# Service difficulty reports: N350PH, cancelled Nov 3, 2009

A list on [N350PH, cancelled Nov 3, 2009](https://openairdocs.org/deregistered/N350PH-2009-11-03.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 6 · 283 reports

- [SDR QXEA2009012600035](https://openairdocs.org/sdr/QXEA2009012600035.md): Switch · malfunctioned · Jan 21, 2009 · N350PH · Dhav DHC8202 · Engine Controls
  > SEA - ON TAKEOFF, NR 1 ENG LAGS BEHIND NR 2 DOESN'T ACCELERATE. REPLACED THE SWITCH ROLLER ASSEMBLY. OPS CHECK GOOD. RETURNED TO SERVICE.
- [SDR QXEA2009012300032](https://openairdocs.org/sdr/QXEA2009012300032.md): Switch · contaminated · Jan 19, 2009 · N350PH · Dhav DHC8202 · Engine Controls
  > SEA - NR 1 ENGINE FAILED TO ACCELERATE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. UPON INSPECTION FOUND MAX AND MIN POSITION ON THE CONDITION LEVERS SWITCHES BELOW THE COCKPIT FLOOR STICKY. CLEANED AND LUBED SWITCH, GROUND RAN ENGINES AT TAKEOFF
- [SDR QXEA200800809](https://openairdocs.org/sdr/QXEA200800809.md): Lamp · malfunctioned · Jul 18, 2008 · N350PH · Dhav DHC8202 · Landing Gear Position and Warning
  > PDX-FLIGHT 2096 (PDT-PDX). ON APPROACH THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ALTERNATE EXTENSION AND RECEIVED 3 GREEN LIGHTS. FLEW BY TOWER TO CONFIRM GEAR DOWN. CHECKS OF CFR CALLED. PERFORMED UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LAM
- [SDR QXEA200800173](https://openairdocs.org/sdr/QXEA200800173.md): Stringer Clip · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Main, Attach Fittings
  > PDX - C5 CHECK - THE STRINGER CLIP AND RIVETS ON STRINGER 23R AT THE FORWARD SIDE OF THE REAR SPAR FRAME X424.124 IS CORRODED. REMOVED CLIP AND INSTALLED NEW CLIP IAW DHC8 200 SRM 51-40-11, 51-20-46, AND 51-20-51.
- [SDR QXEA200800160](https://openairdocs.org/sdr/QXEA200800160.md): Fitting · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Main, Attach Fittings
  > PDX - C5 CHECK - RIGHT MLG RETRACTION ACTUATOR FITTING HAS CORROSION ON FRAME JUST ABOVE TOP BOLT HOLE IN CENTER. REPAIRED IAW DHC8 200 RD8-54-1178, NDTM PT-6 51-00-01, PT-1 51-00-04.
- [SDR QXEA200800157](https://openairdocs.org/sdr/QXEA200800157.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X545 TO X549 ON LEFT OUTBOARD SEAT TRACK NR 3 THERE IS LIGHT CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36.
- [SDR QXEA200800220](https://openairdocs.org/sdr/QXEA200800220.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD MOUNT FLANGE (INBOARD) SIDE OF FLANGE APPROXIMATELY STA X565.00 IS CORRODED. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-40-11.
- [SDR QXEA200800172](https://openairdocs.org/sdr/QXEA200800172.md): Frame · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Main, Frame
  > PDX - C5 CHECK - FRAME CASTELLATION AT STATION X333.3 AFT FACE OF FRAME BETWEEN STRINGERS 23L AND 24L HAS SUSPECT CORROSION. REPAIRED IAW DHC8 200 CPM CHAPTER 4 STEP 8, NDTM PT-1 51-00-04 AND PT-6 51-00-01, DHC8 200 SRM 51-20-11, 51-12-16, 51-20-51 AND 51-40
- [SDR QXEA200800171](https://openairdocs.org/sdr/QXEA200800171.md): Keelbeam · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Main, Keel
  > PDX - C5 CHECK - SUSPECT CORROSION UNDER BRACKET AT VERTICAL KEEL FRAME APPROXIMATELY STATION 202 X 31P. REPAIRED IAW DHC8 200 CPM CHAPTER 4 STEP 8, NDTM PT-1 51-00-04 AND PT-6 51-00-01, SRM 51-40-11, 51-20-11, 51-20-16, 51-20-36 AND 51-40-00.
