# Service difficulty reports: N486US, cancelled Feb 14, 2002

A list on [N486US, cancelled Feb 14, 2002](https://openairdocs.org/deregistered/N486US-2002-02-14.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 · 300 reports

- [SDR QXEA0101181](https://openairdocs.org/sdr/QXEA0101181.md): Support · cracked · Jun 30, 2001 · N486US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > PDX - NOSE LANDING GEAR BAY FORWARD CEILING GRAVEL GUARD SUPPORT FLANGE ATTACHED TO FORWARD FACE OF FRAME 2650 IS CRACKED. REPAIRED IAW HORIZON AIR EA 4-53-1500.
- [SDR QXEA0101180](https://openairdocs.org/sdr/QXEA0101180.md): Panel · chafed · Jun 29, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > PDX - CHAFING DAMAGE AT PANEL 21A APERTURE. REPAIRED IAW FOKKER SRM 53-01-01.
- [SDR QXEA0100936](https://openairdocs.org/sdr/QXEA0100936.md): Receptacle · odor · Jun 9, 2001 · N486US · Fokker F28MK4000 · Buffet/Galleys
  > PDX- FLIGHT ATTENDANT REPORTS ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED BEVERAGE HEATING RECEPTICLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0100743](https://openairdocs.org/sdr/QXEA0100743.md): Frame · corroded · May 11, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - CORROSION FOUND ON UPPER FRAME FLANGE OF FRAME 14755, IN VICINITY OF STRINGER 2. CORROSION BLENDED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. CORROSION BLENDED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. FOUND TO BE BEYOND ACCEPTABLE LIMITS. RE
- [SDR QXEA0100771](https://openairdocs.org/sdr/QXEA0100771.md): Skin · delaminated · May 9, 2001 · N486US · Fokker F28MK4000 · Wing, Plate/Skin
  > YYC - RIGHT-HAND OUTBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. REPAIRED IAW HORIZON AIR EA 4-57-557.
- [SDR QXEA0100770](https://openairdocs.org/sdr/QXEA0100770.md): Skin · delaminated · May 9, 2001 · N486US · Fokker F28MK4000 · Wing, Plate/Skin
  > YYC - RIGHT-HAND OUTBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. MULTIPLE DELAMS OUT MOST OUTBOARD END ON TOP SKIN. REPAIRED IAW HORIZON AIR EA 4-57-557.
- [SDR QXEA0100767](https://openairdocs.org/sdr/QXEA0100767.md): Support · damaged · May 8, 2001 · N486US · Fokker F28MK4000 · Wing, Control Surface Attach Fittings
  > YYC - RIGHT-HAND INBOARD FLAP A-FRAME SUPPORT ASSEMBLY HAS OVER SIZED BORES IN AFT 3 ATTACH HOLES. OVERSIZE HOLES REAMED TO.3125 MIN FOR 5/16 BOLT AS PER FOKKER SRM 51-32-01, PAGE 11, TABLE 6. BOLTS INSTALLED PER FOKKER FAX TS01.54655 AND HORIZON AIR EA 4-5
- [SDR QXEA0100768](https://openairdocs.org/sdr/QXEA0100768.md): Rivet · loose · May 6, 2001 · N486US · Fokker F28MK4000 · Vertical Stabilizer
  > YYC - VERTICAL STABILIZER LEFT-HAND SIDE ABOVE TAIL CONE HAS LOOSE RIVETS. INSTALLED FASTENERS IAW FOKKER SRM 51-32-04 AND HORIZON AIR EA 4-55-289.
- [SDR QXEA0100740](https://openairdocs.org/sdr/QXEA0100740.md): Bracket · cracked · May 6, 2001 · N486US · Fokker F28MK4000 · Landing Gear Door Actuator
  > YYC - TUNNEL BETWEEN WHEELBAYS, RIGHT-HAND AFT MAIN LANDING GEAR DOOR ACTUATOR BACKUP BRACKETS, FORWARD BRACKET CRACKED. REPAIRED IAW FOKKER SRM 51-30-02, PAGE 9 AND 10 AND SRM 51-31-01.
- [SDR QXEA0100739](https://openairdocs.org/sdr/QXEA0100739.md): Bracket · broken · May 6, 2001 · N486US · Fokker F28MK4000 · Landing Gear Doors
  > YYC - TUNNEL BETWEEN WHEELBAYS, LEFT-HAND AFT MAIN LANDING GEAR DOOR BACKUP BRACKETS, FORWARD BRACKET CRACKED, AFT BRACKET HAS LOOSE HI-LOK. REPAIRED IAW FOKKER SRM 51-30-02, PAGES 9 AND 10 AND SRM 51-31-01, PARAGRAPH 7, PAGES 13 AND 14.
