# Service difficulty reports: N906FR, cancelled Dec 1, 2016

A list on [N906FR, cancelled Dec 1, 2016](https://openairdocs.org/deregistered/N906FR-2016-12-01.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 2 · 62 reports

- [SDR F3LA2014120301092](https://openairdocs.org/sdr/F3LA2014120301092.md): Battery · discharged · Dec 3, 2014 · N906FR · Airbus A319111 · Emergency Lighting
  > EPSU BATTERY 13WL AFT LT FAILED CAPACITY TEST. R & R EPSU BATTERY 13WL IAW AMM 33-51-38 PB401. OPERATIONS CHECKED GOOD.
- [SDR F3LA2013102800927](https://openairdocs.org/sdr/F3LA2013102800927.md): Battery · no test · Oct 27, 2013 · N906FR · Airbus A319111 · Emergency Lighting
  > LIGHT BATTERY 12WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY ASSY 12WL.
- [SDR F3LA2013102800926](https://openairdocs.org/sdr/F3LA2013102800926.md): Battery · failed · Oct 27, 2013 · N906FR · Airbus A319111 · Emergency Lighting
  > LIGHT BATTERY 10WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY ASSY 10WL.
- [SDR F3LA2013040200844](https://openairdocs.org/sdr/F3LA2013040200844.md): Floorbeam · corroded · Mar 4, 2013 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM AT L2 ENTRY AREA HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.
- [SDR F3LA2013040200843](https://openairdocs.org/sdr/F3LA2013040200843.md): Tray · cracked · Mar 4, 2013 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > AFT WET AREA LT SHEAR PLATE TRAY CRACKED. R & R LT SHEAR PLATE TRAY IAW SRM 51-42-11, PARA 6 AND 7.
- [SDR F3LA2013040200842](https://openairdocs.org/sdr/F3LA2013040200842.md): Seat Track · corroded · Mar 3, 2013 · N906FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK Y-1292 HAS CORROSION BETWEEN FR17 - 18. R & R BEAM IAW SRM 51-42-11, PARA 5 AND 7.
- [SDR F3LA2013040200841](https://openairdocs.org/sdr/F3LA2013040200841.md): Plate · cracked · Mar 3, 2013 · N906FR · Airbus A319111 · Fuselage Main, Structure
  > LT LATERAL SHEAR PLATE CRACKED AFT OF FR69. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6 AND 10.
- [SDR F3LA2013040200840](https://openairdocs.org/sdr/F3LA2013040200840.md): Plate · cracked · Mar 3, 2013 · N906FR · Airbus A319111 · Fuselage Main, Structure
  > RT LATERAL SHEAR PLATE CRACKED AFT OF FR 69. R & R SHEAR PLATE IAW SRM 51-42-11, PARA 6 AND 10.
- [SDR F3LA2012120600814](https://openairdocs.org/sdr/F3LA2012120600814.md): Lamp · inoperative · Dec 5, 2012 · N906FR · Airbus A319111 · Emergency Lighting
  > DURING HEAVY CHECK FOUND SEAT 22 ABC EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51 -19, PB 401. OPS CHECKED GOOD.
- [SDR F3LA2012120600815](https://openairdocs.org/sdr/F3LA2012120600815.md): Lamp · inoperative · Dec 5, 2012 · N906FR · Airbus A319111 · Emergency Lighting
  > DURING HEAVY CHECK FOUND SEAT 17 ABC EMERGENCY LIGHT INOPERATIVE. R & R SEAT 17 ABC EMERGENCY LIGHT IAW AMM 33-51 -19 PB 401. OPS CHECKED GOOD.
- [SDR F3LA2012062600771](https://openairdocs.org/sdr/F3LA2012062600771.md): Socket · smoke · Jun 24, 2012 · N906FR · Airbus A319111 · Emergency Lighting
  > A/C LP 686501; EMERGENCY EXIT LIGHT PATH 17C ILLUMINATED AND PRODUCED SMOKE AFTER POWER TRANSFER. NOTE; PASSENGER SMASHED LIGHT UNTIL IT QUIT SMOKING. R & R LIGHT ASSY, OPS CHECKED GOOD REF AMM 33-51-19 PB401. INSPECTED SEAT WIRING, NO FURTHER DAMAGED NOTED.
- [SDR F3LA2011063000659](https://openairdocs.org/sdr/F3LA2011063000659.md): Thrust Reverser · damaged · Jun 27, 2011 · N906FR · Airbus A319111 · Engine Thrust Reverser
  > C-CHECK: NON ROUTINE NR 22652; NR 2 ENGINE HAS LIGHTNING STRIKE AT THE 4 O'CLOCK POSITION. REPAIRED NR 2 ENGINE OTBD THRUST REVERSER AT THE 4 O'CLOCK POSITION IAW CMM 54-30-00, REPAIR NR 13.
