# Service difficulty reports: N355PH, cancelled Jan 24, 2013

A list on [N355PH, cancelled Jan 24, 2013](https://openairdocs.org/deregistered/N355PH-2013-01-24.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 · 223 reports

- [SDR QXEA200800697](https://openairdocs.org/sdr/QXEA200800697.md): Oil System · overserviced · Jun 28, 2008 · N355PH · Dhav DHC8202 · Turbine Engine Oil System
  > PDX - CREW REPORTS OIL ODOR IN CABIN. FOUND ENGINE OIL FOR NR 1 OVER SERVICED. ADJUSTED LEVEL. GROUND RUN CHECKS OK. RETURNED TO SERVICE. NO PARTS REPLACED. (A)
- [SDR QXEA200800418](https://openairdocs.org/sdr/QXEA200800418.md): Intercostal · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > C4-CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL AT BELLY SKIN, JUST OB OF STRINGER 31P FROM STA X190 TO X201. REPAIRED IAW SRM. (K)
- [SDR QXEA200800417](https://openairdocs.org/sdr/QXEA200800417.md): Keelbeam · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Keel
  > C4-CHECK- SUSPECT CORROSION ON BOTTOM OF VERT KEEL BEAM AT STR 31P AND STA X201. REPAIRED IAW SRM. (K)
- [SDR QXEA200800425](https://openairdocs.org/sdr/QXEA200800425.md): Hinge Fitting · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Door Hinge
  > PDX C4 CHECK - MCD LAY SHAFT, AFT HINGE FITTING HAS PITTING AROUND BOLT HOLES. REMOVED MCD LAY SHAFT. SEPARATED LAYSHAFT AND DRILLED OUT AFT HINGE FITTING. DRILLED UP AND INSTALL NEW HINGE FITTING REF SRM 51-40-00. INSTALLED MCD LAY SHAFT.
- [SDR QXEA200800442](https://openairdocs.org/sdr/QXEA200800442.md): Strut · chafed · Apr 18, 2008 · N355PH · Dhav DHC8202 · Main Landing Gear Strut/Axle/Truck
  > PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE AT LOWER O/B SURFACE WHERE O/B WOW HARNESS CONDUIT HAS CONTACTED. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP. IAW -8/200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. PERFORMED FP
- [SDR QXEA200800441](https://openairdocs.org/sdr/QXEA200800441.md): Strut · chafed · Apr 18, 2008 · N355PH · Dhav DHC8202 · Main Landing Gear Strut/Axle/Truck
  > PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING MID ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP IAW -8/200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. PERFORMED FPI IAW -8/200 VE
- [SDR QXEA200800440](https://openairdocs.org/sdr/QXEA200800440.md): Strut · chafed · Apr 18, 2008 · N355PH · Dhav DHC8202 · Main Landing Gear Strut/Axle/Truck
  > PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING UPPER ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP. IAW -8/200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. PERFORMED FPI IAW -8/200 V
- [SDR QXEA200800424](https://openairdocs.org/sdr/QXEA200800424.md): Casting · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Cargo/Baggage Doors
  > PDX C4 CHECK. FWD CORNER CASTING ON MCD HAS CORROSION AROUND NUTPLATE, TOP AND BOTTOM. REMOVED FWD CORNER MCD CASTINGS AND INSTALL NEW CASTING REF -8 200 SRM 51-40-00 AND 51-40-11.
- [SDR QXEA200800426](https://openairdocs.org/sdr/QXEA200800426.md): Fitting · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK. TENSION FITTING LOCATED AT FRAME X201 STR 31S HAS CORROSION. REMOVED TENSION FITTING AND INSTALLED NEW FITTING IAW 8 200 SRM 51-40-11, 51-20-36.
- [SDR QXEA200800423](https://openairdocs.org/sdr/QXEA200800423.md): Stop Fitting · worn · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX C4 CHECK. MCD SURROUND STOP FITTINGS ALL HAVE SIGNS OF WEAR. BLENDED FITTINGS IAW -8 200 RD8-53-3933 PG 4, PARA 1.2. WITHIN LIMITS. INSPECTED AS PER RD8-53-3933 NO CRACKS NOTED. COLD GALV. PRIMED STOP FITTINGS IAW -8 200 RD8-53-3933 PG 4, PARA 4-7.
- [SDR QXEA200800421](https://openairdocs.org/sdr/QXEA200800421.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK. CORROSION ON SEAT TRACK NR 4 CAMLOCK RECEP. STA X222. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11 AND RD8-53-1102.
