# Service difficulty reports: N934SW A list on [N934SW](https://openairdocs.org/aircraft/N934SW.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 · 142 reports - [SDR SWIA2019122647126](https://openairdocs.org/sdr/SWIA2019122647126.md): Stringer · corroded · Dec 10, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > WHILE REMOVING FRAME AT FS 589.00 IT WAS NOTICED CORROSION ON STGR 21L AT APPROX. FS 581.00. REPAIRED THE STRINGER IAW SRM. ALL CHECKED GOOD. - [SDR SWIA2019122647127](https://openairdocs.org/sdr/SWIA2019122647127.md): Structure · chafed · Dec 6, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Structure > FS621 LBL9.50 CHAFE AREA REQUIRES REPAIR PER REO (C-CHECK) RO 12/23/2019 PERFORMED REPAIR TO FS621 LBL9.50 CHAFE AREA REF REO. CHECKS GOOD - [SDR SWIA2019122647130](https://openairdocs.org/sdr/SWIA2019122647130.md): Angle · cracked · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Floor Beam > CRACKED CLIP AT BS 280, RBL 9 OTBD SIDE. REMOVED AND INSTALLED A NEW FABRICATED ATTACHING CLIP IAW REO AND SRM. - [SDR SWIA2019122647129](https://openairdocs.org/sdr/SWIA2019122647129.md): Angle · cracked · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Floor Beam > CRACKED CLIP AT BS 280, LBL 9 INBD SIDE. REMOVED, AND INSTALLED A NEW INBD ATTACHMENT CLIP IAW REO, AND SRM. - [SDR SWIA2019122647128](https://openairdocs.org/sdr/SWIA2019122647128.md): Angle · cracked · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Floor Beam > CRACKED CLIP BS 280, LBL 9 OTBD SIDE. FABRICATED, LOCATED, DRILLED AND INSTALLED A NEW CLIP IAW REO, AND LOCATION AND MATERIAL, AND IAW SRM. - [SDR SWIA2019122647125](https://openairdocs.org/sdr/SWIA2019122647125.md): Panel · dirty · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE FLAPPER DRAIN PANEL BETWEEN BS 559+80 TO 559+96, STRINGERS 26L AND 27 HAD CORROSION. CLEANED AREA IAW SRM. UPON CLEANING, FOUND NO CORROSION ON FLAPPER DRAIN PANEL. - [SDR SWIA2019122647124](https://openairdocs.org/sdr/SWIA2019122647124.md): Stringer · dirty · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > STRINGER 26R BETWEEN BS 589 AND 574 HAD CORROSION. CLEANED AREA IAW SRM. UPON CLEANING, FOUND NO CORROSION ON THE STRINGER. - [SDR SWIA2019122647123](https://openairdocs.org/sdr/SWIA2019122647123.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > THE FRAME AT BS 589 FROM STRINGERS 20L TO 17L HAD CORROSION AT MULTIPLE AREAS. REMOVED CORROSION IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS IAW SRM. RESTORED FINISH IAW SRM.. PRESSURE CHECKED GOOD. - [SDR SWIA2019122647122](https://openairdocs.org/sdr/SWIA2019122647122.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > THE FRAME AT BS 589 FROM STRINGERS 24R TO 20L HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND REPLACED THE FRAME IAW SRM. PRESSURE CHECKED GOOD, - [SDR SWIA2019122647121](https://openairdocs.org/sdr/SWIA2019122647121.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > THE FRAME AT BS 589 FROM STRINGERS 17R TO 19R HAD CORROSION. REMOVED CORROSION IAW SRM. MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH AND CIC. - [SDR SWIA2019122647120](https://openairdocs.org/sdr/SWIA2019122647120.