# Service difficulty reports: N825PH, cancelled Sep 16, 2009

A list on [N825PH, cancelled Sep 16, 2009](https://openairdocs.org/deregistered/N825PH-2009-09-16.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 2 · 93 reports

- [SDR CBR2006F00003](https://openairdocs.org/sdr/CBR2006F00003.md): Warning Horn · intermittent · Apr 3, 2006 · N825PH · Dhav DHC8* · Trailing Edge Flap Control System
  > ABORTED TAKEOFF, DURING TAKEOFF ROLL, TAKEOFF CONFIGURATION HORN CAME ON. FLAP CYCLED. SYSTEM FUNCTIONED SATISFACTORY, HORN NO LONGER EVIDENT ON TAKEOFF REF MM. (K)
- [SDR QXEA0101304](https://openairdocs.org/sdr/QXEA0101304.md): Structure · damaged · Aug 2, 2001 · N825PH · Dhav DHC8* · Cargo/Baggage Doors
  > PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING.REPAIRED IAW HORIZON AIR EA 9-52-122.
- [SDR QXEA0101305](https://openairdocs.org/sdr/QXEA0101305.md): Structure · dented · Aug 2, 2001 · N825PH · Dhav DHC8* · Cargo/Baggage Doors
  > PDX - BAGGAGE DOOR INNER STRUCTURE DENTED WITH CRACK ON VERTICAL MEMBER ABOVE FORWARD COUNTERBALANCE ASSEMBLY. REPAIRED DAMAGE IAW E.A. 9-52-123.
- [SDR 1304](https://openairdocs.org/sdr/1304.md): Structure · damaged · Aug 2, 2001 · N825PH · Dhav DHC8102 · Cargo/Baggage Doors
  > PDX - CARGO DOOR DAMAGED AT FORWARD STRUCTURE CABLE FEED-THROUGH BY CABLE CHAFING. REPAIRED IAW HORIZON AIR EA 9-52-122.
- [SDR QXEA011300](https://openairdocs.org/sdr/QXEA011300.md): Inverter · defective · Aug 1, 2001 · N825PH · Dhav DHC8102 · AC Generation System
  > GEG-ELECTRICAL SMELL NOTICED IN FLIGHT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100015](https://openairdocs.org/sdr/QXEA0100015.md): Controller · will not test · Jan 10, 2001 · N825PH · Dhav DHC8102 · Propeller Feathering/Reversing
  > LWS - AUTOFEATHER WILL NOT TEST. CYCLED POWER LEVERS AND CONDITION LEVERS FULL TRAVEL NUMEROUS TIMES. TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100002](https://openairdocs.org/sdr/QXEA0100002.md): Power Supply · inoperative · Jan 2, 2001 · N825PH · Dhav DHC8102 · Emergency Lighting
  > PDX - FOUND LEFT HAND SIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002509](https://openairdocs.org/sdr/QXEA0002509.md): Acm · malfunctioned · Sep 18, 2000 · N825PH · Dhav DHC8102 · Cabin Cooling System
  > SEA- FLIGHT ATTENDANT REPORTED SMELL OF SMOKE ON SHORT AND FINAL APPROACH JUST AFTER BLEED AIR TURNED OFF FOR LANDING. REPLACED AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0001425](https://openairdocs.org/sdr/QXEA0001425.md): Sign · malfunctioned · May 31, 2000 · N825PH · Dhav DHC8102 · Emergency Lighting
  > PDX- FORWARD ENTRY DOOR LOWER EMERGENCY EGRESS EXIT SIGN BROKEN. REPLACED ENTRY DOOR LOWER EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0001126](https://openairdocs.org/sdr/QXEA0001126.md): Inverter · malfunctioned · Apr 19, 2000 · N825PH · Dhav DHC8102 · AC Inverter
  > SEA- DURING FLIGHT AIRCRAFT COCKPIT/CABIN BEGAN TO SMELL OF SMOKE. AUXILIARY INVERTER MASTER CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT
- [SDR QXEA9902718](https://openairdocs.org/sdr/QXEA9902718.md): Web · corroded · Dec 23, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN286.0. REPAIRED IAW DHC-8 SRM 51-40-4.
