N354PH, cancelled Jul 21, 2011

Service difficulty reports · 224

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 = 'N354PH' AND deregistration_id = 'N354PH-2011-07-21'
  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 QXEA200600822Seat Track · corrodedPDX - C4 RIGHT HAND INBOARD SEAT TRACK NR 7 HAS EVIDENCE OF PITTING CORROSION AT STATION X242.00 AND X239.00. REPAIRED IAW RD 8-53-4632.Mar 24, 2006 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200600917Clip · corrodedPDX - C4 CABIN UNDER FLOOR RIGHT HAND OUTBOARD FRAME CLIP IS CORRODED AT X387.350. REPAIRED IAW DHC-8-200 SRM 51-20-11 AND 51-40-00.Mar 23, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Attach FittingsSDR QXEA200501776Computer · malfunctionedPDX FLIGHT NR 2227, WHILE BOARDING, POWER DROPPED OFF AIRCRAFT. THEN RESET, NOTICED AN ELECTRICAL SMELL AND THE AUDIO ALERT C/B WAS POPPED AND THE NAV SWITCH AND ANN 1 C/B WAS POPPED. ALT ALERTER DISPLAY IS DARK. MX FOUND TWO COMPONENTS WITH SIGNS OF OVERHEDec 12, 2005 · N354PH · Dhav DHC8202 · Flight Management Computing Hardware SystemSDR QXEA200501352Shroud · dentedPDX - DENT IN LOWER AILERON SHROUD, RIGHT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-322A.Oct 13, 2005 · N354PH · Dhav DHC8202 · AileronsSDR QXEA200501279Ahrs · failedSEA FLIGHT NR 2297 CAPTAINS AHRS FAILED. MAINTENANCE REPLACED AHRS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 3, 2005 · N354PH · Dhav DHC8202 · Attitude and Direction Data SystemSDR QXEA200501133Relay · failedNR 1 STANDBY HYDRAULIC PRESSURE READS ZERO AFTER SWITCH SELECTED TO NR 1. MAINTENANCE REPLACED RELAY 292-K5, NR 1 STANDBY HYDRAULIC PUMP OPERATES NORMALLY AS PER AMM 29-11-17-710-801. CIRCUIT BREAKER REMAINED SET. AIRCRAFT RETURNED TO SERVICE.Jul 23, 2005 · N354PH · Dhav DHC8202 · Hydraulic System, MainSDR QXEA200501125Switch · malfunctionedSEA - DE-ICE PRESSURE ON DURING DESCENT (9 PSI) DURING TAXI PRESSURE RETURNED TO NORMAL (SELECTED BOOT AIR TO ISO AS PER CHECKLIST). REPLACED NR 1 & 2 LOW PRESSURE SWITCHES (55) PERFORMED FUNCTIONAL CHECK OF BLEED AIR SYSTEM IAW AMM 21-11-00, PAGES 501-503. OPJul 19, 2005 · N354PH · Dhav DHC8202 · Airfoil Anti/De-ice SystemSDR QXEA200501029Generator · malfunctionedNR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED ON APPROACH AS STANDBY HYDRAULIC PUMPS WERE SELECTED ON. CYCLED NR 2 AC GENERATOR SWITCH AS PER EMERGENCY CHECKLIST. LIGHTS EXTINGUSHED. REPLACED NR 2 AC GENERATOR. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.Jun 9, 2005 · N354PH · Dhav DHC8202 · AC Generator-AlternatorSDR QXEA200500958Unknown · multiple failPDX - ON FLIGHT 2139 CAPTAIN'S ADI FAILED, AHRS INVALID MESSAGE, WEATHER RADAR INOP, AND COMM RADIOS P-STATIC. AIRCRAFT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE PERFORMED OPERATIONAL AND FUNCTIONAL CHECKS OF THE COMM SYSTEM, TMay 28, 2005 · N354PH · Dhav DHC8202 · Navigation SystemSDR QXEA200500526Hydraulic Line · leakingYKM-ON FLIGHT NUMBER 2002, AFTER LANDING AND PARKING NOTICED A STRANGE ODOR AND BOTH PILOTS STARTED COUGHING, COULD SEE MIST/SMOKE IN THE COCKPIT. AFTER SHUTDOWN NOTICED FLUID LEAKING FROM BELLY OF AIRCRAFT UNDER COCKPIT. MAINTENANCE INSPECTED AND FOUND HYDRMar 30, 2005 · N354PH · Dhav DHC8202 · Hydraulic System, MainSDR QXEA200500076Nut Plate · spinningPDX - PANEL 121AR HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS.Dec 