# N358PH: 1998 Dehavilland DHC-8-202, registration cancelled 2019-01-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 28, 2019
- Exported to: Guernsey
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-202](https://openairdocs.org/model/dehavilland-dhc-8-202) (registry code 2809007)
- Engine: [Pratt & Whitney Canada PW123](https://openairdocs.org/engine/pratt-whitney-canada-pw123) (registry code 52129)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 506
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: January 29, 1998
- Certificate issued: October 18, 2011
- Last registry action: May 9, 2018
- Mode S code: A403D2
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N358PH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=358PH
- Page: https://openairdocs.org/deregistered/N358PH-2019-01-28

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 Dehavilland DHC-8-202: https://openairdocs.org/model/dehavilland-dhc-8-202.md

## Service difficulty reports (429, newest 50)

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

- [SDR A8ZR20180817001](https://openairdocs.org/sdr/A8ZR20180817001), Aug 11, 2018: SKIN. DENTED. DENT FOUND AT BS331, STRINGER 31L. REFORMED THE DENT AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-061, REV. A.
- [SDR A8ZR20180823007](https://openairdocs.org/sdr/A8ZR20180823007), Jun 27, 2018: STRIKER. OUT OF LIMITS. ACCOMPLISHED RE-CONTOUR OF NR 2 ENGINE I/B COWL DOOR NACELLE STRIP-STRIKER FOR THE UPPER EDGE OF THE DOOR IAW EA 43-2018-083, REV A.
- [SDR A8ZR20180821002](https://openairdocs.org/sdr/A8ZR20180821002), May 7, 2018: SKIN. DENTED. DENT ON FUSELAGE AT STA 328.5 & S13P+6" THAT MEASURES .50"L X .9"W X .006"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH NO OFFSETS TO MATERIAL THICKNESS. CON
- [SDR A8ZR20180821005](https://openairdocs.org/sdr/A8ZR20180821005), May 7, 2018: SKIN. DENTED. DENT ON FUSELAGE AT BS 330 & S13P+3. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055 REV B.
- [SDR A8ZR20180821003](https://openairdocs.org/sdr/A8ZR20180821003), May 7, 2018: SKIN. DENTED. DENT ON FUSELAGE AT STA 327.5 & S13P+8.5" THAT MEASURES .90"L X .9"W X .006"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH NO OFFSETS TO MATERIAL THICKNESS. C
- [SDR A8ZR20180821004](https://openairdocs.org/sdr/A8ZR20180821004), May 7, 2018: SKIN. DENTED. DENT ON FUSELAGE AT BS 332 & S11P+6.25. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055 REV B.
- [SDR A8ZR20180820012](https://openairdocs.org/sdr/A8ZR20180820012), May 7, 2018: SKIN. DENTED. SKIN DENTED AT BS 331.5, STRINGER 16P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055, REV B.
- [SDR A8ZR20180820009](https://openairdocs.org/sdr/A8ZR20180820009), May 7, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 330.5, STRINGER 11P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW 42-2018-055, REV B.
- [SDR A8ZR20180820008](https://openairdocs.org/sdr/A8ZR20180820008), May 7, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED, BS 328, STRINGER 11P. REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055, REV B.
- [SDR A8ZR20180809001](https://openairdocs.org/sdr/A8ZR20180809001), May 7, 2018: SKIN. DENTED. FUSELAGE SKIN AT BS 328, STRINGER 11L WAS FOUND DENTED. COLD WORKED TO ORIGINAL CONTOUR AND ACCOMPLISHED NDT WITH NO CRACKS NOTED IAW EA 42-2018-055, REV B.
- [SDR A8ZR20180820010](https://openairdocs.org/sdr/A8ZR20180820010), May 4, 2018: SKIN. DENTED. SKIN DENTED AT BS 332, STRINGER 11P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-055 REV B.
- [SDR A8ZR20180820011](https://openairdocs.org/sdr/A8ZR20180820011), May 3, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 329, STRINGER 16P. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 42-2018-055 REV B.
