# Service difficulty reports: N912SW

A list on [N912SW](https://openairdocs.org/aircraft/N912SW.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 5 · 232 reports

- [SDR SWIA20230914002](https://openairdocs.org/sdr/SWIA20230914002.md): Unknown · cracked · Sep 12, 2023 · N912SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT WINDOW IN FLIGHT DECK CRACKED WHILE CLIMBING THRU FL270. (FLIGHT 5697 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27153739 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED RH SIDE WINDOW IN REFERENCE TO CRJ200 AMM 56-12-
- [SDR SWIA2023091300002](https://openairdocs.org/sdr/SWIA2023091300002.md): Unknown · cracked · Sep 12, 2023 · N912SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT WINDOW IN FLIGHT DECK CRACKED WHILE CLIMBING THRU FL270. (FLIGHT 5697 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGESS
- [SDR SWIA202157962](https://openairdocs.org/sdr/SWIA202157962.md): Frame · damaged · Mar 30, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Frame
  > RH FRAME AT APPROX. F.S 409+80 REQUIRES CUT AND SPLICE REPAIR AT STG14R FOR ACCESS (REQUIRED FOR STRINGER 17R REPAIR) (C-CHECK RO 5/3/2021) CUT THE FRAME AND FABRICATED AND INSTALLED THE FRAME REPAIR AT THE FS 409+80 FRAME SECTION FROM STR 14R TO STR 20
- [SDR SWIA202157961](https://openairdocs.org/sdr/SWIA202157961.md): Angle · corroded · Mar 27, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CLIP (PN 601R318824-1) COMMON TO PAX DOOR INTERCOSTAL DD7 HAS CORROSION (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR CLIP P/N# 601R318824-1 COMMON TO INTERCOSTAL DD7 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.-N.
- [SDR SWIA202157960](https://openairdocs.org/sdr/SWIA202157960.md): Cleat · corroded · Mar 27, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CLEAT (PN 600-31902-269) COMMON TO PAX DOOR INTERCOSTAL DD6 HAS CORROSION DAMAGE (C-CHECK RO 5/3/2021) REMOVED AND REPLACED THE CLEAT (PN 600-31902-269) COMMON TO PAX DOOR INTERCOSTAL DD6 REF BOMBARDIER DRAWING 601R31702 REV -N & SRM 51-42-06. COMPLIED
- [SDR SWIA202157959](https://openairdocs.org/sdr/SWIA202157959.md): Bracket · corroded · Mar 27, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > BRACKET (PN 601R318084-1) COMMON TO PAX DOOR INTERCOSTAL DD6 HAS CORROSION DAMAGE (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR BRACKET P/N# 601R318084-1 COMMON TO INTERCOSTAL DD6 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R317
- [SDR SWIA202157958](https://openairdocs.org/sdr/SWIA202157958.md): Intercostal · corroded · Mar 26, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND CORROSION ON PAX DOOR INTERCOSTAL DD7A (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD7A REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.N. ALL CHECKS GOOD. / TASK CARD 51-900-1003-SKY COMPLIED WITH.
- [SDR SWIA202157957](https://openairdocs.org/sdr/SWIA202157957.md): Intercostal · corroded · Mar 26, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL DD7 P/N 601R318826-1 (C-CHECK RO 5/3/2021) REMOVED CORROSION ON PAX DOOR INTERCOSTAL DD7 P/N 601R318826-1. OUT OF LIMITS. / REPLACED PASSENGER DOOR INTERCOSTAL DD7 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702
- [SDR SWIA202157956](https://openairdocs.org/sdr/SWIA202157956.md): Post · defective · Mar 24, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Structure
  > F.S 409+128 BL 0.0 LH AFT VERTICAL POST RADIUS DEFECT NOTED. (C-CHECK RO 5/3/2021) INSTALLED NEW ANGLE AT FS409+ 128 BL0.00 LH AFT VERTICAL POST REF REO 601-53-41-889 REV D DATED 2018-10-04 AND CRJ SRM 51-42-06 & DWG NO: 601R32208 REV -T. / ALL CHECKS
- [SDR SWIA202157965](https://openairdocs.org/sdr/SWIA202157965.md): Windshield · cracked · Mar 23, 2021 · N912SW · Cndair CL6002B19 · Flight Compartment Windows
  > PILOT'S CENTER WINDSHIELD HAS MULTIPLE CRACKS TOWARDS THE INBD LOWER CENTER POST. (C-CHECK RO 5/3/2021) PILOTS CENTER WINDSHIELD REMOVE AND REPLACED REF CRJ200 AMM 56-11-01-000-801 AND 56-11-01-400-801, ALL CHECKS GOOD, SEE CONTINUE CARD FOR DETAIL / SK
- [SDR SWIA202157955](https://openairdocs.org/sdr/SWIA202157955.md): Former · corroded · Mar 22, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * PASSENGER DOOR FORMER 320.163 CORRODED (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FORMER AT FS320.163 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DRAWING# 601R31702 REV.N. COMPLIED WITH TASK CARD 51-900-1003-SKY. /
- [SDR SWIA202157954](https://openairdocs.org/sdr/SWIA202157954.md): Intercostal · corroded · Mar 22, 2021 · N912SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * PASSENGER DOOR INTERCOSTAL DD6 CORRODED (C-CHECK RO 5/3/2021) PASSENGER DOOR INTERCOSTAL DD6 BLENDED AND FOUD TO BE OUT OF LIMITS. / REMOVED & INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD6 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.
