# Service difficulty reports: N822PH, cancelled Dec 4, 2001

A list on [N822PH, cancelled Dec 4, 2001](https://openairdocs.org/deregistered/N822PH-2001-12-04.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 · 90 reports

- [SDR QXEA0100227](https://openairdocs.org/sdr/QXEA0100227.md): Bearing · failed · Mar 6, 2001 · N822PH · Dhav DHC8102 · Engine (Turbine/Turboprop)
  > PDX - ON APPROACH TO PDX AN INCREASING ITT ON NR 2 ENGINE NOTED ALONG WITH VIBRATION. AFTER GEAR AND FLAP EXTENSION SMOKE SMELL NOTED. DECLARED AN EMERGENCY. AFTER LANDING TOWER ADVISED SMOKE ON NR 2 ENGINE. THE FIRE/SHUTDOWN ON GROUND CHECKLIST WAS CONDUC
- [SDR QXEA0100014](https://openairdocs.org/sdr/QXEA0100014.md): Light · inoperative · Jan 9, 2001 · N822PH · Dhav DHC8102 · Emergency Lighting
  > PDX - FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED OVERHEAD EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0003050](https://openairdocs.org/sdr/QXEA0003050.md): Rod · lack of lube · Nov 17, 2000 · N822PH · Dhav DHC8102 · Passenger/Crew Doors
  > SEA- MAIN CABIN DOOR SOMETIMES JAMS WHEN OPEN. LEVER AT ABOUT HALFWAY POSITION. LUBED MAIN CABIN DOOR OVERCENTER RODS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA0002725](https://openairdocs.org/sdr/QXEA0002725.md): Sign · inoperative · Sep 27, 2000 · N822PH · Dhav DHC8102 · Emergency Lighting
  > PDX- LOWER EMERGENCY EXIT SIGN IN SEAT 4A IS MISSING COVER. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002486](https://openairdocs.org/sdr/QXEA0002486.md): Strap · out of adj · Aug 28, 2000 · N822PH · Dhav DHC8102 · Passenger/Crew Doors
  > YKM- MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND TEFLON STRIP UNDER DOOR HINGE IMPINGING ON DOOR. ADJUSTED TEFLON STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA0002347](https://openairdocs.org/sdr/QXEA0002347.md): Skin · lightning strike · Aug 22, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- LIGHTNING STRIKES ON AIRCRAFT SKIN. REPAIRED IAW DHC-8 SRM 5-50-31.
- [SDR QXEA0002338](https://openairdocs.org/sdr/QXEA0002338.md): Stiffener · cracked · Aug 21, 2000 · N822PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > YXX- CRACKS AT UPPER END OF VERTICAL STIFFENERS, 4 INCHES OUTBOARD OF CENTER LINE OF AIRCRAFT LEFT AND RIGHT ON BULKHEAD AT FUSELAGE STATION X66.00. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-16 AND 51-40-11.
- [SDR QXEA0002357](https://openairdocs.org/sdr/QXEA0002357.md): Firewall · damaged · Aug 20, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon, Bulkhead/Firewall
  > YXX- LEFT HAND NACELLE FORWARD FIREWALL INBOARD LOWER AREA HAS TWO RIVETS WITH HEADS CHAFED OFF AND AREA OF CHAFING JUST ABOVE XM107-80 AND ZM1.5-00. REPAIRED IAW RD 8-54-1333.
- [SDR QXEA0002328](https://openairdocs.org/sdr/QXEA0002328.md): Shield · cracked · Aug 20, 2000 · N822PH · Dhav DHC8102 · Cargo/Baggage Doors
  > YXX- CARGO DOOR SHIELD AT CEILING IS CRACKED IN SEVERAL LOCATIONS. REPAIRED IAW DHC-8 SRM 51-70-00 PAGE 401.
- [SDR QXEA0002374](https://openairdocs.org/sdr/QXEA0002374.md): Skin · gouged · Aug 18, 2000 · N822PH · Dhav DHC8102 · Passenger/Crew Doors
  > YXX- MAIN CABIN DOOR OUTER SHELL HAS A GOUGE ON SEALING SURFACE OF DOOR SHELL AT LOWER FORWARD CORNER. REPAIRED IAW DHC-8 SRM 51-40-11.
