# Service difficulty reports: N827PH, cancelled Jun 1, 2006

A list on [N827PH, cancelled Jun 1, 2006](https://openairdocs.org/deregistered/N827PH-2006-06-01.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 3 · 106 reports

- [SDR QXEA0201425](https://openairdocs.org/sdr/QXEA0201425.md): Skin · dented · Aug 2, 2002 · N827PH · Dhav DHC8102 · Cargo/Baggage Doors
  > CKB - BAGGAGE BAY DOOR HAS A DENT WITH A SCRATCH AFT OF THE DOOR HANDLE. REPAIRED IAW WVAC EO DH8S-52-0517A AND DHC-8 MM 52-30-00, STEPS 1 TO 32.
- [SDR QXEA0201419](https://openairdocs.org/sdr/QXEA0201419.md): Structure · cracked · Jul 23, 2002 · N827PH · Dhav DHC8102 · Horizontal Stabilizer Structure
  > CKB - HORIZONTAL STABILIZER HAS CRACK INDICATION. COMPLIED WITH SERVICE BULLETIN 8-55-22.
- [SDR QXEA0201411](https://openairdocs.org/sdr/QXEA0201411.md): Angle · cracked · Jun 21, 2002 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > CKB - RIGHT HAND CLOSING ANGLE CRACKED. REPLACED IAW RD 8-53-4556.
- [SDR QXEA0201424](https://openairdocs.org/sdr/QXEA0201424.md): Exhaust Pipe · cracked · Apr 13, 2002 · N827PH · Dhav DHC8102 · Engine Collector/Tailpipe/Nozzle
  > CKB - RIGHT HAND ENGINE FINGERNAIL HAS 1 INCH CRACK ON THE INSIDE EXHAUST OPENING. REPAIRED IAW DHC-8 SRM 51-10-00.
- [SDR QXEA0201413](https://openairdocs.org/sdr/QXEA0201413.md): Angle · cracked · Mar 29, 2002 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > CKB - RIGHT HAND FORWARD CLOSING ANGLE CRACKED. REPAIRED IAW EO DH8S-53-0367A AND HORIZON AIR EA 9-53-636A.
- [SDR QXEA0201414](https://openairdocs.org/sdr/QXEA0201414.md): Angle · cracked · Mar 21, 2002 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > CKB - LEFT HAND FORWARD CLOSING ANGLE CRACKED. REPAIRED IAW RD 8-53-4556.
- [SDR QXEA0201412](https://openairdocs.org/sdr/QXEA0201412.md): Angle · cracked · Mar 21, 2002 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > CKB - LEFT HAND AFT CLOSING ANGLE CRACKED. REPLACED IAW RD 8-53-4556.
- [SDR QXEA0201417](https://openairdocs.org/sdr/QXEA0201417.md): Skin · dented · Mar 11, 2002 · N827PH · Dhav DHC8102 · Vertical Stabilizer, Plate/Skin
  > CKB - DENT ON RIGHT HAND SIDE OF VERTICAL STABILIZER BETWEEN RIBS 10 AND 11. REPAIRED IAW HORIZON AIR EA 9-55-149A AND WVAC EO DH8S-55-0357A.
- [SDR QXEA0201416](https://openairdocs.org/sdr/QXEA0201416.md): Fastener · loose · Feb 28, 2002 · N827PH · Dhav DHC8102 · Fasteners
  > CKB - THREE FASTENERS AT THE BOTTOM RIGHT HAND SIDE OF THE VERTICAL STABILIZER ARE LOOSE. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA0201422](https://openairdocs.org/sdr/QXEA0201422.md): Bolt · worn · Feb 22, 2002 · N827PH · Dhav DHC8102 · Fasteners
  > CKB - ALL THREE ATTACHMENT BOLTS FOR AILERON HINGE FITTING TO HINGE ARM REQUIRES REPLACEMENT DUE TO WEAR SIGNS. REPAIRED IAW HORIZON AIR EA 9-57-583 AND WVAC EO DH8S-57-0364.
- [SDR QXEA0201423](https://openairdocs.org/sdr/QXEA0201423.md): Bolt · worn · Feb 20, 2002 · N827PH · Dhav DHC8102 · Fasteners
  > CKB - ALL THREE ATTCHEMENT BOLTS FOR AILERON HINGE FITTING TO HINGE ARM REQUIRES REPLACEMENT DUE TO WEAR SIGNS. REPAIRED IAW HORIZON AIR EA 9-57-583 AND WVAC EO DH8S-57-0364.
