# Service difficulty reports: N513AE

A list on [N513AE](https://openairdocs.org/aircraft/N513AE.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 · 179 reports

- [SDR VNAA2026062319302](https://openairdocs.org/sdr/VNAA2026062319302.md): Proximity Sensor · false indication · Jun 21, 2026 · N513AE · Cndair CL6002C10 · Landing Gear Position and Warning
  > UPON GEAR RETRACTION ON TO GEAR DISAGREE WARNING, MESSAGE & NOSE GEAR INDICATION WAS AMBER. ADJUST PX21/22 PROX SENSORS IAW AMM 32-61-05-820-804-A01PSA REV C. REMOVED AND REPLACED NLG DOOR RODS IAW AMM 32-22-07-000/400-801-A01 TO FOM. PERFORMED LANDING GEAR
- [SDR VNAA2026010911101](https://openairdocs.org/sdr/VNAA2026010911101.md): Light · odor · Jan 8, 2026 · N513AE · Cndair CL6002C10 · Flight Compartment Lighting
  > FO MAP LIGHT BURING SMELL. REMOVED & REPLACED FO MAP LIGHT IAW CRJ 700 AMM 33-13-03-000/400-801. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2025061711101](https://openairdocs.org/sdr/VNAA2025061711101.md): Selector Valve · faulted · Jun 14, 2025 · N513AE · Cndair CL6002C10 · Landing Gear Position and Warning
  > WHEN SELECTING LANDING GEAR DOWN ON APPROACH, WE GOT A GEAR DISAGREE MSG RAN QRH WHICH HAD US USE ALTERNATE GEAR SYSTEM / REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801. LEAK AND OPS CHECK GOOD.
- [SDR VNAA20250610024](https://openairdocs.org/sdr/VNAA20250610024.md): Support Plate · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00214242 DISCREPANCY: FOUND CORROSION ON LAV SERVICE LIGHT SUPPORT PLATE P/N SH670-37576-3. CORRECTIVE ACTION: REMOVED CORRODED SUPPORT PLATE. FABRICATED AND INSTALLED A NEW SUPPORT PLATE IAW DRAWING SH670-37576 AND CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-4
- [SDR VNAA20250610023](https://openairdocs.org/sdr/VNAA20250610023.md): Retainer · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > BARCODE 210648 DISCREPANCY: FWD BAGGAGE BAY DOOR FWD LOWER SEAL RETAINER IS GOUGED. CORRECTIVE: INSTALLED NEW SERVICEABLE SEAL RETAINER P/N LE670-39644-1 IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR VNAA20250610022](https://openairdocs.org/sdr/VNAA20250610022.md): Door Sill · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > HN00217039 S/N: 538 DISCREPANCY: AFT CARGO DOOR SILL IS CORRODED PN MM670-35655-003
- [SDR VNAA20250610021](https://openairdocs.org/sdr/VNAA20250610021.md): Plate · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00229884 S/N: 852 AFT CARGO DOOR STEP PLATE FWD HINGE PLATE FOUND TO BE CORRODED. CORRECTIVE ACTION: LOCATED, AND DRILLED NEW AFT CARGO DOOR STEP PLATE FWD HINGE PLATE P/N MM670-35622-003 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-40-11-001-001-A01. REFER TO
- [SDR VNAA20250610020](https://openairdocs.org/sdr/VNAA20250610020.md): Plate · damaged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Rudder Structure
  > HN00225374 S/N: 819 DISCREPANCY: FOUND FWD HOLE ON OUTBOARD SIDE OF THE R/H RUDDER FEEL UNIT PLATE TO BE ELONGATED. CORRECTIVE: REPAIRED ELONGATED HOLE IAW MHI RJ REO 670-53-11-2106 REV -A DATED 2025-03-20 PN
- [SDR VNAA20250610019](https://openairdocs.org/sdr/VNAA20250610019.md): Vane · dented · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00219660 S/N: 715 DISCREPANCY: RIGHT INBOARD FLAP VANE LEADING EDGE IS DENTED (MARKED WITH TAPE) CORRECTIVE: DRILLED UP NEW SERVICEABLE LEADING EDGE SKIN (PN CC670-14012-4) IAW CRJ700 SRM 51-40-11-001-001-A01, DRILLED UP NEW SERVICEABLE LEADING EDGE SKIN (PN
- [SDR VNAA20250610018](https://openairdocs.org/sdr/VNAA20250610018.md): Cradle · gouged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Trailing Edge Flaps
  > HN00218095 S/N: 634 DISCREPANCY: RH INBOARD FLAP VANE ACTUATOR AT W.S.102.90 CRADLE ASSY IS GOUGED. CORRECTIVE: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR ASSEMBLY FOR RH WS102.9 (PN CC670-14300-9-01, SN PR1943). LOCATED AND MACHINED 3EA HOLES ON NEW SERVICEA
