N538CA

Service difficulty reports · 219

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 = 'N538CA' 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 ASOA2015112714205Frame · corrodedFRAME 319 AT STR 27 FWD SIDE HAS CORROSION. REMOVED CORROSION AT FS 319.00 STR 27-26R, FWD SIDE IAW SRM 51-12-00-001-001-A01 TR 51-0050 AND 51-21-06-001-001-A01. COMPLIED WITH ECTC EA 26-2015-183, REV A AND COMPLIED WITH STC EA 26-2015-183, REV A.Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Main, FrameSDR ASOA2015112714204Stringer Splice · corrodedSTR SPLICE 26L BETWEEN FS 349-333 HAS CORROSION. REMOVED CORROSION ON STR SPLICE ON 26L AT FS 333, REF: SRM 51-21-06-001-001 A01 FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006 A02. R & R STR 26L, SPLICE AT FS 333, REF SRM 51-40-11-001-001 A01 & SRNov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR ASOA2015112714203Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON RT SIDE SEAT RAIL SEGMENT BETWEEN FS 784.00 AND 847.00 + 16.00. EVALUATED CORROSION IAW REO 670-53-00-013, REV J & FOUND TO BE OUT OF LIMITS. REMOVED RT SIDE WALL SEAT RAIL C, FS 784.00 THRU 847.00 IAW AMM 53-00-49-0Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714202Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON LT SIDE SEAT RAIL SEGMENT BETWEEN F/A 907.00 AND 977.00. CORROSION SEAT RAIL LEFT SIDE FS 907.00-977.00 IS BEYOND LIMITS IAW REO 670-53-00-013, REV J. REMOVED SEAT RAIL AT FS 907.00 AND 977.00 IAW AMM 53-00-49-000-80Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714162Latch · contaminatedSERVICE DOOR FAILED FUNCTIONAL CHECK OF INNER HANDLE TO COMPLETE UNLATCH CYCLE. CLEANED AND LUBED SERVICE DOOR, REF AMM TASK 12-20-52-640-801 A01. FUNCTIONAL TEST OF SERVICE DOOR COMPLIED WITH, REF AMM TASK 52-41-00-720-801 A01. FUNCTIONAL TEST GOOD.Nov 27, 2015 · N538CA · Cndair CL6002D24 · Service DoorsSDR ASOA2015112714161Seat Track · corrodedSEAT TRACK AT LBL9 BETWEEN 379.00 AND 485.00 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01 DAMAGE BEYOND LIMITS IAW REO 670-53-00-013, REV J ON SEAT TRACK AT LBL9 FS 379-485. REMOVED SEAT TRACK AT LBL9, FS 379.00-485.00 IAW AMM 53-00-49-000-8Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714160Crossbeam · corrodedCROSSBEAM AT FS 280.00 HAS CORROSION. NEED EVALUATION. BLENDED AREAS OF CORROSION ON CROSSBEAM FS 280 SPLICE ANGLE IAW SRM 51-12-00-001-001 A01, TR 51-0050 AND 51-21-06-001-001 A01. SUBMITTED STS ENGINEERING FOR PERMANENT DISPOSITION REF: SRM 51-13-01-001-0Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Main, StructureSDR ASOA2015112714159Door Sill · corrodedCORROSION FOUND ALONG SERVICE DOOR CUTOUT, SILL AREA, NEED EVALUATION. UPON FURTHER INVESTIGATION IT IS FOUND THE MOUNTING ANGLE AND LOWER SILL ANGLE WILL NEED REPLACEMENT DUE TO EXFOLIATION CORROSION. REMOVED MOUNTING ANGLE AND LOWER SILL ANGLE IAW SRM 51-1Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015112714158Crossbeam · corrodedPACKER AT FS 333.00 CROSSBEAM AND RBL 9 HAS CORROSION NEED TO BE EVALUATED. EVALUATED AND REMOVED CORROSION REF: SRM 51-21-06-001-001 A01 FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-101-001 A01. R & R PACKER AT FS 333.00 AT RBL9, REF: SRM 51-42-06-001-001 Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Main, StructureSDR ASOA2015112714157Floorbeam · corrodedFS 280 CRAWLWAY FLOORBOARD SUPPORT ANGLE HAS CORROSION. REMOVED CORROSION AT DISCREPANT PART AS NEEDED REF SRM 51-42-06-001-001-A01. R & R ANGLE IAW SRM 51-42-06-001-001-A01 & DWG CC670-34010.Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015112714156Intercostal · corrodedINTERCOSTAL AT FS 364 STR 27R HAS CORROSION. EVALUATED CORROSION DAMAGE AT INTERCOSTAL FS 364, STR 27R AND FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-23-101-003-A01, FIG 53-21-23-991-808. NO DAMAGE ALLOWED ON ATTACHED FLANGE OF LATCH PIN INTERCNov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015112714155Intercostal · corrodedINTERCOSTAL AT FS 364, STR 27L HAS CORROSION. EVALUATED CORROSION DAMAGE AT INTERCOSTAL FS 364 STR 27L IAW SRM 53-21-23-101-003-A01, FIG 53-21-23-991-808. FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS, NO DAMAGE ALLOWED. R & R INTERCOSTAL IAW SRM 51-42-06-001-Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015112714154Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON RT SIDE SEAT RAIL SEGMENT BETWEEN FS 483.00 AND 573.00. BLENDED AND EVALAUTED CORROSION IAW REO 670-53-00-013, REV J AND SRM 51-12-00-001-001-A01, CORROSION FOUND TO BE OUT OF TOLERANCE. REMOVED SIDE RT SEAT RAIL ON Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714153Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON RT SIDE SEAT RAIL SEGMENT BETWEEN FS 573.00 AND 661.00 +14.00. EVALAUTED CORROSION IAW REO 670-53-00-013, REV J CORROSION FOUND TO BE OUT OF LIMITS. REMOVED SIDE SEAT RAIL RT SIDE FS 573.00-661.00+14.00 IAW AMM 53-00Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714152Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON RT SIDE SEAT RAIL SEGMENT BETWEEN FS 661.00 + 90.00 AND 672.00. EVALAUTED CORROSION IAW REO 670-53-00-013, REV J CORROSION FOUND TO BE OUT OF LIMITS. REMOVED RT SIDE SEAT RAIL FS661.00+90.00-672.00 IAW AMM 53-00-49-Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714151Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON RT SIDE SEAT RAIL SEGMENT BETWEEN FS 743.00 AND 763.00. CORROSION EVALUATED IAW REO 670-53-00-013, REV J CORROSION FOUND TO BE OUT OF LIMITS. REMOVED SEAT RAIL, AMM 53-00-49-000-801 A07. COMPLIED WITH EC/TC REO 670-Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714150Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON LT SIDE SEAT RAIL BETWEEN FS 661.00 + 40.00 AND 672.00. EVALUATED CORROSION IAW REO 670-53-00-013, REV J FOUND CORROSION TO BE OUT OF LIMITS. REMOVED SEAT RAIL FROM LT SIDE AT FS 661.00 + 90 +672 IAW AM 53-00-49-000-Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714149Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON LT SIDE SEAT RAIL SEGMENT BETWEEN FS 573.00 AND 661.00 + 14.00. EVALUATED CORROSION IAW REO 670-53-00-013, REV J AND FOUND TO BE OUT OF LIMITS. REMOVED LT SIDE SEAT RAIL DS 573.00-661.00 14.00. FABRICATED LT SIDE SENov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714148Seat Track · corrodedDEFECT DESCRIPTION: / CORROSION ON AND AROUND FASTENER HEADS ON LH SIDE SEAT RAIL SEGMENT BETWEEN FS 672.00 AND 722.00 / RESOLUTION DESCRIPTION: / EVALUATED CORROSION IAW BOMBARDIER REO 670-53-00-013 REV J CORROSION FOUND TO BE OUT TOLERANCE. REMOVED LH SIDENov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714147Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON LT SIDE SEAT RAIL SEGMENT BETWEEN FS 784.00 AND 847.00 + 16.00. EVALUATED CORROSION AND FOUND TO BE OUT OF TOLERANCE IAW REO 670-53-00-013, REV J. REMOVED LT SIDE SEAT RAIL AT LT SIDE FS 784.00 THRU FS 847.00 +16.00 Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112714146Seat Track · corrodedCORROSION ON AND AROUND FASTENER HEADS ON LT SIDE SEAT RAIL SEGMENT BETWEEN FS 847.00 + 16.00 AND 907.00. EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED SEAT RAIL AT FS 847.00-907.00 RT SIDE IAW AMM 53-00-49-000-801, Nov 27, 2015 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015112514201Floor Panel · crackedFLIGHT DECK PANEL 221ELW IS CRACKED. REPLACED THE DAMAGED FLIGHT DECK PANEL WITH SERVICABLE PANEL, PN 601R41255-5, REFER TO M-212 FOR INSTALLATION. DRILLED FASTENER HOLES INTO SERVICABLE, PN 601R41255-5, BY ALIGNING THE SERVICABLE PART WITH THE ORIGINAL PART Nov 25, 2015 · N538CA · Cndair CL6002D24 · Fuselage Floor PanelSDR ASOA2015112514200Floor Panel · crackedLEFT SIDE ELECTIRCAL BAY FLOOR IS CRACKED AT BS 193. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509, REV B, DATED 01-28-2014.Nov 25, 2015 · N538CA · Cndair CL6002D24 · Fuselage Floor PanelSDR ASOA2014080711026Control Panel · intermittentINBOUND, RECEIVED AN UNCOMMANDED LT FULL AILERON TRIM AND LT FULL RUDDER TRIM INDICATIONS. NORMAL CENTRAL FEEL WITH AP DISENGAGED. AP WOULD NOT REENGAGE. EMERGENCY ACTIONS, AILERON TRIM SYSTEM, REMOVED AND RE-INSTALLED AILERON/RUDDER CONTROL PANEL. PERFORAug 3, 2014 · N538CA · Cndair CL6002D24 · Aileron Control SystemSDR ASOA2014062510755Retainer · damagedFWD CARGO BAY DOOR AFT SEAL RETAINER IS DAMAGED. COMPLIED WITH ECTC REO 690-52-35-013.Jun 20, 2014 · N538CA · Cndair CL6002D24 · Cargo/Baggage DoorsSDR ASOA2014062510754Retainer · damagedFWD CARGO BAY DOOR FWD SEAL RETAINER, DAMAGED. REPAIRED IAW REO 690-52-35-013, REV A.Jun 20, 2014 · N538CA · Cndair CL6002D24 · Cargo/Baggage DoorsSDR ASOA2014020709919Floor Support · crackedFOUND RT COCKPIT FLOOR SUPPORT CRACKED. REMOVED RT COCKPIT FLOOR SUPPORT IAW SRM 51-42-11-001-001-A01. INSTALLED RT COCKPIT SUPPORT IAW SRM 51-42-11-001-001 AND DWG CC670 33052 AND SRM 51-42-06.Jan 11, 2014 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014020709918Floor Support · crackedFOUND LT COCKPIT FLOOR SUPPORT CRACKED. REMOVED CRACKED FLOOR SUPPORT. LOCATED, DRILLED AND DEBURRED NEW FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01.Jan 11, 2014 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014020709917Bulkhead Web · corrodedLEFT LOWER FS 280 BULKHEAD WEB CORRODED AND CRACKED ABOVE DS280 CROSSBEAM. COMPLIED WITH REO 670-53-11-594 REV. MAJOR REPAIR.Jan 7, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, BulkheadSDR ASOA2014020709916Frame · corrodedCORROSION ON FRAME FS 295 BETWEEN S26L AND 26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01. FOUND WITHIN LIMITS IAW SRM 53-21-06-101-002-A02, SRM 53-00-00-101-001-A01, MAJOR REPAIR.Jan 5, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, FrameSDR ASOA2014020709915Frame · corrodedCORROSION LOCATED AT FS 310 BETWEEN S26L AND 26R. . REMOVED CORROSION FRAME IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-00-101-002-A02 AND SRM 53-00-00-101-001-A01.Jan 5, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, FrameSDR ASOA2014020709914Skin · corrodedFUSELAGE SKIN UNDER TCAS OMNI-DIRECTIONAL ANTENNA HAS CORROSION BETWEEN FS 295 & FS 310, STR 27. REMOVED CORROSION ON FUSELAGE SKIN EXTERIOR UNDER TCAS ANTENNA BETWEEN FS 295+ FS310, STGR 27 IAW SRM 51-21-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJORJan 4, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2014020709913Floor Panel · crackedRT SIDE FORWARD EQUIPMENT BAY FLOOR HAS A CRACK NEAR ADG STOW PUMP. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509 REV. MAJOR REPAIR.Jan 4, 2014 · N538CA · Cndair CL6002D24 · Fuselage Floor PanelSDR ASOA2014020709912Butt Joint · corrodedFOUND CORROSION ON BUTT-JOINT STRAP AT FS 280 BETWEEN STGR 27L AND 27R. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REMOVED CORROSION ON BUTT JOINT STRAP AT FS280 BETWEEN STGR 26L AND 26R IAW SRM 51-21-06-001-001-A01.