- [SDR QXEA200800420](https://openairdocs.org/sdr/QXEA200800420.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK. SURFACE CORROSION ON SEAT TRACK NR 7 BETWEEN STA X220 AND X226. REMOVED NR 7 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11 AND RD8-53-1102.
- [SDR QXEA200800419](https://openairdocs.org/sdr/QXEA200800419.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK. LT SEAT TRACK NR 2 HAS CORROSION AT APPROX STA 438 STA 466.5, STA 485, AND STA 498. REMOVED SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11.
- [SDR QXEA200800422](https://openairdocs.org/sdr/QXEA200800422.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK. CORROSION ON SEAT TRACK NR 1 AT APPROX. STA X360. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-00. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11.
- [SDR QXEA200800415](https://openairdocs.org/sdr/QXEA200800415.md): Fitting · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK FITTING CORRODED JUST AFT OF CARGO DOOR FUSELAGE CUTOUT, LOWER AFT CORNER. REMOVED CORRODED FITTING AT AFT LOWER CORNER IAW -8 200 SRM 51-40-11. INSTALLED NEW FITTING IAW -8 200 SRM 51-40-11 AND RD8-51-102.
- [SDR QXEA200800416](https://openairdocs.org/sdr/QXEA200800416.md): Floor Skin · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK CORROSION AT CARGO PIT DECK SKIN I/B AND BELOW CORNER FITTING STA X597.5, Y40.95. REMOVED CORROSION USING SCOTCH BRITE PAD IAW -8 200 SRM 51-40-11 AND CPM CHAP 4 PG25-26. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. UT THICKNESS C
- [SDR QXEA200800414](https://openairdocs.org/sdr/QXEA200800414.md): Floor Skin · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK CARGO PIT LOWER FLOOR DECK SKIN HAS CORROSION ALONG RIVET ROW AT STA X600 BETWEEN Y10L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI.040 LO.038. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRA
- [SDR QXEA200800413](https://openairdocs.org/sdr/QXEA200800413.md): Support Bracket · cracked · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK SUPPORT BRACKET UNDER MCD SILL IS CRACKED. R&R SUPPORT BRACKET WITH NEW FROM STOCK REF -8 200 SRM 51-40-11 FOR RIVETING.
- [SDR QXEA200800412](https://openairdocs.org/sdr/QXEA200800412.md): Door · gouged · Apr 18, 2008 · N355PH · Dhav DHC8202 · Cargo/Baggage Doors
  > PDX C4 CHECK CARGO DOOR HAS SEVERAL GOUGES ON CENTER FWD LOWER SIDE. REMOVED DAMAGE IAW -8 200 51-20-11. HFEC INSP IAW -8 200 NDTM PT6, 51-00-01 NO CRACKS NOTED. WITHIN LIMITS PER -8 200 52-00-16. ALODINED PRIMED IAW SRM 51-20-36.
- [SDR QXEA200800410](https://openairdocs.org/sdr/QXEA200800410.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK FUSELAGE INTERIOR WEB THAT TIES INTO LT O/B SEAT TRACK HAS AN OVERSIZED HOLE LOCATED 2" AFT OF FRAME 333.300. REMOVED WEB BETWEEN FRAMES 333.30 AND 354.25 NEXT TO LH O/B SEAT TRACK. FABRICATED NEW WEB IAW T/C 2-53-836. INSTALLED WEB IAW -8 200
- [SDR QXEA200800411](https://openairdocs.org/sdr/QXEA200800411.md): Support Bracket · damaged · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK LT O/B SEAT TRACK SUPPORT BRACKET ON FWD SIDE OF FRAME AT STA X333.3 HAS DAMAGED HOLE, 2ND HOLE AFT TOP. REMOVED LT O/B SEAT TRACK SUPPORT BRACKET FWD SIDE FRAME AT STA X3333.3. INSTALLED NEW BRACKET FROM STOCK AT LT O/B SEAT TRACK ON FWD SIDE O
- [SDR QXEA200800408](https://openairdocs.org/sdr/QXEA200800408.md): Flap · chafed · Apr 18, 2008 · N355PH · Dhav DHC8202 · Trailing Edge Flaps
  > PDX C4 CHECK RT O/B FLAP HAS A CHAFFED AREA AT THE O/B END APPROX 10" FROM THE TRAILING END. BLENDED ARE OF CHAFE, FOUND OUT OF LIMITS IAW -8 200 SRM 57-50-16. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 200 NDTM P
- [SDR QXEA200800409](https://openairdocs.org/sdr/QXEA200800409.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK BRACKET FOR NR 1 SEAT TRACK WEB AFT OF FRAME 354 IS DAMAGED. REMOVED BRACKET IAW -8 200 SRM 51-40-11. INSTALLED NEW BRACKET IAW -8 200 SRM 51-40-00, 51-40-11.
