N752SK

Service difficulty reports · 213

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 = 'N752SK' 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 SWIA2020061051068Floor Support · crackedRT COCKPIT FLOOR SUPPORT ANGLE AT BL 12 (P/N CC670-33199-4) IS CRACKED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CRACKED RT COCKPIT FLOOR SUPPORT ANGLE WITH NEW FLOOR SUPPORT ANGLE (P/N CC670-33199-4) AT RBL 12, FS 259.20 TO FS 280.00 REF SRM, DWG. RESTOREMay 15, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051067Floor Support · crackedLT COCKPIT FLOOR SUPPORT ANGLE AT BL 12 (P/N CC670-33199-3) IS CRACKED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CRACKED LT COCKPIT FLOOR SUPPORT ANGLE WITH NEW FLOOR SUPPORT ANGLE (P/N CC670-33199-3) AT LBL 12, FS 259.20 TO FS 280.00 REF SRM, DWG. RESTOREMay 15, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051066Stringer Splice · corrodedHEAVY EXFOLIATION CORROSION FOUND ON STR 21L JOINT PIECE AT FS333.00. (C-CHECK) RO 4/24/2020 REMOVED AND INSTALLED NEW STR SPLICE AT FS 333.0 STGR 21L REF SRM & DWG. COMPLIED WITH TASK CARD. LEAK CHECK GOOD.May 14, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051065Frame · corrodedMAIN AVIONICS BAY FS364.00 LOWER MACHINED FRAME BETWEEN STR 27 AND STR 25R HAS PITTING CORROSION. (C-CHECK) RO 4/24/2020 EVALUATED MAIN AVIONICS BAY FS364.00 LOWER MACHINED FRAME BETWEEN STR 27 AND STR 25R, FOUND TO BE OUT OF LIMITS, REF SRM. COMPLETED FRAME May 14, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020061051064Stringer · corrodedMAIN AVIONICS BAY STR 26L BETWEEN FS333.00 AND FS349.00 CORRODED. (C-CHECK) RO 4/24/2020 CORROSION ON STR 26L BETWEEN FS333.00 AND FS349.00 FOUND TO BE OUT OF LIMITS. REF SRM. REMOVED AND INSTALLED NEW STR 26L FROM FS333.00 TO FS64.00. REF SRM AND DWG. LEAK CMay 13, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051063Splice · corrodedFS 280 UPPER SPLICE STRIP CORRODED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CORRODED FS 280.0 BL 0.0 UPPER SPLICE STRIP WITH NEW PART, LOCATED, DRILLED AND INSTALLED NEW UPPER SPLICE STRIP, REF SRM AND DWG.May 10, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051062Floorbeam · corrodedFS 280 LT AND RT FLOORBEAMS, CORROSION FOUND ON WEB ELEMENT BETWEEN LBL11 AND RBL11. (C-CHECK) RO 4/24/2020 REMOVED FS 280.0 LT AND RT FLOORBEAM, LOCATED DRILLED AND INSTALLED NEW FS 280.0 RT AND LT FLOORBEAMS, REF SRM AND DWG. COMPLIED WITH TASK CARD STRUCTMay 10, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2020061051061Frame · corrodedAFT SIDE OF FRAME AT FS 319.70 AND STR 21L HAS HEAVY CORROSION. (C-CHECK) RO 4/24/2020 REMOVED CORROSION AND EVALUATED AT FS319.70, FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND INSTALLED NEW FRAME AT FS319.70 BETWEEN STR18L AND STR21L. REF SRM AND DWG. LEAKMay 9, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020061051080Seat Track · corrodedRBL9 FLOOR SEAT TRACK CORRODED FROM FS 349 TO FS 477. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT RAIL FS350-FS485 RBL9 REF AMM.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051060Gusset · corrodedFS 1051 STGR 20L CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED FS 1051 STGR 20L CORNER GUSSET, REF REO, DWG, SRM. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR FOR COMPLIANCE WITH FORM M-337 SEE JOB 71020995.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051059Gusset · corrodedFS 1051 STR 25R CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CORNER GUSSET AT FS 1051 COMMON TO STR 25R WITH NEW, REF SRM AND DWG. COMPLIED WITH TASK CARD FOR STRUCTURAL MAJOR REPAIR FORM 337 CAPTURED ON JOB 71020995.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051058Gusset · corrodedFS 1051 STR 26R CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED FS 1051 STR 26R CORNER GUSSET, REF SRM, DWG AND REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR FOR COMPLIANCE WITH FOR M-337 SEE JOB 71020995.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051057Gusset · corrodedFS 1015 STGR 25R GUSSET AND STRINGER CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1015 STR 25R, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM S6144-32 PO T54399 RMay 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051056Gusset · corrodedFS 1015 STGR 26R GUSSET AND STRINGER CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1015 STR 26R, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM S6144-32 PO T54399 May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051055Gusset · corrodedFS 1015 STGR 27 GUSSET AND STRINGER CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1015 STR 27, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM S6144-32 PO T54399 REFMay 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051054Gusset · corrodedFS 1015 STGR 26L CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1015 STR 26L, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM 7075-T62 PO T54399 REF DWG.