# Service difficulty reports: N525AE

A list on [N525AE](https://openairdocs.org/aircraft/N525AE.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 3 · 133 reports

- [SDR VNAA20260205004](https://openairdocs.org/sdr/VNAA20260205004.md): Fitting · broken · Dec 19, 2025 · N525AE · Bombdr CL6002D15 · Rudder Control System
  > DURING GAPS MEASSUREMENT ON REPLACEMENT OF RUDDER PRIMARY FEEL UNIT SHAFT IN REF TO_27-079-001-20-REQ, PIN FITTING LH SIDE WAS BROKEN. PIN FITTING LH SIDE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-13-001-001-A01 AND (ET) HFEC I
- [SDR VNAA20260205003](https://openairdocs.org/sdr/VNAA20260205003.md): Lug · corroded · Dec 19, 2025 · N525AE · Bombdr CL6002D15 · Ailerons
  > CORROSION WAS FOUND AT LOWER LUG 5 (1EA) AT RH AILERON. LOWER LUG 5 (1EA) AT RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV--.
- [SDR VNAA20260205002](https://openairdocs.org/sdr/VNAA20260205002.md): Hinge · corroded · Dec 19, 2025 · N525AE · Bombdr CL6002D15 · Ailerons
  > NICKS AND CORROSION WERE FOUND AROUND OF INTERNAL LUG ON HINGE #1 ALSO CORROSION INSIDE BORE. LUG ON HINGE #1 WAS REPAIRED PER REO 670-57-51-678 REV --
- [SDR VNAA20260205001](https://openairdocs.org/sdr/VNAA20260205001.md): Floorbeam · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION WAS FOUND AT CROSSBEAM BETWEEN BL 0 TO RBL 9 ON FUSELAGE STA 280. CROSSBEAM BETWEEN BL 0 TO RBL 9 ON FUSELAGE BS 280 WAS EVALUATE FOUND EXCESSIVE DAMAGE PER SRM 53-21-23-101-002-A01 AND REPLACED PER SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-10-001
- [SDR VNAA20260203019](https://openairdocs.org/sdr/VNAA20260203019.md): Strap · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP ON ACCESS FAIRING 196DR. STRAP ON ACCESS FAIRING 196DR WERE INSTALLED PER CRJ-700 SRM 51-42-10- 001-001-A01
- [SDR VNAA20260203018](https://openairdocs.org/sdr/VNAA20260203018.md): Access Panel · damaged · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Wing, Plate/Skin
  > ELONGATED HOLES (2EAS) ON ACCESS PANEL 622AR AT RH WING. ELONGATED HOLES (2EAS) ON ACCESS PANEL 622AR AT RH WING WERE REPAIRED PER EA 5741-2026-0081 REV. A AND PER EA 57-2025-1673 REV A.
- [SDR VNAA20260203017](https://openairdocs.org/sdr/VNAA20260203017.md): Hinge · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Door Hinge
  > CORROSION ON HINGE OF STEP PANEL 832ET. DUE TO EXCESSIVE DAMAGE HINGE OF STEP PANEL 832ET WAS REPLACED PER CRJ-700 SRM 52-11-04-101-001-A01 AND PER CRJ -700 AMM 20-21-00-910-801 (A01)
- [SDR VNAA20260203016](https://openairdocs.org/sdr/VNAA20260203016.md): Angle · cracked · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACKED AFT LWR ANGLE OF REFUEL-DEFUEL ADAPTER SUPPORT STRUCTURE. AFT LWR ANGLE OF REFUEL/DEFUEL ADAPTER SUPORT STRUCTURE WAS REPAIRED PER REO 670-28-25-022 REV --
- [SDR VNAA20260203015](https://openairdocs.org/sdr/VNAA20260203015.md): Hinge Fitting · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Trailing Edge Flaps
  > CORROSION ON FWD, CTR & AFT HINGES OF FLAP STEP PLATE OF AFT BAGGAGE BAY. FWD, CTR & AFT HINGES OF FLAP STEP PLATE OF AFT BAGGAGE BAY WERE REPLACED PER SRM 51-42-06-001-001-A01
- [SDR VNAA20260203014](https://openairdocs.org/sdr/VNAA20260203014.md): Skin · dented · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN BTW BS 1000 -1015, S25L - S26R. THE FUSELAGE SKIN REPAIRED IAW REO 670-53-61-2661 REV-, AND REO 670-51-00-085 REV - A.
- [SDR VNAA20260203013](https://openairdocs.org/sdr/VNAA20260203013.md): Angle · cracked · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > TWO CRACKS ON INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.