- [SDR QXEA9902701](https://openairdocs.org/sdr/QXEA9902701.md): Skin · cracked · Dec 23, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - RIGHT NACELLE EXTERIOR OUTBOARD SKIN HAS.250 CRACK FROM RIVET HOLE TO SKIN PANEL EDGE AT STATION XN122.00 AND YW171.200, ALSO HAS LOOSE WORKING RIVET IN SAME AREA JUST AFT OF PANEL 426AR. REPAIRED IAW HORIZON AIR EA 9-54-239.
- [SDR QXEA9902699](https://openairdocs.org/sdr/QXEA9902699.md): Web · corroded · Dec 23, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX - RIGHT NACELLE TOP DECK AFT PORTION HAS CORROSION WHERE EXHAUST FINGERNAIL MOUNTS BETWEEN STATION XN255 AND XN280.00. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.
- [SDR QXEA9902674](https://openairdocs.org/sdr/QXEA9902674.md): Skin · dented · Dec 23, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > PDX - 4 DENT ON OUTER SKIN AT STATION 507, WL100, BL40RH. REPAIRED IAW HORIZON AIR EA 9-53-531.
- [SDR QXEA9902696](https://openairdocs.org/sdr/QXEA9902696.md): Guard · worn · Dec 21, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - INBOARD MIDDLE GRAVEL GUARD ATTACH POINT WORN EXCESSIVELY THIN. REPAIRED IAW RD8-54-41.
- [SDR QXEA9902673](https://openairdocs.org/sdr/QXEA9902673.md): Skin · chafed · Dec 21, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > PDX - CHAFE DAMAGE AT STATION 242.20 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT. IT IS APPROXIMATELY.035 DEEP. REPAIRED IAW HORIZON AIR EA 9-53-535.
- [SDR QXEA9902669](https://openairdocs.org/sdr/QXEA9902669.md): Bracket · corroded · Dec 21, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CORROSION IN ANGLE BRACKET AT FRAME X600.0 AND STRINGER 21S. REPAIRED IAW HORIZON AIR EA 9-53-536.
- [SDR QXEA9902663](https://openairdocs.org/sdr/QXEA9902663.md): Stringer · gouged · Dec 21, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Longeron/Stringer
  > PDX - SMALL GOUGE IN LEFT-HAND STRINGER 31 AT APPROXIMATELY STATION 550. REPAIRED IAW HORIZON AIR EA 9-53-532.
- [SDR QXEA9902652](https://openairdocs.org/sdr/QXEA9902652.md): Frame · corroded · Dec 21, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - CORROSION ON UNDER SIDE OF HORIZONTAL STIFFENING RIB ON AFT FLANGE OF FRAME 253.400, BETWEEN STRINGERS 24 LT AND 25 LT. REPAIRED IAW HORIZON AIR EA 9-53-534.
- [SDR QXEA9902700](https://openairdocs.org/sdr/QXEA9902700.md): Skin · cracked · Dec 19, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - RIGHT NACELLE EXTERIOR INBOARD SKIN HAS 1.5 CRACK AT STATION XN127.5 AND YW139.200, JUST AFT OF PANEL 425AL TOP EDGE. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902698](https://openairdocs.org/sdr/QXEA9902698.md): Web · punctured · Dec 19, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX - AFT NACELLE TOP DECK HAS A PUNCTURE HOLE AT APPROXIMATELY STATION X236.00 AND YW139.900. REPAIRED IAW HORIZON AIR EA 9-54-237.
- [SDR QXEA9902697](https://openairdocs.org/sdr/QXEA9902697.md): Stringer · damaged · Dec 19, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon, Longeron/Stringer
  > PDX - HOLE IN STRINGER XN176.5 AT STATION ZN17.04. REPAIRED IAW HORIZON AIR EA 9-54-238, FIGURE 2.
- [SDR QXEA9902694](https://openairdocs.org/sdr/QXEA9902694.md): Stringer · cracked · Dec 19, 1999 · N825PH · Dhav DHC8102 · Nacelle/Pylon, Longeron/Stringer
  > PDX - EXHAUST DECK AFT LATERAL STRINGER HAS ONE CRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-40-11.
