# Service difficulty reports: N501BG

A list on [N501BG](https://openairdocs.org/aircraft/N501BG.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 5 · 209 reports

- [SDR VNAA2026040315701](https://openairdocs.org/sdr/VNAA2026040315701.md): Coffeemaker · odor · Apr 1, 2026 · N501BG · Cndair CL6002C10 · Buffet/Galleys
  > BURNING SMELL COMING FROM GALLEY / PERFORMED SEVERAL OPS CHECKS/BREW CYCLES OF BOTH COFFEE POTS IAW CRJ 700 AMM 25-32-06-710-801 AND WHILE BREWING, NOTICED ABNORMAL SMELL COMING FROM BOTH COFFEE POTS AND SUSPECT BOTH COFFEE MAKERS TO BE FAULTY. REMOVED AND REP
- [SDR VNAA2025120111102](https://openairdocs.org/sdr/VNAA2025120111102.md): Unknown · odor · Nov 27, 2025 · N501BG · Cndair CL6002C10 · Air Distribution System
  > BURNING SMELL IN COCKPIT AFTER LANDING / C/W FDE SMOKE AND/OR ABNORMAL SMELL IN CABIN IAW FIM 21-22-00-810-806 NO DEFECTS OR SMELL NOTED AT THIS TIME
- [SDR VNAA20251015093](https://openairdocs.org/sdr/VNAA20251015093.md): Intercostal · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 20R INTERCOSTAL BETWEEN F.S. 319.70 AND F.S. 349.00 IS CORRODED AT MULTIPLE LOCATIONS. REMOVED AND REPLACED INTERCOSTAL BETWEEN IAW CRJ700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA20251015092](https://openairdocs.org/sdr/VNAA20251015092.md): Angle · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Wing Attach Fittings
  > WING TO FUSELAGE SUPPORT ANGLES AT RH SIDE AT FS939 PN SH670-39265-4 AND SH670-39265-6 HAS EXCESSIVE CORROSION REMOVED CORRODED ANGLES. LOCATED AND INSTALLED NEW ANGLES IAW REO 670-53-82-679 REV.--.
- [SDR VNAA20251015091](https://openairdocs.org/sdr/VNAA20251015091.md): Fitting · damaged · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Landing Gear Attach Fittings
  > OTBD BUSHING OF THE OTBD LUG OF THE L/H FITTING FOUND TO BE DAMAGED UPON REMOVAL REPAIRED THE OUTBD LUG OF THE L/H MLG SIDE STAY FITTING IAW MHIRJ REO 670-57-11-321 REV. --, DWG CC670-10608
- [SDR VNAA20251015089](https://openairdocs.org/sdr/VNAA20251015089.md): Insert · damaged · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Engine Thrust Reverser
  > FOUND HOLES FOR UPPER AND LOWER IB RH THRUST REVERSER NYLON INSERTS ELONGATED. PERFORMED REPAIR OF THE R/H THRUST REVERSER HINGE BEAM - P/N: CN624-0103-001, S/N: SB/0034 BY COMPLYING WITH MHIRJ REO 670-54-22-109 REV-- DATED 4-01-2025. VERIFIED CUSTOMER IS MA
- [SDR VNAA20251015088](https://openairdocs.org/sdr/VNAA20251015088.md): Seat Track · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAIL [FS847.00] TO [FS863.00] AND REQUIRES REPLACMENT. UPON FURTHER EVALUATION SIDE SEAT RAIL (FS847.00 TO FS863.00) WAS FOUND TO BE CORRODED OUT OF LIMITS AND REQUIRES REPLACEMENT.: FABRICATED NEW SEAT TRACK (FS847.00 TO FS 863.00) FROM EXTRU
- [SDR VNAA20251015087](https://openairdocs.org/sdr/VNAA20251015087.md): Seat Track · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAIL [FS573.00] TO [FS661.00] IS CORRODED REQUIRES REPLACMENT. REMOVED CORRODED SEAT RAIL. INSTALLED A NEW SEAT RAIL IAW CRJ AMM 53-00-49-001-801-A01.