- [SDR QXEA0002368](https://openairdocs.org/sdr/QXEA0002368.md): Drag Strut · chafed · Aug 18, 2000 · N822PH · Dhav DHC8102 · Main Landing Gear
  > YXX- LEFT HAND MAIN LANDING GEAR DRAG STRUT FOUND WITH CHAFE MARKS. REPAIRED IAW DHC-8 RD 8-32-474, HORIZON AIR EA 9-32-102 AND CONAIR EO 2869.
- [SDR QXEA0002366](https://openairdocs.org/sdr/QXEA0002366.md): Structure · loose · Aug 18, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > YXX- RIGHT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE AS PER DHC-8 100 MM.
- [SDR QXEA0002363](https://openairdocs.org/sdr/QXEA0002363.md): Skin · gouged · Aug 18, 2000 · N822PH · Dhav DHC8102 · Wing, Plate/Skin
  > YXX- GOUGE ON LOWER WING SKIN AT FORWARD END OF LEFT HAND NR 5 FLAP TRACK, LYW373. REPAIRED IAW DHC-8 SRM 57-10-16, 51-00-06, 51-20-16 PAGE 1-4 AND 51-20-36 PAGE 1-9.
- [SDR QXEA0002358](https://openairdocs.org/sdr/QXEA0002358.md): Structure · loose · Aug 18, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > YXX- LEFT HAND NACELLE TO REAR SPAR INBOARD AND OUTBOARD END OF LINK HAS LOOSE HARDWARE. REPLACED WORN HARDWARE PER DHC-8 MM.
- [SDR QXEA0002356](https://openairdocs.org/sdr/QXEA0002356.md): Firewall · chafed · Aug 18, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon, Bulkhead/Firewall
  > YXX- CHAFE DAMAGE ON NR 2 FORWARD OUTBOARD FIREWALL WEB AT STATION YN107.18 AND ZN-10.50. REPAIRED IAW DHC-8 RD 8-54-1330, 8-54-081, AND SRM 51-00-06.
- [SDR QXEA0002350](https://openairdocs.org/sdr/QXEA0002350.md): Mount · chafed · Aug 18, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon, Attach Fittings
  > YXX- LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. BLENDED AREA.
- [SDR QXEA0002329](https://openairdocs.org/sdr/QXEA0002329.md): Skin · dented · Aug 18, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- LEFT HAND FUSELAGE HAS A DENT BETWEEN STRINGER 19 AND 20 FORWARD OF FRAME X405.737. REPAIRED IAW DHC-8 RD 8-53-457 AND DHC-8 SRM 51-00-05, 53-00-16.
- [SDR QXEA0002324](https://openairdocs.org/sdr/QXEA0002324.md): Door Frame · gouged · Aug 18, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Structure
  > YXX- CARGO DOOR CUTOUT UPPER WEB IS GOUGED BESIDE DOOR STOPS AT FUSELAGE STATION X564.5X AND X580.5. REPAIRED IAW DHC-8 SRM 51-20-11 PAGE 7 AND HORIZON AIR EA 9-53-571.
- [SDR QXEA0002349](https://openairdocs.org/sdr/QXEA0002349.md): Skin · dented · Aug 17, 2000 · N822PH · Dhav DHC8102 · Rudder, Plate/Skin
  > YXX- DENT IN UPPER RIGHT HAND SIDE OF FORWARD RUDDER 4 INCHES FORWARD OF AFT SPAR AT UPPER HINGE LINE. REPAIRED IAW DHC-8 SRM 55-40-16, 55-40-28, AND 51-00-06.
- [SDR QXEA0002364](https://openairdocs.org/sdr/QXEA0002364.md): Plate · cracked · Aug 16, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- RIGHT HAND LADDER PLATE HAS A CRACK FROM DEUTCH NUT HOLE. REPAIRED IAW DHC-8 RD 8-57-876.
- [SDR QXEA0002352](https://openairdocs.org/sdr/QXEA0002352.md): Firewall · cracked · Aug 16, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon, Bulkhead/Firewall
  > YXX- LEFT HAND NACELLE FIREWALL EXTENSION TUBE IS CRACKED AT WELD AND BOLT HOLES. REPAIRED IAW DHC-8 RD 8-54-16, AND 8-54-8.