4, 2004 · N354PH · Dhav DHC8202 · FastenersSDR QXEA200500075Nut Plate · spinningPDX - PANEL 122BL HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS.Dec 4, 2004 · N354PH · Dhav DHC8202 · FastenersSDR QXEA200400377Nut Plate · brokenPANEL 122AR ON RT FORWARD FUSELAGE HAS TWO BAD NUTPLATES. REMOVED AND REPLACED NUTPLATES IAW DHC-8 SRM 51-40-11.May 27, 2004 · N354PH · Dhav DHC8202 · FastenersSDR QXEA200400376Wire · brokenSEA - FLIGHT 2296 - WHILE EN ROUTE TO SEA, THE FLIGHT SPOILER 1 PUSH OFF ILLUMINATED. THE NUMBER 1 HYDRAULIC PRESSURE WAS NORMAL AND THE CHECKLIST WAS RUN. THE CREW PUSHED OFF THE FLIGHT SPOILER AND THE MASTER CAUTION ROLL SPOILER INBOARD HYDRAULIC ILLUMINATMay 27, 2004 · N354PH · Dhav DHC8202 · Flight Control System WiringSDR QXEA200400160Ahrs · malfunctionedPDX - ON FLIGHT 2126 HSI HEADING MISMATCH ON ADVISORY DISPLAY. PER CHECKLIST RESETS OK BUT REAPPEARS. REMOVED AND REPLACED NR 1 AHRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Feb 16, 2004 · N354PH · Dhav DHC8202 · Integrated Flight SystemSDR QXEA200400145Generator · failedMFR - ON FLIGHT 2083 IMMEDIATELY AFTER TAKEOFF, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST AND CYCLED NR 2 AC GENERATOR SWITCH OFF, THEN ON. NO CHANGES NOTED. NR 2 AC GENERATOR CAUTION LIGHT IS STILL ILLUMINATED.Feb 13, 2004 · N354PH · Dhav DHC8202 · AC Generation SystemSDR QXEA200400054Warning Light · illuminatedHSI HEADING MISMATCH ILLUMINATED DURING FLIGHT. ACCOMPLISHED CHECKLIST. PRESSED HDG/DG BUTTON TWICE, MESSAGE CLEARED. C/W MTC 9340019 STEPS OF AHRS SYSTEM SELF TEST. SYSTEM CHECKS GOOD, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Jan 21, 2004 · N354PH · Dhav DHC8202 · Attitude and Direction Data SystemSDR QXEA200400031Skin · scratchedPDX - SCRATCHES IN FUSELAGE SKIN UNDER AFT SIDE OF 262DT. REPAIRED IAW HORIZON AIR EA 2-53-530.Jan 7, 2004 · N354PH · Dhav DHC8202 · Fuselage Main, Plate/SkinSDR QXEA200400030Fitting · chafedPDX - AFT LEFTHAND BATH TUB FITTING CHAFED. REPAIRED IAW RD 8-53-2108.Jan 7, 2004 · N354PH · Dhav DHC8202 · Fuselage Main, Attach FittingsSDR QXEA200400029Sill · corrodedPDX - CARGO DOOR SILL CORROSION AROUND NUT PLATES BOTTOM SIDE X571.00 AND YL40.00. REMOVED CORROSION IAW CPM CHAPTER 4D(3A).Jan 6, 2004 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200400025Seat Track · corrodedPDX - RIGHT HAND INBOARD TRACK NR 8 OUTBOARD FLANGE CAMLOCK RECEPTICLE CORRODED. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.Jan 6, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400024Seat Track · corrodedPDX - CARGO COMPARTMENT LEFT INBOARD TRACK NR 6 CORROSION AROUNT NUT PLATE AT APPROXIMATELY X582.00. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36.Jan 6, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400022Seat Track · chafedPDX - RIGHT HAND INBOARD TRACK NR 8 INBOARD FLANGES CHAFED. REPAIRED IAW DHC-8-200 51-20-16.Jan 6, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400021Seat Track · gougedPDX - INBOARD FLANGE GOUGED AND PITTED AROUND CAMLOCK REPECTICAL HOLE OF RIGHT HAND INBOARD TRACK NR 7. REPAIRED IAW DHC-8-200 SRM 51-40-11.Jan 5, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400020Seat Track · gougedPDX - TOP FLANGE GOUGED AND SCRATCHED ON RIGHT HAND OUTBOARD TRACK NR 11. REPAIRED IAW DHC-8-200 SRM 51-40-00.Jan 4, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400019Seat