# Service difficulty reports: N534AE

A list on [N534AE](https://openairdocs.org/aircraft/N534AE.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 2 · 81 reports

- [SDR VNAA202603130001](https://openairdocs.org/sdr/VNAA202603130001.md): Structure · elongated · Mar 13, 2026 · N534AE · Cndair CL6002C10 · Fuselage Main, Structure
  > LH PRESSURE BOX AT FS 847 HAS MULTIPLE ELONGATED HOLES COMMON TO LBL 18 FLOOR BEAM SH670-35834-3 PRESSURE BOX
- [SDR VNAA2025041511102](https://openairdocs.org/sdr/VNAA2025041511102.md): Skin · dented · Apr 13, 2025 · N534AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LH SIDE FWD FUSELAGE DENT (REO) 670-53-11-2108 / C/W REO 670-53-11-2108 REPAIR FOR DENT DAMAGE TO UPPER FUSELAGE SKIN PANEL BETWEEN FS 220.00 - FS250.00 AND STR12L - STR15L
- [SDR VNAA2025041511101](https://openairdocs.org/sdr/VNAA2025041511101.md): Skin · damaged · Apr 13, 2025 · N534AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > (RH) NOSE SKIN DAMAGED AFT OF TRU ACCESS PANEL / C/W REO 670-53-11-815 REPAIR TO UPPER SECTOR FS193.00.
- [SDR VNAA20231014025](https://openairdocs.org/sdr/VNAA20231014025.md): Frame · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME @ F.S 319 STR 25 R HAS CORROSION. REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01.
- [SDR VNAA20231014029](https://openairdocs.org/sdr/VNAA20231014029.md): Skin · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/Skin
  > R/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1291 REV IR DATED 09/19/2023.
- [SDR VNAA20231014028](https://openairdocs.org/sdr/VNAA20231014028.md): Skin · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/Skin
  > R/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, MIDDLE HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1290 REV IR DATED 09/19/2023.
- [SDR VNAA20231014027](https://openairdocs.org/sdr/VNAA20231014027.md): Skin · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/Skin
  > R/H WING, LOWER WING SKIN HAS CHAFE DAMAGE JUST FORWARD OF THE OUTBOARD FLAP, INBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1245 REV IR DATED 09/19/2023.
- [SDR VNAA20231014026](https://openairdocs.org/sdr/VNAA20231014026.md): Stringer Splice · corroded · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR 25R @ MULTIPLE LOCATIONS FROM F.S 280 THRU F.S 333. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA20231014023](https://openairdocs.org/sdr/VNAA20231014023.md): Skin · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/Skin
  > L/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF OUTBOARD FLAP, MID HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1297 REV IR DATED 09/20/2023.
- [SDR VNAA20231014022](https://openairdocs.org/sdr/VNAA20231014022.md): Skin · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/Skin
  > /H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF INBOARD FLAP, OUTBOARD HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX FAIRING. REPAIRED IAW EA 23-C7-57-1251 REV IR DATED 09/20/2023.
- [SDR VNAA20231014024](https://openairdocs.org/sdr/VNAA20231014024.md): Skin · chafed · Oct 17, 2023 · N534AE · Cndair CL6002C10 · Wing, Plate/Skin
  > L/H WING, LOWER WING SKIN IS CHAFED JUST FORWARD OF OUTBOARD FLAP, MID HINGE BOX. DAMAGE IS FROM CONTACT WITH HINGE BOX. REPAIRED IAW OLIVER WYMAN EA 23-C7-57-1297 REV IR DATED 09/20/2023.
- [SDR VNAA20231014013](https://openairdocs.org/sdr/VNAA20231014013.md): Seat Track · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > REMOVED AND REPLACED IAW CRJ 700 AMM 53-00-49-000/400-801-A01 AND CRJ 700 SRM 51-40-11-001-001-A01.
- [SDR VNAA20231014020](https://openairdocs.org/sdr/VNAA20231014020.md): Angle · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL ANGLE IS CORRODED.
- [SDR VNAA20231014015](https://openairdocs.org/sdr/VNAA20231014015.md): Stiffener · cracked · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FWD PAX DOOR WEB STIFFENER IS CRACKED.
