N936FR, cancelled Nov 6, 2012

Service difficulty reports · 27

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

Query with SQL
duckdb -csv -c "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 = 'N936FR' AND deregistration_id = 'N936FR-2012-11-06'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR F3LA2011101800685Solenoid Valve · failedA/C PACK 2 FAILED IN FLIGHT. PACK 1 ON MEL SO PACK 2 FAIL CAUSED A CABIN DEPRESSURIZATION AND 02 MASK TO DEPLOY. R & R PRESSURE REGULATOR VALVE SOLENOID 10HA2 IAW AMM 36-11-55, PB 401. OP'S AND LEAK CHECKED GOOD.Oct 14, 2011 · N936FR · Airbus A319111 · Cabin Cooling SystemSDR F3LA2011032100616Servo · slowON ROTATION ACFT ROLLS RT REGARDLESS OF WIND. PERFORMED FLT CONTROL MOVEMENT CHECKS FOUNFD LT ELEVATOR SERVO SLOW TO REACT. REF LP 596444, ITEM 1, R & R SERVO CONTROL ELEVATOR LT GREEN HYD REF AMM 27-34-51-400-001 AND 27-34-51-0000.001, OPS CHECK NORMAL.Mar 16, 2011 · N936FR · Airbus A319111 · Elevator Control SystemSDR F3LA2011022100607Computer · malfunctionedAT LIFT OFF, AN UNCOMMANDED ACFT ROLLED RT. AT TOUCHDOWN, AT SPEEDBRAKE DEPLOYMENT, ACFT AGAIN ROLLED RT AND REQUIRED SIGNIFICANT LT AILERON INPUT TO KEEP LT MLG ON THE GROUND. REPLACED NR 1 SEC IAW AMM 27-94-34, PB 401. OPS CHECKED GOOD AND OPS CHECK FIGHTFeb 17, 2011 · N936FR · Airbus A319111 · Flight Management Computing Hardware SystemSDR F3LA2011011800585Sill · corrodedL2 DOOR SILL BEAM HAS 3 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R L2 DOOR SILL BEAM IAW SRM 51-72-11, PG 1-2.Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2011011800584Sill · corrodedR2 DOOR SILL BEAM HAS 1 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R R2 DOOR SILL BEAM IAW SRM 51-72-11 PG 1-2.Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2011011800583Shear Plate · corrodedLT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 3 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Main, StructureSDR F3LA2011011800582Shear Plate · corrodedRT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 8 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO53EO31434.Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Main, StructureSDR F3LA2011011800581Shock Absorber · scratchedLT MLG SHOCK ABSORBER SCRATCHED IN CHROME AREA. 60 TO 80 SCRATCHES 18 INCHES LONG X .003 INCHES DEEP ON FWD SIDE OF STRUT. R & R LT MLG SHOCK ABSORBER IAW AMM 32-11-13-020-058B AND 32-11-13-420-054B.Jan 7, 2011 · N936FR · Airbus A319111 · Main Landing Gear Strut/Axle/TruckSDR F3LA2011010600580Floor Panel · puncturedC-CHECK: NON ROUTINE N0665; AFT CARGO COMPARTMENT FLOOR PANEL 151AE HAS 3 EACH PUNCTURES. REPAIRED 3 EACH PUNCTURES WITH WET LAYUP IAW SRM 53-02-00, PARA 8B.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011010600579Floor Panel · puncturedC-CHECK: NON ROUTINE N0660; AFT CARGO COMPARTMENT FLOOR PANEL 151DE HAS 2 EA PUNCTURES. REPAIRED 2 EACH PUNCTURES IAW SRM 53-02-00, PARA 8B.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011010600578Floor Panel · puncturedC-CHECK: NON ROUTINE N0659; AFT CARGO COMPARTMENT FLOOR PANEL 152TG HAS 1 INCH PUNCTURE. REPAIRED PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011010600577Floorboard · puncturedC-CHECK: NON ROUTINE NR N0657; AFT CARGO COMPARTMENT FLOOR PANEL 162CF PUNCTURED. REPAIR PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011010600576Floor Panel · delaminatedC-CHECK: NON ROUTINE N0644; CABIN FLOOR PANEL 242BF DELAMINATED. REPAIRED 56 SQUARE INCHES OF DEBONDED TOP GLASS LAYER OF PANEL 242BF USING MYLAR FOIL IAW SRM 53-02-00, PARA 8J.