N455CA
Service difficulty reports · 201
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 = 'N455CA' 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.
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 = 'N455CA' AND registry_match = 'registration' 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 SWIA2020012147853Coaming · corroded*SERVICE DOOR Ï¿½ LOWER AFT CORNER COMBING IS CORRODED. (C-CHECK) RO:1/17/2020REMOVED CORROSION ON FUSELAGE SIDE OF SERVICE DOOR, LOWER AFT CORNER AT COMBING REF CRJ-200 SRM 51-21-06. ORIGINAL MATERIAL THICKNESS IS .063", LOWEST REMAINING THICKNESS ISDR SWIA2020012147852Hinge · broken* RE FUEL DEFUEL DOOR HAS BROKEN UPPER HINGE. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW REPLACEMENT LATCH ON REFUEL/DEFUEL DOOR WITH REPLACEMENT FASTENERS REF CRJ200 SRM AND REF CRJ200 SRM. ELECTRICAL BONDING TEST GOOD.SDR SWIA2020012147851Vane · chafed* L/H INBD FLAP VANE SKIN CHAFFED 3 AREAS, L/H, CTR, AND R/H FROM T/E SPAR MOUNTED STOP PADS. MARKED WITH GREEN TAPE. (C-CHECK) RO:1/17/2020REMOVED DAMAGE FROM THE LH FLAP VANE CAPS. ALL FOUND OUT OF LIMITS REF REO. REPLACEMENT OF THE 3 LE CAPS COMPLIESDR SWIA2020012147850Vane · chafed* R/H INBD FLAP VANE SKIN CHAFFED 3 AREAS L/H CTR AND R/H FROM SPAR MOUNTED STOP PADS. MARKED WITH GREEN TAPE. (C-CHECK) RO:1/17/2020REMOVED DAMAGE ON THE RH FLAP VANE CAPS REF REO. PARTS OUT OF LIMITS. FLAP VANE CAPS REPLACED ON JOB 2759261 OP 363, JSDR SWIA2020012147849Plate · corrodedSERVICE DOOR PLATE ASSY SHOWING SIGNS OF CORROSION. (EVALUATE) (C-CHECK) RO:1/17/2020REMOVED AND REPLACED SERVICE DOOR PLATE ASSY P/N 601R38957-31. NEW PLATE ASSY INSTALLED ON JOB # 2759260.SDR SWIA2020012147848Washer · corroded* LEFT WING SPOILERON PANEL CORRODED PCU ACTUATOR MOUNTING HARDWARE. BOLT, WASHER AND NUT. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED LH WING INBOARD GROUND SPOILER PCU ACTUATOR ATTACHMENT HARDWARE. (2EA NEW BOLTS, 4EA NEW WASHERS, 2EA NEW NUTS) REF CSDR SWIA2020012147847Bolt · corroded* LEFT WING FLIGHT SPOILER PANEL CORRODED PCU ACTUATOR ATTACHMENT HARDWARE. BOLT, WASHER, AND NUT. (C-CHECK) RO:1/17/2020REPLACED LT WING FLIGHT SPOILERON PANEL PCU ACUATOR ATTACHMENT HARDWARE IAW CRJ200AMM. FOLLOWED PROCEDURES ON STEP F; SUBSTEP: 1 TOSDR SWIA2020012147846Bolt · corroded* LEFT WING BOTH GROUND SPOILER PANELS CORRODED BONDING WIRE ATTACHMENT HARDWARE. (C-CHECK) RO:1/17/2020REMOVED HARDWARE ON BOTH BONDING JUMPERS ON LEFT WING GROUND SPOILER PANEL REF. CRJ-200 SRM. INSTALLED NEW HARDWARE AND ORIGINAL BONDING JUMPERS TOSDR SWIA2020012147845Washer · corroded* LEFT WING OUTBOARD GROUND SPOILER PANEL CORRODED PCU ACTUATOR ATTACHMENT HARDWARE, BOLT, WASHER AND NUT. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE LEFT WING OUTBOARD GROUND SPOILER PANEL PCU ACTUATOR HARDWARE. REF CRJ200 AMM. OPERATIONAL CHECKS GSDR SWIA2020012147844Bolt · corroded* LEFT WING INBOARD GROUND SPOILER PANEL CORRODED PCU ACTUATOR ATTACHMENT HARDWARE BOLT, WASHER, AND NUT. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED LH WING INBOARD GROUND SPOILER PCU ACTUATOR ATTACHMENT HARDWARE. (2EA NEW BOLTS, 4EA NEW WASHERS, 2EA NSDR SWIA2020012147843Bolt · corroded* RIGHT WING SPOILERON PANEL CORRODED BONDING WIRE ATTACHMENT HARDWARE. (C-CHECK) RO:1/17/2020EVALUATED SPOILERON BONDING WIRE HARDWARE AND DETERMINED 3 SCREWS, 10 WASHERS, AND 4 NUTS ARE CORRODED. ORDERED AND RECEIVED 3 SCREWS, 10 WASHERS, AND 4 NUTS. SDR SWIA2020012147842Bolt · corroded* RIGHT WING FLIGHT SPOILER PANEL CORRODED BONDING WIRE ATTACHMENT HARDWARE. (C-CHECK) RO:1/17/2020REMOVED CORRODED HARDWARE FOR RIGHT WING FLIGHT SPOILER BONDING WIRE REF. CRJ-200 SRM. INSTALLED NEW HARDWARE FOR RIGHT WING FLIGHT SPOILER BONDING WIRESDR SWIA2020012147841Bolt · corroded* RIGHT WING INBOARD GROUND SPOILER PANEL CORRODED BONDING WIRE ATTACHMENT HARDWARE. (C-CHECK) RO:1/17/2020REMOVED CORRODED HARDWARE FROM RIGHT WING GROUND SPOILER BONDING WIRE REF. CRJ-200 SRM. INSTALLED NEW HARDWARE FOR RIGHT WING GROUND SPOILER BONSDR SWIA2020012147840Bolt · corroded* RIGHT WING OUTBOARD GROUND SPOILER PANEL PCU ATACHMENT HARDWARE , BOLT, NUT, WASHER CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE RIGHT WING OUTBOARD GROUND SPOILER PANEL PCU ATTACHMENT HARDWARE. REF CRJ200 AMM. OPERATIONAL CHECKS ARE GOODSDR SWIA2020012147839Bolt · corroded* RIGHT WING INBOARD GROUND SPOILER PANEL PCU ATTACHMENT HARDWARE, BOLT, NUT, WASHER CORRODED. (C-CHECK) RO:1/17/2020REMOVED AND REPLACED THE RIGHT WING INBOARD GROUND SPOILER PANEL PCU ATTACHMENT HARDWARE. REF CRJ200 AMM. OPERATIONAL CHECKS ARE GOOD.SDR SWIA2020012147838Fairing · chafed* RIGHT WING TO BODY INBOARD AT STUB FAIRING, MULTIPLE CHAFE MARKS. (C-CHECK) RO:1/17/2020REPLACED CHAFED R/H STUB FAING ASSY. WITH NEW FAIRING ASSY AND HARDWARE. REF CRJ-200 SRM CRJ-200 SRM, CRJ-200 SRM REF CRJ-200 SRM AND DRW, PERFORMED CLEARANCE CHECSDR SWIA2020012147837Vane · chafed* RIGHT WING OUTBOARD FLAP VANE MOUNTS AND STRUCTURE CHAFED AND ROLLED INTO KNIFE EDGE 5 LOCATIONS . MARKED WITH GREEN TAPE AND ORANGE FLAGS. (C-CHECK) RO:1/17/2020COMPLIED WITH ALL STEPS OF REO FOR R/H WING O/B FLAP VANE MOUNTS. EXTENDED AND RETRACTEDSDR SWIA2020012147836Vane · chafed* LEFT WING OUTBOARD FLAP VANE MOUNTS AND STRUCTURE CHAFED AND ROLLED INTO KNIFE EDGE 5 LOCATIONS . MARKED WITH GREEN TAPE/ ORANGE FLAGS. (C-CHECK) RO:1/17/2020COMPLIED WITH ALL STEPS OF REO FOR L/H WING O/B FLAP VANE MOUNTS. EXTENDED AND RETRACTED FLAPSDR SWIA2020012147835Stop Fitting · worn* CREW ESCAPE HATCH ALL FUSELAGE MOUNTED STOP FITTINGS SHOWING EXCESSIVE WEAR. (C-CHECK) RO:1/17/2020CREW ESCAPE HATCH 4 FITTINGS BLENDED REF CRJ 200 SRM. EVALUATED AND FOUND TO BE WITHIN LIMITS, REF REO. ALL STEPS OF BOMBARDIER REO HAVE BEEN COMPLETESDR SWIA2020012147834Structure · chafed* R/H SIDE MLG DOOR HAS CHAFFING DAMAGE ON LEADING EDGE OF DOOR. (C-CHECK) RO:1/17/2020DAMAGE FOUND ON R/H MLG DOOR LEADING EDGE WAS ON TWO PREVIOUS REPAIRS. NO ALLOWABLE DAMAGE LIMITS GIVEN FOR PREVIOUS REPAIRS, OUT OF LIMITS.REMOVED AND REPLACED REPASDR SWIA2020012147833Structure · chafed* L/H SIDE MLG DOOR HAS CHAFFING DAMAGE ON LEADING EDGE OF DOOR. (C-CHECK) RO:1/17/2020DAMAGE FOUND ON L/H MLG DOOR LEADING EDGE WAS ON TWO PREVIOUS REPAIRS. NO ALLOWABLE DAMAGE LIMITS GIVEN FOR PREVIOUS REPAIRS, OUT OF LIMITS.REMOVED AND REPLACED REPASDR SWIA2020012147832Skin · damagedADM# 2935 FWD FUSELAGE BETWEEN FS 265.00-280.00, 1.5" RIGHT OF STR 26R . PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO:1/17/2020REPAIRED FWD FUSELAGE DAMAGE BETWSDR SWIA2020011947831Structure · dentedADM # 1714 LEADING EDGE OF THE RH ENG PYLON APPROX 5.125 IN FROM THE IB EDGE TO FUSELAGE. DENT DIA = .5 INCH DEPTH = .03125 INCH. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (SDR SWIA2018101845156Sensing Element · failedL 14TH DUCT WARNING MESSAGE IN FLIGHT. DID NOT GO AWAY AFTER QRH PROCEDURE. EMERGENCY-DECLARED. LANDED WITHOUT INCIDENT. (FLT 4727) CLOSED REMOVED AND REPLACED LT PYLON SENSING ELEMENT IAW AMM. OPS CHECK GOOD AT THIS TIME.SDR SWIA2017122644093Skin · damagedRIGHT INBD FLAP LOWER SKIN HAS DAMAGE ON THE INBD EDGE. PERFORMED A REPAIR IAW SRM.SDR SWIA201744065Frame · corrodedCORROSION ON FRAME 605 STR 26R- 27 FWD AND AFT SIDE. (C-CHECK) REPLACED FRAME FS605 FROM STR 20R-20L IAW SRM. LEAK CHECK GOOD.SDR SWIA2017082143647Actuator · failedWHEN SELECTING GEAR DOWN. GEAR DISAGREE, RT MLG DID NOT SHOW DOWN AND LOCKED. FOLLOWED FULL QRH PROCEDURE BUT GEAR NEVER SHOWED GREEN. GEAR WAS VISUALLY VERIFIED TO BE DOWN. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT SIDE STAY ACTUATOR ASSY IAW AMM. SDR SWIA201642931Bracket · bentAFTER TAKE OFF NOSE GEAR AND NOSE GEAR DOOR DISAGREE RETURNED TO FIELD. FOUND BRACKET FOR PROXIMITY SENSOR PS146A BENT CAUSING TARGET TO STRIKE SIDE OF PROXIMITY SENSOR. R & R BRACKET FOR PROX SENSOR FOR PS146A ADJUSTED PROXIMITY SENSOR AND PERFORMED NLG SWINSDR SWIA201541664Floor Support · damagedFS 330.00 FLOOR SUPPORT POST AND CROSSBEAM HAVE AN OVERSIZED FASTENER INSTALLED AT LBL 20.00. NOT RELEASED, REPAIRED FASTENER HOLES IN FLOOR SUPPORT POST AND CROSSBEAM IAW REO.SDR SWIA201541666Frame · corrodedFRAME AT FS 333.00 CORRODED IN AVIONICES BAY FROM STR 25R TO STR 25L. NOT RELEASED. R & R FRAME PN 601R32004-55 IAW SRM.SDR SWIA201541665Crossbeam · corrodedFS 280, J-ANGLE AND CROSSBEAM HAVE CORROSION AROUND CAMLOC FASTENER HOLES. NOT RELEASED. R & R J-ANGLE AND REPAIRED CROSSBEAM IAW REO.SDR SWIA201438878Selector Valve · failedDURING DEPARTURE, RECEIVED A NOSE DOOR OPEN WARNING AFTER SELECTING GEAR UP. REPLACED NOSE GEAR DOOR SELECTOR VALVE IAW AMM.SDR SWIA201437722Lamp · burned outMULTIPLE