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2014020709911Antenna · corrodedFOUND TCAS OMNI-DIRECTIONAL ANTENNA CORRODED WHEN REMOVING FOR SHEETMETAL. THIS REPAIR IS CLASSIFIED AS A REPAIR IAW ASA SOP 5702. REMOVED TCAS OMNI-DIRECTIONAL ANTENNA IAW AMM 34-43-07-000-801. INSTALLED SERVICABLE TCAS OMNI-DIRECTIONAL ANTENNA IAW AMM 34-Jan 3, 2014 · N538CA · Cndair CL6002D24 · Flight Environment DataSDR ASOA2014012309802Floorbeam · corrodedBS 280 FLOORBEAM CORRODED BETWEEN LBL 9 AND RBL 9. REPAIRED IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2014012309801Angle · crackedBS 280 ANGLE CRACKED AT LBL 9. R & R IAW SRM 51-42--06-001-001-A01 AND DWG CC670-34010.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014012309800Floor Support · crackedLEFT COCKPIT FLOOR SUPPORT CRACKED JUST FWD OF FS 280 AT LBL 11. REPAIRED IAW SRM 51-42-06-001-001.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014012109787Seat Track · corrodedRBL 9 SEAT TRACK BS 349-485 CORRODED. R & R SEAT TRACK IAW SRM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014012109786Seat Track · corrodedRBL 9 SEAT TRACK BS 581 - 661 CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 AND INSTALLED NEW IAW AMM 53-00-49-400-801.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014012109785Seat Track · corrodedLBL 9 SEAT TRACK FROM FS 364-485 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014012109784Hinge · gougedASD HINGE GOUGED AT 2ND & 11TH LUG. REPAIRED PAX DOOR HINGE, DOOR SIDE IAW REO 670-52-11-511. REPAIR CLASSIFIED AS MAJOR.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage, Door HingeSDR ASOA2014012109783Hinge · gougedHINGE ON AIRFRAME SIDE GOUGED ON AFT END. COMPLIED WITH REO 670-53-21-582 AND ECTC REO 70-53-21-582. REPAIRED PASSENGER DOOR HINGE, FUSELAGE SIDE IAW REO 670-53-21-582. REPAIR CLASSIFIED AS MAJOR.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage, Door HingeSDR ASOA2014012009779Floor Support · crackedRIGHT COCKPIT FLOOR SUPPORT CRACKED JUST FWD OF FS 280 AT RBL 11. FABRICATED REPAIR IAW SRM 51-24-16-001-001. COMPLIED WITH EC/TC REO 690-53-11-623. REPAIR CLASSIFIED AS MAJOR.Jan 3, 2014 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014012309799Floorbeam · corrodedBS 280 FLOORBEAM CAP CORRODED OTBD OF LBL 9. REPAIRED IAW SRM 51-42-06-001.Jan 2, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2014012309798Frame · corrodedCORROSION FOUND ALONG AFT SIDE OF FRAME BS 349 BETWEEN S26L-26R. REPAIRED IAW SRM 51-42-06-001-001-A01 AND SRM 53-21-06-101-006. MAJOR REPAIR.Jan 2, 2014 · N538CA · Cndair CL6002D24 · Fuselage Main, FrameSDR ASOA2014012009778Intercostal · corrodedCORROSION LOCATED ALONG INTERCOSTAL S27L. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-001-001-A01 AND DWG 5H 670-32050. DRILLED HOLES IN SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED INTERCOSJan 2, 2014 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014011709777Retainer · crushedFWD BAGGAGE BAY SEAL RETAINER LOWER AFT CORNER CRUSHED. COMPLIED WITH EC/TC REO 690-52-35-013 REV A. REPAIR CLASSIFED AS MAJOR.Jan 2, 2014 · N538CA · Cndair CL6002D24 · Cargo/Baggage DoorsSDR ASOA2014012309797Intercostal · corrodedCORROSION LOCATED ALONG INTERCOSTAL BETWEEN S26 & 27R. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-001-001-A01 AND DWG 5H 670-32050. INSTALLED INTERCOSTAL IAW SRM 51-42-21-001-001-A01 AND DWG SH670-32050. REPAIR CLASSIFIED AS MAJOR.Dec 31, 2013 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2014012309796Skin · corrodedCORROSION LOCATED IN THE GENERAL VICINITY OF THE VOR ANTENNA, BETWEEN FS 310-295 AND BETWEEN STGRS 26L-26R. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REMOVED CORROSION FROM FS 295, FS 310 FRAMES AND ANTENNA DOUBLER BETWEEN STRG 26L TO 26RDec 31, 2013 · N538CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
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