# Service difficulty reports: N601LR

A list on [N601LR](https://openairdocs.org/aircraft/N601LR.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 · 198 reports

- [SDR REXA2026042100295](https://openairdocs.org/sdr/REXA2026042100295.md): Display · inoperative · Apr 17, 2026 · N601LR · Cndair CL6002D24 · Central Display
  > WHEN STARTING DESCENT FL380 BOTH PFD'S UNRELIABLE AIRSPEED. ISI APPEARED NORMAL. RAN QRH 13-10. UNRELIABLE AIRSPEED APPEARED WHILE IN IMC(IN THE CLOUDS). BOTH AIRSPEED INDICATORS ON PFD'S DISAPPEARED WITH IAS FLAGS. AT APPROX F240 OUT OF CLOUDS CA AISPEED ON P
- [SDR REXA2026073001251](https://openairdocs.org/sdr/REXA2026073001251.md): Angle · corroded · Jun 19, 2025 · N601LR · Cndair CL6002D24 · Service Doors
  > CORROSION WAS FOUND ON BONDING ANGLE AND WEAR ON SERVICE DOOR (142BR) INTERNAL SKIN. CORROSION ON BONDING ANGLE WAS REPLACED IAW SRM 5-42-06-001-001-A01 AND WEAR ON SERVICE DOOR (142BR) WAS EVALUATED OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND WAS REPAIRED
- [SDR REXA2026073001250](https://openairdocs.org/sdr/REXA2026073001250.md): Skin · corroded · Jun 19, 2025 · N601LR · Cndair CL6002D24 · Service Doors
  > CORROSION WAS FOUND ON BONDING ANGLE AND WEAR ON SERVICE DOOR (142BR) INTERNAL SKIN. CORROSION ON BONDING ANGLE WAS REPLACED IAW SRM 5-42-06-001-001-A01 AND WEAR ON SERVICE DOOR (142BR) WAS EVALUATED OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND WAS REPAIRED
- [SDR REXA2026073001249](https://openairdocs.org/sdr/REXA2026073001249.md): Angle · corroded · Jun 19, 2025 · N601LR · Cndair CL6002D24 · Fluid Service Doors
  > CORROSION AT FWD WATER WASTE SERVICE DOOR INTERNAL STRUCTURE DIAPHRAGM FWD WATER WASTE SERVICE DOOR INTERNAL STRUCTURE DIAPHRAGM WAS EVALUATED OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND WAS REPLACED IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2025062600699](https://openairdocs.org/sdr/REXA2025062600699.md): Drag Angle · cracked · Jun 19, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > 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). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM
- [SDR REXA2026073001253](https://openairdocs.org/sdr/REXA2026073001253.md): Hinge Fitting · corroded · Jun 17, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION WAS FOUND ON LT & RT NLG AFT DOOR UPPER FITTINGS AND CORROSION WAS FOUND ON RT HINGE FITTING OF NLG AFT DOOR IAW TASK CARD 900-32-710-902. LT AND RT NLG AFT DOOR UPPER FITTINGS AND RT HINGE FITTING OF NLG AFT DOOR WERE REPLACED IAW SRM 51-41-02-001-0
- [SDR REXA2025071500696](https://openairdocs.org/sdr/REXA2025071500696.md): Step · cracked · Jun 17, 2025 · N601LR · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK WAS FOUND ON AFT/FWD SIDE PANEL BTW TOP-MIDDLE STEPS AT PASSANGER DOOR IN REFERENCE NRC 114 SUMMARY: AFT/FWD SIDE PANEL BTW TOP-MIDDLE STEPS AT PASSANGER DOOR WAS REPAIRED PER CRJ900 SRM 52-11-04-201-004-A01
- [SDR REXA2025062600698](https://openairdocs.org/sdr/REXA2025062600698.md): Support Angle · cracked · Jun 17, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK IN FWD SUPPORTS ANGLES (2EA) AT UPPER ACUMULATOR ON NOSE HYD COMPARTMENT WAS FOUND. FWD SUPPORTS ANGLES (2EA) AT UPPER ACUMULATOR ON NOSE HYD COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2025062600697](https://openairdocs.org/sdr/REXA2025062600697.md): Diaphragm · cracked · Jun 17, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17 CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17 WAS REPAIRED PER EA NO. CRJ953-19412 REV. IR
- [SDR REXA2025062600694](https://openairdocs.org/sdr/REXA2025062600694.md): Angle · cracked · Jun 17, 2025 · N601LR · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (
- [SDR REXA2026073001246](https://openairdocs.org/sdr/REXA2026073001246.md): Angle · cracked · Jun 9, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER PLATE REMOVAL, CRACK ON PLATE ANGLE WAS FOUND AT FWD WASTE INTERNAL STRUCTURE, PLATE ANGLE AT FWD WASTE INTERNAL STRUCTURE WAS REPLACED IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2026073001248](https://openairdocs.org/sdr/REXA2026073001248.md): Floorbeam · corroded · Jun 7, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFTER SEAT TRACKS REMOVAL, CORROSION ON FLOORBEAM LOCATED ON 12LBL AND BS 661+32 TO BS 686 WAS FOUND. FLOORBEAM LBL 12 AND BS 661+32 TO 686 WAS REPAIRED IAW SRM 53-00-41-201-001-A03, AND REO 690-53-31-1022 REV--.
