# Service difficulty reports: N354PH, cancelled Jul 21, 2011 A list on [N354PH, cancelled Jul 21, 2011](https://openairdocs.org/deregistered/N354PH-2011-07-21.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 · 224 reports - [SDR QXEA200800285](https://openairdocs.org/sdr/QXEA200800285.md): Attach Fitting · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Main, Attach Fittings > PDX - C5 - MCD LAY SHAFT FWD AND AFT GOOSE NECK ATTACH FITTINGS ARE PITTING AND CORRODED. REMOVED MCD LAY SHAFT REF -8/200 AMM 52-10-00FIG 501 SHEETS (3&4). REMOVED BOTH FWD AND AFT HINGE FITTINGS FROM FWD AND AFT TUBE ASSEMBLIES REF -8/200 SRM 51-40-11. IN - [SDR QXEA200800284](https://openairdocs.org/sdr/QXEA200800284.md): Bracket · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Main, Attach Fittings > PDX - C5 - MCD SURROUND FWD END OF SILL PLATE BRACKET FOR SILL PLATE CORRODED AGAINST FUSELAGE. REMOVED THE MCD THRESHOLD BY DRILLING OUT THE RIVETS HOLDING THE THRESHOLD TO LOWER SILL PLATE, REMOVED NUTPLATES FROM THE LOWER SILL PLATE. BLENDED OUT CORROSION - [SDR QXEA200800283](https://openairdocs.org/sdr/QXEA200800283.md): Sill · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C5 - MCD SURROUND FWD SIDE OF SILL PLATE AREA, CORROSION AT SEAL INFLATION FEED THROUGH, IPC 52-05-00 FIG 5 ITEM 490. REMOVED MCD SEAL INFLATION TUBE AND REMOVED CORROSION AROUND HOLE REF RD8-53-8921. HFEC INSPECTION IAW -8/200 NDTM PART 6 51-00-01 AND - [SDR QXEA200800282](https://openairdocs.org/sdr/QXEA200800282.md): Sill · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX- C5 - CORROSION ON LOWER SURFACE OF MCD SILL PLATE STATION X250 AT AFT NUT PLATE. BLENDED TO REMOVE CORROSION IAW RD8-53-8921. HFEC INSPECTION OF BLENDED AREA IAW -8/200 NDTM PART 6 51-00-01, NO CRACKS NOTED. AREA IS WITHIN LIMITS, ETCH, ALODINE AND PRI - [SDR QXEA200800272](https://openairdocs.org/sdr/QXEA200800272.md): Bracket · cracked · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C5 - ANGLE BRACKET FORWARD OF STATION 600 AND INBOARD OF STRINGER 31R WEB UNDER FLOOR PANEL 441CZ IS CRACKED IN UPPER RADIUS. DRILLED OUT RIVETS IN THE ANGLE BRACKET. REMOVED IAW D8 200 SRM 51-10-21 PG 2 FIG 1. HFEC INSPECTED CUT AWAY FOR REMOVAL OF C - [SDR QXEA200800270](https://openairdocs.org/sdr/QXEA200800270.md): Attach Angle · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C5 - CARGO BAY ENTRYWAY THRESHOLD ATTACHMENT ANGLE AT APPROXIMATELY STA 580.5 HAS CORROSION AROUND NUT PLATES. REMOVED CARGO BAY THRESHOLD PLATE BY REMOVING BOLTS AND SCREWS. REMOVED ANGLE BRACKET AND NUT PLATES BY REMOVING SOLID RIVETS. BLENDED CORRO - [SDR QXEA200800277](https://openairdocs.org/sdr/QXEA200800277.md): Skin · chafed · Mar 6, 2008 · N354PH · Dhav DHC8202 · Trailing Edge Flaps > PDX - C5 - UPPER SURFACE OF LEFT INBOARD FLAP 5" AFT OF THE LEADING EDGE AT STATION YW139.00 IS CHAFED APPROXIMATELY.30" BY.35". BLENDED OUT CHAFE IAW -8 200 SRM 57-50-16 PG 2 TABLE 1. HFEC INSPECTED BLEND IAW-8 200 NDTM PART 6 51-00-01. NO CRACKS NOTED, - [SDR QXEA200800276](https://openairdocs.org/sdr/QXEA200800276.md): Channel · dented · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C5 - LOWER FORWARD EMERGENCY EXIT THRESHOLD CHANNEL PN 85320693 REQUIRES REPLACEMENT IN ACCORDANCE WITH EA 2-53-733 PERMANENT REPAIR FOR DENT IN CHANNEL. REMOVED FLOORBOARD SUPPORT CHANNEL ASSEMBLY AFT OF EMERGENCY EXIT AND EXIT THRESHOLD COVER PLATE. - [SDR QXEA200800275](https://openairdocs.org/sdr/QXEA200800275.md): Floor Support · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C5 - CORROSION ON FLOOR BOARD NUT PLATE FLANGE UNDER PANEL 144BZ AT STATION 199.5 INBOARD OF SEAT TRACK. REMOVED