N825AS, cancelled Mar 29, 2016

Service difficulty reports · 154

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 = 'N825AS' AND deregistration_id = 'N825AS-2016-03-29'
  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 ASOA2014090211175Door · lack of lubePASSENGER DOOR WOULD NOT OPEN. LUBED PASSENGER DOOR AND OPS CHECK IAW AMM 52-11-00.Aug 29, 2014 · N825AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014030610089Skin · crackedRT FUEL ACCESS PANEL HOLE 640EB HAS MULITPLE INDICATIONS ON THE AFT, INBD & OTBD SIDES 50 PERCENT FCH. FAILED NDT. REMOVED PANEL 640EB FOR INSPECTION IAW AMM 28-11-01-000-802. INSTALLED ACCESS PANEL 640EB IAW AMM 28-11-01-400-802. COMPLIED WITH EC/TC EO 60Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610088Skin · crackedLEFT FUEL ACCESS PANEL HOLE 540EB HAS MULTIPLE INDICATIONS ON INBD, OTBD, FWD & AFT SIDES 60 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610087Skin · crackedRIGHT FUEL ACCESS PANEL HOLE 650AB HAS MULTIPLE INDICATIONS ON THE FWD, INBD & OTBD SIDES 50 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV L.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610086Access Panel · crackedRIGHT FUEL ACCESS PANEL 640AB HAS MULTIPLE INDICATIONS ON THE AFT SIDE 80 PERCENT FCH. FAILED NDT. REMOVED PANEL 640AB FOR INSPECTION IAW AMM 25-11-01-000-802. INSTALLED PANEL 640AB IAW AMM 28-11-01-400-802.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610085Skin · corrodedRIGHT FUEL ACCESS PANEL HOLE 610AB HAS MULTIPLE INDICATIONS ON INBD 7 FWD SIDE 50 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610084Skin · crackedRIGHT FUEL ACCESS PANEL HOLE 650CB HAS MULTIPLE INDICATIONS, GROUND THE ENTIRE CIRCUMFERENCE 70 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610083Skin · crackedLT FUEL ACCESS PANEL HOLE 550CB HAS MULTIPLE INDICATIONS ON INBD 78 FWD SIDE 5 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610082Skin · crackedRT FUEL ACCESS PANEL HOLE 650DB HAS MULTIPLE INDICATIONS ON THE OTBD SIDE 70 PERCENT FCH. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Feb 20, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610081Strap · corrodedPASSENGER DOOR CUTOUT AT FS 349 BETWEEN STRINGERS 3-4L, THE UPPER INNER FRAME STRAP IS CORRODED. FABBED FRAME STRAP IAW EO DWG SNIEO 600-31153 FROM 7075-T6 PO 74097/1. C/W EO 600-31153 SNIEO S01. REMOVED FRAME STRAP AND REPLACED WITH NEW FRAME STRAP, PN 6Feb 19, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030610080Skin · crackedRT WING ACCESS PANEL HOLE 640CB HAS MULTIPLE INDICATIONS ON THE RT SIDE 50 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV L.Feb 19, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610079Skin · crackedRIGHT WING ACCESS PANEL HOLE 640FB HAS MULTIPLE INDICATIONS ON THE INBD SIDE 60 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO600-57-81. C/W IAW REO:601R-57-21-030.Feb 19, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610078Skin · crackedLT WING ACCESS PANEL HOLE 540FB HAS MULTIPLE INDICATIONS ON THE OTBD SIDE 50 PERCENT FSH FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV L.Feb 19, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030610077Angle · crackedLBL 27, BS 484 INBD ANGLE IS CRACKED. R & R IAW SRM 51-42-21 AND SRM 51-42-06.Feb 14, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030610076Angle · crackedRBL 27, BS 484 ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.Feb 14, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030510071Angle · crackedRBL 36, BS 484.00, ANGLE CRACKED. R & R ANGLE IAW REO 601R-53-41-059 AND REO 601R-53-41-059, REV B.Feb 14, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030510070Skin · crackedRIGHT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZ LANDING, 50 PERCENT FSH FAILED NDT. COMPLIED WITH REO: 601R-57-21-2124.Feb 14, 2014 · N825AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014030510069Floor Panel · corrodedTWO AREAS ON LT FLOOR PANEL ARE BEYOND MAXIMUM BLEND DEPTH LIMITS OF REO 601R-53-41-666, SUBSECTION 1.1 AND TABLE 1, REV.C 2012-11-06. C/W REO 601R-53-41-1777 FOR REPAIR OF DAMAGE TO LT PRESSURE FLOOR PANELFeb 12, 2014 · N825AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2014030510068Post · crackedFOUND FS 409.00+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS APPROX .300" LONG 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED, DRILLED, LOCATED AND REPLACED FS 409+128, RBL 18, POST ASSY IAW SRM 51-42-06, 51-42-22, REO 601R-Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030510067Isolator · crackedFOUND REAR PRESSURE BULKHEAD ISOLATORS CRACKED AT LBL 27.50 AND LBL 9.50, WL 98. REMOVED UNSERVICEABLE ISOLATOR MOUNTS IAW SRM 51-42-13. INSTALLED 2 EA NEW ISOLATORS PN SL2337-3 IAW SRM 51-42-13.Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014030510066Angle · crackedCARGO DOOR SUPPORT BEAM LOWER AFT ANGLE CRACKED APPROX 0.3" WIDE. R & R ANGLE ON CARGO DOOR SUPPORT BEAM IAW SRM 51-42-21.Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030510065Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 0, WL 91-48 APPROX 7 INCHES, AREA 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06. COMPLIED WITH REO:601R-53-61-1285, REV D.Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014030510064Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 79.0 APPROX .6 INCHES IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-5186, REV.Feb 11, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014030510063Stringer · crackedSTRINGER 3L CRACKED APPROX 0.70" LONG AT BS 280.8. REPAIRED IAW SRM 51-42-06. REPAIRED IAW SNIEO 601R-31522.Feb 10, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2014030510062Finger Doubler · corrodedFINGER DOUBLERS CORRODED IN MULTIPLE AREAS FS 409+128 - 559. COMPLIED WITH EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C. REPAIRED IAW REO 601R-53-5186, REV.Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014030510061Skin · corrodedSKIN & FINGER DOUBLERS HAVE CORROSION IN MULTIPLE AREAS BS 409+128-559. COMPLIED WITH EC/TC REO 601R-53-41-66601 AND REO 601R-53-41-666, REV C.Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014030510060Cargo Track · corrodedCARGO TRACK RBL 9 BS 559+80-574 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AMM 53-01-11-400-802 AND REO 601R-53-00-485, REV.Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014030510059Cargo Track · corrodedCARGO TRACK LBL 9, BS 559+80-621 CORRODED. R & R CARGO TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802 AND REO NR 601R-53-00-485, REV.Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014030510058Floor Support · corrodedFLOOR SUPPORT AT LBL 27, BS 574-621 CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-21, 51-42-20 & 51-42-06. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778, REV A.Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014030510057Floor Support · corrodedFLOOR SUPPORT AT RBL 45 IS CORRODED FROM BS 559+80 - 574. REPAIRED IAW SRM 51-42-06 & 51-42-21 AND IAW REO 601R-53-00-526.Feb 8, 2014 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013121309645Light · missingSHORT PORTION OF EMERGENCY LIGHT AT 18B MISSING. SECURED EMERGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.Dec 10, 2013 · N825AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201095Connector · looseCLIMBING THROUGH FL 220, RECEIVED RT ENGINE OIL PRESSURE WARNING WITH OIL PRESSURE AT 15 PSI. OIL TEMPERATURE WAS NORMAL OIL PRESS READ NORMAL AFTER DESCENT. (ACFT RETURNED TO CAE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FOUND RT ENGINE OIL TEMPERATMar 29, 2012 · N825AS · Cndair CL6002B19 · Engine Oil System WiringSDR ASOA201201078Scavenge Pump · failedRIGHT ENGINE OIL PRESSURE MASTER CAUTION AT 18000 FT. EMERGENCY DECLARED. R & R RT LUBE AND SCAVENGE PUMP IAW AMM 79-21-01. LEAK AND OPS CHECKED GOOD.Mar 29, 2012 · N825AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA201200502Floor Support · corrodedSERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW AMM 20-21-00-910-001 AND 20-24-00-910-802.Feb 15, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201200436Angle · crackedNLG CUTOUT CORNERS CRACKED AFT OF FOLLOW -UP DOOR HINGES (RADIUS). REPAIRED IAW REO 601R-53-11-0048 IAW 601R-53-11-0048, REV C.Feb 8, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201200546Angle · corrodedSERVICE DOOR SILL FWD UPPER ANGLE CORRODED. R & R CORRODED ANGLE IAW DWG NR 601R38303.Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201200412Seat Track · corrodedSEAT TRACK FS 394 TO 409+128 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200410Seat Track · corrodedSEAT TRACK FS 409+128 TO 559.0 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 51-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-807 AND AMM 53-01-11-400-802.Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200408Attach Angle · crackedATTACH ANGLE CRACKED AFT EQUIPMENT BAY RT SIDE AT PRESSURE BULKHEAD ABOUT 12 INCHES BELOW ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201200406Attach Angle · crackedATTACH FITTING CRACKED AFT EQUIPMENT BAY LT SIDE AT PRESSURE BULKHEAD ABOVE ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. LOCATED SERVICEABLE ATTACH ANGLE IAW STM 51-40-11. INSTALLED ATTACH ANGLE IAW SRM 57-42-22.Feb 6, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201200398Seat Track · corrodedSEAT TRACK FS 364 TO 396 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM TASK 53-01-11-400-802.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200396Seat Track · corrodedSEAT TRACK FS 364-396 AT LBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-420-001.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200394Support Angle · corrodedSERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-26-00. .031" OF MATERIAL REMOVED- .026" MATERIAL REMAINING. REMOVED SILL SUPPORT ANGLE IAW SRM'S 51-42-06, 51-42-21, AND 51-42-13. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND 51-42-Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201200392Floorbeam · corrodedFLOORBEAM FS 280 HAS CORROSION DAMAGE. REMOVED CORROSION IAW SRM 51-21-06. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06. DRILLED NEW ANGLE IAW SRM 51-40-11.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201200390Floorbeam · corrodedCORROSION AROUND NUTPLATE ON FS 280.00 FLOORBEAM. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PRODCEDURES UT-3. MIN MATERIAL REMAINING IS .035".Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201200388Seat Track · corrodedSHORT SEAT TRACK BETWEEN FLOOR PANELS 281BLF AND 281FRF HAS CORROSION. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200386Seat Track · corrodedSHORT SEAT TRACK HAS CORROSION AT LBL9 BETWEEN FLOOR PANEL 281HLF AND 281BLF. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-40-802.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200384Seat Track · corrodedSEAT TRACK HAS CORROSION AT RBL 9 AT 9G BULKHEAD. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201200382Attach Fitting · crackedRIGHT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT RBL 27.0. REMOVED DAMAGED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM AND DWG NR 601R31171.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201200380Attach Fitting · crackedLEFT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT LBL 27.0. REMOVED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-42-21.Feb 3, 2012 · N825AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
Back to N825AS, cancelled Mar 29, 2016