- [SDR A8ZR20180822004](https://openairdocs.org/sdr/A8ZR20180822004), May 2, 2018: SKIN. DENTED. DENT AT BS 313.5, STRINGER 25S-1.15" THAT MEASURES 1.0"L X .85"W X .011"D REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTAB
- [SDR A8ZR20180822001](https://openairdocs.org/sdr/A8ZR20180822001), May 2, 2018: SKIN. DENTED. DENT FOUND AT BS 310, STRINGER 25S -1.5, MEASURES .70 L X .65 W X .004 D. REFORMED TO OROGONAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING CONSIDERED ACCEPTABLE I
- [SDR A8ZR20180822003](https://openairdocs.org/sdr/A8ZR20180822003), May 2, 2018: SKIN. DENTED. DENT AT BS 311.25, STRINGERS 24R & 25R. REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLEREF STS EA 41-2018-045 REV B.
- [SDR A8ZR20180821006](https://openairdocs.org/sdr/A8ZR20180821006), May 2, 2018: SKIN. DAMAGED. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER ON MAIN CABIN DOOR UPPER SECTION FOR DENTS 4.75" BELOW UPPER EDGE AND 5.75" FWD OF AFT EDGE AND MAIN CABIN DOOR FW
- [SDR A8ZR20180827001](https://openairdocs.org/sdr/A8ZR20180827001), Apr 25, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 102.2, STRINGER 24P. REFORMED AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-044, REV A.
- [SDR A8ZR20180820007](https://openairdocs.org/sdr/A8ZR20180820007), Apr 23, 2018: SKIN. DENTED. DENT FOUND ON THE CROWN SKIN, BS 325, 2L+4. REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020, REV A.
- [SDR A8ZR20180820006](https://openairdocs.org/sdr/A8ZR20180820006), Apr 23, 2018: SKIN. DENTED. DENT FOUND ON THE CROWN SKIN AT BS 317.50, STRINGER 2P+5.25. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020 REV A DATED 04/19/2018.
- [SDR A8ZR20180820003](https://openairdocs.org/sdr/A8ZR20180820003), Apr 23, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 301.5, S2P+7. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 42-2018-053.
- [SDR A8ZR20180820005](https://openairdocs.org/sdr/A8ZR20180820005), Apr 23, 2018: SKIN. DENTED. DENT FOUND ON THE CROWN FUSELAGE SKIN AT BS 311.75, STRINGER 3L +1.35. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW EA 38-2018-020, REV A.
- [SDR A8ZR20180820004](https://openairdocs.org/sdr/A8ZR20180820004), Apr 23, 2018: SKIN. DENTED. FUSELAGE SKIN CROWN DENTED AT BS 307.5, STRINGER 2+3.5. REFORMED TO ORIGINAL CONTOUR IAW 42-2018-053, REV A.
- [SDR A8ZR20180820002](https://openairdocs.org/sdr/A8ZR20180820002), Apr 23, 2018: SKIN. DENTED. DENT ON THE CROWN FUSELAGE SKIN AT BS 318.25, STRINGER 2L -4" REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-053 REV A.
- [SDR A8ZR20180821007](https://openairdocs.org/sdr/A8ZR20180821007), Apr 20, 2018: SKIN. DENTED. DENT ON FUSELAGE AT BS 215.5 & S11P THAT MEASURES 4.50"L X 3.30"W X .009"D SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR WITH REMAINING MATERIAL THICKNESS OF 030" A
- [SDR A8ZR20180823003](https://openairdocs.org/sdr/A8ZR20180823003), Apr 19, 2018: SKIN. DENTED. DENT FOUND ON THE RT WING LOWER SURFACE AT YW 88.600 & 2 INCHES AFT OF REAR SPAR THAT MEASURES 1.625"L X 1.25"W X .056"D. REFORMED TO NEW MEASUREMENT OF 1.60"L 
- [SDR A8ZR20180820001](https://openairdocs.org/sdr/A8ZR20180820001), Apr 19, 2018: SKIN. DENTED. DENT WAS FOUND AT BS 418.25, STRINGER 31L. REFORMED TO ORIGINAL CONTOUR IAW EA 32-2018-050, REV B.
- [SDR A8ZR20180817005](https://openairdocs.org/sdr/A8ZR20180817005), Apr 19, 2018: SKIN. DENTED. DENT FOUND AT BS 414.5, STRINGER 31L-3. REFORMED TO ORIGINAL CONTOUR IAW EA 32-2018-050, REV B.
