# Service difficulty reports: N502AE

A list on [N502AE](https://openairdocs.org/aircraft/N502AE.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 · 193 reports

- [SDR VNAA2026062219101](https://openairdocs.org/sdr/VNAA2026062219101.md): Pump · unserviceable · Jun 2, 2026 · N502AE · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), Main
  > HYD SYS 2 AT 0% DURING FLIGHT / PERFORMED INSPECTION OF THE ENGINE DRIVEN PUMP (EDP) AFTER OPERATION WITHOUT HYDRAULIC FLUID IAW AMM 05-51-33-210-801-A01 AND FOUND LEAK ON ENGINE DRIVEN PUMP, EDP, CASING. REMOVED AND REPLACED RT ENG ENGINE DRIVEN PUMP,EDP, IAW
- [SDR VNAA2025062411101](https://openairdocs.org/sdr/VNAA2025062411101.md): Warning Message · false activation · Jun 22, 2025 · N502AE · Cndair CL6002C10 · Central Warning
  > OB SPOILERONS AND OB FLIGHT SPLRS CAUTION IN FLIGHT / INTERROGATED MDC FOUND B1 CODE 007915 TROUBLESHOT IAW CRJ700 FIM 27-64-01-810-807-A01-PSA. PERFORMED SPOST FAULT EXTINGUISHED.
- [SDR VNAA2025050800071](https://openairdocs.org/sdr/VNAA2025050800071.md): Actuator · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN00203692 DISCREPANCY: FOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON L/H FLAP VANE ACTUATOR CRADLE ASSEMBLY (P# CC670-14301-9) @ F.L.S.140.4. CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE L/H FLAP VANE CRADLE ASSEMBLY P/N CC670-14301-9 FOR F.L
- [SDR VNAA2025050800070](https://openairdocs.org/sdr/VNAA2025050800070.md): Actuator · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN00203691 DISCREPANCY: FOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON L/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261-1) @ F.L.S.140.4 CORRECTIVE ACTION: REFF. MWC HN00203957 FOR FABRICATION OF L/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R
- [SDR VNAA2025050800069](https://openairdocs.org/sdr/VNAA2025050800069.md): Actuator · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN00203689 DISCREPANCY: FOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON R/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261-1) @ F.L.S.140.4 CORRECTIVE ACTION: REFF. MWC HN00203955 FOR FABRICATION R/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R142
- [SDR VNAA2025050800068](https://openairdocs.org/sdr/VNAA2025050800068.md): Actuator · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN00203426 DISCREPANCY: FOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON R/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261-1) @ F.L.S. 24. CORRECTIVE ACTION: REFF.MWC HN00203955 FOR FABRICATION R/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261
- [SDR VNAA2025050800066](https://openairdocs.org/sdr/VNAA2025050800066.md): Actuator · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > FOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON R/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261-1) @ F.L.S. 102.9. REF. MWC HN00203955 FOR FABRICATION OF R/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261-1) @ F.L.S. 102.9.
- [SDR VNAA2025050800065](https://openairdocs.org/sdr/VNAA2025050800065.md): Actuator · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN00203422 DISCREPANCY: FOUND CORROSION AROUND FASTENER HOLES (MARKED WITH RED TAPE) ON L/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R14261-1) @ F.L.S. 24. CORRECTIVE ACTION: REFF. MWC HN00203957 FOR FABRICATION L/H FLAP VANE ACTUATOR TRUNNION BODY (P# 601R1426
- [SDR VNAA2025050800064](https://openairdocs.org/sdr/VNAA2025050800064.md): Beam · gouged · May 8, 2025 · N502AE · Cndair CL6002C10 · Engine Thrust Reverser
  > HN00199387 DISCREPANCY: LH LOWER THRUST REVERSER HINGE BEAM HAS TWO GOUGES. CORRECTIVE ACTION: REPAIRED HINGE BEAM IAW MHIRJ REO 670-54-22-093 REV-- DATED 2024-11-15.