- [SDR VNAA20260203012](https://openairdocs.org/sdr/VNAA20260203012.md): Frame · gouged · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > GOUGED FRAME BS 280, WL 79.50 BTWN S25L - S25R AT FWD AVIONICS BAY. THE FRAME WAS REPAIRED IAW 670-53-11-2248 REV-.
- [SDR VNAA20260203011](https://openairdocs.org/sdr/VNAA20260203011.md): Frame · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME STA 863 STRINGER 27. THE FRAME WAS REMOVED IAW SRM 51-21-06-001-001-A01, EVALUATED WITHIN LIMITS IAW SRM 53-51-06-101-003-A01, & SRM 53-00-00-101-001-A01.
- [SDR VNAA20260203010](https://openairdocs.org/sdr/VNAA20260203010.md): Seat Track · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND WEAR SEVERAL POINTS ON SIDE SEAT TRACK, BS 669.40 - 977 LT& RT IN THE PASSENGER CABIN. THE SEAT TRACK WERE REPLACED IAW SRM 53-00-49-400-801 CONF. A03, AND EVALUATE IAW SRM 53-51-49-101-001-A01.
- [SDR VNAA20260202007](https://openairdocs.org/sdr/VNAA20260202007.md): Frame · corroded · Dec 6, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS349.00 BETWEEN STGR25L TO STGR26R. DUE TO EXCESS DAMAGE ON FRAME FS349.00 BETWEEN STGR25L AND STGR26R WAS REPLACED PER SRM 53-00-06-201-005-A01 AND 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR VNAA20260205005](https://openairdocs.org/sdr/VNAA20260205005.md): Floorbeam · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > AFTER REMOVAL ANGLE FLOOR SUPPORT CORROSION WAS FOUND AT CROSSBEAM BETWEEN BL 0 TO LBL 9 ON FUSELAGE STA 280. CROSSBEAM BETWEEN BL 0 TO LBL 9 ON FUSELAGE STA 280.0 WAS REPLACED PER SRM 51-42-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01
- [SDR VNAA20260203009](https://openairdocs.org/sdr/VNAA20260203009.md): Drag Angle · cracked · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRAC
- [SDR VNAA20260203008](https://openairdocs.org/sdr/VNAA20260203008.md): Hinge Fitting · excess play · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Vertical Stabilizer
  > FREE PLAY ON TWO BEARINGS OF CENTER HINGES NR 2 & 3 OF THE RUDDER AT VERTICAL STABILIZER REAR SPAR. THE HINGE FITTINGS WERE REPLACED IAW RIL#2103 REV. B.
- [SDR VNAA20260203007](https://openairdocs.org/sdr/VNAA20260203007.md): Beam · damaged · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION ON UPPER SKIN OF LONGITUDINAL BEAM LBL 9 BTW BS 1069 - 1031IN THE AFT CARGO BAY, PAINT LONGITUDINAL BEAMS WAS REMOVED IAW SRM 51-26-01-001-001-A01, AND THE DAMAGE WAS NOT FOUND AND WAS PAINTED IAW SRM 51-21-11-001-001-A01, SRM 51-25-06-001-001-A01,
- [SDR VNAA20260203006](https://openairdocs.org/sdr/VNAA20260203006.md): Seat Track · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > NICKS, WEAR, AND CORROSION ON RT SIDE SEAT TRACKS, STGR 15R BS 379 - 669 IN THE PAX CABIN. THE SEAT TRACKS DUE EXCESSIVE DAMAGE WERE EVALUATE IAW SRM 53-51-49-101-001-A01. AND REPLACED IAW AMM 53-00-49-400-801.
- [SDR VNAA20260203005](https://openairdocs.org/sdr/VNAA20260203005.md): Seat Track · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > NICKS, WEAR AND CORROSION ON LT SEAT TRACKS AT STGR 15L (SECTION) BS 379 - 483, SEAT TRACK BS 483 - 573, SEAT TRACK BS 573 - 669 IN THE PAX CABIN. THE SEAT TRACKS BS 379 - 669 WERE REMOVED IAW AMM 53-00-49-000-801-A03, & REPLACED IAW AMM 53-00-49-400-801.
- [SDR VNAA20260203004](https://openairdocs.org/sdr/VNAA20260203004.md): Seat Track · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND WEAR ON SEAT TRACKS AT LBL 9, LBL 27, & RBL 9 (3 EACH) BS 349 - 477 IN THE PAX CABIN. THE SEAT TRACKS WERE EVALUATE IAW SRM 53-51-49-101-001-A01 AND REPLACED IAW AMM 53-00-49-400-801.