- [SDR VNAA20250610017](https://openairdocs.org/sdr/VNAA20250610017.md): Cradle · gouged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Trailing Edge Flaps
  > HN00218094 S/N: 633 DISCREPANCY: RH INBOARD FLAP VANE ACTUATOR AT W.S.65.50 CRADLE ASSY IS GOUGED. CORRECTIVE: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR ASSEMBLY FOR RH WS65.5 (PN CC670-14300-9-01, SN PR1932). LOCATED AND MACHINED 3EA HOLES ON NEW SERVICEABL
- [SDR VNAA20250610016](https://openairdocs.org/sdr/VNAA20250610016.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216768 S/N: 513 DISCREPANCY: R/H SLAT TRACK 1-2 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED R/H SLAT TRACK 1-2 I/B AND O/B SIDES IAW MHIRJ REO 670-57-42-1984 REV-- DATED 2025-02-12
- [SDR VNAA20250610015](https://openairdocs.org/sdr/VNAA20250610015.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216753 S/N: 501 DISCREPANCY: R/H SLAT TRACK 2-1 IS CHAFED ON THE LOWER FACE. CORRECTIVE: REPAIRED RH 2-1 SLAT TRACK IAW MHIRJ REO 670-57-42-1993 REV-- DATED 2025-02-13
- [SDR VNAA20250610014](https://openairdocs.org/sdr/VNAA20250610014.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216748 S/N: 497 DISCREPANCY: R/H SLAT TRACK 3-3 IS CHAFED ON THE LOWER FACE. CORRECTIVE: REPAIRED RH SLAT TRACK 3-3 IAW MHIRJ REO 670-57-42-2005 REV -- DATED 2025-02-20 PN
- [SDR VNAA20250610013](https://openairdocs.org/sdr/VNAA20250610013.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216746 S/N: 496 DISCREPANCY: L/H SLAT TRACK 3-3 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 3-3 IAW MHIRJ REO 670-57-42-2004 REV-- DATED 2025-02-20. REF RFTS-119933 FOR TRACKING
- [SDR VNAA20250610012](https://openairdocs.org/sdr/VNAA20250610012.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216745 S/N: 495 DISCREPANCY: L/H SLAT TRACK 3-3 LOWER FACE IS CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 3-3 IAW MHIRJ REO 670-57-42-2004 REV-- DATED 2025-02-20. REF RFTS-119933 FOR TRACKING
- [SDR VNAA20250610011](https://openairdocs.org/sdr/VNAA20250610011.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216742 S/N: 492 DISCREPANCY: L/H SLAT TRACK 3-1 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 3-1 IAW MHIRJ REO 670-57-42-2002 REV-- DATED 2025-02-19. REF RFTS-119925 FOR TRACKING
- [SDR VNAA20250610010](https://openairdocs.org/sdr/VNAA20250610010.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216740 S/N: 491 DISCREPANCY: L/H SLAT TRACK 3-1 UPPER FACE IS CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 3-1 IAW MHIRJ REO 670-57-42-2002 REV-- DATED 2025-02-19. REF RFTS-119925 FOR TRACKING
- [SDR VNAA20250610009](https://openairdocs.org/sdr/VNAA20250610009.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216739 S/N: 490 DISCREPANCY: L/H SLAT TRACK 3-1 LOWER FACE IS CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 3-1 IAW MHIRJ REO 670-57-42-2002 REV-- DATED 2025-02-19. REF RFTS-119925 FOR TRACKING
- [SDR VNAA20250610008](https://openairdocs.org/sdr/VNAA20250610008.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216738 S/N: 489 DISCREPANCY:L/H SLAT TRACK 2-1 LOWER FACE IS CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 2-1 IAW MHIRJ REO 670-57-42-1992 REV-- DATED 2025-02-13. REF RFTS-119784 FOR TRACKING. PN
- [SDR VNAA20250610007](https://openairdocs.org/sdr/VNAA20250610007.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216736 S/N: 488 DISCREPANCY: L/H SLAT TRACK 2-1 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 2-1 IAW MHIRJ REO 670-57-42-1992 REV-- DATED 2025-02-13. REF RFTS-119784 FOR TRACKING
- [SDR VNAA20250610006](https://openairdocs.org/sdr/VNAA20250610006.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216726 S/N: 487 DISCREPANCY: L/H SLAT TRACK 2-3 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 2-3 IAW MHIRJ REO 670-57-42-2001 REV-- DATED 2025-02-17. REF RFTS-119791 FOR TRACKING
