N454SW

Service difficulty reports · 235

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 = 'N454SW'
  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 SWIA202601050221Skin · dentedDURING INSPECTION OF PANELS FOUND DENT IN RT AILERON UPPER SKIN, NEAR THE INBD EDGE. REPAIRED RH AILERON UPPER SKIN NEAR THE INBD EDGE IAW REO 601R-57-61-887 REV -, AND COMPLIED WITH TASK CARD 51-900-1003-SKY.Dec 21, 2025 · N454SW · Cndair CL6002B19 · AileronsSDR SWI2026F00040Angle · corrodedUPON REMOVAL OF LOW-PRESSURE GROUND AIR DOOR STRUCTURES FOUND REINFORCING ANGLE CORRODED. REMOVED CORRODED REINFORCING ANGLE IAW SRM 51-42-06 AND INSTALLED NEW REINFORCING ANGLE IAW SRM 51-42-06 AND DWG 601R36025 REV. P AND COMPLIED WITH TASK 51-900-1003-SKYNov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2026F00039Angle · corrodedUPON REMOVAL OF LOW PRESSURE GROUND AIR DOOR AFTANGLE FOUND LANDING ANGLE CORRODED. REMOVED LOW-PRESSURE GROUND AIR DOOR AFT ANGLE LANDING IAW SRM 51-42-06 AND INSTALLED NEW LOW-PRESSURE GROUND AIR DOOR AFT ANGLE LANDING IAW SRM 51-42-06 AND DWG 601R35226 RNov 2, 2025 · N454SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2026F00038Angle · corrodedLOW PRESSURE GROUND AIR DOOR FWD LANDING ANGLE IS CORRODED. REMOVED FWD LANDING ANGLE IAW SRM 51-42-06 AND INSTALLED NEW FWD LANDING ANGLE IAW SRM 51-42-06 AND DWG 601R35226 REV. P AND COMPLIED WITH TASK CARD 51-900-1003-SKY.Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2026F00037Mount · corrodedLOW PRESSURE GROUND AIR DOOR MOUNTING PLATE IS CORRODED. REMOVED AND REPLACED BY NEW MOUNTING PLATE AT LOW PRESSURE GROUND AIR DOOR, REF. SRM 51-42-06, REV. 39, AND DWG 601R35226 REV. P. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LENov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2026F00036Door Frame · corrodedUPON REMOVAL OF LOW-PRESSURE GROUND AIR DOOR STRUCTURES FOUND FRAME SECTION AT BS 589 CORRODED. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 589, S21-20L IAW SRM 51-42-06, SRM 51-42-21 REV. 39, DWG 601R36025 REV. P, AND DWG 601R35005 REV AG,Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2026F00035Angle · corrodedUPON REMOVAL OF FRAME BS 574 BETWEEN S20R AND S20L FOUND REINFORCING ANGLE CORRODED AT MULTIPLE LOCATION. REMOVED AND REPLACED BY NEW REINFORCING ANGLE AT BS 574 BETWEEN S24L TO S20L IAW SRM 51-42-06 AND SRM 51-42-21 REV. 39, AND DWG 601R36024 REV. N. PERFORNov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20260105102Door · corrodedLOW PRESSURE GROUND AIR DOOR AFT INTERNAL STRUCTURE ANGLE IS CORRODED. REMOVED AFT ANGLE IAW SRM 51-42-06 AND INSTALLED NEW AFT ANGLE IAW SRM 51-42-06 AND IAW DWG 601R35226 REV. P. PERFORMED LEAK CHECK GOOD,Nov 2, 2025 · N454SW · Cndair CL6002B19 · Air Conditioning DoorsSDR SWIA2026010531Door · corrodedLOW PRESSURE GROUND AIR DOOR FWD INTERNAL STRUCTURE IS CORRODED. REMOVED FWD ANGLE IAW SRM 51-42-06 AND INSTALLED NEW FWD ANGLE IAW SRM 51-42-06. PERFORMED LEAK CHECK GOOD.Oct 31, 2025 · N454SW · Cndair CL6002B19 · Air Conditioning DoorsSDR SWI2026F00034Skin · chafedLEFT WING LOWER SKIN CHAFED AT WS 264 WHERE FLAP FAIRING MAKE CONTACT. REPAIRED LH WING LOWER SKIN WS 264 IAW REO 601R-57-21-3988, REV-, & SKYWEST TASK CARD 51-900-1003-SKY.Oct 23, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWI2026F00033Intercostal · crackedBS 625.30, S14L, ATTACHING ANGLE FROM THE FRAME TO THE INTERCOSTAL ON THE REAR PRESSURE BULKHEAD, IS CRACKED. INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL IAW DWG 601-35012 REV D, REO 601R-53-61-422 REV NC, SRM 51-42-21, AND SKYWEST TASK CARD 51-900-1003-SKYOct 23, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2026F00032Skin · chafedLEFT WING LOWER SKIN CHAFFED AT WS127.25 WHERE FLAP FAIRING MAKE CONTACT. REPAIRED LT WING LOWER SKIN WS127.25 IAW REO 601R-57-21-3992 REV -.Oct 23, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026010523Skin · gougedRIGHT WING LOWER SKIN FRETTING AND GOUGED AT TRAILING EDGE BL45.00 WHERE FAIRING MAKES CONTACT. REPAIRED RT WING LOWER SKIN FRETTING AND GOUGE AT TRAILING EDGE BL45.00 WHERE FAIRING MAKES CONTACT REF REO 601R-57-21-880 REV-D, , DWG# 601R10046 REV. V, SRM 51-1Oct 23, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026010500020Frame · corrodedFRAME AT BS 605 AND BETWEEN S20L-18L HAS SEVERAL CORROSION AND CRACKED AT S18L. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 605 BETWEEN S20L-S18L AND WL 73 REF. DWG 601R36026 REV. AF, SRM 51-42-06 AND SRM 51-42-21, REV. 39. COMPLIED WITH TASK CARD 51-90Oct 20, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026010500017Hinge · chafedTHE LT HORIZONTAL STAB ELEVATOR HINGE NR 1 IS CHAFED/GOUGED. REPAIRED LT HORIZONTAL STAB ELEVATOR HINGE NR 1 IAW REO 601R-55-11-807 REV -. AND COMPLIED WITH TASK CARD 51-900-1003-SKY.Oct 17, 2025 · N454SW · Cndair CL6002B19 · Elevator StructureSDR SWI2026F00043Floor Support · corrodedRIGHT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409+128 AND FS559. REMOVED CORROSION ON RT FLOOR SILL BETWEEN FS409+128 AND FS559 AND FOUND TO BE WITHIN LIMITS. REF. GREO 601R-53-41-666, REV. C, DISPOSITION 1.2. COMPLIED WITH TASK CARD 5Oct 15, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20260105001Floor Support · corrodedLEFT HAND PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409 +128 AND FS559. REMOVED CORROSION ON LT FLOOR SILL BETWEEN FS409+128 AND FS559.00 AND FOUND TO BE WITHIN LIMITS. REF. GREO 601R-53-41-666, REV. -C, DISPOSITION 1.2. COMPLIED WITH TASOct 15, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2026F00031Hinge Box · chafedLEFT FLAP HINGE BOX AT WS220 AFT HINGE ATTACH FITTING CHAFED. REPAIRED LH FLAP HINGE BOX AT WS 220 AFT HINGE ATTACH FITTING IAW REO 601R-57-21-3984 REV -. AND COMPLIED WITH TASK CARD 51-900-1003-SKY.Oct 14, 2025 · N454SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWI2026F00030Rib · bentLEFT WING REAR SPAR WS 130.00 RIB IS BENT. REMOVED AND REPLACED BY NEW LH WING REAR SPAR RIB, REF. DWG 601R10339, REV. D, SRM 51-42-21, REVISION 39, AND SRM 51-42-06 REVISION 39, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.Oct 14, 2025 · N454SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWI2026F00029Retainer · chafedFWD UPPER RETAINING PLATE FOR LT WING STUB FAIRING CHAFING AGAINST FUSELAGE EXTERNAL SKIN. REPAIRED FWD UPPER RETAINING PLATE FOR LH WING STUB FAIRING (APRON SKIN) IAW REO 601R-53-41-3365 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.Oct 14, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2026F00028Access Panel · elongated11EA OBLONG HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL REPAIRED ELONGATED SCREW HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF REO 601R-55-11-812 REV. --,Oct 14, 2025 · N454SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA2026010514Access Panel · corroded2EA FASTENER HOLES WITH NOTED CORROSION ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL (MARKED). (C-CHECK RO 01/03/2026)REMOVED CORROSION ON 2EA FASTENER HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF 601R-55-11-812 REV. --, DATED:Oct 14, 2025 · N454SW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR SWI2026F00026Vane · chafedCHAFING ON RT INBD FLAP OTBD FLAP VANE ACTUATOR BODY. REPAIRED RH INBD FLAP OTBD FLAP VANE ACTUATOR BODY IAW REO 601R-57-52-2533 REV.-.Oct 13, 2025 · N454SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20260105013Vane · chafedLEFT INBD FLAP VANE LEADING EDGE IS CHAFED IN MULTIPLE LOCATIONS. LT INBOARD FLAP VANE LEADING EDGE 2 EA. AREAS BLENDED AND REPAIRED TO BE WITHIN LIMITS. REF REO 601R-57-52-004, REV -D, 2012-12-19. 1 EA. BLEND ON SKIN PANEL 601R14303-51 FOUND TO BE OUT OF LIMIOct 13, 2025 · N454SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2026F00042Floor Support · corrodedAFT CARGO FLOOR SUPPORT, RBL 9, BETWEEN BS 559+64 AND BS.559+80 HAS SPOTS OF CORROSION. BLENDED REPORTED CORROSION ON THE FLOOR SUPPORT INNER CAP FLANGE BETWEEN BS 559+64 AND BS 559+80 IAW SRM 51-21-06. BLENDED AREA WAS FOUND OUT OF LIMITED IAW SRM 53-31-43 AOct 12, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2026F00041Hinge Arm · chafedLEFT INBD FLAP OTBD HINGE ARM CHAFED ON FWD PIVOT FITTING 3EA. LOCATIONS. REPAIRED LH INBD FLAP OTBD HINGE ARM CHAFE IAW ALL STEPS OF REO REO 601R-57-54-379 REV -. SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.Oct 12, 2025 · N454SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA2026010500012Hinge Arm · chafedLH INBD FLAP INBD HINGE ARM CHAFFED ON FWD PIVOT FITTING. COMPLIED WITH REPAIR AT LH IB FLAP HINGE ARM REF. CRJ-200 REO 601R-57-54-382 REV-. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.Oct 12, 2025 · N454SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWI2026F00027Cleat · gougedFRAME TO LONGERON CLEAT AT WL73.00, RH FS484.00 IS GOUGED ON AFT SIDE AT FLOOR (C-CHECK RO 01/03/2026)BLENDED GOUGED AREA ON FRAME TO LONGERON CLEAT AT WL73.00 RH FS 484.00 REF REO 601R-53-41-3366 REV -- DATED 2025-11-04 STEPS 1 THROUGH 4. ORIGINAL THICKNESS Oct 9, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2026010509Cleat · gougedFRAME TO LONGERON CLEAT AT WL73.00, LH FS461.50 IS GOUGED ON UPPER FORWARD SIDE. REMOVED AND REPLACED BY NEW FRAME TO LONGERON CLEAT AT WL73.00, LT FS461.50 REF. DWG 601R31145 REV. -P, DWG 601R31034 REV. -F AND SRM 51-42-21, REV. 39, PERFORMED LEAK CHECK GOct 9, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWI2026F00025Floor Support · corrodedRIGHT CARGO FLOOR SILL FROM BS.559+85 TO BS 559+115, RBL 36 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALL A NEW RT CARGO FLOOR SILL, BS 559+85 - 559+115 IAW SRM 51-42-21, SRM 51-42-06, SRM 51-45-00 AND DWG 601R31133, REV J. COMPLIED WITH TASK CARD 51-9Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2026F00024Floorbeam · corrodedRBL9 HAS MULTIPLE SPOTS OF CORROSION ON TOP PLATE BETWEEN BS 409 TO BS 