- [SDR VNAA20260203003](https://openairdocs.org/sdr/VNAA20260203003.md): Seat Track · gouged · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGE ON LOWER SURFACE OF THE LT SEAT TRACK BS 685 IN THE PAX CABIN. THE SEAT TRACK WAS REPAIRED IAW REO 670-53-41-791 REV -.
- [SDR VNAA20260203002](https://openairdocs.org/sdr/VNAA20260203002.md): Hinge Fitting · gouged · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Ailerons
  > GOUGE ON AILERON HINGE FITTING NBR 2 OTBD LUG AT LH WING. THE AILERON HINGE FITTING NR 2 OTBD LUG WAS REPAIRED IAW REO 670-57-51-676, REV -.
- [SDR VNAA20260203001](https://openairdocs.org/sdr/VNAA20260203001.md): Floor Support · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BEHIND FLOOR SUPPORT ANGLES STA 280 AND 12 RBL AND 12 LBL AT PASSENGER CABIN. EVALUATED OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND WERE REPAIRED IAW SRM 53-11-10-201-004-A01.
- [SDR VNAA20260202010](https://openairdocs.org/sdr/VNAA20260202010.md): Angle · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON POST PLATES(2EAS) COCKPIT DOOR FRAME LOWER AREA STA 280 AND 12 RBL AND 12 LBL AT COCKPIT. ANGLES (2 EAS) AND SPLICE PLATE (2 EAS) IN COCKPIT DOOR FRAME LOWER AREA STA 280 AND 12 RBL AND 12 LBL AT COCKPIT WERE REPLACED PER CRJ-700 SRM 51-42-10-001
- [SDR VNAA20260202009](https://openairdocs.org/sdr/VNAA20260202009.md): Floorbeam · corroded · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR ACCESS SUPPORT ANGLE STA 280, BETWEEN 9 RBL AND 9 LBL AT PASSENGER CABIN. FOR EXCESSIVE DAMAGE ON FLOOR ACCESS SUPPORT ANGLE STA 280, BETWEEN 9 RBL AND 9 LBL AT PASSENGER CABIN. MUST BE REPLACED PER CRJ-700 SRM 53-21-23-101-002-A01 PAR.4.A
- [SDR VNAA20260202008](https://openairdocs.org/sdr/VNAA20260202008.md): Drip Tray · damaged · Dec 5, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON RH SIDE DRIP PAN STA 280 AND WL 72.5 AT PASSENGER CABIN. TRAY DRIP ASSY RH PN: SH670-31731-3 WAS REPLECED PER TRAY DRIP ASSY RH PN: BA670-31155-1SB IN ACORDANCE PER SB 670BA-53-041 REV. M AND PER CRJ-700 SRM 51-42-10-001-001-A01
- [SDR VNAA20260205011](https://openairdocs.org/sdr/VNAA20260205011.md): Strap · worn · Dec 4, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > GOUGES ON UPPER STRAP OF PASSENGER DOOR SURROUND STRUCTURE FRAME 349.0 STGR 3LH AT PASSENGER CABIN. GOUGES ON UPPER STRAP OF PASSENGER DOOR SURROUND STRUCTURE FRAME 349.0 STGR 3LH AT PASSENGER CABIN WAS BLEND OUT PER SRM 51-12-00-001-001-A01 AND WAS REPAIRED
- [SDR VNAA20260202006](https://openairdocs.org/sdr/VNAA20260202006.md): Mount · corroded · Dec 4, 2025 · N525AE · Bombdr CL6002D15 · Service Doors
  > CORROSION ON MOUNTING ANGLE OF SERVICE DOOR SILL AT STGR 18R BETWEEN FS295.00 AND FS310.00. FOR EXCESSIVE DAMAGE ON MOUNTING ANGLE OF SERVICE DOOR SILL AT STGR 18R BETWEEN FS295.00 AND FS310.00 WAS REPLACED PER SRM 53-21-23-101-002-A01 AND PER SRM 51-42-06-
- [SDR VNAA20260202005](https://openairdocs.org/sdr/VNAA20260202005.md): Frame · corroded · Dec 4, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME FS364.00, STGR27, BEHIND THE PROXIMITY SWITCH BRACKET OF AVIONICS BAY DOOR. CORROSION ON FRAME FS364.00, STGR27, BEHIND THE PROXIMITY SWITCH BRACKET OF AVIONICS BAY DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01, WAS MEASURED AND FOUNT OUT O
- [SDR VNAA20260202004](https://openairdocs.org/sdr/VNAA20260202004.md): Seat Track · corroded · Dec 4, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACKS RBL 9 & LBL 9 BTW STA 485 - 677. THE SEAT TRACKS WERE EVALUATED IAW SRM 53-21-49-101-001-A01, AND SRM 53-31-49-101-001-A01, & REPLACED IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260202003](https://openairdocs.org/sdr/VNAA20260202003.md): Floorbeam · cracked · Dec 4, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CRACK ON FLOORBEAM, RBL 12, BS 220, BELOW WL79.50. THE FLOORBEAM WAS REPAIRED IAW REO 670-53-11-2238, REV-.
