# Service difficulty reports: N512AE

A list on [N512AE](https://openairdocs.org/aircraft/N512AE.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 4 · 159 reports

- [SDR VNAA2026082023201](https://openairdocs.org/sdr/VNAA2026082023201.md): O-Ring · leaking · Aug 17, 2026 · N512AE · Cndair CL6002C10 · Fuel Storage
  > FUEL LEAK UNDER CENTER TANK. FUMES IN CABIN. FOUND LOWER WIGGINGS FITTING LEAKING ON SINGLE POINT REFUEL TUBE. REMOVED AND REPLACED THE SPFMT 4 O-RINGS IAW AMM 28-25-11-000/400-801-A06. REMOVED AND REPLACED THE ADAPTER ON THE SOV MANIFOLD HOUSING IAW AMM 28-
- [SDR VNAA20260508003](https://openairdocs.org/sdr/VNAA20260508003.md): Skin · ground damage · May 6, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MANLIFT MADE CONTACT WITH AIRCRAFT BETWEEN FS 1144 - FS 1162. REPAIRED AREA BETWEEN SKIN STGR 5L -7L AND FRAME 55.625% - SPAR 67.50% IAW MHIRJ REO 670-53-71-102 REV -- DATED 2026-04-23.
- [SDR VNAA20260511019](https://openairdocs.org/sdr/VNAA20260511019.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NO. 3-1 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 3-1 IAW REO 670-57-42-2332REV: -- DATED:2026-01-16.
- [SDR VNAA20260511018](https://openairdocs.org/sdr/VNAA20260511018.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NO. 2-3 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 2-3 IAW REO 670-57-42-2333 REV:--DATED 2026-01-16.
- [SDR VNAA20260511017](https://openairdocs.org/sdr/VNAA20260511017.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NO. 2-1 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 2-1 IAW MHIRJ REO 670-57-42-2329 REV-- DATED 1-16-26.
- [SDR VNAA20260511016](https://openairdocs.org/sdr/VNAA20260511016.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NO. 1-3 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 1-3 IAW REO 670-57-42-2331 REV-- DATED 2026-03-11.
- [SDR VNAA20260511015](https://openairdocs.org/sdr/VNAA20260511015.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NR 1-2 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 1-2 IAW REO 670-57-42-2323 REV-- DATED 2026-01-15.
- [SDR VNAA20260511014](https://openairdocs.org/sdr/VNAA20260511014.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NR 1-1 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 1-1 IAW MHIRJ REO 670-57-42-2326 REV-- DATED 1-15-26.
- [SDR VNAA20260508011](https://openairdocs.org/sdr/VNAA20260508011.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-3 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 1-2 IAW MHIRJ REO 670-57-42-2334 REV-.
- [SDR VNAA20260508010](https://openairdocs.org/sdr/VNAA20260508010.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-3 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 2-3 IAW MHIRJ REO 670-57-42-2338 REV-.
- [SDR VNAA20260508009](https://openairdocs.org/sdr/VNAA20260508009.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 2-2 IAW MHIRJ REO 670-57-42-2336 REV.-.
- [SDR VNAA20260508008](https://openairdocs.org/sdr/VNAA20260508008.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-3 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-2335 REV-.
- [SDR VNAA20260508007](https://openairdocs.org/sdr/VNAA20260508007.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-2 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RH SLAT TRACK 1-2 IAW REO 670-57-42-2325 REV-.
- [SDR VNAA20260508006](https://openairdocs.org/sdr/VNAA20260508006.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-1 HAS CHAFING/WEAR MARKS FROM CONTACT WITH ROLLERS IN MULTIPLE PLACES. REPAIRED RT SLAT TRACK 1-1 IAW REO 670-57-42-2327 REV: -- DATED 2026-01-16.
- [SDR VNAA20260508005](https://openairdocs.org/sdr/VNAA20260508005.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NO. 3-3 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LH SLAT 3-3 IAW MHIRJ REO 670-57-42-2342 REV:-- DATED: 2026-01-20.
