# Service difficulty reports: N358PH, cancelled Jan 28, 2019

A list on [N358PH, cancelled Jan 28, 2019](https://openairdocs.org/deregistered/N358PH-2019-01-28.md).

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

Page 1 of 9 · 429 reports

- [SDR A8ZR20180817001](https://openairdocs.org/sdr/A8ZR20180817001.md): Skin · dented · Aug 11, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Striker · out of limits · Jun 27, 2018 · N358PH · Dhav DHC8202 · Nacelle/Pylon, Main Frame
  > 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.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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. CONSIDRERED ACCEPTABLE REF STS EA 42-2018-055 REV B DATED 04/19/2018.
- [SDR A8ZR20180821005](https://openairdocs.org/sdr/A8ZR20180821005.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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. CONSIDRERED ACCEPTABLE REF STS EA 42-2018-055 REV B DATED 04/19/2018.
- [SDR A8ZR20180821004](https://openairdocs.org/sdr/A8ZR20180821004.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 7, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 4, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 3, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · May 2, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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 ACCEPTABLE IAW EA 41-2018-045 REV B.
- [SDR A8ZR20180822001](https://openairdocs.org/sdr/A8ZR20180822001.md): Skin · dented · May 2, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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 IAW EA 42-2018-045, REV B.
- [SDR A8ZR20180822003](https://openairdocs.org/sdr/A8ZR20180822003.md): Skin · dented · May 2, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · damaged · May 2, 2018 · N358PH · Dhav DHC8202 · Passenger/Crew Doors
  > 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 FWD EDGE & 11.5" BELOW UPPER EDGE REF STS EA 42-2018-056 REV A DATED 04/30/2018.
- [SDR A8ZR20180827001](https://openairdocs.org/sdr/A8ZR20180827001.md): Skin · dented · Apr 25, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 23, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 20, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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" AND.031" CONSIDERED ACCEPTABLE REF EA 42-2018-059 REV A.
- [SDR A8ZR20180823003](https://openairdocs.org/sdr/A8ZR20180823003.md): Skin · dented · Apr 19, 2018 · N358PH · Dhav DHC8202 · Wing, Plate/Skin
  > 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 X 1.25"W X.045"D CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-052, REV ORIGINAL.
- [SDR A8ZR20180820001](https://openairdocs.org/sdr/A8ZR20180820001.md): Skin · dented · Apr 19, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 19, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 19, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 17, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Skin · dented · Apr 13, 2018 · N358PH · Dhav DHC8202 · Nacelle/Pylon, Plate/Skin
  > 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 OF 1.7"L X 1.7"W X.011"D WITH NO CRACKS NOTED AND MATERIAL OFFSET TO COMPLY WITH SRM 54-00-16, AL
- [SDR A8ZR20180823008](https://openairdocs.org/sdr/A8ZR20180823008.md): Panel · torn · Apr 9, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Structure
  > 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 ORIGINAL.
- [SDR A8ZR20180823001](https://openairdocs.org/sdr/A8ZR20180823001.md): Skin · dented · Apr 9, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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 EA 30-2018-048 REV A.
- [SDR A8ZR20180817002](https://openairdocs.org/sdr/A8ZR20180817002.md): Skin · dented · Apr 4, 2018 · N358PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > 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.md): Shroud · damaged · Mar 27, 2018 · N358PH · Dhav DHC8202 · Wing Miscellaneous Structure
