# Service difficulty reports: N936SW

A list on [N936SW](https://openairdocs.org/aircraft/N936SW.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 · 209 reports

- [SDR SWIA2026100877551](https://openairdocs.org/sdr/SWIA2026100877551.md): Windshield · cracked · Oct 8, 2026 · N936SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT WINDSHIELD IS CRACKED. REMOVED AND REPLACED RT WINDSHIELD IAW TASK CARD 56-220-1000-SKY PERFORMED OPERATIONAL TEST OF RT WINDSHIELD HEAT, OPS CHECK GOOD AT THIS TIME NO LEAKS NOTED.
- [SDR SWIA2026092377329](https://openairdocs.org/sdr/SWIA2026092377329.md): Skin · dented · Sep 23, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT APPROXIMATELY 3 INCHES AFT AIRCRAFT RT KIDNEY PANEL. REPAIRED, BLENDED SCRATCH DAMAGE TO FUSELAGE SKIN PANEL BETWEEN BS 235 - 250, STR 20R IAW REO 601R-53-11-4100, REV-.
- [SDR SWIA2026082477331](https://openairdocs.org/sdr/SWIA2026082477331.md): Landing · dented · Aug 24, 2026 · N936SW · Cndair CL6002B19 · Elevator Miscellaneous Structure
  > LEFT ELEVATOR, LEADING EDGE NUTPLATE LANDING, UNDER PANEL 334AB IS DENTED. REPAIRED DAMAGE TO THE LT ELEVATOR FRONT SPAR LOWER FLANGE IAW REO 601R-51-00-309 REV B.
- [SDR SWIA2026061377309](https://openairdocs.org/sdr/SWIA2026061377309.md): Rib · mislocated · Jun 13, 2026 · N936SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > MISLOCATED LT WING BOX RIB ANGLE AT WS 4830. REMOVED AND REPLACED LT WING BOX BATT-RIB ANGLE IAW DWG 600-10204 REV M AND SRM 51-42-06.
- [SDR SWIA2026060177290](https://openairdocs.org/sdr/SWIA2026060177290.md): Skin · corroded · Jun 1, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING AAI AUDIT IT WAS FOUND THAT THERE IS POSSIBLE CORROSION AROUND THE LOWER SIDE OF THE AFT LAVATORY SERVICING POINT. REPAIRED AROUND THE LOWER SIDE OF THE AFT LAVATORY SERVICING POINT IAW REO 601R-53-51-748 REV -. PERFORMED DISPOSITIONS 1 TO 5, ENSU
- [SDR SWIA2026052877307](https://openairdocs.org/sdr/SWIA2026052877307.md): Former · corroded · May 28, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR, FWD SUPPORT ANGLE FOUND EXFOLIATED CORROSION ON FWD FORMER. REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV N, PRESSURE LEAK WAS GOOD
- [SDR SWIA2026052677293](https://openairdocs.org/sdr/SWIA2026052677293.md): Support Angle · chafed · May 26, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF PAX DOOR FWD PULL IN LEVER FOUND DEEP CHAFE ON ANGLE SUPPORT. REMOVED AND INSTALLED NEW PAX DOOR FWD ANGLE SUPPORT IAW SRM 51-42-06, SRM 51-42-21, & DWG 601R31702, REV N, PRESSURE LEAK CHECK WAS GOOD. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA2026051977322](https://openairdocs.org/sdr/SWIA2026051977322.md): Intercostal · out of limits · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND PREVIOUSLY PLUG REPAIR ON AFT DD4 INTERCOSTAL REQUIRED REPLACEMENT. INSTALLED NEW INTERCOSTAL AFT DD4 ON PAX DOOR IAW SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECKED GOOD.
