N508AE

Service difficulty reports · 237

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 = 'N508AE' 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 VNAA2025121211102Transducer · unserviceableANTI - SKID INBD CAUTION MSG ON APPROACH AND IB GND SPLR FAULT STATUS. REMOVED AND REPLACED RT INBD WHEEL SPEED TRANSDUCER IAW 32-44-01-000/400-801-A01. NO DEFECTS NOTED. OPS CHECKED GOOD.Dec 11, 2025 · N508AE · Cndair CL6002C10 · Brake Anti-Skid SectionSDR VNAA2025081311102Ballast · failedCABIN CREW REPORTS ELECTRICAL/CIRCUITY SMELL IN THE AFT CABIN AT THE LAST FIVE ROWS. GPU ATTACHED. APU ON. PACKS ON. RECRIC FANS ON. NO LOW PRESS AIR ATTACHED. NO FUELER ACTIVITY PRESENT./ PERFORMED TROUBLESHOOTING IAW CRJ700 FIM 21-22-00-810-806. FOUND TOP SIAug 11, 2025 · N508AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202504170108Stringer · corrodedSTRINGER 27 IS CORRODED BETWEEN FS280 AND FS295.CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. SH670-31642-1SApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202504170107Trunnion · corrodedLH INBD FLAP VANE ACTUATOR AT FLS140.4 FWD TRUNNION IS CORRODED. CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 140.4 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Attach FittingsSDR VNAA202504170106Trunnion · corrodedLH INBD FLAP VANE ACTUATOR AT FLS102.9 FWD TRUNNION IS CORRODED CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 102.9 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Attach FittingsSDR VNAA202504170105Trunnion · corrodedL/H I/B FLAP VANE ACUTATOR FWD TRUNNION AT STATION LS 24.0 IS CORRODED.CORRECTIVE ACTION: REPLACED LH INBD FLAP W.S. 24.0 FLAP VANE ACTUATOR PN: CC670-14300-9-01 IAW CRJ700 AMM 27-52-23-000/400-801 A01. CC670-14002-7Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Attach FittingsSDR VNAA20250417001Door Sill · gougedFWD CARGO DOOR SILL INNER CLOSING SKIN HAS MULTIPLE GOUGES BETWEEN FS 565 AND FS 581. CORRECTIVE ACTION: CUT-OUT DAMAGED SECTION OF INNER SKIN AND REMOVED AND DISCARDED JOINT PLATE. FABRICATED AND INSTALLED REPAIR PARTS IAW MHIRJ REO 670-53-31-981 REV. -- DATEApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170104Plate · corrodedWD CARGO DOOR SILL, LOWER AFT JOINT PLATE IS CORRODED. (FS 581) CORRECTIVE ACTION::REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. – DATED 2024-12-18. RWG SH670-33793-3Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170103Plate · corrodedWD CARGO DOOR SILL, LOWER AFT JOINT PLATE IS CORRODED. (FS 581) CORRECTIVE ACTION::REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. – DATED 2024-12-18. RWG SH670-33793-3Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170102Door Sill · corrodedFWD CARGO DOOR SILL, LOWER FWD JOINT PLATE IS CORRODED. (FS 533). REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. – DATED 2024-12-18. DRWG SH670-33793-3"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNA2025F00011Door Sill · corrodedFWD CARGO DOOR SILL, LOWER FWD JOINT PLATE IS CORRODED. (FS 533). REPAIRED CORROSION DAMAGE TO FWD BAGGAGE BAY DOOR SURROUND INNER SKIN BETWEEN FS 533-581 AND STR25L-26L IAW MHIRJ REO 670-53-31-981 REV. – DATED 2024-12-18. DRWG SH670-33793-3"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170101Window Frame · crackedRH WINDSHIELD SIDE POST CRACKED APPROX. 4" DOWN FROM TOP AND 1.5" LONG AT 100% FSH. FAILING NDT CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE WINDSHIELD POST P/N 601R33223-2 IAW CRJ700 SRM 51-42-21-001-001-A01. 