- [SDR VNAA2025050800063](https://openairdocs.org/sdr/VNAA2025050800063.md): Beam · damaged · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H UPPER C-DUCT INBD HINGE BEAM SLIDER BARREL ATTACH HOLES FOR NYLON SLIDER ARE ELONGATED. COMPLIED WITH MHIRJ REO 670-54-22-094 REV-- DATED 2024-11-16 ON L/H UPPER C-DUCT INBD HINGE BEAM; P/N: CN622-0101-009, S/N: SB/0063. NOTIFIED CUSTOMER BY EMAIL OF SDI
- [SDR VNAA2025050800062](https://openairdocs.org/sdr/VNAA2025050800062.md): Trunnion · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Landing Gear Attach Fittings
  > R/H MLG TRUNNION HAS CORROSION IN THE AFT BORE. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-21-1004-A, DATED 3/26/2025. REFERENCE HN00198761 FOR WORK PERFORMED.
- [SDR VNAA2025050800061](https://openairdocs.org/sdr/VNAA2025050800061.md): Bracket · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > CORROSION FOUND ON THE AFT/BOTTOM CORNER OF THE AFT CARGO DOOR STRUCTURE, ON BRACKET THAT ATTACHED TO F.S. 1047.00. REMOVED AND REPLACED BRACKET I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A01, 51-25-00-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001
- [SDR VNAA2025050800060](https://openairdocs.org/sdr/VNAA2025050800060.md): Door Sill · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON LOWER SILL OF THE AFT BAGGAGE BAY DOOR SURROUND. REMOVED AND REPLACED LOWER SILL IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-15-001-001-A01, 51-42-13-001-001-A01, 51-42-06-001-001-A01.
- [SDR VNAA2025050800059](https://openairdocs.org/sdr/VNAA2025050800059.md): Gusset · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY DOOR SURROUND LOWER GUSSET (JOINT PLATE) AT F.S. 533.00 IS CORRODED. REMOVED CORRODED GUSSET, LOCATED FASTENER HOLES AND INSTALLED NEW SERVICEABLE GUSSET (PN SH670-33793-4) IAW CRJ700 SRM 51-42-14-001-001-A01, 51-42-21-001-001-A01, & 51-40-11
- [SDR VNAA2025050800058](https://openairdocs.org/sdr/VNAA2025050800058.md): Stringer · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > HN00196884 DISCREPANCY: STRINGER 25L IS CORRODED BETWEEN FS 310.00 AND 333.00. CORRECTIVE ACTION: REMOVED DAMAGED STRINGER 25L FROM FS280-FS333 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 25L PN: SH670-3121
- [SDR VNAA2025050800057](https://openairdocs.org/sdr/VNAA2025050800057.md): Slat Track · damaged · May 8, 2025 · N502AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00196009 DISCREPANCY: FOUND L/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR OF LH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1806 REV-- DATED 2024-10-28.
- [SDR VNAA2025050800056](https://openairdocs.org/sdr/VNAA2025050800056.md): Slat Track · damaged · May 8, 2025 · N502AE · Cndair CL6002C10 · Leading Edge Devices
  > HN00196008 DISCREPANCY: FOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE AREAS. CORRECTIVE ACTION: PERFORMED MAJOR REPAIR OF RH SLAT TRACK 3-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1807 REV-- DATED 2024-10-28.