- [SDR QXEA200800407](https://openairdocs.org/sdr/QXEA200800407.md): Seat Track · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX C4 CHECK CORROSION ON RT O/B SEAT TRACK AT APPROX X488.5. BLENDED OUT CORROSION IAW RD8-53-10103. ALODINE PRIMED IAW -8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800405](https://openairdocs.org/sdr/QXEA200800405.md): Keelbeam · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Keel
  > PDX C4 CHECK SUSPECT CORROSION AT I/B BOTTOM OF VERTICAL KEELBEAM AT STA X370 AND STR 31P. REMOVED CORROSION AT BOTTOM OF VERTICAL KEEL BEAM STA 370.8. REF CPM CHAP 4 PG 4-25 PARA 9. ORIGINAL THICKNESS.050" REMAINING THICKNESS.046". MAX MATERIAL REMOVED
- [SDR QXEA200800406](https://openairdocs.org/sdr/QXEA200800406.md): Stringer · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer
  > PDX C4 CHECK CORROSION ON STR 23S (X387 TO X392) AND CONNECTING CLIP TO FRONT SPAR MAIN FRAME ON AFT SIDE AT X387.35. REMOVED LIGHT SURFACE FROM STRINGER AND CONNECTING CLIP USING SCOTCH BRITE PAD. ALODINED EXPOSED ALUM. IAW -8 200 CPM CHAP 4 AND 5. NEGLIGI
- [SDR QXEA200800404](https://openairdocs.org/sdr/QXEA200800404.md): Structure · damaged · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Structure
  > PDX C4 CHECK CORROSION ON FORE AND AFT LOWER CORNER COMBING PIECES, I/B FLANGE, ON PAX DOOR APERTURE LOWER EDGE. REMOVED NUTPLATE FROM CASTING AND REMOVED CORROSION. REMOVED.002" MATERIAL REF CPM SECT 4. WITH IN LIMITS PER -8 200 SRM 51-20-11. REINSTALLED
- [SDR QXEA200800403](https://openairdocs.org/sdr/QXEA200800403.md): Frame · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Frame
  > PDX C4 CHECK SUSPECT CORROSION OF FRA X201 AT STR 31S. REMOVED CORROSION IAW CPM CHAP 4 PARA 9A-B(1-6(A)). UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI.032 LOW.029. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. ALODINED PRIMED IAW -8
- [SDR QXEA200800399](https://openairdocs.org/sdr/QXEA200800399.md): Floorbeam · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Floor Beam
  > PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y20L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04, HI.083 LOW.061. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. REMOVED.022" MATE
- [SDR QXEA200800401](https://openairdocs.org/sdr/QXEA200800401.md): Structure · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y565 AND Y25L-Y27L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED.002 MATERIAL FROM ORIGINAL THICKNESS,.043 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-0
- [SDR QXEA200800402](https://openairdocs.org/sdr/QXEA200800402.md): Structure · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y546 AND Y35.5L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED.003 MATERIAL FROM.045 ORIGINAL THICKNESS,.042 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00
- [SDR QXEA200800400](https://openairdocs.org/sdr/QXEA200800400.md): Structure · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX C4 CHECK ZONE 144 SUBFLOOR TOP SURFACE IS CORRODED AT Y580-X581 AND Y24L-Y26L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED.002 MATERIAL FROM ORIGINAL THICKNESS..043 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200
- [SDR QXEA200800398](https://openairdocs.org/sdr/QXEA200800398.md): Floorbeam · corroded · Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Floor Beam
  > PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y29.5R. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04, HI.083 LOW.077. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. REMOVED.006" MATERIAL FO
- [SDR QXEA200800389](https://openairdocs.org/sdr/QXEA200800389.md): Unknown · odor · Apr 16, 2008 · N355PH · Dhav DHC8202 · Air Distribution System
  > SEA - LAVATORY SMOKE DETECTOR WENT OFF FOR THE SECOND TIME. NO SMOKE OR FIRE NOTED. ON THE FLIGHT DECK THOUGH NOTICED A ODOR IN THE AIR AND BOTH PILOTS SENSED A SCRATCHING IN THEIR THROATS. MAINTENANCE FOUND ENGINE OIL IN THE NR 1 LP FOR THE ENGINE. AIRCRAF
- [SDR QXEA200800388](https://openairdocs.org/sdr/QXEA200800388.md): Smoke Detector · malfunctioned · Apr 16, 2008 · N355PH · Dhav DHC8202 · Smoke Detection
  > SEA - LAVATORY SMOKE DETECTOR WENT OFF. NO EVIDENCE OF SMOKE, OR FIRE. MAINTENANCE COMPLIED WITH A OPERATIONAL CHECKS OF THE SYSTEM AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA200800377](https://openairdocs.org/sdr/QXEA200800377.md): Door · open · Apr 12, 2008 · N355PH · Dhav DHC8202 · Doors
  > SEA - AFTER TAKEOFF, TRIED TO RAISE THE GEAR AND THE GEAR DOOR LIGHTS WERE STILL ILLUMINATED ALONG WITH THE LEFT AND RIGHT UNSAFE LIGHTS. A LOUD FLAPPING SOUND WAS HEARD. VISUAL INSPECTION SHOWED THE GEAR TO STILL BE DOWN. CYCLED THE GEAR AND PROBLEM REMAIN
- [SDR QXEA20080339](https://openairdocs.org/sdr/QXEA20080339.md): Connector · damaged · Mar 29, 2008 · N355PH · Dhav DHC8202 · Fire Protection System Wiring
  > SEA - FLIGHT 2101 - LAVATORY SMOKE DETECTOR GOES OFF INTERMITTENTLY IN FLIGHT. MAINTENANCE PLACED ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED ON 3/31 BY CONNECTING THE PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLA
- [SDR QXEA200800298](https://openairdocs.org/sdr/QXEA200800298.md): Acm · malfunctioned · Mar 16, 2008 · N355PH · Dhav DHC8202 · Cabin Cooling System
  > PDX - FLIGHT 2193, ON APPROACH THE LAVATORY SMOKE DETECTOR WENT OFF TWICE. BOTH TIMES THE FLIGHT ATTENDANT REPORTED NO INDICATIONS OF SMOKE. AIR WAS SMOOTH AND THE BLEEDS WERE ON MAX. MAINTENANCE REPLACED THE AIR CYCLE MACHINE, CONDENSER/MIXER AND HEAT EXCH
- [SDR QXEA200800279](https://openairdocs.org/sdr/QXEA200800279.md): Smoke Detector · false activation · Mar 9, 2008 · N355PH · Dhav DHC8202 · Smoke Detection
  > YKM - FLIGHT 2002 - LAVATORY SMOKE DETECTOR WENT OFF WITH NO SMOKE DETECTED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. CLEARED BY REPLACING THE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200800229](https://openairdocs.org/sdr/QXEA200800229.md): Indicator · smoke · Feb 26, 2008 · N355PH · Dhav DHC8202 · Weather Radar System
  > PDX - FLIGHT 2058 - WHEN APPLYING ELECTRICAL POWER TO THE IRU AND FMS. SMOKE NOTICED FROM THE AREA BETWEEN THOSE UNITS AND THE RADAR INDICATOR. MAINTENANCE POWERED UP EACH UNIT ON IT'S OWN. THE RADAR DISPLAY (INDICATOR) STARTED TO SMOKE. REPLACED THE RADAR
- [SDR QXEA200800206](https://openairdocs.org/sdr/QXEA200800206.md): Altimeter · malfunctioned · Feb 18, 2008 · N355PH · Dhav DHC8202 · Altimeter, Barometric/Encoder
  > SEA - FLIGHT 2027, RETURNED TO THE FIELD FOR THE CAPTAIN'S ALTIMETER FLAGGING AT 420 FEET. MAINTENANCE REPLACED THE NR 1 ALTIMETER. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200800179](https://openairdocs.org/sdr/QXEA200800179.md): Servo · jammed · Feb 11, 2008 · N355PH · Dhav DHC8202 · Autopilot System
