N355CA

Service difficulty reports · 245

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 = 'N355CA' 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 REXA202609241877Lamp · inoperative2 EMERGENCY EXIT FLOODLIGHT LAMPS INOPERATIVE. R & R NR 2 EMERGENCY EXIT FLOODLIGHT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.Sep 23, 2026 · N355CA · Cndair CL6002C10 · Emergency LightingSDR REXA2026071001072Lamp · inoperativeTHREE EMERGENCY FLOODLIGHT LAMPS INOPERATIVE. R & R THE THREE EMERGENCY FLOODLIGHT LAMPS IAW AMM 33-51-05. OPS CHECKED GOOD.Jul 10, 2026 · N355CA · Cndair CL6002C10 · Emergency LightingSDR REXA2025081200799Frame · corrodedCORROSION FOUND FRAME AT FS 1015 BETWEEN STGR 21L-25R. REPAIRED FRAME AT F.S.1015 BETWEEN STGR 21L TO 25R IAW ENDEAVOR AIR EA CRJ753-19701 REV IR DATED 7/10/2025.Aug 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR REXA2025090400847Stringer Splice · corrodedFOUND HEAVY CORROSION ON STGR24R SPLICE AT FS333 REMOVED STGR24R SPLICE AT FS333 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01 DRILLED AND LOCATED STGR24R SPLICE PN:SH670-32429-2 IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED STGR24R SPLICE PN:SH670-3242Aug 6, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025081200798Frame · damagedF.S. 280 FRAME HAS 5EA OVERSIZED HOLES (PREVIOUS REPAIR) BETWEEN STGR 17L AND STGR 18L. COMPLIED WITH MHIRJ REO 670-53-11-2156 REV -- DATED 2025-07-28 TEMPORARY REPAIR FOR OVERSIZED HOLES ON F.S.280 FRAME BETWEEN STR17L AND STR18L.Aug 6, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR REXA2025100600907Splice Angle · corrodedUPON REMOVAL OF BOTH LATCH PIN INTERCOSTALS AT STGR 27 FOUND CORROSION ON ATTACHED FLANGE OF FS364 BL0. REMOVED AND REPLACED BROKEN SPLICE (SP124) (P/N: M81714/12-20D-2) (P/N: M39029/1-101) IAW CRJ 700 ESPM 20-44-09 AND IAW CRJ 700 ESPM 20-16-43, OPERATIONAL Jul 29, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025082900843Frame · corrodedFRAME BS 319.70 LT IS CORRODED BETWEEN S20L AND S21L. REMOVED FRAME IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, ORIGINAL THICKNESS 0.050", REMAINING THICKNESS 0.036" DAMAGE IS OUT OF LIMITS, FRAME REQUIRES REPLACEMENT. DRILJul 29, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR REXA2025082500831Stringer Splice · corrodedFOUND CORROSION ON STGR 21L AFT SPLICE AT FS374. UPON FURTHER INVESTIGATION FOUND STGR 21L AFT SPLICE AT FS374 TO BE HEAVILY CORRODED TO THE POINT OF 100% MATERIAL LOSS AND OUT OF LIMITS IAW CRJ700 SRM 53-21-03-101-006-A01. LOCATED AND DRILLED NEW SERVICEABLJul 28, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025082900842Stringer · corrodedFOUND ELONGATED FASTENER HOLES ON STGR 21L BETWEEN FS 333.00-FS349.00. REMOVED AND REPLACED SKIN RIVETS FROM STGR 21L FS333- FS485 IAW CRJ700 SRM 51-42-06-001-001-A01. REMOVED AND REINSTALLED FLOOR LEVEL INTERCOSTAL AT FS364-FS379 LBL 37, STRAP ON STGR21L AT Jul 27, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025072800762Stringer · corrodedSTRINGER AT 20R IS CORRODED BETWEEN FS 364.00 AND 409.00. INSTALLED NEW STGR20R PN:SH670-31405-2S BETWEEN FS364 - FS477 IAW CRJ700 SRM 51-42-06-001-001-A01Jul 27, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025072800761Floorbeam · corrodedR/H F.S. 280 BEAM CAP IS CORRODED BETWEEN BL0 TO RBL9. REPAIRED FS 280 CROSSBEAM IAW MHIRJ GREO 670-53-11-579, REV -B, DATED 2013/05/01 AND 51-42-06-001-001-A01, 51-42-21-001-001-A01.Jul 27, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR REXA2025072100748Stringer · corrodedCORROSION WAS FOUND AROUND THE RIVETS ON STRINGER 22R BETWEEN FS 280 AND FS 295. REMOVED CORRODED STRINGER 22R FROM F.S.280 TO F.S.333 AND