- [SDR VNAA2025050800055](https://openairdocs.org/sdr/VNAA2025050800055.md): Strap · gouged · May 8, 2025 · N502AE · Cndair CL6002C10 · Service Doors
  > HN00195779 DISCREPANCY: GOUGE FOUND ON PAX DOOR SURROUND STRUCTURE STRAP AT FS 349.00 AND STGR 4L. CORRECTIVE ACTION: REMOVED AND REPLACED INNER UPPER FRAME STRAP IAW CRJ-700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR VNAA2025050800054](https://openairdocs.org/sdr/VNAA2025050800054.md): Bracket · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fluid Service Doors
  > HN00195772 DISCREPANCY: BRACKET IN LOWER CHANNEL OF FWD WASTEWATER DOOR IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED PART IAW CRJ 700 SRM 51-42-06-001-001-A01, REPLACED WITH NEW SERVICEABLE PART- PN (SH670-32310-1) IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-
- [SDR VNAA2025050800053](https://openairdocs.org/sdr/VNAA2025050800053.md): Bearing · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Landing Gear Attach Fittings
  > HN00195738 DISCREPANCY: THE STRUCTURE AT THE R/H MLG AFT TRUNNION BEARING HAS PITTING CORROSION. CORRECTIVE ACTION: GRIDDED, BLENDED AND REMOVED CORROSION IAW CRJ700 SRM 57-21-12-101-001-A01 & 51-21-06-001-001-A01. PERFORMED REPAIR IN COMPLIANCE WITH REO 670-5
- [SDR VNAA2025050800052](https://openairdocs.org/sdr/VNAA2025050800052.md): Floor Support · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00195725 DISCREPANCY: RBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069.75. CORRECTIVE ACTION: REMOVED CORRODED SECTION OF FLOORBEAM. FABRICATED REPAIR PARTS AND INSTALLED THEM IAW CRJ 700 SRM 53-00-41-201-001-A01.
- [SDR VNAA2025050800051](https://openairdocs.org/sdr/VNAA2025050800051.md): Floor Support · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00195724 DISCREPANCY: LBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1015 AND FS 1069.75. CORRECTIVE ACTION: REPAIRED FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01.
- [SDR VNAA2025050800050](https://openairdocs.org/sdr/VNAA2025050800050.md): Floor Support · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00195723 DISCREPANCY: L.B.L. 27.00 FLOOR BEAM IS CORRODED BETWEEN F.S. 1000.00 AND F.S. 1051.00. CORRECTIVE ACTION: REPAIRED DAMAGE I.A.W. CRJ 700 SRM 53-00-41-201-001-A01.
- [SDR VNAA2025050800049](https://openairdocs.org/sdr/VNAA2025050800049.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195699 DISCREPANCY:.LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 840 AND FS 863. CORRECTIVE ACTION: REMOVED LH SIDE SEAT RAIL BETWEEN FS 840 AND FS 863 IAW CRJ 700 AMM 53-00-49-000-801-A01. FABRICATED SIDE SEAT RAIL PART SH670-36260-3 FROM 20276-2
- [SDR VNAA2025050800048](https://openairdocs.org/sdr/VNAA2025050800048.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195698 DISCREPANCY: LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 840 AND FS 863. CORRECTIVE ACTION: FABRICATED, LOCATED, AND DRILLED NEW SERVICEABLE LH SIDE SEAT RAIL (P/N: SH670-36260-3) AT STGR15L BETWEEN FS785 - FS840 IAW CRJ700 SRM 53-00-49-201
- [SDR VNAA2025050800047](https://openairdocs.org/sdr/VNAA2025050800047.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195697 DISCREPANCY: LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 708 AND FS 761. CORRECTIVE ACTION: REMOVED DAMAGED SIDE SEAT RAIL IAW CRJ 700 AMM 53-00-49-000-801 (CONFIG A01). INSTALLED NEW SERVICEABLE SIDE SEAT RAIL PN (SH670-37509-1), IAW CRJ 7
- [SDR VNAA2025050800046](https://openairdocs.org/sdr/VNAA2025050800046.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195695 DISCREPANCY: LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 677 AND FS 708. CORRECTIVE ACTION: INSTALLED SIDE SEAT RAIL BETWEEN FS677 TO FS708 LEFT HAND IAW CRJ 700 AMM 53-00-49-400-801-A01.
- [SDR VNAA2025050800045](https://openairdocs.org/sdr/VNAA2025050800045.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195694 DISCREPANCY: LH SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 570 AND FS 645. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01.
