N512AE

Service difficulty reports · 159

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 = 'N512AE' 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 VNAA2026082023201O-Ring · leakingFUEL 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-Aug 17, 2026 · N512AE · Cndair CL6002C10 · Fuel StorageSDR VNAA20260508003Skin · ground damageMANLIFT 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.May 6, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20260511019Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511018Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511017Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511016Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511015Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260511014Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508011Slat Track · wornRIGHT 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-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508010Slat Track · wornRIGHT 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-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508009Slat Track · wornRIGHT 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.-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508008Slat Track · wornRIGHT 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-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508007Slat Track · wornRIGHT 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-.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508006Slat Track · wornRIGHT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508005Slat Track · wornLEFT 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.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508004Slat Track · wornLEFT 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--.Apr 2, 2026 · N512AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20260508014Rib · damagedRIGHT 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 2026-02-16Feb 18, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20260508002Skin · dentedPER 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 Feb 11, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20260508001Retainer · corrodedUPON 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.Feb 9, 2026 · N512AE · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR VNAA20260511010Door Frame · corrodedCOCKPIT 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.Feb 5, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260511011Floorbeam · corrodedF.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.Feb 3, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20260508022Actuator · corrodedRIGHT 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.Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA20260508021Actuator · corrodedRIGHT 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.Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA20260508020Actuator · corrodedRIGHT 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.Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA20260508019Actuator · corrodedRIGHT 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.Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA20260508018Actuator · corrodedLEFT 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.Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA20260508017Actuator · corrodedLEFT 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.Jan 25, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR VNAA20260511025Attach Bracket · corrodedRIGHT 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-A01Jan 24, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20260511013Seat Track · corrodedSEAT 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 53-00-49-400-801Jan 24, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511032Seat Track · corrodedLH 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-A03Jan 22, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511031Seat Track · corrodedLEFT 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-A03Jan 20, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260508016Floor Support · damagedUPON 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.Jan 18, 2026 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260511009Door Frame · corrodedCOCKPIT 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.Jan 17, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260508015Fitting · gougedRIGHT 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 -.Jan 17, 2026 · N512AE · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA20260508013Fitting · crackedLEFT 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.Jan 17, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20260511024Skin · damagedPANEL 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.Jan 16, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20260508012Angle · crackedANGLE 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/SERVICEABLJan 15, 2026 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20260511030Seat Track · corrodedLEFT 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-A03Jan 2, 2026 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511026Fitting · gougedLT 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 --.Jan 2, 2026 · N512AE · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA20260511012Fitting · corrodedFLOOR 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.Jan 2, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20260511021Angle · corrodedAFT 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.Dec 17, 2025 · N512AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA20260511006Bracket · corrodedBRACKET 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.Dec 17, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20260511005Frame · corrodedFRAME 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.Dec 17, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20260511004Floorbeam · corrodedAVI 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.Dec 17, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20260511022Strap · corrodedFS 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.Nov 30, 2025 · N512AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA20260511036Seat Track · corrodedRT 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 STGNov 24, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511008Door Sill · corrodedPASSENGER 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-A01Nov 18, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260511007Door Sill · corrodedPASSENGER 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 PNov 18, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260511003Stringer · corrodedSTGR 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 RNov 16, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20260511038Seat Track · corrodedRBL 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.Nov 14, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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