- [SDR VNAA20260202001](https://openairdocs.org/sdr/VNAA20260202001.md): Roller · worn · Dec 4, 2025 · N525AE · Bombdr CL6002D15 · Passenger/Crew Doors
  > WEAR ON CAM ROLLER FITTING OF PASSENGER DOOR SURROUND STRUCTURE FS 349.0, STGR 5LH AT PASSENGER CABIN. NEW CAM ROLLER FITTING OF PASSENGER DOOR SURROUND STRUCTURE FS 349.0, STGR 5LH AT PASSENGER CABIN WAS REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01
- [SDR VNAA20260205010](https://openairdocs.org/sdr/VNAA20260205010.md): Angle · cracked · Dec 3, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ATTACHEMENT ANGLE OF ACCESS PANEL 542AZ ON LH MLG SHOCK STRUT BAY. THE ANGLE OF ACCESS PANEL 542AZ ON LH MLG SHOCK STRUT BAY WAS REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 PAR. 6.C. AND SRM 51-23-00- 001-001-A01
- [SDR VNAA20260205009](https://openairdocs.org/sdr/VNAA20260205009.md): Skin · worn · Dec 2, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL SKIN BTW FS 977.00 TO FS 985.00 STGR 27 AT EXTERNAL FUSELAGE SKIN. REPAIRED PER REO 670-53-00-290 REV F EXTERNAL SKIN BTW FS 977.00 TO FS 985.00 STGR 27 AT EXTERNAL FUSELAGE SKIN
- [SDR VNAA20260205008](https://openairdocs.org/sdr/VNAA20260205008.md): Angle · cracked · Dec 2, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INNER ANGLE AT WS 25 APPROX AT RH MLG WW. INNER ANGLE AT WS 25 APPROX AT RH MLG WW. WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01
- [SDR VNAA20260205007](https://openairdocs.org/sdr/VNAA20260205007.md): Angle · cracked · Dec 2, 2025 · N525AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 642AZ ON RH MLG SHOCK STRUT BAY. ANGLE OF ACCESS PANEL 642AZ ON RH MLG SHOCK STRUT BAY WAS REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 AND SRM 51-23-00- 001-001-A01.
- [SDR VNAA20260205006](https://openairdocs.org/sdr/VNAA20260205006.md): Latch · gouged · Dec 2, 2025 · N525AE · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR & GOUGES ON FWD & AFT LATCH FITTINGS AT AFT BAGGAGE-BAY DOOR. FWD & AFT LATCH FITTINGS AT AFT BAGGAGE-BAY DOOR. WAS REPAIRED PER REO 670-52-31-184 REV -.
- [SDR VNAA20260205014](https://openairdocs.org/sdr/VNAA20260205014.md): Skin · dented · Dec 1, 2025 · N525AE · Bombdr CL6002D15 · Leading Edge Devices
  > DENTS ON SLAT NO. 1 APPROX STA SS84.00 AND NO. 2 APPROX STA SS213.00 AT RH WING. REPAIRED IAW REO 670-51-00-085 REV. -A, REO 670-57-42-2343 REV -, AND REO 670-57-42-2344 REV -.
