# Service difficulty reports: N207PS

A list on [N207PS](https://openairdocs.org/aircraft/N207PS.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 160 reports

- [SDR SWIA2026101177594](https://openairdocs.org/sdr/SWIA2026101177594.md): Proximity Sensor · false indication · Oct 11, 2026 · N207PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > UPON 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 32-6
- [SDR SWIA2026031176883](https://openairdocs.org/sdr/SWIA2026031176883.md): Skin · cracked · Mar 11, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CRACK 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-.
- [SDR SWIA2026030776886](https://openairdocs.org/sdr/SWIA2026030776886.md): Skin · worn · Mar 7, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN PANEL AT BS 550, LBL47 WORN. REPAIRED THE LT APRON SKIN PANEL BTWN BS 516.85 - 559 IAW REO 601R-53-41-3423, REV -.
- [SDR SWIA2026030776881](https://openairdocs.org/sdr/SWIA2026030776881.md): Skin · worn · Mar 7, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN 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,
- [SDR SWIA2026030376885](https://openairdocs.org/sdr/SWIA2026030376885.md): Skin · dented · Mar 3, 2026 · N207PS · Cndair CL6002B19 · Trailing Edge Flaps
  > LOWER 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.
- [SDR SWIA2026022476884](https://openairdocs.org/sdr/SWIA2026022476884.md): Skin · cracked · Feb 24, 2026 · N207PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN 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.
- [SDR SWIA2026020576882](https://openairdocs.org/sdr/SWIA2026020576882.md): Skin · dented · Feb 5, 2026 · N207PS · Cndair CL6002B19 · Wing, Plate/Skin
  > DENT 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 S
- [SDR SWIA20250512001](https://openairdocs.org/sdr/SWIA20250512001.md): Warning Message · false activation · May 5, 2025 · N207PS · Cndair CL6002B19 · Door Warning System
  > SERVICE 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." (FLIGH
- [SDR SWIA202505060005](https://openairdocs.org/sdr/SWIA202505060005.md): Door · warning message · May 5, 2025 · N207PS · Cndair CL6002B19 · Door Warning System
  > SERVICE 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." (FLIGHT
- [SDR SWIA2025040300314](https://openairdocs.org/sdr/SWIA2025040300314.md): Skin · dented · Mar 14, 2025 · N207PS · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND 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 BET
- [SDR SWIA2025040300010](https://openairdocs.org/sdr/SWIA2025040300010.md): Hinge · gouged · Mar 10, 2025 · N207PS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX 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-53-2
- [SDR SWIA202504030006](https://openairdocs.org/sdr/SWIA202504030006.md): Angle · corroded · Mar 6, 2025 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX 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 51-4
- [SDR SWIA202504030004](https://openairdocs.org/sdr/SWIA202504030004.md): Intercostal · cracked · Mar 4, 2025 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT 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 2008
- [SDR SWI2025F00062](https://openairdocs.org/sdr/SWI2025F00062.md): Window · failed · Jan 14, 2025 · N207PS · Cndair CL6002B19 · Flight Compartment Windows
  > CA 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 CONTROLL
- [SDR SWIA20231229008](https://openairdocs.org/sdr/SWIA20231229008.md): Unknown · warning message · Dec 28, 2023 · N207PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > L 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 CHE
- [SDR SWIA2023101900117](https://openairdocs.org/sdr/SWIA2023101900117.md): Unknown · warning message · Oct 17, 2023 · N207PS · Cndair CL6002B19 · Landing Gear System
  > AFTER 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)
- [SDR SWIA2023101800017](https://openairdocs.org/sdr/SWIA2023101800017.md): Unknown · warning message · Oct 17, 2023 · N207PS · Cndair CL6002B19 · Landing Gear System
  > AFTER 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)
- [SDR SWIA202266459](https://openairdocs.org/sdr/SWIA202266459.md): None · dented · Sep 11, 2022 · N207PS · Cndair CL6002B19 · Aileron Tabs
  > LHOB 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 TIME
- [SDR SWIA202163729](https://openairdocs.org/sdr/SWIA202163729.md): None · mislocated · Dec 5, 2021 · N207PS · Cndair CL6002B19 · Horizontal Stabilizer, Tab Structure
  > L/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 R
- [SDR SWIA202163728](https://openairdocs.org/sdr/SWIA202163728.md): None · dented · Nov 30, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND 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
- [SDR SWIA202163727](https://openairdocs.org/sdr/SWIA202163727.md): None · damaged · Nov 17, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > F.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 SPL
- [SDR SWIA202163737](https://openairdocs.org/sdr/SWIA202163737.md): None · corroded · Nov 14, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > CORROSION 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
- [SDR SWIA202163726](https://openairdocs.org/sdr/SWIA202163726.md): None · dented · Nov 13, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > DISCREPANCY 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 DISP
- [SDR SWIA202163736](https://openairdocs.org/sdr/SWIA202163736.md): Bracket · cracked · Nov 7, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LHS 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 51-42-21
