# Service difficulty reports: N801FR, cancelled Jan 7, 2013

A list on [N801FR, cancelled Jan 7, 2013](https://openairdocs.org/deregistered/N801FR-2013-01-07.md).

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

- [SDR F3LA2012053000764](https://openairdocs.org/sdr/F3LA2012053000764.md): Girt Bar · out of adjust · May 29, 2012 · N801FR · Airbus A318111 · Emergency Equipment
  > L2 DOOR SLIDE DOES NOT SHOW ARMED IN FLIGHT SHOWS ARMED ON GROUND. FOUND L2 DOOR GIRT BAR FITTINGS OUT OF ADJUSTMENT. ADJUSTED GIRT BAR FITTINGS IAW AMM 52-13-22-820-056-A.
- [SDR F3LA2012053000762](https://openairdocs.org/sdr/F3LA2012053000762.md): Actuator · failed · May 25, 2012 · N801FR · Airbus A318111 · Cabin Cooling System
  > STRONG ELECTRICAL/OIL ODOR FUMES IN COCKPIT AND CABIN ON CLIMB. RETURNED TO DEPARTURE. NR 1 PACK OVERHEAT FAULT. SHUTDOWN PACK, BLOWING VERY HOT AIR. REMOVE AND REPLACE NR 1 ACM IAW AMM 21-52-21 PB 401. OPS CHECKED GOOD.
- [SDR F3LA2012003080720](https://openairdocs.org/sdr/F3LA2012003080720.md): Shear Plate · cracked · Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > C-CHECK: FUSELAGE LT SIDE AT FRAME 68, STRINGER 23, LEFT LATERAL SHEAR PLATE CRACKED. R & R PLATE IAW SRM 51-42-11, PAR 6.B.
- [SDR F3LA2012003070719](https://openairdocs.org/sdr/F3LA2012003070719.md): Floorbeam · corroded · Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > C-CHECK: MAIN CABIN FRAME 68 FLOOR PANEL FASTENER HOLES BETWEEN V1292, FLOORBEAM HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-73-00 PARAGRAPH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-14, FIGURE 101, SHEET 1.
- [SDR F3LA2012003060717](https://openairdocs.org/sdr/F3LA2012003060717.md): Floorbeam · corroded · Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > C-CHECK: MAIN CABIN FLOORBEAM HAS CORROSION AROUND FASTENER HOLES FRAME 66 TO FRAME 68, -Y765. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.
- [SDR F3LA2012003060716](https://openairdocs.org/sdr/F3LA2012003060716.md): Frame Splice · corroded · Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Main, Frame
  > C-CHECK: AFT GALLEY AREA FRAME 70, -Y1292 SPLICE PLATE (SHEAR PLATE) HAS CORROSION. R & R AFT GALLEY SHEAR PLATE IAW SRM 51-42-11, PARAGRAPH 17-18 AND EO AO-53EO-31 434, KIT PIN F9-531207DOL R02.
- [SDR F3LA2012022800712](https://openairdocs.org/sdr/F3LA2012022800712.md): Battery · failed · Feb 23, 2012 · N801FR · Airbus A318111 · Emergency Lighting
  > BATTIERY 10 WL FAILED CAPACITY TEST IAW CARD A332204-02. REPLACED EPSU BATTERY 10 WL IAW AMM33-51-38-400-002-A.
- [SDR F3LA2012020700705](https://openairdocs.org/sdr/F3LA2012020700705.md): Engine · making metal · Feb 2, 2012 · N801FR · Airbus A318111 · Engine (Turbine/Turboprop)
  > ABORTED TAKEOFF. UNUSUAL VIBRATION NOTED ON START OF NR 2 ENGINE DURING TAXI. NO ECAMS NOTED. ON APPLICATION OF TAKE OFF THRUST, A LOUD COMPRESSOR STALL, FLAMES NOTED BY TOWER FROM ENGINE REAR. ECAM FOR NR 2 OIL FILTER CLOGGED. IMMEDIATELY SECURED NR 2 EN
- [SDR F3LA2010111400550](https://openairdocs.org/sdr/F3LA2010111400550.md): Battery Pack · discharged · Nov 12, 2010 · N801FR · Airbus A318111 · Emergency Lighting
  > BATTERY PACK 12W FAILED CAPACITY CHECK IAW TASK CARD A332204-02. REPLACED ESPU 12WL IAW AMM 33-51-38, PB 401.
