# Service difficulty reports: N508AE

A list on [N508AE](https://openairdocs.org/aircraft/N508AE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 237 reports

- [SDR VNAA2025121211102](https://openairdocs.org/sdr/VNAA2025121211102.md): Transducer · unserviceable · Dec 11, 2025 · N508AE · Cndair CL6002C10 · Brake Anti-Skid Section
  > ANTI - 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.
- [SDR VNAA2025081311102](https://openairdocs.org/sdr/VNAA2025081311102.md): Ballast · failed · Aug 11, 2025 · N508AE · Cndair CL6002C10 · Air Distribution System
  > CABIN 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 SI
- [SDR VNAA202504170108](https://openairdocs.org/sdr/VNAA202504170108.md): Stringer · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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. SH670-31642-1S
- [SDR VNAA202504170107](https://openairdocs.org/sdr/VNAA202504170107.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Attach Fittings
  > LH 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. CC670-14002-7
- [SDR VNAA202504170106](https://openairdocs.org/sdr/VNAA202504170106.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Attach Fittings
  > LH 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. CC670-14002-7
- [SDR VNAA202504170105](https://openairdocs.org/sdr/VNAA202504170105.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Attach Fittings
  > L/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. CC670-14002-7
- [SDR VNAA20250417001](https://openairdocs.org/sdr/VNAA20250417001.md): Door Sill · gouged · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD 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. -- DATE
- [SDR VNAA202504170104](https://openairdocs.org/sdr/VNAA202504170104.md): Plate · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WD 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 SH670-33793-3
- [SDR VNAA202504170103](https://openairdocs.org/sdr/VNAA202504170103.md): Plate · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WD 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 SH670-33793-3
- [SDR VNAA202504170102](https://openairdocs.org/sdr/VNAA202504170102.md): Door Sill · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD 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"
- [SDR VNA2025F00011](https://openairdocs.org/sdr/VNA2025F00011.md): Door Sill · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD 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"
- [SDR VNAA202504170101](https://openairdocs.org/sdr/VNAA202504170101.md): Window Frame · cracked · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Structure
  > RH 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. 601R33223-2
- [SDR VNAA202504170109](https://openairdocs.org/sdr/VNAA202504170109.md): Frame · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FS319 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 SH670-31355-1S
- [SDR VNAA202504170010](https://openairdocs.org/sdr/VNAA202504170010.md): Stringer · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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 MM6
- [SDR VNA2025F00010](https://openairdocs.org/sdr/VNA2025F00010.md): Stringer Clip · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > "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. N
- [SDR VNAA202504170097](https://openairdocs.org/sdr/VNAA202504170097.md): Slat Track · worn · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge Devices
  > FOUND 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. CC670-12090-3PE
- [SDR VNAA202504170096](https://openairdocs.org/sdr/VNAA202504170096.md): Slat Track · worn · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge Devices
  > FOUND 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. CC670-12090-3PE
- [SDR VNAA202504170095](https://openairdocs.org/sdr/VNAA202504170095.md): Slat Track · worn · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge Devices
  > FOUND 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 CC670-12060-3
- [SDR VNAA202504170094](https://openairdocs.org/sdr/VNAA202504170094.md): Seat Track · damaged · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/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
- [SDR VNAA202504170093](https://openairdocs.org/sdr/VNAA202504170093.md): Seat Track · elongated · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH 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 MHIRJ
- [SDR VNAA202504170092](https://openairdocs.org/sdr/VNAA202504170092.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Wing, Landing Gear Attach Fittings
  > FOUND 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 SNIEO
- [SDR VNAA202504170091](https://openairdocs.org/sdr/VNAA202504170091.md): Intercostal · chafed · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 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 2024-12-24
- [SDR VNAA202504170090](https://openairdocs.org/sdr/VNAA202504170090.md): Web · cracked · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX 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"
- [SDR VNAA202504170089](https://openairdocs.org/sdr/VNAA202504170089.md): Web · cracked · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew Doors
  > " 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"
- [SDR VNAA202504170088](https://openairdocs.org/sdr/VNAA202504170088.md): Seat Track · damaged · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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