- [SDR QXEA0100742](https://openairdocs.org/sdr/QXEA0100742.md): Structure · cracked · May 5, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Structure
  > YYC - FRAME BOX FOR MAIN CABIN DOOR ACTUATOR FOUND TO BE CRACKED. INSTALLED NEW PART IAW FOKKER SRM.
- [SDR QXEA0100780](https://openairdocs.org/sdr/QXEA0100780.md): Skin · damaged · May 4, 2001 · N486US · Fokker F28MK4000 · Passenger/Crew Doors
  > YYC - MAIN CABIN DOOR OUTER SKIN BY GRIP HANDLE SHARP DENT AND CREASE MEASURED AND BEYOND LIMITS. REPAIRED IAW HORIZON AIR EA 4-52-449.
- [SDR QXEA0100772](https://openairdocs.org/sdr/QXEA0100772.md): Skin · delaminated · May 4, 2001 · N486US · Fokker F28MK4000 · Wing, Plate/Skin
  > YYC - LEFT-HAND INBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. REPAIRED IAW HORIZON AIR EA 4-57-536.
- [SDR QXEA0100769](https://openairdocs.org/sdr/QXEA0100769.md): Skin · delaminated · May 4, 2001 · N486US · Fokker F28MK4000 · Wing, Plate/Skin
  > YYC - RIGHT-HAND OUTBOARD WING TRAILING EDGE TAP TEST CARRIED OUT. THREE MINOR DELAMS INNER MOST INBOARD END ON TOP SKIN. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 10B, FIGURE 6B AND PAGE 12.
- [SDR QXEA0100749](https://openairdocs.org/sdr/QXEA0100749.md): Door Frame · corroded · May 4, 2001 · N486US · Fokker F28MK4000 · Passenger/Crew Doors
  > YYC - MAIN CABIN DOOR AFT LOWER CORNER, BENEATH SEAL AND RETAINER CORRODED. FOUND TO WITHIN LIMITS AS PER FOKKER FAX TS01-54526 AND HORIZON AIR EA 4-52-453.
- [SDR QXEA0100766](https://openairdocs.org/sdr/QXEA0100766.md): Bushing · worn · May 3, 2001 · N486US · Fokker F28MK4000 · Spoilers
  > YYC - RIGHT-HAND NR 2 LIFT DUMPER SPIGOT BUSHINGS WORN. RIGHT-HAND NR 2 LIFT DUMPER BELLCRANK REMOVED, INTERNAL BUSHINGS AND SPIGOT MEASURED AS PER FOKKER FAX AND HORIZON AIR EA 8-57-555, ALL WITHIN LIMITS.
- [SDR QXEA0100765](https://openairdocs.org/sdr/QXEA0100765.md): Bushing · worn · May 3, 2001 · N486US · Fokker F28MK4000 · Spoilers
  > YYC - RIGHT-HAND NR 3 LIFT DUMPER SPIGOT BUSHINGS WORN. RIGHT-HAND LIFT DUMPER BELLCRANK REMOVED, INTERNAL BUSHINGS AND SPIGOT MEASURED AS PER FOKKER FAX AND HORIZON AIR EA 4-57-555, ALL WITHIN LIMITS.
- [SDR QXEA0100736](https://openairdocs.org/sdr/QXEA0100736.md): Longeron · cracked · May 3, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Longeron/Stringer
  > YYC - CRACKED LONGERON IN FORWARD LOWER FRONT FUSELAGE JUST AHEAD OF FRAME 3450, RIGHT-HAND SIDE, THIRD LONGERON INBOARD. REPAIRED IAW FOKKER SRM 53-11-05, PAGE 10M ITEM 340 AND SRM 53-32-01, PAGE 15, PARAGRAPH 5.
- [SDR QXEA0100748](https://openairdocs.org/sdr/QXEA0100748.md): Casting · corroded · May 2, 2001 · N486US · Fokker F28MK4000 · Passenger/Crew Doors
  > YYC - MAIN CABIN DOOR AFT LATCH FITTING BACK UP CASTING HAS MINOR CORROSION. BLENDED CORROSION IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. FOUND TO BE WITHIN LIMITS IAW FOKKER SRM 51-00-00, PAGE 2, PARAGRAPH 2.
- [SDR QXEA0100724](https://openairdocs.org/sdr/QXEA0100724.md): Frame · cracked · May 1, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - CORROSION ON CASTELLATION ATTACHED TO FRAME 13815 BETWEEN STRINGER 3 AND 72. REPAIRED IAW FOKKER SRM 53-22-04, FIGURE 14 AND SRM FOKKER SRM 51-31-07, PAGE 13 AND 14.
