# Service difficulty reports: N826PH, cancelled Jun 10, 2013

A list on [N826PH, cancelled Jun 10, 2013](https://openairdocs.org/deregistered/N826PH-2013-06-10.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 · 77 reports

- [SDR QXEA0101355](https://openairdocs.org/sdr/QXEA0101355.md): Skin · cracked · Aug 11, 2001 · N826PH · Dhav DHC8102 · Nacelle/Pylon, Plate/Skin
  > PDX - SEVERAL CRACKS IN AFT CONNECTION ANGLE FOR HORSE COLLAR TO UPPER SKIN AT TOP CENTER OF HORSE COLLAR STRUCTURE (MARKED). REPAIRED IAW EA 9-54-306.
- [SDR QXEA0100795](https://openairdocs.org/sdr/QXEA0100795.md): Stop · lack of lube · May 29, 2001 · N826PH · Dhav DHC8202 · Passenger/Crew Doors
  > SEA - CREW REPORTED MAIN CABIN DOOR HARD TO OPERATE. CLEANED AND LUBED DOOR STOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100790](https://openairdocs.org/sdr/QXEA0100790.md): Sign · inoperative · May 28, 2001 · N826PH · Dhav DHC8202 · Emergency Lighting
  > SEA - EMERGENCY EXIT SIGN AT ROW 4 A/B REPORTED INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100789](https://openairdocs.org/sdr/QXEA0100789.md): Connector · loose · May 24, 2001 · N826PH · Dhav DHC8202 · Emergency Lighting
  > SEA- EMERGENCY EXIT ROW FLOOR PATH LIGHTING FOUND INOPERATIVE. FOUND LOOSE ELECTRICAL CONNECTION. RESEATED CANNON PLUG. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002891](https://openairdocs.org/sdr/QXEA0002891.md): Unknown · odor · Oct 25, 2000 · N826PH · Dhav DHC8202 · Air Distribution System
  > SEA- STRANGE BURNING SMELL COMING FROM COCKPIT. INSPECTED ALL COCKPIT INSTRUMENTS AND LIGHTING. RAN BOTH BLEEDS. NO DEFECTS NOTED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA00002059](https://openairdocs.org/sdr/QXEA00002059.md): Wire · broken · Jul 29, 2000 · N826PH · Dhav DHC8202 · Light System Wiring
  > SEA- BROKEN WIRE FOUND ON AFT EMERGENCY FLOOR TRACK LIGHT. MAINTENANCE REPLACED THE CONNECTOR AT THE EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0000652](https://openairdocs.org/sdr/QXEA0000652.md): Light · malfunctioned · Mar 13, 2000 · N826PH · Dhav DHC8202 · Emergency Lighting
  > PDX- COCKPIT EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY AND RECEPTICLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0000554](https://openairdocs.org/sdr/QXEA0000554.md): Radar Unit · failed · Feb 18, 2000 · N826PH · Dhav DHC8202 · Weather Radar System
  > BOI - ODOR IN COCKPIT APPEARS TO BE COMING FROM RADAR CRT. REMOVED AND REPLACED RADAR CRT UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0000281](https://openairdocs.org/sdr/QXEA0000281.md): Skin · damaged · Jan 31, 2000 · N826PH · Dhav DHC8202 · Passenger/Crew Doors
  > YYC - APPROXIMATELY 2.2 SCRATCH IN PASSENGER DOOR SHELL NEAR BOTTOM FORWARD CORNER. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 52-00-16, PAGE 2 AND SRM 51-20-16, PAGE 4, TABLE 1.
- [SDR QXEA0000266](https://openairdocs.org/sdr/QXEA0000266.md): Structure · dented · Jan 31, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - DENT ON RIGHT SIDE OF FUSELAGE, 1 FORWARD OF STATION X405.737 AND APPROXIMATELY 5 BELOW STRINGER 16S. DENT WITHIN LIMITS DHC 8 SRM 53-00-16, PAGE 2, TABLE 1. YELLOW DOT APPLIED IAW HORIZON AIR YELLOW DOT PROGRAM, GMM 5-5-0.
- [SDR QXEA0000242](https://openairdocs.org/sdr/QXEA0000242.md): Skin · dented · Jan 31, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - DENT IN FUSELAGE 12 AFT OF STATION X312.36 AT STRINGER 2P. REPAIRED IAW RD 8-53-4753.
- [SDR QXEA0000267](https://openairdocs.org/sdr/QXEA0000267.md): Stud · broken · Jan 29, 2000 · N826PH · Dhav DHC8202 · Elevator Structure
  > YYC - STUD FOR BONDING WIRE AT RIGHT OUTBOARD ELEVATOR TAB HINGE POINT BROKEN AWAY FROM TRAILING EDGE OF ELEVATOR. REPAIRED IAW DHC 8 SRM 51-40-00 AND RD 8-53-4758.