NUTPLATE, BLENDED OUT CORROSION IAW DASH 8 200 CPM CHAPTER 4, FOUND TO BE WITHIN LIMITS IAW DASH 8 200 SRM 51-20-11. ALODINED AND PRIMED BLE - [SDR QXEA200800274](https://openairdocs.org/sdr/QXEA200800274.md): Floorboard · corroded · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Floor Panel > PDX - C5 - CORROSION ON FLOORBOARD FLANGE UPPER SURFACE AT STATION 599.5 OUTBOARD OF STRINGER 28R TO END OF FLANGE. REMOVED NUT PLATE, BLENDED OUT CORROSION IAW DASH 8 200 CPM CHAPTER 4, BLENDED AREA WITHIN LIMITS IAW DASH 8 200 SRM 51-20-11. ALODINED AND PR - [SDR QXEA200800269](https://openairdocs.org/sdr/QXEA200800269.md): Threshold · chafed · Mar 6, 2008 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C5 - CARGO BAY ENTRYWAY THRESHOLD HAS SEVERAL AREAS OF LIGHT CHAFING. REPAIRED CHAFE BY BLENDING, MAX MATERIAL REMOVED WAS.005" WITHIN LIMITS REFERENCE TO D-8 200 SRM 51-20-11. - [SDR QXEA200701902](https://openairdocs.org/sdr/QXEA200701902.md): Rod · broken · Dec 14, 2007 · N354PH · Dhav DHC8202 · Landing Gear Door Retract Section > FLIGHT 2035. LT MAIN GEAR DOORS WERE OPEN WITH NO INDICATION FROM THE COCKPIT, ONLY THE LT SIDE OF THE DOOR IS OPEN. MAINTENANCE REPLACED THE SPRING, CONNECT ROD WHICH WERE BROKEN. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA200701586](https://openairdocs.org/sdr/QXEA200701586.md): Outflow Valve · malfunctioned · Oct 20, 2007 · N354PH · Dhav DHC8202 · Pressure Regulator/Outflow Valve > SEA FLIGHT NR 2190 AT LEVEL FLIGHT CABIN DIFFERENTIAL PRESSURE GRADUALLY DECREASED FROM 5.4 PSID TO 0 PSID. UNABLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. MAINTENANCE REPLACED THE FORWARD OUTFLOW VALVE. PRESSURIZED AIRCRAFT IN MANUAL. OPERATIONAL CHECK G - [SDR QXEA200701504](https://openairdocs.org/sdr/QXEA200701504.md): Generator · malfunctioned · Sep 25, 2007 · N354PH · Dhav DHC8202 · AC Generation System > YVR FLIGHT NR 2450, NR 1 AC GENERATOR CAUTION LIGHT WOULD NOT RESET PER CHECKLIST. FERRIED TO PDX. REPLACED NR 1 AC GENERATOR IAW 24-21-00-400-801. ALSO, REPLACED TRANSFORMERS, BOTH GCU'S AND RELAYS 2421-K1 AND K2. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE - [SDR QXEA200701410](https://openairdocs.org/sdr/QXEA200701410.md): Pressure Switch · malfunctioned · Sep 10, 2007 · N354PH · Dhav DHC8202 · Airfoil Anti/De-ice System > PDX FLIGHT NR 2107, 18 PSI BLEED AIR INDICATES 10 PSI WITH POWER LEVERS AT FLIGHT IDLE. INSTALLED NEW 55 AND 65 PSI SWITCHES IN BOTH RIGHT AND LEFT NACELLES IAW AMM 30-10-00-720-001. GROUND RAN BOTH ENGINES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SER - [SDR QXEA200701166](https://openairdocs.org/sdr/QXEA200701166.md): Smoke Detector · inoperative · Jul 18, 2007 · N354PH · Dhav DHC8202 · Smoke Detection > SEA FLIGHT NR 2064, NR 1 ENGINE START SMOKE MASTER WARNING ILLUMINATED. NR 2 SMOKE DETECTOR INOP. PLACED ON MEL 372270. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA200700963](https://openairdocs.org/sdr/QXEA200700963.md): Lens · dislodged · Jun 14, 2007 · N354PH · Dhav DHC8202 · Passenger Compartment Lighting > SEA FLIGHT NR 2026 PLASTIC PIECE FELL OFF FROM CEILING ABOUT 6" LONG. REPORTED BY FLIGHT ATTENDANT. MAINTENANCE RESECURED SIDE WALL LIGHT LENS. PERFORMED GUI OF LENS. NO DEFECT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA200700393](https://openairdocs.org/sdr/QXEA200700393.md): Wire · chafed · Mar 18, 2007 · N354PH · Dhav DHC8202 · Electrical Power System Wiring > SEA FLIGHT 2070 SHORTLY AFTER LIFTOFF NR 2 DC GENERATOR DC GEN HOT CAUTION ILLUMINATED. CAUTION REMAINED ON FOR ENTIRE DURATION OF FLIGHT EVEN AFTER TURNING OFF NR 2 DC GENERATOR. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND WIRES, 77A20N, 715D20, 78A20, 76A16, - [SDR QXEA200700361](https://openairdocs.org/sdr/QXEA200700361.md): Generator · overheated · Mar 11, 2007 · N354PH · Dhav DHC8202 · DC Generating System > SEA FLIGHT NR 2116 - DURING TAXI, NR 2 DC GEN HOT CAUTION ILLUMINATED. AFTER TURNING OFF NR 2 DC GENERATOR (AS PER CHECKLIST) CAUTION EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES. MAINTENANCE REPLACED NR 2 DC GENERATOR IAW MTC 9801001. PERFORMED FUNCTIONAL TE - [SDR QXEA200602066](https://openairdocs.org/sdr/QXEA200602066.md): Galley · odiferous · Aug 13, 2006 · N354PH · Dhav DHC8202 · Buffet/Galleys > SEA FLIGHT NR 2054 ON DESCENT, AIRCRAFT SMELLS LIKE A DIRTY LAV. LAV FLUID HAS BEEN EXCHANGED TWICE, WARDROBE CLOSET HAS BEEN CLEANED. AIRCRAFT STILL SMELLS LIKE DIRTY LAV. REQUESTING BELLY DRAIN BR OPEN WS FOR ANY OVER FLOW FLUID TO ESCAPE. MAINTENANCE FOUN - [SDR QXEA200600999](https://openairdocs.org/sdr/QXEA200600999.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT HAND UNDERWING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200601000](https://openairdocs.org/sdr/QXEA200601000.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600998](https://openairdocs.org/sdr/QXEA200600998.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600997](https://openairdocs.org/sdr/QXEA200600997.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600996](https://openairdocs.org/sdr/QXEA200600996.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 RIGHT UNDERWING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600995](https://openairdocs.org/sdr/QXEA200600995.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 RIGHT UNDERWING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600992](https://openairdocs.org/sdr/QXEA200600992.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-52-350. - [SDR QXEA200600991](https://openairdocs.org/sdr/QXEA200600991.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT UNDER WING EMERGENCY EXIT AFT UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-52-350. - [SDR QXEA200600990](https://openairdocs.org/sdr/QXEA200600990.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT HAND UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-350. - [SDR QXEA200600993](https://openairdocs.org/sdr/QXEA200600993.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 RIGHT HAND UNDERWING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600994](https://openairdocs.org/sdr/QXEA200600994.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 RIGHT HAND UNDER WING EMERGENCY EXIT FORWARD LOWER STOP WORN ON CONTACT. REPAIRED IAW RD 8-53-126. - [SDR QXEA200600989](https://openairdocs.org/sdr/QXEA200600989.md): Stop · worn · Apr 7, 2006 · N354PH · Dhav DHC8202 · Emergency Exits > PDX - C4 LEFT UNDER WING EMERGENCY EXIT FORWARD UPPER STOP WORN ON CONTACT SURFACE. REPAIRED IAW RD 8-53-350. - [SDR QXEA200601001](https://openairdocs.org/sdr/QXEA200601001.md): Stringer · corroded · Apr 6, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer > PDX - C4 CORROSION FOUND ON STRINGER 32R ON AFT SIDE OF FRAME X151.600. REPAIRED IAW DHC-8-200 SRM 51-40-11 AND HORIZON AIR EA 2-53-375. - [SDR QXEA200601003](https://openairdocs.org/sdr/QXEA200601003.md): Skin · corroded · Apr 5, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Plate/Skin > PDX - C4 CORROSION ON INTERNAL SKIN BAGGAGE COMPARTMENT JUST AFT OF DOOR CUTOUT FLOOR LEVEL. SEVERAL AREAS OF SURFACE CORROSION APPROXIMATELY X600-X535 AND STRINGER 23P. REPAIRED IAW RD 8-53-8998. - [SDR QXEA200600938](https://openairdocs.org/sdr/QXEA200600938.md): Threshold · dented · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C4 DENT IN FORWARD EMERGENCY EXIT THRESHOLD HAS TRANSFER THROUGH TO INSIDE LYING STRUCTURE AT X248-249, YW40. REPAIRED IAW HORIZON AIR EA 2-53-733. - [SDR QXEA200600921](https://openairdocs.org/sdr/QXEA200600921.