# Service difficulty reports: N349PH A list on [N349PH](https://openairdocs.org/aircraft/N349PH.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 · 220 reports - [SDR QXEA2008110401158](https://openairdocs.org/sdr/QXEA2008110401158.md): Hydraulic Line · failed · Oct 30, 2008 · N349PH · Dhav DHC8202 · Hydraulic System, Main > PDX - ON DOING DAILY CHECKS, PERFORMED PTU TEST AND LOST ALL HYD ON THE NR 2 SYSTEM. HYDRAULIC FLUID IS ALL OVER ROWS 3/4/5 SEATS. ENGINE SHUTDOWN WITH IN 1 MIN. REPLACED CRACKED NOSE GEAR DOWN LINE, CHECK GOOD. PERFORMED EDP HYD FLUID LOSS INSP IAW MM 05- - [SDR QXEA2008102301140](https://openairdocs.org/sdr/QXEA2008102301140.md): Pressure Switch · malfunctioned · Oct 20, 2008 · N349PH · Dhav DHC8202 · Hydraulic Pressure Sensor > PDX- NR 2 ENG HYD PUMP CAUTION ILLUMINATED. CAUTION REMAINED ILLUMINATED THROUGHOUT LANDING. TAXI AND PARKING. NO LOSS OF HYD PRESS OR QTY. PERFORMED ALTERNATE GEAR EXTENTION. UNEVENTFUL LANDING. REMOVED AND REPLACED NR 2 HYD PRESSURE SWITCH, GROUND RAN N - [SDR QXEA200800535](https://openairdocs.org/sdr/QXEA200800535.md): Switch · malfunctioned · May 31, 2008 · N349PH · Dhav DHC8202 · Propeller Feathering/Reversing > PDX - FLIGHT 2193, AUTOFEATHER ARM LIGHT FLICKERING AND SHOWING AS "ARM" WITHOUT THE BUTTON BEING SELECTED. DURING CLIMB AND CRUISE. MAINTENANCE REPLACED THE AUTOFEATHER SELECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA200800234](https://openairdocs.org/sdr/QXEA200800234.md): Servo · inoperative · Mar 3, 2008 · N349PH · Dhav DHC8202 · Turbine Engine Compressor Section > PDX - FLIGHT 2122 - ENGINE "SURGE" NOISE INTERMITTENT ABOUT EVERY 5-6 MINUTES DURING CLIMB. RTF PDX MAINTENANCE FOUND NR 1 ENGINE IBV SERVO INOPERATIVE, REMOVED AND REPLACE IBV SERVO COMPLETED GROUND RUNS, ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE - [SDR QXEA200800086](https://openairdocs.org/sdr/QXEA200800086.md): Stringer Clip · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Attach Fittings > PDX - C1 CHECK - X466 AND STRINGER 31R SUSPECT CORROSION AT CLIP RADIUS. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED REPAIR AREA. RESTORED FINISH. - [SDR QXEA2008OOO70](https://openairdocs.org/sdr/QXEA2008OOO70.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE REMOVED CORROSION, INSPECTED BLENDED AREA AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER TO REPAIR AREA. - [SDR QXEA200800097](https://openairdocs.org/sdr/QXEA200800097.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SUSPECT CORROSION AROUND 2 SKIN RIVETS X520 TO X522 BELOW SEAT TRACK NR 2. MAINTENANCE REMOVED RIVETS, BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800096](https://openairdocs.org/sdr/QXEA200800096.md): Seat Track · gouged · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X476 TO X 486. MAINTENANCE BLENDED OUT GOUGE. INSPECTED, REMAINED WITHIN LIMITS AND NO CRACK NOTED. RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800095](https://openairdocs.org/sdr/QXEA200800095.md): Seat Track · gouged · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X510 TO 520. MAINTENANCE BLENDED OUT GOUGE ON TRACK, INSPECTED REMAINED WITHIN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800090](https://openairdocs.org/sdr/QXEA200800090.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIVET HEADS ABOVE INNER SKIN ON WEB X528 TO X534 ON THE RIGHT SIDE BELOW SEAT TRACK 8/9 SUSPECT LIGHT CORROSION. MAINTENANCE REMOVED RIVETS AND BLENDED CORROSION FROM WEB, REMAINED WITHIN LIMITS AND INSPECTED NO CRACKS NOTED. INSTALLED NEW R - [SDR QXEA200800081](https://openairdocs.org/sdr/QXEA200800081.md): Skin · dented · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Plate/Skin > PDX - C1 CHECK - SCRATCH AND SMALL DENT AT APPROXIMATELY STA X106.00 AND APPROXIMATELY 4 INCHES ABOVE PANEL 112BR RIGHT EXTERNAL FUSELAGE. MAINTENANCE BLENDED AREA OF SCRATCH TO REMOVE DAMAGE, STILL WITHIN LIMITS AND INSPECTED NO CRACKS NOTED. RESTORED FINIS - [SDR