- [SDR SWIA202163735](https://openairdocs.org/sdr/SWIA202163735.md): None · cracked · Nov 7, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LHS 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 PERF
- [SDR SWIA202163749](https://openairdocs.org/sdr/SWIA202163749.md): None · cracked · Nov 3, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 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 PERFORMED
- [SDR SWIA202163748](https://openairdocs.org/sdr/SWIA202163748.md): None · cracked · Nov 3, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 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 PERFORMED
- [SDR SWIA202163725](https://openairdocs.org/sdr/SWIA202163725.md): None · damaged · Nov 2, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > RH 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 -- DATE
- [SDR SWIA202163724](https://openairdocs.org/sdr/SWIA202163724.md): None · chafed · Nov 2, 2021 · N207PS · Cndair CL6002B19 · Wing Structure
  > RH 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 AT
- [SDR SWIA202163747](https://openairdocs.org/sdr/SWIA202163747.md): None · corroded · Oct 26, 2021 · N207PS · Cndair CL6002B19 · Doors
  > PAX 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 CONTINUAT
- [SDR SWIA202163723](https://openairdocs.org/sdr/SWIA202163723.md): None · cracked · Oct 26, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE 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 FOR
- [SDR SWIA202163750](https://openairdocs.org/sdr/SWIA202163750.md): Washer · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Galley Doors
  > SERVICE 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 SERVIC
- [SDR SWIA202163734](https://openairdocs.org/sdr/SWIA202163734.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR 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 53-01-11-400-802
- [SDR SWIA202163733](https://openairdocs.org/sdr/SWIA202163733.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR 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 53-01-11-400-802
- [SDR SWIA202163732](https://openairdocs.org/sdr/SWIA202163732.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR 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.
- [SDR SWIA202163731](https://openairdocs.org/sdr/SWIA202163731.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR 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 53-01-11-400-802
- [SDR SWIA202163730](https://openairdocs.org/sdr/SWIA202163730.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > FLOOR 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 53-01-11-400-802
- [SDR SWIA202163722](https://openairdocs.org/sdr/SWIA202163722.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR 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 A
- [SDR SWIA202163721](https://openairdocs.org/sdr/SWIA202163721.md): None · cracked · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR 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 BOMBAR
- [SDR SWIA202163720](https://openairdocs.org/sdr/SWIA202163720.md): None · cracked · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR 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-53-11-17
- [SDR SWIA202163719](https://openairdocs.org/sdr/SWIA202163719.md): Angle · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR 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, 51-42-06
- [SDR SWIA202163718](https://openairdocs.org/sdr/SWIA202163718.md): None · cracked · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FLOOR 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-
- [SDR SWIA202163717](https://openairdocs.org/sdr/SWIA202163717.md): None · corroded · Oct 25, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > BEAM 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 BALANCE
- [SDR SWIA202163716](https://openairdocs.org/sdr/SWIA202163716.md): Angle · corroded · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 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 WEIGH
- [SDR SWIA202163715](https://openairdocs.org/sdr/SWIA202163715.md): None · corroded · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 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 WEIGH
- [SDR SWIA202163714](https://openairdocs.org/sdr/SWIA202163714.md): None · gouged · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > PAX 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.
- [SDR SWIA202163713](https://openairdocs.org/sdr/SWIA202163713.md): None · corroded · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Doors
  > PAX 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. NO
- [SDR SWIA202163712](https://openairdocs.org/sdr/SWIA202163712.md): None · corroded · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 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 AT
- [SDR SWIA202163711](https://openairdocs.org/sdr/SWIA202163711.md): None · corroded · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Doors
  > PAX 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.
- [SDR SWIA202163710](https://openairdocs.org/sdr/SWIA202163710.md): None · corroded · Oct 24, 2021 · N207PS · Cndair CL6002B19 · Doors
  > PAX 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.

Next page: https://openairdocs.org/aircraft/N207PS/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N207PS/reports

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