- [SDR VNAA20260508004](https://openairdocs.org/sdr/VNAA20260508004.md): Slat Track · worn · Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT NO. 3-2 HAS MULTIPLE CHAFED SPOTS FROM CONTACT WITH ROLLERS. REPAIRED LT SLAT 3-2 IAW MHIRJ REO 670-57-42-2340 REV--.
- [SDR VNAA20260508014](https://openairdocs.org/sdr/VNAA20260508014.md): Rib · damaged · Feb 18, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT WING I/B FLAP L/E RIB (P/N CC670-14102-2) HAS 1EA ELONGATED NUTPLATE HOLE ON THE O/B SIDE. REPAIRED IAW REO 670-57-52-644 REV-A DATED 2026-02-16
- [SDR VNAA20260508002](https://openairdocs.org/sdr/VNAA20260508002.md): Skin · dented · Feb 11, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PER CUSTOMER REQUEST WORK REO 670-53-61-2676 REV (P1) DATED 2026-02-09 ( REPAIR TO DENTS ON FUSELAGE SKIN BETWEEN FS1000.00-FS1051.30 AND STR24R-STR26L) COMPLIED WITH MHIRJ REO 670-53-61-2676 REV -- DATED 2026-03-04 (REPAIR TO DENTS ON FUSELAGE SKIN BETWEEN
- [SDR VNAA20260508001](https://openairdocs.org/sdr/VNAA20260508001.md): Retainer · corroded · Feb 9, 2026 · N512AE · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > UPON REMOVAL OF MAIN AVIONICS DOOR SEAL FOUND CORROSION ON THE RETAINER OF THE MAIN AVIONICS DOOR. REMOVED AND REPLACED AVIONICS DOOR SEAL RETAINER (PN CC670-38662-5) IAW CRJ-700 SRM 51-42-06-001-001-A01.
- [SDR VNAA20260511010](https://openairdocs.org/sdr/VNAA20260511010.md): Door Frame · corroded · Feb 5, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Structure
  > COCKPIT DOOR POST IS CORRODED AT RBL 11 W.L.72.5. REPAIRED RBL 11 COCKPIT DOOR POST IAW BOMBARDIER GREO 670-53-11-745 REV -A DATED 2016-10-28.
- [SDR VNAA20260511011](https://openairdocs.org/sdr/VNAA20260511011.md): Floorbeam · corroded · Feb 3, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > F.S.280 LOWER WEB IS CORRODED ON EDGE AT LBL 11 BETWEEN CORROSION CAP AND DOOR POST. REPLACED LH FS 280 CROSS BEAM WITH NEW, P/N CC670-34094-1S IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR VNAA20260508022](https://openairdocs.org/sdr/VNAA20260508022.md): Actuator · corroded · Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > RIGHT FLAP VANE ACTUATOR AT FLS 140.4 FWD AND AFT TRUNNION BODY HAVE CORROSION. RECEIVED NEW SERVICEABLE RH FLS 140.4 FWD TRUNNION BODY P/N 601R14261-1. REFERENCE CO: 10110125, HR00593771 FOR ASSY OF RH FLAP VANE ACTUATOR FLS 140.4.
- [SDR VNAA20260508021](https://openairdocs.org/sdr/VNAA20260508021.md): Actuator · corroded · Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > RIGHT FLAP VANE ACTUATOR AT FLS 140.4 FWD AND AFT TRUNNION BODY HAVE CORROSION. RECEIVED NEW SERVICEABLE AFT TRUNNION BODY P/N 601R14270-21. REFERENCE CO: 10110125, HR00593771 FOR ASSY OF RH FLAP VANE ACTUATOR FLS 140.4.
- [SDR VNAA20260508020](https://openairdocs.org/sdr/VNAA20260508020.md): Actuator · corroded · Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > RIGHT FLAP VANE ACTUATOR AT FLS 65.5 FWD AND AFT TRUNNION BODY HAVE CORROSION. RECEIVED NEW SERVICEABLE FWD TRUNNION BODY P/N 601R14261-1 AT FLS 65.5. REFERENCE CO:10110125, HR00593771 FOR ASSEMBLY OF RH FLAP VANE ASSY.
