# Service difficulty reports: N806FR, cancelled Sep 28, 2011 A list on [N806FR, cancelled Sep 28, 2011](https://openairdocs.org/deregistered/N806FR-2011-09-28.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2010031000364](https://openairdocs.org/sdr/F3LA2010031000364.md): Panel · delaminated · Mar 4, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > REFFERENCE NON ROUTINE NR N0072. DURING C4 S1 C-CHECK INSP NOTED AFT CARGO TRANSITION PANEL 151CH DELAMINATED. MX R & R AFT CARGO TRANSITION PANEL 151CH IAW AMM 53-42-14-400-001. - [SDR F3LA2010030800358](https://openairdocs.org/sdr/F3LA2010030800358.md): Plate · corroded · Feb 25, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > REF NON ROUTINE NR N0250. DURING C4 S1 CHECK INSP NOTED SEVERAL GOUGES ON BOTTOM/ EDGE OF R1 DOOR GIRT BAR FWD BRACKET AND CORROSION AT CORNER. MX R & R PLATE IAW SRM 51-72-11. - [SDR F3LA2010030300355](https://openairdocs.org/sdr/F3LA2010030300355.md): Strip · corroded · Feb 25, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C4 SI C-CHECK INSP NOTED CORROSION ON THE R1 DOOR ENTRY WAY STRIP. MX R & R STRIP IAW WC CP053-12. - [SDR F3LA2010030300354](https://openairdocs.org/sdr/F3LA2010030300354.md): Strip · corroded · Feb 25, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > REF NON ROUTINE NR N0249. DURING C4 S1 C CHECK INSP NOTED CORROSION ON L1 DOOR ENTRYWAY STRIP. MX R & R STRIP IAW WC CP053-12. - [SDR F3LA2010030900360](https://openairdocs.org/sdr/F3LA2010030900360.md): Floor Support · corroded · Feb 24, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > REFERENCE NON ROUTINE NR N0195. DURING C4 S1 C-CHECK INSP NOTED CABIN MAIN FLOOR EXTRUSION CORRODED ON TOP AND BOTTOM SURFACE LOCATED BETWEEN FR69 AND FR70, 48 INCHES RT OF CTR LINE. MX R & R EXTRUSION IAW SRM 51-72-11. - [SDR F3LA2010030800359](https://openairdocs.org/sdr/F3LA2010030800359.md): Threshold · corroded · Feb 24, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > NON ROUTINE NR N0196. DURING C4 S1 CHECK INSP, NOTED CORROSION ON THE R2 DOOR THRESHOLD AROUND 2 FASTENERS LOCATED INBD OF THE AFT GIRT BAR LATCH. MX REMOVED LEVEL 1 CORROSION, R & R THRESHOLD PLATE IAW SRM 53-41-14 / 51-21-11 / 54-75-12. - [SDR F3LA2010030900363](https://openairdocs.org/sdr/F3LA2010030900363.md): Panel · delaminated · Feb 23, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C4 S1 C-CHECK INSP NOTED AFT CARGO COMPARTMENT SLOPE PANEL 1151BH DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 9701. - [SDR F3LA2010030900362](https://openairdocs.org/sdr/F3LA2010030900362.md): Panel · delaminated · Feb 23, 2010 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C4 S1 C-CHECK INSP NOTED FWD CARGO COMPARTMENT AFT WALL PANEL 132PW CRACKED AND DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 2001. - [SDR F3LA2010030900361](https://openairdocs.org/sdr/F3LA2010030900361.md): Floor Panel · delaminated · Feb 23, 2010 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C4 S1 C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOOR PANEL 151AH DELAMINATED. MX FABRICATED REPLACEMENT PANEL IAW AIM 9701. - [SDR F3LA2008111900719](https://openairdocs.org/sdr/F3LA2008111900719.md): Warning Light · failed · Nov 17, 2008 · N806FR · Airbus A318111 · Door Warning System > PILOT REPORTED THAT THE LEFT OVERWING EXIT SLIDE ARMED LIGHT IS ILLUMINATED WHEN ON MAINTENANCE BUS. EMERGENCY EXIT OPEN ECAM INDICATION. MAINTENANCE REMOVED AND REPLACED LEFT OVERWING SLIDE ARMED INDICATOR LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE - [SDR F3LA2008111700715](https://openairdocs.org/sdr/F3LA2008111700715.md): Control Panel · failed · Nov 16, 2008 · N806FR · Airbus A318111 · Emergency Lighting > PILOT REPORTED THE LEFT OVERWING EXIT SHOWS OPEN ON LOWER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND LEFT OVERWING LIGHT TO BE AT FAULT. THE WARNING LIGHT PANEL WAS REMOVED, REPLACED AND CHECKED IN ACCORDANCE WITH A318 AMM 52-73-21 PB 401. - [SDR F3LA200800558](https://openairdocs.org/sdr/F3LA200800558.md): Blanking Plate · corroded · Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C-CHECK, INSP NOTED L2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) - [SDR F3LA200800557](https://openairdocs.org/sdr/F3LA200800557.md): Blanking Plate · corroded · Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C-CHECK, INSP NOTED L2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) - [SDR F3LA200800556](https://openairdocs.org/sdr/F3LA200800556.md): Blanking Plate · corroded · Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C-CHECK, INSP NOTED R2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) - [SDR F3LA200800555](https://openairdocs.org/sdr/F3LA200800555.md): Blanking Plate · corroded · Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C-CHECK INSP, NOTED R2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) - [SDR