Track · corrodedPDX - TOP FLANGE NICKED AND CHANNEL PITTED ON RIGHT HAND OUTBOARD SEAT TRACK NR 10. REPAIRED IAW DHC-8-200 SRM 51-40-00.Jan 4, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400023Seat Track · scratchedPDX - RIGHT HAND INBOARD TRACK NR 7 INBOARD FLANGE SCRATCHED 4.5 INCH LONG. REPAIRED IAW DHC-8-200 SRM 51-40-11.Jan 3, 2004 · N354PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA200400033Frame · crackedPDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK APPROXIMATELY 3.4 INCH LONG WHERE FRAME MEETS UP WITH THE 4TH STRINGER FROM THE TOP RIGHT SIDE OF FUSELAGE. REPAIRED IAW RD 8-55-199.Jan 2, 2004 · N354PH · Dhav DHC8202 · Vertical Stabilizer, Spar/RibSDR QXEA200400032Frame · crackedPDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK IN IT WHERE FRAME MEETS UP WITH THE FOURTH STRINGER FROM THE TOP LEFT OF FUSELAGE. REPAIRED IAW RD8-55-199.Jan 2, 2004 · N354PH · Dhav DHC8202 · Vertical Stabilizer, Spar/RibSDR QXEA200301512Stop · lack of lubeMAIN CABIN DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBED DOOR STOP LUGS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Dec 3, 2003 · N354PH · Dhav DHC8202 · Passenger/Crew DoorsSDR QXEA200301291Track · dirtyON FLIGHT 2017 MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. CLEANED DEBRIS FROM TRACK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 16, 2003 · N354PH · Dhav DHC8202 · Passenger/Crew DoorsSDR QXEA200301270Support · gougedGOUGES ON INBOARD LOWER ENGINE SUPPORT STRUT ON NR 1 NACELLE. REPAIRED IAW HORIZON AIR EA 2-54-189.Oct 9, 2003 · N354PH · Dhav DHC8202 · Engine Mount SectionSDR QXEA200301224Engine · failedON FLIGHT 2117 FLIGHT ATTENDENT REPORTED SMOKE IN CABIN. REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 7, 2003 · N354PH · Dhav DHC8202 · Engine (Turbine/Turboprop)SDR QXEA200301213O-Ring · failedON FLIGHT 2006 DURING TAXI OUT, LAVATORY SMOKE ALARM ACTIVATED FOR 1 MINUTE, THEN RESET BY FLIGHT ATTENDANT. FLIGHT ATTENDANT REPORTED SMOKE/FUMES ODOR AND HAZE/SMOKE IN CABIN NO FIRE/SMOKE IN LAVATORY. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE NL POct 3, 2003 · N354PH · Dhav DHC8202 · Smoke DetectionSDR QXEA200301137Valve · malfunctionedON FLIGHT 2208 BLEED SMOKE IN CABIN. REMOVED AND REPLACED NO.2 ENGINE P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Sep 16, 2003 · N354PH · Dhav DHC8202 · Engine Cooling SystemSDR QXEA200301047Inverter · failedSEA- ON FLIGHT 2240 FISH OIL SMELL IN FLIGHT DECK. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Sep 1, 2003 · N354PH · Dhav DHC8202 · AC InverterSDR QXEA200301056Light · failedLT UNDERWING EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS TEST. REMOVED AND REPLACED LT UNDERWING EMERGENCY EXIT DOOR BETA LIGHT.Aug 31, 2003 · N354PH · Dhav DHC8202 · Emergency LightingSDR QXEA200301055Light · failedRT FORWARD EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS TEST. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY EXIT DOOR BETA LIGHT.Aug 31, 2003 · N354PH · Dhav DHC8202 · Emergency LightingSDR QXEA200301054Light · failedRT UNDERWING EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS TEST. REMOVED AND REPLACED EMERGENCY EXIT DOOR BETA LIGHT.Aug 31, 2003 · N354PH · Dhav DHC8202 · Emergency LightingSDR QXEA200300943Structure · scratchedPDX- SCRATCH IN AIRFRAME BELOW RIGHT HAND EMERGENCY EXIT BETWEEN STATION X366-355. REPAIRED IAW DHC-8 RD 8-53-7489 AND HORIZON AIR EA 2-53-462.Aug 1, 2003 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous StructureSDR QXEA200300752Structure · crackedPDX- FORE RUDDER CRACKED AT LOWER LEFT HAND SIDE OF PREVIOUS REPAIR. REPAIRED IAW DHC-8 SRM 55-40-28.Jun 18, 2003 · N354PH · Dhav DHC8202 · Rudder StructureSDR QXEA200300741Strap · corrodedPDX - THE FORWARD LAND STRAP FOR PANEL 422DT HAS CORROSION FORWARD OF THE FASTENERS. MAINTENANCE BLENDED, MAPPED, CHECKED FOR THICKNESS, AND REPAIRED THE AFFECTED AREA IAW EA 2-54-171.Jun 15, 2003 · N354PH · Dhav DHC8202 · Nacelle/Pylon Miscellaneous StructureSDR QXEA0201602Transmitter · inoperativePDX-RETURNED TO FIELD FOR ENGINE OIL PRESSURE INDICATOR 46 PSI THEN WENT TO 55 PSI AT FLIGHT IDLE AND REMAINED FOR REST OF FLIGHT. NO MATER CAUTION OR MASTER WARNING INDICATIONS. REPLACED #1 ENGINE OIL PRESSURE INDICATOR, NO HELP. OIL PRESSURE DROPPED TO 41 PSOct 6, 2002 · N354PH · Dhav DHC8202 · Engine Oil Indicating SystemSDR QXEA0201589Detector · defectiveSEA-LAVATORY FIRE DETECTOR WENT OFF INFLIGHT. PRESSED RESET TO SILENCE, REMAINED QUIET REST OF FLIGHT. REPLACED LAVATORY FIRE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 4, 2002 · N354PH · Dhav DHC8202 · Detection SystemSDR QXEA02011232Odor · detectedSEA- FUMES IN COCKPIT. INSPECTED AIRCRAFT, SMELLED FOR FUMES WITH EXTERIOR POWER ON AND RAN ENGINES WITH AC GENERATORS ONLINE FOR 30 MINUTES USING VARIOUS SYSTEMS. NO EVIDENCE OF FUMES NOTICED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Aug 13, 2002 · N354PH · Dhav DHC8202 · Air Distribution SystemSDR QXEA0200957Servo · fouledPDX - AIRCRAFT RETURNED TO FIELD WHEN A SLIGHT BINDING WAS NOTED IN THE AILERON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPOSITIONED THE SAFETY WIRE PIGTAILS ON THE AILERON SERVO. OPERATIONAL CHECK WAS PERFORMED AND WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVIJul 13, 2002 · N354PH · Dhav DHC8202 · Aileron Control SystemSDR QXEA0200905Line · leakingPDX-AIRCRAFT RETURNED TO FIELD, NR 2 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED ON TAKEOFF. NR 2 HYDRAULIC QUANTITY WAS AT .5 QUARTS. MAITENANCE INSPECTED AIRCRAFT AND FOUND NOSE LANDING GEAR ACTUATOR UPLINE LEAKING. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATJun 24, 2002 · N354PH · Dhav DHC8202 · Hydraulic System, MainSDR QXEA0200479Switch · lack of lubePDX - TAKEOFF WARNING HORN ACTIVATED ON TAKEOFF. ABORTED TAKEOFF, RAN CHECKLIST, TALKED TO MAINTENANCE CONTROL AND RAN TORQUE UP. DID NOT GET THE TAKEOFF WARNING HORN DURING CONFIGURATION CHECK. ATTEMPTED SECOND TAKEOFF AND RECEIVED TAKEOFF WARNING HORN. CMar 14, 2002 · N354PH · Dhav DHC8202 · Central WarningSDR QXEA0200094Light · defectiveGEG- FLIGHT ATTENDANT REPORTS SMOKE WAS COMING FROM AIRSTAIR DOOR LIGHT. RELAMPED LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Feb 7, 2002 · N354PH · Dhav DHC8202 · Passenger Compartment LightingSDR QXEA0102036Warning System · false activationBLI - DURING ADDITION OF TAKEOFF POWER, THE TAKEOFF WARNING HORN ACTIVATED. TAKEOFF WAS ABORTED AND THE REJECTED TAKEOFF LIST WAS COMPLIED WITH. A SECOND TAKEOFF WAS ATTEMPTED AND AGAIN THE TAKEOFF WARNING SOUNDED. THE REJECTED TAKEOFF LIST WAS COMPLIED WITDec 18, 2001 · N354PH · Dhav DHC8202 · Central Warning
Back to N354PH, cancelled Jul 21, 2011