N780SK

Service difficulty reports · 126

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 = 'N780SK' 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 SWIA20230613006Unknown · crackedR/H LOWER TRANSCOWL LATCH COAMING IS CRACKED. (C-CHECK RO 6/9/2023) REPAIRED TRANSCOWL REF REO 670-54-21-1207 REV A DATED 2015-08-27 . COMPLIED WITH SKYCARD 51-900-1002.Apr 26, 2023 · N780SK · Cndair CL6002C10 · Powerplant SystemSDR SWIA20230613005Unknown · crackedR/H UPPER TRANSCOWL INBD "A" STANDOFF BRACKET IS CRACKED. (C-CHECK RO 6/9/2023) INSTALLED NEW "A" BRACKET INTO R/H UPPER TRANSCOWL (PN CN624-2082-201) REF REO# 670-54-21-971, REV A, DATED 5/11/17. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.Apr 26, 2023 · N780SK · Cndair CL6002C10 · Powerplant SystemSDR SWIA20230613004Unknown · crackedL/H LOWER TRANSCOWL INBD "A" STANDOFF CRACKED. (C-CHECK RO 6/9/2023) REMOVED CRACKED I/B STAND-OFF ANGLE P/N CN624-2082-201 FROM L/H LOWER TRANSCOWL, REF. CRJ700 SRM 51-42-28-001-001-A01. INSTALLED NEW I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWERApr 26, 2023 · N780SK · Cndair CL6002C10 · Powerplant SystemSDR SWIA20230613003Unknown · chafedL/H LOWER TRANSCOWL INNER LATCH COAMING CHAFED AT FWD COWL EDGE. (C-CHECK RO 6/9/2023) REMOVED AND REPAIRED DAMAGE FROM L/H LOWER TRANSCOWL INNER LATCH COAMING AT FWD. EDGE PER REO 670-54-21-1028, REV. NC, DATED 2009-06-15 AND CRJ700SRM 51-42-10-001-001Apr 26, 2023 · N780SK · Cndair CL6002C10 · Powerplant SystemSDR SWIA20230613002Unknown · chafedL/H UPPER TRANSCOWL INNER LATCH COAMING CHAFED AT FWD COWL EDGE. (C-CHECK RO 6/9/2023) REPAIRED L/H UPPER TRANSCOWL INNER LATCH COAMING CHAFE AT FWD COWL EDGE PER REO 670-54-21-1028 REV NC DATE 2009-06-15. RIG CHECK GOOD. FUNCTIONAL TEST GOOD. OPS TEST Apr 26, 2023 · N780SK · Cndair CL6002C10 · Powerplant SystemSDR SWIA20230613001Unknown · gougedLH MLG SIDE STAY FITTING HAS GOUGES ON LOWER INBOARD SIDE (MARKED IN RED) (C-CHECK RO 6/9/2023) REPAIRED LH MLG SIDE STAY FITTING PER MHIRJ REO 670-57-11-193 REV-- DATE: 2023-05-05. SEE CONTINUATION CARD FOR DETAILSApr 26, 2023 · N780SK · Cndair CL6002C10 · Landing Gear SystemSDR SWIA202306130425Unknown · chafedDURING AUDIT OF 1C TASK CARD 54-440-301 (INTERNAL ZONAL INSPECTION OF THE RIGHT NACELLE), FOUND RH ENGINE UPPER FWD. CORE COWL T/E CHAFED AT LATCH SIDE OF DOOR. (C-CHECK RO 6/9/2023) REMOVED CHAFE ON RH ENGINE UPPER FWD CORE COWL T/E AT LATCH SIDE OF DOApr 25, 2023 · N780SK · Cndair CL6002C10 · Standard Practices/StructuresSDR SWIA2023061300425Unknown · dentedPROTRUDING DENT ON EXTERNAL AIRCRAFT SKIN BETWEEN FS 280.00 - 295.00, STGR 26L - 25L (C-CHECK RO 6/9/2023) DRESSED BACK PROTRUDING DENT BETWEEN FS280.00-FS295.00 STR25L-STR26L. ENSURED NO OIL CANNING POST HAND DRESS. DIMENSIONS POST DRESS BACK MEASURES Apr 25, 2023 · N780SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA20230613423Unknown · crackedFWD EQUIPMENT COMPARTMENT - R/S SILL CRACKED AT AFT DOOR LATCH RECEPTACLE (C-CHECK RO 6/9/2023) INSTALLED NEW DOOR LANDING/SILL BACK ONTO AIRCRAFT AT R/H