- [SDR QXEA0000278](https://openairdocs.org/sdr/QXEA0000278.md): Panel · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Wing, Plate/Skin
  > YYC- RIGHT WING PANELS, 632AT THROUGH TO 632DT, 626AT, 629BT AND 624CT HAVE CORROSION ON FASTENERS AND PANELS. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000276](https://openairdocs.org/sdr/QXEA0000276.md): Skin · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Wing, Plate/Skin
  > YYC - NUMEROUS FASTENERS AND SURFACE AREAS HAVE LIGHT CORROSION ON RIGHT OUTBOARD WING, UPPER AND LOWER SURFACED, STATION 405.0 TO WING BOX END AT OUTBOARD. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-36 AND SRM 51-20-41.
- [SDR QXEA0000275](https://openairdocs.org/sdr/QXEA0000275.md): Skin · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Wing, Plate/Skin
  > YYC - LIGHT CORROSION ON FASTENERS AND SMALL SURFACE AREAS IN NUMEROUS PLACED OF RIGHT WING, STATION YW171.2-YW405.0. REPAIRED IAW DHC 8 SRM 51-20-11, SRM 51-20-35 AND SRM 51-20-41.
- [SDR QXEA0000274](https://openairdocs.org/sdr/QXEA0000274.md): Skin · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Wing, Plate/Skin
  > YYC- NUMEROUS FASTENERS AND SMALL AREAS HAVE LIGHT CORROSION ON RIGHT WING, UPPER AND LOWER SURFACES, STATION YW139.0-YW171.12. REPAIRED IAW DHC 8 SRM 51-20-00 AND SRM 51-20-11.
- [SDR QXEA0000273](https://openairdocs.org/sdr/QXEA0000273.md): Skin · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Wing, Plate/Skin
  > YYC - RIGHT WING HAS NUMEROUS FASTENERS WITH CORROSION ON AND AROUND FASTENER HEADS. REPAIRED IAW DHC 8 SRM 57-20-00 AND SRM 57-20-11.
- [SDR QXEA0000271](https://openairdocs.org/sdr/QXEA0000271.md): Spar · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Wing Spar
  > YYC - REAR SPAR HAS LIGHT SURFACE CORROSION FROM STATION YW45.0 - 139.0, ON RIGHT WING. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J.
- [SDR QXEA0000270](https://openairdocs.org/sdr/QXEA0000270.md): Skin · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Ailerons
  > YYC - AREAS OF LIGHT CORROSION ON UPPER AND LOWER SKIN OF RIGHT AILERON. REPAIRED IAW DHC 8 SRM 51-20-00 AND SRM 51-20-11.
- [SDR QXEA0000249](https://openairdocs.org/sdr/QXEA0000249.md): Frame · corroded · Jan 28, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Frame
  > YCC - GOUGE MARKS ON THREE FUSELAGE BULKHEAD FRAMES, FROM CONTACT WITH COLLAPSED WALL SUPPORT CHANNEL, STATION X653.34, X618.0 AND X636.0, BETWEEN STRINGERS 15S AND 14S. REPAIRED IAW SRM 53-00-16, TABLE 2 AND DHC-8 SRM 53-20-21, FIGURE 6, PAGE 7.
- [SDR QXEA0000244](https://openairdocs.org/sdr/QXEA0000244.md): Panel · damaged · Jan 28, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - RIGHT ARMPIT PANEL 264BR, TWO ANCHOR NUTS REQUIRE REPLACEMENT. ANCHOR NUTS REPLACED IAW DHC SRM 51-40-11 AND RD 8-53-4758.
- [SDR QXEA0000239](https://openairdocs.org/sdr/QXEA0000239.md): Skin · lightning strike · Jan 28, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - LIGHTNING STRIKE PITS ALONG RIGHT SIDE OF FUSELAGE BETWEEN STATION X222.0 AND X424.12, BETWEEN STRINGER 26S AND 28S. REPAIRED IAW RD 8-53-4762.
- [SDR QXEA0000277](https://openairdocs.org/sdr/QXEA0000277.md): Skin · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Trailing Edge Flaps
  > YYC - RIGHT WING, OUTBOARD FLAP, SEVERAL FASTENERS HAVE CORROSION ON AND AROUND HEADS ON UPPER AND LOWER SKINS. REPAIRED IAW DHC 8 SRM 51-20-11, SRM 51-20-51.