601R33223-2Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202504170109Frame · corrodedFS319 BETWEEN STGR25L & 25R FOUND TO BE CORRODED IN MULTIPLE LOCATIONS ON ATTACH FLANGE. CORRECTIVE ACTION: INSTALLED COMPLETE FRAME LOWER SEGMENT PN: SH670-31355-1S FS319 BETWEEN STGR21L & 23R IAW CRJ700 SRM 51-42-06-001-001-A01 SH670-31355-1SApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202504170010Stringer · corrodedSTRINGER CLIP AT F.S. 985.00, STRINGER 19R IS CORRODED. REMOVED DAMAGED CLIP. FABRICATED AND INSTALLED NEW SERVICEABLE CLIP (P/N MM670-36485-004) I.A.W. CRJ700 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01, 51-25-00-001-001-A01 AND DWG. NO. MM670-36485 MM6Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNA2025F00010Stringer Clip · corroded"STRINGER CLIP AT F.S. 985.00, STRINGER 19R IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED CLIP. FABRICATED AND INSTALLED NEW SERVICEABLE CLIP (P/N MM670-36485-004) I.A.W. CRJ700 SRM 51-24-36-001-001-A01, 51-40-11-001-001-A01, 51-25-00-001-001-A01 AND DWG. NApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202504170097Slat Track · wornFOUND R/H SLAT TRACK 3-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. PERFORMED MAJOR REPAIR ON RH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1854 REV-- (P-1) DATED 2024-12-02. CC670-12090-3PEApr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202504170096Slat Track · wornFOUND L/H SLAT TRACK 3-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1853 REV-- (P-1) DATED 2024-12-02. CC670-12090-3PEApr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202504170095Slat Track · wornFOUND R/H SLAT TRACK 2-3 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. REPAIRED SLAT TRACK IAW MHIRJ REO 670-57-42-1866 REV -- DATED 2024-12-03 CC670-12060-3Apr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202504170094Seat Track · damagedL/H SIDE SEAT REAL EXTRUSION REINFORCEMENT STRAP REQUIRES REPLACEMENT. COMPLETE SNIEO SH670-37532-S01 IN ITS ENTIRETY. FABRICATE NEW REINFORCING STRAP P/N: SH670-37532-S0101 SAME AS ORIGINAL STRAP P/N: SH670-37532-1. PERFORMED MAJOR REPAIR BY COMPLYING WITH Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504170093Seat Track · elongatedLH SIDE SEAT RAIL MOUNTING EXTRUSION HOLES ELONGATED AND PART DENTED DURING REMOVAL OF FASTENERS. REPAIRED LH SIDE SEAT RAIL MOUNTING STRUCTURE BETWEEN FS 741.00 AND 763.00 BY INSTALLING A FREEZE PLUG AND FABRICATING AND INSTALLING REPAIR EXTRUSION IAW MHIRJApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504170092Trunnion · corrodedFOUND 4EA. TRUNNION BODIES CORRODED ON R/H FLS 24, 65, 102, AND FLS 140 THAT REQUIRE FABRICATION. CORRECTIVE ACTION: FABRICATED 4EA TRUNNION BODIES AT R/H FLS 24.00, 65.50, 102.90 AND 140.40 AS REQUIRED USING 7475-T7351 PO# 5-50407 IAW STEPS 1-3 OF MHIRJ SNIEOApr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Landing Gear Attach FittingsSDR VNAA202504170091Intercostal · chafedSTR 9R INTERCOSTAL BETWEEN FS 1144 - FS 1162 HAS CHAFE DAMAGE. PERFORMED A MAJOR REPAIR TO CHAFE DAMAGE ON INTERCOSTAL BETWEEN FS1144.00-FS1162.00, STGR 9R (DEVIATION TO GENERIC REO 670-53-61-292, REV. -E) IAW MHIRJ REO 670-53-61-2437 REV. -- DATED 2024-12-24Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170090Web · crackedPAX DOOR FWD STAIR WEB CRACKED. REMOVED CRACKED WEB. FWD PAX DOOR STAIR WEB HAS BEEN REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01 PN: 601R317071-12S 601R317071-12S"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202504170089Web · cracked" PAX DOOR AFT STAIR WEB IS CRACKED. REMOVED AND REPLACED STAIR WEB IAW CRJ-700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. 