N353PH, cancelled Jul 25, 2011

Service difficulty reports · 200

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 = 'N353PH' AND deregistration_id = 'N353PH-2011-07-25'
  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 QXEA200800522Switch · brokenSEA - FLIGHT 2090 - JUST AFTER TAKEOFF, AND GEAR SELECTED UP, THE FIRST OFFICER USED THE RUDDER TRIM SWITCH, AND IN DOING SO, THE SWITCH BROKE TO THE RIGHT POSITION. RUDDER TRIM MOVED 3/4 TO THE RIGHT. CAPTAIN HELD THE TRIM SWITCH TO THE LEFT AND TRIM MOVEMEMay 25, 2008 · N353PH · Dhav DHC8202 · Rudder Tab Control SystemSDR QXEA200800393Unknown · unknownSEA - BRAKES ARE MUSHY. SIGNIFICANT EFFORT ON PEDALS RESULTS IN NO BRAKING. HIGH FORCE APPLIED TO PEDALS RESULTS IN ADEQUATE BRAKING. MAINTENANCE TAXIED THE AIRCRAFT WITH THE ANTI-SKID ON AND OFF WITH NO DEFECTS NOTED. BRAKING FORCES ARE NORMAL. COULD NOTApr 19, 2008 · N353PH · Dhav DHC8202 · Landing Gear Brake SystemSDR QXEA200800281Rod · brokenALW - UPON TRYING TO OPEN THE MAIN CABIN DOOR, THE GROUND CREW REPORTED THAT THE WERE UNABLE TO DO SO. MAINTENANCE ENTERED AIRCRAFT THROUGH THE CARGO DOOR AND FOUND THAT THE SUPPORTING ROD WAS BROKEN AT THE BASE. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX,Mar 8, 2008 · N353PH · Dhav DHC8202 · Passenger/Crew DoorsSDR QXEA200800057Spring · malfunctionedPDX - MAIN CABIN DOOR DIFFICULT TO OPEN. PDX MAINTENANCE REMOVED AND REPLACED MAIN CABIN DOOR GAS SPRINGS WITH NEW SPRINGS. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE.Feb 3, 2008 · N353PH · Dhav DHC8202 · Passenger/Crew DoorsSDR QXEA200701776Generator · malfunctionedRDM - EMERGENCY LIGHTS IN THE CABIN FLICKER SOMETIMES THROUGH THE DURATION OF THE FLIGHT. SOME LIGHTS ARE ON UP TO 5 SECONDS. THE LIGHTS THAT FLICKER ARE THE EXIT SIGNS AND OVERHEAD. MAINTENANCE REPLACED THE NR 2 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRNov 29, 2007 · N353PH · Dhav DHC8202 · Emergency LightingSDR QXEA200701767Power Supply · inoperativePDX - ON FLIGHT 2139, EMERGENCY LIGHTS IN CABIN FLICKER AFTER TAKEOFF. TURNING OFF THEN ON, ARM STOPS THE FLICKERING. LIGHTS FLICKERING ARE THE EXIT SIGNS AND OVERHEAD. MAINTENANCE REMOVED AND REPLACED PS3 AND PS4 POWER SUPPLIES AND BATTERY PACKS. OPERATIONov 28, 2007 · N353PH · Dhav DHC8202 · Emergency LightingSDR QXEA200701165None · nonePDX - FOUL ODOR THROUGHOUT CABIN AND FLIGHT DECK WORSE DURING TIMES PARKED AT GATE AND ALSO DURING APPROACH AND LANDING. CLEANED REFUSE AND SPILLED BEVERAGES FROM GALLEY WASTE CAN AREA. CLEANED FLOOR. NO FURTHER ODORS NOTED. NO PARTS REPLACED. AIRCRAFT REJul 18, 2007 · N353PH · Dhav DHC8202 · Air Distribution SystemSDR QXEA200701100Unknown · unknownPDX FLIGHT NR 2164, NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED ON TAXI OUT. CYCLED ENGINE MANUAL CIRCUIT BREAKER. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jul 10, 2007 · N353PH · Dhav DHC8202 · Central WarningSDR QXEA200701379Circuit Breaker · trippedSEA - WHEN SELECTING NR 1 STANDBY HYDRAULIC PRESSURE ON DURING APPROACH CHECKLIST NR 1 STANDBY HYDRAULIC PRESSURE INDICATED ZERO. AFTER FLAP SELECTION INDICATOR STILL READ ZERO. MAIN PRESSURE INDICATED NORMALLY AND NO LIGHTS ILLUMINATED. ALL COCKPIT BREAKERJul 4, 2007 · N353PH · Dhav DHC8202 · Hydraulic Power SystemSDR QXEA200701040None · noneSEA - FLIGHT CREW NOTICED ACRID BURNING ODOR IN COCKPIT, NO SMOKE NOTED. ODOR IS STILL NOTICEABLE AFTER PARKING. FOUND CAPTAINS HAT WAS HUNG ON OBSERVERS MAP LIGHT THAT WAS ON. MELTING CAPTAINS HAT CAUSING ACRID ODOR IN COCKPIT. NO OTHER DEFECTS NOTED. NOJun 28, 2007 · N353PH · Dhav DHC8202 · Standard Practices/StructuresSDR QXEA200700821Generator · malfunctionedPDX FLIGHT NR 2149 - DURING TAKEOFF, NR 1 AC GENERATOR CAUTION ILLUMINATED AFTER CYCLING NR 1 AC GENERATOR PER CHECK LIST NR 1 STALL WARNING CAUTION ILLUMINATED THEN WENT OUT. THEN NR 1 AC GENERATOR CAUTION ILLUMINATED AGAIN. MAINTENANCE REPLACED THE NR 1 ACMay 19, 2007 · N353PH · Dhav DHC8202 · AC Generation SystemSDR QXEA200700389Unknown · unknownYVR FLIGHT NR 2029, AFTER TAKEOFF DURING FLAP RETRACTION GOT NR 1 ENGINE HYD PUMP CAUTION LIGHT. PRESSURE INDICATED 2000 PSI ON BOTH STANDBY AND MAIN NR 1 HYDRAULIC PRESSURE GAUGES. WHEN FLAPS WERE UP ALL INDICATIONS WENT BACK TO NORMAL. NO OTHER CAUTION LIFeb 26, 2007 · N353PH · Dhav DHC8202 · Hydraulic System, MainSDR QXEA200700206Unknown · unknownPUW FLIGHT NR 2197, NR 1 DC GENERATOR CAUTION LIGHT BECAME ILLUMINATED DURING TAXI OUT TO RUNWAY. FOLLOWED EMERGENCY CHECKLIST, CAUTION LIGHT STAYED ILLUMINATED NR 1 ENGINE STARTED NORMALLY (DC GENERATOR INOP). MAINTENANCE PLACED ON MEL.Feb 15, 2007 · N353PH · Dhav DHC8202 · DC Generating SystemSDR QXEA200700043Tscu · malfunctionedSEA FLIGHT NR 2257, NR 1 WOULD NOT FEATHER WHEN TESTED DURING DAILY CHECKS. MAINTENANCE REPLACED NR 1 TSCU. PERFORMED GROUND RUNS IAW MTC 9720019. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Jan 20, 2007 · N353PH · Dhav DHC8202 · Propeller Controlling SystemSDR QXEA200700005Potentiometer · out of adjustPSC FLIGHT NR 2094, AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL, AUTO FEATHER SYSTEM INOP. MAINTENANCE ADJUSTED THE POTENTIOMETER. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jan 4, 2007 · N353PH · Dhav DHC8202 · Propeller Feathering/ReversingSDR QXEA200603152Flap System · malfunctionedSEA FLIGHT NR 2194 ON CLIMB-OUT, APPROXIMATELY 2 MINUTES AFTER SELECTING FLAPS UP, FLAP POWER CAUTION LIGHT ILLUMINATED. ALL SYSTEMS INDICATED NORMAL. LIGHT EXTINGUISHED AFTER 4-5 MINUTES. MAINTENANCE SERVICED AND BLED NR 1 HYDRAULIC SYSTEM IAW AMM 12-12-00Dec 8, 2006 · N353PH · Dhav DHC8202 · Trailing Edge Flap Control SystemSDR QXEA200603000Warning System · malfunctionedPDX FLIGHT NR 2228, FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Nov 16, 2006 · N353PH · Dhav DHC8202 · Trailing Edge Flap Control SystemSDR QXEA200601699Panel · dislodgedSEA FLIGHT NR 2273, CEILING PANEL FELL DOWN. MAINTENANCE SECURED. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jun 26, 2006 · N353PH · Dhav DHC8202 · Passenger Compartment EquipmentSDR QXEA200601471Resistor · malfunctionedSEA - NR 2 ENGINE TORQUE LIMITED DUE TO HIGH ITT. MAINTENANCE SECURED TRIM RESISTOR HARDWARE. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Jun 17, 2006 · N353PH · Dhav DHC8202 · Engine EGT/TIT Indicating SystemSDR QXEA200601273Gcu · malfunctionedSEA - ON FLIGHT 2222, RETURNED TO GATE, NR 2 DC GENERATOR CAUTION LIGHT ILLUMINATED. MAINTENANCE, REMOVED AND REPLACED THE NR 2 GCU. FUNCTIONAL TEST GOOD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.May 18, 2006 · N353PH · Dhav DHC8202 · DC Generating SystemSDR QXEA200601258Light · looseSEA - ON FLIGHT 2229, PART OF THE EMERGENCY LIGHT STRIP ON CABIN FLOOR LOOSE. REPLACED FWD SECTION OF EMERGENCY LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.May 15, 2006 · N353PH · Dhav DHC8202 · Emergency LightingSDR QXEA200601218Battery · inoperativePDX - FLIGHT 2207 FLIGHT ATTENDANT ADVISES THAT THE EXIT LIGHT ABOVE THE DOOR FLICKERS ON AND OFF ACCOMPANIED BY A POPPING SOUND. MAINTENANCE REPLACED RELAY 3351-K2 (FOUND BROKEN WIRE ON K-2 RELAY). REPLACED EMERGENCY BATTERIES. OPERATIONAL CHECK GOOD. AIRMay 8, 2006 · N353PH · Dhav DHC8202 · Emergency LightingSDR QXEA200601217Switch · malfunctionedGEG - FLIGHT 2206 EMERGENCY LIGHTS FLICKERED ON AND OFF FOUR TIMES DURING CLIMBOUT, ACCORDING TO THE FLICHT ATTENDANT. MAINTENANCE REPLACED THE EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANT STATION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.May 7, 2006 · N353PH · Dhav DHC8202 · Emergency LightingSDR QXEA200601031Stop Fitting · wornYYC - C4 FUSELAGE RIGHT HAND EMERGENCY EXIT DOOR SURROUND STOP FITTINGS WORN IN EIGHT LOCATIONS. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-36, 51-20-51 AND RD 8-53-126.Apr 12, 2006 · N353PH · Dhav DHC8202 · Emergency ExitsSDR QXEA200601068Skin · dentedYYC - C4 LEFT HAND HORIZONTAL STABILIZER LOWER SKIN HAS TWO DENTS AT YH102 AND YH104.5, BETWEEN STRINGER 1 AND 2. REPAIRED IAW RD 8-55-1685, ISSUE 1.Apr 11, 2006 · N353PH · Dhav DHC8202 · Horizontal Stabilizer, Plate/SkinSDR QXEA200601052Structure · crackedYYC - C4 RIGHT NACELLE LOWER COWL RIGHT SIDE FORWARD LATCH MATTING SURFACE CRACKED. REPAIRED IAW RD 8-71-030, ISSUE 3.Apr 10, 2006 · N353PH · Dhav DHC8202 · Nacelle/Pylon, Main FrameSDR QXEA200601032Angle · crackedYYC - C4 LEFT NACELLE, INBOARD DRAG ANGLE IS CRACKED AT LAST RIVET, AFT ON WING SIDE. REPARIED IAW RD 8-57-1053, ISSUE 2.Apr 10, 2006 · N353PH · Dhav DHC8202 · Nacelle/Pylon Miscellaneous StructureSDR QXEA200601016Attach Fitting · wornYYC - C4 LEFT NACELLE AFT HEAT SHIELD, OUTLET SHROUD ATTACHMENT TABS ARE WORN THROUGH AT STATION 262 - 280 ON INBOARD SIDE AND OUTBOARD SIDE. REPAIRED IAW RD 8-54-163, ISSUE 2.Apr 10, 2006 · N353PH · Dhav DHC8202 · Nacelle/Pylon, Attach