N356PH, cancelled Jun 16, 2014
Service difficulty reports · 206
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 = 'N356PH' AND deregistration_id = 'N356PH-2014-06-16' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR QXEA200800427Indicator · failedPDX- 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 SERVISDR QXEA200800348Flap Track · wornPDX-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 ARESDR QXEA200800352Skin · corrodedUPPER 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 QXEA200800351Skin · damagedBURNED 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 QXEA200800347Structure · corrodedPDX-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 QXEA200800345Skin · corrodedPDX-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 QXEA200800368Skin · damagedPDX-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 QXEA200800367Flap Track · wornPDX-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 QXEA200800357Skin · dentedPDX-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 QXEA200800358Skin · damagedPDX -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 REPSDR QXEA20080344Structure · corrodedPDX 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 QXEA20080343Structure · corrodedPDX 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 QXEA20080342Bracket · loosePDX 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 QXEA20080338Warning Light · intermittentSEA - 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 QUANTITSDR QXEA200800019Inverter · odorPDX - 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 QXEA200701588Warning Light · false activationRDM 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 QXEA200700799Pressure Switch · malfunctionedYVR 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 PCSDR QXEA200700715Computer · inoperativePDX - 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 RIGHTSDR QXEA200700521Switch · failedSEA - 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 QXEA200700508Lamp · inoperativePDX FLIGHT NR 2170, NR 2 TANK AUX PUMP LIGHT OUT. MAINTENANCE RELAMPED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200700392Unknown · unknownPDX 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 QXEA200700247Starter Gen · malfunctionedBOI 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. GROSDR QXEA200602955Pump · malfunctionedSEA 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 QXEA200601849Connector · dirtySEA FLIGHT 2024 LEFT FUEL TEMPERATURE HIGH. MAINTENANCE CLEANED CONNECTOR. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200601730Generator · malfunctionedSEA FLIGHT 2016, NR 2 AC GENERATOR CAUTION. MAINTENANCE REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200601215Pump · malfunctionedPDX FLIGHT NR 2246 - NR 2 HYDRAULIC PUMP CAUTION. MAINTENANCE REPLACED THE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200601200Stringer · crackedPDX - C4 LEFT NACELLE FINGERNAIL DECK STRINGERS CRACKED BOTTOM SIDE AND FORWARD. REPAIRED IAW DHC-8-200 SRM 51-40-11.SDR QXEA200601124Stop · wornPDX - C4 MAIN CABIN DOOR AFT BOTTOM STOP ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.SDR QXEA200601123Stop · wornPDX - C4 MAIN CABIN DOOR AFT TOP STOP GUIDE ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.SDR QXEA200601122Stop · wornPDX - C4 MAIN CABIN DOOR FORWARD TOP STOP GUIDE ON APERATURE IS WORN. REPAIRED IAW RD 8-53-3933, STEPS 4 - 7.SDR QXEA200601121Stop · wornPDX - C4 MAIN CABIN DOOR FORWARD BOTTOM STOP ON APERTURE WORN. REPAIRED IAW RD 8-53-3933, PAGE 4, STEPS 4-7.SDR QXEA200601184Access Panel · corrodedPDX - 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 QXEA200601182Stringer · corrodedPDX - 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 QXEA200601189Skin · dentedPDX - 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 QXEA200601199Sill · corrodedPDX - 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 QXEA200601188Skin · dentedPDX - 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 QXEA200601185Galley Track · corrodedPDX - 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 QXEA200601193Door Frame · corrodedPDX - 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 QXEA200601119Panel · chafedPDX - 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 QXEA200601126Skin · chippedPDX - 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 QXEA200601183Skin · gougedPDX - 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 QXEA200601125Panel · chafedPDX - 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 QXEA200601129Stringer · corrodedPDX - 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 QXEA200601120Attach Angle · crackedPDX - 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 QXEA200601118Riser · corrodedPDX - 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 QXEA200601194Web · corrodedPDX - 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 QXEA200601195Web · corrodedPDX - 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 QXEA200601191Riser · corrodedPDX - 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 QXEA200601197Fitting · corrodedPDX - 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 QXEA200601190Floor Support · corrodedPDX - 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.
Back to N356PH, cancelled Jun 16, 2014