- [SDR VNAA20251015084](https://openairdocs.org/sdr/VNAA20251015084.md): Seat Track · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9.00, FS836.55 TO FS850.45 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ700 SRM 53-00-49-201-002-A01, 51-40-11-001-001-A01 AND 53-00-49-400-801-A01. PAINTED SEAT TRACK P/N (SH670-33425-3), IAW PSA T.O. NUMBE
- [SDR VNAA20251015083](https://openairdocs.org/sdr/VNAA20251015083.md): Seat Track · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9.00 [FS693.00] TO [FS847.00] REQUIRES REPLACMENT. REPLACED SEAT TRACK LBL 9, FS 693 TO 847 (P/N SH670-35864-951) IAW CRJ 700 AMM 53-00-49-400-801-A01.
- [SDR VNAA20251015082](https://openairdocs.org/sdr/VNAA20251015082.md): Seat Track · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND TO BE OUT OF LIMITS ON LBL 9.00 [FS581.00] TO [FS677.00] REUIRES REPLACMENT. REPLACED SEAT TRACK LBL 9,00 FS581.00 TO FS677.00 (P/N SH670-33425-3) IAW CRJ 700 AMM 53-00-49-400-801-A01
- [SDR VNAA20251015081](https://openairdocs.org/sdr/VNAA20251015081.md): Seat Track · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9.00 [FS693.00] TO [FS847.00] FOUND TO BE OUT OF LIMITS DUE TO CORROSION EXTENDING ENTIRE LENGTH OF SEAT TRACK ON MULTIPLE ELEMENTS IAW CRJ700 SRM 53-41-49-101-001-A01. LOCATED AND DRILLED SEAT TRACK RBL9 [FS 693- FS 847] P/N (SH670-33425-3)
- [SDR VNAA20251015080](https://openairdocs.org/sdr/VNAA20251015080.md): Bracket · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR BRACKET AT FORWARD INTERCOSTAL DD5 IS CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET I.A.W. CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. 601R31902-461
- [SDR VNAA20251015079](https://openairdocs.org/sdr/VNAA20251015079.md): Beam · chafed · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT IB FLAP MOVABLE VANE BEAMS (ALL 4) HAVE SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-52-257 REV -A DATED 2024-08-20. REPAIR HAS SDIR IMPLICATIONS THAT NEED CAPTURED-VERIFIED REQUIREMENTS ARE BEING
- [SDR VNAA20251015078](https://openairdocs.org/sdr/VNAA20251015078.md): Intercostal · dented · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL FOWARD DD5 WAS FOUND TO BE DENTED AND BULGED. REMOVED AND REPLACED INTERCOSTAL I.A.W. MHIRJ REO 670-52-11-1459 REV.-.
- [SDR VNAA20251015077](https://openairdocs.org/sdr/VNAA20251015077.md): Intercostal · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR DD1 AFT INTERCOSTAL TO BE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR VNA2025F00039](https://openairdocs.org/sdr/VNA2025F00039.md): Floor Support · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DISCREPANCY: LBL 27 FLOOR BEAM IS CORRODED FROM FS 1000 TO FS 1015. CORRECTIVE ACTION: REPAIRED FLOOR BEAM IAW CRJ-700 SRM 53-00-41-201-001-A01. MM670-35302-005
- [SDR VNAA20251015076](https://openairdocs.org/sdr/VNAA20251015076.md): Cleat · corroded · Oct 17, 2025 · N501BG · Cndair CL6002C10 · Navigation System
  > AV SUPPORT CLEAT ON STR21R AT FS333.00 IS SEVERELY CORRODED. REMOVED AND REPLACED SUPPORT CLEAT IAW CRJ-700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR VNAA20251015075](https://openairdocs.org/sdr/VNAA20251015075.md): Stringer · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > DISCREPANCY: AV SUPPORT CLEAT ON STR21R AT FS333.00 IS SEVERELY CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED SUPPORT CLEAT IAW CRJ-700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01. SH670-32695-7
- [SDR VNAA20251015074](https://openairdocs.org/sdr/VNAA20251015074.md): Stringer · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R SPLICE AT FS333.00 IS SEVERELY CORRODED. REMOVED AND REPLACED STRINGER SPLICE IAW CRJ-700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR VNAA20251015073](https://openairdocs.org/sdr/VNAA20251015073.md): Frame · damaged · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 295 FRAME REQUIRES SPLICE REPAIR TO REMOVE AND REPLACE STGR 18R AND 19R. PERFORMED A CUT AND SPLICE REPAIR TO THE FS 295 FRAME IAW MHIRJ REO 670-53-21-2553 REV-.