- [SDR SWIA202157953](https://openairdocs.org/sdr/SWIA202157953.md): Skin · dented · Mar 20, 2021 · N912SW · Cndair CL6002B19 · Leading Edge Devices
  > *DENT APPROX 9" AFT OF LEADING EDGE, ON THE OTBD OF PANEL 584AB, LH WING INBD FLAP. MARKED (C-CHECK RO 5/3/2021) REPAIRED DENT, PER MHIRJ REO 601R-57-52-2418 REV -- DATED 2021-04-13 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWIA202157974](https://openairdocs.org/sdr/SWIA202157974.md): Stop Fitting · corroded · Mar 18, 2021 · N912SW · Cndair CL6002B19 · Emergency Exits
  > LEFT OVERWING EMERGENCY EXIT DOOR UPPER AFT STOP FITTING HAS CORRODED BOLTS (MARKED) (C-CHECK RO 5/3/2021) REPLACED CORRODED BOLTS LEFT OVERWING EMERGENCY EXIT DOOR UPPER AFT STOP FITTING APPLIED CPP ON NEW BOLTS REF CRJ200 SRM 51-21-11-00 AND TORQUED
- [SDR SWIA202157972](https://openairdocs.org/sdr/SWIA202157972.md): Hinge · corroded · Mar 17, 2021 · N912SW · Cndair CL6002B19 · Spoilers
  > LH INBD GROUND SPOILER, OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED LH INBD GROUND SPOILER OTBD HINGE HARDWARE REF AMM 27-65-01-400-801. OPS TEST GOOD
- [SDR SWIA202157971](https://openairdocs.org/sdr/SWIA202157971.md): Hinge · corroded · Mar 17, 2021 · N912SW · Cndair CL6002B19 · Spoilers
  > * LH OTBD GROUND SPOILER, INBD AND OTBD HINGE HARDWARE IS CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED LH OUTBD GROUND SPOILER OUTBD HINGE ARM HARDWARE REF AMM 27-65-01-400-801. OPS TEST GOOD
- [SDR SWIA202157970](https://openairdocs.org/sdr/SWIA202157970.md): Hinge · corroded · Mar 17, 2021 · N912SW · Cndair CL6002B19 · Spoilers
  > * LH SPOILERON INBD AND OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED INBD AND OTBD L/H SPOILERON CORRODED HARDWARE WITH NEW HARDWARE REF CRJ200 AMM 27-64-01-000-801 AND 27-64-01-400-801. TUC 8615 CAL DUE DATE 10-31-21. OPS TES
- [SDR SWIA202157969](https://openairdocs.org/sdr/SWIA202157969.md): Seat Track · corroded · Mar 17, 2021 · N912SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * LH SIDE SEAT TRACK AT APPROXIMATELY FS499 €“ FS546 CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED LH SIDE SEAT TRACK AT APROXIMATELY FS499-FS546, REF. CRJ200 AMM 53-01-11-000-802 & AMM 53-01-11-400-802. CORROSION WAS FOUND OUT OF LIMITS. SEE CON
- [SDR SWIA202157968](https://openairdocs.org/sdr/SWIA202157968.md): Seat Track · corroded · Mar 17, 2021 · N912SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * LH SIDE SEAT TRACK CHANNEL AT APPROXIMATELY FS559+30 €“ FS559+80 CORRODED/GOUGED (C-CHECK RO 5/3/2021) REMOVED DAMAGE AT LH SIDE SEAT TRACK CHANNEL ATAPPROX FS559+30-FS559+80 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK CHANNEL REF. CRJ
- [SDR SWIA202157952](https://openairdocs.org/sdr/SWIA202157952.md): Hinge Box · corroded · Mar 17, 2021 · N912SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * LH INBD WING FLAPHINGE BOX, CENTER MOUND PLATE IS CORRODED. FLAGGED (C-CHECK RO 5/3/2021) BLENDED LH INBD FLAP HINGE BOX CENTER MOUNT PLATE, WITHIN LIMITS REF REO 601R-57-21-3453 REV -- DATE 2021-04-05. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202157951](https://openairdocs.org/sdr/SWIA202157951.md): Pressure Deck · corroded · Mar 15, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * SEVERAL AREAS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL FS409+128 €“ FS559 (MARKED) (C-CHECK RO 5/3/2021) REMOVED THE CORROSION ON RH PRESSURE FLOOR SILL PANEL AT 7 EACH LOCATIONS FROM FS409+128 TO FS559 REF REO 601R-53-41-666 REV -C DATED 2012-11
