# Service difficulty reports: N903FR, cancelled Feb 17, 2009

A list on [N903FR, cancelled Feb 17, 2009](https://openairdocs.org/deregistered/N903FR-2009-02-17.md).

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

- [SDR F3LA200800587](https://openairdocs.org/sdr/F3LA200800587.md): Power Supply · failed · Aug 25, 2008 · N903FR · Airbus A319112 · Emergency Lighting
  > REFERENCE NON ROUTINE 104231. DURING EXIT CHECK, INSPECTION NOTED LT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED EMERGENCY LIGHTS TEST. MX R&R LT FORWARD EMERGENCY POWER SUPPLY UNIT IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-400-001. UPON COMPL
- [SDR F3LA200800071](https://openairdocs.org/sdr/F3LA200800071.md): Seal · corroded · Feb 18, 2008 · N903FR · Airbus A319111 · Ailerons
  > DURING C5 C CHECK, MAINTENANCE REPORTED CORROSION FOUND ON RIGHT WING AILERON HINGE SEAL NEAR OUTBOARD HINGE LOCATION. MAINTENANCE REMOVED AND REPLACED AILERON SEAL IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-72-11 AND EA A9-57R-30062. TOUCH PAINTING PERF
- [SDR F3LA200800070](https://openairdocs.org/sdr/F3LA200800070.md): Threshold · corroded · Feb 17, 2008 · N903FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C5 C CHECK, INSPECTION REPORTED LEVEL 1 CORROSION OF AFT CARGO PIT DOOR THRESHOLD AT EIGHTEEN (18) LOCATIONS AROUND ATTACHMENT HOLES AND ADJACENT TO THRESHOLD ITSELF. MAINTENANCE REMOVED CORROSION IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-74-00, P
- [SDR F3LA200800057](https://openairdocs.org/sdr/F3LA200800057.md): Profile · corroded · Feb 17, 2008 · N903FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 58, FROM THE RIGHT TO THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE PROFILE, COMMON TO FRAME 58, IN ACCORDANCE WITH THE A319 AMM
- [SDR F3LA200800056](https://openairdocs.org/sdr/F3LA200800056.md): Profile · corroded · Feb 17, 2008 · N903FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING A C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 59, FROM THE RIGHT TO THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE PROFILE, COMMON TO FRAME 59, IN ACCORDANCE WITH THE A319 SR
- [SDR F3LA200700047](https://openairdocs.org/sdr/F3LA200700047.md): Connector · damaged · Apr 2, 2007 · N903FR · Airbus A319112 · Light System Wiring
  > MAINTENANCE REPORTED EPSU AFT L FAULTED. CLEANED AND INSPECTED PINS ON CONNECTOR TO EPSU AFT L POWER SUPPLY. PERFORMED EMERGENCY LIGHT TEST PER AMM 23-73-00-861-001 AND 33-51-38. OPS TEST GOOD.
- [SDR F3LA200600105](https://openairdocs.org/sdr/F3LA200600105.md): Odor · detected · Sep 2, 2006 · N903FR · Airbus A319112 · Air Distribution System
  > BLOCK TURNBACK IN CUN. FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE IN FWD PASSENGER CABIN AREA (APPROXIMATELY ROW 6 AND FWD). MAINTENANCE PERFORMED INSPECTION OF AIRCRAFT MM 24-00-00-810-823. NO SMOKE ODOR OR DISCREPANCIES WERE FOUND. AIRCRAFT WAS RELEASED F
- [SDR F3LA200600102](https://openairdocs.org/sdr/F3LA200600102.md): Epsu · failed · Aug 24, 2006 · N903FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED MID CABIN EPSU FAILED CAPACITY TEST. REPLACED 11WL MID CABIN EPSU. OPS CHECK GOOD IAW AMM 33-51-38, PB401.
- [SDR F3LA200600101](https://openairdocs.org/sdr/F3LA200600101.md): Battery Pack · failed · Aug 24, 2006 · N903FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED LT. MID CABIN EPSU 12WL FAILED CAPACITY TEST. REPLACED BATTERY PACK 12WL. OPS CHECK NORMAL IAW AMM 33-51-38, PB 401.