QXEA200800092](https://openairdocs.org/sdr/QXEA200800092.md): Shear Tie · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Internal Mounting Structure > PDX - C1 CHECK - X545 STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION FROM CLIP, BLEND REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800109](https://openairdocs.org/sdr/QXEA200800109.md): Support Angle · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C1 CHECK - CORROSION UNDER AFT CARGO DOOR THRESHOLD SUPPORT ANGLE APPROXIMATELY STA X600 STRINGER 28L. MAINTENANCE REMOVED RIVETS BLENDED CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINI - [SDR QXEA200800107](https://openairdocs.org/sdr/QXEA200800107.md): Skin · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Plate/Skin > PDX - C1 CHECK - SPOT OF CORROSION ON THE INNER SKIN AROUND RIVET HOLE FORWARD OF FRAME STA 201 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED MINOR CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA - [SDR QXEA200800105](https://openairdocs.org/sdr/QXEA200800105.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SUSPECT CORROSION AROUND RIVET ON VERTICAL FRAME SUPPORT FOR NR 4 SEAT TRACK AT STA X370.00 INBOARD OF STRINGER 31L BOTTOM MOST INBOARD RIVET. MAINTENANCE REMOVED RIVET BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NO - [SDR QXEA200800100](https://openairdocs.org/sdr/QXEA200800100.md): Skin · dented · Jan 14, 2008 · N349PH · Dhav DHC8202 · Rudder, Plate/Skin > PDX - C1 CHECK - FORE RUDDER HAS A 1/4 BY 1/2 DENT ON RIGHT SIDE 13 INCHES FROM TOP EDGE 4 INCHES FROM TRAILING EDGE. MAINTENANCE CUT OUT SKIN DAMAGE, INSPECTED FOR CRACKS, NO CRACKS NOTED. REPAIRED IAW RD 8-55-1905 AND DHC8 200 SRM. - [SDR QXEA200800099](https://openairdocs.org/sdr/QXEA200800099.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SEAT TRACK NR 11 AT X496 HAS A CORROSION PIT ON TOP ANGLE. MAINTENANCE BLENDED OUT THE CORROSION, INSPECTED, REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800098](https://openairdocs.org/sdr/QXEA200800098.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SUSPECT LIGHT CORROSION FORMING ON WEB TIE RIVET HEADS BELOW FLOOR AND SEAT TRACK. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AR - [SDR QXEA200800082](https://openairdocs.org/sdr/QXEA200800082.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - NR 4 SEAT TRACK HAS CORROSION AT CAMLOCK RECEPTACLE UNDER DRIP TRAY AT STA X240. MAINTENANCE REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK. - [SDR QXEA200800085](https://openairdocs.org/sdr/QXEA200800085.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SEAT TRACK NR 5 AT X468 HAS 2 CORROSION PITS ON INNER FLOORBOARD FLANGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800110](https://openairdocs.org/sdr/QXEA200800110.md): Skin · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Plate/Skin > PDX - C1 CHECK - LAV SERVICE DOOR APERATURE AFT LOWER CORNER CORRODED AROUND FASTENER. MAINTENANCE REMOVED LAV SERVICE DOOR CUT OUT DAMAGED AREA, FABRICATED REPAIR PACKER AND BACKING PLATE AND INSTALLED PACKER AND BACKING PLATE. - [SDR QXEA200800106](https://openairdocs.org/sdr/QXEA200800106.md): Threshold · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C1 CHECK - MAIN CABIN DOOR THRESHOLD HAS LIGHT CORROSION AT 5 EA NUTPLATES. MAINTENANCE REMOVED MCD THRESHOLD AND NUTPLATES. REMOVED LIGHT SURFACE CORROSION FROM LOWER SILL PLATE AND INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. - [SDR QXEA200800101](https://openairdocs.org/sdr/QXEA200800101.md): Flap Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Trailing Edge Flaps > PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK LOWER SIDE THERE ARE TWO AREAS OF ROLLER CHAFE DAMAGE WITH PITTING CORROSION IN BETWEEN. MAINTENANCE BLENDED OUT CHAFE AND PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. - [SDR QXEA200800111](https://openairdocs.org/sdr/QXEA200800111.