- [SDR F3LA2010072500474](https://openairdocs.org/sdr/F3LA2010072500474.md): Encoder · faulty · Jul 21, 2010 · N801FR · Airbus A318111 · Audio/Video Monitoring
  > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0526. EMERGENCY LIGHT OPERATIONAL TEST FAILED WITH A CLASS 1 MESSAGE EPSU (11WL) AND (12WL). FOUND HIGH AND LOW CODING SWITCHES ON TERMINATION/CONNECTION BOX 3000RH8-DEU B TO BE CODED ONE NOTCH OFF. SET CODING POTENT
- [SDR F3LA2010072500473](https://openairdocs.org/sdr/F3LA2010072500473.md): Light · inoperative · Jul 20, 2010 · N801FR · Airbus A318111 · Emergency Lighting
  > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0499. DURING TEST FORWARD EMERGENCY LIGHT 61WL WOULD NOT ILLUMINATE. TROUBLESHOT SYSTEM IAW A318 TSM 25-62-00-810-813. FOUND TWO BULBS BURNT OUT. REPLACED BULBS IAW A318 AMM 33-51-15 PAGE BLOCK 401. OPERATIONAL TES
- [SDR F3LA2010072500472](https://openairdocs.org/sdr/F3LA2010072500472.md): Flap · damaged · Jul 12, 2010 · N801FR · Airbus A318111 · Trailing Edge Flaps
  > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0001. TEMPORARY REPAIR TO LIGHTNING STRIKE DAMAGE ON RIGHT WING OUTBOARD FLAP TRAILING EDGE 4.25 INCHES FROM OUTBOARD EDGE AND 3.5 INCHES FROM TRAILING EDGE. DAMAGE MEASURED 1.75 X 0.50 INCH. INSTALLED PERMANENT REPA
- [SDR F3LA2009042100078](https://openairdocs.org/sdr/F3LA2009042100078.md): Computer · inoperative · Apr 20, 2009 · N801FR · Airbus A318111 · Flight Control System
  > PILOT REPORTED AFTER TAKEOFF THE AIRCRAFT DID NOT AUTO TRIM, CONSTANT FORWARD PRESSURE WAS REQUIRED TO MAINTAIN DESIRED PITCH. SAME RESULT ON BOTH STICKS. AIRCRAFT TRIMMED NOSE UP IF NO STICK INPUT RUNAWAY NOSE UP. MAINTENANCE REMOVED AND REPLACED THE NR 2
- [SDR F3LA2008111900718](https://openairdocs.org/sdr/F3LA2008111900718.md): Fitting · out of adjust · Nov 18, 2008 · N801FR · Airbus A318111 · Fuselage Main, Attach Fittings
  > DURING C4 C-CHECK, INSPECTION NOTED THE R2 DOOR ARMED HANDLE WAS SPONGY WHEN IN THE ARMED POSITION. MAINTENANCE ADJUSTED THE R2 GIRT BAR FITTING AND PERFORMED OPERATION CHECK IN ACCORDANCE WITH A318 AMM 52-13-00-820-001.
- [SDR F3LA2008111800717](https://openairdocs.org/sdr/F3LA2008111800717.md): Battery · failed · Nov 18, 2008 · N801FR · Airbus A318111 · Emergency Lighting
  > DURING C4 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY LIGHT TEST THROUGH THE CENTRALIZED FAULT DISPLAY UNIT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN ACCORDANCE WITH AMM 33-51-38-000-001.
- [SDR F3LA2008111800716](https://openairdocs.org/sdr/F3LA2008111800716.md): Hook · worn · Nov 17, 2008 · N801FR · Airbus A318111 · Passenger/Crew Doors
  > DURING C4 C-CHECK, INSPECTION NOTED THAT DURING INSTALLATION OF THE ESCAPE SLIDE THE L2 DOOR HANDLE WAS ABLE TO MOVE INTO THE CLOSED POSITION BEFORE THE DOOR WAS CLOSED. MAINTENANCE REMOVED AND REPLACED THE DOOR HOOK IN ACCORDANCE WITH AMM 52-13-21-420-052.
- [SDR F3LA2008111700713](https://openairdocs.org/sdr/F3LA2008111700713.md): Hinge Fitting · gouged · Nov 15, 2008 · N801FR · Airbus A318111 · Spoilers
  > DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 4 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.
- [SDR F3LA2008111700712](https://openairdocs.org/sdr/F3LA2008111700712.md): Hinge Fitting · gouged · Nov 15, 2008 · N801FR · Airbus A318111 · Spoilers
  > DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 3 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776.
- [SDR F3LA200700379](https://openairdocs.org/sdr/F3LA200700379.md): Battery Pack · inoperative · Dec 24, 2007 · N801FR · Airbus A318111 · Emergency Lighting
  > FLIGHT CREW REPORTED EPSU "13WL" AFT LEFT MESSAGE. REPLACED EPSU BATTERY AT 13WL LOCATION IAW AMM 33-51-38-400-002. OPS CHECK GOOD.