- [SDR F3LA200600100](https://openairdocs.org/sdr/F3LA200600100.md): Epsu · failed · Aug 24, 2006 · N903FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED FWD EMERGENCY POWER SUPPLY UNIT (EPSU) FAILED EMERGENCY LIGHTS CAPACITY TEST. REPLACED EPSU 10WL. OPS CHECK NORMAL PER AMM 33-51-38, PB 401.
- [SDR F3LA200600095](https://openairdocs.org/sdr/F3LA200600095.md): Slat Track · damaged · Aug 18, 2006 · N903FR · Airbus A319112 · Leading Edge Devices
  > DURING C-4 CHECK, INSPECTION REPORTED LT WING, NR 1 SLAT I/B SLAT TRACK CUTOUT DAMAGED. REMOVED DAMAGED AREAS AND PERFORMED HFEC INSPECTION. NO FAULTS OR CRACKS NOTED. APPLIED ALODINE TREATMENT EPOXY PRIMER AND PAINT TO AFFECTED AREAS. REFERENCE A319 SRM 5
- [SDR F3LA200600092](https://openairdocs.org/sdr/F3LA200600092.md): Valve · corroded · Aug 18, 2006 · N903FR · Airbus A319112 · Cabin Pressure Control System
  > LEFT HAND CABIN PRESSURE SAFETY VALVE (7HL) POSITION SWITCH STICKS AND IS CORRODED. NEW VALVE WAS INSTALLED PER AMM 21-31-52-400-001. BONDING CHECK PERFORMED ON BONDING STRAP PER AMM 20-28-00-912-004. CHECK WAS GOOD.
- [SDR F3LA200600094](https://openairdocs.org/sdr/F3LA200600094.md): Threshold · corroded · Aug 15, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED MINOR CORROSION ON R1 DOOR THRESHOLD STRIP. FOUND R1 DOOR THRESHOLD STRIP TO BE OUT OF LIMITS PER SRM 51-70-00. FABRICATED AND INSTALLED REPLACEMENT R1 DOOR SILL COVER PER AIRBUS DWG B5 D53610197, SRM 51-27-00, SRM 51-44
- [SDR F3LA200600093](https://openairdocs.org/sdr/F3LA200600093.md): Threshold · corroded · Aug 15, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED MINOR CORROSION ON L1 DOOR THRESHOLD STRIP. FOUND L1 DOOR THRESHOLD STRIP TO BE OUT OF LIMITS PER SRM 51-70-00. FABRICATED AND INSTALLED REPLACEMENT L1 DOOR SILL COVER PER AIRBUS DWG B5 D53610197, SRM 51-27-00, SRM 51-44
- [SDR F3LA200600089](https://openairdocs.org/sdr/F3LA200600089.md): Floor Support · corroded · Aug 10, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > FLOORBEAM FROM 68-69 LT SIDE, JUST INSIDE L-2 DOOR WAS CORRODED. NEW FLOORBEAM AND SPLICE ANGLE INSTALLED PER A319 SRM 51-42-11.
- [SDR F3LA200600099](https://openairdocs.org/sdr/F3LA200600099.md): Seat Track · corroded · Aug 9, 2006 · N903FR · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED AFT FUSELAGE CABIN FLOOR STRUCTURE FR66, Y1292, CORRODED UNDER NUT CLIPS. BURNISHED CORROSION ON SEAT TRACK/STRUCTURE AT FR66 PER SRM 53-00-15, FIG 101, SECTION E-E, PAGES 101-104. UPON FURTHER INVESTIGATION, MORE CORROS
- [SDR F3LA200600098](https://openairdocs.org/sdr/F3LA200600098.md): Beam · corroded · Aug 9, 2006 · N903FR · Airbus A319112 · Fuselage Main, Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION AND HOLE THROUGH Y254 BEAM AT FR20 FWD ENTRY CENTER. FOUND CORRODED AREA TO BE OUT OF LIMITS PER SRM 53-11-14, FIG 104. CUT OUT AND REMOVED CORRODED SECTION FROM TOP FLANGE OF FLOOR SUPPORT PER SRM 53-11-14, FI
- [SDR F3LA200600097](https://openairdocs.org/sdr/F3LA200600097.md): Floor Support · corroded · Aug 9, 2006 · N903FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED LT SIDE FLOOR SUPPORT STRINGER NUT CLIPS AND NUT PLATES FOR ATTACHMENT OF FLOOR AND TRANS PANELS IN FWD CARGO COMPARTMENT CORRODED. REMOVED LT SIDE FLOOR SUPPORT STRINGER (TRANSITION PLATE) BETWEEN FR28 AND FR30 PER A319
- [SDR F3LA200600096](https://openairdocs.org/sdr/F3LA200600096.md): Dummy Rail · corroded · Aug 9, 2006 · N903FR · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION IN FWD LAV AREA, FR16 AND Y503.2. DUMMY RAIL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-11-14. REMOVED CORRODED DUMMY RAIL PER SRM 51-42-11. LOCATED AND DRILLED NEW DUMMY RAIL PER SRM 51-44-11 AND AIRBUS DWG B2