- [SDR QXEA0201420](https://openairdocs.org/sdr/QXEA0201420.md): Rivet · loose · Feb 15, 2002 · N827PH · Dhav DHC8102 · Fasteners
  > CKB - RIGHT HAND ELEVATOR TOP SIDE AT ELEVATOR MASS BALANCE TEN RIVETS IN SKID ARE LOOSE. REPAIRED IAW DHC-8 SRM 51-40-11, PAGE 1, STEP 16.
- [SDR QXEA0201418](https://openairdocs.org/sdr/QXEA0201418.md): Spar · gouged · Feb 5, 2002 · N827PH · Dhav DHC8102 · Wing Spar
  > CKB - RIGHT HAND WING FORWARD SPAR TOP FLANGE OUTBOARD OF NR 2 NACELLE AT 24 INCHES HAS GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, METHOD 2.
- [SDR QXEA0101411](https://openairdocs.org/sdr/QXEA0101411.md): Servo · malfunctioned · Aug 24, 2001 · N827PH · Dhav DHC8102 · Aileron Control System
  > PDR - AIRCRAFT HARD TO ROLL LEFT AND HARD TO RETURN WINGS LEVEL AT 200-220 KNOTS. REPLACED AUTO PILOT AILERON SERVO MOTOR. INSPECTED AILERONS AND SPOILER CONTROL, NO DISCREPANCIES NOTED. OPERATIONAL CHECK FLIGHT IS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100118](https://openairdocs.org/sdr/QXEA0100118.md): Odor · detected · Feb 15, 2001 · N827PH · Dhav DHC8102 · Air Distribution System
  > PDX- STRONG FUEL ODOR AFTER ENGINE START. GROUND RAN ENGINES. NO FUEL SMELL NOTED IN BLEED SYSTEM. SUSPECT SLIGHT TAIL WIND CAUSED FUEL VAPOR TO ENTER BLEED SYSTEM OF NR 2 ENGINE DURING NR 1 ENGINE START. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCR
- [SDR QXEA0002895](https://openairdocs.org/sdr/QXEA0002895.md): Battery · inoperative · Oct 28, 2000 · N827PH · Dhav DHC8102 · Emergency Lighting
  > SEA- EMERGENCY LIGHT BATTERY AT 3351 PS3 HAS NO POWER. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002260](https://openairdocs.org/sdr/QXEA0002260.md): Strut · failed · Aug 8, 2000 · N827PH · Dhav DHC8102 · Passenger/Crew Doors
  > PDX- MAIN CABIN DOOR HARD TO OPEN FROM INSIDE. REMOVED AND REPLACED LIFTING ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002259](https://openairdocs.org/sdr/QXEA0002259.md): Stop · out of adj · Aug 8, 2000 · N827PH · Dhav DHC8102 · Passenger/Crew Doors
  > PDX- FLIGHT ATTENDANT UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE, HANDLE IS STIFF. ADJUSTED DOOR STOPS, CLEANED AND LUBED ROLLERS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA0001999](https://openairdocs.org/sdr/QXEA0001999.md): Bearing · lack of lube · Jul 21, 2000 · N827PH · Dhav DHC8102 · Passenger/Crew Doors
  > PDX- MAIN CABIN DOOR HARD TO OPEN. LUBED OVERCENTER PUSH TUBE BEARING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA0000234](https://openairdocs.org/sdr/QXEA0000234.md): Actuator · damaged · Feb 2, 2000 · N827PH · Dhav DHC8102 · Landing Gear Door Actuator
  > YKM - LEFT SIDE MAIN GEAR DOOR FAILED TO RETRACT UPON GEAR RETRACTION. INSPECTED, FOUND GEAR DOOR ACTUATOR HARDWARE MISSING. REMOVED AND REINSTALLED GEAR DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9902677](https://openairdocs.org/sdr/QXEA9902677.md): Cable · lack of lube · Dec 26, 1999 · N827PH · Dhav DHC8102 · Passenger/Crew Doors
  > PDX - MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE LUBRICATED THE MAIN CABIN DOOR CABLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA9902622](https://openairdocs.org/sdr/QXEA9902622.md): Controller · malfunctioned · Dec 17, 1999 · N827PH · Dhav DHC8102 · Flight Compartment Windows
  > PDX- ON APPROACH, A STRONG SMELL WAS NOTED IN THE COCKPIT. AFTER LANDING AND ENGINE SHUT DOWN, SMELL LINGERED. SMOKE AND SMELL WAS NOTED IN THE COCKPIT ONLY, NOT THE CABIN. MAINTENANCE REPLACED THE PILOT'S WINDSHIELD AND WINDSHIELD HEAT CONTROLLER. OPERATI
- [SDR QXEA9902265](https://openairdocs.org/sdr/QXEA9902265.md): Fairing · delaminated · Nov 3, 1999 · N827PH · Dhav DHC8102 · Aerodynamic Fairings
  > PDX - THERE ARE NUMEROUS DELAMINATED AREAS ON COMPOSITE AERODYNAMIC FAIRING AROUND ACCESS PANEL 261AT. REPAIRED IAW HORIZON AIR EA 9-53-492, STEPS 13-20, AND SRM 51-40-11.
