N355PH, cancelled Jan 24, 2013

Service difficulty reports · 223

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR QXEA200800697Oil System · overservicedPDX - 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)Jun 28, 2008 · N355PH · Dhav DHC8202 · Turbine Engine Oil SystemSDR QXEA200800418Intercostal · corrodedC4-CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL AT BELLY SKIN, JUST OB OF STRINGER 31P FROM STA X190 TO X201. REPAIRED IAW SRM. (K)Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800417Keelbeam · corrodedC4-CHECK- SUSPECT CORROSION ON BOTTOM OF VERT KEEL BEAM AT STR 31P AND STA X201. REPAIRED IAW SRM. (K)Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, KeelSDR QXEA200800425Hinge Fitting · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Door HingeSDR QXEA200800442Strut · chafedPDX 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 FPApr 18, 2008 · N355PH · Dhav DHC8202 · Main Landing Gear Strut/Axle/TruckSDR QXEA200800441Strut · chafedPDX 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 VEApr 18, 2008 · N355PH · Dhav DHC8202 · Main Landing Gear Strut/Axle/TruckSDR QXEA200800440Strut · chafedPDX 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 VApr 18, 2008 · N355PH · Dhav DHC8202 · Main Landing Gear Strut/Axle/TruckSDR QXEA200800424Casting · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Cargo/Baggage DoorsSDR QXEA200800426Fitting · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800423Stop Fitting · wornPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, StructureSDR QXEA200800421Seat Track · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800420Seat Track · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800419Seat Track · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800422Seat Track · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800415Fitting · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800416Floor Skin · corrodedPDX 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 CApr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800414Floor Skin · corrodedPDX 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 CRAApr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800413Support Bracket · crackedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800412Door · gougedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Cargo/Baggage DoorsSDR QXEA200800410Seat Track · corrodedPDX 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 Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800411Support Bracket · damagedPDX 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 OApr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800408Flap · chafedPDX 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 PApr 18, 2008 · N355PH · Dhav DHC8202 · Trailing Edge FlapsSDR QXEA200800409Seat Track · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800407Seat Track · corrodedPDX 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.Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200800405Keelbeam · corrodedPDX 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 Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, KeelSDR QXEA200800406Stringer · corrodedPDX 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. NEGLIGIApr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA200800404Structure · damagedPDX 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 Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, StructureSDR QXEA200800403Frame · corrodedPDX 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 -8Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, FrameSDR QXEA200800399Floorbeam · corrodedPDX 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" MATEApr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Floor BeamSDR QXEA200800401Structure · corrodedPDX 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, 51-00-0Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800402Structure · corrodedPDX 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, 51-00Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800400Structure · corrodedPDX 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 Apr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200800398Floorbeam · corrodedPDX 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 FOApr 18, 2008 · N355PH · Dhav DHC8202 · Fuselage Main, Floor BeamSDR QXEA200800389Unknown · odorSEA - 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. AIRCRAFApr 16, 2008 · N355PH · Dhav DHC8202 · Air Distribution SystemSDR QXEA200800388Smoke Detector · malfunctionedSEA - 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.Apr 16, 2008 · N355PH · Dhav DHC8202 · Smoke DetectionSDR QXEA200800377Door · openSEA - 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 REMAINApr 12, 2008 · N355PH · Dhav DHC8202 · DoorsSDR QXEA20080339Connector · damagedSEA - 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 REPLAMar 29, 2008 · N355PH · Dhav DHC8202 · Fire Protection System WiringSDR QXEA200800298Acm · malfunctionedPDX - 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 EXCHMar 16, 2008 · N355PH · Dhav DHC8202 · Cabin Cooling SystemSDR QXEA200800279Smoke Detector · false activationYKM - 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.Mar 9, 2008 · N355PH · Dhav DHC8202 · Smoke DetectionSDR QXEA200800229Indicator · smokePDX - 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 RADARFeb 26, 2008 · N355PH · Dhav DHC8202 · Weather Radar SystemSDR QXEA200800206Altimeter · malfunctionedSEA - 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.Feb 18, 2008 · N355PH · Dhav DHC8202 · Altimeter, Barometric/EncoderSDR QXEA200800179Servo · jammedPDX - 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 SEFeb 11, 2008 · N355PH · Dhav DHC8202 · Autopilot SystemSDR QXEA200702031Drain Mast · frozenRDM - 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 TEMPERDec 25, 2007 · N355PH · Dhav DHC8202 · Turbine Engine Combustion SectionSDR QXEA200701771Lamp · inoperativePDX - 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.Dec 1, 2007 · N355PH · Dhav DHC8202 · Flight Compartment LightingSDR QXEA200701342Blade · malfunctionedBOI 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.Aug 17, 2007 · N355PH · Dhav DHC8202 · Propeller Blade SectionSDR QXEA200700776Relay · malfunctionedSEA 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.May 9, 2007 · N355PH · Dhav DHC8202 · Propeller Feathering/ReversingSDR QXEA200700641Autofeather Sys · noneSEA 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. AIRCRApr 17, 2007 · N355PH · Dhav DHC8202 · Propeller Controlling SystemSDR QXEA200700395Unknown · odorSEA FLIGHT NR 2017, BURNING RUBBER ODOR FROM MAPCO, GALLEY EQUIPMENT INOP. MAINTENANCE PLACED MAPCO ON MEL.Mar 19, 2007 · N355PH · Dhav DHC8202 · Buffet/GalleysSDR QXEA200700127Transducer · malfunctionedPDX 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. OPERATIONAFeb 3, 2007 · N355PH · Dhav DHC8202 · Stall Warning SystemSDR QXEA200603228Latch · unsecureSEA - ON FLIGHT 2224, RETURNED TO GATE. ENGINE COWL NR 2 LATCH OPEN. MAINTENANCE SECURED LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Dec 23, 2006 · N355PH · Dhav DHC8202 · Engine Cowling System
Back to N355PH, cancelled Jan 24, 2013