409+64. REPAIRED MULTIPLE SPOTS OF CORROSION ON TOP PLATE OF FLOORBEAM CAP REF SRM 53-00-43, REPAIR 2, STEP 5 A (7) FIG. 203 , REO. 601R-53-31-1354, REV--, STEPS 1 - 9, ALL OTHER REQUIREOct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2026F00023Floor Support · corrodedCORROSION ON TOP OF RBL9 BETWEEN FS513.00 TO FS529.00. REPAIRED RBL9 BETWEEN FS513 TO FS529 FLOOR SUPPORT EXTRUSION AT RBL 9.00 FS409.00+128-FS529.00. REF. REO 601R-53-41-3361 REV -, DWG 601R31005 REV. B, DWG 601R31118 REV. L, LEAK CHECK GOOD, NO LEAKS NOTEDOct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2026F00022Door Sill · corrodedAFT CARGO DOOR LOWER SILL HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 01/03/2026)AFT CARGO DOOR LOWER SILL IS REMOVED AND REPLACED WITH NEW IAW DWG 601R35011 REV. -R, SRM 51-42-06, SRM 51-42-21 AND REO 601R-53-61-593, REV. -A,Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026010508Strap · corrodedFS559.00 ON RT SIDE JUST ABOVE SILL CORRODED ON STRAP OF INNER FACE OF FRAME. REPLACED WITH NEW STRAP P/N: 601R32026-321 AT BULKHEAD ON RH SIDE @FS559.00 IAW DWG 601R32026 REV. -T, REF SRM 51-42-06, APPLIED FILLET SEAL TO PARTS REF AMM 51-23-00 AND RESTORED Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026010507Support Angle · corrodedCORROSION ON THE LOWER SUPPORT ANGLE AT FS409.00 BETWEEN STGR26L - 26R. REMOVED AND REPLACED BY NEW LOWER SUPPORT ANGLE P/N 601R32200-17 AT FS409.00 BETWEEN STGR26L - 26R REF. DWG 601R31057 REV. -J, DWG 601R32200 REV. -V, CRJ-200, SRM 51-42-06 AND CRJ-200, SROct 7, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2026F00021Skin · chafedLH AILERON LOWER LEADING EDGE CHAFFED. )REMOVED AND INSTALLED NEW LH AILERON INBOARD LOWER LEADING EDGE SKIN SHROUD P/N CC670-13053-1 REF. DWG CC670-13000 REV. -D, CRJ200 SRM 51-42-21 AND CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.Oct 6, 2025 · N454SW · Cndair CL6002B19 · AileronsSDR SWIA2026010500006Skin · chafedLEFT AILERON UPPER LEADING EDGE CHAFED. REMOVED DAMAGED LH AILERON UPPER LEADING EDGE SKIN REF. SRM 51-42-06, SRM 51-42-21 AND SRM 51-42-22 AND INSTALLED NEW LH AILERON UPPER LEADING EDGE SKIN REF. DWG CC670-13000 REV. -D, SRM 51-42-06, SRM 51-42-21 AND SOct 6, 2025 · N454SW · Cndair CL6002B19 · AileronsSDR SWIA20260105930Fairing · damaged1EA ELONGATED HOLE NOTED UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96. REPAIRED 1EA ELONGATED HOLE UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96, REF. REO REO 601R-53-31-1356 REV -.Sep 30, 2025 · N454SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA20260105927Skin · dentedRH OVERWING EMERGENCY EXIT HAS DENT ON EXTERNAL SKIN LOWER FWD CORNER (MARKED) (C-CHECK RO 01/03/2026)REPAIRED RH OVERWING EMER EXIT DENT IAW ALL STEPS OF REO 601R-52-21-172 REV -A DATED 2025-11-20. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.Sep 27, 2025 · N454SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA20260105926Skin · damagedRIGHT WING LEADING EDGE HAS A FASTENER MISSING AT OTBD JOINT SEAM AT APPROX WS 353. REPAIRED RH WING LEADING EDGE ELONGATED HOKES AT OTBD JOINT SEAM @ APROX WS353.00 IAW REO 601R-57-41-1206 REV. --,Sep 26, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWI2026F00020Frame · corrodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA92210-601R-53-61-8197 