- [SDR F3LA2010061400441](https://openairdocs.org/sdr/F3LA2010061400441.md): Connector · cocked · Jun 13, 2010 · N906FR · Airbus A319111 · Light System Wiring
  > REF HEAVY MX NON ROUTINE N0674. OPS TEST OF EMERGENCY LIGHTS FAILS. FOUND CONNECTOR FOR EPSU 10WL COCKED. RESEATED CONNECTOR. PERFORMED OPS CHECK IAW AMM 33-51-00-710-050. OPS CHECK GOOD.
- [SDR F3LA2010061000438](https://openairdocs.org/sdr/F3LA2010061000438.md): Floor Support · corroded · Jun 6, 2010 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON-ROUTINE N0480. AFT CABIN RT FLOORBEAM -Y1292 FROM FRAME 66 TO FRAME 68 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.
- [SDR F3LA2010061000440](https://openairdocs.org/sdr/F3LA2010061000440.md): Floor Support · corroded · Jun 4, 2010 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON ROUTINE N0478. AFT CABIN RT FLOORBEAM -Y765 FROM FRAME 67 TO FRAME 70 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.
- [SDR F3LA2010061000439](https://openairdocs.org/sdr/F3LA2010061000439.md): Floor Support · corroded · Jun 4, 2010 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON ROUTINE N0477. AFT CABIN LT FLOORBEAM Y1292 FROM FRAME 68 TO FRAME 69 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.
- [SDR F3LA2010061000437](https://openairdocs.org/sdr/F3LA2010061000437.md): Floor Support · corroded · Jun 4, 2010 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON ROUTINE N0479. AFT CABIN RIGHT HAND FLOORBEAM -Y1293 FROM FRAME 68 TO FRAME 69 TOP SURFACE HAS CORROSION. R & R FLOORBEAM REF A319 AMM 51-72-11.
- [SDR F3LA2010061000436](https://openairdocs.org/sdr/F3LA2010061000436.md): Floorbeam · corroded · Jun 4, 2010 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REF HEAVY MX NON-ROUTINE N0476. AFT CABIN LT FLOORBEAM Y1292 FROM FRAME 66 TO FRAME 68 HAS CORROSION ON TOP SURFACE. R & R FLOORBEAM REF AMM 51-72-11.
- [SDR F3LA2010033000378](https://openairdocs.org/sdr/F3LA2010033000378.md): Proximity Sensor · inoperative · Mar 26, 2010 · N906FR · Airbus A319111 · Escape Slide
  > REF LOG PAGE NRS 537910 AND 537923. CAPTAIN NOTED RT OVERWING EXIT SLIDE NOT SHOWING ARMED. MX ISSUED MEL 25-60-04C, CONTROL NR 1074315, TO THE RT OVERWING SLIDE, REF LOG PAGE NR 537910. MX R & R PROXIMITY DETECTOR IAW AMM 52-73-11-400-004A. OPS CHECK GOOD,
- [SDR F3LA2010032200369](https://openairdocs.org/sdr/F3LA2010032200369.md): Hose · leaking · Mar 20, 2010 · N906FR · Airbus A319111 · Hydraulic System, Main
  > FLIGHT CREW NOTED GREEN RESERVOIR HYD PUMP LOW PRESSURE ECAM MESSAGE. AN EMERGENCY WAS DECLARED AND FLIGHT DIVERTED. MX AND INSP NOTED THE LT MLG DOOR ACTUATOR HYD LINE LEAKING. MX R & R LT MLG DOOR ACTUATOR HYD LINE IAW AMM 32-31-39, PB 401 AND SERVICED TH
- [SDR F3LA2009092500183](https://openairdocs.org/sdr/F3LA2009092500183.md): Strut · corroded · Sep 22, 2009 · N906FR · Airbus A319111 · Main Landing Gear Strut/Axle/Truck
  > LINE MX PERFORMED THE LT MLG STRUT REPACK AND FOUND CORROSION ON THE MAIN FITTING BORE WHERE THE LWR BRG IS INSTALLED. MX REMOVED THE CORROSION, PERFORMED NDT OF AREA, FLAP PEENED AREA, CADMIUM PLATED AREA, APPLIED PRIMER TO AREA AND REASSEMBLED STRUT. REF EA
- [SDR F3LA2008102700684](https://openairdocs.org/sdr/F3LA2008102700684.md): Heat Exchanger · odor · Oct 26, 2008 · N906FR · Airbus A319111 · Heating System
