N207PS

Service difficulty reports · 160

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 = 'N207PS' 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 SWIA2026101177594Proximity Sensor · false indicationUPON SELECTING GEAR UP, GOT GEAR DISAGREE, NOSE DOOR WARNINGS, WOW INPUT, STEERING INOP CAUTIONS AND WOW STATUS MESSAGE RAN QRH FOR ALL ITEMS, UPON LANDING ALL CAUTION AND STATUS MESSAGES WENT AWAY, NOSEWHEEL STEERING OPERATED NORMALLY FLIGHT 5094. FIM 32-6Oct 11, 2026 · N207PS · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2026031176883Skin · crackedCRACK FOUND IN FUSELAGE SKIN AT BS 235 AT AFT LEFT CORNER OF NLG CUTOUT. REPAIRED THE SKIN IAW REO 601R-53-11-048 REV-D, & REO 601R-53-11-4076, REV-.Mar 11, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026030776886Skin · wornSKIN PANEL AT BS 550, LBL47 WORN. REPAIRED THE LT APRON SKIN PANEL BTWN BS 516.85 - 559 IAW REO 601R-53-41-3423, REV -.Mar 7, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026030776881Skin · wornSKIN PANEL AT BS 550, RBL47 WORN. REPAIRED THE RT APRON SKIN PANEL BETWEEN BS 516.85 - 559 IAW REO 601R-53-41-3423 REV -, SKYWEST CONTINUE CARDS, ITEMS 1-32; 1-22; 1-22,Mar 7, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026030376885Skin · dentedLOWER SKIN OF RT INBD FLAP HAS MULTIPLE SMALL DENTS & ROCK DAMAGE. REPAIRED THE SKIN OF THE RT INBD FLAP IAW REO 601R-57-52-2555 REV--. APPLIED SURFACE FINISH IAW SRM 51-25-01, & SRM 51-26-00.Mar 3, 2026 · N207PS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026022476884Skin · crackedSKIN CRACKED AT BS 235, STR 26R AT AFT CORNER OF NLG CUTOUT. REPAIRED THE SKIN RADIUS AT BS 235 IAW REO 601R-53-11-048, REV -D. & REO 601R-53-11-4076, REV--, SRM 51-42-06, SRM 51-25-01, & AMM 32-22-05.Feb 24, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026020576882Skin · dentedDENT 28.5" FROM RT WING IBD FLAP OTBD EDGE & 5.75" FROM TE ON UPPER SKIN. DENT FOUND TO BE 1.2" X 1" AT A DEPTH OF 0.028". REPAIRED THE RT WING INBD FLAP OTBD EDGE AND 5.75 FROM TE ON UPPER SKIN IAW REO 601R-57-52-2555, REV--. APPLIED SURFACE FINISH IAW SFeb 5, 2026 · N207PS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20250512001Warning Message · false activationSERVICE DOOR CAUTION MESSAGE PASSING THROUGH 10,000. PRESSURE STAYED NORMAL. DOORS PAGE SHOWED OUTER HANDLE, MESSAGE DISAPPEARED AND REAPPEARED MULTIPLE TIMESC: MEL 52-70-5CAT C DUE DATE IS 05/15/2025"SMOD APPROVAL REQUIRED BEFORE RTS AFTER COMPLETION." (FLIGHMay 5, 2025 · N207PS · Cndair CL6002B19 · Door Warning SystemSDR SWIA202505060005Door · warning messageSERVICE DOOR CAUTION MESSAGE PASSING THROUGH 10,000. PRESSURE STAYED NORMAL. DOORS PAGE SHOWED OUTER HANDLE, MESSAGE DISAPPEARED AND REAPPEARED MULTIPLE TIMES, MEL 52-70-5CAT C DUE DATE IS 05/15/2025"SMOD APPROVAL REQUIRED BEFORE RTS AFTER COMPLETION." (FLIGHTMay 5, 2025 · N207PS · Cndair CL6002B19 · Door Warning SystemSDR SWIA2025040300314Skin · dentedFOUND 1 DENT LOCATED ON THE SKIN EDGE OF THE PAX DOOR SURROUND OPENING AT FS 310.00 BETWEEN STRINGERS 14L AND 13L.  