- [SDR VNAA20250610005](https://openairdocs.org/sdr/VNAA20250610005.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > BARCODE HN00216720 S/N: 484 DISCREPANCY: L/H SLAT TRACK 1-3 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-1985 REV-- DATED 2025-02-12 REFERENCED PSA RII REFERENCE GUIDE REV 00 DATED 29,NOV,24
- [SDR VNAA20250610004](https://openairdocs.org/sdr/VNAA20250610004.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00216719 S/N: 483 DISCREPANCY: L/H SLAT TRACK 1-3 LOWER FACE IS CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-1985 REV-- DATED 2025-02-12 REFERENCED PSA RII REFERENCE GUIDE REV 00 DATED 29,NOV,24
- [SDR VNAA20250610003](https://openairdocs.org/sdr/VNAA20250610003.md): Seal Rest · dented · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > HN00236686 S/N: 899 THE AFT CARGO DOOR SEAL LOWER RETAINER HAS DENT AT OUTBOARD SIDE OF AFT LOWER STOP FITTING. LOWER RETAINER FOUND BADLY DAMAGED AND CORROSION AROUND AND ON 1 OF RIVET AND LOWER SEAL RETAINER REQ REPLACEMENT. CORRECTIVE ACTION: REMOVED AND RE
- [SDR VNAA20250610002](https://openairdocs.org/sdr/VNAA20250610002.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > L/H SLAT TRACK 1-1 I/B AND O/B SIDES ARE CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 1-1 IAW MHIRJ REO 670-57-42-1978 REV-- DATED 2025-02-11 REFERENCED PSA RII REFERENCE GUIDE REV 00 DATED 29,NOV,24 HN00216717 S/N: 481
- [SDR VNAA20250610001](https://openairdocs.org/sdr/VNAA20250610001.md): Slat Track · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > L/H SLAT TRACK 1-1 LOWER FACE IS CHAFED. CORRECTIVE: REPAIRED LH SLAT TRACK 1-1 IAW MHIRJ REO 670-57-42-1978 REV-- DATED 2025-02-11 HN00216716 S/N: 480
- [SDR VNAA20250610078](https://openairdocs.org/sdr/VNAA20250610078.md): Skin · chafed · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > DURING ELECTRICAL RETRACTION OF THE SLATS, FOUND THAT MIDDLE OF SLAT 3 BOTTOM HAS EVIDENCE OF CHAFFING. COMPLIED WITH PSA EA 57-2025-0684 REV-- DATED 2025-05-19. COMPLIED WITH MHIRJ REO 670-57-42-2071, REV--, DATE: 2025-05-08. INSTALLED NEW SERVICEABLE RH FI
- [SDR VNAA20250610077](https://openairdocs.org/sdr/VNAA20250610077.md): Spar · gouged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Wing Spar
  > WHILE PERFORMING NDTM PART 6 53-41-116-250-A01 FOUND LEFT OUTBOARD FORWARD BOLT HOLE ON REAR SPAR LATERAL BEAM AND LEFT SIDE STAY FITTING TO HAVE DEEP GOUGES IN INNER BORE. PERFORMED REPAIR FOR GOUGE DAMAGE TO OUTBOARD FWD HOLE BORE OF LHS SIDE STAY BRACKET
- [SDR VNAA20250610076](https://openairdocs.org/sdr/VNAA20250610076.md): Frame · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND FRAME AT F/S 1051 TO BE CORRODED AT STR 27. REPAIRED CORROSION FOUND ON F/S 1051 AT STR 27 IAW REO 670-53-61-2476 REV: -- DATED: 2025-03-07 PN MM670-36152
- [SDR VNAA20250610075](https://openairdocs.org/sdr/VNAA20250610075.md): Floor Support · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT MULTIPLE LOCATIONS ON TOP OF FLOOR SUPPORT BEAM LBL27 FROM FS985 TO FS1047. REPAIRED FLOOR BEAM LBL27 FROM F.S.985 TO F.S.1047 IAW CRJ 700 SRM 53-00-41-201-001-A01. PN MM670-35302-005
- [SDR VNAA20250610074](https://openairdocs.org/sdr/VNAA20250610074.md): Floor Support · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT MULTIPLE LOCATIONS ON TOP OF FLOOR SUPPORT BEAM LBL27 FROM FS985 TO FS1047. REPAIRED FLOOR BEAM LBL27 FROM F.S.985 TO F.S.1047 IAW CRJ 700 SRM 53-00-41-201-001-A01. PN MM670-35302-005
- [SDR VNAA20250610073](https://openairdocs.org/sdr/VNAA20250610073.md): Fitting · gouged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT MLG SIDE STAY FITTING O/B LUG IS GOUGED AND CORRODED. PN CC670-10608-8.