  > 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.md): Inlet · chafed · Mar 8, 2018 · N358PH · Dhav DHC8202 · Turbine Engine Air Inlet Section
  > 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 AND IS IN A SERVICEABLE CONDITION FOR CONTINUED OPERATION SUBJECT TO PERFORM MAINTENANCE NECESSARY TO
- [SDR JJBA20170607006](https://openairdocs.org/sdr/JJBA20170607006.md): Connector · unsecure · Jun 7, 2017 · N358PH · Dhav DHC8202 · Light System Wiring
  > 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.md): Cover · unsecure · May 3, 2017 · N358PH · Dhav DHC8202 · Emergency Exits
  > EMERGENCY EXIT HANDLE COVER AT SEAT 18A LOOSE. SECURED THE EMERGENCY EXIT HANDLE COVER AS REQUIRED.
- [SDR JJBA20170404004](https://openairdocs.org/sdr/JJBA20170404004.md): Light · unknown · Apr 4, 2017 · N358PH · Dhav DHC8202 · Emergency Lighting
  > 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.md): Bushing · worn · Feb 25, 2017 · N358PH · Dhav DHC8202 · Rudder Structure
  > FORE RUDDER HAS DROPPED, RUDDER HINGES AND VERTICAL STABILIZER REAR SPAR HINGES FITS AND CLEARANCE GAPS NOT WITHIN ALLOWABLE ACCEPTABLE LIMITATIONS OUTLINED IN AMM 55-40-11. TOP AND BOTTOM FORE RUDDER FAILSAFE HINGES ZERO GAP. HINGE PIVOTING ON HINGE, METAL
- [SDR JJBA20170302002](https://openairdocs.org/sdr/JJBA20170302002.md): Support Bracket · cracked · Feb 25, 2017 · N358PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET CRACKED. THE SUPPORT BRACKET WAS REPLACED.
- [SDR JJBA20170302001](https://openairdocs.org/sdr/JJBA20170302001.md): Bracket · chafed · Feb 24, 2017 · N358PH · Dhav DHC8202 · Rudder Structure
  > 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.md): Connector · dirty · Nov 15, 2016 · N358PH · Dhav DHC8202 · Light System Wiring
  > 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.md): Wire · disconnected · Aug 9, 2016 · N358PH · Dhav DHC8202 · Flight Control System Wiring
  > 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 TIME.
- [SDR JJBA20160720004](https://openairdocs.org/sdr/JJBA20160720004.md): Hydraulic System · low · Jul 20, 2016 · N358PH · Dhav DHC8202 · Hydraulic System, Main
  > 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 CYCLING TEST OF HYDRAULIC SYSTEM NO LEAKS NOTED. OPS CHECK SAT.
- [SDR JJBA20160712003](https://openairdocs.org/sdr/JJBA20160712003.md): Tscu · inoperative · Jul 12, 2016 · N358PH · Dhav DHC8202 · Engine BMEP/Torque Indicating
  > NR 2 ENGINE FEATHERED UNCOMMANDED. POWER UPTRIM ILLUMINATED. WHEN THE POWER WAS RETARDED THE PROP UNFEATHERED. WITH THE SYS DESELECTED, OFF AND POWER APPLIED THE ENGINE/PROP OPERATE NORMALLY. DEFERRED IAW MEL. R&R TSCU. OPS CHECK SAT. MEL CLOSED.
- [SDR JJBA20160622010](https://openairdocs.org/sdr/JJBA20160622010.md): Seal · out of position · Jun 22, 2016 · N358PH · Dhav DHC8202 · Passenger Compartment Windows
  > INNER WINDOW SEAL POPPED OUT AT 4AB INFLIGHT. SECURED WINDOW PANE, NO OTHER DEFECTS.
- [SDR JJBA20160304002](https://openairdocs.org/sdr/JJBA20160304002.md): Sign · inoperative · Mar 4, 2016 · N358PH · Dhav DHC8202 · Emergency Lighting
  > 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.md): Seat Track · corroded · Nov 4, 2015 · N358PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Seat Track · corroded · Nov 4, 2015 · N358PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Smoke Detector · faulty · Apr 25, 2015 · N358PH · Dhav DHC8202 · Smoke Detection
  > CARGO SMOKE WARNING LIGHT FLASHED. R & R FWD & AFT BAGGAGE SMOKE DETECTORS.

Next page: https://openairdocs.org/deregistered/N358PH-2019-01-28/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N358PH' AND deregistration_id = 'N358PH-2019-01-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N358PH-2019-01-28/reports

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