  > PDX - FLIGHT 2193 (OTH-PDX) ON APPROACH WITH THE AUTOPILOT ON, EXPERIENCED A UNCOMMANDED ROLL TO THE LEFT. AUTOPILOT WAS TURNED OFF AND THE WHEEL APPEARED TO BE JAMMED (NO MOVEMENT POSSIBLE). CONTROL THEN BECAME UN-JAMMED AND OPERATED NORMALLY AFTER A FEW SE
- [SDR QXEA200702031](https://openairdocs.org/sdr/QXEA200702031.md): Drain Mast · frozen · Dec 25, 2007 · N355PH · Dhav DHC8202 · Turbine Engine Combustion Section
  > RDM - FLIGHT 2191 - ON SHUTDOWN AT THE GATE, RAMP NOTICED SMOKE FROM THE TOP OF NR 1 ENGINE. MAINTENANCE CHECKED NACELLE AND ENGINE AREA AND FOUND NO SOURCE FOR THE SMOKE. FOUND SOME ICE IN THE COWL DRAIN MAST AND THAWED OUT. PERFORMED ENGINE RUNS AT TEMPER
- [SDR QXEA200701771](https://openairdocs.org/sdr/QXEA200701771.md): Lamp · inoperative · Dec 1, 2007 · N355PH · Dhav DHC8202 · Flight Compartment Lighting
  > PDX - FLIGHT 2011 - HEATER LIGHT ON LEFT ENGINE INTAKE BYPASS DOOR DOES NOT TEST. RETURNED TO THE GATE. MAINTENANCE REPLACED THE LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200701342](https://openairdocs.org/sdr/QXEA200701342.md): Blade · malfunctioned · Aug 17, 2007 · N355PH · Dhav DHC8202 · Propeller Blade Section
  > BOI FLIGHT NR 2115, SPARKS OBSERVICED FROM NR 2 PROP ON CLIMB-OUT. REPLACED BLADES NR 1 AND NR 4 ON NR 2 PROP PER TC 9611003. S/N 9801028-23, TSN 89.53, CSN 134. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200700776](https://openairdocs.org/sdr/QXEA200700776.md): Relay · malfunctioned · May 9, 2007 · N355PH · Dhav DHC8202 · Propeller Feathering/Reversing
  > SEA FLIGHT NR 2019 ON TAKEOFF, AUTOFEATHER FAILED TO ARM. REPLACED NR 1 POWER LEVER LIMIT SWITCH 6121-S7, ADJUSTED SWITCH. REPLACED RELAY 6121-K15. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200700641](https://openairdocs.org/sdr/QXEA200700641.md): Autofeather Sys · none · Apr 17, 2007 · N355PH · Dhav DHC8202 · Propeller Controlling System
  > SEA FLIGHT NR 2110 ON TAKEOFF, AUTOFEATHER SWITCH LIGHT DAR. TAKEOFF ABORTED AT 60KTS. MAINTENANCE PERFORMED AUTOFEATHER SYSTEM AND POWER UPTRIM TEST IAW -8200 ENGINE RIG MANUAL 6-8, PAGE 3-65, STEPS B1-13. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCR
- [SDR QXEA200700395](https://openairdocs.org/sdr/QXEA200700395.md): Unknown · odor · Mar 19, 2007 · N355PH · Dhav DHC8202 · Buffet/Galleys
  > SEA FLIGHT NR 2017, BURNING RUBBER ODOR FROM MAPCO, GALLEY EQUIPMENT INOP. MAINTENANCE PLACED MAPCO ON MEL.
- [SDR QXEA200700127](https://openairdocs.org/sdr/QXEA200700127.md): Transducer · malfunctioned · Feb 3, 2007 · N355PH · Dhav DHC8202 · Stall Warning System
  > PDX FLIGHT NR 2200, IMMEDIATELY AFTER TAKEOFF, NR 1 STALL WARNING CAUTION LIGHT ILLUMINATED STALL WARNING INOP. MAINTENANCE REPLACED THE NR 1 STALL WARNING TRANSDUCER. COMPLIED WITH FUNCTION TEST OF STALL WARNING SYSTEM IAW AMM 27-330-00-720-801. OPERATIONA
- [SDR QXEA200603228](https://openairdocs.org/sdr/QXEA200603228.md): Latch · unsecure · Dec 23, 2006 · N355PH · Dhav DHC8202 · Engine Cowling System
  > SEA - ON FLIGHT 2224, RETURNED TO GATE. ENGINE COWL NR 2 LATCH OPEN. MAINTENANCE SECURED LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N355PH-2013-01-24/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 = 'N355PH' AND deregistration_id = 'N355PH-2013-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N355PH-2013-01-24/reports

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