This N-number isn't registered right now. Below is its last known registration, canceled Feb 11, 2020.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2016)30 ADs may apply231 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
incorrect installation of the frangible towing fuse that prevented the nose landing gear from extending.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA16CA226)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-11-06 | Hardware; 51, Standard practices/structures | Jul 9, 2026 | Airframe (DHC-8-202) |
| 2021-19-11 | Flight controls | Nov 18, 2021 | Airframe (DHC-8-202)Serial numbers per De Havilland Service Bulletin 8-27-123, Revision A (DHC-8-100/200/300); De Havilland Service Bulletin 84-27-74, Revision B (DHC-8-400) |
| 2019-12-17 | Stabilizers | Aug 12, 2019 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| 2018-23-04 | Ignition; 76, Engine Controls | Mar 15, 2019 | Airframe (DHC-8-202)Certain serial numbers: 003–540. Only with: Bombardier Service Bulletin 8-74-02 (original or Revision A) accomplished concurrently with or after Bombardier Service Bulletin 8-76-35 or 8-76-24. |
| 2018-20-12 | Ice and rain protection | Nov 23, 2018 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2017-15-11 | Landing Gear | Sep 5, 2017 | Airframe (DHC-8-202)Certain serial numbers: 003–672. Only with: Equipped with MLG retraction actuator assembly P/N 10500-101, -103, -501, -551, or -553. |
| 2017-08-02 | Ignition | May 17, 2017 | Airframe (DHC-8-202)Certain serial numbers: 003–672. Only with: Bombardier ModSum 8Q100813 or Bombardier Service Bulletin 8-74-02 incorporated. |
| 2016-24-06 | Ice and rain protection | Jan 12, 2017 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| 2016-24-01 | Electrical Power | Dec 30, 2016 | Airframe (DHC-8-202)Certain serial numbers: 003–672. Only with: Terminal block part number 82450075-001 installed. |
| 2016-10-07 | Electrical power | Jun 23, 2016 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| 2015-21-02 | Electrical Power | Nov 24, 2015 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| 2015-14-03 | Fuel | Aug 21, 2015 | Airframe (DHC-8-202)Certain serial numbers: 003–624; 626 |
| 2015-04-08 | Landing Gear | Apr 27, 2015 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| 2013-15-06 | Electrical Power | Oct 20, 2014 | Airframe (DHC-8-202)Certain serial numbers: 003–on |
| 2014-15-07 | Wings | Sep 2, 2014 | Airframe (DHC-8-202)Certain serial numbers: 003–672 |
| 2014-13-18 | Instruments; Code 76, Engine Controls | Aug 19, 2014 | Airframe (DHC-8-202)Certain serial numbers: 003–672. Only with: Beta warning horn (BWH) (Mod 8/2852) incorporated; excludes airplanes with Bombardier option CR873CH00003, CR873CH00005, CR873SOO8112, or MS8Q902206 incorporated. |
| 2014-05-17 | Fuel | May 2, 2014 | Airframe (DHC-8-202)Certain serial numbers: 002–672 |
| 2013-22-04 | Flight controls | Dec 5, 2013 | Airframe (DHC-8-202)Certain serial numbers: DHC-8-102 003–672; DHC-8-103 003–672; DHC-8-106 003–672; DHC-8-201 003–672; DHC-8-202 003–672; DHC-8-301 003–672; … |
| 2013-15-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Sep 17, 2013 | Engine (PW123)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table. |
| 2013-14-09 | Landing gear | Sep 10, 2013 | Airframe (DHC-8-202)Certain serial numbers: 003–on |
| 2013-04-07 | Electrical Power | Apr 9, 2013 | Airframe (DHC-8-202)Certain serial numbers: 002–672 |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW123)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2012-04-08 | Flight controls | Apr 10, 2012 | Airframe (DHC-8-202)Certain serial numbers: DHC-8-102 003–672; DHC-8-103 003–672; DHC-8-106 003–672; DHC-8-201 003–672; DHC-8-202 003–672; DHC-8-301 003–672; … |
