# Service difficulty reports: N433SW A list on [N433SW](https://openairdocs.org/aircraft/N433SW.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 3 · 140 reports - [SDR SWIA202266590](https://openairdocs.org/sdr/SWIA202266590.md): None · failed · Oct 4, 2022 · N433SW · Cndair CL6002B19 · Fire Bottle, Portable > APU FIREX BOTTLE TEST CAUSES EMERGENCY APU SHUTDOWN WITH CODE 227 ON APU ECU (FILED CLOSED) REMOVED AND REPLACED PBA SWITCH FOR APU FIRE IN REFERENCE TO CRJ200 ESPM 20-24-00. NO FIX. REMOVED AND REPLACED FIRE DETECTION PANEL IN REFERENCE TO CRJ200 AMM 26 - [SDR SWIA202264221](https://openairdocs.org/sdr/SWIA202264221.md): None · cracked · Feb 13, 2022 · N433SW · Cndair CL6002B19 · Engine Exhaust System > UPON INSPECTION FOUND RH ENGINE LOWER I/B THRUST REVERSER MAIN TRACK CRACKED. (FILED - CLOSED) REMOVED AND REPLACED RH ENGINE LOWER I/B THRUST REVERSER MAIN TRACK IN REFERENCE WITH CRJ200 AMM 78-34-11. OPS CHECK GOOD AT THIS TIME. - [SDR SWIA202161788](https://openairdocs.org/sdr/SWIA202161788.md): Stringer · damaged · Oct 4, 2021 · N433SW · Cndair CL6002B19 · Fuselage Main, Keel > STRINGER 26L REQUIRES REPLACEMENT BETWEEN FRAME FS364.00 AND APPROX. FS341. (FILED CLOSED) REPLACED DAMAGED SECTION OF STR26L FROM FS364.00 TO SPLICE REPAIR BETWEEN FS333.00 - FS 349.00. SPLICE PERFORMED IN REF TO SRM 53-00-03, FIG 202, SHEET 1 (REPAIR F - [SDR SWIA202161784](https://openairdocs.org/sdr/SWIA202161784.md): Rail · corroded · Sep 20, 2021 · N433SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings > SEAT TRACK HAS CORROSION BELOW WINDOW 3AB. (FILED CLOSED) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK FROM FS409.00+18.02 - FS409.00+111.02 IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21, REPAIR B USING MCFARLANE P/N 6656 SEAT TRACK IN REF TO REO 6 - [SDR SWIA202161787](https://openairdocs.org/sdr/SWIA202161787.md): None · corroded · Sep 17, 2021 · N433SW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 394, FWD LOWER DOUBLER BETWEEN STR 26L AND 27 HAS CORROSION. (FILED CLOSED) REMOVED AND REPLACED SKIN SUPPORT ON FWD SIDE OF FRAME 394.00 BETWEEN STR25L-STR25R IN REF TO SRM 51-42-06 AND REO 601R-53-21-3502, REV--, DATED 2021-09-28. COMPLIED WITH T - [SDR SWIA202161786](https://openairdocs.org/sdr/SWIA202161786.md): Bracket · cracked · Sep 17, 2021 · N433SW · Cndair CL6002B19 · Doors > CARGO DOOR AFT COUNTERBALANCE SPRING ATTACHMENT BRACKET IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT COUNTERBALANCE SPRING ATTACHMENT BRACKET USING ALTERNATE FASTENERS IN REF TO REO 601R-53-61-7721, REV--, DATED 2021-09-19. COMPLIED WITH - [SDR SWIA202161783](https://openairdocs.org/sdr/SWIA202161783.md): Rail · corroded · Sep 17, 2021 · N433SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings > SEAT TRACK HAS CORROSION DIRECTLY BELOW WINDOW 4AB. (FILED CLOSED) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK FROM FS409.00+18.02 - FS409.00+111.02 IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21, REPAIR B USING MCFARLANE P/N 6656 SEAT TRACK IN REF - [SDR SWIA202161785](https://openairdocs.org/sdr/SWIA202161785.md): Track · gouged · Sep 15, 2021 · N433SW · Cndair CL6002B19 · Doors > CARGO DOOR AFT ROLLER GUIDE TRACK IS GOUGED NEAR THE UPPER STOP. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT ROLLER GUIDE TRACK IN REF TO SRM 51-21-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337. - [SDR SWIA2019101646469](https://openairdocs.org/sdr/SWIA2019101646469.md): Vane · out of limits · Oct 2, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE L/E OUTBOARD PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE OTBD PANEL IAW SRM. - [SDR SWIA2019101646468](https://openairdocs.org/sdr/SWIA2019101646468.md): Vane · damaged · Oct 2, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE (CENTER OTBD PANEL) IAW SRM. - [SDR SWIA2019101646467](https://openairdocs.org/sdr/SWIA2019101646467.md): Vane · damaged · Sep 17, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP VANE OTBD L/E IS CHAFED OUT OF LIMITS. (CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP OTBD L/E VANE PANEL IAW SRM. - [SDR SWIA2019101646466](https://openairdocs.org/sdr/SWIA2019101646466.md): Vane · damaged · Sep 17, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP VANE CNTER L/E IS CHAFED OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP CENTER VANE PANEL IAW SRM. - [SDR SWIA2019101646465](https://openairdocs.org/sdr/SWIA2019101646465.md): Floor Support · out of limits · Sep 13, 2019 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REPLACE RH FLOOR SILL FS 310.00 TO FS 319.70 DUE TO OUT OF LIMITS (C-CHECK) RO: 10/13/2019 R/H FLOOR SILL FS310 TO FS319 REPLACED IAW SRM. - [SDR SWIA2019101646483](https://openairdocs.org/sdr/SWIA2019101646483.md): Retainer · gouged · Sep 11, 2019 · N433SW · Cndair CL6002B19 · Cargo/Baggage Doors > AFT CARGO DOOR SEAL RETAINER GOUGED UPPER AFT CORNER MARKED (C-CHECK) RO: 10/13/2019 REMOVED CARGO DOOR (UPPER,AFT) SEAL RETAINER, AND INSTALLED NEW CARGO DOOR (UPPER,AFT) SEAL RETAINER IAW SRM. - [SDR SWIA2019101646470](https://openairdocs.org/sdr/SWIA2019101646470.md): Door Frame · corroded · Sep 11, 2019 · N433SW · Cndair CL6002B19 · Fuselage Main, Structure > PAX DOOR CUT OUT FRAME AT STR 16 1/2 L FROM FS 295.0 TO FS 310.0 HAS CORROSION (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED INTERCOSTAL ON PAX DOOR CUT OUT FRAME AT STGR 16 1/2 L FROM FS295.00 TO FS310.00 IAW SRM. - [SDR SWIA2019101646482](https://openairdocs.org/sdr/SWIA2019101646482.md): Door Sill · corroded · Sep 10, 2019 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > SERVICE DOOR SILL ANGLE HAS CORROSION (C-CHECK) RO: 10/13/2019 SERVICE DOOR SILL ANGLE IS CORRODED AND REPLACED WITH NEW SILL ANGLE IAW SRM. - [SDR SWIA2019101646481](https://openairdocs.org/sdr/SWIA2019101646481.md): Door Sill · corroded · Sep 10, 2019 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RH SILL JUST FWD OF SERVICE DOOR CUTOUT AND BACK TO FS 409.0 HAS CORROSION (C-CHECK) RO: 10/13/2019 BLENDED OUT CORROSION ON RH FLOOR SILL FROM FS 310.00 TO FS 319.70 & FROM FS349.00 TO FS409.00 +5 IAW SRM. - [SDR SWIA2019101646480](https://openairdocs.org/sdr/SWIA2019101646480.md): Web · corroded · Sep 9, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR AFT WEB CORRODED AT ACCESS PNL CUTOUTS AND STAIR LANDINGS (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PAX DOOR AFT WEB STEP LANDINGS IAW SRM. REMOVED AND REPLACED PAX DOOR AFT WEB IAW SRM. - [SDR SWIA2019101646479](https://openairdocs.org/sdr/SWIA2019101646479.md): Web · corroded · Sep 9, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR FWD WEB CORRODED AT STEP LANDINGS AND ACCESS PNL CUTOUTS (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PAX