  > FLIGHT CREW MADE AN UNSCHEDULED LANDING DUE TO A STRONG ELECTRICAL SMELL THROUGHOUT THE AIRCRAFT CABIN ON CLIMB-OUT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THAT ALL AIRCRAFT BAY HEAT EXCHANGERS WERE REPLACED THE NIGHT BEFORE DURING SCHEDULED OVERNIGHT MAINT
- [SDR FLA200800128](https://openairdocs.org/sdr/FLA200800128.md): Light · inoperative · Mar 17, 2008 · N906FR · Airbus A319111 · Emergency Lighting
  > DURING THE CABIN CHECK, THE INSPECTION DISCLOSED EMERGENCY LIGHTS WERE NOT FUNCTIONING ON TWO ROWS (ROWS 8 AND 15). MAINTENANCE REPLACED THE EMERGENCY LIGHTS ON THE TWO MALFUNCTIONING ROWS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-19 PB 401. UPON COOM
- [SDR F3LA200700281](https://openairdocs.org/sdr/F3LA200700281.md): Wire Harness · damaged · Oct 14, 2007 · N906FR · Airbus A319111 · Light System Wiring
  > INSPECTION REPORTED SEAT ROW 9ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED WIRE HARNESS AT SEAT ROW 9ABC IAW ESPM 20-33-00. PERFORMED OPERATIONAL TEST ON EMERGENCY LIGHTS IAW AMM 33-51-00-710-007. OPS CHECK GOOD.
- [SDR F3LA200700081](https://openairdocs.org/sdr/F3LA200700081.md): Battery Pack · failed · Apr 18, 2007 · N906FR · Airbus A319111 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED FWD LEFT AND AFT LEFT EPSU BATTERIES FAILED CAPACITY CHECK. REPLACED EMERGENCY ESCAPE PATH LIGHT BATTERY PACKS, FWD, AFT, MID L AND MID R. OPS CHECKS NORMAL IAW AMM 33-51-38-00-002 AND 33-51-38-400-002.
- [SDR F3LA200700080](https://openairdocs.org/sdr/F3LA200700080.md): Wire Harness · damaged · Apr 17, 2007 · N906FR · Airbus A319111 · Light System Wiring
  > DURING C4/S1 CHECK, INSPECTION REPORTED SEAT EMERGENCY LIGHT AT ROW 21 INOP. REPINNED WIRE HARNESS ASSY 350WL10 UNDER ROW 21 IAW ASM 33-51-00, SCH 04, P101, SHEET 3. OPS CHECKED GOOD IAW AMM 33-51-00-710-008.
- [SDR F3LA200700062](https://openairdocs.org/sdr/F3LA200700062.md): Fire Detector · no test · Apr 16, 2007 · N906FR · Airbus A319111 · Fire Detection
  > DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT DETECTORS (2) FAILED TEST. REPLACED AFT CARGO COMPARTMENT FIRE DETECTORS (5WH AND 6WH). PERFORMED OPS TEST OF CARGO SMOKE DETECTORS IAW A319 AMM 26-16-15-000-001.
- [SDR F3LA200700056](https://openairdocs.org/sdr/F3LA200700056.md): Lamp · inoperative · Apr 16, 2007 · N906FR · Airbus A319111 · Emergency Lighting
  > DURING C4/S1 CHECK, INSPECTION REPORTED BULBS INOP IN ROW 4 AND 6 ABC SEAT FLOOR PATH LIGHTING. RELAMPED ROW 4 AND 6 ABC SEAT FLOOR PATH LIGHTS. OPS CHECK NORMAL IAW A319 AMM 33-51-00-710-007.
- [SDR F3LA200700078](https://openairdocs.org/sdr/F3LA200700078.md): Mount · chafed · Apr 11, 2007 · N906FR · Airbus A319111 · Battery Box Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED FRETTING ON BATTERY RACK MOUNTS. REPLACED (4) MOUNT FITTINGS AT FR 10 IAW EA NR A9-53R-10649.
- [SDR F3LA200700077](https://openairdocs.org/sdr/F3LA200700077.md): Bushing · worn · Apr 11, 2007 · N906FR · Airbus A319111 · Fuselage Main, Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED FRETTING ON C-16 CROSSBEAM, DOOR ACCESS 812 (LT AVIONICS DOOR). REMOVED BOLT. FOUND WEAR ON THE BUSHING. CLEANED AREA IAW A319111 SRM 51-42-11, DRAWING D53913231. REASSEMBLED WITH NEW BUSHING IAW A319111 AMM 20-21-11
- [SDR F3LA200700072](https://openairdocs.org/sdr/F3LA200700072.md): Floorbeam · corroded · Apr 9, 2007 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND FASTENER HOLES WHERE FLOORBEAM Y1292 ATTACHES TO FR68. REMOVED AND REPLACED FLOORBEAM ASSY. IAW A319 SRM 51-42-11.