- [SDR VNAA20260508019](https://openairdocs.org/sdr/VNAA20260508019.md): Actuator · corroded · Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > RIGHT FLAP VANE ACTUATOR AT FLS 65.5 FWD AND AFT TRUNNION BODY HAVE CORROSION. RECEIVED NEW SERVICEABLE AFT TRUNNION BODY P/N 601R14270-21. REFERENCE HR593771 FOR ASSY OF RH FLAP VANE ACTUATOR ASSY FLS65.5.
- [SDR VNAA20260508018](https://openairdocs.org/sdr/VNAA20260508018.md): Actuator · corroded · Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > LEFT FLAP VANE ACTUATOR AT FLS 102.9 FWD AND AFT TRUNNION BODY HAVE CORROSION. RECEIVED NEW LH FLS 102.9 FWD TRUNNION BODY P/N 601R14261-1. REFERENCE HR593712 FOR ASSY OF LH FLS 102.9 FLAP VANE ACTUATOR.
- [SDR VNAA20260508017](https://openairdocs.org/sdr/VNAA20260508017.md): Actuator · corroded · Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > LEFT FLAP VANE ACTUATOR AT FLS 102.9 FWD AND AFT TRUNNION BODY HAVE CORROSION. RECEIVED NEW LH FLS 102.9 AFT TRUNNION BODY P/N 601R14270-21. REFERENCE HR00593712 FOR ASSY OF LH FLS 102.9 FLAP VANE ACTUATOR.
- [SDR VNAA20260511025](https://openairdocs.org/sdr/VNAA20260511025.md): Attach Bracket · corroded · Jan 24, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT O/B FLAP HINGE ARM AFT FAIRING BRACKET IS CORRODED AT WS 178. REMOVED AND REPLACED BRACKET P/N 601R14629-82 I.A.W. CRJ-700 S.R.M. 51-42-06-001-001-A01
- [SDR VNAA20260511013](https://openairdocs.org/sdr/VNAA20260511013.md): Seat Track · corroded · Jan 24, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT LBL27 BETWEEN F.S.364 TO F.S.477 IS CORRODED. REMOVED AND REPLACED CORRODED SEAT TRACK AT LBL 27 BETWEEN FS 364.00 AND FS 477.00 WITH NEW SERVICEABLE SEAT TRACK PN: SH690-32127-3 IAW CRJ-700 AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801
- [SDR VNAA20260511032](https://openairdocs.org/sdr/VNAA20260511032.md): Seat Track · corroded · Jan 22, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 785 AND FS 863. INSTALLED NEW LH SIDE SEAT RAIL AT STGR 15L BETWEEN FS 785 AND FS 863 PN SH670-36260-5 IAW CRJ 700 AMM 53-00-49-400-801-A03
- [SDR VNAA20260511031](https://openairdocs.org/sdr/VNAA20260511031.md): Seat Track · corroded · Jan 20, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 708 AND FS 761. INSTALLED NEW LH SIDE SEAT RAIL FROM FS 708 TO FS 761 PN SH670-37509-1 IAW CRJ 700 AMM 53-00-49-400-801-A03
- [SDR VNAA20260508016](https://openairdocs.org/sdr/VNAA20260508016.md): Floor Support · damaged · Jan 18, 2026 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF LH FS 280 CROSS BEAM FOUND SEVERAL OVERSIZED FASTENER HOLES IN THE LH FLOOR SILL BETWEEN FS 280 AND FS 290. REPAIRED LH FLOOR SILL OVERSIZED FASTENER HOLES BETWEEN FS 280 AND FS 290 REO 670-53-21-2788 REV-- DATED 2-25-26.