- [SDR VNAA20250610072](https://openairdocs.org/sdr/VNAA20250610072.md): Slat Track · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 IS CHAFED ON THE LOWER FACE. REPAIRED IAW MHIRJ REO 670-57-42-2007 REV-- DATED 2025-02-25. REFERENCED PSA RII GUIDE REV 00 DATED 29,NOV,24 PN CC670-12081-7
- [SDR VNAA20250610071](https://openairdocs.org/sdr/VNAA20250610071.md): Seat Track · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BETWEEN FS 677 AND FS 708 IS GOUGED AND CORRODED IN MULTIPLE AREAS. REMOVED & REPLACED LH SEAT RAIL FS677-FS708 (P/N SH670-36255-3) IAW CRJ-700 AMM 53-00-49-400-801-A03, 53-00-49-000-801-A03
- [SDR VNAA20250610070](https://openairdocs.org/sdr/VNAA20250610070.md): Floor Support · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DISCREPANCY:FOUND AFT SUPPORT STRUCTURE UNDER PANEL 195DR AND 195DL TO HAVE CORROSION AROUND NUTPLATES. MARKED WITH ORANGE TAPE. REMOVED CORRODED ANGLE P/N SH670-39189-1 AND REPLACED WITH NEW IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR VNAA20250610069](https://openairdocs.org/sdr/VNAA20250610069.md): Floor Support · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND A POSSIBLE CORROSION ON AFT CARGO LBL 9 FLOOR BEAM BETWEEN FS 1000 TO FS 1051. REPAIRED AFT CARGO FLOOR BEAM AT LBL9 BETWEEN FS985 TO FS1060 IAW CRJ-700 SRM 53-00-41-201-001-A01. PN N126-1731
- [SDR VNAA20250610068](https://openairdocs.org/sdr/VNAA20250610068.md): Door Sill · damaged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > HN00221315 DISCREPANCY:UPON REMOVAL OF THE SERVICE DOOR SILL ANGLE, FOUND ADDITIONAL CORROSION ON THE SERVICE DOOR SILL. CORRECTIVE ACTION:UPON FURTHER EVLUATION, FOUND SERVICE DOOR SILL TO BE OUT OF LIMITS DUE TO CORROSION BEING ON MORE THAN 50% OF THE PART
- [SDR VNAA20250610067](https://openairdocs.org/sdr/VNAA20250610067.md): Pressure Deck · damaged · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > WHILE PERFORMING T.O. 53-079-001-23 FOUND 1EA ELONGATED HOLE ON THE FLOOR PRESSURE SILL DECK AT F.S 797.00 ON THE R/H SIDE. COMPLIED WITH REO 670-53-41-717 REV -- DATED 2025-04-02. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF RETURN TO SERVICE DATE FOR THE SHEE
- [SDR VNAA20250610066](https://openairdocs.org/sdr/VNAA20250610066.md): Fitting · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > GALLEY 1 FWD FLOOR FITTINGS FS 285.00 L/H AND R/H ARE CORRODED ON UPPER SURFACE. REMOVED BOTH R/H AND L/H FLOOR (P/N- SH670-32149-3) IAW CRJ 700 SRM1-42-21-001-001-A01. INSTALLED BOTH NEW SERVICEABLE FLOOR FITTINGS (P/N-SH670-32149-3) IAW CRJ 700 SRM 51-42-2
- [SDR VNAA20250610065](https://openairdocs.org/sdr/VNAA20250610065.md): Drag Angle · cracked · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Vertical Stabilizer
  > RIGHT VERTICAL STAB AFT DRAG ANGLE APPEARS CRACKED. NOTE: DUE TO HEAVY PAINT IN AREA STRIP AND VERIFY WITH NDT. CRACKED DRAG ANGLE P/N AV670-21186-004 REMOVED IAW CRJ700 SRM TASK 51-42-21-001-001-A01, TASK 51-42-22-001-001-A01, TASK 51-42-13-001-001-A01. NEW
- [SDR VNAA20250610064](https://openairdocs.org/sdr/VNAA20250610064.md): Drag Angle · cracked · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Vertical Stabilizer