- [SDR VNAA20231014012](https://openairdocs.org/sdr/VNAA20231014012.md): Seat Track · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > .LH #2 SEAT TRACK IS CORRODED AT LBL 9
- [SDR VNAA20231014011](https://openairdocs.org/sdr/VNAA20231014011.md): Former · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Structure (General)
  > REMOVED AND REPLACED IAW CRJ700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA20231014021](https://openairdocs.org/sdr/VNAA20231014021.md): Cleat · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLIPS THAT ATTACH TO THE FWD AND AFT ENDS OF "ANGLE C" LOCATED ON INNER PORTION OF OUTER HANDLE BOX BELOW HINGE ARE CORRODED.
- [SDR VNAA20231014010](https://openairdocs.org/sdr/VNAA20231014010.md): Angle · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SILL ANGLE IS CORRODED.
- [SDR VNAA20231014009](https://openairdocs.org/sdr/VNAA20231014009.md): Intercostal · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 27 RH INTERCOSTAL IS CORRODED BETWEEN FS 349.00 AND 364.00.
- [SDR VNAA20231014008](https://openairdocs.org/sdr/VNAA20231014008.md): Intercostal · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 20R INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND 349.00.
- [SDR VNAA20231014007](https://openairdocs.org/sdr/VNAA20231014007.md): Skin · cracked · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND CRACK ON PAX DOOR INNER SKIN AT PANEL CUTOUT.
- [SDR VNAA20231014030](https://openairdocs.org/sdr/VNAA20231014030.md): Joint · chafed · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 280.00 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STRINGER 27 AND 26R.
- [SDR VNAA20231014005](https://openairdocs.org/sdr/VNAA20231014005.md): Frame · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 310.00 FRAME IS CORRODED BETWEEN STRINGER 26L AND STRINGER 26R.
- [SDR VNAA20231014004](https://openairdocs.org/sdr/VNAA20231014004.md): Stringer · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R AT F.S. 300.00 HAS CORROSION AROUND FASTENER HOLE.
- [SDR VNAA20231014003](https://openairdocs.org/sdr/VNAA20231014003.md): Stringer Splice · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R SPLICE AT F.S. 333.00 IS CORRODED
- [SDR VNAA20231014017](https://openairdocs.org/sdr/VNAA20231014017.md): Floor Support · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED BETWEEN FS 280.00 AND 319.70.
- [SDR VNAA20231014016](https://openairdocs.org/sdr/VNAA20231014016.md): Door Sill · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL IS CORRODED BEYOND REPAIRABLE LIMITS
- [SDR VNAA20231014018](https://openairdocs.org/sdr/VNAA20231014018.md): Coaming · chafed · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RH UPPER TRANSCOWL FWD HOOK LATCH (INNER DOUBLER) IS CHAFED.
- [SDR VNAA20231014002](https://openairdocs.org/sdr/VNAA20231014002.md): Strap · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Wing Miscellaneous Structure
  > 670-57-21-867_REV-A (PERM REPAIR-LOWER SKIN ASSY AND INSTL WINGBOX) REPAIR IAW REO-670-57-21-867 WITHIN 8000 FH OR NEXT "C" CHECK.
- [SDR VNAA20231014001](https://openairdocs.org/sdr/VNAA20231014001.md): Skin · damaged · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Trailing Edge Flaps
  > LH I/B FLAP PANEL 584KB & UNDERLYING STRUCTURE HAS 1EA ELONGATED HOLE.
- [SDR VNAA20231014006](https://openairdocs.org/sdr/VNAA20231014006.md): Stiffener · cracked · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FWD PAX DOOR WEB STIFFENER IS CRACKED.
- [SDR VNAA20231014014](https://openairdocs.org/sdr/VNAA20231014014.md): Seat Track · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH #5 SEAT TRACK IS CORRODED AT LBL 9.
- [SDR VNAA20231014019](https://openairdocs.org/sdr/VNAA20231014019.md): Angle · corroded · Oct 14, 2023 · N534AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL MID CAP ANGLE IS CORRODED.
