# Service difficulty reports: N514AE

A list on [N514AE](https://openairdocs.org/aircraft/N514AE.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 · 135 reports

- [SDR VNAA2026070820901](https://openairdocs.org/sdr/VNAA2026070820901.md): Windshield · failed · Jul 4, 2026 · N514AE · Cndair CL6002C10 · Flight Compartment Windows
  > FO WINDSHIELD SPARKED THEN SHATTERED. REMOVED AND REPLACED FO WINDSHIELD IAW AMM 56-11-01-000/400-801-A01-PSA. ALL OPS CHECKS GOOD AT THIS TIME.
- [SDR VNAA2026011311101](https://openairdocs.org/sdr/VNAA2026011311101.md): Warning Message · false activation · Jan 10, 2026 · N514AE · Cndair CL6002C10 · Elevator Control System
  > PITCH FEEL CAUTION MSG. / CYCLED SYSTEM CBS. MSG EXTINGUISHED. NO DEFECTS NOTED AT THIS TIME.
- [SDR VNAA2025111411101](https://openairdocs.org/sdr/VNAA2025111411101.md): Unknown · odor · Nov 13, 2025 · N514AE · Cndair CL6002C10 · Air Distribution System
  > VERY STRONG CHEMICAL BURNING LIKE SMELL INTERMITTENT IN FLIGHT DECK AND CABIN. NO VISIBLE SMOKE OR OTHER ABNORMAL INDICATIONS. STRONGEST DURING T/O AND 2 TIMES IN CRUISE FLT / T/S PER FIM 21-21-00-810-806-A01/ FIM 21-22-00-810-806-A01, PERFORMED CLEANING OF BO
- [SDR VNAA20250525026](https://openairdocs.org/sdr/VNAA20250525026.md): Retainer · corroded · Apr 24, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > AFTER REMOVAL SEAL IN REFERENCE TO NRC 00025, CORROSION ON RETAINER LOWER AND REATINER SEAL LOWER FWD WAS FOUND. DUE EXCCESIVE DAMAGE ON RETAINER LOWER AND RETAINER SEAL LOWER WERE REPLACED PER CRJ700 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01.
- [SDR VNAA20250525013](https://openairdocs.org/sdr/VNAA20250525013.md): Skin · dented · Apr 24, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > DENTS (2EAS) ON FUSELAGE SKIN LOCATED BTW FS280/ FS310 AND STGR23L / STGR25L. DENTS (2EAS) ON FUSELAGE SKIN LOCATED BTW FS280/ FS310 AND STGR23L / STGR25L WERE REPAIRED PER REO 670-53-21-2608 REV. -- AND REO 670-51-00-085 REV - A.
- [SDR VNA2025F00014](https://openairdocs.org/sdr/VNA2025F00014.md): Fitting · corroded · Apr 22, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTING PN: 9391251-3 (1EA) UNDER THE FLIGHT ATTENDANT SEAT AT ENTRANCE COMPARTMENT. NEW FITTING PN: 9391251-3 UNDER THE FLIGHT ATTENDANT SEAT AT ENTRANCE COMPARTMENT WAS REPLACED PER SAFRAN CMM 25-23-35
- [SDR VNAA20250525024](https://openairdocs.org/sdr/VNAA20250525024.md): Drain Pan · corroded · Apr 19, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON DRAIN PLATE OF FLOOR PANEL 232BRF. CORROSION ON DRAIN PLATE OF FLOOR PANEL 232BRF WAS EVALUATED BY EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ/900 AMM 53-00-47-000-802 (CONFIG A19) AND AMM 53-00-47-400-802 (CONFI
- [SDR VNAA20250525030](https://openairdocs.org/sdr/VNAA20250525030.md): Stringer Splice · corroded · Apr 14, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > AFTER SPLICE REMOVAL CORROSION ON SPLICE STGR 26 RH FS 333.00 WAS FOUND. SPLICE STGR 26 RH FS 333.00 WAS EVALUATED OUT OF LIMITS AND REPLACED PER CRJ700 SRM 53-00-00-101-001-A01 AND MUST BE INSTALLED UNDER NRC 00193.
- [SDR VNAA20250525029](https://openairdocs.org/sdr/VNAA20250525029.md): Angle · cracked · Apr 10, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE CAP RH/LH OF FS280 BULKHEAD. ANGLE CAP RH/LH OF FS280 BULKHEAD WERE REPLACED PER CRJ700 SRM 51-42-10-001-001-A01, ANGLE CAP LH WAS INSTALLED UNDER NRC 00194.