THE DENT MEASURES .800€? X .250€? X .114€? MAX DEPTH. (FILED CLOSED)REPAIRED FUSELAGE SKIN EDGE AT THE PASSENGER DOOR CUTOUT AT FS310.00 BETMar 14, 2025 · N207PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2025040300010Hinge · gougedPAX DOOR HINGE PIN, SPRING PIN AT THE VERY AFT END OF THE HINGE HAS MIGRATED OUT AND GOUGED THE AIRFRAME HINGE HALF LUG LAND. (FILED CLOSED)BLENDED MCD AIRFRAME SIDE VERY AFT HINGE LUG LAND IN REF. TO REO 601R-53-21-3738, REV.--, DATED 2025-03-22 AND 601R-53-2Mar 10, 2025 · N207PS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202504030006Angle · corrodedPAX DOOR SURROUND STRUCTURE LOWER SILL ANGLE (SRM 53-21-23 ITEM 56B) CORRODED. (FILED CLOSED)REMOVED AND REPLACED THE PAX DOOR SURROUND STRUCTURE LOWER SILL ANGLE IN REFERENCE WITH THE CRJ-200 SRM 53-21-23, SRM 51-42-21, SRM 51-42-06, SRM 51-42-13 AND SRM 51-4Mar 6, 2025 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202504030004Intercostal · crackedAFT SIDE OF PRESSURE BULKHEAD FS621.00 INTERCOSTAL INLINE WITH STRINGER 14L AND LBL36.20 CRACKED. (FILED CLOSED)REMOVED AND REPLACED FS621.00 STR 14L LBL36.20 INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD WITH REFERENCE TO REO 601R-53-61-100 REV "-A" DATED 2008Mar 4, 2025 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F00062Window · failedCA WINDOW SHATTERED WHILE TAXIING ON RAMP TO RUNWAY. (FLIGHT 4663 - FILED CLOSED) PLEASE REFERENCE AML 1514132. REMOVED AND REPLACED CA SIDE WINDOW REF THE APPLICABLE STEPS OF CRJ AMM 56-12-01. PERFORMED OPERATIONAL CHECK OF THE WINDOW HEAT TEMP CONTROLLJan 14, 2025 · N207PS · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA20231229008Unknown · warning messageL WINDOW HEAT CAUTION IN FLIGHT. QRH DID NOT CLEAR THE MESSAGE. (FILED CLOSED)REMOVED AND REPLACED (LEFT WINDOW SIDE) WINDSHIELD AND SIDE HEATER CONTROLLER IN REFERENCE TO CRJ 200 AMM 30-41-01. PERFORMED OPS CHECK IN REFERENCE TO CRJ 200 AMM 30-41-01, OPS CHEDec 28, 2023 · N207PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR SWIA2023101900117Unknown · warning messageAFTER TAKEOFF, GOT €˜GEAR DISAGREE€™ WARNING MESSAGE. NOSE GEAR REMAINED DOWN AND GREEN. RAN QRH, LOWERED THE GEAR, GOT 3 GREEN. RETURNED TO FIELD. (FLIGHT 4680 FILED CLOSED)Oct 17, 2023 · N207PS · Cndair CL6002B19 · Landing Gear SystemSDR SWIA2023101800017Unknown · warning messageAFTER TAKEOFF, GOT €˜GEAR DISAGREE€™ WARNING MESSAGE. NOSE GEAR REMAINED DOWN AND GREEN. RAN QRH, LOWERED THE GEAR, GOT 3 GREEN. RETURNED TO FIELD. (FLIGHT 4680 FILED OPEN)Oct 17, 2023 · N207PS · Cndair CL6002B19 · Landing Gear SystemSDR SWIA202266459None · dentedLHOB FLAP LOWER SURFACE HAS DENT ON TRAILING EDGE @ WS 236.00 (FILED CLOSED) REMOVED AND REPLACED LEFT WING OUTBOARD FLAP, COMPLIED WITH TASK CARD 27-900-1006-SKY, RIG AND OPS CHECK GOOD AT THIS TIMESep 11, 2022 · N207PS · Cndair CL6002B19 · Aileron TabsSDR SWIA202163729None · mislocatedL/H HORZONAL STAB TIP PANEL HAS MISLOCATED NUTPLATE ON INBOARD EDGE, THIRD NUTPLATE FWD OF TRAILING EDGE OF STAB TIP. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RIB AND SPLICE WITH NEW FABRICATED PN: 600-23079-S0101 RIB AND PN: 600-23037-22 SPLICE IAW RDec 5, 2021 · N207PS · Cndair CL6002B19 · Horizontal Stabilizer, Tab StructureSDR SWIA202163728None · dentedFOUND DENT ON EXTERNAL SKIN BETWEEN FS589 AND FS605 FROM STGR25L TO 27 (C-CHECK RO 1/5/2022) REMOVED DAMAGE FROM EXTERNAL SKIN AT FS 589 - FS 605 FRM STR 25L TO STR 27 AND REPAIRED IAW REO 601R-53-61-7762 REV -- DATED 2021-12-09. COMPLETE SKYWEST MAJOR Nov 30, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163727None · damagedF.S 605 FRAME SPLICE ANGLE PN: 601R36026-19 LOCATED BETWEEN STGR 20L & 21L REQUIRE REPLACEMENT PART TO BE FABRICATED AS PER SAMPLE PART PN: 601R36026-19 (C-CHECK RO 1/5/2022) REMOVE AND REPLACED FRAME SPLICE PN: 601R3606-19 WITH NEW FABRICATED FRAME SPLNov 17, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163737None · corrodedCORROSION ON RBL 9 SEAT TRACK BETWEEN FS 559 AND FS 559+99. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RBL 9 SEAT TRACKS BETWEEN FS 559 TO FS 559+99 IAW CRJ 200 AMM 53-01-11-000/400-802 REF CAMP # 23855408 FOR FABRICATION AND ATTACHED CONTINUATION CARD Nov 14, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163726None · dentedDISCREPANCY TRANSFERRED FROM CAMP#23757786. FUSELAGE EXTERNAL SKIN HAS A DENT AT FS 636 BETWEEN STR 20L AND 21L (C-CHECK RO 1/5/2022) DRESSED BACK DENT AT F.S 636 BETWEEN STGR 20L AND 21L IAW REO 601R-51-00-309 REV: A DATE:2017-08-23 AND COMPLETED DISPNov 13, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163736Bracket · crackedLHS STR 15 L FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED ON THE AFT SIDE OF THE FS621 BULKHEAD (C-CHECK RO 1/5/2022) REMOVED AND REPLACED OBLIQUE ANGLE FS621 TO FS625 LH STR15 IAW CRJ200 SRM 51-42-21Nov 7, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202163735None · crackedLHS FS 621 TO FS 625 OBLIQUE ANGLE AT STR 14L IS CRACKED ON THE AFT SIDE OF THE FS 621 BULKHEAD (C-CHECK RO 1/5/2022) REMOVED AND REPLACED LHS FS 621 TO FS 625 OBLIQUE ANGLE AT STR 14L IAW CRJ 200 SRM 51-42-21. SEE CONTINUE CARD FOR DETAILS OF WORK PERFNov 7, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202163749None · crackedFS 484 ANGLE OB SIDE OF RBL 27 IS CRACKED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FS 484 ANGLE OB SIDE OF RBL 27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEDNov 3, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163748None · crackedFS 484 ANGLE OB SIDE OF LBL 27 IS CRACKED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FS 484 ANGLE OF SIDE OF LBL 27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEDNov 3, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163725None · damagedRH FUEL BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS 50% FSH AROUND ENTIRE CIRCUMFERENCE ON THE LANDING AND VERTICAL SURFACES. FAILED NDT INSPECTION. (C-CHECK RO 1/5/2022) REMOVED DAMAGE FROM RH FUEL BOOST PUMP CUT OUT IAW REO 601R-57-21-3457 REV -- DATENov 2, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163724None · chafedRH AILERON UPPER SKIN LEADING EDGE IS CHAFED IN MULTIPLE AREAS (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RH AILERON UPPER SKIN LEADING EDGE IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATNov 2, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163747None · corrodedPAX DOOR FITTINGS, FWD UPPER PIN STOP FITTING HARDWARE CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED HARDWARE FOR THE PASSENTER DOOR FWD UPPER STOP FITTING IAW CRJ 200 AMM 53-21-23-000/400-801 ADJUSTMENT AND OPS CHECKS GOOD REF ATTACHED CONTINUATOct 26, 2021 · N207PS · Cndair CL6002B19 · DoorsSDR SWIA202163723None · crackedPRESSURE BULKHEAD TOP SPLICE ANGLE AT FS 621.00 STGR 0 POSSIBLE CRACKED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED TOP SPLICE ANGLE AT FS 621 IAW CRJ 200 SRM 51-42-06, AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FOROct 26, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202163750Washer · corrodedSERVICE DOOR FWD AND AFT STOP FITTING HARDWARE CORRODED. (C-CHECK RO 1/5/2022) REMOVED CORRODED HARDWARE AND INSTALLED NEW HARDWARE IAW CRJ-200, SRM 51-41-02. SAFETY CABLIED NEW HARDWARE IAW CRJ-200, AMM 20-24-00-910-803. OPERATIONAL TEST OF THE SERVICOct 25, 2021 · N207PS · Cndair CL6002B19 · Galley DoorsSDR SWIA202163734None · corrodedFLOOR SEAT TRACK AT RBL9 FS 409+128 TO FS 559.00 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RBL FLOOR SEAT TRACK AT FS 409+128 - FS 559 IAW CRJ 200 AMM 53-01-11-400-802Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163733None · corrodedFLOOR SEAT TRACK AT RBL9 FS 399.00 TO FS 409+128 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RBL FLOOR SEAT TRACK AT FS 399 - FS 409+128 IAW CRJ 200 AMM 53-01-11-400-802Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163732None · corrodedFLOOR SEAT TRACK AT LBL9 FS 399.00 TO FS 409+128 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SEAT TRACK LBL 9 FROM FS399.00-FS409+128 IAW CRJ 200 AMM 53-01-11-000/400-802. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163731None · corrodedFLOOR SEAT TRACK AT RBL9 FS 364.00 TO FS 399.00 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED NEW SEAT TRACK AT RBL 9 FS 364 TO FS 399 PN# 601R31032-15 PO# 69772 IAW CRJ 200 AMM 53-01-11-000-802 AND CRJ 200 AMM 53-01-11-400-802Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163730None · corrodedFLOOR SEAT TRACK AT LBL9 FS 364.00 TO FS 399.00 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FS 364 TO FS 399 PN# 601R31032-15 PO# 69772 IAW CRJ 200 AMM 53-01-11-000-802 AND CRJ 200 AMM 53-01-11-400-802Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163722None · corrodedFLOOR SUPPORT BEAM AT FS 349.00 RBL36 IS CORRODED. (C-CHECK RO 1/5/2022) REPAIRED FLOOR SUPPORT BEAM AT F.S. 349.00 RBL 36 IAW BOMBARDIER REO 601R-53-21-2745 REV - - DATED 2016-11-18. COMPLETED TASK CARD 51-900-1003-SKY AND M-337. NO CHANGE TO WEIGHT AOct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202163721None · crackedFLOOR SUPPORT STRUCTURE AT FS280 AND AT RBL9 O/B OF FLOOR BEAM, ANGLE CRACKED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ANGLE ON FLOOR SUPPORT STRUCTURE AT FS280 AND AT RBL9 O/B OF FLOOR BEAM IAW CRJ 200 SRMM 51-42-21, 51-40-11, 51-25-00, REF BOMBAROct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202163720None · crackedFLOOR SUPPORT STRUCTURE AT FS280 AND AT RBL9 IB