- [SDR SWIA2026051977321](https://openairdocs.org/sdr/SWIA2026051977321.md): Intercostal · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON MID DD4 INTERCOSTAL MX 32285045 C-CHECK RO 9262026REPLACED WITH NEW PAX DOOR MID DD4 INTERCOSTAL AND NEW CLEAT IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV N COMPLIED WITH WIT
- [SDR SWIA2026051977318](https://openairdocs.org/sdr/SWIA2026051977318.md): Intercostal · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON MID DD1 INTERCOSTAL. EVALUATED LIMITS PAX DOOR MID DD1 INTERCOSTAL HAS EXFOLIATED CORROSION ON 2 ELEMENT OUT OF LIMITS IAW SRM 52-00-00. INSTALLED A NEW PAX DOOR MID DD1 INTERCOSTAL IAW SRM 51-42-06, SRM
- [SDR SWIA2026051977316](https://openairdocs.org/sdr/SWIA2026051977316.md): Intercostal · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON FWD DD3 INTERCOSTAL. PAX DOOR FWD DD3 INTERCOSTAL HAS EXFOLIATED CORROSION ON 2 ELEMENT OUT OF LIMITS IAW SRM 52-00-00. REPLACE INTERCOSTAL INSTALLED NEW PAX DOOR INTERCOSTAL IAW SRM 51-42-06 AND DWG 601
- [SDR SWIA2026051977313](https://openairdocs.org/sdr/SWIA2026051977313.md): Intercostal · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON AFT DD6 INTERCOSTAL. PAX DOOR AFT DD6 INTERCOSTAL HAS EXFOLIATED CORROSION ON 2 ELEMENT OUT OF LIMITS IAW SRM 52-00-00. REMOVED INTERCOSTAL IAW SRM 51-42-06. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06 AND
- [SDR SWIA2026051977312](https://openairdocs.org/sdr/SWIA2026051977312.md): Intercostal · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON MID DD3 INTERCOSTAL. REMOVED AND INSTALLED NEW PAX DOOR MID DD3 INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31702 REV N, LEAK CHECK WAS GOOD,
- [SDR SWIA2026051977311](https://openairdocs.org/sdr/SWIA2026051977311.md): Skin · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON FRAME AT FS 31356. REMOVED AND INSTALLED NEW CLEAT AND NEW FRAME AT FS 31356 IAW SRM 51-42-06 AND DWG 601R31702 REV N, PRESSURE LEAK CHECK WAS GOOD.
- [SDR SWIA2026051977310](https://openairdocs.org/sdr/SWIA2026051977310.md): Skin · corroded · May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND CORROSION ON AFT DD5 INTERCOSTAL. PAX DOOR AFT DD5 INTERCOSTAL HAS EXFOLIATED CORROSION ON 2 ELEMENT OUT OF LIMITS IAW SRM 52-00-00DRILLED AND LOCATED NEW AFT DD5 INTERCOSTAL IAW SRM 51-42-06 AND DWG 601R31702 REV N
- [SDR SWIA2026051877327](https://openairdocs.org/sdr/SWIA2026051877327.md): Intercostal · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON AFT DD7 INTERCOSTAL. REMOVED AND INSTALLED NEW INTERCOSTAL AFT DD7 IAW SRM 51-42-06 AND DWG 601R31702, REV N. PRESSURE LEAK CHKD GOOD.
- [SDR SWIA2026051877324](https://openairdocs.org/sdr/SWIA2026051877324.md): Intercostal · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON FWD DD1 INTERCOSTAL. CW NDT INSP IAW NDTM PT1 51-20-06, FOUND CRACKED. INSTALLED NEW PAX DOOR FWD DD1 INTERCOSTAL IAW SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECKED GOOD.
- [SDR SWIA2026051877323](https://openairdocs.org/sdr/SWIA2026051877323.md): Intercostal · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON AFT DD1A INTERCOSTAL. CW NDT INSP IAW NDTM PT1 51-20-06 INSTALLED NEW PAX DOOR AFT DD1A INTERCOSTAL IAW SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECKED GOOD.
- [SDR SWIA2026051877317](https://openairdocs.org/sdr/SWIA2026051877317.md): Intercostal · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON FWD DD7 INTERCOSTAL. REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL FWD DD7, IAW SRM 51-42-06, AND DWG 601R31702, REV N, PRESSURE LEAK CHKD GOOD.
- [SDR SWIA2026051877314](https://openairdocs.org/sdr/SWIA2026051877314.md): Intercostal · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON AFT DD1 INTERCOSTAL. REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL IAW SRM 51-42-06 AND DWG 601R31702, REV N, PRESSURE LEAK CHECKED GOOD.
- [SDR SWIA2026051877308](https://openairdocs.org/sdr/SWIA2026051877308.md): Doubler · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON AFT PULL IN CAM DOUBLER. REMOVED AND INSTALLED PAX DOOR AFT PULL IN CAM DOUBLER REF SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702 -REV N,
- [SDR SWIA2026051877292](https://openairdocs.org/sdr/SWIA2026051877292.md): Former · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF PAX DOOR INNER SKIN FOUND SUSPECTED CRACK ON AFT FORMER. REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER IAW SRM 51-42-06, SRM 51-42-21, & DWG 601R31702, REV N, COMPLIED WITH 51-900-1003-SKY, PERFORMED PAX DOOR PRESSURIZATION LEAK CHECK IAW AMM
- [SDR SWIA2026051877285](https://openairdocs.org/sdr/SWIA2026051877285.md): Doubler · cracked · May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF THE PAX DOOR INNER SKIN, FOUND SUSPECTED CRACK ON THE FWD PULL IN CAM DOUBLER. REMOVED AND INSTALLED A NEW PAX DOOR FWD PULL IN CAM DOUBLER IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702 REV N.
