# Service difficulty reports: N356PH, cancelled Jun 16, 2014

A list on [N356PH, cancelled Jun 16, 2014](https://openairdocs.org/deregistered/N356PH-2014-06-16.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 5 · 206 reports

- [SDR QXEA200800427](https://openairdocs.org/sdr/QXEA200800427.md): Indicator · failed · Apr 25, 2008 · N356PH · Dhav DHC8202 · Engine BMEP/Torque Indicating
  > PDX- FLIGHT 2011, RETURNED TO THE FIELD FOR A NR 1 ENGINE TORQUE SURGE. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRESSURE TRANSDUCER WITH NO HELP. THEN REPLACED THE PRESSURE INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVI
- [SDR QXEA200800348](https://openairdocs.org/sdr/QXEA200800348.md): Flap Track · worn · Mar 30, 2008 · N356PH · Dhav DHC8202 · Trailing Edge Flaps
  > PDX-C5 CHECK- LT NR 3 FLAP TRACK HAS SEVERAL AREAS OF WEAR ON THE LOWER HORIZONTAL TRACK UPPER SURFACE APPROX.500 INCHES BY.300 INCHES BY.010 DEEP. BLENDED AFFECTED AREAS ON NR 3 FLAP TRACK LOWER HORIZONTAL UPPER IAW RD8-57-987. HFEC INSPECTED BLENDED ARE
- [SDR QXEA200800352](https://openairdocs.org/sdr/QXEA200800352.md): Skin · corroded · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > UPPER COMM ANTENNA HAS CORROSION ON MOUNTING AREA ON ACFT SKIN. REMOVED LIGHT CORROSION IAW CPC MANUAL CHAPTER 4 AND SRM 51-20-11. NO MEASURABLE MATERIAL REMOVED. (S)
- [SDR QXEA200800351](https://openairdocs.org/sdr/QXEA200800351.md): Skin · damaged · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > BURNED RIVET AT STA X190.00 APPROX 1 INCH BELOW STR 4L. REMOVED RIVET AND FOUND DAMAGE LIMITED TO ONE RIVET ONLY. INSTALLED RIVET IAW D8-200 SRM 51-40-11. (S)
- [SDR QXEA200800347](https://openairdocs.org/sdr/QXEA200800347.md): Structure · corroded · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX-C5 CHECK. CORROSION ON FLANGE AT GALLEY OUTBOARD AFT ATTACH POINT AT STA X227.70. BLENDED SURFACE CORROSION APPROX.001 MATERIAL REMOVED IAW DHC 8 200 SRM. ETCHED, ALODINED AND PRIMED SURFACE IAW DHC 8 200 SRM 51-20-16. (S)
- [SDR QXEA200800345](https://openairdocs.org/sdr/QXEA200800345.md): Skin · corroded · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX-C5 CHECK- AFT BAG PIT UPPER SKIN AT A LIGHTENING HOLE HAS LIGHT CORROSION FORMING IN RECESS HOLE Z100 X557 AND 27L. BLENDED OUT CORROSION AND MEASURED BLENDED AREA IAW DASH 8 200 SRM 51-20-11. ALODINED, PRIMED, AND PAINTED BLENDED AREA IAW DHC 8 200 SRM
- [SDR QXEA200800368](https://openairdocs.org/sdr/QXEA200800368.md): Skin · damaged · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX-C4 CHECK - BURNT RIVET APPROX 6 INCHES AFT OF STA X160.500 & 3 INCHES OUTBOARD OF STR 4L. REPAIRED DAMAGE TO SKIN PER D8-200 RD8-53-137 PG 3 STEP 1. HFEC IAW PSM 1-82-7A PART 6 51-00-02 PER RD8-53-137. NO DEFECTS NOTED. (S)
- [SDR QXEA200800367](https://openairdocs.org/sdr/QXEA200800367.md): Flap Track · worn · Mar 30, 2008 · N356PH · Dhav DHC8202 · Trailing Edge Flaps
  > PDX-C4 CHECK - LT WING NR 5 FLAP TRACK OUTBOARD LOWER TRACK UPPER SURFACE HAS WEAR MARKS. BLENDED IAW RD8-57-989. HFEC INSPECTED IAW D8-200 NDTM PART 651-00-01. NO CRACKS NOTED. (S)
- [SDR QXEA200800357](https://openairdocs.org/sdr/QXEA200800357.md): Skin · dented · Mar 30, 2008 · N356PH · Dhav DHC8202 · Elevator, Plate/Skin
