# Service difficulty reports: N803FR, cancelled Jan 22, 2014

A list on [N803FR, cancelled Jan 22, 2014](https://openairdocs.org/deregistered/N803FR-2014-01-22.md).

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

- [SDR F3LA2013071700885](https://openairdocs.org/sdr/F3LA2013071700885.md): Unknown · vibration · Jul 9, 2013 · N803FR · Airbus A318111 · Flight Control System
  > AIR TURN BACK DUE TO SEVERE AIRFRAME VIBRATION. BEGAN AT 25,500 FT AND AROUND 330 KIAS. DID NOT STOP UNTIL SPEED MANUALLY FLOWN LESS THAN 300 KIAS. EMERGENY DECLARED. R & R LT AND RT ELEVATOR ATTACH HARDWARE AND BEARINGS REF AMM 27-34-41, PAGE BLOCK 401.
- [SDR F3LA2012041000740](https://openairdocs.org/sdr/F3LA2012041000740.md): Plate · corroded · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > LATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 RT TO STRINGER 24 RT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51 -42-11, PARA 6 B-18, D 1-5 AND EO AO-53EO-31 434.
- [SDR F3LA2012041000739](https://openairdocs.org/sdr/F3LA2012041000739.md): Plate · corroded · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > LATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 LT TO STRINGER 24 LT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 B-1 B, 0 1-5 AND EO AO-53EO-31434.
- [SDR F3LA2012041000738](https://openairdocs.org/sdr/F3LA2012041000738.md): Floorbeam · corroded · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM FRAME 66 Y765 CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000737](https://openairdocs.org/sdr/F3LA2012041000737.md): Floor Support · corroded · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > AFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOOR SUPPORT HAS CORROSION IN 3 AREAS. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000734](https://openairdocs.org/sdr/F3LA2012041000734.md): Floorbeam · corroded · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > AFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOORBEAM HAS CORROSION IN 3 AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000736](https://openairdocs.org/sdr/F3LA2012041000736.md): Floorbeam · corroded · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > AFT CABIN FRAME 68, Y-1292 FLOORBEAM HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.
- [SDR F3LA2012041000735](https://openairdocs.org/sdr/F3LA2012041000735.md): Tray · cracked · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69. STRINGER 23 RT TO STRINGER 24, RT IS CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51 -42-11, PARAGRAPH 5, 6, 7 AND 13.
- [SDR F3LA201204100734](https://openairdocs.org/sdr/F3LA201204100734.md): Plate · cracked · Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > C-CHECK, SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69, S23-24L CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51-42-11 PARAGRAPH 5, 6, 7 AND 13.
- [SDR F3LA2011080900665](https://openairdocs.org/sdr/F3LA2011080900665.md): Battery Pack · failed · Aug 5, 2011 · N803FR · Airbus A318111 · Emergency Lighting
  > ESPU LLWL (13WL) FAILED SYS TEST IAW A-CHECK CARD A332201-03. REPLACED BATTERY PACK ON ESPU LLWL(13WL) IAW AMM 33-51-38, PB 401.
- [SDR F3LA2011051800641](https://openairdocs.org/sdr/F3LA2011051800641.md): Battery · failed · May 13, 2011 · N803FR · Airbus A318111 · Emergency Lighting
  > ACFT LP 598021 I2M: EPSU TEST FAILED 11WL BATTERY. R & R EPSU BATTERY FOR 11WL IAW A318 AMM 33-51-38-000-002 AND 33-51-38-400-002. TEST OK.
- [SDR F3LA2011032100618](https://openairdocs.org/sdr/F3LA2011032100618.md): Windshield · cracked · Mar 17, 2011 · N803FR · Airbus A318111 · Flight Compartment Windows
  > F/O FRONT WINDSHIELD CRACKED, ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O FRONT WINDSHIELD IAW AMM 56-11-11-400-000-001.
- [SDR F3LA2011022100605](https://openairdocs.org/sdr/F3LA2011022100605.md): Engine · overtemp · Feb 16, 2011 · N803FR · Airbus A318111 · Engine (Turbine/Turboprop)
  > AIR TURN BACK DUE TO BIRDSTRIKE ON NR 1 ENGINE. ENGINE SHUTDOWN, INVESTIGATION FOR ENGINE SHUTDOWN SHOWS THE EGT WAS EXCEEDED AT 1015 DEGREES CELCIUS FOR 21 SECONDS. PERFORMED AN AIRFRAME AND ENG NR 1 BIRDSTRIKE INSP. REF TASK CARDS MP05510-02 AND MP72400-0