- [SDR VNAA20251015072](https://openairdocs.org/sdr/VNAA20251015072.md): Stringer · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 18 R IS CORRODED BETWEEN F.S. 280 TO F.S. 295. FOUND TO BE OUT OF LIMITS DUE TO CORROSION ON MULTIPLE ELEMENTS. REMOVED STGR 18 R BETWEEN F.S. 280 TO F.S. 295 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED, DRILLED, AND DEBURR
- [SDR VNAA20251015071](https://openairdocs.org/sdr/VNAA20251015071.md): Door · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO DOOR IS CHAFFED ON INNER DOOR SKIN AT/ABOVE IB DOOR STOP, FWD AND AFT. REMOVED DAMAGE AND COMPLIED WITH MHIRJ REO 670-52-35-528 REV -.
- [SDR VNAA20251015070](https://openairdocs.org/sdr/VNAA20251015070.md): Slat Track · damaged · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-1 HAS WEAR DAMAGE IN MULTIPLE AREAS. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-57-42-1956 REV. -- DISPOSITION FOR BLENDED WEAR DAMAGE TO SLAT TRACK 3-1, RHS. REFERENCE HR00504995 AND HN00253015 FOR ASSOCIATED WORK PERFORMED.
- [SDR VNAA20251015069](https://openairdocs.org/sdr/VNAA20251015069.md): Fairing · damaged · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Aerodynamic Fairings
  > FOUND ENLONGATED HOLE UNDER LH SIDE WING TO FUSELAGE FAIRING AT FS FS893. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-51-335 REV --.
- [SDR VNAA20251015068](https://openairdocs.org/sdr/VNAA20251015068.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1961 REV-.
- [SDR VNAA20251015067](https://openairdocs.org/sdr/VNAA20251015067.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT SLAT TRACK 3-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 3-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1961 REV--.
- [SDR VNAA20251015066](https://openairdocs.org/sdr/VNAA20251015066.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 2-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1954 REV--.
- [SDR VNAA20251015065](https://openairdocs.org/sdr/VNAA20251015065.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 2-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1951 REV--.
- [SDR VNAA20251015064](https://openairdocs.org/sdr/VNAA20251015064.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 2-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1939 REV--.
- [SDR VNAA20251015063](https://openairdocs.org/sdr/VNAA20251015063.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 1-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1940 REV-- DATED 2025-01-29. CC670-12030-1
- [SDR VNAA20251015062](https://openairdocs.org/sdr/VNAA20251015062.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 1-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1935 REV--.
- [SDR VNAA20251015061](https://openairdocs.org/sdr/VNAA20251015061.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 1-1 BY COMPLYING WITH MHIRJ REO 670-57-42-2008 REV--.
- [SDR VNAA20251015060](https://openairdocs.org/sdr/VNAA20251015060.md): Skin · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Ailerons
  > DISCREPANCY:R/H AILERON LOWER SKIN CHAFED WS 348.00 TO WS 353.00 CORRECTIVE ACTION: SERVICEABLE PART P/N CC670-13054-2 DRILLED UP AND INSTALLED IAW CRJ 700 SRM TASK 51-42-06-001-001-A01, AND SRM TASK 51-42-21-001-001-A01 CC670-13054-2
- [SDR VNAA20251015059](https://openairdocs.org/sdr/VNAA20251015059.md): Vane · gouged · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP VANE LEADING EDGE HAS AN APPROXIMATELY 4" LONG GOUGE FROM CONTACT WITH BUCKTAIL ON TRAILING EDGE OF WING AT WS 231.23. COMPLIED WITH REO 670-57-53-395 REV --.
- [SDR VNAA20251015058](https://openairdocs.org/sdr/VNAA20251015058.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1964 REV--.
- [SDR VNAA20251015057](https://openairdocs.org/sdr/VNAA20251015057.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 2-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 2-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1953 REV -.