- [SDR QXEA9902271](https://openairdocs.org/sdr/QXEA9902271.md): Support · corroded · Nov 2, 1999 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - INBOARD AND OUTBOARD FLOOR SUPPORTS FOR WARDROBE ARE CORRODED ALONG UPPER SURFACE. REPAIRED IAW HORIZON AIR EA 9-53-483.
- [SDR QXEA9902300](https://openairdocs.org/sdr/QXEA9902300.md): Seat Track · corroded · Oct 31, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LEFT INBOARD CABIN SEAT TRACK AT FUSELAGE STATION 597.500 HAS CORROSION ON TOP SURFACE. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902270](https://openairdocs.org/sdr/QXEA9902270.md): Seat Track · corroded · Oct 31, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - NUMEROUS CORROSION DISCREPANCIES ON LEFT INBOARD CENTER SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902249](https://openairdocs.org/sdr/QXEA9902249.md): Frame · damaged · Oct 30, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - FORWARD SIDE OF OUTBOARD MAIN LANDING GEAR FRAME, TWO DRILL MARKS, JUST AFT OF ENGINE BAY FIREWALL. REPAIRED IAW HORIZON AIR EA 9-54-221.
- [SDR QXEA9902234](https://openairdocs.org/sdr/QXEA9902234.md): Angle · damaged · Oct 30, 1999 · N827PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX - ANGLE ATTACHMENT FOR OUTBOARD NACELLE SKIN TO WIG BOX, TO FROM MAIN LANDING GEAR FRAME. REPAIRED IAW HORIZON AIR EA 9-53-485.
- [SDR QXEA9902296](https://openairdocs.org/sdr/QXEA9902296.md): Channel · corroded · Oct 29, 1999 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - RIGHT FORWARD DRAIN CHANNEL ATTACHED TO RIGHT INBOARD CABIN SEAT TRACK HAS FRETTING CORROSION AND IS CRACKED AROUND FORWARD ATTACH RIVET HOLES AT STATION 182.000. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902276](https://openairdocs.org/sdr/QXEA9902276.md): Frame · corroded · Oct 29, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - FORWARD SIDE OF FRAME 510.00 HAS CORROSION AT OUTBOARD SIDE OF STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-490.
- [SDR QXEA9902275](https://openairdocs.org/sdr/QXEA9902275.md): Structure · corroded · Oct 29, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Structure
  > PDX - THERE IS CORROSION ON SKIN AND FRAME FORWARD OF 531.500 AT STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-489 AND DHC-8 SRM 51-40-11.
- [SDR QXEA9902250](https://openairdocs.org/sdr/QXEA9902250.md): Firewall · cracked · Oct 29, 1999 · N827PH · Dhav DHC8102 · Nacelle/Pylon, Bulkhead/Firewall
  > PDX - THERE IS A CRACK IN THE AFT FIREWALL OF THE NR 2 ENGINE, OUTBOARD SIDE, AT BEND IN MATERIAL JUST ABOVE FIRE DETECTION LOOP BRACKET. REPAIRED IAW HORIZON AIR EA 9-54-219 AND RD 8-54-430.
- [SDR QXEA9902280](https://openairdocs.org/sdr/QXEA9902280.md): Frame · corroded · Oct 28, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - FORWARD SIDE OF FRAME 467 HAS CORROSION AT STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-488.
- [SDR QXEA9902279](https://openairdocs.org/sdr/QXEA9902279.md): Frame · corroded · Oct 28, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - FORWARD SIDE OF FRAME 488.5 IS CORRODED AT STRINGER 341S. REPAIRED IAW HORIZON AIR EA 9-53-487.
- [SDR QXEA9902274](https://openairdocs.org/sdr/QXEA9902274.md): Frame · corroded · Oct 28, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - FRAME 545.00 HAS CORROSION ON FORWARD SIDE JUST OUTBOARD OF STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-486 AND DHC-8 SRM 51-40-11.
- [SDR QXEA9902273](https://openairdocs.org/sdr/QXEA9902273.md): Frame · corroded · Oct 28, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - FRAME 531.5 HAS CORROSION ON AFT SIDE JUST OUTBOARD OF STRINGER 31S. REPAIRED IAW HORIZON AIR EA 9-53-489 AND DHC-8 SRM 51-40-11.