INSTALLED NEW SERVICABLE STRINGER P/N SH670-31210-2U IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jul 21, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025120200997Stringer · corrodedCORROSION FOUND ON STGR 23L BETWEEN FS 1015-1031. CUT AWAY AND REMOVED SHARP EDGES OF STRINGER 23L AT FS1000+9 AND FS1051+6 FOR REMOVAL IAW CRJ700 SRM 53-00-03-201-001-A01 STEPS 5A(1-2), REPAIR S6232. FABRICATED, LOCATED, AND DRILLED: STRINGER SECTION FS1000+9Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025090300846Intercostal · corrodedINTERCOSTAL AT 20R IS CORRODED BETWEEN FS 310.00 AND 319.70. INSTALLED NEW INTERCOSTAL P/N: SH670-32047-1 FROM STR20R BETWEEN FS310.00 TO FS319.70 IAW CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025072100747Intercostal · corrodedPAX DOOR DD2 AFT FOUND TO BE CORRODED REQUIRES REPLACEMENT. REMOVED PAX DOOR AFT DD2 INTERCOSTAL IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR AFT DD2 INTERCOSTAL IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 NEW SERVICEABLE PAX DOORJul 15, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2025071600743Stringer · corrodedSTRINGER 26L IS CORRODED BETWEEN FS 265.00 AND 280.00 REPAIRED STRINGER 26L BETWEEN F.S.265 TO F.S.280 IAW MHIRJ REO 670-53-11-2158 REV -- DATED 2025-07-14Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025071600742Stringer · corrodedSTRINGER 19R IS CORRODED BETWEEN FS 295.00 AND 310.00. UPON FURTHER INVESTIGATION, FOUND STR 20R TO BE CORRODED BETWEEN FS 295 AND FS 310. REMOVED STGR 20R FROM FS280-FS319 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED STGR 20R PN:SH670-312Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025071500725Stringer · corrodedSTRINGER AT 19R IS CORRODED BETWEEN FS 394.00 AND 409.00. RECEIVED AND COMPLIED WITH ENDEAVOR AIR EA CRJ753-19649 REV IR DATED 7-1-2025Jul 11, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025120200996Hinge · damagedPAX DOOR FUSELAGE SIDE HINGE LUGS (13 OF THE 27 AFT LUGS) EXCEEDS .295"" AND REQUIRES REPAIR OR REPLACEMENT. IAW CRJ 700 SRM 53-21-23-201-A01. COMPLIED WITH MHI RJ REO 670-53-21-2676 REV -.Jul 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage, Door HingeSDR REXA2025082500830Stringer · corrodedSTGR 23L IS CORRODED AT FS 581 TO FS 597 (MARKED WITH RED TAPE) REPAIRED STR 23L IAW ENDEAVOR AIR EA CRJ753-19988 REV IR DATED 8-14-25Jul 7, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025080600784Angle · damagedPAX DOOR AFT SUPPORT ANGLE FOUND EXTRA HOLE FROM PREVIOUS REPAIR REQUIRE REPLACEMENT LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT SUPPORT ANGLE P/N#601R318732-3 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01. REFERENCE HN00249365 FOR INSTALLATIONJul 7, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2025070900713Former · corrodedPAX DOOR INSIDE ACCESS HOLE 832FL FWD. FORMER IS CORRODED AND APPEARS ALSO TO GO UNDER FORMER REMOVED PAX DOOR FWD FORMER IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01, AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FWD FORMER P/N: 6Jul 6, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2025092300874Angle · corrodedAFTER REMOVAL OF PASSENGER DOOR SURROUND MID CAP ANGLE FOUND KICK PLATE ANGLE TO BE CORRODED, REMOVED AND REPLACED KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01, LOCATED AND DRILLED UP A SERVICABLE KICKPLATE ANGLE IAW CRJ700 SRM 5Jul 2, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025080600783Frame · corrodedPAX DOOR F.S. BETWEEN FWD DD4 AND DD5 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED DAMAGED FRAME. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FRAME, FS313.56, BETWEEN DD4 & DD5 P/N# 601R318086-1 IAW CRJ-700 SRM TASK 51-40-11-001-00Jun 24, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2025080600782Former · corrodedPAX DOOR AFT FORMER FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED DAMAGED AFT FORMER. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER FS 347 P/N#601R318034-5 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-00Jun 24, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2025071100720Intercostal · corrodedPASSENGER DOOR MID DD4 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT INSTALLED NEW SERVICEABLE PAX DOOR MID DD4 INTERCOSTAL P/N:601R318081-1S IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01Jun 24, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR REXA2025072100746Frame · corrodedFS 549 FRAME CORRODED BETWEEN STR 17L AND STR 18L. REPAIRED IAW ENDEAVOR AIR EA CRJ753-19587 REV IR DATED 06-24-2025.Jun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR REXA2025070900712Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN FS 280.00 AND 319.70. REMOVED CORROSION ON STR 26R BETWEEN FS 280 AND FS 310 IAW CRJ700 SRM 51-21--06-001-001-A01. STR 26R FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS BETWEEN FS 280 AND FS 310 IN MULTIPLE AREAS IAW CRJun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025070900711Stringer · corrodedSTRINGER 25R IS CORRODED BETWEEN FS 295.00 AND 310.00 REMOVED CORROSION FROM STR 25R BETWEEN 295 & FS 310 IAW CRJ700 SRM 51-- 21-06-001-001-A01. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM TASK 53-21-- 03-101-002-A01. FOUND DAMAGE TO BE OUT OF LIMITS. R & R STRJun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025062300675Stringer · corrodedJOINT PIECE SPLICE (P/N:SH670-32429-2) AT FS333 STR 22R FOUND TO BE CORRODED REMOVED UNSERVICEABLE JOINT PIECE SPLICE (P/N:SH670-32429-2) AT FS333 STGR 22R IAW CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE JOJun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025062300674Stringer · corrodedSTRINGER AT 22R IS CORRODED BETWEEN FS 333.00 AND 349.00. REMOVED UNSERVICEABLE STR 22R (P/N:SH670-31379-1) BETWEEN FS333-FS349 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STR 22R (P/N:SH670-31379-1) BEJun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025092300872Floor Support · corrodedRBL 9 FLOOR SUPPORT IS CORRODED BETWEEN F.S. 501 - 549. R & R ENTIRE FLOOR SUPPORT RBL 9 FS 477 - 571 IAW MHI RJ REO 670-53-31-1054 REV --. FABRICATED RBL9 FLOOR SUPPORT FROM FS 477 - 571 USING EXTRUSION, LOCATED, DRILLED UPPER & LOWER FLANGE IAW SRM 53-00-4Jun 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025072800760Floorbeam · corrodedF.S. 280 BEAM CAP IS CORRODED BETWEEN LBL9 TO LBL27. REMOVED FS 280.00 L/H CROSSBEAM BETWEEN LBL 0-LBL 42, IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED NEW SERVICEABLE FS 280.00 L/H CROSSBEAM PN CC670-34Jun 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR REXA2025082900841Stringer · corrodedSTRINGER AT 24R IS CORRODED BETWEEN BS 333.- 349. BLENDED CORROSION ON STRINGER IAW SRM 51-21-06-001-001-A01. NO DAMAGE IS ALLOWED TO STRINGER 24R IAW SRM 53-21-03-101-006-A01. PERFORMED UT THICKNESS ON REWORKED AREAS ON STRINGER IAW NDTM PT 1 51-20-004-270-Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025082600835Stringer · corrodedSTRINGER AT 19L IS CORRODED BETWEEN FS 379.00 AND 453.00. BLENDED CORROSION FROM STGR 19L BETWEEN FS379 - FS453 FOUND MULTIPLE SPOT OF 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 51-21-06-001-001-A01, SRM 53-21-03-101-005-A01. REMOVED AND REPJun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025081800749Stringer · corrodedSTGR 19R IS CORRODED BETWEEN