- [SDR VNAA20260511009](https://openairdocs.org/sdr/VNAA20260511009.md): Door Frame · corroded · Jan 17, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Structure
  > COCKPIT DOOR POST IS CORRODED AT LBL 11 W.L.72.5. REPAIRED LBL 11 COCKPIT DOOR POST IAW BOMBARDIER GREO 670-53-11-745 REV -A DATED 2016-10-28.
- [SDR VNAA20260508015](https://openairdocs.org/sdr/VNAA20260508015.md): Fitting · gouged · Jan 17, 2026 · N512AE · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > RIGHT AILERON HINGE FITTING NO. 3 (WING SIDE) IS GOUGED ON THE LOWER SIDE. REPAIRED RH AILERON HINGE FITTING#3 AT WS323.058 IAW MHIRJ REO 670-57-51-677 REV -.
- [SDR VNAA20260508013](https://openairdocs.org/sdr/VNAA20260508013.md): Fitting · cracked · Jan 17, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT FLAP HINGE BOX AFT MOUNTING FITTING AT WS 54.55 (WING SIDE) HAS GOUGES ON THE I/B LUG. REPAIRED INBD FLAP HINGE BOX ATTACHMENT, AFT HINGE FITTING AT WS54.55 LHS IAW MHIRJ REO 670-57-21-1101 REV -- DATED 2026-01-07.
- [SDR VNAA20260511024](https://openairdocs.org/sdr/VNAA20260511024.md): Skin · damaged · Jan 16, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flaps
  > PANEL 584FB HAS DAMAGED SCREW HOLE FROM WHAT APPEARS TO BE SOMEONE DRILLING OUT A SCREW. REPAIRED LH I/B FLAP FWD SPAR LOWER FLANGE IAW MHIRJ REO 670-57-52-642 REV-- DATED 2026-01-16.
- [SDR VNAA20260508012](https://openairdocs.org/sdr/VNAA20260508012.md): Angle · cracked · Jan 15, 2026 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE ASSY IN FLIGHT DECK AT LBL9 (PN CC670-33199-3) BETWEEN FS259.20-FS280 IS CRACKED. CRACK IS APPROXIMATLY.250 IN LENGTH. REMOVED DESCREPANT LBL9 (PN CC670-33199-3) CAM LOC ASSY (ANGLE ASSY) IAW CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW/SERVICEABL
- [SDR VNAA20260511030](https://openairdocs.org/sdr/VNAA20260511030.md): Seat Track · corroded · Jan 2, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 573 AND FS 677. INSTALLED NEW SERVICEABLE PN SH670-33558-3 ON LH STGR 15L BETWEEN FS 573 AND FS677 IAW AMM 53-00-49-400-801-A03
- [SDR VNAA20260511026](https://openairdocs.org/sdr/VNAA20260511026.md): Fitting · gouged · Jan 2, 2026 · N512AE · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > LT FLAP HINGE BOX AFT MOUNTING FITTING AT WS 128 (WING SIDE) HAS GOUGES ON THE I/B LUG. REPAIRED LH FLAP HINGE BOX AFT MOUNTING FITTING AT WS 128 I/B LUG IAW MHIRJ REO 670-57-51-1093 REV --.
- [SDR VNAA20260511012](https://openairdocs.org/sdr/VNAA20260511012.md): Fitting · corroded · Jan 2, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FLOOR FITTING HAS CORROSION AROUND NUT PLATE AT APPROX. RBL15 AND F.S.285. REMOVED UNSERVICABLE FITTING AND INSTALLED NEW SERVICEABLE FLOOR FITTING P/N SH670-32149-3 LOCATED AT APPROX RBL 15 AND F.S. 285.00 IAW CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR VNAA20260511021](https://openairdocs.org/sdr/VNAA20260511021.md): Angle · corroded · Dec 17, 2025 · N512AE · Cndair CL6002C10 · Aerodynamic Fairings
  > AFT FUSELAGE FAIRING SUPPORT WEB IS CORRODED ON THE FWD FACE AT FS 939. INSTALLED NEW SERVICEABLE CENTER ANGLE PN: SH670-39189-1 ON AFT FUSELAGE FAIRING SUPPORT WEB AFT FACE AT FS 939 IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A01.