- [SDR QXEA0100751](https://openairdocs.org/sdr/QXEA0100751.md): Frame · cracked · Apr 30, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 18575, STRINGER 57, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3 AND SRM 53-30-02, PAGES 9 AND 10.
- [SDR QXEA0100722](https://openairdocs.org/sdr/QXEA0100722.md): Bracket · corroded · Apr 30, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Structure
  > YCC - UPPER TORSION BOX OF REAR CARGO DOOR APERTURE HAS CORROSION AFT OF AFT HOOK LATCH BRACKET. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH B, PAGE 6, AND FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 7.
- [SDR QXEA0100756](https://openairdocs.org/sdr/QXEA0100756.md): Frame · cracked · Apr 29, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - LEFT-HAND SIDE FRAME 50-2, STRINGER 27, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484.
- [SDR QXEA0100755](https://openairdocs.org/sdr/QXEA0100755.md): Frame · cracked · Apr 29, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - RIGHT-HAND SIDE FRAME 50-2, STRINGER 50, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484.
- [SDR QXEA0100754](https://openairdocs.org/sdr/QXEA0100754.md): Frame · cracked · Apr 29, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 50-2, STRINGER 48, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484.
- [SDR QXEA0100753](https://openairdocs.org/sdr/QXEA0100753.md): Frame · cracked · Apr 29, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 50-2, STRINGER 4B, CASTELLATION CRACKED. REPAIRED IAW FOKKER FAX TS97.59355 AND HORIZON AIR EA 4-53-1484.
- [SDR QXEA0100716](https://openairdocs.org/sdr/QXEA0100716.md): Door Frame · cracked · Apr 28, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Structure
  > YYC-CRACKS UNDER DOOR SUPPORT ROD BRACKET ON AFT CARGO DOOR APERTURE. REPAIRED IAW FOKKER SRM 53-02-16, PAGE 4.
- [SDR QXEA0100782](https://openairdocs.org/sdr/QXEA0100782.md): Bushing · worn · Apr 27, 2001 · N486US · Fokker F28MK4000 · Spoilers
  > YYC - LEFT-HAND NR 1 LIFT DUMPER SPIGOT BUSHINGS WORN. LEFT-HAND NR 1 LIFT DUMPER BELLCRANK REMOVED, SPIGOT AND BELLCRANK BUSHING MEASURED AS PER HORIZON AIR EA 4-57-554. FOUND TO BE WITHIN LIMITS.
- [SDR QXEA0100781](https://openairdocs.org/sdr/QXEA0100781.md): Bushing · worn · Apr 27, 2001 · N486US · Fokker F28MK4000 · Spoilers
  > YYC - LEFT-HAND LIFT DUMPER SPIGOT BUSHINGS WORN. LEFT-HAND NR 2 LIFT DUMPER BELLCRANK REMOVED SPIGOT AND BELLCRANK BUSHING MEASURED AS PER HORIZON AIR EA 4-57-554, FOUND WITHIN LIMITS.
- [SDR QXEA0100764](https://openairdocs.org/sdr/QXEA0100764.md): Fitting · corroded · Apr 27, 2001 · N486US · Fokker F28MK4000 · Stabilizer Actuator
  > YYC - HORIZONTAL STAB DRIVE FITTING HAS SOME FRETTING OF THE RIGHT-HAND AFT LUGS, INBOARD SIDE. REPAIRED IAW HORIZON AIR EA 4-55-290 AND FOKKER FAX TS06.54293.
- [SDR QXEA0100763](https://openairdocs.org/sdr/QXEA0100763.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 32-2 AND STRINGER 30, CASTELLATION FOUND TO BE CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.
- [SDR QXEA0100762](https://openairdocs.org/sdr/QXEA0100762.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 32-2 AND STRINGER 44, CASTELLATION FOUND TO BE CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.
- [SDR QXEA0100761](https://openairdocs.org/sdr/QXEA0100761.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 32-2, STRINGER 22, CASTELLATION FOUND TO BE CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.
- [SDR QXEA0100758](https://openairdocs.org/sdr/QXEA0100758.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - LEFT-HAND SIDE FRAME 32-2, STRINGER 28, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.
- [SDR QXEA0100757](https://openairdocs.org/sdr/QXEA0100757.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - LEFT-HAND SIDE FRAME 32-2, STRINGER 21A, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.
- [SDR QXEA0100752](https://openairdocs.org/sdr/QXEA0100752.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FRAME 32-2, STRINGER 50, CASTELLATION CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3.