FittingsSDR QXEA200601057Bushing · wornYYC - C4 TRAILING RUDDER CENTER HINGE UPPER ATTACHMENT BOLT HOLE WORN EXCESSIVE AND LOWER BUSHING WORN. REPAIRED IAW RD 8-55-554, ISSUE 1.Apr 7, 2006 · N353PH · Dhav DHC8202 · Rudder StructureSDR QXEA200601055Push-Pull Rod · gougedYYC - C4 TRAILING RUDDER LOWER HINGE PUSH/PULL ROD ATTACHMENT BRACKET HAS A DEEP GOUGE AND BOLT OPENING HOLE WORN EXCESSIVE. REPAIRED IAW RD 8-55-168, ISSUE 5.Apr 7, 2006 · N353PH · Dhav DHC8202 · Rudder StructureSDR QXEA200601067Skin · damagedYUYC C4 - LEFT NACELLE INBOARD SIDE SKIN HAS LOOSE RIVETS ABOVE AND BEHIND ACCESS DOOR 416AR. ONE RIVET WORN THROUGH COUNTER SINK. REPAIRED IAW RD 8-54-1193, ISSUE 3.Apr 6, 2006 · N353PH · Dhav DHC8202 · Nacelle/Pylon, Plate/SkinSDR QXEA200601066Hinge · gougedYYC - C4 RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE GOUGED AT AFT SIDE OF FORWARD LUG BY BRG BRACKET AND SPACER CONTACT SURFACE WORN. REPAIRED IAW HORIZON AIR EA 2-54-276 AND RD 8-54-2164, ISSUE 1.Apr 6, 2006 · N353PH · Dhav DHC8202 · Landing Gear DoorsSDR QXEA200601059Skin · chafedYYC - C4 LEFT INBOARD FLAP UPPER SKIN HAS CHAFED MARK. REPAIRED IAW DHC-8-200 RD 8-57-1023 AND DHC-8-200 AMM 20-30-11.Apr 6, 2006 · N353PH · Dhav DHC8202 · Trailing Edge FlapsSDR QXEA200601019Stop Fitting · chafedYYC - C4 PASSENGER DOOR AFT NR 1 AND NR 2 STOP ASSEMBLIES LIGHTLY CHAFED. REPARIED IAW RD 8-52-8222, ISSUE 1 AND HORIZON AIR EA 2-52-237.Apr 6, 2006 · N353PH · Dhav DHC8202 · Passenger/Crew DoorsSDR QXEA200601020Skin · damagedYYC - C4 FUSELAGE EXTERIOR BELLY SKIN BETWEEN STATION X530 - X566 AND STRINGERS 23P - 28P HAS A LARGE AREA OF NICKS IN SKIN. REPAIRED IAW DHC-8-200 SRM 51-20-11, 20-34-11-370-801, RD 8-53-8986 AND HORIZON AIR EA 2-53-731.Apr 6, 2006 · N353PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR QXEA200601022Skin · dentedYYC - C4 FUSELAGE EXTERIOR SKIN AT STATION X302, BETWEEN STRINGERS 17S - 20S HAS SEVERAL DENTS. REPAIRED IAW DHC-8-200 SRM 51-20-91, RD 8-53-4984, ISSUE 1 AND HORIZON AIR EA 2-53-730.Apr 5, 2006 · N353PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR QXEA200601062Hinge · wornYYC - C4 VERTICAL STABILIZER REAR SPAR TOP FORE RUDDER ATTACH SAFETY HINGE HAS WEAR DAMAGE ON TOP FACE. REPARIED IAW DHC-8-200 SR, 51-40-11, PAGES 1-4 AND RD 8-51-102, ISSUE 1.Apr 4, 2006 · N353PH · Dhav DHC8202 · Rudder Miscellaneous StructureSDR QXEA200601063Hinge · wornYYC - C4 VERTICAL STABILIZER REAR SPAR FORE RUDDER ATTACH BOTTOM SAFETY HINGE HAS WEAR DAMAGE ON TOP FACE. REAPIRED IAW RD 8-51-102, ISSUE 1 AND DHC-8-200 SRM 51-40-11, PAGES 1-4.Apr 4, 2006 · N353PH · Dhav DHC8202 · Rudder Miscellaneous StructureSDR QXEA200601043Fastener · looseYYC - C4 LEFT WING INTERIOR, STATION YW138.0 ON FRONT SPAR HAS TWO LOWER LOOSE HILOCKS. REPLACED IAW DHC-8-200 SRM 51-40-00.Apr 4, 2006 · N353PH · Dhav DHC8202 · Wing SparSDR QXEA200601035Fitting · wornYYC - C4 LEFT ELEVATOR SPRING TAB DRIVE HINGE FITTING IS