- [SDR QXEA9902660](https://openairdocs.org/sdr/QXEA9902660.md): Stringer · corroded · Dec 19, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Longeron/Stringer
  > PDX - CORROSION INBOARD SIDE OF RIGHT-HAND STRINGER 32 AT FRAME STATION 488. INSTALLED NEW STRINGER SPLICE IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902683](https://openairdocs.org/sdr/QXEA9902683.md): Splice · corroded · Dec 18, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5 AND STRINGER 30RH. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902682](https://openairdocs.org/sdr/QXEA9902682.md): Splice · corroded · Dec 18, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CORROSION ON STRINGER SPLICE AT STATION 488.5, STRINGER 29RH. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902651](https://openairdocs.org/sdr/QXEA9902651.md): Floor Panel · corroded · Dec 18, 1999 · N825PH · Dhav DHC8102 · Fuselage Floor Panel
  > PDX - MAIN ENTRY THRESHOLD WHERE FLOOR PANEL ATTACHES HAD NUMEROUS SPOTS OF CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902692](https://openairdocs.org/sdr/QXEA9902692.md): Ice Shield · scratched · Dec 17, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > PDX - TWO DEEP SCRATCHES FOUND ABOVE RIGHT ICE SHIELD. REPAIRED IAW HORIZON AIR EA 9-53-530.
- [SDR QXEA9902691](https://openairdocs.org/sdr/QXEA9902691.md): Threshold · corroded · Dec 17, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - MINOR SURFACE CORROSION AROUND NUT PLATES UNDER MAIN CABIN DOOR THRESHOLD. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 6, PARAGRAPH 2C.
- [SDR QXEA9902720](https://openairdocs.org/sdr/QXEA9902720.md): Fitting · corroded · Dec 16, 1999 · N825PH · Dhav DHC8102 · Landing Gear Actuator
  > PDX - RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER MOUNTING PADS. REPAIRED IAW HORIZON AIR EA 9-54-233 AND EA 9-54-233A.
- [SDR QXEA9902719](https://openairdocs.org/sdr/QXEA9902719.md): Fitting · corroded · Dec 16, 1999 · N825PH · Dhav DHC8102 · Landing Gear Actuator
  > PDX - LEFT MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION ON H MEMBER. REPAIRED IAW HORIZON AIR EA 9-54-233 AND EA 9-54-233A.
- [SDR QXEA9902687](https://openairdocs.org/sdr/QXEA9902687.md): Seat Track · chafed · Dec 16, 1999 · N825PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RIGHT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT APPROXIMATELY STATION 282. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902653](https://openairdocs.org/sdr/QXEA9902653.md): Splice · corroded · Dec 16, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CORROSION ON STRINGER SPLICE AT STATION 531 AND STRINGER 30 RT. REPAIRED IAW DHC-8 SRM 51-20-16, SRM 51-40-11 AND SRM 51-20-36.
- [SDR QXEA9902643](https://openairdocs.org/sdr/QXEA9902643.md): Clip · corroded · Dec 16, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CLIP CORROSION BETWEEN LEFT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
- [SDR QXEA9902642](https://openairdocs.org/sdr/QXEA9902642.md): Clip · corroded · Dec 16, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CLIP CORROSION BETWEEN RIGHT-HAND STRINGER 32 AND 33 AT FRAME STATION 445. REPAIRED IAW DHC-8 SRM 53-20-21, FIGURE 1.
- [SDR QXEA9902690](https://openairdocs.org/sdr/QXEA9902690.md): Sill · damaged · Dec 15, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - NICKS BELOW CARGO DOOR SILL. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2.
- [SDR QXEA9902672](https://openairdocs.org/sdr/QXEA9902672.md): Skin · chafed · Dec 15, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > PDX - CHAFE DAMAGE AT STATION 262.400 AND STRINGER 11S, ABOVE RIGHT FORWARD EXIT, IT IS APPROXIMATELY.003 DEEP. REMOVAL WAS.001. FOUND TO BE WITHIN LIMITS IAW DHC-8 SRM PAGE 4, TABLE 2.
- [SDR QXEA9902668](https://openairdocs.org/sdr/QXEA9902668.md): Frame · gouged · Dec 15, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - GOUGE AT FRAME X618.0, BETWEEN STRINGERS 21S AND 20S. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902644](https://openairdocs.org/sdr/QXEA9902644.md): Connector · corroded · Dec 15, 1999 · N825PH · Dhav DHC8102 · Airfoil Anti/De-ice System
  > PDX - INSPECT DEICE DISTRIBUTOR CANNON PLUGS AND PRESSURE SWITCHES FOR CORROSION AND SERVICEABILITY. REMOVED AND REPLACED PRESSURE SWITCHES. (S/N 6503, 3509, 7020 AND 6951).