- [SDR QXEA0002351](https://openairdocs.org/sdr/QXEA0002351.md): Mount · chafed · Aug 16, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon, Attach Fittings
  > YXX- RIGHT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. REPAIRED IAW DHC-8 RD 8-54-523 AND SRM 51-00-06.
- [SDR QXEA0002372](https://openairdocs.org/sdr/QXEA0002372.md): Skin · lightning strike · Aug 15, 2000 · N822PH · Dhav DHC8102 · Passenger/Crew Doors
  > YXX- MAIN CABIN DOOR OUTER SHELL EXTERIOR SKIN HAS LIGHTNING STRIKES. REPARIED IAW DHC-8 SRM 51-20-11, 52-00-16, 51-00-05 AND 20-34-11 PAGE 17.
- [SDR QXEA0002371](https://openairdocs.org/sdr/QXEA0002371.md): Skin · lightning strike · Aug 15, 2000 · N822PH · Dhav DHC8102 · Emergency Exits
  > YXX- RIGHT HAND EMERGENCY EXIT DOOR HAS LIGHTNING STRIKES. REPAIRED IAW DHC-8 SRM 51-20-11, 52-00-16, 51-00-05 AND 51-20-00 PAGE 5.
- [SDR QXEA0002359](https://openairdocs.org/sdr/QXEA0002359.md): Skin · damaged · Aug 15, 2000 · N822PH · Dhav DHC8102 · Wing, Plate/Skin
  > YXX- LEFT HAND WING TIP LEADING EDGE ERRODED. REPAIRED IAW DHC-8 RD 8-57-071.
- [SDR QXEA0002348](https://openairdocs.org/sdr/QXEA0002348.md): Antenna · damaged · Aug 15, 2000 · N822PH · Dhav DHC8102 · Visual Omnirange (VOR) System
  > YXX- DAMAGE ON LEFT HAND VOR ANTENNA AND FORWARD MOUNT ON VERTICAL FIN RIB 9 AND X848. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-55-955.
- [SDR QXEA0002342](https://openairdocs.org/sdr/QXEA0002342.md): Skin · dented · Aug 15, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- DENT AT FUSELAGE STATION X282.400 BETWEEN STRINGER 10 AND 11 JUST FORWARD OF ICE SHIELD. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-06 AND 51-00-05.
- [SDR QXEA0002369](https://openairdocs.org/sdr/QXEA0002369.md): Skin · dented · Aug 12, 2000 · N822PH · Dhav DHC8102 · Entrance Stairs
  > YXX- AIRSTAIR DOOR OUTER SKIN HAS MANY DENTS AND SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-26 PAGE 6, 51-20-11, 52-00-16 AND 51-00-06.
- [SDR QXEA0002367](https://openairdocs.org/sdr/QXEA0002367.md): Skin · chafed · Aug 12, 2000 · N822PH · Dhav DHC8102 · Wing, Plate/Skin
  > YXX- RIGHT HAND UPPER WING SKIN AFT OF NR 2 ENGINE HAS CHAFE DAMAGE FROM PANEL 422ET. REPAIRED IAW DHC-8 SRM 57-10-16, 51-00-06 AND 51-20-00.
- [SDR QXEA0002362](https://openairdocs.org/sdr/QXEA0002362.md): Skin · gouged · Aug 12, 2000 · N822PH · Dhav DHC8102 · Wing, Plate/Skin
  > YXX- LEFT HAND UPPER WING SKIN AFT OF NR 1 ENGINE NACELLE HAS A GOUGE FROM PANEL 412ET. REPAIRED IAW DHC-8 SRM 57-10-16, 51-20-11 AND 51-20-00 PAGE 5.
- [SDR QXEA0002361](https://openairdocs.org/sdr/QXEA0002361.md): Skin · gouged · Aug 12, 2000 · N822PH · Dhav DHC8102 · Wing, Plate/Skin
  > YXX- LEFT HAND WING CENTER SECTION OF UPPER SKIN AT YW70.00 HAS GOUGE. REPAIRED IAW DHC-8 SRM 51-20-11, 57-10-16 PAGE 2 AND 51-20-00 PAGE 5.
