# Service difficulty reports: N937FR, cancelled Dec 3, 2012 A list on [N937FR, cancelled Dec 3, 2012](https://openairdocs.org/deregistered/N937FR-2012-12-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2011032100617](https://openairdocs.org/sdr/F3LA2011032100617.md): Windshield · cracked · Mar 17, 2011 · N937FR · Airbus A319111 · Flight Compartment Windows > F/O WINDSHIELD CRACKED FOLLOWING ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O WINDSHIELD WITH SERVICEABLE WINSHIELD REF AMM 56-11-11-400-000-001. - [SDR F3LA2011031500614](https://openairdocs.org/sdr/F3LA2011031500614.md): Hinge Fitting · corroded · Mar 11, 2011 · N937FR · Airbus A319111 · Landing Gear Doors > A/C C-CHECK: NON ROUTINE; FWD AIRFRAME HINGE FITTING FOR LT MAIN GEAR DOOR, FWD LUG FACE OF FITTING, HAS WEAR.013" TO.018" DEEP. CAUSED BY BOLT ROTATING. SPOT FACED FWD LUG BOLT HOLE FACE AND INSTALLED BUSHING. MILLED BUSHING TO LUG THICKNESS. FABRICATE - [SDR F3LA2011031500613](https://openairdocs.org/sdr/F3LA2011031500613.md): Floorbeam · corroded · Mar 11, 2011 · N937FR · Airbus A319111 · Fuselage Main, Floor Beam > ACFT C-CHECK: NON ROUTINE NR 31644; MAIN CABIN FLOORBEAM HAS CORROSION 6" OF FR 66, Y 1732. CORROSION NOTED IS EXFOLIATION AND OUT OF LIMITS IAW SRM 53-41-14 P 103/104, R & R FLOORBEAM ASSY. - [SDR F3LA2011031500612](https://openairdocs.org/sdr/F3LA2011031500612.md): Sill · corroded · Mar 11, 2011 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > ACFT C-CHECK: NON ROUTINE; MAIN CABIN FLOOR SILL BEAM (L2 DOOR) CORRODED BEYOND LIMITS AT FR 66, Y 1732 IAW SRM 53-41-14, P 4.B, FIG. 101. BLENDED CORROSION TREATED AND PRIMED. INSTALLED REPAIR WITH FILLER AND 2 SPLICE ANGLES. SRM 53-41-14, 2(P) AND (Q). - [SDR F3LA2010090100500](https://openairdocs.org/sdr/F3LA2010090100500.md): Pitch Control · malfunctioned · Sep 16, 2010 · N937FR · Airbus A319111 · Autopilot System > PILOT REPORTED, ACFT PITCH WILL NOT STABLE WHILE HAND FLYING, UNCOMMANDED INCREASE IN PITCH UP. MX PERFORMED BITE TEST OF THE EFCS IAW AMM 27-96-00-740-001 WITH NO DEFECTS NOTED. PERFORMED OPS TEST OF THE AFS IAW AMM 22-96-00-710-001 WITH NO DEFECTS NOTED. - [SDR F3LA2010030700357](https://openairdocs.org/sdr/F3LA2010030700357.md): Servo · worn · Mar 4, 2010 · N937FR · Airbus A319111 · Elevator Control System > AIR TURN BACK DUE TO AIRFRAME VIBRATION ON CLIMB OUT. AIRSPEED 280 KIAS. ALTITUDE APPROX 17,000 FT. LOW FREQUENCY SIGNIFICANT AMPLITUDE INCREASING WITH FORE AND AFT MOVEMENT OF SIDE STICK. MX R & R LT ELEVATOR GREEN SYS SERVO AND RT ELEVATOR YELLOW SYS SERVO - [SDR F3LA2010021700344](https://openairdocs.org/sdr/F3LA2010021700344.md): Cylinder · low · Feb 15, 2010 · N937FR · Airbus A319111 · Crew Oxygen System > DURING CRUISE ALTITUDE THE FLIGHT CREW NOTED THE CREW OXYGEN LOW. MAINTENANCE SERVICED THE CREW OXYGEN AND RESET THE CREW OXYGEN MASKS IAW AMM 12-35-10 PB301, NO LEAKS NOTED. - [SDR F3LA2009082500140](https://openairdocs.org/sdr/F3LA2009082500140.md): Floor Support · corroded · Aug 21, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOORBEAM Y1292 AND FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 53-41-14, 51-42-11 AND DRAWING D53472780. - [SDR F3LA2009082500139](https://openairdocs.org/sdr/F3LA2009082500139.md): Shear