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051053Gusset · corrodedFS 1015 STGR 23L CORNER CUSSET CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1015 STR 23L, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM 7075-T62 PO T54399 REF DWGMay 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051052Gusset · corrodedFS 1015 STGR 20L DORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1015 STR 20L, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM 7075-T62 PO T54399 REF DWG.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051051Gusset · corrodedFS 1000 STGR 23R CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1000 STR 23R, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM S3144-32 PO T000051222 REF May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051050Gusset · corrodedFS 1000 STGR 26R CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1000 STR 26R, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM S3144-32 PO T000051222 REF May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051049Gusset · corrodedFS 1000 STGR 24L CORNER GUSSET CORRODED. (C-CHECK) RO 4/24/2020 EVALUATED CORROSION FROM CLIP AT FS1000 STR 24R, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS REF SRM. COULD NOT AQUIRE A NEW CLIP SO FABRICATED REPLACEMENT CLIP FROM 7075-T62, .040" PO T0000543May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051048Gusset · dentedBS 1000, STRINGER 19L, CORNER GUSSET DENTED. FABRICATED REPLACEMENT GUSSET IAW DWG AND SRM. REMOVED AND REPLACED THE GUSSET IAW DWG AND SRM.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051047Gusset · corrodedBS 985, STRINGER 26R CORRNER GUSSET CORRODED. REMOVED CORROSION IAW SRM AND FOUND TO BE OUT OF LIMITS. FABRICATED A REPLACEMENT IAW DWD. REMOVED THE GUSSET IAW DWG AND SRM.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051046Gusset · corrodedBS 985, STRINGER 20L CORNER GUSSET CORRODED. REMOVED CORROSION IAW SRM AND FOUND TO BE OUT OF LIMITS. FABRICATED REPLACEMENT GUSSET IAW DWG. REMOVED AND REPLACED IAW DWG AND SRM.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051045Support · corrodedBACK UP SILL AT STRINGER 21L BETWEEN BS 310 AND 319 WAS CORRODED. EVALUATED AND FOUND TO OUT OF LIMITS IAW SRM. REMOVED AND REPLACED IAW SRM, DWG SH670-31630, REV K, AND DWG, PRESSURE CHECKED GOOD.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051044Support · corrodedBACK UP SILL AT STR21L BETWEEN FS333.00 AND FS349.00 IS CORRODED. REMOVED AND IAW SRM, DWGS. LEAK CHECKED GOOD.May 7, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051079Seat Track · corrodedTHE SEAT TRACK SECTION AT LBL9.00 FROM FS485.00 TO FS581.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT RAIL FS485-FS581 LBL9 REF AMM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051078Seat Track · corrodedTHE SEAT TRACK SECTION AT RBL9.00 FROM FS485.00 TO FS581.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT RAIL FS485-FS581 RBL9 REF AMM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051077Seat Track · corrodedTHE SEAT TRACK SECTION AT RBL9.00 FROM FS581.00 TO APPROX FS693.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT RAIL FS581-FS693 RBL9 REF AMM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051076Seat Track · corrodedTHE SEAT TRACK SECTION AT LBL9.00 FROM FS581.00 TO APPROX FS693.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT RAIL FS581-FS693 LBL 9 REF SRM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051075Seat Track · corrodedFS847.00 FS969.00 RBL 9 PASSENGER FLOOR SEAT TRACK HAS CORROSION AROUND SEVERAL FASTENERS. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FS 847.00 TO FS 969.00 AT RBL 9 REF SRM, AMM. SEE CONTINUATION FOR DETAILS.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051074Seat Track · corrodedFS847.00 - FS969.00 LBL 9 PASSENGER FLOOR SEAT TRACK HAS CORROSION AROUND SEVERAL FASTENERS. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FS 847.00 TO FS 969.00 AT LBL 9 REF SRM. SEE CONTINUATION FOR DETAILS.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020061051069Support Angle · crackedFS280 CABIN SIDE FLOOR SUPPORT STRUCTURE CLIP ANGLE FOR INTERCOSTAL AT APPROXIMATELY LBL 12 : SUSPECT CRACK IN RADIUS. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CLIP ANGLE FOR FLOOR SUPPORT INTERCOSTAL AT FS280 APPROX LBL 12 REF SRM. NDT VERIFIED SUPPORT AMay 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051043Intercostal · corrodedBS 349 - 364 INTERCOSTAL AT STRINGER 26R CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW DWG AND SRM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051042Intercostal · corrodedBS 349 - 364 INTERCOSTAL BETWEEN STRINGERS 26 - 27R CORRODED. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM, AND DWG. PRESSURE LEAK CHECKED GOOD.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051041Stringer · corrodedBS 333 - 349, STRINGER 25R WAS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND INSTALLED A NEW STRINGER IAW SRM AND DWG. LEAK CHECKED GOOD.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051040Stringer · corrodedBS 333 - 349, STRINGER 26R WAS CORRODED. BLENDED AND EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AMM, SRM, AND DWG. REMOVED AND INSTALLED A NEW STRINGER IAW SRM AND DWG. LEAK CHECKED GOOD.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051039Frame · corrodedTHE FRAME AT FS549.00 BETWEEN STRINGER 17L AND 18L WAS CORRODED. CUT AND REMOVED DAMAGED FRAME AND REINFORCEMENT ANGLE AT FS549.00 BETWEEN STRG 18L AND STRG 16L. SPLICED IN NEW FRAME AND REINFORCEMENT ANGLE REF REO. PERFORMED PRESSURIZATION LEAK CHECK AT RMay 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020061051038Stringer Splice · corrodedSTRINGER SPLICE 26R, ON BS 333, WAS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM, AND DWG. PRESSURE LEAK CHECKED GOOD IAW AMM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051037Doubler · corrodedDOUBLER FOR TCAS OMNIDIRECTIONAL ANTENNA HAD CORROSION. REMOVED AND REPLACED THE ANTENNA DOUBLER IAW DWG & SRM. COMPLIED WITH TASK CARD. LEAK CHECKED GOOD. OPS CHECKED GOOD.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2020061051036Stringer · corrodedSTRINGER 25R CORRODED BETWEEN BS 280 AND 295. EVALUATED AND FOUND TO BE OUT OF LIMITS, IAW SRM. REMOVED AND REPLACED THE STRINGER IAW SRM AND DWG. PRESSURE LEAK CHECKED GOOD.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051035Support Angle · corrodedBS 280 AVIONICS CRAWLWAY SUPPORT ANGLE HAD CORROSION. BLENDED THE CORROSION IAW SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW DWG AND SRM. REPLACED SUPPORT ANGLE IAW SRM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051034Floorbeam · crackedBS 280 FLOORBEAM ANGLE RBL 12, SUSPECTED CRACK IN RADIUS. REMOVED AND REPLACED THE FLOORBEAM ANGLE WITH NEW, LOCATED,DRILLED AND INSTALLED THE NEW ANGLE IAW SRM AND DWG.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2020061051033Floorbeam · corrodedBS 280 FLOORBEAM ANGLE ON FRONT HAD EVIDENCE OF CORROSION ON UPPER RADIUS AND IN OTHER MARKED LOCATIONS. REMOVED AND REPLACED FLOORBEAM ANGLE WITH NEW IAW DWG, AND SRM. COMPLIED WITH CARD.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2020061051032Floorbeam · corrodedBS 280 FLOORBEAM ON LT SIDE WAS CORRODED. EVALUATED CORROSION FROM THE FLOORBEAM, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED CORRODED FLOORBEAM ANGLE AND INSTALLED NEW IAW DWG, AND SRM.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2020061051031Stringer · chafedUPON REMOVAL OF BRACKET AT STGR. 7L BETWEEN FS 1144.00 AND FS 1162.00 IN THE AFT EQUIPMENT BAY, FOUND STRG 7L TO BE CHAFED. (C-CHECK) RO 4/24/2020 CUT DAMAGED STRINGER 7L SECTION AT F.S. 1144.00 TO1162.00 AND REPLACED WITH NEW STRINGER SECTION AND SPLICE.May 6, 2020 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020061051030Fitting · corrodedTHE PAX DOOR CLEAT AT FS320.163 AND DD6 HAD CORROSION. REMOVED CORROSION FROM PAX DOOR CLEAT IAW SRM, EVALUATED AND FOUND TO BE OUT OF LIMITS, IAW SRM AND REO. FABRICATED NEW PAX DOOR CLEAT IAW DWG, INSTALLED NEWLY FABRICATED CLEAT USING NEW HARDWARE REF REMay 6, 2020 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020061051029Fitting · corrodedTHE PAX DOOR CLEAT AT FS338.963 AT DD6 HAS CORROSION. FABRICATED AND INSTALLED NEW PAX DOOR CLEAT AT FS338.963 AT DD6 REF DWG AND REO. COMPLIED WITH TASK CARDMay 6, 2020 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020061051028Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE REQUIRES SKIN SEGMENT REPLACEMENT DUE TO MULTIPLE DENTS. R/H I/B FLAP LOWER SURFACE HAS BEEN REPAIRED IAW SRM, SPLICE REPAIR FROM FLS42.000 TO FLS48.000, FIG.COMPLIED WITH TASK CARDMay 5, 2020 · N752SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2020061051027Hinge · out of limitsREPLACE THE PAX DOOR FUSELAGE SIDE PIANO HINGE WITH NEW DUE TO INNER PIN BORE OUT OF LIMITS. REMOVED OUT OF LIMITS PAX DOOR FUSELAGE SIDE PIANO HINGE AND INSTALLED NEW PAX DOOR FUSELAGE SIDE PIANO HINGE, IAW SRM. PRESSURE LEAK CHECKED GOOD.May 2, 2020 · N752SK · Cndair CL6002C10 · Fuselage, Door Hinge
Back to N752SK