  > PDX-C4 CHECK FOUND DENT ON THE BOTTOM OF THE RT ELEVATOR AT STN YH92.20, APPROX 13 INCHES FWD OF THE AFT SPAR. FOUND OUT OF LIMITS IAW RD8-55-1448. HFEC INSP FOR CRACKS, NO CRACKS NOTED. REMOVED RIVETS, FABRICATED REPAIR DOUBLER IAW RD8-55-1930. INSTALLED
- [SDR QXEA200800358](https://openairdocs.org/sdr/QXEA200800358.md): Skin · damaged · Mar 30, 2008 · N356PH · Dhav DHC8202 · Elevator, Plate/Skin
  > PDX -C4 CHECK- FOUND A CREASE ON THE BOTTOM OF THE RT ELEVATOR AT STN YH94.20, APPROX 6 INCHES FWD OF THE AFT SPAR. CREASE IS APPROX 5.5 INCHES LONG. FOUND OUT OF LIMITS IAW RD8-55-1448. HFEC INSP FOR CRACKS, NO CRACKS NOTED. REMOVED RIVETS, FABRICATED REP
- [SDR QXEA20080344](https://openairdocs.org/sdr/QXEA20080344.md): Structure · corroded · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C5 CHECK, AFT BAGGAGE PIT Z100 X600 AND 27R THERE IS LIGHT CORROSION FORMING TOPSIDE AND UNDERSIDE OF THE NUTPLATE. REMOVED THE NUTPLATE AND BLENDED LIGHT CORROSION. AREA REMOVED WAS.005". ALODINED PRIMED AND PAINTED AREA.
- [SDR QXEA20080343](https://openairdocs.org/sdr/QXEA20080343.md): Structure · corroded · Mar 30, 2008 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C5 CHECK, AFT BAGGAGE PIT HAS LIGHT CORROSION AT Z100 X 600 AND 21L UNDERSIDE AT NUTPLATE. REMOVED NUTPLATE AND BLENDED MINOR SURFACE CORROSION. BLENDED AREA WITHIN LIMITS. ALODINED PRIMED AND PAINTED AREA.
- [SDR QXEA20080342](https://openairdocs.org/sdr/QXEA20080342.md): Bracket · loose · Mar 30, 2008 · N356PH · Dhav DHC8202 · Elevator Structure
  > PDX C5 CHECK - ELEVATOR BUMP STOP BRACKET IS LOOSE ON THE RIGHT SIDE WHERE IT ATTACHES TO THE HORIZ STAB. REMOVED THE JO-BOLTS AS REQUIRED. REPLACED FASTENERS PER INSTRUCTIONS IN RD 8-55-112.
- [SDR QXEA20080338](https://openairdocs.org/sdr/QXEA20080338.md): Warning Light · intermittent · Mar 28, 2008 · N356PH · Dhav DHC8202 · Fire Detection
  > SEA - ON TAXI, THE FIRE DETECTION LIGHT WAS FLASHING AND THE FAULT "B" LIGHT ILLUMINATED WITH A FLASHING INDICATION. RETURNED TO THE GATE AND PLACED THE SYSTEM ON MEL 26-1. AIRCRAFT RETURNED TO SERVICE. 4/5 MEL CLEARED BY PERFORMING A RESISTANCE AND QUANTIT
- [SDR QXEA200800019](https://openairdocs.org/sdr/QXEA200800019.md): Inverter · odor · Jan 7, 2008 · N356PH · Dhav DHC8202 · DC Generating System
  > PDX - FLIGHT 2172 - STRANGE ODOR FROM THE PRIMARY INVERTER. MAINTENANCE PLACED ON MEL 24-8. AIRCRAFT RETURNED TO SERVICE. REPLACED THE INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200701588](https://openairdocs.org/sdr/QXEA200701588.md): Warning Light · false activation · Oct 20, 2007 · N356PH · Dhav DHC8202 · Central Warning
  > RDM FLIGHT NR 2126, ON START UP NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. COMPLIED WITH SUPPLEMENTAL PROCEDURE ON DASH 8 FSM PAGE 7.3.11. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200700799](https://openairdocs.org/sdr/QXEA200700799.md): Pressure Switch · malfunctioned · May 16, 2007 · N356PH · Dhav DHC8202 · Elevator Control System
  > YVR FLIGHT NR 2035 - DURING NR 2 PROP TRANSITION FROM START/FEATHER TO 1200, RUD FULL PRESS CAUTION LIGHT INTERMITTENTLY ILLUMINATED SOMETIMES STAYING ON FOR A COUPLE OF MINUTES, SOMETIMES JUST A FEW SECONDS. REMOVED PANEL 322HR. CLED AIR FROM NR 2 RUDDER PC