- [SDR QXEA200800170](https://openairdocs.org/sdr/QXEA200800170.md): Stringer Clip · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Main, Attach Fittings
  > PDX - C5 CHECK - FOUND CORROSION ON STRINGER CLIP, STRINGER 23R AT FRAME 387 AFT SIDE. REMOVED AND INSTALLED NEW STRINGER CLIP IAW DHC8 200 SRM 51-40-11.
- [SDR QXEA200800169](https://openairdocs.org/sdr/QXEA200800169.md): Skin · gouged · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > PDX - C5 CHECK - RIGHT SIDE OF FUSELAGE EXTERNAL SKIN HAS GOUGE AT BASE OF V-STAB APPROXIMATELY 10 INCHES AFT OF FRAME 5. REPAIRED IAW DHC8 RD8-53-2181 AND NDTM PT-6 51-00-01.
- [SDR QXEA200800168](https://openairdocs.org/sdr/QXEA200800168.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 6 SEAT TRACK OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGE SUSPECT CORROSION FROM STATION X582.00 - 600.00. REPAIRED IAW DHC8 200 RD8-53-4936, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36
- [SDR QXEA200800167](https://openairdocs.org/sdr/QXEA200800167.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD SUPPORT MOUNT FLANGE HAS CORRODED NUTPLATE AT STATION X593.00. REPAIRED IAW DHC8 200 RD8-53-784, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800166](https://openairdocs.org/sdr/QXEA200800166.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X545.00 TO X600.00. REPAIRED IAW DHC8 200 RD8-53-4936, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800165](https://openairdocs.org/sdr/QXEA200800165.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X582.00. REPAIRED IAW DHC8 200 RD8-53-784, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800164](https://openairdocs.org/sdr/QXEA200800164.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X545.00. REPAIRED IAW DHC8 200 RD8-53-4936, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800163](https://openairdocs.org/sdr/QXEA200800163.md): Bracket · chafed · Jan 30, 2008 · N350PH · Dhav DHC8202 · Nacelle/Pylon, Main Frame
  > PDX - C5 CHECK - NR 2 ENGINE COWLING NR 3 BRACKET ON INBOARD SIDE IS CHAFED. REMOVED FIRE SEAL BRACKET FROM LOWER COWL AND INSTALLED NEW FIRE SEAL BRACKET IAW DHC8 200 SRM 51-40-00.
- [SDR QXEA200800162](https://openairdocs.org/sdr/QXEA200800162.md): Intercostal · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C5 CHECK - SUSPECT CORROSION ON FLOOR PAN INTERCOSTAL AT STR 24P FROM STA X510 TO X531. REPAIRED IAW DHC8 200 SRM 51-20-11 AND 51-20-16.
- [SDR QXEA200800161](https://openairdocs.org/sdr/QXEA200800161.md): Intercostal · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > PDX - C5 CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL INBOARD AND OUTBOARD SIDES OF INTERCOSTAL AT STATION X201.15 AND STR 31P. REPAIRED IAW DHC8 200 CPM CHAPTER 4 PG 4-25 PARA 9B(6)(A), DHC8 200 NDTM PT-6 51-00-01, PT-1 51-00-04, AND DHC8 200 SRM 51
- [SDR QXEA200800159](https://openairdocs.org/sdr/QXEA200800159.md): Frame · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Landing Gear Attach Fittings
  > PDX - C5 CHECK - LEFT MLG RETRACTION ACTUATOR FITTING HAS CORROSION ON ATTACHMENT FRAME ON LOWER OUTBOARD BOLT HOLE. REPAIRED IAW DHC8 200 RD8-54-1178, NDTM PT-6 51-00-01, PT-1 51-00-04.