MINIATURE LAMPS BURNED OUT ON BOTH INTERIOR DOOR EMERGENCY EXIT SIGNS AND AFT FORWARD FACING CEILING EMERGENCY EXIT SIGN, REPLACED THE LAMPS.SDR SWIA201437640Bushing · galledRIGHT ENGINE AFT ENGINE MOUNT SPHERICAL BUSHING SHOWING SIGNS OF GALLING. R & R RT ENGINE MOUNT SPHERICAL BUSHING IAW AMM.SDR SWIA201437639Housing · galledRT ENGINE AFT MOUNT HOUSING SHOWING SIGNS OF GALLING. R & R RT ENGINE AFT MOUNT HOUSING IAW AMM.SDR SWIA201437525Lamp · burned outFLOOR EMERGENCY FLOOD LIGHT NEXT TO PASSENGER DOOR HAS IS BURNED OUT. REPLACED THE LAMP.SDR SWIA201437571Battery Pack · failedOVERWING EMERGENCY LIGHTS AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED FWD EMERGENCY LIGHT BATTERY PACK IAW AMM.SDR SWIA201437570Skin · puncturedFUSELAGE IS CRACKED FORWARD OF AFT EQUIPMENT BAY. CLASSIFIED AS A PUNCTURE, REMOVED DAMAGE IN FUSELAGE FORWARD OF AFT EQUIPMENT BAY IAW SRM.SDR SWIA201437569Structure · damagedON LANDING HAD A RT WING STRIKE ON WING TIP. DAMAGE DETERMINED TO BE A MAJOR REPAIR IAW GMM. REPLACED RT WINGLET/PLUG ASSY IAW IRL.SDR SWIA201335942Skin · chafedLT AILERON UPPER LE IS CHAFED IN 3 LOCATIONS OTBD, MID OTBD & MID. C-CHECK REPLACED THE UPPER LE SKIN OF THE LT AILERON IAW SRM.SDR SWIA201336032Hinge · gougedPAX DOOR HINGE ON FUSELAGE SIDE IS GOUGED. C-CHECK REPLACED FUSELAGE SIDE HINGE IAW SRM.SDR SWIA201335532Hinge · gougedPASSENGER DOOR HINGE ON FUSELAGE SIDE IS GOUGED. C-CHECK REPLACED SIDE HINGE IAW SRM.SDR SWIA201335943Floorbeam · corrodedRBL 9.00 HAS CORROSION ON THE OTBD FLANGE BETWEEN FS 589 & FS 621. C-CHECK REPLACED RBL 9.00 FLOOR BEAM CAP.SDR SWIA201335930Floorbeam · corrodedRBL 27 FLOOR BEAM CAP HAS CORROSION ON INBD & OTBD FLANGES BETWEEN FS 574 & FS 621. C-CHECK REPLACED RBL 27 FLOOR BEAM CAP.SDR SWIA201335929Floorbeam · corrodedLBL 27 FLOOR BEAM HAS CORROSION ON OTBD FLANGE FROM FS 574.00 TO FS 621.00. C-CHECK REPLACED LBL 27 FLOOR BEAM CAP.SDR SWIA190036033Bulkhead · crackedREAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROXIMATELY .200 INCHES IN LENGTH 50% FSH. C-CHECK REPAIRED REAR PRESS BULKHEAD IAW REO.SDR SWIA201335531Bulkhead · crackedREAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROXIMATELY .200 INCHES IN LENGTH. C-CHECK REPAIRED REAR PRESSURE BULKHEAD WEB HAS INDICATION AT LBL 27.50, WL 130 IAW REO.SDR SWIA201334959Battery Pack · failedNR 2 OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. FLT#4480 REPLACED NR 4 BATTERY PACK IAW AMM. PN AD-2013-1A SN ON 79584 SN OFF 84040SDR SWIA201334961Battery Pack · failedEMERGENCY LIGHTING SYSTEM DOES NOT ILLUMINATE. FLT#4845 REPLACED ALL 4 ELBPS. PN'S ON AD-2013-1A, SN'S ON 75706, 84040, 77126, & 69414, PN'S OFF 2013-1A , SN'S OFF 49803, 53490, & 106953, PN OFF AD-2013-1A, SN OFF 43882SDR SWIA201334481Light · inoperativeOVERHEAD EMERGENCY LIGHT BURNED OUT. FLT#455CA RELAMPED.
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