SIDE FWD EQUIPMENT COMPARTMENT. REF: CRJ-700 S.R.M. 51-42-06-001-001-A01,51-42-13-001-001-A01, DWGApr 23, 2023 · N780SK · Cndair CL6002C10 · DoorsSDR SWIA2023061300423Unknown · frayedAFT BAGGAGE BAY FWD CURTAIN SUPPORT BEAM HAS BEEN FRAYED FROM CABLE. FLAGGED (C-CHECK RO 6/9/2023) REPLACED AFT BAGGAGE BAY FWD CURTAIN SUPPORT BEAM WITH NEW PN MM670-35502-14S PO# 10277-0009 AFTER FOUND OUT OF LIMIT PER CRJ 700 SRM 53-00-00-101-001-A0Apr 23, 2023 · N780SK · Cndair CL6002C10 · DoorsSDR SWIA202265544None · failedLEFT FADEC CAUTION ON DEPARTURE. PERFORMED QRH. ENG IND NORMAL AT IDLE. (FLIGHT 5721 - FILED CLOSED) PLEASE REFERENCE AML 898483 FOR REMOVAL AND INSTALLATION OF THE LEFT FADEC AND PLEASE REFERENCE AML 898484 FOR THE OPS CHECK OF THE LEFT FADEC. / PERMay 1, 2022 · N780SK · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR SWIA202265369None · failedBLEED AIR DUCT WARNING AT FL290 RAN QRH AND STARTED EMERGENCY DESCENT. (FLIGHT 5579 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24657255 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH FLEET COORDINATOR REQUEST TO PERFORM RIL 5458.Apr 13, 2022 · N780SK · Cndair CL6002C10 · Pneumatic SystemSDR SWIA2020040850061Bulkhead · corrodedCORROSION ON LH FS 280 BULKHEAD LOWER WEB. (C-CHECK) RO 4/6/2020 INSTALLED NEW LOWER BULKHEAD WEB LH FS 280.00. REF REO. COMPLIED WITH SKYCARD STRUCTURAL MAJOR REPAIR (**RII**) AND M-337 FORMMar 12, 2020 · N780SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2020040850063Support Angle · crackedBULKHEAD VIRTICAL SUPPORT ANGLE CRACKED FS 280 RBL 26 (C-CHECK) RO 4/6/2020 REPLACED WITH NEW VERTICAL SUPPORT ANGLE PN CC670-34117-6 FS 280 RBL 26 REF CRJ 700 SRMMar 10, 2020 · N780SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2020400850060Bulkhead · corrodedCORROSION ON RH 280 BULKHEAD LOWER WEB (C-CHECK) RO 4/6/2020 REMOVED AND REPLACED 1EA RH 280 BULKHEAD WEB REF REO. COMPLIED WITH M-337 FOR MAJOR REPAIR.Mar 10, 2020 · N780SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2020040850059Floorbeam · corrodedFS 280.00 LH AND RH FLOOR BEAMS CORRODED. (C-CHECK) RO 4/6/2020 REMOVED AND INSTALLED 1EA NEW RH 280 FLOOR BEAM REF CRJ 700 SRM AND DWG REMOVED AND INSTALLED NEW L/H FS 280.00 BULKHEAD FLOOR BEAM. REF BOMBARDIER DRAWING. COMPLIED WITH SKYCARD (CL600-2C10)Mar 7, 2020 · N780SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2020040850075Fitting · corroded* CORROSION DETECTED ON FUSELAGE FLOOR STRUCTURE AT PAX DOOR OPENING, ON FWD AND AFT DOOR HINGE CUP FITTINGS, AROUND FLOOR BOARD NUT/PLATE HOLES (MARKED). (C-CHECK) RO 4/6/2020 REMOVED CORROSION PER CRJ 700 SRM. ORIGINAL MATERIAL THICKNESS FWD CLOSING FITMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850074Frame · corroded* FRAME AT FS1047 LH HAS CORROSION ON INBD FLANGE JUST ABOVE FLOOR LEVEL (C-CHECK) RO 4/6/2020 INB. FLANGE (BRACKET P.N. MM670-34112-013) FOUND OUT. OF LIMITS. REMOVED AND REPLACED. REF CRJ700 SRM.Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020040850073Angle · corroded* CORROSION DETECTED ON SERVICE DOOR , LWR DOOR SEAL "STRIKER" ANGLE ON LWR SILL STRUCTURE, THAT FLOOR PROTECTOR PLATE ATTACHES TO, IN SEVERAL LOCATIONS (MARKED). (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON SERVICE DOOR. LWR DOOR SEAL €ŒSTRIKER€? ANGLE ONMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850072Seat Track · corroded* LH SIDE SEAT RAIL CORRODED FROM APROX FS 673 TO FS 711 MARKED (C-CHECK) RO 4/6/2020 REMOVED CORROSION AT MULTIPLE SPOTS ON LH SIDE SEAT RAIL APROX FS673 TO FS711 IAW. BLENDED OUT CORROSION IN MULTIPLE AREAS ON SIDE SEAT RAIL. NO MORE THAN ONE TYPE OF DAMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850071Support Angle · corroded* AV BAY FORWARD FLOOR BOARD SUPPORT ANGLE CORRODED AT FS280 BETWEEN LBL 7 AND RBL 7 (C-CHECK) RO 4/6/2020 REMOVED CORROSION REF CRJ 700 SRM. ORIGINAL THICKNESS IS .050,MATERIAL LOSS IS .006 AND MATERIAL REMAINING IS .044 FOUND TO BE OUT OF LIMIT PER CRJ Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850070Seat Track · corroded* LH SEAT RAIL FROM FS 581 TO FS 693 PITTED AND CORRODED LBL 9 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON LH SEAT RAIL AT FS 581 TO FS 693 AT LBL 9 IAW CRJ700 SRM. MATERIAL REMOVED AFTER BLEND .038" MAXIMUM ALLOWABLE DAMAGE .035" SEAT RAIL OUT OF LIMITS.Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850069Seat Track · corroded* RH SEAT RAIL FROM FS 581 TO FS 693 PITTED AND CORRODED RBL 9 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON RH SEAT RAIL AT FS 581 TO FS 693 AT RBL 9 IAW CRJ 700 SRM. MATERIAL REMOVED AFTER BLEND .045" MAXIMUM ALLOWABLE DAMAGE .035" SEAT RAIL OUT OF LIMITSMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850068Seat Track · corroded* LH SEAT RAIL FROM FS 501 TO FS 581 PITTED AND CORRODED LBL 9 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON LH SEAT RAIL AT FS 501 TO FS 581 AT LBL9 IAW CRJ 700 SRM. MATERIAL REMOVED AFTER BLEND .046" MAXIMUM ALLOWABLE DAMAGE .035" SEAT RAIL OUT OF LIMITSMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850067Seat Track · corroded* RH SEAT RAIL FROM FS 501 TO FS 581 PITTED AND CORRODED RBL 9 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON RH SEAT RAIL AT FS501 TO FS581 AT RBL9 IAW CRJ700 SRM. MATERIAL REMOVED AFTER BLEND .039" MAXIMUM ALLOWABLE DAMAGE .035" SEAT RAIL OUT OF LIMITS. REMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850066Seat Track · corroded* LH SEAT RAIL FROM FS 379 TO FS437 PITTED AND CORRODED LBL (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON LH SEAT RAIL AT FS 379 -437 AT LBL 27 IAW CRJ 700 SRM. / MATERIAL REMOVED IS NOT ALLOWED ON SEAT RAIL AREA. REPLACE SEAT RAIL AT LH LBL27 FS379 - FS437 Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850062Door Sill · corroded* AFT CARGO DOOR SILL IS CORRODED REJECTION COMMENTS: MISSING REF (C-CHECK) RO 4/6/2020 REMOVED AND REPLACED AFT CARGO DOOR SILL, REF CRJ 700 SRM AND BOMBARDEIR DWG. COMPLIED WITH SKYWEST TASK CARD STRUCTURAL MAJOR REPAIR AND M-337.Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850058Frame · corroded* FRAME 549 CORRODED AFT SIDE ABOVE FWD BAGGAGE BAY DOOR MARKED (C-CHECK) RO 4/6/2020 REMOVED CORROSION AND SOLID RIVETS (3 EA) AT FRAME 549 AFT ABOVE FWD BAGGAGE BAY DOOR REF. CRJ700 SRM ORIGINAL THICKNESS WAS .050". NDT MEASURED REMAINING THICKNESS AMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020040850057Door Sill · corroded* CORROSION DETECTED ON R/H FLOOR "SILL" BEHIND GALLEY #1 AREA, BETWEEN F.S. 280.00 AND F.S. 319.70. (2) PLACES BETWEEN F.S. 280.00 AND 295.00 AND (2) PLACES BETWEEN F.S. 310.00 AND 319.70, (MARKED). (C-CHECK) RO 4/6/2020 REPLACED FLOOR SILL BEHIND GALLEY Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850056Door Sill · corroded* AFT CARGO DOOR SILL IS CORRODED (C-CHECK) RO 4/6/2020 REPLACED AFT CARGO DOOR SILL AS PER CRJ 700 SRM.Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850055Floor Support · corroded* CORROSION ON LBL9 LONGITUDINAL FLOOR BEAM AT FS1031 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON LBL 9 LONGITUDINAL FLOOR BEAM AT FS 1031.00. REF CRJ700 SRM ORIGINAL MATERIAL THICKNESS AT BLENDED AREAS OF LBL 9 FLOOR BEAM IS 0.120" PER BOMBARDIER DRAWING. Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850054Floor Support · corroded* CORROSION ON LBL27 LONGITUDINAL FLOOR BEAM AT FS1031 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON LBL 27 LONGITUDINAL FLOOR BEAM AT FS 1031.00. REF CRJ700 SRM ORIGINAL MATERIAL THICKNESS AT BLENDED AREAS OF LBL 27 FLOOR BEAM IS 0.120" PER BOMBARDIER DRAWIMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850053Intercostal · corroded* IN AV BAY LH INTERCOSTAL CORRODDED INBD AND OUTBD SIDES AT APROX LBL 3 BETWEEN FS 349 AND FS 364.0 MARKED (C-CHECK) RO 4/6/2020 REPLACED INTERCOSTAL AT LBL3 BETWEEN FS 349.00 AND FS364.00 AS PER CRJ 700 SRM AND DWG SKYWEST TASK CARD COMPLIED WITH. COMPLIMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850052Intercostal · corroded* IN AV BAY RH INTERCOSTAL CORRODDED INBD AND OUTBD SIDES AT APROX RBL 3 BETWEEN FS 349 AND FS 364.0 MARKED (C-CHECK) RO 4/6/2020 REPLACED RH INTERCOSTAL AT RBL 3 FS 349.00 TO FS 364.00 AS PER CRJ 700 SRM & DWG COMPLIED WITH SKYCARD (CL600-2C10) STUCTURAL Mar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850051Support Angle · corroded* FLIGHT DECK FLOOR BOARD SUPPORT ANGLE CORRODED AT FS280 BETWEEN LBL9 AND RBL 9 (C-CHECK) RO 4/6/2020 REMOVED AND INSTALLED NEW FLIGHT DECK FLOOR BOARD SUPPORT ANGLE. REF. BOMBARDIER DRAWING COMPLIED WITH SKYCARD (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RMar 5, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850065Seat Track · corroded* RH SEAT RAIL FROM FS 349 TO FS 501 PITTED AND CORRODED RBL 9 (C-CHECK) RO 4/6/2020 REMOVED CORROSION ON RH SEAT RAIL AT FS 349 TO FS 501 IAW CRJ700 SRM. MATERIAL REMOVED IS NOT ALLOWED ON SEAT RAIL AREA. REPLACE SEAT RAIL. IAW CRJ700 SRM. INSTALLED NEW Mar 4, 2020 · N780SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020040850064Door Sill · corroded*GALLEY SERVICE DOOR SILL HAS SERVERAL AREA'S OF CORROSION. FLAGGED (C-CHECK) RO 