- [SDR QXEA200700715](https://openairdocs.org/sdr/QXEA200700715.md): Computer · inoperative · May 3, 2007 · N356PH · Dhav DHC8202 · Autopilot System
  > PDX - ON FLIGHT 2211, ON CLIMB-OUT FO WAS HAND FLYING THE AIRCRAFT WHEN THE AUTOPILOT ENGAGED AND TURNED TO THE RIGHT. THE FO HIT THE DISENGAGE BUTTON ON THE YOKE AND THE AUTOPILOT DISENGAGED AND FLEW NORMALLY. AFTER THAT, THE FO WAS STARTING A SHALLOW RIGHT
- [SDR QXEA200700521](https://openairdocs.org/sdr/QXEA200700521.md): Switch · failed · Apr 7, 2007 · N356PH · Dhav DHC8202 · Propeller Feathering/Reversing
  > SEA - ON FLIGHT 2085, AUTO FEATHER SELECT LIGHT INDICATION FAILS TO ILLUMINATE UPON BEING DEPRESSED. MAINTENANCE REMOVED AND REPLACED THE AUTO FEATHER SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200700508](https://openairdocs.org/sdr/QXEA200700508.md): Lamp · inoperative · Apr 2, 2007 · N356PH · Dhav DHC8202 · Indicating/Recording System
  > PDX FLIGHT NR 2170, NR 2 TANK AUX PUMP LIGHT OUT. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200700392](https://openairdocs.org/sdr/QXEA200700392.md): Unknown · unknown · Mar 18, 2007 · N356PH · Dhav DHC8202 · Engine (Turbine/Turboprop)
  > PDX FLIGHT NR 2030 ON TAXI OUT, NR 1 ENGINE MANUAL CAUTION LIGHT ILLUMINATED DURING BETA BACKUP FIRST FLIGHT OF DAY CHECK. MAINTENANCE C/W REST PROCEDURE IAW AIRCRAFT FLIGHT STANDARDS MANUAL. CAUTION LIGHT EXTINGUISHED. NO DEFECT NOTED. NO PARTS REPLACED.
- [SDR QXEA200700247](https://openairdocs.org/sdr/QXEA200700247.md): Starter Gen · malfunctioned · Feb 26, 2007 · N356PH · Dhav DHC8202 · Starter-Generator
  > BOI FLIGHT NR 2192, DURING AFTER START FLOW WITH LEFT ENGINE FEATHERED WHEN TURNING MAIN BUSS TIE TO OFF AUX INVERTER CAUTION ILLUMINATED ALONG WITH SEVERAL ASSOCIATED ITEMS. MAINTENANCE REPLACED NR 1 STARTER/GENERATOR IAW AMM 80-10-11 TASK CARD 9801001. GRO
- [SDR QXEA200602955](https://openairdocs.org/sdr/QXEA200602955.md): Pump · malfunctioned · Nov 6, 2006 · N356PH · Dhav DHC8202 · Hydraulic Pump, Auxiliary
  > SEA FLIGHT NR 2162, NR 2 STANDBY HYDRAULIC PRESSURE GAUGE SHOW A READING BETWEEN 200-500 PSI. MAINTENANCE REPLACED NR 1 STANDBY HYDRAULIC PUMP UNIT IAW AMM 29-11-17, PAGE 401-405. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601849](https://openairdocs.org/sdr/QXEA200601849.md): Connector · dirty · Jul 17, 2006 · N356PH · Dhav DHC8202 · Fuel System Wiring
  > SEA FLIGHT 2024 LEFT FUEL TEMPERATURE HIGH. MAINTENANCE CLEANED CONNECTOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601730](https://openairdocs.org/sdr/QXEA200601730.md): Generator · malfunctioned · Jun 30, 2006 · N356PH · Dhav DHC8202 · AC Generation System
  > SEA FLIGHT 2016, NR 2 AC GENERATOR CAUTION. MAINTENANCE REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601215](https://openairdocs.org/sdr/QXEA200601215.md): Pump · malfunctioned · May 9, 2006 · N356PH · Dhav DHC8202 · Hydraulic Pump (Electric/Engine), Main
  > PDX FLIGHT NR 2246 - NR 2 HYDRAULIC PUMP CAUTION. MAINTENANCE REPLACED THE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200601200](https://openairdocs.org/sdr/QXEA200601200.md): Stringer · cracked · Apr 25, 2006 · N356PH · Dhav DHC8202 · Nacelle/Pylon, Frame/Spar/Rib
  > PDX - C4 LEFT NACELLE FINGERNAIL DECK STRINGERS CRACKED BOTTOM SIDE AND FORWARD. REPAIRED IAW DHC-8-200 SRM 51-40-11.
