N936SW

Service difficulty reports · 209

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 = 'N936SW' 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 SWIA2026100877551Windshield · crackedRIGHT 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 .Oct 8, 2026 · N936SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA2026092377329Skin · dentedDENT 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-.Sep 23, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026082477331Landing · dentedLEFT 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.Aug 24, 2026 · N936SW · Cndair CL6002B19 · Elevator Miscellaneous StructureSDR SWIA2026061377309Rib · mislocatedMISLOCATED 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.Jun 13, 2026 · N936SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2026060177290Skin · corrodedDURING 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, ENSUJun 1, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026052877307Former · corrodedUPON 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 GOODMay 28, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026052677293Support Angle · chafedON 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.May 26, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977322Intercostal · out of limitsUPON 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.May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977321Intercostal · corrodedUPON 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 WITMay 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977318Intercostal · corrodedON 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 May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977316Intercostal · corrodedUPON 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 601May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977313Intercostal · corrodedON 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 May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977312Intercostal · corrodedUPON 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,May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977311Skin · corrodedUPON 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.May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051977310Skin · corrodedUPON 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 May 19, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877327Intercostal · crackedUPON 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.May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877324Intercostal · crackedUPON 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.May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877323Intercostal · crackedUPON 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.May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877317Intercostal · crackedON 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.May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877314Intercostal · crackedON 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.May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877308Doubler · crackedUPON 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,May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877292Former · crackedON 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 May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051877285Doubler · crackedON 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.May 18, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051777306Trunnion · gougedRH 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 -.May 17, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWIA2026051777296Hinge Fitting · damagedDURING 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.May 17, 2026 · N936SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2026051677328Floorbeam · corrodedFLOORBEAM, 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-.May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2026051677325Hinge Fitting · corrodedUPON 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-May 16, 2026 · N936SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2026051677319Skin · dentedTHERE 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.May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026051677301Lug · gougedLEFT 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-.May 16, 2026 · N936SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA2026051677299Seat Track · damagedSEAT 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 THICKMay 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2026051677295Support Angle · crackedPANEL 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.May 16, 2026 · N936SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA2026051677286Floor Support · corrodedFLOOR 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 -.May 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026051577333Rib · crackedLH 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.May 15, 2026 · N936SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2026051577332Floor Support · damagedPRESSURE 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.May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026051577315Skin · dentedPAX 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.May 15, 2026 · N936SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051577305Support · corrodedPRESSURE 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-53-41-666May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026051577304Fitting · wornPASSENGER 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.May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026051577302Fitting · wornPASSENGER 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.May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026051577297Door Sill · corrodedPASSENGER 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.May 15, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026051477294Hinge · damagedPAX 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 53-21-2May 14, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2026051377298Mount · gougedRIGHT 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 -.May 13, 2026 · N936SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA2026051277303Bracket · crackedPILOTS 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.May 12, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026051177300Bracket · crackedPILOTS 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.May 11, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026050977288Skin · damagedLEFT APRON SKIN PANEL ASSY HAD CHAFE AND GOUGE DAMAGE. REPAIRED THE APRON ASSY SKIN PANEL, IAW REO 601R-53-41-3446, REV-.May 9, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWIA2026050677287Window Post · crackedCRACK 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.May 6, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026043077330Skin · erodedEROSION 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 -.Apr 30, 2026 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026043077326Skin · dentedDENT 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.Apr 30, 2026 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026043077289Vane · erodedEROSION 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 TIMEApr 30, 2026 · N936SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026041677320Pressure Blkhd · crackedNONDESTRUCTIVE 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 INSPECApr 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2026041677291Trunnion · crackedCOMPLY 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 60Apr 16, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
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