- [SDR A8ZR20180817004](https://openairdocs.org/sdr/A8ZR20180817004), Apr 19, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 408.5, STRINGER 31P. ACCOMPLISHED INSTALLATION OF EXTERNAL DOUBLER IAW EA 32-2018-050, REV B.
- [SDR A8ZR20180823002](https://openairdocs.org/sdr/A8ZR20180823002), Apr 17, 2018: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 753.9, BETWEEN STRINGERS 12P AND 13P. REPAIRED IAW EA 42-2018-063, REV ORIGINAL.
- [SDR A8ZR20180823005](https://openairdocs.org/sdr/A8ZR20180823005), Apr 13, 2018: SKIN. DENTED. A DENT WAS FOUND ON THE NR 2 LOWER NACELLE SKIN AT XN 177.0 JUST ABOVE THE SKIN DOUBLER REPAIR THAT MEASURES 1.5"L X .75"W X .050"D. REFORMED TO NEW MEASUREMENT
- [SDR A8ZR20180823008](https://openairdocs.org/sdr/A8ZR20180823008), Apr 9, 2018: PANEL. TORN. ACCOMPLISHED INSTALLATION OF INTERNAL DOUBLER AND FILLER, OF TORN METAL ON FUSELAGE AT PANEL 112BR CUTOUT THAT MEASURES 1.32"L X .56"W, IAW EA 45-2018-034 REV O
- [SDR A8ZR20180823001](https://openairdocs.org/sdr/A8ZR20180823001), Apr 9, 2018: SKIN. DENTED. DENT AT BS 413, STRINGER 15P-3 THAT MEASURES 8.4"L X 3.0"W X .013"D REFORMED TO ORIGINAL CONTOUR WITH NO MATERIAL LOSS OR CRACKING AND CONSIDERED ACCEPTABLE IAW
- [SDR A8ZR20180817002](https://openairdocs.org/sdr/A8ZR20180817002), Apr 4, 2018: SKIN. DENTED. DENT FOUND AT BS 340 & STRINGER 31L. REFORMED TO ORIGINAL CONTOUR IAW EA 42-2018-061, REV A.
- [SDR A8ZR20180823004](https://openairdocs.org/sdr/A8ZR20180823004), Mar 27, 2018: SHROUD. DAMAGED. RIGHT UPPER SHROUD PANEL T/E AT APPROX. YW377 WAS DAMAGED. TRIMMED OUT DAMAGE AND PERFORMED TAP TEST WITH NO DEFECTS NOTED.
- [SDR A8ZR20180823006](https://openairdocs.org/sdr/A8ZR20180823006), Mar 8, 2018: INLET. CHAFED. NR 2 ENGINE, LT FRONT INLET CASE HAD CHAFE DAMAGE OF .053 INCH IN DEPTH. HAS BEEN DETERMINED THAT THE ENGINE CONTINUES TO COMPLY WITH ITS CERTIFICATION BASIS AN
- [SDR JJBA20170607006](https://openairdocs.org/sdr/JJBA20170607006), Jun 7, 2017: CONNECTOR. UNSECURE. FWD CEILING EMERGENCY LIGHT OVER AISLE INOPERATIVE. SECURED FWD OVERHEAD EMERGENCY EXIT SIGN LIGHT CONNECTOR PLUG 9811-P181. OPS CHECKED GOOD.
- [SDR JJBA20170503003](https://openairdocs.org/sdr/JJBA20170503003), May 3, 2017: COVER. UNSECURE. EMERGENCY EXIT HANDLE COVER AT SEAT 18A LOOSE. SECURED THE EMERGENCY EXIT HANDLE COVER AS REQUIRED.
- [SDR JJBA20170404004](https://openairdocs.org/sdr/JJBA20170404004), Apr 4, 2017: LIGHT. UNKNOWN. FRONT SERVICE DOOR EMERGENCY LIGHTS FLICKERED. PERFORMED EXTENSIVE OPS CHECK OF EMERGENCY LIGHTS, OPS TEST GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR JJBA20170302003](https://openairdocs.org/sdr/JJBA20170302003), Feb 25, 2017: BUSHING. WORN. FORE RUDDER HAS DROPPED, RUDDER HINGES AND VERTICAL STABILIZER REAR SPAR HINGES FITS AND CLEARANCE GAPS NOT WITHIN ALLOWABLE ACCEPTABLE LIMITATIONS OUTLINED IN 
- [SDR JJBA20170302002](https://openairdocs.org/sdr/JJBA20170302002), Feb 25, 2017: SUPPORT BRACKET. CRACKED. CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET CRACKED. THE SUPPORT BRACKET WAS REPLACED.
