA2014070779), Jul 7, 2014: SKIN. DENTED. FUSELAGE EXTERNAL SKIN DENTED APPROX X269 ABOVE STRINGER 23R. REPAIRED DENT IN FUSELAGE EXTERNAL SKIN AT FS X269 ABOVE STRINGER 23R IAW RD 8-53-13690.
- [SDR 39LA2014070778](https://openairdocs.org/sdr/39LA2014070778), Jul 7, 2014: SKIN. CHIPPED. FUSELAGE EXTERNAL SKIN CHIPPED APPROX X269.0 ABOUT STRINGER 15R. REPAIRED FUSELAGE EXTERNAL SKIN CHIPPING AT FS 270.5, STRINGER 15R IAW RD8-53-13689.
- [SDR 39LA2014070776](https://openairdocs.org/sdr/39LA2014070776), Jul 7, 2014: SKIN PANEL. DENTED. EXTERNAL SKIN DENTED AT FS 610 & STRINGER 18R. REPAIRED DENT AT FS 610 & STRINGER 18R IAW RD 8-53-13688.
- [SDR 39LA2014070775](https://openairdocs.org/sdr/39LA2014070775), Jul 7, 2014: SKIN PANEL. DENTED. DENT, AFT FUSELAGE X492.5 & STRINGER 26L. REPAIRED DENT AFT FUSELAGE X492.5 & STRINGER 26L IAW RD 8-53-13686.
- [SDR 39LA2014070774](https://openairdocs.org/sdr/39LA2014070774), Jul 7, 2014: SKIN. CHAFED. AFT CARGO DOOR OUTER SKIN CHAFED AT UPPER AFT CORNER. REPAIRED AFT CARGO DOOR OUTER SKIN CHAFING IAW RD 8-52-1369.
- [SDR 39LA2014070773](https://openairdocs.org/sdr/39LA2014070773), Jul 7, 2014: ACCESS PANEL. CORRODED. ELEVATOR PANEL 343FT CORRODED AT SCREW HOLES. FABRICATED NEW PANEL 343FT IAW DASH-8-100 SRM 51-24-00 & 51-40-07.
- [SDR 39LA2014011050](https://openairdocs.org/sdr/39LA2014011050), Jan 10, 2014: WIRE. SHORTED. NR 1 ENG OIL PRESS GAGE INDICATING 0 PERFORMED PRECAUTIONARY ENG SHUTDOWN. FOUND WIRE 10004C22-BLK, BETWEEN P7700 P1 & 9811 J17 SHORTED TO GND. CLEANED BOTH CON
- [SDR 39LA2012122500001](https://openairdocs.org/sdr/39LA2012122500001), Dec 25, 2012: WIRE. BROKEN. DURING TAKEOFF ROLL, SPOILER 1 PUSH OFF LIGHT ILLUMINATED. CREW REJECTED TAKEOFF AND RETURNED TO THE GATE. DURING THE INSPECTION OF SPOILER FLIGHT CONTROL SYS, 
- [SDR P4YA2012092300001](https://openairdocs.org/sdr/P4YA2012092300001), Sep 23, 2012: ACTUATOR. INOPERATIVE. RIGHT MAIN GEAR DID NOT COME DOWN WHEN SELECTED. USED ALTERNATE EXTENSION METHOD. UPON INSPECTION, REPLACED FAULTY DOOR ACTUATOR.
- [SDR P4YA2012062000001](https://openairdocs.org/sdr/P4YA2012062000001), Jun 19, 2012: SELECTOR VALVE. FAILED. AC ENTERED LT DOWN WIND LANDING RUNWAY 34 RIGHT INTO OASH, UPON BEING CLEARED TO LAND AND ABEAM THE NUMBERS, PIC CALLED FOR GEAR DOWN AT THE APPROPRIATE SPEED. 

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.