WORN. REPARIED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.Apr 4, 2006 · N353PH · Dhav DHC8202 · Elevator, Tab StructureSDR QXEA200601024Stop Fitting · wornYYC - C4 FUSELAGE AFT BAGGAGE DOOR SURROUND STOP FITTINGS WORN AT EIGHT LOCATIONS. REPAIRED IAW DHC-8-200 SRM 52-30-00-820-001 AND RD 8-104, ISSUE 3.Apr 4, 2006 · N353PH · Dhav DHC8202 · Cargo/Baggage DoorsSDR QXEA200601033Clip · crackedYYC - C4 FUSELAGE INTERIOR AT STATION X240 UNDER PASSENGER DOOR SILL, CLIP IS CRACKED. REPAIRED IAW DHC-8-200 SRM, 51-40-11, PAGES 1-4.Apr 3, 2006 · N353PH · Dhav DHC8202 · Fuselage Main, Attach FittingsSDR QXEA200601034Sill · corrodedYYC - C4 FUSELAGE INTERIOR PASSENGER DOOR OPENING, LOWER SILL ASSEMBLY HAS PITTING CORROSION ON TOP SURFACE UNDER TEFLON RUB STRIP. REPAIRED IAW DHC-8-200 SRM 51-20-11, PAGES 1-11, 51-40-11 AND AMM 20-30-11.Apr 3, 2006 · N353PH · Dhav DHC8202 · Fuselage Main, StructureSDR QXEA200601064Access Panel · corrodedYYC - C4 RIGHT HAND WING ACCESS PANEL 622AT COUNTER SINK SCREW HOLES HAVE FRETTING CORROSION. REPAIRED IAW RD 8-57-1715, ISSUE 3, DHC-8-200 SRM 51-20-16, PARAGRAPH D AND DHC-8-200 MM 20-32, PAGES 1-3.Apr 2, 2006 · N353PH · Dhav DHC8202 · Wing, Plate/SkinSDR QXEA200601048Skin · corrodedYYC - C4 RIGHT INBOARD LEADING EDGE 611AR LOWER ATTACHMENT REBATE INBOARD HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-811, DHC-8-200 SRM 51-40-11, PAGES 1-4 AND DHC-8 AMM 20-34-11.Apr 2, 2006 · N353PH · Dhav DHC8202 · Leading Edge DevicesSDR QXEA200601061Structure · corrodedYYC - C4 RIGHT HORIZONTAL STABILIZER ELEVATOR HORN HAS FRETTING DAMAGE ON INTERNAL REBATE ALONG INBOARD EDGE. REPAIRED IAW DHC-8-200 CORROSIOON PREVENTION MANUAL CHAPTER 4, PART 1 AND DHC-8 MM 20-21-03, PAGES 1-7.Apr 1, 2006 · N353PH · Dhav DHC8202 · Horizontal Stabilizer StructureSDR QXEA200601038Line · chafedYYC - C4 LEFT WING FUEL BAY 524AT HAS RUBBING LINE ON STRUCTURE AT YW207. REPAIRED IAW DHC-8-200 SRM 51-20-11 AND AMM SUB TASK 28-43-11-120-001.Apr 1, 2006 · N353PH · Dhav DHC8202 · Fuel StorageSDR QXEA200601030Stringer · corrodedYYC - C4 FUSELAGE INTERIOR, RIGHT SIDE SUPPORT CHANNEL X240, STRINGER 22S HAS CORROSION ON END. REPAIRED IAW CORROSION PREVENTION CONTROL MANUAL, CHAPTER, PART 1, DHC-8-200 SRM 51-40-11, PAGES 1-4 AND 51-40-00, PAGES 1-5.Apr 1, 2006 · N353PH · Dhav DHC8202 · Fuselage Main, Longeron/StringerSDR QXEA200601029Sill · corrodedICY - C4 FUSELAGE RIGHT EMERGENCY EXIT DOOR SURROUND STRUCTURE, LOWER SILL HAS AREA OF CORROSION FROM X240 TO X264. REPAIRED YAW CORROSION PREVENTION MANUAL, CHAPTER 4, PART 1.Apr 1, 2006 · N353PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200601028Doubler · corrodedYYC - C4 FUSELAGE INTERIOR, RIGHT EMERGENCY EXIT LOWER FRAME DOUBLER HAS AREA OF CORROSION FROM X240 TO X264, STRINGER 24S. REPAIRED IAW DHC-8-200 SRM 51-40-00.Apr 1, 2006 · N353PH · Dhav DHC8202 · Fuselage Main, Structure
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