- [SDR QXEA0000269](https://openairdocs.org/sdr/QXEA0000269.md): Skin · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Ailerons
  > YYC - CORROSION ON AND AROUND FASTENERS ON RIGHT AILERON. REPAIRED IAW DHC 8 SRM 51-20-00, SRM 51-20-11, SRM 51-40-00 AND SRM 57-60-16, PAGE 2, TABLE 1.
- [SDR QXEA0000265](https://openairdocs.org/sdr/QXEA0000265.md): Structure · gouged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - GOUGES ON RIGHT FUSELAGE, 6 AFT OF STATION X333.3 BETWEEN STRINGER 16S AND 17S. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B AND RD 8-53-2432.
- [SDR QXEA0000264](https://openairdocs.org/sdr/QXEA0000264.md): Skin · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - SCRATCH ON FUSELAGE ROOF BETWEEN STATION X618 AND X636, STRINGER 3P. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000263](https://openairdocs.org/sdr/QXEA0000263.md): Skin · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - SCRATCH ON FUSELAGE ROOF ABOVE CARGO DOOR, APPROXIMATELY STATION X580.0, STRINGER 3P. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000262](https://openairdocs.org/sdr/QXEA0000262.md): Skin · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - SCRATCH ON FUSELAGE ROOF, 6 FORWARD OF STATION 291.0, STRINGER 5S. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000261](https://openairdocs.org/sdr/QXEA0000261.md): Structure · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SCRATCHES ON FUSELAGE FOOR BEHIND COMM ANTENNA, APPROXIMATELY STATION X302.0 ON ROOF CENTER LINE. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000260](https://openairdocs.org/sdr/QXEA0000260.md): Structure · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SCRATCH ON RIGHT FUSELAGE, APPROXIMATELY STATION 467.0, STRINGER 15S. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000259](https://openairdocs.org/sdr/QXEA0000259.md): Structure · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - CORROSION SPOT ON RIGHT FUSELAGE, STATION 387.35, STRINGER 13S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-16, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000258](https://openairdocs.org/sdr/QXEA0000258.md): Structure · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SCRATCH ON RIGHT FUSELAGE AT APPROXIMATELY STATION 282.4, STRINGER 20S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000257](https://openairdocs.org/sdr/QXEA0000257.md): Structure · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - TWO NICKS/CORROSION SPOTS ON RIGHT SIDE FUSELAGE BETWEEN STATION X405.73 AND 424.12, STRINGER 16S AND 17S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000256](https://openairdocs.org/sdr/QXEA0000256.md): Structure · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - CORROSION SPOT ON RIGHT SIDE FUSELAGE, APPROXIMATELY STATION X545.01, STRINGER 12S. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000255](https://openairdocs.org/sdr/QXEA0000255.md): Structure · gouged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SMALL GOUGE ON LEFT SIDE OF FUSELAGE, FORWARD OF STATION X167.0, STRINGER 18P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000254](https://openairdocs.org/sdr/QXEA0000254.md): Structure · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SCRATCHES ON LEFT SIDE OF FUSELAGE, APPROXIMATELY STATION X467.0, STRINGER 16P. REPAIRED IAW DHC-8 SRM 51-20-16, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000253](https://openairdocs.org/sdr/QXEA0000253.md): Structure · damaged · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SMALL NICK IN LEFT FUSELAGE AT APPROXIMATELY STATION 480.0, STRINGER 13P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 6, SECTION C AND SRM 51-20-36, PAGE 6, SECTION F-J.
- [SDR QXEA0000252](https://openairdocs.org/sdr/QXEA0000252.md): Structure · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - TWO SMALL CORROSION SPOTS ON LEFT SIDE OF FUSELAGE JUST AFT OF CARGO DOOR, APPROXIMATELY STATION X606, STRINGER 17P. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-36, PAGE 6, SECTION F-J AND SRM 51-20-41.
- [SDR QXEA0000248](https://openairdocs.org/sdr/QXEA0000248.md): Seat Track · corroded · Jan 27, 2000 · N826PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > YYC - LIGHT TO MODERATE CORROSION ON AFT SEAT TRACK, STATION X545.0 TO STATION X600.0, PARTICULARLY NEAR STATION 600.0, LEFT AND RIGHT TRACKS. REPAIRED IAW SRM 51-20-00 AND RD 8-53-4768.
- [SDR QXEA0000280](https://openairdocs.org/sdr/QXEA0000280.md): Skin · damaged · Jan 25, 2000 · N826PH · Dhav DHC8202 · Cargo/Baggage Doors
  > YYC - BAGGAGE DOOR EXTERNAL SKIN HAS A DEEP SCRATCH AT TOP OF DOOR. REPAIRED IAW DHC 8 SRM 51-20-11, PAGE 8, FIGURE 4, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-41 AND SRM 52-00-16, PAGE 2, TABLE 1.
