# Service difficulty reports: N907FR, cancelled Jul 9, 2009 A list on [N907FR, cancelled Jul 9, 2009](https://openairdocs.org/deregistered/N907FR-2009-07-09.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA200700142](https://openairdocs.org/sdr/F3LA200700142.md): Attach Angle · damaged · Jun 23, 2007 · N907FR · Airbus A319112 · Fuselage Main, Attach Fittings > DURING C4/S1 CHECK, INSPECTION REPORTED ANGLE AT FR67 JUST BELOW L2 DOOR SILL WHICH ATTACHES DOOR SILL TO FRAME WAS FOUND DAMAGED. - [SDR F3LA200700141](https://openairdocs.org/sdr/F3LA200700141.md): Floorboard · delaminated · Jun 14, 2007 · N907FR · Airbus A319112 · Fuselage Floor Panel > DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBOARD 231EF DELAMINATED AROUND ONE OF THE FWD SCREW HOLES. REPAIRED DAMAGE TO TOP SKIN OF FLOORBOARD 231EF IAW EA NR A9-53R-11965. - [SDR F3LA200700133](https://openairdocs.org/sdr/F3LA200700133.md): Floor Panel · delaminated · Jun 14, 2007 · N907FR · Airbus A319112 · Fuselage Floor Panel > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221PF DELAMINATED NEAR THE LAV MOUNTS AND A PUNCTURE NEAR THE LAV DOOR AREA. REPAIRED DAMAGE TO THE TOP SKIN PANEL OF FLOOR PANEL 221PF IAW A319 SRM 53-02-00, PARA 8A, FIG 201 AND 202. DELAMINATION WAS DETE - [SDR F3LA200700132](https://openairdocs.org/sdr/F3LA200700132.md): Floorboard · punctured · Jun 13, 2007 · N907FR · Airbus A319112 · Fuselage Floor Panel > DURING C4/S1 CHECK, INSPECTION REPORTED PUNCTURE IN LT CORNER AREA OF FLOORBOARD 231MF. REPAIRED SMALL PUNCTURE TO THE TOP SKIN, FWD LT CORNER SURFACE OF FLOORBOARD PANEL 231MF IAW A319 SRM 53-02-00, PARA 8A, FIG 201 AND 202. - [SDR F3LA200700140](https://openairdocs.org/sdr/F3LA200700140.md): Floor Panel · corroded · Jun 10, 2007 · N907FR · Airbus A319112 · Fuselage Floor Panel > DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL 262FF AND R2 DOOR THRESHOLD IAW SRM 53-42-12, PB 401. - [SDR F3LA200700139](https://openairdocs.org/sdr/F3LA200700139.md): Girt Bar · corroded · Jun 10, 2007 · N907FR · Airbus A319112 · Escape Slide > DURING C4/S1 CHECK, INSPECTION REPORTED LIGHT CORROSION ON L2 DOOR GIRT BAR FITTING AFT OF C66, JUST FWD AND INBD OF SCREW HOLE. FOUND L2 DOOR SILL TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. REPLACED L2 DOOR SILL IAW SRM'S 51-42-11, 51-44-11, 51-41-11 AN - [SDR F3LA200700138](https://openairdocs.org/sdr/F3LA200700138.md): Nut Plate · corroded · Jun 10, 2007 · N907FR · Airbus A319112 · Escape Slide > DURING C4/S1 CHECK, INSPECTION REPORTED R1 GIRT BAR FITTING NUT PLATE ASSY CORRODED, FWD AND AFT. REPLACED FWD AND AFT GIRT BAR FITTINGS AND NUT PLATE ASSEMBLIES IAW SRM 51-42-11, PAGE 44, STEP 7D AND PARA 7. - [SDR F3LA200700131](https://openairdocs.org/sdr/F3LA200700131.md): Door Frame · corroded · Jun 10, 2007 · N907FR · Airbus A319112 · Fuselage Main, Structure > DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR FRAME 61 COVER SHEET FOR NUT PLATES CORRODED AROUND SEVERAL RIVET HEADS. REMOVED AND REPLACED WEB IAW A319 SRM 51-42-11 AND 51-44-21. - [SDR F3LA200700137](https://openairdocs.org/sdr/F3LA200700137.md): Floor Panel · corroded · Jun 9, 2007 · N907FR · Airbus A319112 · Fuselage Floor Panel > DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED AT FWD INBD CORNER ON UNDERSIDE OF PANEL. REPLACED FLOOR PANEL IAW AMM 53-32-12-400-002. - [SDR F3LA200700136](https://openairdocs.org/sdr/F3LA200700136.md): Dummy Rail · corroded · Jun 9, 2007 · N907FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4/S1 CHECK, INSPECTION REPORTED HEAVY CORROSION ON TOP FLANGE OF DUMMY RAIL AT Y81, BETWEEN FR12 AND FR14. REPLACED DUMMY RAIL IAW SRM 51-42-11, PARA. 8, AND SRM 51-41-11, PARA 3. - [SDR F3LA200700134](https://openairdocs.org/sdr/F3LA200700134.md): Floorbeam · corroded · Jun 9, 2007 · N907FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4/S1 CHECK, INSPECTION REPORTED TWO AREAS OF CORROSION ON FLOORBEAM +Y1292 AT FR68. REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND EA #A0-53T-11472. - [SDR F3LA200700135](https://openairdocs.org/sdr/F3LA200700135.md): Floorbeam · corroded · Jun 9, 2007 · N907FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4/S1 CHECK, INSPECTION REPORTED ONE AREA OF CORROSION ON FLOORBEAM +Y1292 AT FR67. REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11, AND EA #A0-53T-11472. - [SDR F3LA200600003](https://openairdocs.org/sdr/F3LA200600003.md): Floorbeam · corroded · Feb 14, 2006 · N907FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C3-CHECK, INSPECTION REPORTED GALLEY BEAM BETWEEN FR 66 AND FR 68, LBL Y1292, CORRODED. FOUND GALLEY BEAM TO BE OUT OF LIMITS. REPLACED FLOORBEAM PER SRM 51-42-11, 51-44-11 AND EA A9-53R-11257. - [SDR F3LA200600002](https://openairdocs.org/sdr/F3LA200600002.md): Shear Plate · corroded · Feb 14, 2006 · N907FR · Airbus A319112 · Fuselage Main, Structure > DURING C3-CHECK, INSPECTION REPORTED RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IN AFT GALLEY CORRODED. REPLACED RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IAW SRM 51-42-11. - [SDR F3LA200600001](https://openairdocs.org/sdr/F3LA200600001.md): Shear Plate · corroded · Feb 14, 2006 · N907FR · Airbus A319112 · Fuselage Main, Structure > DURING C3-CHECK, INSPECTION REPORTED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IN AFT GALLEY CORRODED. REPLACED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IN AFT GALLEY PER SRM 51-42-12. - [SDR F3LA200400101](https://openairdocs.org/sdr/F3LA200400101.md): Slide · out of adjust · Sep 26, 2004 · N907FR · Airbus A319112 · Escape Slide > BLOCK TURNBACK. FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT ARM. REMOVED, ADJUSTED AND REINSTALLED L1 DOOR SLIDE. OPS CHECK GOOD PER MM 25-62-44-000-062. - [SDR F3LA200300153](https://openairdocs.org/sdr/F3LA200300153.md): Control Unit · inoperative · Nov 14, 2003 · N907FR · Airbus A319111 · Landing Gear Retraction/Extension System > EN ROUTE TO DEN, ECAM STATUS SHOWED FOLLOWING MESSAGE: INOP SYS: ANTI SKID, N/W STRG/ BRK SYS 1, BRK SYS 2. N/W STEERING SWITCH WAS ON. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. AIRCRAFT HAD NO N/W SHEERING AND NO SYS ## 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 = 'N907FR' AND deregistration_id = 'N907FR-2009-07-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N907FR-2009-07-09/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.