- [SDR F3LA200700074](https://openairdocs.org/sdr/F3LA200700074.md): Bracket · corroded · Apr 8, 2007 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-4/S-1 CHECK, INSPECTION REPORTED BRACKET FOR ANTENNA CORRODED IN AFT PIT UNDER FLOOR PANEL 151VG, AT APPROX STR 43, BETWEEN FR 58 AND FR 59. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET IAW A319 SRM 51-42-11, PARA 6 D AND FIG 8; 51-31-00, TA
- [SDR F3LA200700060](https://openairdocs.org/sdr/F3LA200700060.md): Shear Tie · corroded · Apr 1, 2007 · N906FR · Airbus A319111 · Fuselage Internal Mounting Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED WEB PLATE SUPPORT UNDER SHEAR PLATE BETWEEN FR 69 AND FR 70 JUST BEHIND FLOORBEAM -Y1292 SUPPORT FRAME CORRODED. FOUND WEB PLATE SUPPORT TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, FIG 101. REMOVED AND REPLACED SHEAR PL
- [SDR F3LA200700053](https://openairdocs.org/sdr/F3LA200700053.md): Beam · bent · Mar 31, 2007 · N906FR · Airbus A319111 · Fuselage Main, Bulkhead
  > DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD BULKHEAD BEAM RT OF CENTER BENT. REPLACED BULKHEAD BEAM IAW A319 SRM 51-42-11, PARA. 5, PG 6-7 AND PARA 6, PG 22-23, AND SRM 51-44-21.
- [SDR F3LA200700079](https://openairdocs.org/sdr/F3LA200700079.md): Floorbeam · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLE AT FR 66 ON FLOORBEAM BETWEEN FR 66 AND FR 64 AT Y1292. REMOVED AND REPLACED FLOORBEAM ASSY IAW A319 SRM 51-42-11.
- [SDR F3LA200700076](https://openairdocs.org/sdr/F3LA200700076.md): Attach Fitting · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Nose/Tail Landing Gear
  > DURING C4/S1 CHECK, INSPECTION REPORTED INTERNAL CASTING AND THROUGH PIN BUSHING ON NLG UPPER TORSION LINK LUG CORRODED. REMOVED CORROSION AT UPPER TORSION LINK. TREATED, CAD PLATED AND REINSTALLED BUSHINGS IAW EA A9-32R-11842.
- [SDR F3LA200700054](https://openairdocs.org/sdr/F3LA200700054.md): Floorbeam · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 68 AND FR 69 AT Y1292. FLOORBEAM FOUND TO BE OUT OF LIMITS PER A319 ARM 51-00-14, FIG 101. REPLACED FLOORBEAM IAW A319 SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA200700064](https://openairdocs.org/sdr/F3LA200700064.md): Floorbeam · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR68 AND FR69 AT -Y1162. FOUND TO BE OUT LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED AND INSTALLED FLOORBEAM ASSY IAW A319 SRM 51-42-11.
- [SDR F3LA200700051](https://openairdocs.org/sdr/F3LA200700051.md): Bushing · broken · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C4/S1 CHECK, INSPECTION REPORTED RT SIDE FLOOR EXPANSION JOINT AT FRAME 35 HAD BROKEN BUSHING ON BOTH SEAT TRACK BEAMS. REMOVED AND REPLACED PLASTIC BUSHINGS ON BOTH RT SEAT TRACKS EXPANSION JOINTS AT FS 35 IAW A319 SRM 51-42-11, PARA 5.
- [SDR F3LA200700052](https://openairdocs.org/sdr/F3LA200700052.md): Bushing · broken · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4/S1 CHECK, INSPECTION REPORTED LT SIDE FLOOR EXPANSION JOINT AT FRAME 35 HAD BROKEN BUSHING ON BOTH SEAT TRACK BEAMS. REPLACED BOLTS AND BUSHINGS IN THE EXPANSION JOINTS AT FS 35 ON THE LT SIDE SEAT TRACKS IAW A319 SRM 51-42-11.
- [SDR F3LA200700057](https://openairdocs.org/sdr/F3LA200700057.md): Floor Support · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLE ON FLOORBEAM BETWEEN FR 66AND FR 68 AT Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW A319 SRM 51-00-14, FIG 8. REPLACED FLOORBEAM IAW A319 SRM 51-44-11 3B AND 51-42-11.