- [SDR QXEA0000251](https://openairdocs.org/sdr/QXEA0000251.md): Web · corroded · Jan 25, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - LIGHT CORROSION FOUND ON WEB FROM STATION X531.5 THROUGH TO STATION X600.0 AND AROUND THE AFT SEAT TRACK ON LEFT SIDE IN CARGO BAY AREA. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, SECTION B, SRM 51-20-16, PAGE 4, SECTION C, SRM 51-20-36, PAGE 6, SECTION F
- [SDR QXEA0000250](https://openairdocs.org/sdr/QXEA0000250.md): Intercostal · bent · Jan 22, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - INTERCOSTAL FLANGE BENT, BAGGAGE COMPARTMENT, BETWEEN STATION X636.0 AND X653.34 AT STRINGER 18S. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 2, TABLE 1.
- [SDR QXEA0000247](https://openairdocs.org/sdr/QXEA0000247.md): Angle · corroded · Jan 22, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - LIGHT TO MODERATE CORROSION ON FLOOR SUPPORT ANGLE AT BASE OF COCKPIT FLOOR RISER BETWEEN THE INBOARD SEAT TRACKS, STATION 182.0. REPAIRED IAW SRM 51-20-11, PAGE 8, FIGURE 4, SRM 51-20-16, PAGE 4, SECTION C AND SRM 51-20-36, PAGE 6, SECTION F-J.
- [SDR QXEA0000246](https://openairdocs.org/sdr/QXEA0000246.md): Angle · corroded · Jan 22, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - LIGHT CORROSION ON FLOOR TO RISER PANEL CLOSING ANGLE, STATION X600 FROM APPROXIMATELY AIRCRAFT CENTER LINE TO RIGHT END OF ANGLE. REPAIRED IAW SRM 51-20-11, PAGE 8, FIGURE 4, SRM 51-20-16, PAGE 4, SECTION C AND SRM 51-20-36, PAGE 6, SECTION F-J.
- [SDR QXEA0000272](https://openairdocs.org/sdr/QXEA0000272.md): Skin · debonding · Jan 21, 2000 · N826PH · Dhav DHC8202 · Wing, Plate/Skin
  > YYC - RIGHT OUTBOARD LEADING EDGE HAS ALUMINUM STRIP DISBONDING ON UPPER EDGE. REPAIRED IAW DHC SRM 51-20-76, PAGES 1-5 AND RD 8-57-170.
- [SDR QXEA0000241](https://openairdocs.org/sdr/QXEA0000241.md): Skin · dented · Jan 21, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - MULTIPLE DENTS IN FUSELAG SKIN, DIRECTLY AFT OF 229 AND LEFT ICE SHIELD, 6 FORWARD OF STN X333.30. APPROXIMATELY STRINGER 12P-13P. REPAIRED IAW DHC SRM 53-00-10 AND RD 8-53-4754.
- [SDR QXEA0000245](https://openairdocs.org/sdr/QXEA0000245.md): Skin · corroded · Jan 17, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - LIGHT CORROSION ON LAP JOINT, FUSELAGE ROOF STATION X370.80, STRINGER 3P. REPAIRED IAW SRM 51-20-11, SRM 51-20-16 AND SRM 51-20-26.
- [SDR QXEA0000240](https://openairdocs.org/sdr/QXEA0000240.md): Skin · dented · Jan 17, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - DENT WITH DIMPLE CREASE IN THE CENTER, 4 FORWARD OF STATION 222.0, DIRECTLY ABOVE STRINGER 16S. REPAIRED IAW HORIZON AIR EA 9-53-537, DHC-8 SRM 53-00-16, RD 8-53-4749.
- [SDR QXEA0000268](https://openairdocs.org/sdr/QXEA0000268.md): Structure · damaged · Jan 13, 2000 · N826PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > YYC - SCRATCH ON FORWARD SPAR TOP SIDE OF BOTTOM LEADING EDGE ATTACH AREA BEHIND ANCHOR NUTS BETWEEN YW171.400 AND YW202..00. REPAIRED IAW DHC SRM 51-20-00 AND SRM 51-20-11.
- [SDR QXEA0000243](https://openairdocs.org/sdr/QXEA0000243.md): Skin · gouged · Jan 13, 2000 · N826PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > YYC - GOUGE IN FUSELAGE SKIN ON ROOF, 19 AFT OF STATION X312.36, APPROXIMATELY STRINGER 1S-2S. REPAIRED IAW DHC SRM 51-20-11, FIGURE 3 AND SRM 53-00-16, TABLE 1, SHEET 2.

Next page: https://openairdocs.org/deregistered/N826PH-2013-06-10/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 = 'N826PH' AND deregistration_id = 'N826PH-2013-06-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N826PH-2013-06-10/reports

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