- [SDR VNAA20260205013](https://openairdocs.org/sdr/VNAA20260205013.md): Cowl Door · dented · Nov 29, 2025 · N525AE · Bombdr CL6002D15 · Nacelle/Pylon, Main Frame
  > DENT ON LOWER FAN COWL DOOR APPOX 6 O'CLOCK POSITION AL LH ENGINE. DRESSED BACK IAW 670-54-14-1012 REV. B AND REO 670-54-14-1332 REV. - -
- [SDR VNAA20260205012](https://openairdocs.org/sdr/VNAA20260205012.md): Hinge Bracket · corroded · Nov 29, 2025 · N525AE · Bombdr CL6002D15 · Fuselage, Door Hinge
  > CORROSION ON BOTH HINGE UPR/LWR (2 EA), AS WELL ON HINGE BRACKET OUTBD (1 EA) OF THE AFT LAVATORY SERVICE DOOR 196ER. EVALUATED WITH EXCEEDED ALLOWABLE DAMAGE PER CRJ700 SRM 52-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-41-02-001-001-A01
- [SDR VNAA2024102211001](https://openairdocs.org/sdr/VNAA2024102211001.md): Manifold · unserviceable · Oct 19, 2024 · N525AE · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG AFTER TAKE OFF RAN QRH MSG PERSISTED DIVERTED TO IAD. / REMOVED AND REPLACED THE NOSEWHEEL STEERING MANIFOLD IAW CRJ700 AMM 32-51-50-000/400-801-A01. PERFORMED GVI OF STEERING MANIFOLD LINES AND CONNECTIONS FOR EXTERNAL LEAK, NO LEAK
- [SDR VNAA2023122911101](https://openairdocs.org/sdr/VNAA2023122911101.md): Duct · unknown · Dec 26, 2023 · N525AE · Cndair CL6002C10 · Ice/Rain Protection System
  > ANTI ICE DUCT WARNING IN FLIGHT / REMOVED AND REPLACED THE LH IB TELESCOPIC HARNESS ASSY PER CRJ 700 AMM 30-11-10-000/400-802. OPS CHECK GOOD. ALSO COMPLETED LEAK TEST OF THE WING ANTI-ICE DUCTS (IAW CRJ-700 AMM 30-11-00-790-801) NO LEAKS NOTED. ALSO REPLACED
- [SDR VNAA202305121111](https://openairdocs.org/sdr/VNAA202305121111.md): Unknown · unknown · May 11, 2023 · N525AE · Cndair CL6002C10 · Landing Gear Brake System
  > PLANE WONT MOVE WITH PARKING BRAKE OFF / OPS CHECKED PARKING BRAKE SHUT OFF VALVE IAW CRJ 700 AMM 32-45-13-710-801-A01. NO DEFECTS NOTED AT THIS TIME. BRAKE SYSTEM OPS CHECK GOOD IAW CRJ 700 AMM 32ˆ’43ˆ’00ˆ’710ˆ’801-A01. BLED L/H AND R/H INBOARD BRAKES IAW
- [SDR DALA202210200001](https://openairdocs.org/sdr/DALA202210200001.md): None · none · Oct 20, 2022 · N525AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > PAX DOOR FRAME CRACKED AT STA 280 STR3L LENTIL CLIP CORRECTIVE ACTION: REPAIRED PAX DOOR FRAME AT STA 280 STR 3L LENTIL CLIP IAW REO 670-53-21-493 REV D 2015-07-10 AND SB 6708A-53-40 REV C SEPT 20 2012
- [SDR DALA20221020001](https://openairdocs.org/sdr/DALA20221020001.md): Frame · cut · Oct 20, 2022 · N525AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > SPLICE REPAIR AT FS 319 AT STR 27 IN FWD AVIONICS BAY. CORRECTIVE ACTION: PERFORMED REPAIR TO FS 319 (P
- [SDR DALA20221020003](https://openairdocs.org/sdr/DALA20221020003.md): None · none · Oct 20, 2022 · N525AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > THE FOLLOWING SOR V0XD20220202001 WAS SUBMITTED WITH THE INCORRECT OPERATOR DESIGNATOR REGION CODE VNAA GO 1S AND SHOULD BE VNAA GL 05
- [SDR V0XD20220325001](https://openairdocs.org/sdr/V0XD20220325001.md): Frame · corroded · Mar 25, 2022 · N525AE · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME 319 BETWEEN STR 26L AND 26R HAS SIGNS OF CORROSION - CORRECTIVE ACTION: BLENDED OUT CORROSION PERFORMED NDT BLENDOUT WITHIN LIMITS IAW BOMBARDIER REO 670-53-21-1308 REV -- DATED 2016/09/06
- [SDR V0XD20220321011](https://openairdocs.org/sdr/V0XD20220321011.md): Floor Support · corroded · Mar 21, 2022 · N525AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR BEAM LBL 9 BETWEEN F.S. 1000 AND F.S. 1088.20 IS CORRODED. CORRECTIVE ACTION: REPAIRED THE FLOOR BEAM AT LBL9 BETWEEN F.S. 1000 AND F.S. 1088.20 IAW BOMBARDIER REO 670-53-61-2054 REV. -- DATED 2022-02-01.

Next page: https://openairdocs.org/aircraft/N525AE/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 = 'N525AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N525AE/reports

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