- [SDR VNAA202301201111](https://openairdocs.org/sdr/VNAA202301201111.md): Selector Valve · faulted · Jan 17, 2023 · N534AE · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > ONCE IN GEAR UP POSITION GOT GEAR DISAGREE WITH IND. THREE GREEN WHILE HANDLE IN UP POSITION. ALSO GOT NWS INOP CAUT MSG. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801-A01 OPS CHECK GOOD, GEAR SWING GOOD.
- [SDR VNAA2020031311102](https://openairdocs.org/sdr/VNAA2020031311102.md): Warning System · false activation · Mar 9, 2020 · N534AE · Cndair CL6002C10 · Leading Edge Slat Position Indicating System
  > SLATS FAIL CAUTION WHEN DEPLOYING FLAPS FOR LANDING. FLAPS 45 SLATS 0. PERFORMED SELF TEST OF SFECU IAW CRJ 700 AMM 27-51-05-740-801. TEST PASSED. PERFORMED OPS TEST OF FLAPS / SLATS SYSTEM IAW 27-50-00-710-801. OPS TEST GOOD.
- [SDR VNAA2020022061103](https://openairdocs.org/sdr/VNAA2020022061103.md): Slat System · malfunctioned · Feb 16, 2020 · N534AE · Cndair CL6002C10 · Leading Edge Slat Control System
  > 20 MIN OUT OF DCA THE CREW RECEIVED A SLAT FAIL MSG. THEY DIVERTED TO IAD FOR THE RW LENGTH. AC LANDED, AND TAXIED TO THE GATE SAFE. CLEARED SFECU INHIBITS IAW CRJ 700 AMM. PERFOMED SELF TEST OF SFECU AND OPS TEST OF SLATS AND FLAPS SYSTEM IAW CRJ 700 AMM. TES
- [SDR VNAA2019082199907](https://openairdocs.org/sdr/VNAA2019082199907.md): Seat Track · corroded · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT RAIL, 3RD FROM FRONT, STARTING AT APPROX FS581.00 GOUGED/CORRODED IN MULTIPLE LOCATIONS. FABRICATED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK AMM 53-00-49-400-801-A03 SEAT TRACK LBL 9 FROM FS 581-FS 677 SRM 53-00-49-201-002-A01.
- [SDR VNAA2019082199906](https://openairdocs.org/sdr/VNAA2019082199906.md): Seat Track · corroded · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT RAIL, 3RD FROM FRONT, STARTING AT APPROX FS581.00 CORRODED. FABRICATED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK AMM 53-00-49-400-801-A03 SEAT TRACK RBL 9 FROM FS 581-FS 677 SRM 53-00-49-201-002-A01.
- [SDR VNAA2019082199905](https://openairdocs.org/sdr/VNAA2019082199905.md): Floor Support · corroded · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FLOOR SILL ANGLE IS CORRODED BETWEEN FS 1000 AND FS 1047.00. REPAIRED AFT CARGO DOOR FLOOR SILL ANGLE BETWEEN FS 1000 TO FS 1047 IAW BOMBARDIER REO #670-53-61-913 REV A DATE 2012-11-02.
- [SDR VNAA2019082199904](https://openairdocs.org/sdr/VNAA2019082199904.md): Frame · corroded · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > FS 349 FRAME IS CORRODED ON AFT SIDE BETWEEN STR27 & 26R. REPAIRED FS 349 AFT SIDE BETWEEN STR 27 AND 26R IAW REO 670-53-21-1308.
- [SDR VNAA2019082199903](https://openairdocs.org/sdr/VNAA2019082199903.md): Frame · corroded · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > FS333 FRAME IS CORRODED ON AFT SIDE BETWEEN STR 27 & 26R. REPAIRED FS 333 ON AFT SIDE BETWEEN STR 27 AND STR 26L AND STR 27 AND STR 26L IAW REO 670-53-21-1308.
- [SDR VNAA2019082199902](https://openairdocs.org/sdr/VNAA2019082199902.md): Stringer · cracked · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > AFT OF FS280 AT STR 3L, LINTEL IS CRACKED APPROX 1" LONG. REPAIRED PAX DOOR LINTEL (STR 3LZ) IAW REO 670-53-21-493 REV D DATE 2015-07-10 AND SB#670BA-53-040 PART B.