N454SW MXCODEID76131-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 92210CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L. PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OFAug 18, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2026F00019Skin · damagedPERMANENT DISPOSITION FOR BLENDED SKIN AND MISDRILL DAMAGE TO FUSELAGE SKIN BETWEEN FS559+112 €“ FS574.00 & STR15L €“ STR16L., COMPLIED WITH PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN FS559+112-FS574.00, STGR15L-STGR16L, REF. REO 601R-53-61-8417, REV. --, DATAug 18, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2026F00018Skin · damagedPERFORMED TEMPORARY REPAIR TO 4 DAMAGED RIVETS AND 1 BURN MARK ON RH SIDE OF FUSELAGE BETWEEN FS409+16 AND FS409+32, ALSO BETWEEN STR23R AND STR24R. WORK DONE IN ACCORDANCE WITH REO 601R-53-31-1134 REV A DATED: 2020-08-19. COMPLIED WITH EDDY CURRENT INSPECTIAug 18, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026010200818Not Reported · not reportedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA92498-601R-53-61-8196 MXCODEID76417-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 92498THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1700 FLIGHT HOURS FROM INCORPORATION OF REO 601R-53-61-8196., PART NUMBER: - Aug 18, 2025 · N454SW · Cndair CL6002B19 · Standard Practices/StructuresSDR SWIA202507070004A/C Pack · odorBURNING SMELL FOR 1-2 MINUTES COMING FROM CAPTAINS SIDE COCKPIT VENT. ONCE WE IDENTIFIED IT WAS COMING FROM CA SIDE VENT, SMELL STARTED TO GO AWAY ON ITS OWN WITHOUT ANY INTERVENTION. REFER TO ML 30434357 FOR REMOVAL AND REPLACEMENT OF THE LH AIR CYCLE MACHINEJul 4, 2025 · N454SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA2024092500001Landing Gear · warning messageD: GEAR DISAGREE WARNING MESSAGE, SHOWED THE RIGHT LANDING GEAR WAS NOT RETRACTED. RAN QRH AND FIXED THE PROBLEM. GOT THREE GREEN LIGHTS AND RETURNED TO PRC.C: MEL 32-30-1CAT: A DUE DATE: 1 FC TAC NOT EXCEED: 36090. ODI EVENT REQUIRES UPPER MANAGEMENT APPROVASep 24, 2024 · N454SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA202408140007Skin · puncturedPUNCTURE ON THE R/H FUSELAGE BETWEEN FS 559+96 AND 559+112 AND BETWEEN STGR 16R AND 17R MEASURING APPROX 3.5" H X 4" L. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED PERMANENT REPAIR ON R/H FUSELAGE BETWEEN FS 559+96Aug 7, 2024 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202407101Web · corrodedCORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED CLOSED) PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OF FRAME FS 574.00 BETWEEN STR20L - 21L WITH REFERENCE TO REO 601R-53-61-8197 REV A DATED 07/11/2024. PERFORMED EDDY CUJul 10, 2024 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202407120010Web · corrodedCORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSJul 10, 2024 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202407290008Skin · dentedDENT LOCATED 1.5" FORWARD OF FS 605.00 BETWEEN STR 19L AND STR 20L. (FILED CLOSED)REPAIRED DENT LOCATED 1.5" FORWARD OF FS 605.00 BETWEEN STR 19L AND STR 20L IN REF TO REO 601R-53-61-8202, REV--, DATED 2024-07-18. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.Jul 8, 2024 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
Back to N454SW