- [SDR QXEA200601124](https://openairdocs.org/sdr/QXEA200601124.md): Stop · worn · Apr 21, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 MAIN CABIN DOOR AFT BOTTOM STOP ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.
- [SDR QXEA200601123](https://openairdocs.org/sdr/QXEA200601123.md): Stop · worn · Apr 21, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 MAIN CABIN DOOR AFT TOP STOP GUIDE ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.
- [SDR QXEA200601122](https://openairdocs.org/sdr/QXEA200601122.md): Stop · worn · Apr 21, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 MAIN CABIN DOOR FORWARD TOP STOP GUIDE ON APERATURE IS WORN. REPAIRED IAW RD 8-53-3933, STEPS 4 - 7.
- [SDR QXEA200601121](https://openairdocs.org/sdr/QXEA200601121.md): Stop · worn · Apr 21, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 MAIN CABIN DOOR FORWARD BOTTOM STOP ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.
- [SDR QXEA200601184](https://openairdocs.org/sdr/QXEA200601184.md): Access Panel · corroded · Apr 20, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 LAV ACCESS CUTOUT, THE LOWER EDGE HAS CORROSION AROUND ONE FASTENER. REPAIRED IAW DHC-8-200 SRM 51-20-11, RD 8-53-3299 AND HORIZON AIR EA 2-53-736.
- [SDR QXEA200601182](https://openairdocs.org/sdr/QXEA200601182.md): Stringer · corroded · Apr 20, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer
  > PDX - C4 THERE IS CORROSION ON STRINGER 31L ABOUT 4" FORWARD OF PILOT BULKHEAD X102.00. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20-36.
- [SDR QXEA200601189](https://openairdocs.org/sdr/QXEA200601189.md): Skin · dented · Apr 19, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX - C4 DENT ON LEFT FUSELAGE (UNDER LEFT ICE SHIELD) APPROXIMATELY STATION X303.0, Z156.5. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-16, 51-20-36, AND HORIZON AIR EA 2-53-541.
- [SDR QXEA200601199](https://openairdocs.org/sdr/QXEA200601199.md): Sill · corroded · Apr 19, 2006 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C4 MAIN CABIN DOOR SILL HAS CORROSION ON UPPER AND LOWER SURFACE. REPAIRED IAW DHC-8-200 SRM 51-00-01, 51-20-16 AND 51-20-36.
- [SDR QXEA200601188](https://openairdocs.org/sdr/QXEA200601188.md): Skin · dented · Apr 19, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX - C4 DENT ON LEFT SIDE OF FUSELAGE (UNDER LEFT ICE SHIELD) APPROXIMATELY STATION X301.0 Z158.0. REPAIRED IAW RD 8-53-7988, DHC-8-200 SRM 51-20-16, 50-20-36, 51-40-11 AND HORIZON AIR EA 2-53-541.
- [SDR QXEA200601185](https://openairdocs.org/sdr/QXEA200601185.md): Galley Track · corroded · Apr 19, 2006 · N356PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C4 CORROSION ON GALLEY OUTBOARD MOUNT TRACK JUST FORWARD OF RIGHT EMERGENCY DOOR, AROUND RIVET HOLES. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20-36, RD 8-53-9027 AND HORIZON AIR EA 2-53-739.
- [SDR QXEA200601193](https://openairdocs.org/sdr/QXEA200601193.md): Door Frame · corroded · Apr 18, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 CORROSION ON AFT LOWER PASSENGER DOOR FRAME. JUST FORWARD OF FRAME 253.4. REPAIRED IAW DHC-8-200 SRM 51-20-11, 2C (3), PAGE 7.
- [SDR QXEA200601119](https://openairdocs.org/sdr/QXEA200601119.md): Panel · chafed · Apr 18, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX - C4 REAR MATING SURFACE ON AIRCRAFT FOR PANEL 261NT HAS CHAFED AREA IN CENTER SECTION. REPAIRED IAW RD 8-57-1441 AND AMM 53-50-01.