- [SDR VNAA20260511006](https://openairdocs.org/sdr/VNAA20260511006.md): Bracket · corroded · Dec 17, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > BRACKET IS CORRODED AT STRINGER 22R AND F.S.285. INSTALLED BRACKET P/N SH670-96034-5 AT STRINGER 22R FS 285 IAW SRM 51-42-001-001-A01.
- [SDR VNAA20260511005](https://openairdocs.org/sdr/VNAA20260511005.md): Frame · corroded · Dec 17, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SECTOR AT F.S.319 IS CORRODED AT STRINGER 21L. INSTALLED NEW FRAME AT FS 319, P/N SH670-31891-3, IAW SRM 51-42-06-001-001-A01.
- [SDR VNAA20260511004](https://openairdocs.org/sdr/VNAA20260511004.md): Floorbeam · corroded · Dec 17, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AVI FLOORBOARD SUPPORT ANGLE ON THE F.S.280 FRAME IS CORRODED. REMOVED AND REPLACED AVI FLOORBOARD ANGLE ON FS280 FRAME IAW SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-06-001-001-A01.
- [SDR VNAA20260511022](https://openairdocs.org/sdr/VNAA20260511022.md): Strap · corroded · Nov 30, 2025 · N512AE · Cndair CL6002C10 · Aerodynamic Fairings
  > FS 629 WING-TO-FUSELAGE FAIRING SUPPORT STRAP IS CORRODED ON THE LOWER SIDE. INSTALLED NEW WING-TO-FUSELAGE FAIRING SUPPORT STRAP (P/N SH670-39054-3) AT FS 629 IAW CRJ-700 SRM 51-23-00-001-001-A01 AND CRJ-700 SRM 51-25-16-001-001-A01.
- [SDR VNAA20260511036](https://openairdocs.org/sdr/VNAA20260511036.md): Seat Track · corroded · Nov 24, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 785 AND FS 863. REMOVED RH SIDE SEAT RAIL AT STGR 15R BETWEEN FS 785 AND FS 863, P/N SH670-36260-5, IAW CRJ 700 AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICEABLE SIDE SEAT RAIL, P/N SH670-36260-5, AT STG
- [SDR VNAA20260511008](https://openairdocs.org/sdr/VNAA20260511008.md): Door Sill · corroded · Nov 18, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR LOWER SILL ANGLE IS CORRODED. REPLACED PAX DOOR LOWER SILL ANGLE P/N SH670-31875-3S WITH NEW SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR VNAA20260511007](https://openairdocs.org/sdr/VNAA20260511007.md): Door Sill · corroded · Nov 18, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR LOWER SILL MID CAP ANGLE IS CORRODED. EVALUATED CORRODED PASSENGER DOOR LOWER SILL MID CAP ANGLE AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW CRJ-700 SRM 53-21-23-101-001-A01 DUE TO EXCESSIVE CORROSION AND MATERIAL LOSS. REMOVED AND REPLACED P
- [SDR VNAA20260511003](https://openairdocs.org/sdr/VNAA20260511003.md): Stringer · corroded · Nov 16, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 20L IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REMOVED CORROSION AT STGR 20L BETWEEN FS349 TO FS364 FOUND TO BE OUT OF LIMITS NO DAMAGE ALLOWED AT STRINGER 20L IAW CRJ 700 SRM 53-21-03-101-001-A01. PERFORMED STGR 20L SPLICE REPAIR IAW REO 670-53-21-2774 R
- [SDR VNAA20260511038](https://openairdocs.org/sdr/VNAA20260511038.md): Seat Track · corroded · Nov 14, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 485 AND FS 581. INSTALLED NEW SERVICEABLE RBL 9 SEAT RAIL BETWEEN FS 485 AND FS 581 PN SH670-33426-1 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Next page: https://openairdocs.org/aircraft/N512AE/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 = 'N512AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N512AE/reports

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