F3LA200800554](https://openairdocs.org/sdr/F3LA200800554.md): Floor Panel · corroded · Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF WITH A NEW PANEL AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) - [SDR F3LA200800559](https://openairdocs.org/sdr/F3LA200800559.md): Shear Plate · corroded · Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C-CHECK INSP, NOTED CORROSION AROUND NUT CLIP HOLE APPROX 4.25 INCHES AFT OF FWD END ON RT SIDE FLOORBEAM ALONG Y1292 BETWEEN FR68 AND FR69. MAINTENANCE BLENDED AREA, FABRICATED FLANGE BUSHING AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZA - [SDR F3LA200800552](https://openairdocs.org/sdr/F3LA200800552.md): Sill · corroded · Aug 12, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSPECTION NOTED THE VERY AFT NUT PLATE HOLE ON L-2 DOOR SILL AT FRAME 68, JUST AFT OF GIRT BAR FITTING ASSEMBLY, WAS CORRODED. MAINTENANCE CUTOUT DAMAGE, MANUFACTURED REPAIR DOUBLER AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORI - [SDR F3LA200800553](https://openairdocs.org/sdr/F3LA200800553.md): Floorbeam · corroded · Aug 12, 2008 · N806FR · Airbus A318111 · Fuselage Main, Floor Beam > DURING C-CHECK, INSP NOTED 3 OB NUT CLIP HOLES CORRODED ON FLOORBEAM Y1292 (L-2) AT FR 67. MAINT REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) - [SDR F3LA200800550](https://openairdocs.org/sdr/F3LA200800550.md): Floor Panel · gouged · Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT RT AFT UPPER TRANSITION PANEL 132EG HAD A GOUGE. MAINTENANCE REPAIRED DAMAGED PANEL 132EG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSP - [SDR F3LA200800549](https://openairdocs.org/sdr/F3LA200800549.md): Floor Panel · damaged · Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT RT TRANSITION PANEL 162BF WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 162BF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN - [SDR F3LA200800548](https://openairdocs.org/sdr/F3LA200800548.md): Floor Panel · damaged · Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT TRANSITION PANEL 161CF WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 161CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND - [SDR F3LA200800547](https://openairdocs.org/sdr/F3LA200800547.md): Floor Panel · punctured · Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131CG HAS SEVERAL HOLES. MAINTENANCE REPAIRED DAMAGED PANEL 131CG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED - [SDR F3LA200800546](https://openairdocs.org/sdr/F3LA200800546.md): Floor Panel · punctured · Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131AF HAS SEVERAL HOLES. MAINTENANCE REPAIRED DAMAGED PANEL 131AF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTE - [SDR F3LA200800551](https://openairdocs.org/sdr/F3LA200800551.md): Floor Panel · damaged · Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT LT TRANSITION PANEL 151HH WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 151HH IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPSH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOU - [SDR F3LA200800385](https://openairdocs.org/sdr/F3LA200800385.md): Servo Control · inoperative · Jun 23, 2008 · N806FR · Airbus A318111 · Landing Gear Steering System > DURING TAXI OUT, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING FAULT AND LOSS OF STEERING. MAINT REMOVED AND REPLACED NLG STEERING SERVO CONTROL VALVE IAW AMM 32-51-51 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND OP - [SDR F3LA200700360](https://openairdocs.org/sdr/F3LA200700360.md): Tube · damaged · Dec 1, 2007 · N806FR · Airbus A318111 · Hydraulic System, Main > FLIGHT CREW REPORTED YELLOW HYDRAULIC RESERVOIR LOW LEVEL INDICATION IN COCKPIT. REF TSM 52-36-00-810-805, FOUND YELLOW SYSTEM LOW PRESSURE SWITCH TUBE DAMAGED. REMOVED AND REPLACED LOW PRESSURE SWITCH TUBE IAW AMM 29-13-49-000-005 AND 29-13-49-400-005. PER - [SDR F3LA200700130](https://openairdocs.org/sdr/F3LA200700130.md): Line · worn · Jun 9, 2007 · N806FR · Airbus A318111 · Hydraulic System, Main > FLIGHT CREW REPORTED YELLOW HYDRAULIC QUANTITY LOW. FOLLOWED HYD QTY LOW ECAM: PTU-OFF; ENG DRIVEN PUMP-OFF. YELLOW HYDRAULIC PUMP NEVER CAVITATED OR OVERHEATED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. PERF - [SDR F3LA200500019](https://openairdocs.org/sdr/F3LA200500019.md): Cooling Fan · inoperative · May 18, 2005 · N806FR · Airbus A318111 · Air Distribution Fan > FLIGHT CREW REPORTED LIVE TV SMOKE WARNING LIGHT DURING FLIGHT. INSPECTED LIVE TV RACK, FOUND COOLING FAN INOP (NO SMOKE PRESENT). REPLACED LTV COOLING FAN ASSY PER LTV AMM 44-25-00. OPS CHECK NORMAL. ## 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 = 'N806FR' AND deregistration_id = 'N806FR-2011-09-28' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N806FR-2011-09-28/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.