- [SDR F3LA200700055](https://openairdocs.org/sdr/F3LA200700055.md): Floorbeam · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 67 AND FR 68 AT-Y1292. FLOORBEAM WAS FOUND TO BE OUT OF LIMITS PER A319 SRM 51-00-14, FIG 101. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11.
- [SDR F3LA200700050](https://openairdocs.org/sdr/F3LA200700050.md): Sill · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED NUT CLIP AREA CORRODED ON FLOORBEAM Y1732 AT FR 66, FWD OF L-2 DOOR FRAME. REMOVED FASTENERS FROM L-2 DOOR SILL IAW A319 SRM 51-42-11, PARA. 5. REPLACED L2 DOOR SILL IAW A319 SRM 51-42-11, SRM 51-75-12, SRM 51-44-11, A
- [SDR F3LA200700070](https://openairdocs.org/sdr/F3LA200700070.md): Floorbeam · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C4/S1 CHECK, INSPECTION REPORTED LIGHT CORROSION AROUND NUT PLATE HOLE ON SEAT TRACK AT -Y1292, FR65. REMOVED AND INSTALLED FLOORBEAM IAW A319 SRM 51-42-11; 51-42-11, FIG 8; 51-42-11, PARA 7; AND 51-42-11, STEP 7 B.
- [SDR F3LA200700073](https://openairdocs.org/sdr/F3LA200700073.md): Shear Tie · sheared · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Internal Mounting Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE WAS SHEARED BETWEEN FR 68 AND FR 69 JUST OTBD OF FLOORBEAM Y1292. FABRICATED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11, FIG 7 AND 8; 53-41-14, FIG 18; 51-42-11; AND 51-20-00, PARA. 3; 51-23-11.
- [SDR F3LA200700049](https://openairdocs.org/sdr/F3LA200700049.md): Sill · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED NUT CLIP AREA CORRODED ON FLOORBEAM -Y1732 AT FR 66, FWD OF R-2 DOOR FRAME. REMOVED AND REPLACED R-2 DOOR SILL IAW A319 SRM 51-42-11; 51-42-11, FIG 8; 51-42-11, PARA. 6; 51-21-11; 51-75-12; 51-12-11; 51-45-11, FIG 8; AN
- [SDR F3LA200700058](https://openairdocs.org/sdr/F3LA200700058.md): Support · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED LT SUPPORT FRAME CORRODED BETWEEN FR 69 AND FR 70, JUST BEHIND FLOORBEAM -Y1292. FOUND SUPPORT FRAME TO BE OUT OF LIMITS IAW A319 SRM 51-74-00. REMOVED AND REPLACED SUPPORT FRAME IAW A319 SRM 51-72-11, PAGES 1 AND 2.
- [SDR F3LA200700063](https://openairdocs.org/sdr/F3LA200700063.md): Shear Tie · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Internal Mounting Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT SHEAR PLATE CORRODED BETWEEN FR 69 AND FR 70, JUST BEHIND FLOORBEAM Y1292. REMOVED AND REPLACED SHEAR PLATE SUPPORT FRAME AND SHEAR PLATE IAW A319 SRM 51-42-11, FIG. 8; 51-44-11, TABLE 3; 51-72-11, PARA. 5.A.; 5
- [SDR F3LA200700061](https://openairdocs.org/sdr/F3LA200700061.md): Shear Tie · corroded · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Internal Mounting Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT FRAME (SHEAR PLATE) BETWEEN FR69 AND FR70, JUST BEHIND FLOORBEAM -Y1292 CORRODED. FOUND SHEAR PLATE TO BE OUT OF LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED SHEAR PLATE IAW A319 SRM 51-42-11, FIG 8. LOCATE
- [SDR F3LA200700059](https://openairdocs.org/sdr/F3LA200700059.md): Shear Tie · sheared · Mar 30, 2007 · N906FR · Airbus A319111 · Fuselage Internal Mounting Structure
  > DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR PLATE SHEARED BETWEEN FR 68 AND FR 69, JUST OTBD OF FLOORBEAM -Y1292. REMOVED AND INSTALLED SHEAR PLATE IAW A319 SRM 53-41-14, FIG 18, 51-42-11, 51-20-00, PARA 3, AND 51-23-11.

Next page: https://openairdocs.org/deregistered/N906FR-2016-12-01/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 = 'N906FR' AND deregistration_id = 'N906FR-2016-12-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N906FR-2016-12-01/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.