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011010600575Skin · gougedC-CHECK: NON ROUTINE N0633; NR 2 ENGINE OTBD THRUST REVERSER LOWER BLOCKER INTERNAL SIDE THE PERFORATED SKIN HAS A GOUGE MEASURING .7500 INCH LONG, .2500 INCH WIDE AND .115 INCH DEEP. REPAIRED IAW CMM 78-32-36, REPAIR NR8.Jan 6, 2011 · N936FR · Airbus A319111 · Engine Thrust ReverserSDR F3LA2011010600574Cowl Door · dentedC-CHECK: NON ROUTINE NR N0636; NR 2 ENGINE OTBD THRUST REVERSERS INNER PERFORATED COWL BELOW THE UPPER BLOCKER DOOR THERE IS A DENT MEASURING .1250 INCH CIRCUMFERENCE AND .030 INCHES DEEP. REPAIRED 1 INCH DENT IAW CMM 78-32-36, REPAIR NR8.Jan 6, 2011 · N936FR · Airbus A319111 · Engine Thrust ReverserSDR F3LA2011010600573Floor Panel · damagedC-CHECK: NON ROUTINE NR N0282; AFT CARGO FLOOR PANEL 152WG DAMAGED, SKIN SEPARATED FROM HONEYCOMB. FABRICATED REPLACEMENT PANEL IAW IRM 9701, REV G.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2011010600572Floorboard · damagedC-CHECK: NON ROUTINE N0278; MAIN CABIN FLOORBOARD 252NF HAS COMPOSITE DAMAGE DAMAGE 40 SQUARE INCHES. REPAIRED 40 SQUARE OF COMPOSITE DAMAGE, IAW A319 SRM 53-02-00 PARAGRAPH 8J.Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2009071700106Floor Panel · crackedREF: NON ROUTINE C064113. DURING C3 C-CHECK, INSP NOTED THE L2 DOOR FWD SIDE FLOOR PANEL IS CRACKED. MX REMOVED AND REPLACED THE FWD L2 DOOR BLANKING PLATE IAW AMM 52-13-31-000-007 AND 52-13-31-400-007.Jul 14, 2009 · N936FR · Airbus A319111 · Fuselage Floor PanelSDR F3LA2009071700105Floorbeam · corrodedDURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 RT, BETWEEN FR 66 AND FR 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-72-11 AND EO A0-53T-11472.Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2009071700104Floorbeam · corrodedDURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 LT, BETWEEN FRAME 66 AND FRAME 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX REMOVED AND REPLACED THE FLOORBEAM IAW A319 SRM 51-42-11 AND DWG D53475815.Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2009071500103Shear Plate · corrodedDURING C3 C-CHECK, INSP NOTED THAT RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009071500100Support · corrodedDURING C3 C-CHECK, INSP NOTED THAT THE RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT, SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009071500102Shear Plate · corrodedDURING C3 C-CHECK, INSP NOTED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009071500101Support · corrodedDURING C3 C-CHECK, INSP NOTED THE LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW A319 SRM 51-42-11 PARAGRAPH 6 AND 7.Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2009072000107Strut · chafedDURING C3 C-CHECK, INSP NOTED THE ELECTRICAL CABLE FOR THE TOWING BYPASS SWITCH WAS RUBBING ON THE NLG STRUT. MX REMOVED DAMAGE, PERFORMED FLUORESCENT PENETRANT INSP AND ROTORY FLAP PEENED BLENDED AREAS IAW SRM 51-73-00 AND EA A9-32R-31199. (MAJOR REPAIR)Jul 11, 2009 · N936FR · Airbus A319111 · Nose/Tail Landing Gear Strut/AxleSDR F3LA200700046Light · inoperativeMAINTENANCE REPORTED RT AFT EMERGENCY OVERWING OUTSIDE LIGHT (62WL) INOP. REPLACED LIGHT ASSY (62WL) IAW 33-51-15-400-001.Mar 19, 2007 · N936FR · Airbus A319111 · Emergency LightingSDR F3LA200600086Light · failedEPSU TEST FAILED IAW HEAVY CHECK WORK CARD. REPLACED RT OVERWING EXIT HATCH HANDLE LIGHT IAW MM 23-73-47, PB 401 AND 33-51-11-420-052A, PERFORMED ANOTHER EPSU TEST AND CHECKED GOOD.Jul 29, 2006 · N936FR · Airbus A319111 · Emergency Lighting
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