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 31L AND 32L. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-21-10 AND SRM 51-25-15. - [SDR QXEA200600925](https://openairdocs.org/sdr/QXEA200600925.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600931](https://openairdocs.org/sdr/QXEA200600931.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 30L AND 31L. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600924](https://openairdocs.org/sdr/QXEA200600924.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 28L AND 29L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600932](https://openairdocs.org/sdr/QXEA200600932.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 29L AND 30L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600930](https://openairdocs.org/sdr/QXEA200600930.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 31L AND 32L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600929](https://openairdocs.org/sdr/QXEA200600929.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 32L AND 33L. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600928](https://openairdocs.org/sdr/QXEA200600928.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 30R AND 31R. REPAIRED IAW DHC-8-200 SRM 53-00-16, 51-20-11, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600923](https://openairdocs.org/sdr/QXEA200600923.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 29L AND 30L. REPAIRED IAW DHC-82 SRM 51-00-02, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600934](https://openairdocs.org/sdr/QXEA200600934.md): Stringer · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer > PDX - C4 STRINGER 31R APPEARS CORRODED WHERE PAINT IS MISSING AT STATION 175.0. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-00-04, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600926](https://openairdocs.org/sdr/QXEA200600926.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 32R AND 33R. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-10 AND SRM 51-25-15. - [SDR QXEA200600922](https://openairdocs.org/sdr/QXEA200600922.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 151.6 CASTELLATION IS CORRODED BETWEEN STRINGERS 30L AND 31L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-20-11, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600927](https://openairdocs.org/sdr/QXEA200600927.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 31R AND 32R. REPAIRED IAW DHC-8-200 SRM 51-70-16, 51-40-11, 51-21-10, 51-25-10 AND SRM 51-25-15. - [SDR QXEA200600933](https://openairdocs.org/sdr/QXEA200600933.md): Frame · corroded · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Main, Frame > PDX - C4 FRAME 167.0 CASTELLATION IS CORRODED BETWEEN STRINGERS 28L AND 29L. REPAIRED IAW DHC-8-200 SRM 51-20-16, 51-40-11, 51-21-10, 51-25-10 AND 51-25-15. - [SDR QXEA200600915](https://openairdocs.org/sdr/QXEA200600915.md): Sill · dented · Apr 3, 2006 · N354PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C4 RIGHT FORWARD EMERGENCY EXIT LOWER SILL HAS DENT BY FORWARD DOOR LUG RECEPTACLE. REPAIRED IAW DHC-8-200 SRM 51-40-00 AND HORIZON AIR EA 2-53-729. Next page: https://openairdocs.org/deregistered/N354PH-2011-07-21/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 = 'N354PH' AND deregistration_id = 'N354PH-2011-07-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N354PH-2011-07-21/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.