- [SDR SWIA2026051777306](https://openairdocs.org/sdr/SWIA2026051777306.md): Trunnion · gouged · May 17, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RH SIDE AFT TRUNNION HAS GOUGE MARKS ON FWD FACE. REPAIRED GOUGE DAMAGE TO THE MLG TRUNNION FITTING NEAR AFT LUG BORE, RT IAW REO 601R-57-21-4093, REV -.
- [SDR SWIA2026051777296](https://openairdocs.org/sdr/SWIA2026051777296.md): Hinge Fitting · damaged · May 17, 2026 · N936SW · Cndair CL6002B19 · Elevator Structure
  > DURING REMOVAL OF BEARING ON RT ELEVATOR INBD HINGE FITTING. FOUND BEARING BORES TO BE PITTED, REQUIRING REPLACEMENT. REMOVED AND REPLACED THE RT ELEVATOR HINGE FITTING ASSY IAW DWG 600-24025, REV R.
- [SDR SWIA2026051677328](https://openairdocs.org/sdr/SWIA2026051677328.md): Floorbeam · corroded · May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 613, RBL 9, WAS CORRODED, BLENDED CORROSION TO A SMOOTH CONTOUR IAW SRM 51-21-06, AND COMPLIED WITH ALL DISPOSITION INSTRUCTION OUTLINED IN REO 601R-53-61-8544, REV-.
- [SDR SWIA2026051677325](https://openairdocs.org/sdr/SWIA2026051677325.md): Hinge Fitting · corroded · May 16, 2026 · N936SW · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL ON, FOUND LT ELEVATOR LE HINGE FITTING ASSY TO HAVE PITTING CORROSION IN BEARING BORES ON BOTH HINGE HALVES REPLACE HINGE FITTING ASSY. INSTALLED 1 EA NEW LE HINGE FITTING ASSY ON LT ELEVATOR IAW DWG 601R24025, REV-G, SRM 51-42-06, AND SRM 51-
- [SDR SWIA2026051677319](https://openairdocs.org/sdr/SWIA2026051677319.md): Skin · dented · May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THERE WAS A DENT BELOW THE AFT CARGO DOOR SCUFF PLATE APPROX BS 605. REPAIRED THE SKIN BELOW THE AFT CARGO DOOR SCUFF PLATE IAW REO 601R-53-61-8549, REV -. PERFORMED PRESSURIZED LEAK CHECK OF THE SCUFF PLATE, LEAK CHECKED GOOD.
- [SDR SWIA2026051677301](https://openairdocs.org/sdr/SWIA2026051677301.md): Lug · gouged · May 16, 2026 · N936SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LEFT INBD FLAP, INBD HINGE ARM, FWD LOWER HINGE LUG GOUGED. REWORKED AND RESTORED GOUGED DAMAGED AREA AT LT INBD FLAP, INBD HINGE ARM, FWD LOWER HINGE LUG. COMPLIED WITH STEPS 1-6 OF REO 601R-57-54-403, REV-.
- [SDR SWIA2026051677299](https://openairdocs.org/sdr/SWIA2026051677299.md): Seat Track · damaged · May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, BS 559.203 RBL 9, BENT, CRACKED & CORRODED AT BS 559.72 AREA. BLENDED THE CORROSION TO A SMOOTH CONTOUR IAW SRM 51-21-06 AND EVALUATED THE SEAT TRACK NOMINAL THICKNESS FLANGE AREA 0050 IAW CMS 6830, REV-. BLEND DIMENSIONS, L27 W 500 CURRENT THICK
- [SDR SWIA2026051677295](https://openairdocs.org/sdr/SWIA2026051677295.md): Support Angle · cracked · May 16, 2026 · N936SW · Cndair CL6002B19 · Aerodynamic Fairings
  > PANEL 161DL SUPPORT ANGLE CRACKED AT APPROXIMATELY BS 476. REMOVED AND INSTALLED A NEW PANEL 161DL SUPPORT ANGLE, BRACKET (PN 601R31037-33) IAW DWG 601R31037, REV F, SRM 51-41-02, SRM 51-42-06, SRM 51-42-10, AND AMM 20-21-00-910-801.