- [SDR QXEA200800158](https://openairdocs.org/sdr/QXEA200800158.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X547 TO X549 ON LEFT INBOARD SEAT TRACK NR 6 THERE IS CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36.
- [SDR QXEA200800156](https://openairdocs.org/sdr/QXEA200800156.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X532 ON LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION ON THE TOP OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36.
- [SDR QXEA200800155](https://openairdocs.org/sdr/QXEA200800155.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X504 ON THE LEFT INBOARD SEAT TRACK NR 5 THERE IS CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36.
- [SDR QXEA200800154](https://openairdocs.org/sdr/QXEA200800154.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C4 CHECK - AT APPROXIMATELY STATION X488 THE LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36.
- [SDR QXEA200800153](https://openairdocs.org/sdr/QXEA200800153.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X468 THE LEFT OUTBOARD SEAT TRACK NR 2 HAS A GOUGE ON THE EDGE OF THE CLAW ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND THE DHC8 200 51-20-16, 51-20-36.
- [SDR QXEA200800152](https://openairdocs.org/sdr/QXEA200800152.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X455 LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36.
- [SDR QXEA200800151](https://openairdocs.org/sdr/QXEA200800151.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STA X350 TO X356 LEFT OUTBOARD SEAT TRACK NR 1 HAS GOUGES ON THE TOP AT THE INBOARD EDGE. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16, 51-20-36.
- [SDR QXEA200800150](https://openairdocs.org/sdr/QXEA200800150.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STA X265 THE LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF TRACK. REPAIRED IAW DHC 8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-10, 51-20-36.
- [SDR QXEA200800192](https://openairdocs.org/sdr/QXEA200800192.md): Flap Track · damaged · Jan 30, 2008 · N350PH · Dhav DHC8202 · Trailing Edge Flaps
  > PDX - C5 CHECK - THERE IS ONE DIVOT ON THE UPPER SIDE OF THE OUTBOARD LOWER FLANGE OF THE RIGHT NR 4 FLAP TRACK. REPAIRED IAW DHC8 200 RD8-57-988, NDTM PT-6 51-00-01.
- [SDR QXEA200800182](https://openairdocs.org/sdr/QXEA200800182.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - SEAT TRACK NR 10 HAS CORROSION AT STA Y265. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 SRM 51-40-11, 51-40-00.
- [SDR QXEA200800191](https://openairdocs.org/sdr/QXEA200800191.md): Mount · damaged · Jan 30, 2008 · N350PH · Dhav DHC8202 · Wing Miscellaneous Structure
  > PDX - C5 CHECK - THE OUTBOARD STATIC WICK MOUNT PAD APPEARS TO HAVE LIGHTNING STRIKE DAMAGE ON THE RIGHT AILERON. REMOVED AILERON TRAILING EDGE AND INSTALLED A NEW TRAILING EDGE IAW RD8-57-2269, DHC8 AMM 23-60-01, SRM 51-20-26 AND 57-60-71 PARA 2B. PERFORMED
- [SDR QXEA200800190](https://openairdocs.org/sdr/QXEA200800190.md): Skin · damaged · Jan 30, 2008 · N350PH · Dhav DHC8202 · Ailerons
  > PDX - C5 CHECK - LEFT AILERON OUTBOARD TRAILING EDGE JUST OUTBOARD OF STATIC WICK APPEARS TO BE A LIGHTING EXIT POINT. REMOVED TRAILING EDGE AND INSTALLED NEW TRAILING EDGE IAW DHC8 200 SRM 51-40-00, 51-20-26, 57-60-71 PARA 2B. PERFORMED WICK CHECK IAW DHC8 2
- [SDR QXEA200800189](https://openairdocs.org/sdr/QXEA200800189.md): Flap Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Trailing Edge Flaps
  > PDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON THE LOWER SURFACE OF THE UPPER INBOARD FLANGE AT THE ROLLERS ZERO DEGREE POSITION. REPAIRED IAW DHC 8 200 RD8-57-989, NDTM PT-6 51-00-01.