- [SDR JJBA20170302001](https://openairdocs.org/sdr/JJBA20170302001), Feb 24, 2017: BRACKET. CHAFED. FORE RUDDER TOP HINGE BRACKET HAS WEAR CHAFE DAMAGE ON TOP OF BRACKET UNDER BOLT HEAD ATTACHMENT. REPAIRED IAW RD 8-55-1128.
- [SDR JJBA20161115018](https://openairdocs.org/sdr/JJBA20161115018), Nov 15, 2016: CONNECTOR. DIRTY. FWD EMERGENCY LOWER HORIZONTAL LIGHT FLICKERS IN FLIGHT. CLEANED CONNECTION OPS CHECKED GOOD ON GROUND, NO DEFECTS NOTED.
- [SDR JJBA20160809007](https://openairdocs.org/sdr/JJBA20160809007), Aug 9, 2016: WIRE. DISCONNECTED. SPOILER NR 1, NR 2 ILLUMINATED ON TAKEOFF. INSP FOUND WIRES IN THE MICROSWITCH DISCONNECTED. RECONNECTED AND SPLICED WIRES. OPS CK SAT NO DEFECTS NOTED AT THIS 
- [SDR JJBA20160720004](https://openairdocs.org/sdr/JJBA20160720004), Jul 20, 2016: HYDRAULIC SYSTEM. LOW. POSSIBLE HYD LEAK NR 1 HYD SYS. QTY DROPPED FROM 1.9 TO 0.9 IN FLIGHT. SERVICED NR 1 HYD SYSTEM TO 2 QUARTS. PERFORMED ENGINE RUNS IAW 71-00-00 PERFORMED CYCLIN
- [SDR JJBA20160712003](https://openairdocs.org/sdr/JJBA20160712003), Jul 12, 2016: TSCU. INOPERATIVE. NR 2 ENGINE FEATHERED UNCOMMANDED. POWER UPTRIM ILLUMINATED. WHEN THE POWER WAS RETARDED THE PROP UNFEATHERED. WITH THE SYS DESELECTED, OFF AND POWER APPLIED TH
- [SDR JJBA20160622010](https://openairdocs.org/sdr/JJBA20160622010), Jun 22, 2016: SEAL. OUT OF POSITION. INNER WINDOW SEAL POPPED OUT AT 4AB INFLIGHT. SECURED WINDOW PANE, NO OTHER DEFECTS.
- [SDR JJBA20160304002](https://openairdocs.org/sdr/JJBA20160304002), Mar 4, 2016: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN BY FLIGHT ATTENDANT JUMP SEAT WILL NOT ILLUMINATE. R & R EMER EXIT SIGN, PN 2LA007344-80.
- [SDR JJBA20151104004](https://openairdocs.org/sdr/JJBA20151104004), Nov 4, 2015: SEAT TRACK. CORRODED. MULTIPLE SPOTS OF CORROSION ON THE RT SEAT RAIL & DRIP TRAY FROM FS 180-234.5. REPLACED RT SEAT RAIL IAW RD 8-53-3074.
- [SDR JJBA20151104003](https://openairdocs.org/sdr/JJBA20151104003), Nov 4, 2015: SEAT TRACK. CORRODED. MULTIPLE SPOTS OF CORROSION ON THE LT SEAT RAIL & DRIP TRAY FROM FS 180-234.5. REPLACED LT SEAT RAIL IAW RD 8-53-3074.
- [SDR JJBA20150425011](https://openairdocs.org/sdr/JJBA20150425011), Apr 25, 2015: SMOKE DETECTOR. FAULTY. CARGO SMOKE WARNING LIGHT FLASHED. R & R FWD & AFT BAGGAGE SMOKE DETECTORS.

All 429: https://openairdocs.org/deregistered/N358PH-2019-01-28/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020212004289I](https://openairdocs.org/incident/20020212004289I), Feb 12, 2002: Dhav DHC8202 (N358PH), Redmond, OR. (-23) During descent to rdm, smoke entered cabin with lav smoke alarm sounding. Flight initiated smoke evacuation procedures and notifed CFR@rdm. Aircraft…

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