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > THE FRAME AT BS 605 FROM STRINGERS 20L TO 17L HAD CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. LEAK CHECKED GOOD. - [SDR SWIA2019122647119](https://openairdocs.org/sdr/SWIA2019122647119.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > THE FRAME AT BS 605 FROM STRINGERS 25R TO 20L HAD CORROSION AT MULTIPLE LOCATIONS. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS.. LEAK CHECKED GOOD. - [SDR SWIA2019122647118](https://openairdocs.org/sdr/SWIA2019122647118.md): Doubler · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE AFT DRAIN DOUBLER BETWEEN BS 621 AND 605, BETWEEN STRINGERS 26R AND 25R HAD MULTIPLE AREAS OF CORROSION. REMOVED AND INSTALLED NEW DRAIN MAST DOUBLER IAW SRM AND DWG. ALL CHECKED GOOD. - [SDR SWIA2019122647117](https://openairdocs.org/sdr/SWIA2019122647117.md): Angle · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE FS 621.00 BELOW FLOOR ANGLE FROM STRINGER 24R TO 19L HAD CORROSION IN MULTIPLE LOCATIONS. REMOVED CORROSION IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS IAW SRM. RESTORED FINISH TO AREA IAW SRM. PRESSURE CHECKED GOOD. - [SDR SWIA2019122647116](https://openairdocs.org/sdr/SWIA2019122647116.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > THE FRAME AT FS 574.00 FROM STRINGER 24L TO 25R HAS CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. OPS CHECKED GOOD. - [SDR SWIA2019122647115](https://openairdocs.org/sdr/SWIA2019122647115.md): Frame · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Frame > * THE FRAME AT FS 574.00 FROM STRINGER 17L TO 18L HAS CORROSION. (C-CHECK) RO 12/23/2019 REMOVED CORROSION FROM FS 574.00 FRAME BETWEEN STRINGER 17L AND18L AND RESTORED FINISH. REF CRJ200 SRM. REMAINING MATERIAL THICKNESS IS WITHIN LIMITS. SEE CONTINUE CARD - [SDR SWIA2019122647114](https://openairdocs.org/sdr/SWIA2019122647114.md): Strap · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE CROSSBEAM/STRAP AT BS 559 +80 FROM RBL 9 TO RBL 27 HAD CORROSION. REMOVED CORROSION FROM THE CROSSBEAM/STRAP IAW SRM. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM. - [SDR SWIA2019122647113](https://openairdocs.org/sdr/SWIA2019122647113.md): Strap · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE CROSSBEAM/STRAP AT BS 559 FROM RT EDGE MEMBER, SILL TO RBL 27 HAD CORROSION. REMOVED CORROSION AT CROSSBEAM/STRAP IAW SRM 51-21-06, AREA IS WITHIN LIMITS IAW SRM 53-00-00. - [SDR SWIA2019122647112](https://openairdocs.org/sdr/SWIA2019122647112.md): Strap · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > THE CROSSBEAM/STRAP AT BS 559 FROM LT EDGE MEMBER, SILL TO LBL 27 HAD CORROSION. REMOVED AND INSTALLED A NEW SERVICEABLE CROSSBEAM STRAP AT BS.559 IAW DWG. PERFORMED PRESSURE CHECK IAW AMM. PRESSURE CHECKED GOOD. PERFORMED OPS TEST OF THE MLG OVERHEAT DETEC - [SDR SWIA2019122647111](https://openairdocs.org/sdr/SWIA2019122647111.md): Floor Support · corroded · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LH