- [SDR VNAA202504170087](https://openairdocs.org/sdr/VNAA202504170087.md): Stringer · damaged · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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. MM670-35119-002
- [SDR VNAA202504170086](https://openairdocs.org/sdr/VNAA202504170086.md): Seat Track · elongated · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH 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 IAW
- [SDR VNAA202504170084](https://openairdocs.org/sdr/VNAA202504170084.md): Intercostal · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX 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-
- [SDR VNAA202504170083](https://openairdocs.org/sdr/VNAA202504170083.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RH 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 601R14270-21
- [SDR VNAA202504170082](https://openairdocs.org/sdr/VNAA202504170082.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge Flaps
  > "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"
- [SDR VNAA202504170079](https://openairdocs.org/sdr/VNAA202504170079.md): Skin · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > UPON 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 I
- [SDR VNAA202504170081](https://openairdocs.org/sdr/VNAA202504170081.md): Cradle · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge Flaps
  > "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"
- [SDR VNAA202504170080](https://openairdocs.org/sdr/VNAA202504170080.md): Trunnion · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RH 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 601R14270-21
- [SDR VNAA202504170078](https://openairdocs.org/sdr/VNAA202504170078.md): Gusset · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GUSSET 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-
- [SDR VNAA202504170077](https://openairdocs.org/sdr/VNAA202504170077.md): Frame · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FS295 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
- [SDR VNAA202504170076](https://openairdocs.org/sdr/VNAA202504170076.md): Intercostal · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STGR 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. SH670-31822-1S
- [SDR VNAA202504170075](https://openairdocs.org/sdr/VNAA202504170075.md): Doubler · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX 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 STE
- [SDR VNAA202504170074](https://openairdocs.org/sdr/VNAA202504170074.md): Doubler · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Antenna/Radome Anti-Ice/De-Ice System
  > ANTENNA 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.
- [SDR VNAA202504170073](https://openairdocs.org/sdr/VNAA202504170073.md): Stringer · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 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 N
- [SDR VNAA202504170072](https://openairdocs.org/sdr/VNAA202504170072.md): Intercostal · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GUSSET 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"
- [SDR VNAA202504170070](https://openairdocs.org/sdr/VNAA202504170070.md): Intercostal · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVIONICS 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. SH670-32075-3
- [SDR VNAA202504170069](https://openairdocs.org/sdr/VNAA202504170069.md): Floorbeam · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26R CORRECTIVE ACTION: FRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26R
- [SDR VNAA202504170068](https://openairdocs.org/sdr/VNAA202504170068.md): Floorbeam · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > DISCREPANCY: F.S. 295 BETWEEN STGR 26L & 26R PREVIOUS REPAIR IS CORRODED.
- [SDR VNAA202504170067](https://openairdocs.org/sdr/VNAA202504170067.md): Floor Support · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1015 AND FS 1051.
- [SDR VNAA202504170066](https://openairdocs.org/sdr/VNAA202504170066.md): Floor Support · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "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. S6
- [SDR VNAA202504170065](https://openairdocs.org/sdr/VNAA202504170065.md): Floor Support · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "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. S6
- [SDR VNAA202504170064](https://openairdocs.org/sdr/VNAA202504170064.md): Floorbeam · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL 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 MM670-35302-035
- [SDR VNAA202504170063](https://openairdocs.org/sdr/VNAA202504170063.md): Door Sill · corroded · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > THE AFT CARGO DOOR FLOOR SILL IS CORRODED.
- [SDR VNAA202504170062](https://openairdocs.org/sdr/VNAA202504170062.md): Slat Track · worn · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge Devices
  > FOUND 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. CC670-12070-3PE
- [SDR VNAA202504170061](https://openairdocs.org/sdr/VNAA202504170061.md): Slat Track · worn · Apr 17, 2025 · N508AE · Cndair CL6002C10 · Leading Edge Devices
  > DISCREPANCY: 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. CC670-12070-3PE

Next page: https://openairdocs.org/aircraft/N508AE/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N508AE/reports

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