- [SDR QXEA200800188](https://openairdocs.org/sdr/QXEA200800188.md): Flap Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Trailing Edge Flaps
  > PDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON UPPER SURFACE OF THE LOWER OUTBOARD FLANGE AT THE ROLLERS ZERO DEGREE POSITION. REPAIRED IAW DHC 8 200 RD8-57-989, AND NDTM PT-6 51-00-01.
- [SDR QXEA200800187](https://openairdocs.org/sdr/QXEA200800187.md): Mount · loose · Jan 30, 2008 · N350PH · Dhav DHC8202 · Wing, Attach Fittings
  > PDX - C5 CHECK - THE BOTTOM RIVETS ON THE AILERON TRIM ACTUATOR HINGE ARM MOUNTING PLATE ARE LOOSE AND WORKING. REMOVED AND REPLACED RIVET AT AILERON TRIM ACTUATOR AS PER DHC 8 200 SRM 51-40-11.
- [SDR QXEA200800186](https://openairdocs.org/sdr/QXEA200800186.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGE SUSPECTED CORROSION AT STATION X565.00. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM PT-6 51-00-01, AND SRM 51-40-11.
- [SDR QXEA200800185](https://openairdocs.org/sdr/QXEA200800185.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 6 SEAT TRACK INBOARD FLOORBOARD MOUNT FLANGE, SUSPECTED CORROSION FROM STA X545.00 - X600.00. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM PT-6 51-00-01 AND SRM 51-40-11.
- [SDR QXEA200800184](https://openairdocs.org/sdr/QXEA200800184.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD MOUNT FLANGE (INBOARD) SIDE OF FLANGE APPROXIMATELY STATION X582.00 IS CORRODED. REPAIRED IAW DHC 8 200 RD 8-53-784, NDTM PT-6 51-00-01, RD 8-53-9998, AND DHC 8 200 SRM 51-40-11, 51-20-96.
- [SDR QXEA200800183](https://openairdocs.org/sdr/QXEA200800183.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - SEAT TRACK NR 7 HAS CORROSION ON THE TOP BETWEEN STA Y213 TO Y240. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 SRM 51-40-11, AND RD 8-53-1102.
- [SDR QXEA200800181](https://openairdocs.org/sdr/QXEA200800181.md): Seat Track · corroded · Jan 30, 2008 · N350PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - C5 CHECK - AT APPROXIMATELY STATION X264 THE LEFT INBOARD SEAT TRACK NR 4 HAS CORROSION ON TOP OF TRACK. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 SRM 51-40-11, 51-40-00, RD 8-53-1102, AND RD 8-53-4473.
- [SDR QXEA200702035](https://openairdocs.org/sdr/QXEA200702035.md): Transducer · malfunctioned · Dec 26, 2007 · N350PH · Dhav DHC8202 · Airfoil Anti/De-ice System
  > PDX - FLIGHT 2094 - LEFT DE-ICE PRESSURE GAUGE SHOWS GREATER THEN 30 PSI. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 30-8B. AIRCRAFT RETURNED TO SERVICE. REPLACED THE LT PRESSURE TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SER
- [SDR QXEA200701718](https://openairdocs.org/sdr/QXEA200701718.md): Actuator · malfunctioned · Nov 12, 2007 · N350PH · Dhav DHC8202 · Engine Air Intake System
  > PDX FLIGHT NR 2119, NR 2 ENGINE BYPASS DOOR DOES NOT INDICATE OPEN (LIGHT TEST OK) FROM CRUISE (FL230/-20'C) TO PARKING (+10"C). REPAIRED CHAFFED WIRES AND REPLACED NR 2 ENGINE INTAKE BYPASS DOOR LINEAR ACTUATOR. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO S