DOOR FWD WEB STEP LANDINGS IAW SRM. REMOVED REPLACED PAX DOOR FWD WEB IAW SRM. - [SDR SWIA2019101646478](https://openairdocs.org/sdr/SWIA2019101646478.md): Vane · chafed · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP VANE L/E HAS THREE CHAFFS ( OUTBD, MIDDLE, INBD). (C-CHECK) RO: 10/13/2019 BLENDED RIGHT INBD FLAP VANE L/E IN THREE SPOTS ( OUTBD, MIDDLE, INBD). RIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS AND REPLACED. RIGHT INBD FLAP - [SDR SWIA2019101646477](https://openairdocs.org/sdr/SWIA2019101646477.md): Vane · chafed · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP VANE L/E HAS THREE CHAFFS ( OUTBD, MIDDLE, INBD). (C-CHECK) RO: 10/13/2019 BLENDED OUTAND REPAIRED CHAFFING MARKS ON THE LEFT HAND I/B FLAP VANE L/E AT THE 3EA. LOCATION I/B, O/B AND MIDDLE. REPLACED LEFT INBD FLAP (CENTER) VANE L/E PANEL, AND - [SDR SWIA2019101646476](https://openairdocs.org/sdr/SWIA2019101646476.md): Panel · corroded · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR PANEL 832AT HAS CORROSION AROUND FASTENER HOLES AND CHAFING DAMAGE ALONG LOWER FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION & CHAFING DAMAGES ON PANEL 832AT AROUND SCREW HOLES IAW SRM. - [SDR SWIA2019101646475](https://openairdocs.org/sdr/SWIA2019101646475.md): Panel · corroded · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR PANEL 832BR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED CORROSION ON PASSENGER DOOR PANEL 832BR IAW SRM. - [SDR SWIA2019101646474](https://openairdocs.org/sdr/SWIA2019101646474.md): Panel · corroded · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR PANEL 832CR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832CR IAW SRM. - [SDR SWIA2019101646473](https://openairdocs.org/sdr/SWIA2019101646473.md): Panel · corroded · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR PANEL 832EL HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832EL IAW SRM. - [SDR SWIA2019101646472](https://openairdocs.org/sdr/SWIA2019101646472.md): Panel · corroded · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR PANEL 832ER HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832ER IAW SRM. - [SDR SWIA2019101646471](https://openairdocs.org/sdr/SWIA2019101646471.md): Panel · corroded · Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR PANEL 832GR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832GR, FOUND TO BE OUT OF LIMITS IAW SRM. - [SDR SWIA2019082746230](https://openairdocs.org/sdr/SWIA2019082746230.md): Proximity Sensor · failed · Aug 26, 2019 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > CREW REPORTS "GEAR DISAGREE" AFTER TAKEOFF. CREW REPORTED NOSE GEAR WOULD NOT RETRACT AFTER ROTATION. RETURNED TO FIELD. REMOVED AND REPLACED THE NLG STRUT-CENTERED PROXIMITY SENSOR HARNESS ASSY IAW AMM. PERFORMED OPS CHECK OF EXTENSION AND RETRACTION SYSTEM I - [SDR SWIA2019022145534](https://openairdocs.org/sdr/SWIA2019022145534.md): Selector Valve · leaking · Feb 21, 2019 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > GEAR DISAGREE ON TAKEOFF WHEN TRYING TO RETRACT THE GEAR. BOTH MAINS RETRACTED FULLY BUT THE NOSE GEAR STAYED DOWN. COMPLIED WITH QRH AND ALL GEAR INDICATED DOWN AND 3 GREEN. RETURNED TO FIELD. (FLT#4105) REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. HYD SY - [SDR SWIA2019021945528](https://openairdocs.org/sdr/SWIA2019021945528.md): Selector