- [SDR SWIA2026051677286](https://openairdocs.org/sdr/SWIA2026051677286.md): Floor Support · corroded · May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT, BS 574 - 621, LBL 27, WAS CORRODED, REMOVED CORROSION FROM FLOOR SUPPORT IAW SRM 51-21-06 AND COMPLIED WITH ALL STEPS 1-6 OF REO 601R-53-61-8543, REV -.
- [SDR SWIA2026051577333](https://openairdocs.org/sdr/SWIA2026051577333.md): Rib · cracked · May 15, 2026 · N936SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LH BATT RIB CANON PLUG DOUBLER AT APPROX WS 5850 FOUND TO BE CRACKED. REMOVED AND REPLACED LT WING BATT-RIB AND ELECTRICAL CONNECTOR DOUBLER IAW DWG 601R10203, REV G, AND SRM 51-42-06 AND 51-42-21.
- [SDR SWIA2026051577332](https://openairdocs.org/sdr/SWIA2026051577332.md): Floor Support · damaged · May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR, RIGHT SUPPORT HAD CORROSION AND TOOLING MARKS AT VARIOUS AREAS. REMOVED CORROSION AND TOOL MARKS ON PRESSURE FLOOR RT SUPPORT FROM BS 409.128 TO 559 IAW SRM 51-21-06 AND SRM 51-12-00 AND REO 601R-53-41-666, REV -C.
- [SDR SWIA2026051577315](https://openairdocs.org/sdr/SWIA2026051577315.md): Skin · dented · May 15, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER SKIN OUTBOARD OF DOOR HINGE CENTER OF SKIN HAS DENT. REMOVED AND INSTALLED CENTER SEAL RETAINER IAW SRM 51-42-06, AND DWG 601R31702, REV -N, PERFORMED PAX DOOR PRESSURIZATION LEAK CHECK IAW AMM 21-32-00-863-801, LEAK CHKD GOOD, NO LEAK NOTED.
- [SDR SWIA2026051577305](https://openairdocs.org/sdr/SWIA2026051577305.md): Support · corroded · May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR, LEFT SUPPORT HAD CORROSION AND TOOLING MARKS IN VARIOUS AREAS, REMOVED CORROSION AND TOOL MARKS ON PRESSURE FLOOR LEFT SUPPORT FROM BS 409 TO 559 IAW SRM 51-21-06, & SRM 51-12-00. EVALUATED ALL THE BLENDS WITH-IN LIMITS IAW REO 601R-53-41-666
- [SDR SWIA2026051577304](https://openairdocs.org/sdr/SWIA2026051577304.md): Fitting · worn · May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR CUTOUT AFT CAM FITTING WORN. REMOVED AND INSTALLED A NEW CAM FITTING IAW SRM 51-42-21-00 AND DWG 600-31900, REV K. PAX DOOR OP TESTED GOOD.
- [SDR SWIA2026051577302](https://openairdocs.org/sdr/SWIA2026051577302.md): Fitting · worn · May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR CUTOUT FORWARD CAM FITTING WORN. REMOVED AND INSTALLED A NEW FITTING ON PASSENGER DOOR CUTOUT FORWARD IAW DWG 601R31900, REV F, AND SRM 51-42-21, REV 39. OP TESTED GOOD.
- [SDR SWIA2026051577297](https://openairdocs.org/sdr/SWIA2026051577297.md): Door Sill · corroded · May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR OPENING, LOWER SILL ANGLE HAD MULTIPLE SPOTS OF CORROSION BTWN BS 310 - 349. INSTALLED NEW LOWER SILL ANGLE IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-13, AND DWG 601R31527, REV AM, OPS TEST OF THE PAX DOOR WARNING SYSTEM WAS GOOD.
- [SDR SWIA2026051477294](https://openairdocs.org/sdr/SWIA2026051477294.md): Hinge · damaged · May 14, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE FUSELAGE SIDE FWD AND AFT LUGS INNER SURFACE ARE ELONGATED OUT OF LIMITS REQUIRE REPLACEMENT. REMOVED PAX DOOR PIANO HINGE FUSELAGE SIDE IAW SRM 53-21-23 4 PROCEDURE A, B, C. INSTALLED A NEW PAX DOOR PIANO HINGE FUSELAGE SIDE IAW 53-21-2
- [SDR SWIA2026051377298](https://openairdocs.org/sdr/SWIA2026051377298.md): Mount · gouged · May 13, 2026 · N936SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > RIGHT WING HINGE BOX AT WS 178 WAS GOUGED ON AFT WING MOUNT FITTING. BLENDED DAMAGE TO A SMOOTH CONTOUR AT RT WING HINGE BOX AT WS 178 AFT WING MOUNT FITTING AND REPAIRED IN COMPLIANCE WITH STEPS 1-5 OF REO 601R-57-21-4095, REV -.