- [SDR VNAA2025050800043](https://openairdocs.org/sdr/VNAA2025050800043.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195688 DISCREPANCY: L/H SIDE SEAT RAIL AT STRINGER 15L IS CORRODED BETWEEN F.S. 379.00 AND F.S. 453.00. CORRECTIVE ACTION: FABRICATED LH SIDE SEAT RAIL AT STGR 15L BETWEEN FS 379 AND FS 453 IAW CRJ700 SRM 53-00-49-201-002-A01. INSTALLED NEW SERVICEABLE SID
- [SDR VNAA2025050800042](https://openairdocs.org/sdr/VNAA2025050800042.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195687 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 915 AND FS 969. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01 AND SRM 53-00-49-201-002-A01.ZX
- [SDR VNAA2025050800041](https://openairdocs.org/sdr/VNAA2025050800041.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195685 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 863 AND FS 915. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01 AND SRM 53-00-49-201-002-A01.
- [SDR VNAA2025050800040](https://openairdocs.org/sdr/VNAA2025050800040.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195684 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 840 AND FS 863. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01 AND SRM 53-00-49-201-002-A01.
- [SDR VNAA2025050800039](https://openairdocs.org/sdr/VNAA2025050800039.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195683 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 785 AND FS 840. CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE SEAT RAIL IAW CRJ700 SRM 51-40-11-001-001-A01, USED ALTERNATE MATERIAL IAW CRJ700 SRM 53-00-49-201-002-A01. INST
- [SDR VNAA2025050800038](https://openairdocs.org/sdr/VNAA2025050800038.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195680 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 715 AND FS 761. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49-400-801 (CONFIG A01).
- [SDR VNAA2025050800037](https://openairdocs.org/sdr/VNAA2025050800037.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195679 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 677 AND FS 715. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01 AND SRM 53-00-49-201-002-A01.
- [SDR VNAA2025050800036](https://openairdocs.org/sdr/VNAA2025050800036.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 570 AND FS 661. CORRECTIVE ACTION: REPLACED RH SIDE SEAT RAIL PN: SH670-33558-3 AT STGR 15R BETWEEN FS 570 AND FS 661 IAW CRJ 700 AMM 53-00-49-000/400-801-A01
- [SDR VNAA2025050800035](https://openairdocs.org/sdr/VNAA2025050800035.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00195677 DISCREPANCY: RH SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 489 AND FS 570. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01.
- [SDR VNAA2025050800034](https://openairdocs.org/sdr/VNAA2025050800034.md): Skin · cracked · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > HN00195027 DISCREPANCY: AFT FUSELAGE SKIN DOUBLER AT LAV SERVICING LOCATION IS CHAFED AND MULTIPLE FASTENERS ARE CHAFED. CORRECTIVE ACTION: REMOVED AND REPLACED DOUBLER IAW CRJ-700 SRM 51-42-06-001-001-A01.
- [SDR VNAA2025050800033](https://openairdocs.org/sdr/VNAA2025050800033.md): Latch · cracked · May 8, 2025 · N502AE · Cndair CL6002C10 · Passenger/Crew Doors
  > HN00195019 DISCREPANCY: PAX DOOR, AFT LATCH / CAM BACK-UP FITTING IS CRACKED. CORRECTIVE ACTION: FABRICATED 1EA PAX DOOR UPPER FRAME FITTING AS REQUIRED USING 7050-T7451 PO# 5-12717 IAW STEPS 1 AND 2.A-2.C OF MHIRJ SNIEO 601R318042 IDENTIFIER S02 AND INSTALLED
- [SDR VNAA2025050800032](https://openairdocs.org/sdr/VNAA2025050800032.md): Latch · chafed · May 8, 2025 · N502AE · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > HN00194545 DISCREPANCY: LH UPPER TRANSCOWL HAS CHAFING UNDER LATCH PANEL. CORRECTIVE ACTION: UPON FURTHER EVALUATION, FOUND DAMAGE TO BE LOCATED ON L/H UPPER TRANSCOWL LATCH DOOR COAMING P/N CN624-2060-205. EVALUATED CHAFE DAMAGE ON THE L/H UPPER TRANSCOWL LAT
- [SDR VNAA2025050800031](https://openairdocs.org/sdr/VNAA2025050800031.md): Skin · gouged · May 8, 2025 · N502AE · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > HN00194156 DISCREPANCY: LH PYLON SYSTEM PANEL LANDING HAS GOUGE DAMAGE. CORRECTIVE ACTION: REPAIRED IAW MHIRJ REO 670-53-61-2398 REV-- DATED 10-26-2024
- [SDR VNAA2025050800030](https://openairdocs.org/sdr/VNAA2025050800030.md): Bracket · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > HN00193853 DISCREPANCY: L/H MLG WHEEL WELL HYDRAULIC BRACKET JUST INBOARD OF F.S. 797.00 WING ATTACH FITTING IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET I.A.W. CRJ700 SRM 51-41-02-001-001-A01.