- [SDR QXEA0002360](https://openairdocs.org/sdr/QXEA0002360.md): Skin · gouged · Aug 12, 2000 · N822PH · Dhav DHC8102 · Wing, Plate/Skin
  > YXX- THREE GOUGES ON LEFT HAND UPPER WING SKIN BETWEEN YW139.000 AND YW171.000. REPAIRED IAW DHC-8 SRM 51-20-11, AND 57-10-16 PAGE 2.
- [SDR QXEA0002355](https://openairdocs.org/sdr/QXEA0002355.md): Structure · cracked · Aug 12, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > YXX- RIGHT HAND NACELLE FOUND TO HAVE TWO CRACKS ABOVE ACCESS HOLES FOR MAIN LANDING GEAR RETRACT ACTUATOR ATTACH HARDWARE. REPAIRED IAW DHC-8 RD 8-54-109 PAGE 3 AND 4, SRM 54-00-00 PAGE 1 AND 20-21-18.
- [SDR QXEA0002353](https://openairdocs.org/sdr/QXEA0002353.md): Structure · cracked · Aug 12, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > YXX- CRACKED STRUCTURE ON NR 2 NACELLE BETWEEN MID DOOR''S FORWARD HINGE AND FORWARD BRACKET OF EXTENSION HANDLE. REPAIRED IAW DHC-8 RD 8-54-239 AND SRM 51-40-11 PAGES 1-4 AND 32-10-21.
- [SDR QXEA0002337](https://openairdocs.org/sdr/QXEA0002337.md): Skin · dented · Aug 12, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- LEFT HAND FUSELAGE HAS A DENT JUST AFT OF STATION X636.00 BETWEEN STRINGER 16 AND 15. REPAIRED IAW DHC-8 SRM 53-00-16, 51-00-06, 51-00-05, RD 8-53-5230 AND HORIZON AIR EO 2857.
- [SDR QXEA0002336](https://openairdocs.org/sdr/QXEA0002336.md): Skin · dented · Aug 12, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- LEFT HAND FUSELAGE JUST FORWARD OF MAIN CABIN DOOR THERE IS A DENT FORWARD OF STATION X545.00 BETWEEN STRINGER 22 AND 23. REPAIRED IAW DHC-8 SRM 51-20-26, 53-00-16 AND 51-00-06.
- [SDR QXEA0002373](https://openairdocs.org/sdr/QXEA0002373.md): Skin · chafed · Aug 11, 2000 · N822PH · Dhav DHC8102 · Passenger/Crew Doors
  > YXX- MAIN CABIN DOOR OUTER SHELL HAS CHAFE DAMAGE ON INTERIOR LIP, 18 INCHES FROM DOOR CABLE ATTACH POINT. REPAIRED IAW DHC-8 SRM 52-00-16 AND 51-20-16 PAGE 1-5.
- [SDR QXEA0002354](https://openairdocs.org/sdr/QXEA0002354.md): Firewall · cracked · Aug 11, 2000 · N822PH · Dhav DHC8102 · Nacelle/Pylon, Bulkhead/Firewall
  > YXX- RIGHT HAND NACELLE FIREWALL FOUND CRACKED ABOVE INBOARD END OF OIL COOLER. REPAIRED IAW DHC-8 SRM 51-40-11, 54-00-00 PAGE 1 AND 20-21-18.
- [SDR QXEA0002326](https://openairdocs.org/sdr/QXEA0002326.md): Skin · dented · Aug 11, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- LEFT HAND FUSELAGE HAS DENTS BETWEEN 30 AND 31 AT STATION X151.600. REPAIRED IAW DHC-8 RD 8-53-5206, DHC-8 SRM 53-00-16 AND 51-00-05.
- [SDR QXEA0002325](https://openairdocs.org/sdr/QXEA0002325.md): Skin · dented · Aug 11, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Structure
  > YXX- RIGHT HAND FUSELAGE HAS DENT BETWEEN STRINGER 29 AND 30 AT STATION X182.00. REPAIRED IAW HORIZON AIR EA 9-53-561 AND DHC-8 SRM 51-00-05.