- [SDR QXEA0100741](https://openairdocs.org/sdr/QXEA0100741.md): Mount · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Miscellaneous Structure
  > YYC - LEFT-HAND ACM BAY HAS CRACKED MOUNTING BOX FOR MIXING DUCT ELBOW ATTACH. REPAIRED IAW FOKKER SRM 53-11-05, PAGE 2, FIGURE 01, ITEM 730.
- [SDR QXEA0100737](https://openairdocs.org/sdr/QXEA0100737.md): Floorbeam · corroded · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Floor Beam
  > YYC - CORROSION ON FLOORBEAM AT FRAME 1385 AND BL280L. BLENDED AS PER FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. ALODINED AS PER FOKKER SRM 51-10-04, PAGE 7, PARAGRAPH 4.
- [SDR QXEA0100720](https://openairdocs.org/sdr/QXEA0100720.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - CRACKED CASTELLATION ON FRAME 13815A AT STRINGER 2. REPAIRED IAW HORIZON AIR EA 4-53-1480.
- [SDR QXEA0100719](https://openairdocs.org/sdr/QXEA0100719.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - CRACKED CASTELLATION ON FRAME 13815B AT STRINGER 73. REPAIRED IAW HORIZON AIR EA 4-53-1481.
- [SDR QXEA0100718](https://openairdocs.org/sdr/QXEA0100718.md): Frame · cracked · Apr 27, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - CRACKED CASTELLATION ON FRAME 13815B AT STRINGER 2. REPAIRED IAW HORIZON AIR EA 4-53-1482.
- [SDR QXEA0100760](https://openairdocs.org/sdr/QXEA0100760.md): Skin · dented · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YYC - TAIL SECTION HAS DENTS LEFT-HAND FUSELAGE, STATION 23003, STRINGER 19. REPAIRED IAW HORIZON AIR EA 4-53-1485 AND FOKKER FAX TS01-54512.
- [SDR QXEA0100759](https://openairdocs.org/sdr/QXEA0100759.md): Skin · canning · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YYC - REAR PRESSURE BULKHEAD AT FRAME 17065 SKIN IS OIL CANNING BETWEEN HORIZONTAL BEAMS 4 AND 5 AND BL1050L AND 4256. REPAIRED IAW HORIZON AIR EA 4-53-1483.
- [SDR QXEA0100738](https://openairdocs.org/sdr/QXEA0100738.md): Floorbeam · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Floor Beam
  > YYC - CORROSION ON FLOORBEAM AT FRAME 1890 AND BL280L. BLENDED AS PER FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4A. ALODINED AS PER FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 7.
- [SDR QXEA0100734](https://openairdocs.org/sdr/QXEA0100734.md): Frame · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Frame
  > YYC - FORWARD PIT AT STATION 9305 AND STRINGER 2 HAS CORROSION UNDER ANCHOR NUT OF FRAME FLANGE. BLENDED OUT CORROSION AS PER FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A. FOUND TO BE WITHIN LIMITS IAW FOKKER SRM 53-01-01, PAGE 8, PARAGRAPH B. INSTALLED ANCHOR
- [SDR QXEA0100731](https://openairdocs.org/sdr/QXEA0100731.md): Skin · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YYC - CORROSION ON FUSELAGE SKIN UNDER FORWARD RAD ALT BLANKING PLATE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4.
- [SDR QXEA0100730](https://openairdocs.org/sdr/QXEA0100730.md): Skin · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YYC - CORROSION ON SKIN UNDER FORWARD RAD ALT ANTENNA. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A.
- [SDR QXEA0100729](https://openairdocs.org/sdr/QXEA0100729.md): Skin · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YYC - CORROSION ON FUSELAGE SKIN UNDER AFT RAD ALT BLANKING PLATE. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4A.
- [SDR QXEA0100727](https://openairdocs.org/sdr/QXEA0100727.md): Skin · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YYC - CORROSION ON FUSELAGE SKIN UNDER AFT DME ANTENNA. REPAIRED IAW FOKKER SRM 51-10-09, PAGE 9, PARAGRAPH 4 AND SRM 51-10-04.
- [SDR QXEA0100726](https://openairdocs.org/sdr/QXEA0100726.md): Skin · corroded · Apr 26, 2001 · N486US · Fokker F28MK4000 · Fuselage Main, Plate/Skin
  > YCC - CORROSION ON FUSELAGE SKIN UNDER MARKER BEACON ANTENNA. REPAIRED IAW FOKKER SRM 51-10-09, PAGE 9, PARAGRAPH 4 AND SRM 51-10-04.

Next page: https://openairdocs.org/deregistered/N486US-2002-02-14/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 = 'N486US' AND deregistration_id = 'N486US-2002-02-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N486US-2002-02-14/reports

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