OF FLOOR BEAM, ANGLE CRACKED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE ANGLE AT FS 280.00 AND AT RBL9 IB IAW CRJ 200 SRM 51-42-21,51-40-11, 51-25-00, BOMBARDIER REO 601R-53-11-17Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202163719Angle · corrodedFLOOR SUPPORT STRUCTURE AT FS280 AND BETWEEN RBL9 AND LBL9 UNDER PANEL 221ALF, ANGLE CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE ANGLE AT FS280 BETWEEN RBL9 AND LBL9 UNDER PANEL 221ALF IAW CRJ 200 SRM 51-40-11, 51-42-06Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202163718None · crackedFLOOR SUPPORT STRUCTURE AT FS280 AND BETWEEN RBL9 AND LBL9 "J"ANGLE CRACKED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE AT FS280 AND BETWEEN RBL9 AND LBL9 AFT "J"ANGLE AND RH REPAIR SPLICE IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202163717None · corrodedBEAM CORRODED AT RBL9 BETWEEN FS 409.00 AND FS 409+16 (C-CHECK RO 1/5/2022) REPAIRED FLOOR BEAM AT RBL9 BETWEEN F.S. 409.00 - 409.00+16 IAW CRJ-200 SRM 53-00-43 REPAIR NO. 2. COMPLETED TASK CARD 53-900-1003-SKY AND M-337. NO CHANGE TO WEIGHT AND BALANCEOct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163716Angle · corrodedFRAME AT FS 409+64 CORRODED BETWEEN STGR26L AND STGR26R. (C-CHECK RO 1/5/2022) REMOVED DAMAGE FROM FS 409+64 FRAME FRROM STR 26L AND 26R AND COMPLIED WITH SRM 53-00-15. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. NO WEIGHOct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163715None · corrodedFRAME AT FS 349.00 CORRODED BETWEEN STGR27 AND STGR26R. (C-CHECK RO 1/5/2022) REMOVD AND REPLACED LOWER FRAME SECTOR AT FS 349 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-42-13. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. NO WEIGHOct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163714None · gougedPAX DOOR HINGE (DOOR SIDE) LUGS GOUGED AND CHAFED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR HINGE DOOR SIDE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202163713None · corrodedPAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN FS320.163 AND FS338.963. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. NOOct 24, 2021 · N207PS · Cndair CL6002B19 · DoorsSDR SWIA202163712None · corrodedFS 589 FRAME IS CORRODED FROM 25L TO 26R IN SEVERAL LOCATIONS BOTTOM END OF FRAME AND FLANGE (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FS 589 FRAME LOWER SEGMENT IAW CRJ 200 SRM 51-42-21 AND 51-42-06. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATOct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163711None · corrodedPAX DOOR AFT FORMER AT FS347.27 CORRODED IN SEVERAL LOCATIONS. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER @ FS 327.27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. Oct 24, 2021 · N207PS · Cndair CL6002B19 · DoorsSDR SWIA202163710None · corrodedPAX DOOR FWD FORMER AT FS311.75 CORRODED IN SEVERAL LOCATIONS. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER @ FS 311.75 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. Oct 24, 2021 · N207PS · Cndair CL6002B19 · Doors
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