- [SDR QXEA0002312](https://openairdocs.org/sdr/QXEA0002312.md): Threshold · corroded · Aug 11, 2000 · N822PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > YXX- SEVERAL AREAS OF PITTING AND SURFACE CORROSION ON THRESHOLD OF MAIN CABIN DOOR CUTOUT, AT FLOOR LEVEL BETWEEN FUSELAGE STATION 222.000AND X252.700. REPAIRED IAW DHC-8 SRM 51-20-00, 51-40-00 AND 20-21-21.
- [SDR QXEA0002332](https://openairdocs.org/sdr/QXEA0002332.md): Skin · dented · Aug 10, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- LEFT HAND FUSELAGE HAS DENT AND GOUGE BETWEEN STRINGER 17 AND 19 AT FRAME 151.600. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND 51-00-06.
- [SDR QXEA0002315](https://openairdocs.org/sdr/QXEA0002315.md): Seat Track · corroded · Aug 10, 2000 · N822PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > YXX- LEFT HAND OUTBOARD FORWARD SEAT TRACK HAS PITTING CORROSION WHERE SEATS ATTACH TO TRACK. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11.
- [SDR QXEA0002370](https://openairdocs.org/sdr/QXEA0002370.md): Structure · chafed · Aug 9, 2000 · N822PH · Dhav DHC8102 · Emergency Exits
  > YXX- RIGHT HAND EMERGENCY EXIT DOOR, BOTTOM AFT CORNER OF DOOR HAS CHAFE DAMAGE TO DOOR STRUCTURE AND RIVETS. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5, 51-40-11 PAGE 1-4 AND 52-00-16 TABLE 2.
- [SDR QXEA0002346](https://openairdocs.org/sdr/QXEA0002346.md): Intercostal · corroded · Aug 8, 2000 · N822PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > YXX- RIGHT HAND FORWARD OUTBOARD SEAT TRACK INTERCOSTAL TO FRAME X356, Z102 AND Y42 HAVE CORROSION. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-00 PAGE 5 AND 51-20-11.
- [SDR QXEA0002343](https://openairdocs.org/sdr/QXEA0002343.md): Frame · gouged · Aug 4, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Frame
  > YXX- AFT FACE OF FRAME X240.50 BETWEEN STRINGER 19 AND 22 HAVE MINOR SCRATCHES AND GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, 53-00-16 AND 51-20-00.
- [SDR QXEA0002323](https://openairdocs.org/sdr/QXEA0002323.md): Skin · corroded · Aug 3, 2000 · N822PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > YXX- CORROSION AROUND MARKER BEACON ANTENNA. REPAIRED IAW DHC-8 SRM 53-00-16, 51-20-11 AND 51-20-00.
- [SDR QXEA0002316](https://openairdocs.org/sdr/QXEA0002316.md): Seat Track · corroded · Aug 3, 2000 · N822PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > YXX- LEFT HAND INBOARD FORWARD SEAT TRACK HAS EVIDENCE OF PITTING CORROSION AT SEAT ATTACH SPOTS. REPAIRED IAW DHC-8 AD 8-53-3074 AND 8-53-1339.
- [SDR QXEA0002365](https://openairdocs.org/sdr/QXEA0002365.md): Skin · unbonded · Aug 2, 2000 · N822PH · Dhav DHC8102 · Wing, Control Surfaces
  > YXX- RIGHT HAND AILERON TIP TRAILING EDGE IS DISBONDING. REPAIRED IAW DHC-8 SRM 57-60-63.
- [SDR QXEA0002345](https://openairdocs.org/sdr/QXEA0002345.md): Seat Track · corroded · Aug 2, 2000 · N822PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > YXX- SURFACE CORROSION ON RIGHT HAND INBOARD SEAT TRACK AT CARGO HOLD DOWN ATTACH POINT X597.500 AND 9.250. REPAIRED IAW DHC-8 SRM 51-20-00 PAGE 5 AND RD 8-53-4936.

Next page: https://openairdocs.org/deregistered/N822PH-2001-12-04/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 = 'N822PH' AND deregistration_id = 'N822PH-2001-12-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N822PH-2001-12-04/reports

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