F.S. 565 TO F.S. 581. BLENDED CORROSION IAW SRM 53-31-03-101-004-A04. PERFORMED LPI ON REWORKED AREAS ON S19R BETWEEN BS 565 AND 581 IAW NDTM PT 1 51-20-008-230-A01. NO INDICATIONS NOTED. PERFORMED UT THICKNESS ON REWORKED AREAS Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025081300804Stringer · corrodedSTRINGER AT 21R IS CORRODED BETWEEN FS 394.00 AND 453.00. REMOVED CORROSION 100% MATERIAL LOSS STRINGER REQUIRE REPLACEMENT IAW CRJ700 SRM 51-21-06-001-001-A01, REMOVED STGR21R FROM FS394 - FS477 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01 INSTALLEJun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025071500739Stringer · corrodedSTRINGER 19R IS CORRODED BETWEEN FS 295.00 AND 310.00. REMOVED CORROSION ON STR 19R BETWEEN FS 295 AND FS 310 IAW CRJ700 SRM 51-21-06-001-001-A01, FOUND TO HAVE 100% MATERIAL LOSS. REMOVED AND REPLACED STGR 19R FROM FS280-FS310 PN:SH670-31632-1 IAW CRJ700 SRMJun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR REXA2025071500723Frame · corrodedFRAME AT FS 319.70 IS CORRODED BETWEEN STGR 25L AND 24R. FS 319 IS FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS DUE TO HAVING 100% MATERIAL LOSE IAW CRJ 700 SRM 53-21-06-101-002-A01 REMOVED PREVIOUS SPLICE REPAIR AND FRAME SEGMENT FROM FS319 STGR25L - STGR23R IJun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR REXA2025062500684Floor Support · corrodedCORROSION FOUND ON FLOOR BEAM AT LBL 9.00 BETWEEN FS 969.00-1088.20. REPAIRED FLOOR BEAM AT LBL 9.00 BETWEEN FS 969.00-1088.20 IAW ENDEAVOR AIR EA CRJ753-19590 REV IR DATE 06/21/2025. REMOVED AND REINSTALLED CARGO TIE-DOWN TRACK FROM FS988 TO FS1041 IAW CRJ700Jun 7, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2025071100719Intercostal · corrodedPAX DOOR INTERCOSTAL DD3 IS CORRODED. INSTALLED NEW SERVICEABLE PAX DOOR MID DD3 INTERCOSTAL 601R318056-1 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01May 23, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew DoorsSDR N6WA2017083101Warning Message · illuminatedRIGHT EMERGENCY DOOR CAUTION MESSAGE. OPENAug 31, 2017 · N355CA · Cndair CL6002C10 · Door Warning SystemSDR N6WA2017071301Warning Message · illuminatedRIGHT EMERGENCY DOOR CAUTION MESSAGE ON GROUND.Jul 13, 2017 · N355CA · Cndair CL6002C10 · Door Warning SystemSDR N6WA2017070402Warning Message · false activationRIGHT EMERGENCY EXIT CAUTION MESSAGE ON LANDING. PERFORMED OPS CHECK OF RT EMERG EXIT DOOR IAW AMM 52-21-00. OPS CHECK GOOD.Jul 4, 2017 · N355CA · Cndair CL6002C10 · Door Warning SystemSDR N6WA2017062101Warning Light · illuminatedINTERMITTENT RT EMERGENCY EXIT CAUTION DISPLAYED AFTER LANDING.Jun 21, 2017 · N355CA · Cndair CL6002C10 · Door Warning SystemSDR V0XD201706190003Frame · corrodedFRAME BS 863 HAS SIGNS OF CORROSION BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-51-115, REV A.Jun 2, 2017 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR V0XD201706190002Frame · corrodedFRAME BS 879 BETWEEN STRINGERS 26L AND 26R HAS SIGNS OF CORROSION. REPAIRED THE FRAME IAW REO 670-53-51-115, REV A.Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage Main, FrameSDR V0XD201706130005Seat Track · corrodedLEFT INBD SEAT TRACK FROM BS 581-677 FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20170613DP04Seat Track · corrodedSEAT TRAC,K HAS MULTIPLE SPOTS OF CORROSION FROM BS 485 TO 677. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, SRM 51-40-11, AND REO 670-53-00-343 REV M.Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR V0XD20170613DP03Seat Track · corrodedRT SIDE SEAT TRACK FROM BS 669 TO 713 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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