| 2011-24-10 | Bombardier, Inc. Airplanes | Dec 16, 2011 | Airframe (DHC-8-202)Certain serial numbers: 003–on. Only with: FAA STC ST00753NY (TCCA STC SA97-106) installed. |
| 2011-21-04 | Bombardier Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes… | Nov 16, 2011 | Airframe (DHC-8-202)Certain serial numbers: 003–557. Only with: Equipped with cockpit door installation P/Ns 82510074 (all), 82510294 (all), 82510310-001, 8Z4597-001, H85250010 (all), 82510700 (all), or 82510704 (all except -502 and -503), per table 1 of this AD. |
| 2011-09-12 | Bombardier, Inc. Model DHC-8-101, -102, -103, -106, -201, -202, -301, -311, -315, -401… | Jun 6, 2011 | Airframe (DHC-8-202)Certain serial numbers: DHC-8-101 003–566; DHC-8-102 003–566; DHC-8-103 003–566; DHC-8-106 003–566; DHC-8-201 003–566; DHC-8-202 003–566; … |
| 2010-21-02 | Bombardier, Inc. Model DHC-8 Airplanes | Nov 12, 2010 | Airframe (DHC-8-202)Certain serial numbers: DHC-8-101 003–658; DHC-8-102 003–658; DHC-8-103 003–658; DHC-8-106 003–658; DHC-8-201 003–658; DHC-8-202 003–658; … |
| 2010-19-02 | Bombardier, Inc. Model DHC-8-200 and DHC-8-300 Series Airplanes | Oct 18, 2010 | Airframe (DHC-8-202)Certain serial numbers: 644–664 |
| 2010-04-12 | Bombardier, Inc. Model DHC-8-100 and DHC-8-200 Series Airplanes, and Model DHC-8-301… | Apr 8, 2010 | Airframe (DHC-8-202)Certain serial numbers: 003–on |
| 2004-20-01 | Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B… | Nov 5, 2004 | Engine (PW123)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
AFT RT EMERGENCY BETA LAMP FAILED BRIGHTNESS TEST. BETA LAMP ASSY REMOVED AND REPLACED REF AMM 33-51-00 REV 38 DATED MAY 15/17.
From FAA Service Difficulty Reports; matched by N-number and serial number.ACCOMPLISHED REPLACEMENT OF DOUBLER TO UPPER SKIN ON AIRSTAIR DOOR FOR DENT, REF BOMBARDIER RD 8-52-040 ISSUE 4 DATED 2014-06-05.
From FAA Service Difficulty Reports; matched by N-number and serial number.ACCOMPLISHED REPLACEMENT ON MAIN AIRSTAIR DOOR AFT EDGE MEMBER UPPER SECTION FOR CRACKS, REF STS EA 32-2018-078 REV IR DATED 06/15/2018.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE FUSELAGE SKIN AT BS 240.5 BETWEEN STRINGERS 29P & 30P WAS DENTED. REPAIRED IAW EA 42-2018-040, REV A-P2.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT LOWER SURFACE OF THE HORIZONTAL STABILIZER 15.5 INCHES INBD FROM OTBD EDGE AND 6.5 INCHES FWD OF AFT EDGE WAS DENTED. ACCOMPLISHED DOUBLER REPAIR IAW EA 45-2018-074, REV IR.
From FAA Service Difficulty Reports; matched by N-number and serial number.BS 293 TO 321.85, STRINGER 24S WAS DENTED. ACCOMPLISHED A DOUBLER AND TRIPLER REPAIR IAW EA 42-2018-041, REV B.
From FAA Service Difficulty Reports; matched by N-number and serial number.SKIN DENTED AT BS 307.5, STRINGER 26S+1.60/ SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-041, REV B.
From FAA Service Difficulty Reports; matched by N-number and serial number.SKIN DENTED AT BS 321.6, STRINGER 24S-3.5, SUCCESSFULLY REFORMED BACK TO ORIGINAL CONTOUR WITH NO INDICATIONS FOR CRACKS AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-041, REV B.
From FAA Service Difficulty Reports; matched by N-number and serial number.SKIN PANEL DENTED ON THE RT AILERON TRIM TAB. REPAIRED IAW SRM 51-42-45.
From FAA Service Difficulty Reports; matched by N-number and serial number.ACCOMPLISHED A SKIN REPLACEMENT AND SPLICE 10.8 INCH X 1.70 INCH ON THE RT ELEVATOR SPRING TAB UPPER SURFACE, 2.5 INCHES INBD OF HINGE NR 2, 2.8 INCHES FWD OF THE T/E IAW RD 8-55-037, ISSUE 6.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 231 reports.