- [SDR F3LA200700108](https://openairdocs.org/sdr/F3LA200700108.md): Oxygen Mask · no test · May 4, 2007 · N801FR · Airbus A318111 · Passenger Oxygen System
  > WHILE PERFORMING MASK DROP TEST, ROWS 15 AND AFT ON BOTH SIDES, 7, 8, AND 9 RT SIDE, R2 DOOR AND C LAV DID NOT DROP COMPLETELY. RESET MASKS AND PERFORMED TEST AGAIN IAW AMM 35-23-00-710-001. OPS CHECKED GOOD.
- [SDR F3LA200700101](https://openairdocs.org/sdr/F3LA200700101.md): Shear Plate · corroded · Apr 27, 2007 · N801FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C-3 CHECK, INSPECTION REPORTED LT SIDE OF CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11.
- [SDR F3LA200700091](https://openairdocs.org/sdr/F3LA200700091.md): Web · corroded · Apr 27, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED RT SIDE CABIN FLOOR WEB 69 AND 70 HAD VERY LIGHT CORROSION AT NUT PLATES, MOSTLY ON LWR SIDE. REPLACED SHEAR PLATE IAW SRM 51-42-11.
- [SDR F3LA200700107](https://openairdocs.org/sdr/F3LA200700107.md): Floorbeam · damaged · Apr 25, 2007 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED FWD SPLICE OF R2 DOOR SILL HAD TWO DOUBLE DRILLED HOLES, ONE COMPLETELY THROUGH THE FWD FLOORBEAM. REPLACED DAMAGED FLOORBEAM IAW SRM 51-42-11.
- [SDR F3LA200700106](https://openairdocs.org/sdr/F3LA200700106.md): Floor Panel · corroded · Apr 25, 2007 · N801FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C-3 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF AT R-2 DOOR CORRODED ON BOTTOM OF PANEL. REPLACED FLOORBOARD 262FF IAW AMM 53-42-12-400-001.
- [SDR F3LA200700098](https://openairdocs.org/sdr/F3LA200700098.md): Rib · scratched · Apr 25, 2007 · N801FR · Airbus A318111 · Vertical Stabilizer, Spar/Rib
  > DURING C-3 CHECK, INSPECTION REPORTED LE OF VERTICAL STAB FIN HAD DEEP SCRATCH MARKS (TOOL MARKS) BETWEEN PANELS NR 322BL AND 322CL ON ATTACHMENT BRACKET WHERE PANEL 322BL ATTACHES. REPLACED RIB FOR VERT STAB LE BETWEEN PANELS 322BL AND 322CL IAW SRM 51-42-11
- [SDR F3LA200700099](https://openairdocs.org/sdr/F3LA200700099.md): Latch · missing · Apr 24, 2007 · N801FR · Airbus A318111 · Escape Slide
  > DURING C-3 CHECK, INSPECTION REPORTED AFT OTBD NUTPLATE FOR THE AFT FILLER PLATE AROUND THE L2 DOOR GIRT BAR LATCH MISSING. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700097](https://openairdocs.org/sdr/F3LA200700097.md): Splice · corroded · Apr 24, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON OTBD UPPER ANGLE AFT ATTACHMENT HOLE UPON REMOVAL OF L2 DOOR SILL SPLICE ANGLES FWD OF FR66. REPLACED L2 DOOR SILL SPLICE ANGLES IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700096](https://openairdocs.org/sdr/F3LA200700096.md): Sill · corroded · Apr 24, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLE UNDER THE FWD GIRT FITTING ON THE L2 DOOR SILL. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700095](https://openairdocs.org/sdr/F3LA200700095.md): Sill · corroded · Apr 24, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUTPLATE HOLES ON THE L2 DOOR SILL PLATE AT FR66. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700094](https://openairdocs.org/sdr/F3LA200700094.md): Sill · corroded · Apr 24, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL PLATE HAD CORROSION FWD OF FR66. REPLACED L2 DOOR SILL IAW 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700093](https://openairdocs.org/sdr/F3LA200700093.md): Sill · corroded · Apr 24, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR SILL THRESHOLD HAD CORROSION AROUND SEVERAL NUTPLATE HOLES. REPLACED L2 DOOR SILL IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700092](https://openairdocs.org/sdr/F3LA200700092.md): Floorboard · corroded · Apr 24, 2007 · N801FR · Airbus A318111 · Fuselage Floor Panel
  > DURING C-3 CHECK, INSPECTION REPORTED FLOORBOARD 222FF (R1 ENTRY) CORRODED. REPLACED FLOORBOARD 222FF IAW AMM 53-12-12-400-001.
- [SDR F3LA200700100](https://openairdocs.org/sdr/F3LA200700100.md): Sill · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Fuselage Miscellaneous Structure
  > DURING C-3 CHECK, INSPECTION REPORTED R2 DOOR SILL PLATE CORRODED FWD OF FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11.
- [SDR F3LA200700090](https://openairdocs.org/sdr/F3LA200700090.md): Floorbeam · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM -Y1292, AFT OF FR68. REPLACED FLOORBEAM AT FR68 STATION -Y1292 IAW SRM 51-42-11.