- [SDR QXEA9902272](https://openairdocs.org/sdr/QXEA9902272.md): Frame · corroded · Oct 28, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - CORROSION ON FORWARD SIDE OF FRAME 4885 FROM STRINGER 32P TO STRINGER 32S. REPAIRED IAW HORIZON AIR EA 9-53-487.
- [SDR QXEA9902255](https://openairdocs.org/sdr/QXEA9902255.md): Skin · dented · Oct 28, 1999 · N827PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - DENT ON INBOARD SIDE OF LEFT NACELLE AT APPROXIMATELY XN 155.30 AND ZN 24.25. REPAIRED IAW SRM 54.30.21, PAGE 2, FIGURE 2.
- [SDR QXEA9902267](https://openairdocs.org/sdr/QXEA9902267.md): Seat Rack · coroded · Oct 27, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - NUMEROUS CORROSION DISCREPANCIES ON LEFT INBOARD FORWARD SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902282](https://openairdocs.org/sdr/QXEA9902282.md): Support · failed · Oct 25, 1999 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - THE VERTICAL FLOOR SUPPORT WEB AT Y9.250 RIGHT IS BUCKLED APPROXIMATELY.090 AT THE TOP JUST AFT OF X601 TO ABOUT X611. REPAIRED IAW HORIZON AIR EA 9-53-478.
- [SDR QXEA9902253](https://openairdocs.org/sdr/QXEA9902253.md): Skin · chafed · Oct 23, 1999 · N827PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - RIGHT NACELLE EXHAUST FINGERNAIL DECK HAS 1.5 BY.75 HOLE CHAFED THROUGH AT STATION XN 224.76. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 THROUGH 4.
- [SDR QXEA9902252](https://openairdocs.org/sdr/QXEA9902252.md): Skin · chafed · Oct 23, 1999 · N827PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - RIGHT NACELLE EXHAUST FINGERNAIL DECK HAS DEEP CHAFE MARKS AT STATION XN 224.76. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 THROUGH 4.
- [SDR QXEA9902298](https://openairdocs.org/sdr/QXEA9902298.md): Seat Track · corroded · Oct 22, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LEFT OUTBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 436.500 AND 456.500 HAS CORROSION ON TOP SURFACE AND INSIDE CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902297](https://openairdocs.org/sdr/QXEA9902297.md): Seat Track · corroded · Oct 22, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - LEFT OUTBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 291.400 AND 366.000 HAS CORROSION ON TOP SURFACE AND INSIDE CHANNEL. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902295](https://openairdocs.org/sdr/QXEA9902295.md): Seat Track · corroded · Oct 22, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RIGHT INBOARD CABIN SEAT TRACK BETWEEN FUSELAGE STATION 182.500 AND 240.500 HAS CORROSION ON TOP SURFACE AND AROUND 4 SCREW HOLES. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902288](https://openairdocs.org/sdr/QXEA9902288.md): Seat Track · corroded · Oct 22, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - RIGHT INBOARD CABIN SEAT TRACK AT STATION 597.000 HAS CORROSION ON TOP SURFACE AROUND TIE DOWN PEG HOLES. REPAIRED IAW DHC-8 SRM 51-40-00, TABLE 4.
- [SDR QXEA9902269](https://openairdocs.org/sdr/QXEA9902269.md): Seat Track · corroded · Oct 22, 1999 · N827PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX - NUMEROUS CORROSION AND DAMAGE DISCREPANCIES ON RIGHT CENTER SEAT TRACK. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA9902266](https://openairdocs.org/sdr/QXEA9902266.md): Threshold · corroded · Oct 22, 1999 · N827PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX - MAIN CABIN DOOR THRESHOLD BEAM AND NUTPLATES HAVE CORROSION TOP SIDE AND UNDER SIDE X224 TO X248 Z100. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902251](https://openairdocs.org/sdr/QXEA9902251.md): Skin · chafed · Oct 22, 1999 · N827PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - RIGHT NACELLE UPPER DECK FOR EXHAUST FINGERNAIL IS CORRODED AND HAS SEVERAL AREAS WITH DEEP CHAFE MARKS. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA9902258](https://openairdocs.org/sdr/QXEA9902258.md): Frame · corroded · Oct 21, 1999 · N827PH · Dhav DHC8102 · Fuselage Main, Frame
  > PDX - PITTING CORROSION ON TOP HOLE OF LEFT MAIN LANDING GEAR FRAME WHERE MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING IS MOUNTED. REPAIRED IAW HORIZON AIR EA 9-54-213.

Next page: https://openairdocs.org/deregistered/N827PH-2006-06-01/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 = 'N827PH' AND deregistration_id = 'N827PH-2006-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N827PH-2006-06-01/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.