N832AS, cancelled Jan 7, 2016

Service difficulty reports · 143

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 = 'N832AS' AND deregistration_id = 'N832AS-2016-01-07'
  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 ASOA2014051410492Sign · brokenEXIT SIGN IN GALLEY AREA FELL OFF AND IS BROKEN, LIGHT LENS COVERS, INCLUDING EMERGENCY LIGHT. REPLACED THE GALLEY EXIT SIGN IAW AMM 33-51-13, OPS CHECKED GOOD.May 10, 2014 · N832AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013122709698Sensor · failedGEAR DISAGREE MESSAGE DURING SELECTION OF GEAR UP. COMPLETED WITH QRH, MANUALLY EXTENDED GEAR. NOSE GEAR DID NOT SHOW UP AND LOCKED DURING THE GEAR DISAGREE. ALL GEAR SHOWED DOWN AND LOCKED AFTER MANUEL EXTENSION TO LANDING. RETURNED TO DEPARTURE, R & RDec 24, 2013 · N832AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA2013102309245Bulkhead · crackedBS 202 BULKHEAD IS CRACKED. CUT OUT AND REMOVED ALL CRACKS FROM 202 BULKHEAD AND REMOVED ALL BURRS IAW STEP 1 AND STEP 2 OF REO 601R-53-11-563, REV C. FABRICATED AND DRILLED TO FULL SIZE ALL REPAIR PARTS IAW REO 601R-53-11-563, REV C FAY SEALED ALL REPAIR PAOct 20, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013082808913Heat Exchanger · dentedCLIMBING THROUGHT FL210, ALL AIRFLOW FROM GASPERS STOPPED CABIN STARTED TO SLOWLY CLIMB. WE STARTED A EMERGENCY DESCENT AND RETURN TO DEPARTURE. REPEAT WRITE UP. ACFT RETURNED TO DEPARTURE AFTER T/O. R & R HEAT EXCHANGER IAW AMM 21-51-07, ITEM 45B (21-51-0Aug 26, 2013 · N832AS · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA2013080808850Light · inoperativeRT LOWER EMERGENCY EXIT LIGHT AT EMERGENCY EXIT IS INOPERATIVE. R & R RT LOWER EMERGENCY EXIT LIGHT AT OVERWING EMERGENCY EXIT IAW AMM 33-51-10-400-801. OPS CHECKED GOOD.Aug 5, 2013 · N832AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013080608836Access Panel · crackedCRACK INDICATION NOTED POSSIBLY CORROSION ON THE LT WING LOWER PLANK ACCESS HOLE LANDING FOR PANEL 550FB, 65 PERCENT FULL SCREEN HEIGHT FAILING NDT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J.Jul 19, 2013 · N832AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013080508827Skin · corrodedUPPER FUSELAGE ADF ANTENNA CUTOUT HAS FRETTING DAMAGE AROUND CIRCUMFERENCE AND SCREW HOLES APPROX 6" L X .125 W X .005 AT WORST LOCATION. REPAIRED IAW BSC EO CL600-2B19-53-I00360, REV A.Jul 17, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2013080908851Bulkhead · crackedFS 621 BULKHEAD, LBL 27.50 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BETWEEN WL 104 AND 110. REPAIRED IAW REO 601R-53-61-1285, REV D DATED 10/31/2011.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013080808849Bulkhead · chafedFS 621 BULKHEAD HAS SIX CHAFED AREAS AT WL 102: LBL 27.5-RBL 36.20. REPAIRED IAW REO 601R-53-61-2155.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013080808848Floor Support · corrodedCARGO COMPARTMENT RT FLOOR SUPPORT HAS MINOR CORROSION AROUND FASTENER HOLES FROM FS 559+80 TO 559+112. COMPLIED WITH REO 601R-53-00-526. REMOVED FLOOR SUPPORT IAW SRM 200 51-41-00-00 AND 51-42-06-00. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPORT IAW SRM Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013072508776Bulkhead · crackedFS 621, BULKHEAD RBL 27.50 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT AT WL 109 AND 110. REPAIRED IAW REO 601R-53-61-1285, REV D, DATED 10/31/2011.