- [SDR VNAA2019082199901](https://openairdocs.org/sdr/VNAA2019082199901.md): Drag Angle · cracked · Aug 21, 2019 · N534AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LEFT AFT FUSELAGE AFT DRAG ANGLE CRACKED. INSTALLED NEW L/H AFT FUSELAGE AFT DRAG ANGLE IAW CRJ700 SRM 51-42-10-001-001-A01, 51-42-21-001-A01.
- [SDR VNAA2019062861102](https://openairdocs.org/sdr/VNAA2019062861102.md): Shutoff Valve · failed · Jun 26, 2019 · N534AE · Cndair CL6002C10 · Pneumatic Indicating System
  > DURING CRUISE AT 35,800 FEET THE CREW RECEIVED A BLEED DUCT WARNING MESSAGE. THE OXYGEN MASKS DEPLOYED AND THE CREW FOLLOWED THE INSTRUCTIONS OF THE QRH AND LANDED AT THE NEAREST SUITABLE AIRPORT USING A DESCENT RATE OF 4200-4500 FPM. THE FLIGHT LANDED WITHOU
- [SDR VNAA2019061761102](https://openairdocs.org/sdr/VNAA2019061761102.md): Controller · failed · Jun 16, 2019 · N534AE · Cndair CL6002C10 · Pneumatic Distribution System
  > R BLEED DUCT (W/C) AND L BLEED DUCT (W/C) ALONG WITH RH/LH COWL A/I CAUTIONS. AS A RESULT BLEED VALVES CLOSED AND CABIN PRESSURE WAS LOST AIRCRAFT DIVERTED TO PITTSBURGH. GROUND RAN AIRCRAFT AND C/W LEAK CHECKS OF BLEED DUCTS AND A/C UNITS, NO LEAKS FOUND. FER
- [SDR VNAA2018010211101](https://openairdocs.org/sdr/VNAA2018010211101.md): Smoke Detector · false activation · Jan 2, 2018 · N534AE · Cndair CL6002C10 · Smoke Detection
  > THE CREW REPORTED AN AFT LAVATORY WARNING MESSAGE. THERE WAS NO PHYSICAL SMOKE OR ODOR OF SMOKE. THE SMOKE DETECTOR ALARM WILL NOT TURN OFF. MX R & R THE LAVATORY SMOKE DETECTOR. OPS CHECKED GOOD.
- [SDR VNAA2017101711101](https://openairdocs.org/sdr/VNAA2017101711101.md): Bpsu · warning message · Oct 17, 2017 · N534AE · Cndair CL6002C10 · Trailing Flap Position Indicating System
  > CREW RECEIVED FLAPS FAIL MESSAGE ON RETRACTION. RAN CHECKLIST AND DECLARED EMERGENCY. R & R THE LT BPSU, OPS CHECKED GOOD.
- [SDR VNAA2017070411103](https://openairdocs.org/sdr/VNAA2017070411103.md): Fadec · failed · Jul 4, 2017 · N534AE · Cndair CL6002C10 · Fuel Controlling System
  > FLIGHT DIVERTED DUE TO AN AMBER LEFT FADEC CAUTION MESSAGE. WAS ABLE TO TAXI TO A GATE. MX REPLACED THE FADEC.
- [SDR VNAA2017070399904](https://openairdocs.org/sdr/VNAA2017070399904.md): Doubler · cracked · Jul 2, 2017 · N534AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR PULL IN CAM DOUBLER CRACKED. REPLACED THE DOUBLER.
- [SDR SIMA20170510001](https://openairdocs.org/sdr/SIMA20170510001.md): Stiffener · cracked · May 10, 2017 · N534AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FUSELAGE BULKHEAD AT BS 202.75 STIFFENER AT RBL 30 LOWER END FOUND BENT AND CRACKED. REPAIRED IAW ERS-CR-53MR-2412.

Next page: https://openairdocs.org/aircraft/N534AE/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 = 'N534AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N534AE/reports

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