4/6/2020 REPLACED GALLEY SERVICE DOOR SILL AS PER CRJ 700 SRMFeb 27, 2020 · N780SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020040850050Skin Panel · damagedD: DAMAGE TO LH WINGLET OUTBOARD SKIN PANEL. COMPLIED WITH TEMPORARY REPAIR PER REO, PERMANENT REPAIR DUE WITHIN 5750 FH PER REV A OF REO. PERMANENT REPAIR DUE BY TAT 31330.1 C: MCI RA# 41829 NOTE: BUILT MX CODE TO TRACK 800 FLT HRS REINSP ***** DO NOT Feb 16, 2020 · N780SK · Cndair CL6002C10 · Wing, Plate/SkinSDR SWIA2019111246761Engine · malfunctionedWHILE SETTING THRUST FOR TAKEOFF, THE ENGINE NEVER SPOOLED UP PAST 56% N1, EVEN WHEN INSIDE THE CLIMB DETENT. ABORTED TAKEOFF, COMPLIED WITH REJECTED TAKEOFF QRH PROCEDURE, AND RETURNED TO GATE. FLIGHT # 5341 CLOSED VERIFIED ABORTED TAKE-OFF INSPECTION NOT Nov 12, 2019 · N780SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201743175Skin · damagedMULTIPLE FASTENER HOLES IN THE FUSELAGE SKIN ELONGATED, BS 310 BETWEEN STRINGER 26L AND 26R. REPAIRED IAW REO. NO DEFECTS NOTED IAW AMM.Mar 22, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA201743174Stringer · corrodedCORROSION FOUND ON STRINGER 26R BETWEEN BS 319.7 AND 333. INSTALLED A NEW STRINGER IAW SRM.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743173Stringer · corrodedCORROSION FOUND ON STRINGER 25R BETWEEN BS 319.7 AND 333. INSTALLED A NEW STRINGER IAW SRM.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743172Longeron · corrodedCORROSION FOUND ON THE LONGERON BETWEEN BS 333 AND 349 COMMON TO STRINGER 25R. INSTALLED NEW SERVICEABLE LONGERON IAW SRM.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743171Stringer · corrodedCORROSION FOUND ON STRINGER 26R BETWEEN BS 333 AND 364. INSTALLED NEW SERVICEABLE STRINGER IAW SRM.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743170Frame · corrodedCORROSION FOUND ON THE FRAME AT BS 310 BETWEEN STRINGERS 26L AND 25R. REPAIRED IAW REO.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201743169Frame · corrodedCORROSION FOUND ON THE FRAME AT BS 295 BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW REO.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201743168Frame · corrodedCORROSION FOUND ON FRAME AT BS 319.7 BETWEEN STRINGERS 26L AND 26R. COMPLIED WITH ALL STEPS FOR PERMANENT REPAIR IAW REO.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201743167Frame · corrodedCORROSION FOUND ON FRAME AT BS 333 BETWEEN STRINGER 26L AND 26R. COMPLIED WITH ALL STEPS FOR PERMANENT REPAIR IAW REO.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201743166Frame · corrodedCORROSION FOUND ON FRAME AT BS 364 BETWEEN STRINGERS 25 AND 27R. COMPLIED WITH ALL STEPS FOR PERMANENT REPAIR IAW REO.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201743165Attach Angle · corrodedCORROSION FOUND ON THE RT ATTACH ANGLE BETWEEN BS 349 AND 364 COMMON TO STRINGER 26R. REMOVED AND INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW SRM.Mar 19, 2017 · N780SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
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