PRESSURE FLOOR SILL ANGLE HAS MULTIPLE AREAS OF CORROSION. BLENDED OUT CORROSION ON L/H FLOOR SILL ANGLE AND REPLACED FASTENERS A REQUIRED IAW REO. ALL CHECKED GOOD - [SDR SWIA2019122647110](https://openairdocs.org/sdr/SWIA2019122647110.md): Floorbeam · cracked · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Floor Beam > *PRESSURE FLOOR SKIN IS CRACKED AT FS 461 BETWEEN BL 0 AND LBL 9. REPAIRED CRACKED PRESSURE FLOOR SKIN AT APPROX FS461 BETWEEN LBL9 AND RBL9 IAW REO. ALL CHECKED GOOD - [SDR SWIA2019122647109](https://openairdocs.org/sdr/SWIA2019122647109.md): Angle · cracked · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CLIP ON INTERCOSTAL AT FS 484 OTBD OF RBL27 IS CRACKED. (C-CHECK) RO 12/23/2019 REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP (P/N 601R31171-9) ON INTERCOSTAL AT FS 484.00, OTBD RBL 27 REF CRJ-200 SRM. RESTORD FINISH AND APPLIED CIC TO REWORKED AREA REF CRJ - [SDR SWIA2019122647108](https://openairdocs.org/sdr/SWIA2019122647108.md): Angle · cracked · Nov 26, 2019 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CLIP ON INTERCOSTAL AT FS 484 OTBD OF LBL27 IS CRACKED. REMOVED AND REPLACED CRACKED CLIP WITH NEW CLIP ON INTERCOSTAL AT FS 484.00, OTBD LBL 27 IAW SRM. RESTORD FINISH AND APPLIED CIC TO REWORKED AREA REF SRM. - [SDR SWIA2019122647107](https://openairdocs.org/sdr/SWIA2019122647107.md): Bracket · cracked · Nov 25, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > AFT EQUIPMENT COMPARTMENT HAS CRACKED CLIP ATTACHED TO FS 625.00 FRAME NEAR R/H STGR 14. REMOVED AND REPLACED CLIP P/N: 601-35012-52 AT FS 625.00 FRAME NEAR R/H STGR 14R IAW SRM. - [SDR SWIA2019122647106](https://openairdocs.org/sdr/SWIA2019122647106.md): Bracket · cracked · Nov 25, 2019 · N934SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > * AFT EQUIPMENT COMPARTMENT HAS CRACKED CLIP ATTACHED TO FS 625.00 FRAME NEAR L/H STGR 14. REMOVED AND REPLACED CLIP P/N: 601-35012-51 AT FS 625.00 FRAME NEAR L/H STGR 14L IAW SRM. - [SDR SWIA2019081446180](https://openairdocs.org/sdr/SWIA2019081446180.md): Uplock · failed · Aug 14, 2019 · N934SW · Cndair CL6002B19 · Landing Gear Position and Warning > GEAR DISAGREE IN FLIGHT. COMPLIED WITH QRH. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. (FLT#5045) CLOSED REMOVED AND REPLACED NLG UPLOCK ASSEMBLY AND NLG UPLOCK HARNESS ASSEMBLY IAW AMM. LEAK CHECK GOOD AT THIS TIME. OPS TEST OF PSS SYSTEM GOOD AT THIS TIME. - [SDR SWIA2017122644110](https://openairdocs.org/sdr/SWIA2017122644110.md): Skin · dented · Nov 29, 2017 · N934SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DENTED BS 654 & 672 BETWEEN STRINGERS 26L & 26R. REPAIRED THE SKIN IAW REO. - [SDR SWIA2017122644109](https://openairdocs.org/sdr/SWIA2017122644109.md): Structure · chafed · Nov 29, 2017 · N934SW · Cndair CL6002B19 · Ailerons > RIGHT AILERON INBOARD FIXED LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE AILERON INBOARD FIXED LEADING EDGE IAW SRM. - [SDR SWIA201541669](https://openairdocs.org/sdr/SWIA201541669.md): Vane · chafed · Nov 15, 2015 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT SIDE INBD FLAP, MOVABLE VANE OTBD L/E HAS CHAFE. REMOVED, FABRICATED, INSTALLED NEW LT INBD FLAP, OTBD FLAP VANE CAP IAW SRM. - [SDR SWIA201540593](https://openairdocs.org/sdr/SWIA201540593.md): Unknown · smoke · Jan 13, 2015 · N934SW · Cndair CL6002B19 · Air Distribution System > DURING CLIMB OUT, CREW RECEIVED SMOKE TOILET CAUTION MESSAGE. F/A REPORTED NO EVIDENCE OF SMOKE OR ODOR IN THE CABIN. RAN ACFT ABOUT 15 MIN AND TRIED EVER COMBINATION OF BLEED AIR AND ELECTRICAL BUT UNABLE TO DUPLICATE. NO INDICATION IN COCKPIT OR VISUAL. - [SDR SWIA201440427](https://openairdocs.org/sdr/SWIA201440427.md): Door Frame · dented · Dec 24, 2014 · N934SW · Cndair CL6002B19 · Fuselage Main, Structure > DENT ON THE FWD PAX DOOR FRAME BS 310 S16L. REPAIRED IAW REO. - [SDR SWIA201438902](https://openairdocs.org/sdr/SWIA201438902.md): Battery Pack · inoperative · Jul 26, 2014 · N934SW · Cndair CL6002B19 · Emergency Equipment > F/A FLASHLIGHT IS INOPERATIVE. R & R BATTERY ON F/A FLASHLIGHT IAW AMM. OPS CHECKED GOOD. - [SDR SWIA201437452](https://openairdocs.org/sdr/SWIA201437452.md): Lamp · burned out · May 8, 2014 · N934SW · Cndair CL6002B19 · Emergency Lighting > EXTERIOR OVERWING EXIT EMERGENCY LIGHT ON RT SIDE FUSELAGE IS BURNED OUT, REPLACED LAMP. - [SDR SWIA201436580](https://openairdocs.org/sdr/SWIA201436580.md): Light · inoperative · Feb 28, 2014 · N934SW · Cndair CL6002B19 · Emergency Lighting > NR 4 EMERGENCY POD LIGHT IS BURNED OUT. FLT 5641 RELAMPED. - [SDR SWIA201436281](https://openairdocs.org/sdr/SWIA201436281.md): Light · inoperative · Feb 5, 2014 · N934SW · Cndair CL6002B19 · Emergency Lighting > AFT OVERHEAD EMERGENCY EXIT SIGN IS BURNED OUT. SERVICE RELAMPED. - [SDR SWIA201436280](https://openairdocs.org/sdr/SWIA201436280.md): Light · inoperative · Feb 5, 2014 · N934SW · Cndair CL6002B19 · Emergency Lighting > FLOOR LEVEL EMERGENCY EXIT SIGN IS BURNED OUT AT MCD ENTRY. SERVICE RELAMPED. - [SDR SWIA201436233](https://openairdocs.org/sdr/SWIA201436233.md): Bulkhead · cracked · Jan 23, 2014 · N934SW · Cndair CL6002B19 · Fuselage Main, Bulkhead > TWO EACH CRACKS NOTED ON FS 621 AFT PRESS BULKHEAD FWD FACE AT LBL 27.50 BETWEEN WL 120.00 & WL 75.00. C-CHECK CUT AWAY DAMAGE, FABRICATED NEW PARTS & INSTALLED ON FS 621 AFT PRESS BULKHEAD IAW REO. - [SDR SWIA201436240](https://openairdocs.org/sdr/SWIA201436240.md): Post · cracked · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 409.0+128 BL 0.00 FWD RADIUS OF VERTICAL POST CRACK INDICATION NOTED. C-CHECK REPLACED FS 409+128 BL 0 VERTICAL POST IAW SRM & REO. - [SDR SWIA201436239](https://openairdocs.org/sdr/SWIA201436239.md): Vane · chafed · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > LT INBD FLAP, OTBD FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON LT INBD FLAP, OTBD FLAP VANE LE IAW REO. - [SDR SWIA201436238](https://openairdocs.org/sdr/SWIA201436238.md): Vane · chafed · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > LT INBD FLAP, MIDDLE FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON LT INBD FLAP, MIDDLE FLAP VANE LE