- [SDR F3LA2010100600529](https://openairdocs.org/sdr/F3LA2010100600529.md): Lens · cracked · Oct 17, 2010 · N803FR · Airbus A318111 · Emergency Lighting
  > C-CHECK: NON ROUTINE N0616; L-1 ENTRY LOWER EXIT LIGHT, THE LENS IS ILLEGIBLE. R & R LENS ASSY ON L-1 DOOR LOWER EXIT LIGHT IAW AMM 33-51-13-400-001 PAGE 3 STEP A 3 AND AMM 33-51-13-020-050 STEP A(1)(A)(B).
- [SDR F3LA2010100600528](https://openairdocs.org/sdr/F3LA2010100600528.md): Floor Panel · delaminated · Oct 17, 2010 · N803FR · Airbus A318111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0613; AFT CARGO FLOOR PANEL 161DF EDGE DELAMINATED AND EDGE FILLER DAMAGED 10 INCH. FABRICATED REPLACEDMENT FLOOR PANEL IAW MCG IRM 9701, REV G.
- [SDR F3LA2010100600527](https://openairdocs.org/sdr/F3LA2010100600527.md): Lens · cracked · Oct 17, 2010 · N803FR · Airbus A318111 · Emergency Lighting
  > C-CHECK: NON ROUTINE N0610; EMERGENCY LIGHT ABOVE L-1 DOOR, THE LENS IS CRACKED. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-11-020-050B AND AMM 33-51-11-420-050A.
- [SDR F3LA2010100600526](https://openairdocs.org/sdr/F3LA2010100600526.md): Power Supply · no test · Oct 17, 2010 · N803FR · Airbus A318111 · Emergency Lighting
  > C-CHECK: NON ROUTINE N0607; NUMEROUS EMERGENCY PATH LIGHTS INOP ON SEATS AND CEILING PANELS. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-710-059A. EMERGENCY POWER SUPPLY UNIT 10WL FAILED SYS TEST "BATT FAULT' LIGHT ILLUMINATED. R & R EPSU 10WL IAW
- [SDR F3LA2010100600525](https://openairdocs.org/sdr/F3LA2010100600525.md): Fitting · gouged · Oct 17, 2010 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0124; FWD CARGO LOWER FWD CORNER SEALING SECTION FITTING GOUGED.1250 IN X.2500 IN X.040 INCH. R & R FWD LOWER SEALING SECTION FITTING IAW SRM 51-72-11, PAGE 1.
- [SDR F3LA2010100600524](https://openairdocs.org/sdr/F3LA2010100600524.md): Connector · misinstalled · Oct 17, 2010 · N803FR · Airbus A318111 · Light System Wiring
  > C-CHECK: NON ROUTINE N0033, EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. FOUND CONNECTOR AT LIGHT ASSEMBLY TO BE INPROPERLY CONNECTED. RE-SEATED CONNECTOR IAW AIRBUS A318 AMM 33-51-19-400-003 SUBTASK 33-51-19-420-052 STEP A(1)(A)(B). OPS CHECK GOOD IAW AMM 33-51-00
- [SDR F3LA200700193](https://openairdocs.org/sdr/F3LA200700193.md): Floor Panel · corroded · Aug 3, 2007 · N803FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD CORRODED ON SURFACE OF PANEL 261FF. REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.
- [SDR F3LA200700190](https://openairdocs.org/sdr/F3LA200700190.md): Floor Support · corroded · Aug 3, 2007 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT FR 66 TO FR 70 AT Y1292, FWD INBD FASTENER LOCATIONS. REPLACED FLOOR SUPPORT BETWEEN FR 66 AND FR 68 PER SRM 51-42-11. REPAIRED OTHER DAMAGE TO FLOOR SUPPORT IAW EA A8-53R-12042.
- [SDR F3LA200700192](https://openairdocs.org/sdr/F3LA200700192.md): Plate · corroded · Aug 1, 2007 · N803FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES IAW AMM 52-11-31-991-011/012.
- [SDR F3LA200700191](https://openairdocs.org/sdr/F3LA200700191.md): Girt Bar · corroded · Jul 31, 2007 · N803FR · Airbus A318111 · Escape Slide
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR SEAL NUT PLATE HOLE AFT OF AFT GIRT BAR FITTING PLATE. REPAIRED PER EA A8-53R-12044.
- [SDR F3LA200700188](https://openairdocs.org/sdr/F3LA200700188.md): Plate · corroded · Jul 30, 2007 · N803FR · Airbus A318111 · Escape Slide
  > DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES CORRODED. REPLACED BLANKING PLATES IAW A318 SRM 51-42-11 AND AMM 52-13-31-400-007.
- [SDR F3LA200700187](https://openairdocs.org/sdr/F3LA200700187.md): Floor Panel · corroded · Jul 28, 2007 · N803FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C-3 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001.
- [SDR F3LA200700185](https://openairdocs.org/sdr/F3LA200700185.md): Torque Link · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Main Landing Gear
  > DURING C-3 CHECK, INSPECTION REPORTED PITTING AND CORROSION ON NLG UPPER TORQUE LINK ATTACH POINT. REMOVED PITS AND CORROSION AND CADMIUM PLATED INNER BORE IAW EA A8-23R-12046.