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - NR 1 SEAT TRACK WEB TO FRAME ANGLE CLIP IS CRACKED FORWARD SIDE OF FRAME 312. MAINTENANCE REMOVED AND INSTALLED NEW CLIP. - [SDR QXEA200800108](https://openairdocs.org/sdr/QXEA200800108.md): Intercostal · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C1 CHECK - CORROSION ON AVIONICS RACK INTERCOSTAL AT FS X202 TO FS 198.300 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800094](https://openairdocs.org/sdr/QXEA200800094.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SEAT TRACK NR 5 X447 TO X457 IS GOUGED. MAINTENANCE BLENDED OUT GOUGE ON SEAT TRACK, INSPECTED AND REMAINED WITHIN LIMITS, NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800093](https://openairdocs.org/sdr/QXEA200800093.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - SEAT TRACK 36 AT X545 HAS PIT OF CORROSION THAT IS OUT OF LIMITS AT.028 DEEP. MAINTENANCE REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK. - [SDR QXEA200800087](https://openairdocs.org/sdr/QXEA200800087.md): Stringer Clip · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Attach Fittings > PDX - C1 CHECK - X468 AND STRINGER 31R SUSPECT CORROSION AT CLIP EDGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800079](https://openairdocs.org/sdr/QXEA200800079.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE BLENDED OUT CORROSION, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800083](https://openairdocs.org/sdr/QXEA200800083.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - NR 2 SEAT TRACK HAS VERY LIGHT PITTING IN THE CHANNEL AT APPROXIMATELY X488. MAINTENANCE BLENDED THE PITTED AREA, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800102](https://openairdocs.org/sdr/QXEA200800102.md): Flap Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Trailing Edge Flaps > PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK INBOARD SIDE LOWER SURFACE OF UPPER FLANGE. THERE IS PITTING CORROSION AT ROLLER CONTACT AREA. MAINTENANCE BLENDED OUT THE PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. - [SDR QXEA200800091](https://openairdocs.org/sdr/QXEA200800091.md): Skin · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Plate/Skin > PDX - C1 CHECK - X534 AND STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION AT CLIP, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. INSTALLED NEW RIVETS AND RESTORED FINISH TO REPAIR AREA. - [SDR QXEA200800084](https://openairdocs.org/sdr/QXEA200800084.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX -C1 CHECK - SEAT TRACK NR 3 HAS A CORROSION PIT IN THE CHANNEL AT X544. MAINTENANCE BLENDED THE AREA, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800080](https://openairdocs.org/sdr/QXEA200800080.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 IS CORRODED ON THE FRONT OUTBOARD CORNER AT APPROX X262. MAINTENANCE BLENDED OUT CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800103](https://openairdocs.org/sdr/QXEA200800103.md): Flap Track · damaged · Jan 14, 2008 · N349PH · Dhav DHC8202 · Trailing Edge Flaps > PDX - C1 CHECK - RIGHT OUTBOARD FLAP AREA NR 5 FLAP TRACK. THERE ARE TWO ROLLER CHAFE AREAS ON THE UPPER SURFACE. MAINTENANCE BLENDED AREA, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. - [SDR QXEA200800078](https://openairdocs.org/sdr/QXEA200800078.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X330. MAINTENANCE BLENDED CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800077](https://openairdocs.org/sdr/QXEA200800077.