- [SDR QXEA200601126](https://openairdocs.org/sdr/QXEA200601126.md): Skin · chipped · Apr 17, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX - C4 THERE IS PAINT CHIPPING AND GOUGING WHERE THE CARGO NET HAS HIT THE FUSELAGE SKIN BETWEEN STRINGER 26L AND 27L, FUSELAGE STATION 539.00 AND 549.00. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20-26, PAGE 7.
- [SDR QXEA200601183](https://openairdocs.org/sdr/QXEA200601183.md): Skin · gouged · Apr 17, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX - C4 THERE IS GOUGING WHERE THE CARGO NRT HAS HIT THE FUSELAGE SKIN AT STRINGER 29L, FUSELAGE STATION 590.000 TO 597.000. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20-26, PAGE 7, PARAGRAPH 5 1-4.
- [SDR QXEA200601125](https://openairdocs.org/sdr/QXEA200601125.md): Panel · chafed · Apr 16, 2006 · N356PH · Dhav DHC8202 · Wing, Plate/Skin
  > PDX - C4 RIGHT INBOARD WING LOWER INBOARD FLANGE FOR LEADING EDGE PANEL 611AR CHAFED. REPAIRED IAW RD 8-57-811, ISSUE 3, PAGE 4 STEPS 4-7.
- [SDR QXEA200601129](https://openairdocs.org/sdr/QXEA200601129.md): Stringer · corroded · Apr 16, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer
  > PDX - C4 CORROSION ON STRINGER 31 AT FRAME 202.75, FORWARD SIDE AROUND RIVETS. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-41.
- [SDR QXEA200601120](https://openairdocs.org/sdr/QXEA200601120.md): Attach Angle · cracked · Apr 16, 2006 · N356PH · Dhav DHC8202 · Wing, Attach Fittings
  > PDX - C4 CENTER MOUNT ANGLE FOR WING DEICE TEE DUCT IS CRACKED AT RIGHT HAND END. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND 51-40-00.
- [SDR QXEA200601118](https://openairdocs.org/sdr/QXEA200601118.md): Riser · corroded · Apr 16, 2006 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C4 CARGO FLOOR RISER MACHINED DIAGONAL STIFFENER AT LOWER AFT CORNER OF DOOR OPENING, IS CORRODED ON BOTTOM SIDE AT 90 DEGREE RADIUS. REPAIRED IAW DHC-8-200 SRM 51-40-00.
- [SDR QXEA200601194](https://openairdocs.org/sdr/QXEA200601194.md): Web · corroded · Apr 15, 2006 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C4 CORROSION AROUND SCREW HOLE ON TOP OF CARGO FLOOR WEB AT Y36L, X548. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36 AND 51-20-56.
- [SDR QXEA200601195](https://openairdocs.org/sdr/QXEA200601195.md): Web · corroded · Apr 15, 2006 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C4 CORROSION AROUND SCREW HOLE ON TOP OF CARGO FLOOR WEB AT Y20L, X555. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36 AND 51-20-56.
- [SDR QXEA200601191](https://openairdocs.org/sdr/QXEA200601191.md): Riser · corroded · Apr 15, 2006 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C4 CARGO FLOOR RISER BOTTOM FLANGE CORRODED ON TOP FORM Y0 TO Y30, RIGHT SIDE. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36 AND SRM 51-20-56.
- [SDR QXEA200601197](https://openairdocs.org/sdr/QXEA200601197.md): Fitting · corroded · Apr 15, 2006 · N356PH · Dhav DHC8202 · Fuselage Main, Attach Fittings
  > PDX - C4 CORROSION ON UPPER CARGO FLOOR DECK AROUND SCREW HOLE JUST INBOARD OF AFT WALL BOTTOM LEFT HAND MOUNT FITTING AT Y21L, X649. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16, 51-20-36 AND 51-20-56.
- [SDR QXEA200601190](https://openairdocs.org/sdr/QXEA200601190.md): Floor Support · corroded · Apr 15, 2006 · N356PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C4 CORRODED NUT PLATE ON BOTTOM CARGO FLOOR SUPPORT, AFT LEFT CORNER OF 144BZ. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-16, 51-20-36 AND SRM 51-20-56.

Next page: https://openairdocs.org/deregistered/N356PH-2014-06-16/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 = 'N356PH' AND deregistration_id = 'N356PH-2014-06-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N356PH-2014-06-16/reports

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