# Service difficulty reports: N808FR, cancelled Jun 4, 2009

A list on [N808FR, cancelled Jun 4, 2009](https://openairdocs.org/deregistered/N808FR-2009-06-04.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR F3LA2008111000710](https://openairdocs.org/sdr/F3LA2008111000710.md): Solenoid · failed · Nov 6, 2008 · N808FR · Airbus A318111 · Passenger Oxygen System
  > REFERENCE NON-ROUTINE 104853. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABIN CONFIGURATION, THE OXYGEN CONTAINER AT THE TWELFTH ROW OF SEATS ON THE LEFT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGEN
- [SDR F3LA2008111000709](https://openairdocs.org/sdr/F3LA2008111000709.md): Solenoid · failed · Nov 6, 2008 · N808FR · Airbus A318111 · Passenger Oxygen System
  > REFERENCE NON-ROUTINE 104852. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABIN CONFIGURATION, THE OXYGEN CONTAINER AT THE FIFTEENTH ROW OF SEATS ON THE LEFT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGE
- [SDR F3LA2008111000708](https://openairdocs.org/sdr/F3LA2008111000708.md): Solenoid · failed · Nov 6, 2008 · N808FR · Airbus A318111 · Passenger Oxygen System
  > REFERENCE NON-ROUTINE 104851. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABIN CONFIGURATION, THE OXYGEN CONTAINER AT THE SECOND ROW OF SEATS ON THE RIGHT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGEN
- [SDR F3LA200800624](https://openairdocs.org/sdr/F3LA200800624.md): Floor Panel · debonded · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151DH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OF
- [SDR F3LA200800625](https://openairdocs.org/sdr/F3LA200800625.md): Floor Panel · damaged · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY TRANSITION PANEL 132EG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00 PARA 8F AND EO A0-53F-12307. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACC
- [SDR F3LA200800626](https://openairdocs.org/sdr/F3LA200800626.md): Floor Panel · debonded · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151BH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OF
- [SDR F3LA200800627](https://openairdocs.org/sdr/F3LA200800627.md): Floor Panel · debonded · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151CH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OF
- [SDR F3LA200800619](https://openairdocs.org/sdr/F3LA200800619.md): Floor Panel · damaged · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131CG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800620](https://openairdocs.org/sdr/F3LA200800620.md): Floor Panel · damaged · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131AF HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800621](https://openairdocs.org/sdr/F3LA200800621.md): Floor Panel · damaged · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131EG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800622](https://openairdocs.org/sdr/F3LA200800622.md): Floor Panel · damaged · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131DG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800623](https://openairdocs.org/sdr/F3LA200800623.md): Floor Panel · damaged · Sep 25, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131BF HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800521](https://openairdocs.org/sdr/F3LA200800521.md): Floor Panel · damaged · Jul 26, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > LINE MAINT NOTED THE AFT CARGO COMPARTMENT TRANSITION PANEL 151FH WAS DAMAGED. MAINT REPAIRED TRANSITION PANEL 151FH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800522](https://openairdocs.org/sdr/F3LA200800522.md): Floor Panel · damaged · Jul 26, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > LINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151DH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800523](https://openairdocs.org/sdr/F3LA200800523.md): Floor Panel · damaged · Jul 26, 2008 · N808FR · Airbus A318111 · Fuselage Floor Panel
  > LINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151CH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151CH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800130](https://openairdocs.org/sdr/F3LA200800130.md): Unknown · smoke · Mar 19, 2008 · N808FR · Airbus A318111 · Air Distribution System
  > DURING LANDING ROLL OUT, THE FLIGHT CREW REPORTED WHITE/GRAY SMOKE AND ACRID ODOR IN THE COCKPIT AND PASSENGER CABIN. MAINTENANCE PERFORMED IDLE LEAK CHECK OF BOTH ENGINES IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 71-00-00-710-006 AND PERFORMED A CHECK OF TH
- [SDR F3LA200700376](https://openairdocs.org/sdr/F3LA200700376.md): Light · inoperative · Dec 15, 2007 · N808FR · Airbus A318111 · Emergency Lighting
  > MAINTENANCE REPORTED ONE LIGHT IN EMERGENCY SEAT MOUNTED LIGHT ASSY AT ROW 5ABC INOP. REMOVED AND REPLACED ROW 5ABC EMERGENCY SEAT MOUNTED LIGHT ASSY IAW AMM 33-51-11-PB401. OPS CHECK GOOD.

## 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 = 'N808FR' AND deregistration_id = 'N808FR-2009-06-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N808FR-2009-06-04/reports

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