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT OUTBOARD SET TRACK NR 10 HAS SMALL AREA OF CORROSION AT APPROX X346. MAINTENANCE BLENDED CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. - [SDR QXEA200800076](https://openairdocs.org/sdr/QXEA200800076.md): Seat Track · chafed · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - TOP OF RIGHT OUTBOARD SEAT TRACK NR 10 IS CHAFED AT APPROX X362. MAINTENANCE BLENDED CHAFED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMED AREA. - [SDR QXEA200800075](https://openairdocs.org/sdr/QXEA200800075.md): Seat Track · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X364. MAINTENANCE REMOVED CORROSION, INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO BLENDED AREA. - [SDR QXEA200800074](https://openairdocs.org/sdr/QXEA200800074.md): Seat Track · gouged · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings > PDX - C1 CHECK - RIGHT INBOARD SEAT TRACK NR 7 HAS APPROX.060 GOUGE ON THE OUTBOARD FLANGE AT APPROX X256. MAINTENANCE REMOVED TRACK AND INSTALL NEW TRACK. - [SDR QXEA200800073](https://openairdocs.org/sdr/QXEA200800073.md): Bracket · cracked · Jan 14, 2008 · N349PH · Dhav DHC8202 · Wing Miscellaneous Structure > PDX - C1 CHECK - LT WING INBOARD LEADING EDGE LOWER OUTBOARD BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACE LEADING EDGE BRACKET. - [SDR QXEA200800072](https://openairdocs.org/sdr/QXEA200800072.md): Floorbeam · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Floor Beam > PDX - C1 CHECK - FLOORBOARD SUPPORT ANGLE CORRODED AT APPROX STA X599.00, Y26.00 RT TO Y31.00 RT, Y 0.00 TO Y 8.00 RT, Y 0.00 TO Y 6.00 LT. MAINTENANCE REMOVED CORROSION INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKED NOTED. ALODINED, PRIMED AND PAINTED. - [SDR QXEA200800069](https://openairdocs.org/sdr/QXEA200800069.md): Nut Plate · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Main, Attach Fittings > PDX - C1 CHECK - NUTPLATE AND MOUNTING SURFACE AT STA X599.00 Y21.00 LT IS CORRODED. MAINTENANCE REMOVED NUTPLATE AND REMOVED CORROSION. INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER, AND PAINT. INSTALLED NEW NUTPLATE. - [SDR QXEA200800068](https://openairdocs.org/sdr/QXEA200800068.md): Support Angle · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C1 CHECK - SUPPORT ANGLE AT APPROX STA X600.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE. - [SDR QXEA200800067](https://openairdocs.org/sdr/QXEA200800067.md): Support Angle · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X594.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION. INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED - [SDR QXEA200800066](https://openairdocs.org/sdr/QXEA200800066.md): Support Angle · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C CHECK - SUPPORT ANGLE AT APPROX X586.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED NEW NUTPLATE - [SDR QXEA200800065](https://openairdocs.org/sdr/QXEA200800065.md): Support Angle · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C CHECK - SUPPORT ANGLE AT APPROX STA X569.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS NO CRACKS NOTED. ALODINED, PRIMED AND PAINTED. IN - [SDR QXEA200800064](https://openairdocs.org/sdr/QXEA200800064.md): Support Angle · corroded · Jan 14, 2008 · N349PH · Dhav DHC8202 · Fuselage Miscellaneous Structure > PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X553.00 AT DOOR THRESHOLD HAS CORROSSION ON NUTPLATES AND MOUNTING SURFACE. REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND WITHIN LIMITS NO CRACKS FOUND. ALODINED PRIMED AND PAINTED INSTALLED NUTPL - [SDR QXEA200702046](https://openairdocs.org/sdr/QXEA200702046.md): Smoke Detector · malfunctioned · Dec 30, 2007 · N349PH · Dhav DHC8202 · Smoke Detection > MFR - ON TAXI THE LAV SMOKE DETECTOR WENT OFF. RETURNED TO THE GATE AND RESET THE DETECTOR. MAINTENANCE COULD NOT DUPLICATE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. - [SDR QXEA200702043](https://openairdocs.org/sdr/QXEA200702043.md): Engine · malfunctioned · Dec 30, 2007 · N349PH · Dhav DHC8202 · Engine (Turbine/Turboprop) > MFR - FLIGHT 2150 - SHORTLY AFTER TAKEOFF, THE LAV SMOKE DETECTOR WENT OFF. THE FLIGHT ATTENDANT CHECKED AND SAW NO SMOKE, BUT DID SMELL A HOT DUSTY SMELL. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN Next page: https://openairdocs.org/aircraft/N349PH/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 = 'N349PH' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N349PH/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.