Valve · failed · Feb 18, 2019 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > FLT#3703, UPON GEAR RETRACTION, NOSE GEAR DID NOT SHOW AN UP INDICATION. GEAR DISAGREE WARNING MESSAGE APPEARED.FOLLOWED QRH PROCEDURE AND GEAR EXTENDED TO DOWN POSITION CORRECTLY. NO GEAR SPEED LIMITS WERE EXCEEDED. INSTALLED NLG SELECTOR VALVE IAW AMM. BLED - [SDR SWIA2019011545442](https://openairdocs.org/sdr/SWIA2019011545442.md): Bracket · bent · Jan 11, 2019 · N433SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle > GEAR DISAGREE ON T/O. NOSE WHEEL DID NOT RETRACT. FOLLOWED QRH. RTF. (FLT#4106) CLOSED REMOVED AND REPLACED NLG OLEO BRACKET AND ADJUSTED PROXIMITY SENSOR. PERFORMED OPS CHECK IAW AMM. OPS CHECK GOOD, SWUNG GEAR MULTIPLE TIMES. - [SDR SWIA2018111645188](https://openairdocs.org/sdr/SWIA2018111645188.md): Uplock · failed · Oct 25, 2018 · N433SW · Cndair CL6002B19 · Landing Gear Position and Warning > AS WE PUT DOWN THE LANDING GEAR, WE WOULD GET A MOMENTARY GEAR DISAGREE CAUTION MESSAGE. (FLT# 7413) FO: 10/29/2018. CLOSED REMOVED AND REPLACED LEFT MLG UPLOCK ASSY IAW AMM. LEAK AND OPS CHECKS GOOD. - [SDR SWIA2017091943771](https://openairdocs.org/sdr/SWIA2017091943771.md): Unknown · cracked · Aug 29, 2017 · N433SW · Cndair CL6002B19 · Wing Structure > FOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO. - [SDR SWIA2017091943770](https://openairdocs.org/sdr/SWIA2017091943770.md): Unknown · cracked · Aug 29, 2017 · N433SW · Cndair CL6002B19 · Wing Structure > FOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO. - [SDR SWIA2017091943775](https://openairdocs.org/sdr/SWIA2017091943775.md): Floor Support · corroded · Aug 28, 2017 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CARGO FLOOR SUPPORT JUST INSIDE CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES. INSTALLED NEW CARGO FLOOR SUPPORT IAW REO. - [SDR SWIA201743774](https://openairdocs.org/sdr/SWIA201743774.md): Skin · dented · Aug 25, 2017 · N433SW · Cndair CL6002B19 · Wing, Plate/Skin > RT WING LEADING EDGE WING STATION 166. HAD A SMALL DENT.009 INCH DEEP X 3/4 INCH WIDE AND 1/2 INCH LONG. HAND DRESSED THE SKIN BACK TO ORIGINAL CONTOUR IAW REO.CHECKED GOOD. - [SDR SWIA2017091943773](https://openairdocs.org/sdr/SWIA2017091943773.md): Structure · dented · Aug 25, 2017 · N433SW · Cndair CL6002B19 · Wing Structure > LEFT WING LEADING EDGE LWS 185. HAD A SMALL DENT THAT MEASURES.019 INCH IN DEPTH, X.75 INCH IN LENGTH, AND.5 INCH IN WIDTH. COMPLIED WITH DRESS BACK REPAIR TO DENT ON THE LH WING LEADING EDGE IAW REO. LEAK CHECKED GOOD. - [SDR SWIA201743772](https://openairdocs.org/sdr/SWIA201743772.md): Structure · dented · Aug 25, 2017 · N433SW · Cndair CL6002B19 · Wing Structure > WING STATION 139. HAS A DENT 3/4 INCH WIDE AND.010 INCH DEEP. HAND FORMED THE DENT BACK TO ORIGINAL CONTOUR IAW REO. CHECKED GOOD.. - [SDR SWIA201743085](https://openairdocs.org/sdr/SWIA201743085.md): Priority Valve · failed · Mar 1, 2017 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > PILOT REPORTED NOSE GEAR WOULD NOT RETRACT WITH GEAR DISAGREE. REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. SWUNG GEAR, OPS CHECKED GOOD. - [SDR SWIA201541642](https://openairdocs.org/sdr/SWIA201541642.md): Strut · overserviced · Nov 25, 2015 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD. FOUND NOSE STRUT OVER SERVICED CORRECTED, OPS