- [SDR F3LA200700184](https://openairdocs.org/sdr/F3LA200700184.md): Plate · damaged · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Structure
  > DURING C-3 CHECK, INSPECTION REPORTED HOLES ON JOINT PLATE COMMON TO FLOORBEAM AT -Y1292 BETWEEN FR68 AND FR69 DAMAGED. FABRICATED AND INSTALLED REPLACEMENT JOINT PLATE IAW A318 SRM 53-41-14, FIG 17, AND 51-42-11, STEP 7B.
- [SDR F3LA200700183](https://openairdocs.org/sdr/F3LA200700183.md): Skate Angle · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Attach Fittings
  > DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF R2 DOOR GIRT BAR CUTOUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, STEPS B AND D.
- [SDR F3LA200700182](https://openairdocs.org/sdr/F3LA200700182.md): Skate Angle · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Attach Fittings
  > DURING C-3 CHECK, INSPECTION REPORTED MODERATE CORROSION IN NUT PLATE MOUNT HOLES OF SKATE ANGLE AFT OF L2 DOOR GIRT BAR CUT OUTS. REMOVED AND REPLACED SKATE ANGLE IAW A318 SRM 51-42-11, PARA. 5, 6 AND 13.
- [SDR F3LA200700181](https://openairdocs.org/sdr/F3LA200700181.md): Floorbeam · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.
- [SDR F3LA200700180](https://openairdocs.org/sdr/F3LA200700180.md): Floorbeam · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF R2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, STEP 7B.
- [SDR F3LA200700179](https://openairdocs.org/sdr/F3LA200700179.md): Floorbeam · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INBD OF L2 DOOR GIRT BAR CUTOUTS HAD LIGHT TO MODERATE CORROSION AT ALL NUT PLATE ATTACH POINTS. REPLACED FLOORBEAM IAW A318 SRM 51-42-11, PARA 5-7.
- [SDR UPS07449033](https://openairdocs.org/sdr/UPS07449033.md): Floorbeam · corroded · Jul 24, 2007 · N803FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED AFT GALLEY RT FLOORBEAM -Y1292, FR 68 TO FR69 CORRODED AT NUT PLATE FASTENER LOCATIONS.
- [SDR F3LA200700084](https://openairdocs.org/sdr/F3LA200700084.md): Contactor · damaged · Apr 27, 2007 · N803FR · Airbus A318111 · Electrical Power System Wiring
  > AIR RETURN AT 0130Z FOR MULTIPLE ECAMS ASSOCIATED W/AC ESS BUSS. DEPARTURE OUT OF KDEN, LEVELING AT 35,000 FT, RECEIVED ECAM ENG 1 IGN A AND ENG 2 IGN A, C/B TRIPPED L ELEC BAY, YAW DAMPER 1, RUD TRIM 1, AND TRV LIM 1. CAPTAINS PFD ND FWD DISPLAYS ALL WENT B
- [SDR F3LA200600063](https://openairdocs.org/sdr/F3LA200600063.md): Line · leaking · Jun 30, 2006 · N803FR · Airbus A318111 · Hydraulic System, Main
  > DURING CRUISE, FLIGHT CREW REPORTED -Y- HYDRAULIC SYSTEM LEVEL LOW. AS A PRECAUTIONARY MEASURE, AN EMERGENCY WAS DECLARED UPON LANDING AT PDX. REPLACED NR 2 ENGINE YELLOW SYSTEM CASE DRAIN RETURN LINE FOR LEAKING. RAN NR 2 ENGINE. OPS AND LEAK CHECKED NORM
- [SDR F3LA200500032](https://openairdocs.org/sdr/F3LA200500032.md): Controller · unserviceable · Jul 15, 2005 · N803FR · Airbus A318111 · Cabin Pressure Controller
  > FLT CREW REPORTED CABIN PRESSURIZATION FLUCTUATING FOLLOWED BY NR 2 CONTROLLER FAILURE. ECAM EXCESS CABIN ALT. AT APPROX 30,000 FT & CLIMBING. NOTICED CABIN ALT SHOWING IN EXCESS OF 29,000 FT, CABIN MODE NR 1 CONTROLLER LATER ASSUMED CONTROL & CABIN PRESSURE
- [SDR F3LA200400065](https://openairdocs.org/sdr/F3LA200400065.md): Control Unit · odor · Jun 6, 2004 · N803FR · Airbus A318111 · Auto Flight System
  > IN CRUISE CREW REPORTED SMOKE COMING FROM FLIGHT CONTROL UNIT. NO ECAMS NOTED, SMOKE/AVNCS SMOKE. QRH PROCEDURE APPLIED, EMERGENCY DECLARED. DIVERTED TO OKC & LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF FWD E&E BAY, MID & AFT E&E BAY, MID LT E&E BAY A
- [SDR F3LA200300136](https://openairdocs.org/sdr/F3LA200300136.md): Power Supply · inoperative · Sep 15, 2003 · N803FR · Airbus A318111 · Emergency Lighting
  > FLIGHT CREW REPORTED SEAT BELT/NO SMOKING LIGHTS AND FWD GALLEY EXIT SIGNS INOPERATIVE. REPLACED EPSU IAW MM 33-51-13-04.

## 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 = 'N803FR' AND deregistration_id = 'N803FR-2014-01-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N803FR-2014-01-22/reports

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