- [SDR VNAA20251015056](https://openairdocs.org/sdr/VNAA20251015056.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 2-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1953 REV -.
- [SDR VNAA20251015055](https://openairdocs.org/sdr/VNAA20251015055.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 2-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1943 REV -.
- [SDR VNAA20251015054](https://openairdocs.org/sdr/VNAA20251015054.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 2-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1941 REV -.
- [SDR VNAA20251015053](https://openairdocs.org/sdr/VNAA20251015053.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT SLAT TRACK 1-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 1-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1938 REV -.
- [SDR VNAA20251015052](https://openairdocs.org/sdr/VNAA20251015052.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 1-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1936 REV -.
- [SDR VNAA20251015051](https://openairdocs.org/sdr/VNAA20251015051.md): Slat Track · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge Devices
  > DISCREPANCY: LH SLAT TRACK 1-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 1-1 BY COMPLYING WITH MHIRJ REO 670-57-42-2009 REV -.
- [SDR VNAA20251015050](https://openairdocs.org/sdr/VNAA20251015050.md): Drag Angle · cracked · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > VERTICAL STAB RH DRAG ANGLE IS CRACKED (PREVIOUSLY REPAIRED AREA) CORRECTIVE ACTION: REPAIRED RH DRAG ANGLE IAW MHIRJ REO 670-55-31-188 REV -- DATED: 2025-03-04 AND BOMBARDIER REO 670-55-31-018 REV -A DATED: 2016-11-10.
- [SDR VNAA20251015049](https://openairdocs.org/sdr/VNAA20251015049.md): Attach Angle · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > DISCREPANCY: INTERCOSTAL ATTACH ANGLES AT F.S 517-533 STR 26L ARE CORRODED AND HAVE OVERSIZE HOLES CORRECTIVE ACTION: INSTALLED NEW PN: SH670-33399-951 AND PN: SH670-33600-983 BETWEEN FS 517 - FS 533, STR 27 - STR 26L (LBL 2.6) IAW CRJ-700 SRM 51-42-06-001-001
- [SDR VNAA20251015048](https://openairdocs.org/sdr/VNAA20251015048.md): Fitting · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Structure
  > FITTING P/N SH670-33389-1 @ F.S 533 STR 25L IS CORRODED. INSTALLED NEW FITTING P/N SH670-33389-1 IAW CRJ 700 SRM 51-42-21-001-001-A01 & CRJ 700 SRM 51-45-00-001-001-A01 SH670-33389-1
- [SDR VNAA20251015047](https://openairdocs.org/sdr/VNAA20251015047.md): Frame · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Frame
  > INTERCOSTAL FOR ACCESS TO FRAME CORROSION @ STR 25L F.S 517-F.S533 FOUND IT HAS INCOMING OVERSIZE RIVET HOLES. INSTALLED NEW INTERCOSTAL PN SH670-33568-5 IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR VNAA20251015046](https://openairdocs.org/sdr/VNAA20251015046.md): Angle · corroded · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS280 J ANGLE IS CORRODED. NEW SERVICEABLE ANGLE DRILLED UP AND INSTALLED IAW CRJ 700 SRM TASK 51-42-21-001-001-A01, AND SRM TASK 51-42-06-001-001-A01.
- [SDR VNAA20251015045](https://openairdocs.org/sdr/VNAA20251015045.md): Window Frame · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Structure
  > PILOT AND COPILOT'S WINDOW UPPER SILL IS GOUGED ABOVE THE LH AND RH WINDSHIELD SIDE POST. REPAIRED UPPER SILL IAW MHIRJ REO 670-53-11-2088 REV-.
- [SDR VNAA20251015044](https://openairdocs.org/sdr/VNAA20251015044.md): Beam · chafed · Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge Flaps
  > RH IB FLAP MOVABLE VANE BEAMS (ALL 4) HAVE SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-52-257 REV -A DATED 2024-08-20. REPAIR HAS SDIR IMPLICATIONS THAT NEED CAPTURED-VERIFIED REQUIREMENTS ARE BEING TR

Next page: https://openairdocs.org/aircraft/N501BG/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 = 'N501BG' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N501BG/reports

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