- [SDR QXEA9902689](https://openairdocs.org/sdr/QXEA9902689.md): Seat Track · chafed · Dec 14, 1999 · N825PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LEFT INBOARD SEAT TRACK CHAFFED AND LUG LIP WORN AT STATION 300. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902688](https://openairdocs.org/sdr/QXEA9902688.md): Seat Track · chafed · Dec 14, 1999 · N825PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LEFT INBOARD SEAT TRACK CHAFFED IN BOTTOM OF TRACK APPROXIMATELY AT STATION 330. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902686](https://openairdocs.org/sdr/QXEA9902686.md): Seat Track · gouged · Dec 14, 1999 · N825PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - SMALL GOUGE IN BOTTOM OF LEFT INBOARD SEAT TRACK, APPROXIMATELY STATION 377. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902664](https://openairdocs.org/sdr/QXEA9902664.md): Seat Track · chafed · Dec 14, 1999 · N825PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LEFT OUTBOARD SEAT TRACK HAS CHAFING PITS ON INBOARD LIP APPROXIMATELY STATION 242. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.
- [SDR QXEA9902693](https://openairdocs.org/sdr/QXEA9902693.md): Seat Track · corroded · Dec 12, 1999 · N825PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LIGHT SURFACE CORROSION ON RIVET HEADS AND WEB PLATE FROM RIGHT-HAND OUTBOARD SEAT TRACK TO STRINGER 23, BETWEEN FRAMES 387.350 AND 405.737. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902639](https://openairdocs.org/sdr/QXEA9902639.md): Stringer · corroded · Dec 12, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Longeron/Stringer
  > PDX - CORROSION AROUND RIVET LEFT-HAND SIDE OF STRINGER 33 AT FRAME STATION 488. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902685](https://openairdocs.org/sdr/QXEA9902685.md): Frame · corroded · Dec 11, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - CORROSION ON FRAME FLANGE AT STATION 531 BETWEEN STRINGERS 30 AND 31 RT. REMOVED LIGHT CORROSION IAW PSM 1-GEN-5, CHAPTER 4, PAGE 4-21, PARAGRAPH 8D. FOUND WITHIN LIMITS IAW DHC-8 SRM 53-00-16, PAGE 4, TABLE 2.
- [SDR QXEA9902684](https://openairdocs.org/sdr/QXEA9902684.md): Frame · corroded · Dec 11, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - CORROSION ON FRAME FLANGE AT STATION 510 BETWEEN STRINGERS 30 AND 31 RT. REPAIRED IAW 20-32-02, PAGE 2, PARAGRAPH A, B AND C.
- [SDR QXEA9902667](https://openairdocs.org/sdr/QXEA9902667.md): Frame · corroded · Dec 11, 1999 · N825PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - CORROSION NUMEROUS PLACED AROUND RIVETS ON TOP OF FRAME X653.349, BETWEEN STRINGER 23S AND 23P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2, SRM 51-20-11, PAGE 6, PARAGRAPH 2C AND SRM 51-40-11.
- [SDR QXEA9902661](https://openairdocs.org/sdr/QXEA9902661.md): Clip · corroded · Dec 11, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - CLIP HAS CORROSION BETWEEN RIGHT-HAND STRINGER 31 AND 32 AT FRAME STATION 531. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 1-2, PARAGRAPH 1 AND 2 AND SRM 51-20-11, PAGE 6, PARAGRAPH 2C.
- [SDR QXEA9902655](https://openairdocs.org/sdr/QXEA9902655.md): Splice · corroded · Dec 11, 1999 · N825PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - MINOR CORROSION ON TOP FLANGE OF STRINGER SPLICE AT STATION 531 AND STRINGER 28 RT. ACID ETCHED, ALODINED, AND PRIMED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW DHC-8 SRM 53-00-16, PAGE 4, TABLE 2.

Next page: https://openairdocs.org/deregistered/N825PH-2009-09-16/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 = 'N825PH' AND deregistration_id = 'N825PH-2009-09-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N825PH-2009-09-16/reports

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