CHECKS GOOD, GEAR SWING ACCOMPLISHED. - [SDR SWIA201439964](https://openairdocs.org/sdr/SWIA201439964.md): Bracket · bent · Nov 16, 2014 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > ON DEPARTURE, NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD. MAIN GEAR EXTENDED NORMALLY. DUE TO IMPROPER PLACEMENT OF TOW STRAP, R & R BENT AND MISALIGNED NLG CENTERED PROX SENSOR BRACKET IAW AMM, PN: 16215-105. - [SDR SWIA201438417](https://openairdocs.org/sdr/SWIA201438417.md): Lamp · inoperative · Jun 26, 2014 · N433SW · Cndair CL6002B19 · Emergency Lighting > LEFT MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. - [SDR SWIA201437681](https://openairdocs.org/sdr/SWIA201437681.md): Light · burned out · May 21, 2014 · N433SW · Cndair CL6002B19 · Emergency Lighting > EXTERIOR EMERGENCY LIGHT NR 7 IS BURNED OUT. R & R EXTERIOR EMERGENCY LIGHT IAW AMM. - [SDR SWIA201437133](https://openairdocs.org/sdr/SWIA201437133.md): Actuator · failed · Apr 14, 2014 · N433SW · Cndair CL6002B19 · Autopilot System > YAW DAMPER NR 2 KEEPS DISCONNECTING AND WHEN ENGAGED CAUSES UNCOMMANDED RUDDER MOVEMENT. R & R YAW DAMPER NR 2 LINEAR ACTUATOR IAW AMM, PN ON/OFF: 622-9968-001, SN ON: 2497, SN OFF: 2561. - [SDR SWIA201436645](https://openairdocs.org/sdr/SWIA201436645.md): Light · inoperative · Mar 6, 2014 · N433SW · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHT NEXT TO MAIN CABIN DOOR IS BURNED OUT. FLT 4699 RELAMPED. - [SDR SWIA201436082](https://openairdocs.org/sdr/SWIA201436082.md): Computer · faulty · Jan 21, 2014 · N433SW · Cndair CL6002B19 · Autopilot Computer > AIRCRAFT INITIATED A SEVERE CLIMB TO CAPTURE GLIDE SLOPE, DISCONNECTED THE AUTO PILOT, GOT THE AIRCRAFT STABLE & RESUMED THE APPROACH. WHEN THE AUTO PILOT WAS RECONNECTED, AT APPROXIMATELY 3500 ', THE FLIGHT DIRECTOR COMMANDED A 15 DEGREE NOSE DOWN PITCH. DI - [SDR SWIA201335354](https://openairdocs.org/sdr/SWIA201335354.md): Floor Support · corroded · Nov 10, 2013 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CABIN FLOOR SUPPORT BEAM FS 349.00 AT PAX DOOR HAS CORROSION ON UNDERSIDE & CORRODED FASTENERS. C-CHECK REPAIRED CABIN FLOOR SUPPORT BEAM AT FS 349 LBL 40.00 IAW STS EA. - [SDR SWIA201335355](https://openairdocs.org/sdr/SWIA201335355.md): Stiffener · chafed · Nov 8, 2013 · N433SW · Cndair CL6002B19 · Wing Miscellaneous Structure > INTERNAL LT SIDE OF CTR WING FUEL TANK, FUEL PANEL 510BB. FUEL TUBE ASSEMBLY IN FWD PORTION OF TANK, CHECK VLV IS CHAFING ON THE STIFFENER. C-CHECK BLENDED CHAFED AREA ON STRINGER 23 JUST OTBD OF WS 29.4 IAW SRM. - [SDR SWIA201335357](https://openairdocs.org/sdr/SWIA201335357.md): Angle · cracked · Nov 7, 2013 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > AFT PRESSURE BULKHEAD, AFT SIDE, FRAME JUST AFT OF BULKHEAD HAS 2 EA CRACKED "L" ANGLES, 1 AT LT SIDE, 1 AT RT SIDE. C-CHECK R & R 2 EA "L" ANGLES AT FS 625 STRINGER 14 IAW SRM & REO. - [SDR SWIA201335356](https://openairdocs.org/sdr/SWIA201335356.md): Skin · chafed · Nov 7, 2013 · N433SW · Cndair CL6002B19 · Ailerons > RT AILERON UPPER LE SKIN IS CHAFED. C-CHECK REPLACED RT AILERON UPPER LE SKIN PN 601R13031-166 IAW SRM. Next page: https://openairdocs.org/aircraft/N433SW/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 = 'N433SW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N433SW/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.