N845AS

Service difficulty reports · 177

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 = 'N845AS' AND registry_match = 'registration'
  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 ASOA201201156Structure · corrodedFS 349 CORRODED BETWEEN LBL 26 AND RBL26 BOTH SIDES. CORROSION IS OUT OF LIMITS IAW SRM 53-00-00. R & R FRAME IAW SRM 51-42-06.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201201154Frame · corrodedFS 364 FRAME CORRODED BETWEEN LBL 26 AND RBL 26.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201201150Floorbeam · corrodedFS 349 AND LBL 40, FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM AND FOUND OUT OF LIMITS IAW SRM 53-00-00. INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-42-06.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201148Frame · corrodedFRAME 310 CORRODED BETWEEN LBL 26 AND RBL 26 BOTH SIDES. FRAME SECTION CORRODED BEYOND LIMITS IAW SRM 53-00-00. REMOVED FRAME IAW SRM 51-42-21 AND SRM 51-42-21. INSTALLED FRAME SECTION IAW SRM 51-42-06 AND 51-42-21.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201201146Floor Support · corrodedSERVICE DOOR FLOOR SUPPORT ANGLE CORRODED AT 314.00 AND RBL 40. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00. INSTALLED SERVICEABLE ANGLE IAW DWG 601R38303, REV AR AND SRM 51-42-21.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201201144Floorbeam · corrodedSERVICE DOOR AREA AT BS 340 RBL 40 CROSSBEAM CORRODED AT TEE AND ATTACHING ANGLE BRACKET. REPAIRED IAW SRM 51-42-21-00.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201201142Intercostal · crackedCARGO DOOR INTERCOSTAL CRACKED LOWER AFT CORNER. REMOVED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06, 51-42-21, & 51-40-11.Apr 3, 2012 · N845AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA201201119Floorbeam · crackedCABIN FLOORBEAM ANGLE CRACKED AT FS 280 AND LBL 9. R & R FLOORBEAM ANGLE IAW SRM 51-42-20.Apr 2, 2012 · N845AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201201117Floorbeam · crackedCABIN FLOORBEAM ANGLE CRACKED AT FS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-20.Apr 2, 2012 · N845AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201200623Hydraulic System · failedAFTER TAKE OFF HYD 1 LOW PRESSURE CAUTION MESSAGE, QTY AND PRESSURE ZERO. ENGINE RAN FOR 25 MINUTES EMPTY, COMPLIED WITH QRH DIVERTED AND EMERGENCY DECLARED.Feb 24, 2012 · N845AS · Cndair CL6002B19 · Hydraulic System, MainSDR ASOA201200484Rod · damagedPAX DOOR WILL NOT OPEN. R & R SPRING ROD ASSY ON PAX DOOR IAW AMM 52-11-15. OPS CHECKED GOOD.Feb 12, 2012 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102403Cover · missingEMERGENCY LIGHT COVER IN GALLEY NEAR SERVICE DOOR IS MISSING THE EXIT COVER. R & R IAW AMM 33-51-05. PERFORMED OP TEST IAW AMM 33-51-00-710-801. NO FAULTS.Dec 20, 2011 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2011121602374Lamp · burned outCABIN CEILING EMERGENCY LIGHT, 2ND FROM FRONT, INOPERATIVE. RELAMPED IAW AMM 33-51-16. OPS CHECKED GOOD.Dec 16, 2011 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201102168Lamp · burned outAFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.Nov 12, 2011 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101757Flashlight · inoperativeCAPTAIN`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.Sep 18, 2011 · N845AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201101756Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.Sep 18, 2011 · N845AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201101196Lamp · burned outCABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED CABIN AFT MOST CEILING EMERGENCY LIGHT AS REQUIRED. OPS CK GOOD IAW AMM 33-51-00.Jun 17, 2011 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101009Battery Pack · failedNR 1 & NR 2 EXTERIOR AND NR 1 INTERIOR CEILING EMERGENCY LIGHTS INOP. R & R NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD. R & R NR1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CK GOOD.May 19, 2011 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100511Skin · crackedWHILE PERFORMING NDT INSP, IN THE LOCAL AREA, FOUND A VISIUAL INDICATION OF A CRACK JUST OTBD OF THE LT WING JACKING POINT AT WS 148.00 AT THE AFT SPAR AREA. WORK COMPLETED IAW: REO 601R-57-21-1409.Mar 17, 2011 · N845AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201001998Battery · inoperativeCAPTAINS FLASHLIGHT IN-OP. REPLACED CAPTAINS FLASHLIGHT BATTERIES IAW AMM 25-61-00.Dec 21, 2010 · N845AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001910Handle · brokenRAMP REPORTS PAX DOOR HANDLE BROKE. INSPECTED AND LUBRICATED OUTER AND INNER HANDLES, AND FOUND SAFETY WIRE ON OUTER DOOR HANDLE LUBRICATION POINT BROKEN AND RESAFETIED, OPS CHECK GOOD IAW AMM 52-11-00 AND 52-11-23. (CLOSED)Dec 10, 2010 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001496Bulb · burned outSERVICE DOOR LWR EMERGENCY EXIT SIGN HAS 2 BURNED OUT BULBS. R & R INOP BULBS FROM SVC DOOR LWR EMERGENCY EXIT SIGN IAW AMM 33-51-14.OPS CHECKED GOOD. R & R INOPERATIVE BULBS FROM SERVICE DOOR LWR EMERGENCY EXIT SIGN IAW AMM 33-51-14. OPS CHECKED GOOD.Oct 3, 2010 · N845AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201000644Placard · missingPLACARDS ARE MISSING ON EXTERIOR OF COCKPIT EMERGENCY EXIT DOOR. USED SILKSCREEN METHOD TO LABEL PLACARDS THAT ARE MISSING IAW AMM TASK 11-10-03-000-801.Apr 26, 2010 · N845AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000596Skin · corrodedCORROSION FOUND ON SKIN SPLICE AT FS 333 BETWEEN STR 27 AND 26. REPAIRED IAW REO 601R-53-21-1125.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201000598Bracket · crackedCARGO DOOR SUPPORT BEAM HAS CRACKED BRACKET WHERE IT MAKE TO 621.00 BULKHEAD. (LT 04/18/10) (RESOLVED ON W/O: 155601 TASKCARD: N/R-00390 ) JOB 8732425 /OPERATION 207/ REMOVED CRACKED BRACKET FOR CARGO DOOR SUPPORT BEAM AT FS 621.00 BULKHEAD IAW SRM 51-42-21. Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000597Stringer · corrodedCORROSION FOUND ON STR 26R 3" AFT OF FS 333. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. STARTED SPLICE REPAIR FOR STRG 26R IAW SRM 53-00-03. PERFORMED ET INSPECTION OF CUT LINES IAW SRM 53-00-03 PARA.4.(5) IAW NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. CApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201000595Bracket · crackedBRACKET CRACKED AT FS469.63 BELOW LT WING ENERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 161DL ATTACHES TO RT 161728. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00370 ) JOB 8732425 /OPERATION / REMOVED CRACKED ANGLE AT FS 469.93 JUST BELOW LT WING EMERGENCY EXIApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000594Bracket · crackedBRACKET CRACKED AT FS 449.85 BELOW LT WING EMERGENCY EXIT THAT THE FUSELAGE OVER WING PANEL 161DL ATTACHES TO RT 161728. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00369 ) JOB 8732425 /OPERATION 186/ BRACKET CRACKED AT FS 449.85 BELOW LT WING EMERGENCY EXIT THAT TApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000593Bracket · crackedBRACKET CRACKED AT FS 449.85 BELOW RT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 162DL ATTACHES TO RJ161728. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000592Bracket · crackedBRACKET CRACKED AT FS 469.63 BELOW RT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 162EL ATTACHES TO RT 161728. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE ALL WORK DONE IAW SRM 51-42-06 AND SRM 51-42-21.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000591Bulkhead · crackedCRACK INDICATION FOUND ON AFT PRESSURE BULKHEAD LOCATED AT THE TOP OF THE AFT CARGO DOOR TRACK. AREA IS MARKED. PERFORMED CUT OUT ON AFT PRESSURE BULKHEAD AND FABRICATED FILLER AND DOUBLES IAW REO 601R-53-61-1541. NDT REQUIRED OF CUT LINE. PERFORMED ET INSApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000590Bulkhead · crackedCRACK INDICATION FOUND AT AFT PRESSURE BULKHEAD LOCATED AT THE TOP OF THE LINTEL ATTACH POINT. AREA IS MARKED. REPAIRED IAW EC/TC REO 601R53-61-1230.Apr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201000589Frame · corrodedFRAME SECTION AT FS 333 FOUND CORRODED AT APPROX RBL 9 AT GROUND STUD ATTATCH POINTS, ONE GROUND STUD CORRODED OUT OF FRAME. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00318 ) JOB 8732425/ OPERATION 135/ REMOVED UNSERVICABLE FRAME FROM FS 333 AND INSTALLED SERVICEApr 19, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201000571Bracket · crackedAFT PRESSURE BULKHEAD FS 621, ISOLATOR NUT PLATE BRACKET CRACKED AT 1ST ROW FROM BOTTOM LBL 27.50. R & R ONE ISOLATOR WITH CR3213-5-2 RIVETS AT FS 621 ROW 1 ON LBL 27.50 IAW SRM 51-42-13.Apr 16, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000570Isolation Mount · crackedAFT PRESSURE BULKHEAD FS 621, NUT PLATE ISOLATOR BRACKET CRACKED AT 2ND ROW FROM BOTTOM LBL 27.50. R & R ISOLATOR IAW SRM 51-42-13.Apr 16, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000569Bracket · crackedCABIN AFT PRESSURE BULKHEAD FS 621, NUT PLATE ISOLATOR BRACKET CRACKED AT 2ND ROW FROM BOTTOM LBL 9.50. R & R 2 ISOLATOR IAW SRM 51-42-13.Apr 16, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000568Bracket · crackedCABIN AFT PRESSURE BULKHEAD FRAME 621 NUT PLATE ISOLATOR BRACKET CRACKED AT 2ND ROW FROM BOTTOM RBL 9.50.Apr 16, 2010 · N845AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201000358Spring · failedPASSENGER BOARDING DOOR WILL NOT OPEN NORMALY WITH OUT EXTERIOR ASSISTANCE. R & R PASSINGER DOOR PRESSURE VENT-FLAP DOOR SPRING IAW AMM 5 2-11-15 OPS CHECK GOOD.Mar 5, 2010 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201000263Placard · missingF/A REPORTS OPEN AND EXIT PLACARDS MISSING FROM PAX DOOR. INSTALLED PLACARDS AMM 11-30-00.Feb 16, 2010 · N845AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201000262Handle · lack of lubeF/A REPORTS PAX DOOR DIFFICULT TO OPEN. LUBRICATED HANDLE, INSPECTED DOOR MECHINISM, AND OPERATIONAL TEST GOOD. AMM 52-11-01.Feb 16, 2010 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201000153Handle · bindingF/A REPORTS ENTRY DOOR HARD TO CLOSE/OPEN HANDLE MESSED UP. PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW AMM 52-11-00. NO DEFECTS NOTED.Feb 3, 2010 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201000090Roller Cam · lack of lubeMAIN PAX DOOR STICKING AND HARD TO OPEN. LUBED PAX DOOR HANDLE ROLLER GUIDE IAW AMM 12-20-52. OP CK GOOD. ACFT OK FOR SERVICE.Jan 22, 2010 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901458Door · stuckPAX DOOR WOULDNT OPEN FROM THE INSIDE.Dec 25, 2009 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901441Pin · stuckFA REPORTS WHEN THEY TRY TO OPEN THE PAX DOOR PINS WILL NOT DISENGAGE NEEDS TO MOVE HANDLE DOWN AND UP A FEW TIMES TO OPEN.Dec 19, 2009 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901177Door · stuckF/A UNABLE TO OPEN PAX DOOR WITHOUT ASSISTANCE FROM OUTSIDE.Oct 24, 2009 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200901112Angle · crackedWHILE PERFORMING HFEC INSP OF F.S. 559.0 WEB AND CAP ANGLE, THREE INDICATIONS WERE NOTED AS LISTED 1) 2", 100% FSH IND NOTED AT RBL 18.0 WL 59.10 IN CHEM MILLED RADIUS, 2) .1", 75% FSH IND NOTED AT RBL 9.0 WL 58.70 APPROX Ï¿½" O/B OF CHEM MILLED RADIUS, AND .2Oct 8, 2009 · N845AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901111Floor Skin · crackedHFEC INDICATION NOTED AT 60% FSH APPROX 1" LONG IN THE PRESSURE FLOOR AT RBL 4.50 APPROX 1.25" FWD OF THE F.S. 460 INTERCOSTAL. INDICATION APPEARS TO RUN PARALLEL WITH INTERCOSTALS. FAILS NDT INSP AT THIS TIME. COMPLIED WITH EC/TC REO 601R-53-41-884A BY PERFOOct 8, 2009 · N845AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA200900997Door · stiffF/A REPORTS PAX DOOR VERY DIFFICULT TO OPEN. " MUST JIGGLE.'Sep 12, 2009 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900970Lock · inoperativeMAIN ENTRANCE DOOR NOT RELEASE LOCKS WHEN OPENEDSep 2, 2009 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900659Light · inoperativeRT FWD EXTERIOR EMERGENCY LIGHT BURNED OUT.Jun 11, 2009 · N845AS · Cndair CL6002B19 · Emergency Lighting
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