- [SDR QXEA200701275](https://openairdocs.org/sdr/QXEA200701275.md): Warning Light · none · Aug 10, 2007 · N350PH · Dhav DHC8202 · Central Warning
  > PDX FLIGHT NR 2184 ECU MANUAL CAUTION LIGHT. MAINTENANCE CYCLED BETA LOCKOUT CIRCUIT BREAKER. MANUAL LIGHT EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200701211](https://openairdocs.org/sdr/QXEA200701211.md): Unknown · unknown · Jul 21, 2007 · N350PH · Dhav DHC8202 · AC Generation System
  > PSC - DURING INITIAL CLIMB NR 1 AC GENERATOR CAUTION ILLUMINATED. FOLLOWING THE CHECKLIST, THE LIGHT EXTINGUSHED. 90 SECONDS LATER, THE LIGHT RE-ILLUMINATED. A SECOND RESET WAS NOT ATTEMPTED. NR 2 AC GENERATOR LOADS WERE MONITORED AND NO LIMITATIONS WERE EX
- [SDR QXEA200700778](https://openairdocs.org/sdr/QXEA200700778.md): Indicator · malfunctioned · May 11, 2007 · N350PH · Dhav DHC8202 · Weather Radar System
  > IDA FLIGHT NR 2165, AFTER TURNING ON ALL ELECTRONICS IN THE FLIGHT DECK THERE WAS A SLIGHT ELECTRICAL ODOR AFTER ONE MINUTE IT WAS VERY STRONG AND REACHED BACK TO ROW THREE. THERE WAS NO SMOKE THAT WE NOTICED BUT SOMETHING WAS BURNING. REPLACED WEATHER RADAR
- [SDR QXEA200700388](https://openairdocs.org/sdr/QXEA200700388.md): Unknown · unknown · Feb 28, 2007 · N350PH · Dhav DHC8202 · Hydraulic Power System
  > SEA FLIGHT NR 2077 INFLIGHT, NR 2 SPU AUX POWER CAUTION LIGHT ILLUMINATED RAN APPROPRIATE CHECKLIST NO OTHER CAUTION LIGHTS AT THE TIME. MAINTENANCE GROUND RAN ENGINES FOR AC POWER 2 SPU AUX POWER CAUTION LIGHT REMAINS EXTINGUISHED WITH AC GEN POWER APPLIED.
- [SDR QXEA200700124](https://openairdocs.org/sdr/QXEA200700124.md): Brake Assy · vibration · Feb 3, 2007 · N350PH · Dhav DHC8202 · Landing Gear Brake System
  > SEA FLIGHT NR 2010, VIBRATION COMING FROM LEFT SIDE BRAKES. MAINTENANCE REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. BLED AND LEAK CHECKED BRAKES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200602688](https://openairdocs.org/sdr/QXEA200602688.md): Threshold · corroded · Oct 5, 2006 · N350PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > BAGGAGE COMPARTMENT THRESHOLD PLATE SUPPORT ANGLE ON VERTICAL WEB AT STA X600 LBL30.0 HAS CORROSION ON BOTH TOP AND BOTTOM SURFACE. REPAIRED IAW SRM 51-40-11.
- [SDR QXEA200602674](https://openairdocs.org/sdr/QXEA200602674.md): Skin · damaged · Oct 1, 2006 · N350PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > C4 YYC - RIGHT FORWARD FUSELAGE EXTEROIR SKIN AT STATION 222.7 AND STRINGER 26 HAS NICKS ON SKIN. REPAIRED IAW RD8-53-5384 AND SRM 51-20-51.
- [SDR QXEA200602673](https://openairdocs.org/sdr/QXEA200602673.md): Skin · gouged · Oct 1, 2006 · N350PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > C4 YYC - RIGHT FORWARD FUSELAGE EXTEROIR SKIN AT STATION 222.7 AND STRINGER 27 SKIN IS GOUGED. REPAIRED IAW RD8-53-5384 AND SRM 51-20-51.

Next page: https://openairdocs.org/deregistered/N350PH-2009-11-03/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 = 'N350PH' AND deregistration_id = 'N350PH-2009-11-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N350PH-2009-11-03/reports

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