- [SDR VNAA20250525028](https://openairdocs.org/sdr/VNAA20250525028.md): Hinge Fitting · corroded · Apr 9, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Door Hinge
  > CORROSION HINGE FITTINGS BORE LH/RH (2E/A) OF NLG DOOR ON FUSELAGE WAS FOUND. EVALUATED, DUE TO EXCESSIVE DAMAGE ON HINGE FITTINGS BORE LH/RH (2E/A) OF NLG DOOR ON FUSELAGE WAS FOUND PER CRJ 700 SRM 53-00-01-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21
- [SDR VNAA20250525023](https://openairdocs.org/sdr/VNAA20250525023.md): Drain Pan · corroded · Apr 5, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON DRAIN PLATE AT FLOOR PANEL 232BRF. CORROSION ON DRAIN PLATE AT FLOOR PANEL 232BRF
- [SDR VNAA20250525022](https://openairdocs.org/sdr/VNAA20250525022.md): Floor Support · corroded · Apr 5, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE SUPPORTS (3EAS) BTW FS280 TO FS265 AND BTW LBL 12 TO RBL12 AT FLIGHT COMPARTMENT. FLOOR ANGLE SUPPORT (LH AND RH) WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01, MANUFACTURATED PER DWG NO. CC670-33199 AND REPLACED P
- [SDR VNAA20250524002](https://openairdocs.org/sdr/VNAA20250524002.md): Angle · corroded · Apr 5, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON SETTLEMENT AREA OF FAIRINGS 195AL, 195BB, 195DL, 196AR AND 196DR BTW FS 847.00 TO FS 977.00 AT AFT FUSELAGE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. ON SKIN SETTLEMENT AREA WAS EVALUATED WITHIN LIMITS PER CRJ-700 SRM 53-51-01-101-003-A01
- [SDR VNAA20250525011](https://openairdocs.org/sdr/VNAA20250525011.md): Housing · worn · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV -B
- [SDR VNAA20250525010](https://openairdocs.org/sdr/VNAA20250525010.md): Track · worn · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Cargo/Baggage Doors
  > WEAR AND BEND ON FWD/AFT DOOR TRACKS AT AFT BAGGAGE BAY DOOR. FWD DOOR TRACK AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-53-61-2502 REV --. AFT DOOR TRACK AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ700 SRM 53-61-58-201-002-A01.
- [SDR VNAA20250525009](https://openairdocs.org/sdr/VNAA20250525009.md): Stringer · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 26LH BTW FS310 TO FS349 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 26LH BTW FS310 TO FS349 AT MAIN AVIONICS COMPARTMENT. WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND
- [SDR VNAA20250525006](https://openairdocs.org/sdr/VNAA20250525006.md): Stringer · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICES OF STRG (25, 24)RH, FS 333 AT MAIN AVIONICS COMPARTMENT. SPLICES OF STRG (25, 24)RH, FS 333 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AN
- [SDR VNAA20250525005](https://openairdocs.org/sdr/VNAA20250525005.md): Stringer · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 27 BTW FS310 TO FS319 AND STGR 25LH BTW FS319 TO FS333 AT MAIN AVIONICS COMPARTMENT. STGR 27 BTW FS310 TO FS319 AND STGR 25LH BTW FS319 TO FS333 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 A
- [SDR VNAA20250525004](https://openairdocs.org/sdr/VNAA20250525004.md): Stringer · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 23RH BTW FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT. STGR 23RH BTW FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01.
- [SDR VNAA20250525003](https://openairdocs.org/sdr/VNAA20250525003.md): Fitting · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Equipment Attach Fittings
  > CORROSION ON FLOOR FITTING ACCESS 211 COUNTER AT GALLEY 2. FLOOR FITTING ACCESS 211 COUNTER AT GALLEY 2 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-32-78
- [SDR VNAA20250525020](https://openairdocs.org/sdr/VNAA20250525020.md): Seat Track · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL27 (2EA) BTW FS280 TO FS477 AT PAX CABIN. CORROSION ON SEAT RAIL LBL27 (2EA) BTW FS280 TO FS477 AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A01 AND WERE REPLACED PER AMM 53-00-49 (CONFIG A03).
- [SDR VNAA20250524014](https://openairdocs.org/sdr/VNAA20250524014.md): Stringer · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON STGR 19LH AND CONECTOR SUPPORT BTW FS 319 TO FS333 AT MAIN AVIONICS COMPARTMENT. STGR 19L BTW FS 319 TO FS333 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-
- [SDR VNAA20250524012](https://openairdocs.org/sdr/VNAA20250524012.md): Seat Track · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 LH SIDE. CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 LH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-31-49-101-001-A01 AND WERE REPLACED PER CRJ700 AMM 53-00-49 (CONFIG A03).
- [SDR VNAA20250524011](https://openairdocs.org/sdr/VNAA20250524011.md): Seat Track · corroded · Apr 4, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 RH SIDE. CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 RH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-41-49-101-001-A01 AND WERE REPLACED PER CRJ700 AMM 53-00-49 (CONFIG A03).