601R317071-11"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202504170088Seat Track · damagedDURING REMOVAL OF L/H SIDE SEAT RAIL MOUNTING EXTRUSION 1EA. HOLE LOCATION AT FS 752.50 JUST BELOW STRG 15L WAS ELONGATED IN UNDERLYING STRUCTURE (LOWER FRAME SECTOR P/N SH670-35522-11) AND REQUIRES REPAIR. CORRECTIVE ACTION: PERFORMED A MAJOR REPAIR TO GOUGE Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504170087Stringer · damagedSTRINGER 7R IS DAMAGED BETWEEN FS 1144 AND FS 1162. CORRECTIVE ACTION: REPAIRED STRINGER IAW BOMBARDIER REO 670-53-61-292 REV E DATED 2017-01-11. MM670-35119-002Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202504170086Seat Track · elongatedLH SIDE SEAT RAIL MOUNTING EXTRUSION HOLES ELONGATED AND PART DENTED DURING REMOVAL OF FASTENERS. PART REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED, FABRICATED LEFT SIDE SEAT RAIL EXTRUSION, AND INSTALLED FABRICATED SEAT RAIL EXTRUSION PN SH670-37522-1 IAWApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202504170084Intercostal · corrodedPAX DOOR INTERCOSTAL AFT DD1 FOUND TO BE CRACKED. REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED PAX DOOR INTERCOSTAL AFT DD1 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED PAX DOOR INTERCOSTAL AFT DD1 NEW SERVICEABLE P/N: 601R31902-318 IAW CRJ700 SRM 51-42-Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202504170083Trunnion · corrodedRH OUTBD FLAP W.S. 140.4 AFT TRUNNION HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 140.0 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202504170082Trunnion · corroded"RH OUTBD FLAP W.S. 102.9 AFT TRUNNION HAS CORROSION DAMAGE REQUIRES REPAIR CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 120.9 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202504170079Skin · corrodedUPON PERFORMING TO_53-079-001-23 REV ORIGINAL DATED 1/25/23 ON STEP (8) CORROSION WAS OBSERVED EXTENDING FROM THE REMOVED FASTENER HOLES IN THE RH FS797.00 AFT OB REMOVED FASTENER HOLES (2) REQUIRING ENGINEERING. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER IApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202504170081Cradle · corroded"R/H INBD FLAP W.S. 65.5 CRADLE ASSY HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: RECEIVED SERVICEABLE RH WS 65.5 CRADLE ASSEMBLY PN CC670-14301-9. REFERENCE BARCODE HR483812 FOR INSTALL. CC670-14301-9"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202504170080Trunnion · corrodedRH INBD FLAP W.S. 65.5 AFT TRUNNION HAS CORROSION REQUIRES REPAIR. CORRECTIVE ACTION: REPLACED RH INBD FLAP W.S. 65.5 AFT TRUNNION PN: 601R14270-21 IAW CRJ700 AMM 27-52-23-000/400-801 A01. REFER TO BARCODE HR00483808 FOR INSTALLATION 601R14270-21Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202504170078Gusset · corrodedGUSSET AT FS 295 CONNECTING TO STGR 21L FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVED GUSSET IAW CRJ700 SRM 51-42-06-001-001-A0. FABRICATED, LOCATED, DRILLED, AND DEBURRED GUSSET PN:SH670-32605-2 FROM S6144-13 IAW CRJ700 SRM 51-40-11-001-001-A01 & 51-24-36-Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170077Frame · corrodedFS295 FRAME LOWER ELEMENT AND WEB CORRODED FROM STGR 20L TO 22L. CORRECTIVE ACTION: FS295 FROM STGR 20L TO 22L FOUND TO BE OUT OF LIMITS PER NOTE 1: DAMAGE IS ALLOWED ONLY IN ONE ELEMENT AT A GIVEN CROSS-SECTION. REMOVED DAMAGE AT ONE ELEMENT MUST NOT OVERLAP Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202504170076Intercostal · corrodedSTGR 21L INTERCOSTAL BETWEEN FS310 AND FS333 CORRODED ON BOTH SIDES OF INTERCOSTAL. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. SH670-31822-1SApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170075Doubler · corrodedPAX DOOR STEP PANEL ASSEMBLY (832AT) HAS (3) EACH CRACKS, (3) EACH DENTS WITH ONE EXTENDING INTO THE INTERIOR CENTER RIB, A BENT MOUNTING LUG, AND SPOTS OF CORROSION THROUGHOUT REQUIRING EVAL CORRECTIVE ACTION: REMOVED AND REPLACED NEW SERVICEABLE PAX DOOR STEApr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202504170074Doubler · corrodedANTENNA INNER DOUBLER AT STGR 27 BETWEEN FS 295 AND FS 310 FOUND TO BE CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED DOUBLER IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Apr 17, 2025 · N508AE · Cndair CL6002C10 · Antenna/Radome Anti-Ice/De-Ice SystemSDR VNAA202504170073Stringer · corrodedSTGR 21L BETWEEN FS280 AND FS295 FOUND TO BE CORRODE IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: STGR 21L BETWEEN FS 280 AND FS295 REQUIRES REPLACEMENT DUE TO BEING IN A NO DAMAGE ALLOWED ZONE IAW CRJ700 SRM 53-21-03-101-002-A01. LOCATED, DRILLED, AND DEBURRED NApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202504170072Intercostal · corrodedGUSSET AT FS349 AND STRINGER 25L IS CORRODED CORRECTIVE ACTION: INSTALLED NEW GUSSET AT FS349 AND STRINGER 25L IAW CRJ700 SRM 51-42-21-001-001-A01. SH670-32072-1"Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170070Intercostal · corrodedAVIONICS BAY DOOR SURROUND INTERCOSTAL 27L BETWEEN F.S 349 AND FS364 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL I.A.W. CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. SH670-32075-3Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170069Floorbeam · corrodedFRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26R CORRECTIVE ACTION: FRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26RApr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202504170068Floorbeam · corrodedDISCREPANCY: F.S. 295 BETWEEN STGR 26L & 26R PREVIOUS REPAIR IS CORRODED.Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202504170067Floor Support · corrodedRBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1015 AND FS 1051.Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170066Floor Support · corroded"LBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: FOUND LBL 9 FLOOR BEAM BETWEEN FS 1000 & FS1069 TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-61-43-101-001-A01. REPAIR REQUIRED. PERFORMED REPAIR IAW CRJ-700 SRM 53-00-41-201-001-A01. S6Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170065Floor Support · corroded"LBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: FOUND LBL 9 FLOOR BEAM BETWEEN FS 1000 & FS1069 TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-61-43-101-001-A01. REPAIR REQUIRED. PERFORMED REPAIR IAW CRJ-700 SRM 53-00-41-201-001-A01. S6Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170064Floorbeam · corrodedLBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: REPAIRED AND REPLACED WITH NEW FLOOR BEAM LBL27 FS1000-1069 P/N MM670-35302-035 IAW SRM 53-00-41-201-001-A01 MM670-35302-035Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202504170063Door Sill · corrodedTHE AFT CARGO DOOR FLOOR SILL IS CORRODED.Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504170062Slat Track · wornFOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON RH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1857 REV-- DATED 2024-12-02. CC670-12070-3PEApr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202504170061Slat Track · wornDISCREPANCY: FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR ON LH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1856 REV-- DATED 2024-12-02. CC670-12070-3PEApr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge Devices
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