- [SDR VNAA2025050800029](https://openairdocs.org/sdr/VNAA2025050800029.md): Bracket · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > HN00193853 DISCREPANCY: R/H MLG WHEEL WELL HYDRAULIC BRACKET JUST INBOARD OF F.S. 797.00 WING ATTACH FITTING IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET I.A.W. CRJ700 SRM 51-41-02-001-001-A01.
- [SDR VNAA2025050800028](https://openairdocs.org/sdr/VNAA2025050800028.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00218262 DISCREPANCY: FOUND CORROSION ON LBL 9 SEAT TRACK AT FS 985 AND FS 1005. CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK PN# SH670-37412-951 BETWEEN FS985- FS1005 IAW MHIRJ REO 670-53-00-773 REV-- DATED 2025-02-02
- [SDR VNAA2025050800027](https://openairdocs.org/sdr/VNAA2025050800027.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00218261 DISCREPANCY: FOUND CORROSION ON RBL 9 SEAT TRACK AT FS 977 AND FS 1005. CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK PN# SH670-37411-951 BETWEEN FS977- FS1005 IAW MHIRJ REO 670-53-00-773 REV-- DATED 2025-02-03
- [SDR VNAA2025050800026](https://openairdocs.org/sdr/VNAA2025050800026.md): Seat Track · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00218203 DISCREPANCY:LBL27 SEAT TRACKS (P/N: SH670-37412-951 & SH670-37380-953) BETWEEN FS922 - FS977 FOUND TO BE CORRODED. REPAIR/REPLACEMENT REQUIRED. CORRECTIVE ACTION: INSTALLED NEW SEAT TRACK PN# SH670-37412-3 BETWEEN FS922- FS977 IAW CRJ 700 AMM 53-00-
- [SDR VNA2025F00012](https://openairdocs.org/sdr/VNA2025F00012.md): Floorbeam · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN00208289 DISCREPANCY: RBL9 FLOOR BEAM FROM FS525.00 TO FACTORY SPLICE AT FS575.00 HAS MULTIPLE SPOTS OF CORROSION.
- [SDR VNAA2025050800025](https://openairdocs.org/sdr/VNAA2025050800025.md): Floorbeam · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN00208288 DISCREPANCY: LBL9 FLOOR BEAM FROM FS F533.00 TO FACTORY SPLICE AT FS575.00 HAS MULTIPLE SPOTS OF CORROSION. CORRECTIVE ACTION: UPON FURTHER INVESTIGATION, FOUND LBL9 FLOOR BEAM (P/N: SH670-33416-1) TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED ON UPP
- [SDR VNAA2025050800024](https://openairdocs.org/sdr/VNAA2025050800024.md): Floor Support · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00208288 DISCREPANCY: LBL9 FLOOR BEAM FROM FS F533.00 TO FACTORY SPLICE AT FS575.00 HAS MULTIPLE SPOTS OF CORROSION. CORRECTIVE ACTION: UPON FURTHER INVESTIGATION, FOUND LBL9 FLOOR BEAM (P/N: SH670-33416-1) TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED ON UPP
- [SDR VNAA2025050800023](https://openairdocs.org/sdr/VNAA2025050800023.md): Support · corroded · May 8, 2025 · N502AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00206830 DISCREPANCY: BACKUP SILL PN: SH670-31823-1 ON STR21L BETWEEN FS333.00 AND FS349.00 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED BACK-UP SILL IAW CRJ-700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Next page: https://openairdocs.org/aircraft/N502AE/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 = 'N502AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N502AE/reports

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