- [SDR F3LA200700088](https://openairdocs.org/sdr/F3LA200700088.md): Floorbeam · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 FWD OF FR68. REPLACED FLOORBEAM AT Y1292 FWD OF FR68 IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700087](https://openairdocs.org/sdr/F3LA200700087.md): Floorbeam · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE ON FLOORBEAM Y1292, AFT OF FR66. REPLACED FLOORBEAM AT Y1292 AFT OF FR66 IAW SRM 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700089](https://openairdocs.org/sdr/F3LA200700089.md): Floorbeam · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Fuselage Main, Floor Beam
  > DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM Y1292 AFT OF FR68. REPLACED FLOORBEAM AT Y1292 AFT OF FR68 IAW 51-42-11, FIG 6 AND 7.
- [SDR F3LA200700086](https://openairdocs.org/sdr/F3LA200700086.md): Bushing · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Nose/Tail Landing Gear
  > DURING C-3 CHECK, INSPECTION REPORTED NLG UPPER TORSION LINK FROM STRUT CORRODED INSIDE ATTACH LUG. REMOVED CORROSION UNDER BUSHINGS OF NLG UPPER TORSION LINK ATTACH POINT AND REPLACED BUSHINGS IAW EA NR A8-32R-11869.
- [SDR F3LA200700085](https://openairdocs.org/sdr/F3LA200700085.md): Bolt · corroded · Apr 21, 2007 · N801FR · Airbus A318111 · Wing, Attach Fittings
  > DURING C-3 CHECK, INSPECTION REPORTED WINGLET ATTACH HARDWARE RUSTY. REPLACED WINGLET ATTACH HARDWARE (MILD SURFACE CORROSION ON BOLT HEADS) ON LT WING IAW AMM 57-31-22-400-001.
- [SDR F3LA200600048](https://openairdocs.org/sdr/F3LA200600048.md): Computer · failed · Jun 8, 2006 · N801FR · Airbus A318111 · Elevator Control System
  > AIR TURNBACK. FLIGHT CREW REPORTED AILERON SERVO ECAM ON CLIMB. NORMAL LAW WAS LOST. RETURNED TO DEN AND PERFORMED AN OVERWEIGHT LANDING WITHOUT INCIDENT. REPLACED ELAC NR 2 PER TSM 27-93-00-810-855. OPS CHECKED GOOD PER AMM 27-93-34. PERFORMED AFS LAND
- [SDR F3LA200500042](https://openairdocs.org/sdr/F3LA200500042.md): Computer · failed · Sep 17, 2005 · N801FR · Airbus A318111 · Pitot/Static Anti-Ice System
  > FLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR 20 MIN OUT FROM DEN FL390. APPROXIMATELY 20 SEC AFTER ODOR BEGAN, ECAM ANTI-ICE CAPT L & R STAT ILLUMINATED. REPLACED PROBE HEAT COMPUTER PER MM 30-31-34, PB 401. COMPLIED WITH MM 24-00-00-810-823 AND 30-31-20-
- [SDR F3LA200500037](https://openairdocs.org/sdr/F3LA200500037.md): Cooling Fan · failed · Aug 12, 2005 · N801FR · Airbus A318111 · Entertainment System
  > FLIGHT CREW REPORTED LIVE TV SMOKE DETECTION WARNING HORN SOUNDED DURING FLIGHT. LIVE TV FAN C/B 2000VU POPPED AND WOULD NOT RESET. REPLACED AFT RACK COOLING FAN PER AMM 44-25-00, PAGE 471. OPS CHECK GOOD.
- [SDR F3LA200400070](https://openairdocs.org/sdr/F3LA200400070.md): Sleeve · damaged · Jul 19, 2004 · N801FR · Airbus A318111 · Wheel/Ski/Float
  > FLIGHT CREW REPORTED NOSE WHEEL VIBRATION ON GEAR RETRACTION. FOUND NOSE WHEEL LT BEARING AND SLEEVE DAMAGED. REMOVED SLEEVE AND INSPECTED AXLE FOR DAMAGE. NO DAMAGE NOTED. INSTALLED SERVICEABLE AXLE SLEEVE AT LT POSITION PER AMM 32-41-12-000-002 AND 32-41
- [SDR F3LA200400005](https://openairdocs.org/sdr/F3LA200400005.md): Windshield · cracked · Feb 4, 2004 · N801FR · Airbus A318111 · Flight Compartment Windows
  > AIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S WINDSHIELD PER 56-11-11-000-001 AND 56-11-11-400-001. PERFORMED TEST OF WINDOW HEAT AND DEFOGGING PER 30

## 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 = 'N801FR' AND deregistration_id = 'N801FR-2013-01-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N801FR-2013-01-07/reports

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