N930FR, cancelled May 28, 2013
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 = 'N930FR' AND deregistration_id = 'N930FR-2013-05-28' 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.
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 = 'N930FR' AND deregistration_id = 'N930FR-2013-05-28' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR F3LA2012041900746Transducer · defectiveELAC 2 FAULT (UNCOMMANDED PITCH +/··150'). TROUBLESHOT IAW TM 27-93-Q0-810-808-A, R & R F/O SIDE STICK TRANSDUCER (4E4) REF AMM 27-92-41-Q00-002-A AND 27-92-41-40O-Q02-A. OPS CHECKED GOOD, REF AMM27-92-41-710-001-A.SDR F3LA2011090800668O-Ring · deterioratedHYD Y RESERVOIR LOW LEVEL DURING FLIGHT. SUBSEQUENT Y SYS FAILURE INDICATIONS. REMOVED AND INSTALLED SERVICEABLE O-RING ON REDUCER ON PTU MANIFOLD. PERFORMED OPS CK AND LEAK CK. NO FAULTS OR LEAKS NOTED. REF AMM 29-13-15 PB 401, PG 5, STEP 4 A (2) (E) AND (F).SDR F3LA2010041500390Wire Harness · brokenREFERENCE C CHECK NON ROUTINE N0636. EMERGENCY LIGHTS AT SEAT 20C AND RIGHT AFT DOOR DO NOT ILLUMINATE. REMOVED AND REPLACED WIRING HARNESS 860W AT SEAT 20C IAW AIRBUS A319 AMM 33-51-08. RESEATED PIN 3 OF EXIT LIGHT ASSEMBLY ON RIGHT AFT DOOR 32WL IAW AIRBUSDR F3LA2010041400382Leg Assy · corrodedREF C-CHECK NON ROUTINE N0565. AFTER REMOVAL OF RT MLG SLIDING TUBE FOUND CORROSION ON INNER BORE AT LOWER BRG AREA. REPAIRED CORRODED AREA IAW EA A9-32R-31730.SDR F3LA2010041500389Frame · corrodedREFERENCE C CHECK NON ROUTINE N0307. AFT CARGO COMPARTMENT FRAME 59 TWELVE INCHES RIGHT OF CENTERLINE PROFILE TOP SURFACE CORRODED. REMOVED AND REPLACED PROFILE IAW AIRBUS A319 SRM 51-40-00.SDR F3LA2010041500388Plate · corrodedREFERENCE C CHECK NON ROUTINE N0291. FORWARD CARGO COMPARTMENT TRANSITION PLATE BETWEEN FRAME 28 RIGHT AND FRAME 30 RIGHT CORRODED. REMOVED AND REPLACED PLATE IAW AIRBUS A319 SRM 51-72-11.SDR F3LA2010041500387Plate · corrodedREFERENCE C CHECK NON ROUTINE N0289. FORWARD CARGO COMPARTMENT TRANSITION PLATE AT STRINGER 38 LEFT BETWEEN FRAME 28 AND FRAME 30 IS CORRODED. REMOVED AND REPLACED PLATE IAW AIRBUS A319 SRM 51-72-11.SDR F3LA2010041500385Blanking Plate · corrodedREFERENCE C CHECK NON ROUTINE N0290. FORWARD CARGO COMPARTMENT AFT BULKHEAD PLATE BETWEEN FRAME 28 AND FRAME 29 CORRODED. REMOVED AND REPLACED BULKHEAD PLATE IAW AIRBUS A319 SRM 51-40-12.SDR F3LA2010041500384Floor Panel · debondedREFERENCE C CHECK NON ROUTINE N0295. AFT CARGO FLOOR PANEL 151ZG DISBONDED. REPAIRED DISBONDED AREA IAW AIRBUS A319 SRM 53-02-00.SDR F3LA2010041400383Floor Panel · debondedREF C-CHECK NON ROUTINE N0135. MAIN CABIN FLOOR PANEL 252 NF DISBONDED. REPAIRED DISBONDED AREA IAW SRM 53-02-00.SDR F3LA2010041400381Floor Panel · delaminatedREF C-CHECK NON ROUTINE N0136. MAIN CABIN FLOOR PANEL 252 HG DISBONDED. REPAIRED FLOOR PANEL IAW SRM 53-02-00.SDR F3LA2009060100088Windshield · crackedPILOT REPORTED THAT THE CAPTAIN'S FORWARD WINDSCREEN CRACKED DURING CLIMB THROUGH FL210. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD, REFERENCE AMM 56-11-11-000-001 AND 56-11-11-400-001.SDR F3LA2009040800074Windshield · crackedDURING CRUISE FLIGHT, PILOT REPORTED THE RT WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD, REFERENCE AMM 56-11-11 PB 401.SDR F3LA2009033000069Light · inoperativeREFERENCE LOG PAGE 371414. MAINTENANCE NOTED THAT THE EMERGENCY LIGHT AT ROW 11 ABC WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AND PERFORMED OPERATIONAL CHECK IAW AMM 33-51-19 PB 401.SDR F3LA200800611Floor Panel · damagedREFERENCE NON ROUTINE CO51333. DURING C3 C CHECK, INSPECTION NOTED FLOOR PANEL 261EF HAD DAMAGED AREA AROUND INSERT ON OTBD EDGE. MX REMOVED FLOOR PANEL AND REPLACED WITH NEW IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPON COMPLETION SDR F3LA200800612Scuff Plate · corrodedREFERENCE NON ROUTINE C051324. DURING C3 C CHECK, INSPECTION NOTED THE L2 DOOR AFT OTBD SCUFF PLATE SUPPORT ATTACHMENT HAD A CORRODED FASTENER. MX REMOVED CORNER ANGLE, OVERSIZED 3 HOLES, FABRICATED 3 FREEZE PLUGS, INSTALLED CORNER ANGLE AND NEW SCUFF PLATE SDR F3LA200800615Sill · corrodedREFERENCE NON ROUTINE CO51321. DURING C3 C CHECK INSPECTION NOTED THE L2 DOOR SILL AFT OTBD NUT PLATE HOLE WAS CORRODED. MX CUT CORRODED AREA OUT OF THE SILL WEB, FABRICATED REPAIR FILLER AND INSTALLED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 5SDR F3LA200800614Floorbeam · corrodedDURING C3 C-CHECK INSPECTION NOTED FLOORBEAMS INBOARD OF THE L2 DOOR SILL CORRODED AND CORROSION IN ALL NUT PLATE HOLES. MX REMOVED FLOORBEAMS, REMOVED BARREL NUT FITTING AND SPLICE, DRILLED HOLES IN SERVICEABLE BEAM, INSTALLED BARREL NUT FITTING AND SPLICE ASDR F3LA200800613Sill · corrodedDURING C3 C-CHECK, INSPECTION NOTED THE L2 FORWARD GIRT BAR ATTACH FITTING, AFT INBOARD HOLE HAD CORROSION. MX CUT CORRODED AREA OUT OF THE SILL WEB, FABRICATED REPAIR FILLER AND INSTALLED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-41-14, 51-75SDR F3LA200800609Floorbeam · corrodedDURING C3 C-CHECK, INSPECTION NOTED THE FLOORBEAM IB OF THE R2 DOOR SILL HAS CORROSION IN ALL NUT PLATE HOLES. MAINT REMOVED AND REPLACED FLOORBEAM. Y1292 IAW THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ASDR F3LA200800610Shear Plate · corrodedREFERENCE NOT ROUTINE C051378. DURING C3 C-CHECK, INSP NOTED THE RT SHEAR PLATE FROM FR 69 TO FRAME 70 WAS CORRODED. MAINT REMOVED AND REPLACED SHEAR PLATE ASSY AND SUPPORT FRAME IAW THE REQUIREMENTS OF A319, SRM 51-42-11, PARA 6 AND 7. UPON COMPLETION OF THSDR F3LA200800606Panel · puncturedREFERENCE NON-ROUTINE C050859. DURING C3 C-CHECK. INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR. IT WAS INSPECTEDSDR F3LA200800607Panel · puncturedREFERENCE NON-ROUTINE C050860. DURING C3-C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED ASDR F3LA200800608Panel · puncturedREF NON-ROUTINE C050863. DURING C3-C-CHECK. INSP NOTED THE AFT PIT TRANSITION PANEL 151TG WAS DAMAGED. MAINT REPAIRED DAMAGED FLOOR PANEL IAW WITH THE REQUIREMENTS OF SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR. IT WAS INSPECTED AND FOUND ACCEPTABSDR F3LA200800618Floor Panel · corrodedREFERENCE NON ROUTINE CO51286. DURING C3 C CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAD CORROSION ON AFT BOTTOM SURFACE. MX REMOVED FLOOR PANEL AND INSTALLED NEW IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAISDR F3LA200800617Floor Panel · corrodedREFERENCE NON ROUTINE CO51223. DURING C3 C CHECK INSPECTION NOTED FLOOR PANEL 261FF HAD CORROSION ON UPPER AND LOWER SURFACES. MX REMOVED FLOOR PANEL AND INSTALLED NEW IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPON COMPLETION OF THE SDR F3LA200700039Stringer · corrodedDURING C-2 CHECK INSPECTION, REPORTED FWD CARGO COMPARTMENT STRINGER 42R AT THE AFT END OF ZONE 131, INBD OF CARGO DOOR FROM F24 TO F28, HAD EXFOLIATION/CORROSION AROUND RIVETS. REMOVED CORRODED RIVETS IAW SRM 51-42-11. PERFORMED HFEC INSPECTION OF HOLES IAW
Back to N930FR, cancelled May 28, 2013