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013072508775Bulkhead · crackedFS 621 BULKHEAD FAILS NDT RBL 18 WITH INDICATION 50 PERCENT SCREEN HEIGHT WL 123 AND 124. REPAIRED IAW REO 601R-53-61-1285, REV D, DATED 10/31/2011.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013072508774Bulkhead · crackedFS 621 BULKHEAD FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BL 0 BETWEEN WL 109 AND 111. REPAIRED IAW SRM 51-41-04 AND REO 601R-53-61-1285, REV D, DATED 10/31/2011.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013072508773Bulkhead · crackedFS 621 BULKHEAD, LBL 18 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BETWEEN WL 117.5 AND 118.5. REPAIRED IAW SRM 51-42-06, 51-41-04 AND REO 601R-53-61-1285, REV D DATED 10/31/2011.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013072508772Bulkhead · crackedFS 621 BULKHEAD LBL 27.50 FAILS NDT WITH INDICATION FULL SCREEN HEIGHT AT UPPER CARGO TRACK WL 131. REPAIRED IAW SRM 51-42-06 AND REO 601R-53-61-1541, REV D DATED 10/31/2011.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013072308750Angle · crackedFS 280, LBL 9.0 INBD SUPPORT ANGLE CRACKED. REPAIRED IAW SRM 51-42-21, 51-20-06, REO 601R-53-11-726 AND REO 601R-53-11-926.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013072308749Support Angle · crackedFS 621 CARGO DOOR BEAM BOTTOM SUPPORT ANGLE IS CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE BRACKET ANGLE IAW SRM 51-42-21.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013071808724Lens · crackedEMERGENCY LIGHT COVER CRACKED. REMOVED AND INSTALLED NEW EMERGENCY LIGHT COVER IAW MM 41-10, 33-60-13.Jul 16, 2013 · N832AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013020702970Lamp · burned outRT EXTERIOR AFT EMERGENCY LIGHT INOP. REPLACED LAMP IAW AMM 33-51-21, OPS CHECK GOOD.Feb 4, 2013 · N832AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012082402095Fan · failedDISPLAY COOL CAUTION MESSAGE IN FLIGHT. FOLLOWED QRH. WHEN SWITCHING FROM NORMAL TO FLIGHT ALTERNATE SMELLED ELECTRICAL BURNING ODOR FOR 10 SECONDS. RECEIVED ODOR TWICE MORE FOR SHORT DURATION OF TIME (DISPLAY COOLING FANS) R & R DISPLAY FAN IAW AMM 21-24-1Aug 20, 2012 · N832AS · Cndair CL6002B19 · Air Distribution FanSDR ASOA2012072001948Door · bindingAIRSTAIR DOOR REQUIRES EXCESSIVE FORCE TO OPEN, DOOR STICKS IN CLOSED POSITION. PERFORMED OPS CHECK ON AIRSTAIR DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. SDR CLOSED.Jul 17, 2012 · N832AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012071101885Bracket · unserviceableGEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH 14,000 FT. COMPLETED QRH PROCEDURE. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED NORMALLY. R & R NLG WOW AND CENTERING SENSOR HARNESS BRACKET IAW AMM 32-61-25. ADJUSTED IAW AMM 32-61-05. PERFORMED GJul 5, 2012 · N832AS · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR ASOA201201633Hydraulic Line · disconnectedON LANDING, LOST BRAKING, ALL TIRES BLOWN EXCEPT LEFT OTBD. R & R ALL MLG TIRES IAW AMM 32-41-01. FOUND HYD QUICK DISCONETION LINE LOOSE. RESECURED LINE IAW AMM 32-43-26.May 10, 2012 · N832AS · Cndair CL6002B19 · Landing Gear Brake SystemSDR ASOA201200803Unknown · multiple failSTARTED APU AT 10K AFTER A COUPLE OF MINUTES, TRANSFERED THE BLEEDS TO APU. RECEIVED AN APU OVERTEMP FOLLOWED BY APU FIRE, FOLLOWED BY APU FIRE FAIL, RAN 1A1 CORD AND BLEW BOTTLE THEN RECEIVED APU FIRE EXTINGUISHING SYS FAULT. EMERGENCY DECLARED. R & R APU Mar 7, 2012 · N832AS · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR ASOA201101954Step · crackedPAX DOOR LOWER STEP IS CRACKED. R & R LOWER PAX DOOR STEP IAW AMM 52-11-04. OP'S CHECKED GOOD.Oct 12, 2011 · N832AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101549Handle · bindingF/A REPORTS PAX DOOR IS HARD TO OPEN DUE TO LATCH STICKING. CYCLED PAX DOOR SEVERAL TIMES NO DEFECTS NOTED AT THIS TIME OPS CHECKED GOOD IAW AMM 52-11-01. OK FOR SERVICE.Aug 21, 2011 · N832AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101537Sign · brokenEMERGENCY EXIT SIGN ON MAIN CABIN DOOR BULKHEAD IS BROKEN. R & R EXIT SIGN IAW AMM 33-51-01. OPS CHECKED GOOD.Aug 19, 2011 · N832AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101470Door · bindingMAIN PAX WOULD NOT UNLATCH/OPEN. PERFORMED OPS TEST OF PASSENGER DOOR. DOOR OPS CHECKED GOOD IAW AMM 52-11-05. NO DISCREPANCIES NOTED. ACFT OK FOR SERVICE.Aug 6, 2011 · N832AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101407Floorbeam · corrodedFS 349, SERVICE DOOR FLOOR SUPPORT CORRODED. COMPLY WITH STEPS 3 AND 4 OF REO 601R-53-21-1321. COMPLIED WITH STEP 3 OF REO 601R-53-21-1321. COMPLY WITH STEP 4 OF REO 601R-53-21-1321. COMPLIED WITH STEP 4 OF REO 601R-53-21-1321. COMPLY WITH EC/TC REO. COMPJul 29, 2011 · N832AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101393Floor Support · corrodedPAX DOOR FLOOR SUPPORT ANGLE JUST ABOVE SILL CORRODED. FORMED AND BENT PAX DOOR FLOOR SUPPORT ANGLE IAW SRM 51-24-21 AND DWG 601R31527. HEAT TREATED FORMED REPAIR PART FROM O TO T62 IAW SRM 51-24-06. TRIMMED AND FITTED FABRICATED PART TO ACFT BBD DWG 601RJul 28, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101389Floor Support · corrodedSERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE ABOVE SILL AT FS 349 CORRODED. REPAIRED IAW SRM 51-41-02.Jul 27, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101332Frame · corrodedCORROSION FOUND AT FS 349 FRAME ON FRONT AND AFT FACE AT S27L. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 51-21-06.Jul 14, 2011 · N832AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201101376Door · out of adjustEMERGENCY EXIT DOOR, LT, IS BINDING WHEN OPENING. CHECK DOOR FOR PROPER OPERATION, ADJUST AS REQ. CHECK DOOR FOR PROPER OPERATION, ADJUST AS REQ. FOUND RESISTANCE IN THE HANDLE MECANISIM WAS EXCESSIVE ADJUSTED OVER-WING EXIT IAW AMM 52-21-00-820-801, & PERFOJul 11, 2011 · N832AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201101288Floor Support · corrodedCORROSION FOUND ON LBL 27 FS 568-621 FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-20. ITEM 2. FOUND OUT OF LIMITS. INSTALLED FLOOR SUPPORT NEW IAW REO 601R-53-61-378-78.Jul 6, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101286Floorbeam · crackedFS 484 OTBD, RBL27 FLOOR SUPPORT ANGLE CRACKED PREVIOUS REPAIRED ANGLE MK7236. R & R FLOOR SUPPORT ANGLE IAW SRM 51-40-11, 51-42-21. THIS IS A MINOR REPAIR.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101285Floorbeam · corrodedFLOOR SUPPORT AT FS 349.00 LT SIDE UNDER PANEL 231CLF CORRODED. CLEAN CORROSION IAW 51-21-06 AND VERIFY LIMITS. REMOVED CORROSION FROM FS 349 CROSSBEAM AT LBL 40, WL 73, TOP FLANGE IAW SRM 51-21-06. REPAIR DIMENSIONS: 1"X 1.5" X .003" DEEP ORIGINAL THICKNESJul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101284Floor Support · corrodedFS 295 OTBD OF LBL 27 FLOOR SUPPORT BOX CORRODED. REMOVED CORROSION IAW SRM 51-21-06. REMOVED DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101283Web · crackedFS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION IAW NDT INSPECTION PROCEDURES ET-2. ANGLE VERIFIED AS CRACKED. CUT OUT DAMAGED AREA, NDT CUTOUT AREA IAW NDTM 51-20-06. NO CRACK NOTED. REPAIRED IAW REO 601R-53-11-926.