IAW REO. - [SDR SWIA201436237](https://openairdocs.org/sdr/SWIA201436237.md): Vane · chafed · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > LT INBD FLAP, INBD FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON LT INBD FLAP, INBD FLAP VANE LE IAW REO. - [SDR SWIA201436236](https://openairdocs.org/sdr/SWIA201436236.md): Vane · chafed · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > RT INBD FLAP, INBD FLAP VANE IS CHAFED. C-CHECK BLENDED CHAFE ON RT INBD FLAP, INBD FLAP VANE LE IAW REO. - [SDR SWIA201436235](https://openairdocs.org/sdr/SWIA201436235.md): Vane · chafed · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > RT INBD FLAP, MIDDLE FLAP VANE IS CHAFED. C-CHECK REPAIRED IAW REO. - [SDR SWIA201436234](https://openairdocs.org/sdr/SWIA201436234.md): Vane · chafed · Jan 22, 2014 · N934SW · Cndair CL6002B19 · Trailing Edge Flaps > RT INBD FLAP, OTBD FLAP VANE IS CHAFED. C-CHECK NEW CAP WAS INSTALLED IAW REO. - [SDR SWIA201335281](https://openairdocs.org/sdr/SWIA201335281.md): Control Handle · failed · Nov 14, 2013 · N934SW · Cndair CL6002B19 · Landing Gear Selector > RECEIVED ANTI-SKID INBD CAUTION MESSAGE, FOLLOWED BY PARKING BRAKE SOV CAUTION MESSAGE. GEAR DID NOT RETRACT, FOLLOWED QRH WITH GEAR SELECTED DOWN, ALL MESSAGES CLEARED. FLT 6405 REPLACED LANDING GEAR SELECTOR HANDLE ASSEMBLY IAW AMM. PERFORMED GEAR SWINGS, - [SDR SWIA201335228](https://openairdocs.org/sdr/SWIA201335228.md): Shutoff Valve · failed · Nov 10, 2013 · N934SW · Cndair CL6002B19 · Landing Gear Brake System > UPON SELECTING GEAR UP AFTER TAKEOFF RECEIVED ANTI-SKID INBD CAUTION, THEN A PARK BRAKE SOV CAUTION MESSAGE & GEAR WOULD NOT RETRACT. UPON SELECTING GEAR DOWN BOTH MESSAGES CLEARED & LANDING GEAR REMAINED DOWN. FLT 6427 REPLACED PARKING BRAKE SOV, PERFORMED - [SDR SWIA201335185](https://openairdocs.org/sdr/SWIA201335185.md): Button · dirty · Nov 2, 2013 · N934SW · Cndair CL6002B19 · Passenger/Crew Doors > MAIN CABIN DOOR JAMMED COULD NOT OPEN. FLT 6252 INSPECTED MAIN CABIN DOOR & FOUND CABIN DOOR PUSH BUTTON ASSIST MOTOR STUCK. CLEANED DEBRIS FROM PUSH BUTTON. DOOR NO LONGER JAMMED SHUT. - [SDR SWIA201334898](https://openairdocs.org/sdr/SWIA201334898.md): Light · inoperative · Oct 8, 2013 · N934SW · Cndair CL6002B19 · Emergency Lighting > NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#6217 RELAMPED. - [SDR SWIA201333959](https://openairdocs.org/sdr/SWIA201333959.md): Lamp · burned out · Jul 15, 2013 · N934SW · Cndair CL6002B19 · Emergency Lighting > FLT 6308, NR 4 EMERGENCY OVERHEAD LIGHT BURNED OUT. REPLACED LAMPS. - [SDR SWIA201333584](https://openairdocs.org/sdr/SWIA201333584.md): Guide · lack of lube · May 31, 2013 · N934SW · Cndair CL6002B19 · Passenger/Crew Doors > MAIN CABIN DOOR IS DIFFICULT TO OPEN. LUBED THE HANDLE ROLLER GUIDE. REPLACED MAIN CABIN DOOR ICE BREAKER CABLE, IAW AMM. Next page: https://openairdocs.org/aircraft/N934SW/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 = 'N934SW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N934SW/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.