- [SDR SWIA2026051277303](https://openairdocs.org/sdr/SWIA2026051277303.md): Bracket · cracked · May 12, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOTS SIDE WINDSHIELD SIDE POST LWR OTBD BRACKET CRACKED. REMOVED PILOTS SIDE WINDSHIELD SIDE POST LWR OTBD BRACKET IAW SRM 51-42-21-00 AND INSTALLED NEW PILOTSSIDE WINDSHIELD SIDE POST LWR OTBD BRACKET IAW SRM 51-42-21-00, AND DWG 601R33007, REV U.
- [SDR SWIA2026051177300](https://openairdocs.org/sdr/SWIA2026051177300.md): Bracket · cracked · May 11, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOTS SIDE WINDSHIELD CENTER POST LWR BRACKET CRACKED. REMOVED & REPLACED THE PILOTS SIDE WINDSHIELD CENTER POST LWR BRACKET IAW SRM 51-42-21-00, & DWG 601R33007, REV U.
- [SDR SWIA2026050977288](https://openairdocs.org/sdr/SWIA2026050977288.md): Skin · damaged · May 9, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LEFT APRON SKIN PANEL ASSY HAD CHAFE AND GOUGE DAMAGE. REPAIRED THE APRON ASSY SKIN PANEL, IAW REO 601R-53-41-3446, REV-.
- [SDR SWIA2026050677287](https://openairdocs.org/sdr/SWIA2026050677287.md): Window Post · cracked · May 6, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK NOTED, LT WINDSHIELD SIDE POST SUPPORT FRAME SECTOR AT BS 235. VERIFIED CRACK AT THE LEFT WINDSHIELD SIDE POST. REPLACED THE POST IAW SRM 51-42-06-00, AND DWG 601R34032, REV V. PRESSURE CHECKED GOOD.
- [SDR SWIA2026043077330](https://openairdocs.org/sdr/SWIA2026043077330.md): Skin · eroded · Apr 30, 2026 · N936SW · Cndair CL6002B19 · Trailing Edge Flaps
  > EROSION NOTED AT LT INBD, FLAP LOWER SKIN BETWEEN FLS 50-59 AND FLS 78-85. REPAIRED THE INBD FLAP LOWER SKIN BETWEEN FLS 50498 - FLS 74-718, LT IAW REO 601R-57-52-2563 -.
- [SDR SWIA2026043077326](https://openairdocs.org/sdr/SWIA2026043077326.md): Skin · dented · Apr 30, 2026 · N936SW · Cndair CL6002B19 · Trailing Edge Flaps
  > DENT NOTED ON LT INBD FLAP LOWER SKIN AT APPROX FLS 71-72 AND 15 INCHES FROM TE. INSTALLED REPAIR DOUBLER AND APPLIED AERODYNAMIC SEALANT AT LT INBD FLAP LOWER SKIN IAW REO 601R-57-52-678, REV-C.
- [SDR SWIA2026043077289](https://openairdocs.org/sdr/SWIA2026043077289.md): Vane · eroded · Apr 30, 2026 · N936SW · Cndair CL6002B19 · Trailing Edge Flaps
  > EROSION NOTED ON THE LT INBD FLAP VANE LOWER SKIN AT FLS 50 - 59 AND FLS 78 - 85. THE LT INBD FLAP WAS REPLACED ON HN 310594, MX TRANS 32170861. NO FURTHER ACTION REQUIRED AT THIS TIME
- [SDR SWIA2026041677320](https://openairdocs.org/sdr/SWIA2026041677320.md): Pressure Blkhd · cracked · Apr 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IAW AWL 53-61-153 OF TR 2B-2187, TO APPENDIX BAIRWORTHINESS LIMITATIONS, OF PART 2 OF THE MRM J2, MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPEC
- [SDR SWIA2026041677291](https://openairdocs.org/sdr/SWIA2026041677291.md): Trunnion · cracked · Apr 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE RA18382-601R-57-21-1703-PR. COMPLY WITH PERMANENT REPAIR ON RA ID 183824. FASTNER HOLES IN LT MLG TRUNNION ARE CRACKED. REPAIRED IAW REO 601R-57-21-1703, REV -. REPLACED THE LT TRUNNION MLG AND STEEL STRAP POST SB 60

Next page: https://openairdocs.org/aircraft/N936SW/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 = 'N936SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N936SW/reports

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