- [SDR VNAA20250525027](https://openairdocs.org/sdr/VNAA20250525027.md): Hinge Fitting · excess play · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Rudder Structure
  > AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL#2103 REV. B.
- [SDR VNAA20250525025](https://openairdocs.org/sdr/VNAA20250525025.md): Cap · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL MID CAP IN REFERENCE TO NRC 00214, CORROSION ON MID CAP AND FWD CAPANGLE WAS FOUND. CORROSION ON MID CAP AND FWD CAPANGLE WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 WERE REPLACED AND MUST BE INSTALLED UNDER NRC0214.
- [SDR VNAA20250525021](https://openairdocs.org/sdr/VNAA20250525021.md): Intercostal · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTALS (1 EAS) STGR 21LH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL AT STGR 21LH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ 70
- [SDR VNAA20250525019](https://openairdocs.org/sdr/VNAA20250525019.md): Diaphragm · worn · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON DIAPHRAGM LBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. DIAPHRAGM LBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV. -A.
- [SDR VNAA20250525017](https://openairdocs.org/sdr/VNAA20250525017.md): Skin · dented · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Nacelle/Pylon, Plate/Skin
  > SEVERAL DENTS ON LOWER FAN COWL BTW 5 O'CLOCK TO 8 O'CLOCK POSITION AT LEFT ENGINE. DENT ON LOWER FAN COWL BTW 5 O´CLOCK AT LH ENGINE WAS REPAIRED PER REO 670-54-14-1314 REV. --
- [SDR VNAA20250525008](https://openairdocs.org/sdr/VNAA20250525008.md): Fitting · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON 8 EA. FITTINGS BTW FS280 TO FS 310 FROM LBL38 TO RBL38. EXCESSIVE DAMAGE FOUND OUT OF LIMITS 8EA. BTW FS280 TO FS310 FROM LBL38 TO RBL38 REPLACED PER CRJ 700 SRM 51-42-21-001-AO1
- [SDR VNAA20250525007](https://openairdocs.org/sdr/VNAA20250525007.md): Diaphragm · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV. -A.
- [SDR VNAA20250525002](https://openairdocs.org/sdr/VNAA20250525002.md): Seat Track · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS 2 (EAS) AT LBL9 AND LBL 27 FROM FS 847 TO FS977. EVALUATED SEAT RAILS 2 (EAS) AT LBL9 AND LBL 27 FROM FS 847 TO FS977. DUE TO NOT ALLOWABLE DAMAGES PER CRJ-700 SRM 53-41-49-101-001-A01 AND REPLACED PER CRJ-700 AMM 53-00-49-400-801 (CO
- [SDR VNAA20250525001](https://openairdocs.org/sdr/VNAA20250525001.md): Seat Track · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: CORROSION ON SEAT RAILS 2 (EAS) AT RBL9 AND RBL 27 FROM FS 847 TO FS977. SEAT RAILS 2 (EAS) AT RBL9 AND RBL 27 FROM FS 847 TO FS977 WERE EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-41-49-101-001-A03 AND REPLACED PER CRJ 700 AMM 53-00-49-400-801
- [SDR VNAA20250524019](https://openairdocs.org/sdr/VNAA20250524019.md): Seat Track · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CENTER SEAT RAILS LBL9/RBL9 (6EAS) BTW STA 280 TO STA 708 AT PAX CABIN. SEAT RAILS LBL9/RBL9 (6EAS) BTW STA 280 TO STA 708 AT PAX CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A01 AND SRM 53-41-49
- [SDR VNAA202504018](https://openairdocs.org/sdr/VNAA202504018.md): Angle · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE KICKPLATE OF PASSENGER DOOR SURROUND STRUCTURE FROM FS 310 TO FS EN 349 AT PAX CABIN. ANGLE KICKPLATE OF PASSENGER DOOR SURROUND STRUCTURE AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER CRJ700 53-21-23-101-001-A01 AND WAS REPLACED PER CRJ70
- [SDR VNAA202504017](https://openairdocs.org/sdr/VNAA202504017.md): Frame · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Frame
  > CORROSION ON FRAME PLATE FS 319.70 AND WL 72 AT PAX CABIN. CORROSION ON FRAME PLATE FS 319.70 AND WL 72 AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER CRJ 700 SRM 53-21-23-101-002-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.