  > LEFT VERTICAL STAB FWD DRAG ANGLE PREVIOUS REPAIR APPEARS CRACKED. NOTE: DUE TO HEAVY PAINT IN AREA STRIP AND VERIFY WITH NDT. REMOVED DAMAGED PREVIOUS REPAIR IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. FABRICATED AND INSTALLED NEW DRAG ANG
- [SDR VNAA20250610063](https://openairdocs.org/sdr/VNAA20250610063.md): Seal Rest · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > HN00218168 DISCREPANCY: SERVICE DOOR SEAL RETAINER CORRODED AROUND SCREW HOLES FOR GALLEY PROTECTOR PLATE CORRECTIVE: REMOVED AND REPLACED SERVICE DOOR LOWER SEAL RETAINER FORWARD AND AFT SPLICE PLATES P/N SH670-31423-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR VNAA20250610062](https://openairdocs.org/sdr/VNAA20250610062.md): Door Sill · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > SERVICE DOOR SILL ANGLE CORRODED IN MULTIPLE AREAS. REMOVED SERVICE DOOR SILL ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED SERVICEABLE SERVICE DOOR LOWER SILL ANGLE P/N SH670-31986-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND
- [SDR VNAA20250610061](https://openairdocs.org/sdr/VNAA20250610061.md): Bracket · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT COCKPIT FLOOR POST FS 280.00 LBL 9.0 WL 72.0 ATTACH ANGLE IS CORRODED. REPLACED BRACKET [P/N CC670-34191-1] AND GUSSET [P/N CC670-33467-1] IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. PAINTED RIVET HEADS AND TAILS IAW CRJ 700 SRM 51
- [SDR VNAA20250610060](https://openairdocs.org/sdr/VNAA20250610060.md): Post · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT COCKPIT FLOOR POST FS 280.00 LBL 9.0 WL 72.0 ATTACH ANGLE IS CORRODED. REPLACED BRACKET [P/N CC670-34191-1] AND GUSSET [P/N CC670-33467-1] IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. PAINTED RIVET HEADS AND TAILS IAW CRJ 700 SRM 51
- [SDR VNAA20250610059](https://openairdocs.org/sdr/VNAA20250610059.md): Floor Support · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP OF FLOOR SUPORT RBL9 FROM FS985 TO FS1000. COMPLETED FLOOR SUPPORT REPAIR AT RBL9 FROM FS985 TO FS1000 IAW CRJ-700-SRM-53-00-41-201-001-A01.
- [SDR VNAA20250610058](https://openairdocs.org/sdr/VNAA20250610058.md): Pin · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO DOOR OUTER HANDLE TAPPER PINS ARE CORRODED REQUIRE REPLACEMENT. INSTALLED 2EA NEW SERVICEABLE FWD CARGO DOOR OUTER HANDLE TAPER PINS PN AN386-1-9A IAW CRJ 700 LATECOERE CMM 52-35-00 AND CRJ 700 SRM 51-43-00-001-001-A01 PN AN386-1-9A.
- [SDR VNAA20250610057](https://openairdocs.org/sdr/VNAA20250610057.md): Seat Track · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT RAIL MOUNTING STRUCTURE IS CORRODED FROM FS752-761. REPLACED RH SEAT RAIL MOUNTING STRUCTURE FROM FS752-761 (P/N SH670-37557-3) IAW CRJ-700 SRM 51-23-00-001-001-A01.
- [SDR VNAA20250610056](https://openairdocs.org/sdr/VNAA20250610056.md): Seat Track · corroded · Jun 10, 2025 · N513AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT RAIL MOUNTING STRUCTURE IS CORRODED FROM FS785-797. REPAIRED LH SEAT RAIL MOUNTING STRUCTURE FROM FS785-797 IAW PSA EA 53-2025-0330 REV-- DATED 3-13-25.

Next page: https://openairdocs.org/aircraft/N513AE/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 = 'N513AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N513AE/reports

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