- [SDR SWIA202157950](https://openairdocs.org/sdr/SWIA202157950.md): Pressure Deck · corroded · Mar 15, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * SEVERAL AREAS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL FS409+128 €“ FS559 (MARKED) (C-CHECK RO 5/3/2021) REPAIRED LH PRESSURE FLOOR SILL PANEL FS409+128 €“ FS559 REF REO 601R-53-41-666 REV-C DATED 2012-11-06 & REO 601R-53-41-2897 REV -- DATE 202
- [SDR SWIA202157949](https://openairdocs.org/sdr/SWIA202157949.md): Skin · dented · Mar 14, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * FUSELAGE SKIN DENTED AND GOUGED AT APPROXIMATELY FS202 BETWEEEN RBL5 - RBL10 (C-CHECK RO 5/3/2021) REPAIRED FUSELAGE SKIN AT APPROXIMATELY FS202 BETWEEEN RBL5 - RBL10 REF REO 601R-53-11-3680 REV --, DATED 2021-04-19 ALL STEPS COMPLIED WITH. COMPLIED
- [SDR SWIA202157948](https://openairdocs.org/sdr/SWIA202157948.md): Lug · gouged · Mar 14, 2021 · N912SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * RH INBD FLAP, OTBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) COMPLIED WITH REO 601R-57-52-2414 REV -- DATE 2021-03-19 STEPS 1-4. ENSURED BLENDOUT OF GOUGE TO A SMOOTH CONTOUR USING (20:1 TRANSITION RATIO). ENSURED BLENDOUT DIMENSION ARE NOT MORE THA
- [SDR SWIA202157947](https://openairdocs.org/sdr/SWIA202157947.md): Lug · gouged · Mar 14, 2021 · N912SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * RH INBD FLAP, INBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) COMPLIED WITH REO 601R-57-52-2414 REV -- DATE 2021-03-19 STEPS1-4. ENSURED BLENDOUT OF GOUGE WAS PERFORMED TO A SMOOTH CONTOUR USING A (20:1 TRASITION RATIO). ENSURED BLENDOUT DIMENSION WE
- [SDR SWIA202157946](https://openairdocs.org/sdr/SWIA202157946.md): Lug · gouged · Mar 14, 2021 · N912SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * LH INBD FLAP, INBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) REPAIRED GOUGE ON LH INBD FLAP, INBD HINGE ARM LUG PER REO 601R-57-52-2413 REV -- DATED 2021-03-19 / COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202157945](https://openairdocs.org/sdr/SWIA202157945.md): Channel · dented · Mar 14, 2021 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * FS280 RBL9 CHANNEL DENTED AT APPROXIMATELY 3€? FROM UPPER SKIN & 2€? ABOVE FLOOR LEVEL (C-CHECK RO 5/3/2021) REPAIRED FS280 RBL 11 CHANNEL ( LOCATION CLARIFIED IN CONTINUATION) REF REO 601R-53-11-3679 REV-- DATED 2021-04-26. COMPLIED WITH SKYWEST
- [SDR SWIA202157944](https://openairdocs.org/sdr/SWIA202157944.md): Access Panel · corroded · Mar 13, 2021 · N912SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING ACCESS PANEL 640CT HOLE LIP HAS MULTIPLY PLACES OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 640CT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMP
- [SDR SWIA202157943](https://openairdocs.org/sdr/SWIA202157943.md): Access Panel · corroded · Mar 13, 2021 · N912SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING ACCESS PANEL 640BT HOLE LIP HAS MULTIPLY PLACES OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 640BT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMP
- [SDR SWIA202157942](https://openairdocs.org/sdr/SWIA202157942.md): Access Panel · corroded · Mar 13, 2021 · N912SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING ACCESS PANEL 640AT HOLE LIP HAS MULTIPLY PLACES OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 640AT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPL
- [SDR SWIA202157941](https://openairdocs.org/sdr/SWIA202157941.md): Access Panel · corroded · Mar 13, 2021 · N912SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING ACCESS PANEL 540CT HOLE LIP HAS MULTIPLY PLACE OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 540CT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPL
- [SDR SWIA202157940](https://openairdocs.org/sdr/SWIA202157940.md): Access Panel · corroded · Mar 13, 2021 · N912SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING ACCESS PANEL 540BT HOLE LIP HAS MULTIPLY PLACES OF CORRSION ON UPPER AND LOWER SURFACE AS MARKED. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 540BT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND CO
- [SDR SWIA202157939](https://openairdocs.org/sdr/SWIA202157939.md): Access Panel · corroded · Mar 13, 2021 · N912SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING ACCESS PANEL 540AT HOLE HAS MULTIPLY PLACES OF CORRSION ON UPPER AND LOWER SURFACE LIP. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 540AT LIP CRJ200 SRM 51-21-06. WITHIN LIMITS REF. REO 601R-57-21-3442 REV --, DATED:
- [SDR SWIA202157964](https://openairdocs.org/sdr/SWIA202157964.md): Stop Fitting · cracked · Mar 12, 2021 · N912SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR CLOSE STOP AND SWITCH BRACKET IS CRACKED AS MARKED. (C-CHECK RO 5/3/2021) SERVICE DOOR STOP BRACKET REMOVED AND REPLACED WITH NEW, REF CRJ 200 SRM 51-42-21. OPERATIONAL TEST OF THE SERVICE DOOR WARNING SYSTEM CHECKED GOOD. SEE CONTINUATIO
- [SDR SWIA202157963](https://openairdocs.org/sdr/SWIA202157963.md): Stop Fitting · cracked · Mar 12, 2021 · N912SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR FWD LOWER STOP BACKUP FITTING IS CRACKED AS MARKED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED SERVICE DOOR FWD LWR STOP FITTING WITH NEW. REF CRJ200 SRM 51-42-21
- [SDR SWIA202157938](https://openairdocs.org/sdr/SWIA202157938.md): Stop Fitting · gouged · Mar 12, 2021 · N912SW · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH RH FWD STOP FITTING IS GOUGED AS MARKED (C-CHECK RO 5/3/2021) BLENDED OUT GOUGE ON CREW ESCAP HATCH RH FWD STOP FITTING IAW REO 601R-52-22-043, REV. --, DATED 04/05/2021. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202157937](https://openairdocs.org/sdr/SWIA202157937.md): Stop Fitting · gouged · Mar 12, 2021 · N912SW · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH LH FWD STOP FITTING IS GOUGED AS MARKED (C-CHECK RO 5/3/2021) REPAIRED CREW ESCAPE HATCH LH FWD STOP FITTING, REF REO 601R-52-22-043 REV -- DATED 2021-04-05, CHECKS GOOD / C/W TASK CARD 51-900-1003-SKY
- [SDR SWIA202157936](https://openairdocs.org/sdr/SWIA202157936.md): Support Angle · corroded · Mar 11, 2021 · N912SW · Cndair CL6002B19 · Emergency Exits
  > LH EMER DOOR SUPPORT ANGLE UNDER COVER PLATE CORRODED (C-CHECK RO 5/3/2021) REMOVED CORROSION ON LH EMER DOOR SUPPORT ANGLE UNDER COVER PLATE, REF CRJ 200 SRM 51-21-06, THE LH EMER DOOR SUPPORT ANGLE UNDER COVER PLATE, ORIGINAL THICKNESS 0.040"" REF CR
- [SDR SWIA202157935](https://openairdocs.org/sdr/SWIA202157935.md): Housing · chafed · Mar 8, 2021 · N912SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > * AFT CARGO DOOR HANDLE HOUSING CHAFED (C-CHECK RO 5/3/2021) AFT CARGO DOOR HANDLE ASSEMBLY REPLACED REF CRJ200 SRM 51-42-21, DWG NO. CC670-38702 REV C, ALL CHECKS GOOD, SEE CONTINUE CARD FOR DETAIL / SKYCARD 51-900-1003-SKY COMPLIED WITH
- [SDR SWIA202157934](https://openairdocs.org/sdr/SWIA202157934.md): Skin · damaged · Mar 3, 2021 · N912SW · Cndair CL6002B19 · Rudder, Plate/Skin
  > CREASE FOUD ON TRAILING EDGE OF RUDDER MIDWAY UP. TWO DENTS FOUND ON LH RUDDER SURFACE AND ONE DENT ON RH RUDDER SURFACE. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICE/PROCEDURE
- [SDR SWIA202157933](https://openairdocs.org/sdr/SWIA202157933.md): Skin · dented · Mar 3, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS IN AREA BELOW AND BEHIND LOW PRESSURE AIR ACCESS DOOR. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICE/PROCEDURES. (C-CHECK RO 5/3/2021) CUT OUT DAMAGE AND