- [SDR F3LA200600091](https://openairdocs.org/sdr/F3LA200600091.md): Switch · corroded · Aug 8, 2006 · N903FR · Airbus A319112 · Cabin Pressure Control System
  > RIGHT HAND CABIN PRESSURE SAFETY VALVE (GHL) FAILED OPERATION TEST. POSITION SWITCH WAS CORRODED. NO OPEN INDICATION ON ECAM. VALVE WAS REPLACED PER AMM 21-31-52-400-001.
- [SDR F3LA200600090](https://openairdocs.org/sdr/F3LA200600090.md): Guide Vane · cracked · Aug 6, 2006 · N903FR · Airbus A319112 · Turbine Engine Air Inlet Section
  > ENGINE NR 1, 14 OUTLET GUIDE VANES DOUBLERS WERE CRACKED AND WERE OUT OF LIMITS. REPAIRED AND REPLACED PER AMM 72-23-00-400-008.
- [SDR F3LA200600011](https://openairdocs.org/sdr/F3LA200600011.md): Engine · bird ingestion · Mar 22, 2006 · N903FR · Airbus A319112 · Engine (Turbine/Turboprop)
  > BIRD STRIKE TO NR 2 ENGINE ON APPROACH TO MKE. DUE TO N1/N2 ROLLBACK, DAMAGE WAS SUSPECTED AND AGENT NR 1 FIRE BOTTLE WAS DISCHARGED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. A BORESCOPE OF THE NR 2 ENGINE WAS PERFORMED AND MAJOR DAMA
- [SDR F3LA200500041](https://openairdocs.org/sdr/F3LA200500041.md): Fitting · corroded · Sep 7, 2005 · N903FR · Airbus A319112 · Wing, Landing Gear Attach Fittings
  > INSPECTION REPORTED CORROSION IN FWD BORE FROM 4 O'CLOCK TO 7 O'CLOCK LT WING, RIB 5, LANDING FITTING. BORED OUT CORROSION PER SRM 57-26-13.
- [SDR F3LA200500040](https://openairdocs.org/sdr/F3LA200500040.md): Fitting · corroded · Sep 7, 2005 · N903FR · Airbus A319112 · Wing, Landing Gear Attach Fittings
  > INSPECTION REPORTED CORROSION ON FWD FACE, FWD LUG, LT WING RIB 5, LANDING GEAR FITTING. MACHINED CORROSION ON LUG FACE PER SRM 57-26-13.
- [SDR F3LA200500039](https://openairdocs.org/sdr/F3LA200500039.md): Fitting · corroded · Sep 7, 2005 · N903FR · Airbus A319112 · Wing, Landing Gear Attach Fittings
  > INSPECTION REPORTED CORROSION ON AFT FACE, FWD LUG, LT WING LANDING FITTING, RIB 5. MACHINED CORROSION PER SRM 57-26-13.
- [SDR F3LA200500038](https://openairdocs.org/sdr/F3LA200500038.md): Coffeemaker · odor · Aug 15, 2005 · N903FR · Airbus A319112 · Buffet/Galleys
  > AIR DIVERSION, SMOKE SMELL IN AFT GALLEY. DECLARED AN EMERGENCY. MX PERFORMED TSM TASK 24-00-00-810-823, FOUND AFT NR 2 COFFEEMAKER C/B'S POPPED ON REAR OF COFFEEMAKER. REMOVED AFT NR 1 COFFEEMAKER & INSTALLED INTO NR 2 POSITION, OPS NORMAL. NO ARCING OR D
- [SDR F3LA200500005](https://openairdocs.org/sdr/F3LA200500005.md): Smoke · detected · Feb 17, 2005 · N903FR · Airbus A319112 · Air Distribution System
  > ON INBOUND TAXI, FLIGHT CREW REPORTED SMOKE IN CABIN. RAN ENGINES PER AMM 71-00-00-710-006. CYCLED AIR CONDITIONING PACKS. RAN APU. CYCLED APU BLEED AIR. INSPECTED CARGO BINS, E/E BAYS AND CABIN FOR SMOKE. NO FAULTS NOTED, COULD NOT DUPLICATE DISCREPANCY
- [SDR F3LA200300126](https://openairdocs.org/sdr/F3LA200300126.md): Skin · dented · Sep 6, 2003 · N903FR · Airbus A319111 · Fuselage Main, Plate/Skin
  > DURING WALKAROUND, MAINTENANCE FOUND TWO SMALL DENTS AFT AND EVEN WITH FORWARD ENTRY DOOR, APPROXIMATELY 3 FT. AFT OF DOOR AT STA. 950, STR. 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EA A9-53R-10127 AND SRM 53-00-11.

## 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 = 'N903FR' AND deregistration_id = 'N903FR-2009-02-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N903FR-2009-02-17/reports

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