Plate · corroded · Aug 21, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE LT SHEAR PLATE BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED THE LT SHEAR PLATE IAW SRM 52-41-11, 52-42-21 AND EA A0-53T-31040. - [SDR F3LA2009082500145](https://openairdocs.org/sdr/F3LA2009082500145.md): Shear Plate · corroded · Aug 18, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE RT SIDE LATERAL SHEAR PLATE WAS CORRODED AT FRAME 69 AND FRAME 70. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11 AND EA A0-53T-31040. - [SDR F3LA2009082500144](https://openairdocs.org/sdr/F3LA2009082500144.md): Floor Support · corroded · Aug 18, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE R2 DOOR LONGITUDINAL FLOORBEAM -Y1292 AFT OF FRAME 66 HAS CORROSION AROUND NUTPLATES. MAINT REMOVED CORROSION AND PERFORMED REPAIR IAW EA A9-53R-31267. - [SDR F3LA2009082500143](https://openairdocs.org/sdr/F3LA2009082500143.md): Floor Support · corroded · Aug 18, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE L2 DOOR LONGITUDINAL FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED CORROSION AND PERFORMED REPAIR IAW EA A9-53R-31266. - [SDR F3LA2009082500142](https://openairdocs.org/sdr/F3LA2009082500142.md): Sill · corroded · Aug 18, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE L2 DOOR SILL PLATE HAS CORROSION AT FRAME 68. MX REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EA A9-53R-31275. - [SDR F3LA2009082500141](https://openairdocs.org/sdr/F3LA2009082500141.md): Floor Support · corroded · Aug 18, 2009 · N937FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOOR SUPPORT Y1292 AFT OF FRAME 66 AND FWD OF FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11 AND DWG D53472780. - [SDR F3LA200800131](https://openairdocs.org/sdr/F3LA200800131.md): Floor Panel · damaged · Mar 19, 2008 · N937FR · Airbus A319111 · Fuselage Floor Panel > DURING C2 C CHECK, INSPECTION REPORTED A HOLE WAS PUNCTURED INTO THE UPPER SKIN OF AFT CARGO PIT FLOOR PANEL 151VG, NEAR THE FORWARD EDGE, IN THE CENTER. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14 PB 4 - [SDR F3LA200700385](https://openairdocs.org/sdr/F3LA200700385.md): Engine · failed · Dec 24, 2007 · N937FR · Airbus A319111 · Engine (Turbine/Turboprop) > FLIGHT CREW REPORTED INFLIGHT SHUTDOWN OF NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY/OIL PRESSURE. NR 1 ENGINE IS IN THE PROCESS OF BEING REPLACED. 1/7/008 FLT CREW REPORTED NT 1 ENGINE FAILURE IN FLT. SMELLED BURNING OIL, CLASS II ECAM ENGINE NR 1 OIL FILT - [SDR F3LA200500049](https://openairdocs.org/sdr/F3LA200500049.md): Actuator · tripped · Dec 21, 2005 · N937FR · Airbus A319111 · Leading Edge Slat Actuator > UPON APPROACH, FLIGHT CREW REPORTED ECAM F/CTL SLATS FAULT. PERFORMED TSM TASK 27-81-00-810-810. FOUND TORQUE LIMITERS POPPED ON SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM. REPLACED SLAT ROTARY ACTUATORS 6079 CM AND 6029 CM PER AMM 27-84-49-000-001 AND 27-84 ## 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 = 'N937FR' AND deregistration_id = 'N937FR-2012-12-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N937FR-2012-12-03/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.