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101282Web · crackedFS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION OF WEB IAW NDT INSPECTION PROCEDURE ET-2. WEB IS VERIFIED AS CRACKED. WEB REPAIRED IAW REO 601R-53-11-926.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101281Structure · crackedFS 280, LBL 9 INBD CLIP CRACKED. REMOVED DAMAGED CLIP, LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-11, 51-42-20. PERFORMED NDI IAW REO 601R-53-11-926, NO INDICATIONS NOTED. INSTALLED NEW CLIP IAW REO 601R-53-11-926.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101280Structure · crackedFS 280, RBL 9 INBD CLIP CRACKED. REMOVED CRACKED CLIP IAW SRM 51-42-20. FABRICATED NEW CLIP IAW REO 601R-53-11-926 NOTE 20. INSTALLED NEW CLIP IAW REO 601R-53-11-926, ECTC REO 601R-53-11-926. PERFORMED NDI IAW REO 601R-53-11-926, NO INDICATIONS NOTED.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101279Structure · crackedFS 280, RBL 9 OTBD CLIP CRACKED. REMOVED DAMAGED CLIP IAW SRM 51-42-20. FABRICATED NEW CLIP IAW REO 601R-53-11-926 NOTE 20 IAW EC/TC 601R-53-11-926. PERFORMED NDT IAW REO 601R-53-11-926 NOTE 20, NO INDICATIONS NOTED. INSTALLED NEW CLIP IAW REO 601R-53-11-926Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101278Angle · corrodedFS 280 FWD J-ANGLE CORRODED IN FLIGHT DECK DOORWAY. REMOVED J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED FASTENER HOLES IN NEW J-ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 AND 51-42-21. MINOR REPAIR.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101277Angle · crackedFS 280 LT ANGLE CRACKED OTBD OF RBL 27. VERIFY POSSIBLE CRACK (NDT) AND LENGTH. PERFORMED RT INSP IAW MAC NDT INSPECTED PROCEDURE ET-2 NO INDICATIONS NOTED AT THIS TIME.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101276Floor Support · corrodedFLOOR SUPPORT FITTING AT FS 310 BY SERVICE DOOR CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-20. DRILLED & REAMED NEW FLOOR SUPPORT IAW REO 601R-53-21-1332 & ALODINED HOLES & TOP COATED BARE METAL ON ALL ATTACH PARTS IAW CRM 51-21-11 FOR CODING 51-25-01-31-2Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101275Floor Support · corrodedFS 349 AT SERVICE DOOR FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 601R-53-21-1321.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101274Floor Support · corrodedSERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE ABOVE SILL AT FS 349, CORRODED. REMOVED ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 AND 51-42-21.Jul 5, 2011 · N832AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101265Cargo Track · corroded5 CARGO BAY TIE DOWN POINTS ARE CORRODED, 3 AT LBL 27.00 2 AT LBL 9.0. REMOVED CORRODED FTGS (5 PLACES ) AND REPLACED WITH NEW FTGS IAW SRM 51-41-02.Jun 30, 2011 · N832AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101259Cargo Track · corrodedCARGO TRACK AT APPROX FS 574 CORRODED. R & R CARGO TRACK IAW AMM 20-21-00-02 AND 53-01-11-04.Jun 30, 2011 · N832AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101248Frame · corrodedFS 319.70 FRAME CORRODED FROM STR 25-27L. R & R FRAME IAW SRM 51-42-06. MAJOR REPAIR.Jun 30, 2011 · N832AS · Cndair CL6002B19 · Fuselage Main, Frame
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