- [SDR VNAA202504016](https://openairdocs.org/sdr/VNAA202504016.md): Intercostal · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AND CLEATS (3 EAS) AT STGR 20R BTW FS319.70 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-002-A02 AND CORROSION ON CLEATS (3 EAS) AT STGR 20R BTW FS319.70
- [SDR VNAA20250524008](https://openairdocs.org/sdr/VNAA20250524008.md): Floorbeam · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > AFTER FLOOR SUPPORT ANGLE AT CROSSBEAM REMOVAL, CORROSION FOUND ON WEBS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9, PREVIOUS REPAIR ON WEBS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9 WERE REPLACED PER SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR VNAA20250524007](https://openairdocs.org/sdr/VNAA20250524007.md): Stringer · corroded · Apr 3, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRG 26R BTW FS 333 AND FS 349 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRG 26R BTW FS 333 AND FS 349 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-03-101-006-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-0
- [SDR VNAA20250524015](https://openairdocs.org/sdr/VNAA20250524015.md): Handle · corroded · Apr 2, 2025 · N514AE · Bombdr CL6002D15 · Service Doors
  > CORROSION ON R1 HANDLE GUARD. R1 HANDLE GUARD PN: 9329222BK1 ITEM [225] WAS VERIFIED AND REPLACED PER CRJ-700 AIPC 25-26-07.
- [SDR VNAA20250524013](https://openairdocs.org/sdr/VNAA20250524013.md): Seat Frame · corroded · Apr 2, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/A). VALUATED,LH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/AS). DUE TO NOT ALLOWABLE DAMAGES PER CRJ-700 SRM 53-41-49-101-001-A01 AND REPLACED PER AMM 53-00-49-400-801 (CONFIGA03).
- [SDR VNAA20250524010](https://openairdocs.org/sdr/VNAA20250524010.md): Bracket · corroded · Apr 2, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH/LH MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AT MLG WHEEL WELL AREAS, RBL40, RBL 45 AND LBL45, RBL40. CORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH/LH MLG HYDRAULIC LINES SUPPO
- [SDR VNAA20250524009](https://openairdocs.org/sdr/VNAA20250524009.md): Door Frame · corroded · Apr 2, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > CORROSION FOUND ON POSTS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9. POSTS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9 WERE REPAIRED PER CRJ 700 SRM 53-11-10-201-006-A01
- [SDR VNAA20250524006](https://openairdocs.org/sdr/VNAA20250524006.md): Stringer · corroded · Apr 2, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRG 21R BTW FS 364 AND FS 379 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRG 21R BTW FS 364 AND FS 379 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-03-101-006-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-0
- [SDR VNAA20250524001](https://openairdocs.org/sdr/VNAA20250524001.md): Seat Track · corroded · Apr 2, 2025 · N514AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/A). EVALUATED,RH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/A) ARE OUT OFF LIMITS PER CRJ-700 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A01 AND REPLACED PER CRJ-700 AMM 53-00-49.
- [SDR VNAA20250524005](https://openairdocs.org/sdr/VNAA20250524005.md): Fitting · damaged · Apr 1, 2025 · N514AE · Bombdr CL6002D15 · Nacelle/Pylon, Main Frame
  > TOOL MARK ON FITTING OF SPRING CONTRABALANCE AT LH NACELLE. FITTING OF SPRING CONTRABALANCE AT LH NACELLE WAS REPAIRED PER REO 670-54-20-003 REV --
- [SDR VNAA20250524004](https://openairdocs.org/sdr/VNAA20250524004.md): Floorbeam · corroded · Apr 1, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT ANGLE AT CROSSBEAM FS 280.00 BTW LBL 9 AND RBL 9. CORROSION ON FLOOR SUPPORT ANGLE AT CROSSBEAM FS 280.00 BTW LBL 9 AND RBL 9 WAS EVALUATED OUT OF LIMITS PER SRM 53-00-01-101-001-A01 AND WAS FABRICATED AND REPLACED PER DRAWING CC6
- [SDR VNAA20250524003](https://openairdocs.org/sdr/VNAA20250524003.md): Bracket · cracked · Mar 31, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > TEMP SIDE POSITION FOR CRACK DAMAGE TO PAX DOOR STOP BRACKET. STOP BRACKET TO PAX DOOR LH WAS REPLACED PER CRJ 700 SRM 51-42-21-00-AO1.
- [SDR VNAA20250525018](https://openairdocs.org/sdr/VNAA20250525018.md): Plate · worn · Mar 30, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Structure
  > WEAR ON EXTERNAL TRIPLER PROTECTOR PLATE BTW FS 893.00 TO FS 909.00, AT STGR 27. EXTERNAL PROTECTOR PLATE BTW FS 893.00 TO FS 909.00, AT STGR 27 WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01
- [SDR VNAA20250525016](https://openairdocs.org/sdr/VNAA20250525016.md): Skin · worn · Mar 29, 2025 · N514AE · Bombdr CL6002D15 · Trailing Edge Flaps
  > WEAR ON LWR SKIN OF LH OUTBD FLAP BTW FL168.63 TO WS 262. REPAIRED PER REO 670-57-53-409 REV--.

Next page: https://openairdocs.org/aircraft/N514AE/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 = 'N514AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N514AE/reports

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