N979SW

Service difficulty reports · 165

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 = 'N979SW' 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 SWIA2019101846529Rib · crackedL/H MLG BATT RIB IS CRACKED AT W.S. 53.60. (C-CHECK) RO: 10/16/2019 REPAIRED LH MLG BATT RIB AT WS 53.6 IAW REO.Sep 17, 2019 · N979SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2019101846528Rib · crackedR/H MLG BATT RIB AT W.S. 53.60 IS CRACKED. (C-CHECK) RO: 10/16/2019 REPAIRED RH MLG BATT RIB AT WS 53.6 IAW REO.Sep 17, 2019 · N979SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2019101846527Bracket · crackedR/H MLG WHEEL WELL AFT HYD FUSE BRACKET IS CRACKED. (C-CHECK) RO: 10/16/2019REMOVED AND REPLACED BRACKET IAW SRM.Sep 17, 2019 · N979SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2019101846526Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE ELEVATOR CONTROL CABLES FOUND THE RH ELEVATOR CONTROL CABLE CIRCUIT TO BE OUT OF LIMITS. AT 70 DEGREES THE MEASUREMENT IS 120, THE ALLOWABLE MEASUREMENT AT 70 DEGREES IS 125-135 (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING TSep 17, 2019 · N979SW · Cndair CL6002B19 · Elevator Control SystemSDR SWIA2019101846525Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE ELEVATOR CONTROL CABLES FOUND THE LH ELEVATOR CONTROL CABLE CIRCUIT TO BE OUT OF LIMITS. AT 70 DEGREES THE MEASUREMENT IS 120, THE ALLOWABLE MEASUREMENT AT 70 DEGREES IS 125-135 (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING OSep 17, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846546Vertical Support · damagedFS409+128 RBL18 VERT POST HAS INDICATIONS NOTED ON BOTH SIDES IN THE AFT FLANGE RADIUS AT WL69 GREATER THAN 50%FSH. I/B SIDE IS 0.250" LONG AND O/B SIDE IS 0.250" LONG. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED F/S 409+128 RBL 18 VERT POST IAW REO.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019101846545Skin · chafedFUSELAGE SKIN AROUND APU EXHAUST IS CHAFED AT TWO LOCATIONS BETWEEN F.S. 654.20 TO F.S. 672.20. CHAFES ARE APPROX 0.125 LONG, 0.125 WIDE AND 0.015 DEEP. (C-CHECK) RO: 10/16/2019 REMOVED DAMAGE @ FS 654 - FS 672.20 AROUND APU EXH IAW REO.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2019101846524Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE LH TENSION REGULATOR TO BE OUT OF LIMITS AND REQUIRES ADJUSTMENT (C-CHECK) RO: 10/16/2019 PERFORMED ADJUSTMENT OF THE LH AILERON WING CIRCUIT IAW AMM.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846523Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE RH TENSION REGULATOR TO BE OUT OF LIMITS AND REQUIRES ADJUSTMENT (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING OF THE RH AILERON WING CIRCUIT IAW AMM.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846522Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE RH O/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 60 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 PERFORMED TENSIONING OF THE Sep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846521Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE RH I/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 60 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 RH IB AND OB COLUMN CONTROL Sep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846520Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE LH O/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 60 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 ADJUSTED THE LH AILERON CONTSep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846519Control Cable · damagedWHILE PERFORMING TENSION CHECKS OF THE AILERON CONTROL CABLES FOUND THE LH I/B CONTROL COLUMN CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 55 AT 80 DEGREES. THE ALLOWABLE MEASUREMENT AT 80 DEGREES IS 65-75 (C-CHECK) RO: 10/16/2019 LH I/B AND O/B CONTROL COLUMSep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846518Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE AILERON CONTROL CABLES FOUND THE R/H I/B FUSELAGE CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 100 AT 80 DEGREES, THE ALLOWABLE MEASUREMENT IS 120-130 AT 80 DEGREES (C-CHECK) RO: 10/16/2019 PERFORMED RIGGING OF THE RH AILSep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846517Control Cable · damagedWHILE PERFORMING TENSION CHECK OF THE AILERON CONTROL CABLES FOUND THE LH O/B FUSELAGE CABLE TO BE OUT OF LIMITS. THE MEASUREMENT IS 145 AT 80 DEGREES THE ALLOWABLE MEASUREMENT IS 120-130 AT 80 DEGREES. (C-CHECK) RO 10/16/2019 PERFORMED RIGGING OF THE LH FUSESep 16, 2019 · N979SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA2019101846516Turnbuckle · damagedLH ENGINE FIXED CORE COWL AFT UPPER MOUNTING TURNBUCKLE HAS BEARING PUSHED OUT OF UPPER ROD END AND LOWER ROD END IS BENT. (C-CHECK) RO: 10/16/2019 TRANSFERED TO MX SHOP WORK ORDER.