- [SDR SWIA202157932](https://openairdocs.org/sdr/SWIA202157932.md): Skin · cracked · Mar 3, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 588779: CRACK/PUNCTURE DAMAGE TO SIDE FUSELAGE SKIN (DWG 601R38321, 0.045" / THK IN CHEM MILL POCKET & 0.058" THK IN PAD UP AREA, REF) BETWEEN FS409.00+48 - FS409.00+64 / AND STR 16R - STR 18R (C-CHECK RO 5/3/2021) REMOVED TEMPORARY
- [SDR SWIA202156592](https://openairdocs.org/sdr/SWIA202156592.md): Skin · punctured · Feb 27, 2021 · N912SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PUNCTURE HOLE ON RIGHT SIDE OF FUSELAGE BETWEEN THE SERVICE DOOR AND WING. APPROXIMATELY 2 INCH BY 2 INCH HOLE. FLIGHT 5217 - FILED CLOSED INSPECTED AND FOUND CRACK/PUNCTURE DAMAGE TO SIDE FUSELAGE SKIN (DWG 601R38321, 0.045" / THK IN CHEM MILL POCKET &
- [SDR SWIA202054715](https://openairdocs.org/sdr/SWIA202054715.md): Flap · obstructed · Dec 24, 2020 · N912SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING APPROACH, TRIED TO EXTEND FLAPS AT 190KTS, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22038403 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH AD AND AMOC APPROVAL LETTER BY PERFO
- [SDR SWIA202053865](https://openairdocs.org/sdr/SWIA202053865.md): Channel · cracked · Oct 30, 2020 · N912SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK SUPPORT LOWER C? CHANNEL HAS A CRACK. C-CHECK RO 11/6/2020. REMOVED AND REPLACED WITH NEW C CHANNEL PN 601R35050-25, REF DWG, CRJ 200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA202053864](https://openairdocs.org/sdr/SWIA202053864.md): Floor Support · corroded · Oct 30, 2020 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM AT FS 409-409+16 LBL 9 COROSON IN TWO SPOTS ON INBOARD SIDE, MARKED. C-CHECK RO 11/6/2020. REMOVED CORROSION ON FLOOR BEAM AT LBL 9 BETWEEN FS 409-FS 409+16, INBOARD FLANGE AT 2 EA LOCATIONS IN SHADED ZONE, REF REO. REPAIRED PER REO. COMPLIED WIT
- [SDR SWIA202053863](https://openairdocs.org/sdr/SWIA202053863.md): Angle · cracked · Oct 29, 2020 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY, CLIP ON FS 625 AT APPROXIMATELY STR 14L APPEARS TO HAVE A CRACK. C-CHECK RO 11/6/2020. REMOVED AND REPLACED CLIP AT FS 625 STGR 14L, REF CRJ 200 SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053862](https://openairdocs.org/sdr/SWIA202053862.md): Angle · cracked · Oct 29, 2020 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY, CLIP ON FS 625 AT APPROXIMATELY STR 14R APPEARS TO HAVE A CRACK. C-CHECK RO 11/6/2020. REMOVED AND REPLACED CLIP AT FS 625 STGR 14R, REF CRJ 200 SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202053861](https://openairdocs.org/sdr/SWIA202053861.md): Vane · chafed · Oct 24, 2020 · N912SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 7" FROM OUTBOARD END. C-CHECK RO 11/6/2020. REMOVED AND REPLACED RT INBOARD FLAP VANE (OUTBOARD LEADING EDGE CAP), REF CRJ 200 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2019072346084](https://openairdocs.org/sdr/SWIA2019072346084.md): Warning System · activated · Jul 23, 2019 · N912SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > IN CLIMB RECEIVED A GEAR DISAGREE. RETURNED TO FIELD. GEAR EXTENDED NORMALLY. (FLT#5672) CLOSED DEFERRED LANDING GEAR EXTENSION RETRACTION SYSTEM IAW MEL.

Next page: https://openairdocs.org/aircraft/N912SW/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 = 'N912SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N912SW/reports

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