N609SK

Service difficulty reports · 373

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 = 'N609SK' 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 SWIA2026080776754Window · crackedFO SIDE WINDOW CRACKED INFLIGHT IN TWO PLACES. ONE IS AN ARC AND THE OTHER IS VERTICAL (FLIGHT 6234) TRANSFERRED TO CAMP ITEM 32787656. R & R FO SIDE WINDOW IAW AMM 56-12-01.Aug 7, 2026 · N609SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2026052976109Skin · scratchedFOUND SCRATCH ON LE SLAT 3 MEASURING 1.2"L X 0.100"W X 0.013"D. COMPLIED WITH REO 670-57-42-2512 DATED: 2026-05-29 REV: -- DISPOSITION FOR BLENDED SCRATCH DAMAGES TO OUTER SKIN OF LH SLAT #3 BETWEEN TRACK 3-3 & SS446.38. BLENDED THE SCRATCH/GOUGE DAMAGE TO A May 29, 2026 · N609SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026052976108Skin · gougedFOUND GOUGE ON LE SLAT 3 MEASURING 1.6"L X .150"W X .025"D. BLENDED SCRATCH DAMAGES TO OUTER SKIN OF LH SLAT NR 3 BETWEEN TRACK 3-3 & SS446.38. BLENDED THE SCRATCH/GOUGE DAMAGE TO A SMOOTH TRANSITION ON THE LH #3 SLAT SKIN LEADING EDGE FROM SLAT STATION NEAR May 29, 2026 · N609SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022705384Stringer · fomREMOVED STRINGER 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) TO FOM. (C-CHECK RO 02/25/2026)INSTALLED STR 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337. REFERENCE CP# 316Feb 3, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202602275365Frame · damagedREMOVED SUB-FRAME, FS 317 REFERENCE SRM 53-21-23 ITEM 34. INSTALLED SUB-FRAME BS 317 IAW SRM 51-42-06 AND SRM 51-42-21.Feb 3, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026020375360Fitting · fomREMOVED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 TO FOM. INSTALLED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.Feb 3, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026013075371Lintel · corrodedCORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN BS 333 - 343.13, STR 3L UNDERNEATH AFT SPIGOT. COMPLIED WITH REO 670-53-21-2805, REV -. REPAIR FOR CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS333.00 - FS343.13 AT STR3L (UNDERNEATH AFT SPIGOT).Jan 30, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026022705387Frame · damagedREMOVED SUB-FRAME BS 317 REFERENCE SRM 53-21-23 ITEM 34. INSTALLED SUB-FRAME BS 317 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jan 29, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202602275377Stringer · fomREMOVED STRINGER 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) TO FOM. INSTALLED STR 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jan 29, 2026 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026012975361Fitting · fomREMOVED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 TO FOM. INSTALLED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.Jan 29, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026012975105Lintel · corrodedCORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS315.95 - FS323.43 AT STR 3L (UNDERNEATH FWD SPIGOT. (C-CHECK RO 02/25/2026)REPAIRED CORROSION DAMAGE TO PAX DOOR UPPER LINTEL BETWEEN FS315.95 - FS323.43 AT STR 3L (UNDERNEATH FWD SPIGOT). COMPLIED WITH REOJan 29, 2026 · N609SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202602274765Floor Support · corrodedCOMPLY WITH REO 670-53-11-745 DATED: 2016-10-28 REV: A GENERIC REPAIR FOR NOSE FUSELAGE CENTER FLOOR ANGLE REPLACEMENT AND DOOR POST AT FS 28.00 ( LBL 11.128 AND RBL 11.128) DUE TO CORROSION FOUND ON THE DOOR POST. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670Dec 18, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F01831Angle · corrodedCOMPLY WITH REO 670-53-11-745 DATED: 2016-10-28 REV: A GENERIC REPAIR FOR NOSE FUSELAGE CENTER FLOOR ANGLE REPLACEMENT AND DOOR POST AT FS 28.00 ( LBL 11.128 AND RBL 11.128) DUE TO CORROSION FOUND ON THE DOOR POST. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGDec 18, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026022705383Floor Support · corrodedCORROSION FOUND ON FLOOR BEAM AT WL 73.00 AND RBL 9.00 FROM FS 565.00 - FS 581.00 (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-31-1142 DATED: 2025-12-16 REV"A" DISPOSITION FOR ELONGATED HOLES AND LOW E.D. CONDITION ON RBL9.0 FLOOR BEAM AND REPAIR SPLICE BNov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202602274474Buttstrap · corrodedCORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (C-CHECK RO 02/25/2026)CHAFFING UNDER FUSELAGE SKIN ON STRG 27, FS 977.00 TO 989.00 BLEND-OU AND FOUND WITHIN LIMITS IAW MHICRJ700 SRM 53-00-01-101-001-A01, L:3" W:2" D:0.016",SURFACE REPROTECTED IANov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202512011126Buttstrap · corrodedCORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (FILED CLOSED)CHAFFING UNDER FUSELAGE SKIN ON STRG 27, FS 977.00 TO 989.00 BLEND-OU AND FOUND WITHIN LIMITS IAW MHICRJ700 SRM 53-00-01-101-001-A01, L:3" W:2" D:0.016",SURFACE REPROTECTED IAW SRM CRJNov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025112800006Buttstrap · corrodedCORROSION ON BUTTSTRAP AT FS280.00 BTW STR 25R - STR 23R (FILED OPEN)Nov 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025110675378Bracket · damagedFWD FACE RH FS 280.00 BULKHEAD BRACKET ASSY, FIRE EXT HAS ELONGATED SCREW HOLES AND REQUIRES REPLACEMENT. REMOVED AND REPLACED THE FWD FACE RH FS 280 BULKHEAD BRACKET ASSY, FIRE EXT IAW SRM 51-42-06.Nov 6, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202602275372Skin · corrodedCORROSION FOUND ON INNER FUSELAGE BELLY SKIN 2 INCHES FWD OF BS 265 RIGHT NEXT TO STR 27. COMPLIED REO 670-53-11-2208, REV-. DISPOSITION FOR BLENDED CORROSION DAMAGE TO FUSELAGE SKIN PANEL NEAR BS 265 BTWN STR 26R-STR27. PERFORMED EDDY CURRENT INSPECTION WIOct 31, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202602275375Bracket · crackedBS 280 STICK PUSHER BRACKET CRACKED. REMOVED AND REPLACED THE RT FWD BS 280 STICK PUSHER BRACKET IAW SRM 51-42-06.Oct 30, 2025 · N609SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020227675364Stringer · corrodedSTRINGER 27 CORRODED BETWEEN FS 250.00 & FS 265. COMPLIED WITH REO 670-53-11-2202, REV -. REPAIRED BS 250 LOWER FRAME SECTOR BETWEEN STRINGER 27 - 25R AND STRINGER SPLICE 27. COMPLIED WITH TASK CARD 51-900-1002-SKY.Oct 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026022705379Frame · corrodedBS 250, STR 26L - STR 26R AFT FACE OF FRAME AND SKIN FLANGE CORRODED. COMPLIED WITH REO 670-53-11-2202 DATED:2025-12-16 REV: -- REPAIR TO FS250.00 LOWER FRAME SECTOR BETWEEN STR27 - STR25R AND STRINGER STR27 SPLICE.Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202602275374Floorbeam · corrodedBS 280 RT CAP ANGLE REF SRM 53-11-10, ITEM 121, CORRODED AND DISTORTED. REMOVED AND REPLACED THE BS 280 RT CAP ANGLE. WORK DONE IAW SRM 51-42-06, SRM 51-42-21, SRM 53-11-10, GREO 670-53-11-594, REV A, AND REO 670-53-11-2182, REV--.Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202510275362Floorbeam · corrodedCRAWLWAY FLOOR ANGLE SUPPORT AT FS280.00 IN AVIONICS BAY CORRODED. REMOVED AND REPLACED CRAWLWAY FLOOR SUPPORT AT FS280.00 IN AVIONICS BAY WITH REFERENCE TO SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21.Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA20202274125Floorbeam · corrodedFS280.00 RH FLOOR BEAM CORRODED (REF SRM 53-11-10 ITEM 119). (C-CHECK RO 02/25/2026)REMOVED AND REPLACED THE FS280.00 RH FLOOR BEAM. WORK DONE IN REFERENCE WITH THE CRJ-700 SRM 51-42-06, SRM 51-42-21, SRM 53-11-10 AND GREO 670-53-11-594 DATED: 2015/06/26 REV Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202602274124Floorbeam · corrodedFS280.00 LH FLOOR BEAM CORRODED (REF SRM 53-11-10 ITEM 118). (C-CHECK RO 02/25/2026)REMOVED AND REPLACED THE FS280.00 LH FLOOR BEAM. WORK DONE IN REFERENCE WITH THE CRJ-700 SRM 51-42-06, SRM 51-42-21, SRM 53-11-10 AND GREO 670-53-11-594 DATED: 2015/06/26 REVOct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2025F01456Floorbeam · corrodedFS280.00 RH FLOOR BEAM CORRODED (REF SRM 53-11-10 ITEM 119). OPEN)Oct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2025102400023Floorbeam · corrodedFS280.00 LEFT FLOORBEAM CORRODED (REF SRM 53-11-10 ITEM 118). OPENOct 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026022705382Floorbeam · crackedLEFT COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR BS 280 & LBL 11.128 AND AT WL 72.10 IS CRACKED. REMOVED AND REPLACED THE LT COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR BS 280 & LBL 11.128 AND AT WL 72.10 IAW SRM 51-42-06.Oct 16, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2025101675370Floorbeam · crackedRIGHT COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR FS 280.00 & RBL 11.128 AND AT WL 72.10 IS CRACKED. REMOVED AND REPLACED THE RH COCKPIT CENTER FLOOR PANEL LANDING/ANGLE NEAR FS 280.00 & RBL 11.128 AND AT WL 72.10 IN REFERENCE WITH THE SRM 51-42-06.Oct 16, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2025101475368Floorbeam · crackedFLOORBEAM AT BS 280 AND RBL 12 CRACKED ON THE AFT OUTBOARD FLANGE FROM APPROX WL 70.00 - WL 72.50. COMPLIED WITH REO 670-53-11-896 REV-. GENERIC REPAIR TO CENTER COCKPIT FLOORBEAM BS 280, WL70 - 72.50. AND REO 670-53-11-2195 REV -. REPAIR TO CENTER COCKPIOct 14, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026227873969Stringer · corrodedSTRINGER 21L IS CORRODED BETWEEN FS437.00 & FS453.00. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-21-2698 DATED: 2025-10-07 REV: A, REPAIR FOR CORROSION DAMAGE TO STRINGER STR21L BETWEEN FS 437.00 - FS 453.00. COMPLIED WITH TASK CARD 51-900-1002-SKY. COSep 28, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2025F01395Stringer · corrodedSTRINGER 21L IS CORRODED BETWEEN FS437.00 & FS453.00. (FILED OPEN)Sep 28, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2025092375386Hinge Arm · gougedLEFT OUTBOARD FLAP. INBOARD HINGE ARM (WS178.00) HAS GOUGES ON EDGE OF HOUSING FOR SPHERICAL BEARING. REPAIRED DAMAGE ON LH OUTBOARD FLAP. INBOARD HINGE ARM (WS178.00) IN COMPLIANCE WITH REO 670-57-53-428 REV-- DATED 2025-09-26. PERFORMED EDDY CURRENT INSPECTISep 23, 2025 · N609SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2025092375359Floorbeam · corrodedLEFT & RIGHT BS 280, COCKPIT FLOOR POST REINFORCEMENT PLATE/SKIN HAS CORROSION. COMPLIED WITH REO 670-53-11-2182 REV--. DISPOSITION FOR RE-INCORPORATION OF BULKHEAD LOWER WEB REPAIR AT FS280.00 (LHS AND RHS) PER SRM TASK 53-11-10-201-004-A01 (GREO 670-53-11-5Sep 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202602275358Skin · chafedRH INBOARD FLAP LOWER SKIN HAS CHAFE DAMAGE AT INBOARD INTERFACE OF FAIRING. (C-CHECK RO 02/25/2026)REPAIRED RH INBOARD FLAP LOWER SKIN WITH REFERENCE TO SRM 57-52-01 AND REO 670-57-52-628 REV "--" DATED 2025-10-15. REPLACED RH INBOARD FLAP LOWER SKIN WITH Sep 22, 2025 · N609SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2025091875385Hinge Fitting · gougedLEFT WING #5 FLAP HINGE BOX AFT IB ATTACHMENT FITTING LUG IS GOUGED. BLENDED GOUGE ON LT WING NR 5 FLAP HINGE BOX AFT IB ATTACHMENT FITTING LUG IN REFERENCE TO SRM 51-12-00. PERFORMED EDDY CURRENT IN REFERENCE TO NDTM 51-20-006 AND FOUND REWORKED AREA TO BE CSep 18, 2025 · N609SK · Cndair CL6002C10 · Wing Main, Frame StructureSDR SWIA2025091675369Floorbeam · corrodedFWD CENTER FLOOR PANEL SUPPORT ANGLE AT FS280.00 HAS SURFACE CORROSION. REMOVED AND REPLACED THE FWD CENTER FLOOR PANEL SUPPORT ANGLE AT BS 280 IAW SRM 51-42-06, SRM 53-11-10 AND SRM 53-11-43 .Sep 16, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2025090375391Roller · damagedRH SLAT TRACK ROLLER 1-2 OUTBOARD AFT SIDE ROLLER HAS FLAT SPOTS. REPLACED RH 1-2 OUTBOARD AFT SIDE SLAT TRACK ROLLER AS PER AMM 27-81-44. SEE TASK CARD 27-630-101 IN CP 30270403-1 FOR OPS CHECK.Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2025090375390Roller · wornRIGHT SLAT TRACK 3-2 INBD AFT SIDE ROLLER IS WORN. REMOVED AND REPLACED RT SLAT TRACK 3-2, INBD AFT SIDE ROLLER IN REFERENCE TO AMM 27-81-44.Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022705389Roller · damagedLEFT SLAT TRACK 2-2 INBOARD FORWAD SIDE ROLLER IS FLAT SPOTTED. REMOVED AND REPLACED LT SLAT TRACK 2-2 INBOARD FORWARD SIDE ROLLER IN REFERENCE TO AMM 27-81-44.Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022705388Roller · damagedL/H SLAT TRACK 1-2 INBOARD AFT SIDE ROLLER IS FLAT SPOTTED. (C-CHECK RO 02/25/2026)REMOVED AND REPLACED L/H SLAT TRACK 1-2 INBOARD AFT SIDE ROLLER, REFERENCE CP 30270403 FOR COMPLETION OF TASK CARD 27-520-120.Sep 3, 2025 · N609SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026022705380Frame · damagedREMOVED FRAME SEGMENT 18-20L STGR FS 295.00 TO FACILITATE REPLACEMENT OF STGR 20L. INSTALLED FRAME SEGMENT BS 295, STGR 18L - STGR 20L IAW SRM 51-42-06, SRM 51-42-21 AND REO 670-53-21-2688 REV--. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM 53-0Aug 28, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2026022775381Stop Fitting · crackedPAX DOOR SURROUND FWD UPPER STOP BRACKET IS CRACKED. REMOVED AND REPLACED PAX DOOR SURROUND FWD UPPER STOP BRACKET WITH REFERENCE TO SRM 51-42-21.Aug 27, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202602273555Door Frame · crackedAFT BAGGAGE BAY DOOR CUTOUT SURROUND STRUCTURE FS1047.00 LOWER CHANNEL CRACKED (SRM 53-61-58 ITEM 16). (C-CHECK RO 02/25/2026)REMOVED AND REPLACED AFT BAGGAGE BAY DOOR CUTOUT SURROUND STRUCTURE FS1407.00 LOWER CHANNEL (SRM 53-61-58 ITEM 16) WITH REFERENCE TO Aug 26, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025082700006Channel · crackedAFT BAGGAGE BAY DOOR CUTOUT SURROUND STRUCTURE FS1047.00 LOWER CHANNEL CRACKED (SRM 53-61-58 ITEM 16). (FILED OPEN)Aug 26, 2025 · N609SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202602275357Skin · dentedDENT ON FUSELAGE SKIN BETWEEN FS349.00 AND FS 364.00 AND BETWEEN STGR 22L AND STGR 23L. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-21-2681 DATED: 2025-08-28 REV -- PERMANENT DISPOSITION FOR REWORKED DENTS ON LOWER FUSELAGE SKIN BETWEEN FS349.00 - FS409.Aug 23, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2025082075376Hinge Fitting · gougedPAX DOOR FUSELAGE SIDE HINGE AFT LUG LANDING HAS A SMALL GOUGE FROM HINGE PIN RETAINER PIN CONTACT/WEAR. PERFORMED REPAIR OF PAX DOOR FUSELAGE SIDE HINGE AFT LUG LANDING WITH REFERENCE TO REO 670-53-21-582 REV "-G" DATED 2024-02-18 TYPE IV: DISPOSITION FOR Aug 20, 2025 · N609SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2025082075373Doubler · gougedTWO SMALL SCREW GOUGES ON A DOUBLER AT STGR 27 BETWEEN BS 969 AND 985 ON THE EXTERIOR OF THE AIRCRAFT. COMPLIED WITH REO 670-53-61-352, REV A. REPAIRED THE FUSELAGE SKIN AT BS 977 AND STR 27 BY REMOVING AND REPLACING A NEW SERVICEABLE DOUBLER. MAJOR REPAIR.Aug 20, 2025 · N609SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2025081375366Mount · brokenGALLEY 1, MOST AFT INBD MOUNTING NUT PLATE IS BROKEN. UPON INSPECTION FOUND THE NUTPLATE BROKEN AND GALLEY 1, MOST AFT INBD MOUNTING FITTING ASSEMBLY TO BE CORRODED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED THE GALLEY 1, MOST AFT INBD MOUNTING FITTING ASAug 13, 2025 · N609SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
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