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR SWIA2019101846515Vertical Support · damagedFS409+128 BL0 VERT POST HAS INDICATIONS NOTED ON BOTH SIDES IN THE AFT FLANGE RADIUS AT WL69 GREATER THAN 50%FSH. L/H SIDE IS 0.350" LONG AND R/H SIDE IS 0.300" LONG. MARKED ON A/C. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED F/S 409+128 BL 0 VERT POST IAW RSep 16, 2019 · N979SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019101846514Bearing · out of limitsWHILE PERFORMING BACKLASH CHECK ON THE RH ELEVATOR FOUND THE #1 BEARING TO BE OUT OF LIMITS. THE MEASUREMENT IS .265, THE MAX ALLOWABLE IS .210 (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED ELEVATOR BUSHINGS IAW AMM.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2019101846513Bearing · out of limitsWHILE PERFORMING BACKLASH CHECK ON LH ELEVATOR FOUND #3 BEARING TO BE OUT OF LIMITS. MEASUREMENT IS .245, THE MAX ALLOWABLE IS .210 (C-CHECK) RO: 10/16/2019 REPLACEMNET OF LEFT HAND ELEVATOR BUSHING'S AND BEARINGS.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2019101846512Bearing · out of limitsWHILE PERFORMING BACKLASH CHECK ON LH ELEVATOR FOUND #2 BEARING TO BE OUT OF LIMITS. MEASUREMENT IS .267, THE MAX ALLOWABLE IS .210 (C-CHECK) RO: 10/16/2019 REPLACEMENT OF LEFT HAND ELEVATOR BUSHING'S AND BEARING'S.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2019101846511Bearing · out of limitsWHILE PERFORMING BACKLASH CHECK ON LH ELEVATOR FOUND #1 BEARING TO BE OUT OF LIMITS. (C-CHECK) RO: 10/16/2019 REMOVED AND REPLACED LH ELEVATOR BUSHINGS IAW AMM.Sep 16, 2019 · N979SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2019101846510Step · corrodedSERVICE DOOR STEP PLATE HAS CORROSION ON LOWER SIDE AROUND FASTENER HOLES (C-CHECK) RO: 10/16/2019 DRILLED AND LOCATED NEW PLATE ASSY IAW SRM.Sep 15, 2019 · N979SW · Cndair CL6002B19 · Service DoorsSDR SWIA2019101846509Proximity Sensor · damagedL/H MLG WOW 1 AND WOW 2 PROX SENSOR GAPS ARE OUT OF LIMITS. BOTH PROX SENSOR GAPS MEASURE 0.030 IN AND SHOULD BE 0.040 - 0.050 IN. (C-CHECK) RO: 10/16/2019 ADJUSTED L/H MLG WOW 1 AND WOW 2 PROX SENSOR GAPS TO CORRECT GAP IAW AMM.Sep 14, 2019 · N979SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2017071943520Control Unit · failedFLAP FAILED AFTER TAKE OFF AT 8 DEGREES. DECLARED AN EMERGENCY. REPLACED THE FECU AND C/W AD.Jul 18, 2017 · N979SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA201743344O-Ring · failedLOST HYD 2 PRESSURE DURING FINAL APPROACH. HYD 2 LOW PRESSURE CAUTION MESSAGE. CAPTAIN DECLARED AN EMERGENCY. REMOVED AND REPLACED A BLOWN O-RING IAW AMM.May 30, 2017 · N979SW · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA201439032Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. R & R F/A FLASHLIGHT IAW AMM. OPS CHECKED GOOD.Aug 10, 2014 · N979SW · Cndair CL6002B19 · Emergency EquipmentSDR SWIA201438513Priority Valve · failedAFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. ABOUT TWO MINUTES LATER WHILE RUNNING THE QRH NOSE GEAR DID COME UP. RETURNED TO THE FIELD. R & R NLG PRIORITY VALVE IAW AMM. PERFORMED GEAR SWINGS AND EVERYTHING FUNCTIONS NORMALLY. OPS CHECKED GOOD.Jun 22, 2014 · N979SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201438007Light · inoperativeLEFT NR 3 EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R LT NR 3 EXTERNAL EMERGENCY LIGHT IAW AMM.Jun 2, 2014 · N979SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201437007Lamp · burned outFORWARD CEILING EMERGENCY LIGHT IS BURNED OUT. REPLACED LAMP.Apr 4, 2014 · N979SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436150Light · inoperativeEMERGENCY LOWER RT OVERWING EXIT SIGN IS BURNED OUT. FLT 6485 RELAMPED.Jan 28, 2014 · N979SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436015Vane · wornRT INBD FLAP, MID VANE CAP IS WORN BEYOND LIMITS. C-CHECK R & R RT INBD FLAP MID VANE CAP IAW SRM.Jan 8, 2014 · N979SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436010Bulkhead · crackedCRACK INDICATION NOTED AT FS 621 AFT PRESS BULKHEAD ON WEB AT LBL 18.00 BETWEEN WL 120.43 & WL 73.50. C-CHECK REPAIRED THE CRACK AT FS 621 AFT PRESS BULKHEAD ON WEB AT LBL 18.00 BETWEEN WL 120.43 & WL 73.50 IAW REO.Jan 8, 2014 · N979SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201436009Sill · corrodedCARGO DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES. C-CHECK REMOVED CORROSION FROM CARGO DOOR SILL AROUND THE NUTPLATE HOLES IAW REO.Jan 8, 2014 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201436016Vane · chafedRT WING INBD FLAP VANE LE CHAFFED INBD OF INBD ACTUATOR TUBE. C-CHECK REPAIRED IAW REO.Jan 7, 2014 · N979SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436014Vane · chafedRT WING INBD FLAP VANE LE CHAFFED OTBD OF OTBD ACTUATOR TUBE. C-CHECK REPAIRED IAW REO.Jan 7, 2014 · N979SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436013Vane · chafedLT WING INBD FLAP VANE LE CHAFFED INBD OF INBD ACTUATOR TUBE. C-CHECK REPAIRED IAW REO.Jan 7, 2014 · N979SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436012Vane · chafedLT WING INBD FLAP VANE LE CHAFFED OTBD OF CTR ACTUATOR TUBE. C-CHECK REPAIRED IAW REO.Jan 7, 2014 · N979SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436011Vane · chafedLT WING INBD FLAP VANE LE CHAFFED OTBD OF OTBD ACTUATOR TUBE. C-CHECK REPAIRED IAW REO.Jan 7, 2014 · N979SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201335735Hydraulic Line · chafedLOW PRESS HYD SYSTEM 1 CAUTION. FLT 6393 REPLACED NR 1 ENG PRESS LINE CHAFED BY ADEL CLAMP JUST BELOW NR 1 RESERVOIR.Dec 23, 2013 · N979SW · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA201334464Skin · damagedLOWER SKIN FROM FS 193-202 REMOVED. SERVICE REPLACED IAW SRM.Jul 22, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201334460Skin · damagedSKIN DAMAGED ON RT SIDE FROM FS 202-280 STRINGER 16-23. SERVICE REPLACED SKIN IAW SRM.Jul 14, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201334458Attach Angle · out of alignmentTHREE WEB ATTACH ANGLES ON FWD SIDE FS 202 BULKHEAD AT WL 79.5 HAVE PILOT HOLES WHICH DO NOT ALIGN WITH EXISTING STRUCTURE HOLES. SERVICE REPLACED IAW SRM. PN 601R33017-3, 601R33018-2 & 601R33019-1.Jul 3, 2013 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201334457Web · out of alignmentRT & LT NOSE WELL WEBS FROM FS 193-202 AT RBL 13.5 & LBL 13.5 NEED TO BE REPLACED DUE TO HOLES NOT LINING UP. SERVICE FABRICATED NEW RT & LT NOSE WHEEL WELL WEBS IAW SRM.Jul 1, 2013 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201334456Strap · out of alignmentRT LOWER NOSE SECTION INTERNAL SKIN STRAP FROM FS 192-202 AT 24A R REQUIRES REPLACEMENT DUE TO HOLES NOT LINING UP. SERVICE REPLACED IAW SRM.Jul 1, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201334455Strap · out of alignmentLT LOWER NOSE SECTION INTERNAL SKIN STRAP FROM FS 193-202 AT STRINGER 24A L REQUIRES REPLACEMENT DUE TO HOLES NOT LINING UP. SERVICE REPLACED IAW SRM.Jul 1, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201334454Strap · out of alignmentRT INTERNAL SKIN STRAP AT FS 202 REQUIRES REPLACEMENT DUE TO HOLES NOT LINING UP. SERVICE FABRICATED & INSTALLED RT INTERNAL SKIN STRAP AT FS 202 IAW SRM.Jul 1, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201334453Skin · damagedSKIN DAMAGED ON LT SIDE FROM FS 202-280 STRINGER 16-23. SERVICE REPLACED LT FS SKIN IAW SRM.Jun 25, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201334452Strap · damagedLT BULKHEAD STRAP AT FS 202 IS DAMAGED. SERVICE FABRICATED NEW LT BULKHEAD STRAP AT FS 202. MATERIAL USED, .050" 2024-T3 PO P1332476 IAW SRM.Jun 25, 2013 · N979SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201334451Stringer · damagedSTRINGER 17L AT FS 202 IS DAMAGED. C-CHECK REPAIRED STRINGER 17L BETWEEN FS 202 TO 220 IAW REO.Jun 25, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA201334459Skin · damagedUPPER LT SKIN FS 193-202 IS DAMAGED. SERVICE REPLACED IAW SRM.Jun 24, 2013 · N979SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
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