- [SDR REXA2025062600693](https://openairdocs.org/sdr/REXA2025062600693.md): Bracket · cracked · Jun 6, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER REMOVE OF EXTERNAL SERVICE PANEL (PL101), CRACK ON LOWER SUPPORT BRACKET WAS FOUND LOCATED BTW FS193.00/FS202.75 AND BTW STGR19R/21R. LOWER SUPPORT BRACKET WAS FOUND LOCATED BTW FS193.00/FS202.75 AND BTW STGR19R/21R WAS REPLACED PER CRJ-900 SRM 51-42-21
- [SDR REXA2026073001254](https://openairdocs.org/sdr/REXA2026073001254.md): Hinge Fitting · corroded · Jun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION WAS FOUND ON SERVICE DOOR HINGES PADS (3 EAS). PADS (3 EAS) ON SERVICE DOOR HINGES WERE FABRICATED IAW EA CRJ953-19481 REV IR & EA CRJ953-19480 REV IR AND THEY WERE REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-41-02-001-001-A01.
- [SDR REXA2026073001252](https://openairdocs.org/sdr/REXA2026073001252.md): Hinge · corroded · Jun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION WAS FOUND ON SERVICE DOOR HINGES PADS (3 EAS). PADS (3 EAS) ON SERVICE DOOR HINGES WERE FABRICATED IAW EA CRJ953-19481 REV IR AND EA CRJ953-19480 REV IR AND THEY WERE REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-41-02-001-001-A01.
- [SDR REXA2026073001244](https://openairdocs.org/sdr/REXA2026073001244.md): Plate · corroded · Jun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER DRAIN VALVE (FWD LAV) REMOVAL, CORROSION ON PLATE WAS FOUND AT FWD WASTE SURROUND STRUCTURE BTW BS 379 TO BS 394 AND STR 21R-23R, REF NRC 00267. PLATE AT FWD WASTE SURROUND STRUCTURE BTW BS 379 TO 394, STR 21R-23R, REPAIRED PER EA CRJ953-19495 REV.A
- [SDR REXA2025062600692](https://openairdocs.org/sdr/REXA2025062600692.md): Canister · cracked · Jun 5, 2025 · N601LR · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK IN CANISTER, WELDED NO.1-3 SLAT TRACK BTW WS148.00 TO WS 163.00 AT RH MAIN FUEL TANK. CANISTER WELDED NO.1-3 SLAT TRACK BTW WS148.00 TO WS 163.00 AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577.REV. - -
- [SDR REXA2025062600691](https://openairdocs.org/sdr/REXA2025062600691.md): Angle · cracked · Jun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER DIAPHRAGM REMOVAL, CRACK ON FWD ANGLE AND ALSO HAS CORROSION WERE FOUND, AT WATER/WASTE SERVICE DOOR SURROUND STRUCTURE OVER FS 379.00 AND BTW STGR 21R-23R. FWD ANGLE WAS REPAIRED PER EA CRJ953-19508 REV IR AND CORROSION AT WATER/WASTE SERVICE DOOR SURRO
- [SDR REXA2026073001259](https://openairdocs.org/sdr/REXA2026073001259.md): Support Plate · cracked · Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT RH CORNER SUPPORT PLATE OF THE JB 6 MODULE AT INTERNAL FORWARD EQUIPMENT COMPARTMENT SUPPORT PLATE OF THE JB 6 MODULE AT INTERNAL FORWARD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2025062600690](https://openairdocs.org/sdr/REXA2025062600690.md): Web · cracked · Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CRACK ON WEB BTW FS193.00/STGR16LH AT INTERNAL FORWARD EQUIPMENT COMPARTMENT. WEB BTW FS193.00/STGR16LH AT INTERNAL FORWARD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR REXA2025062600689](https://openairdocs.org/sdr/REXA2025062600689.md): Door Sill · cracked · Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON RH DOOR LANDING STRUCTURE AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FORWARD EQUIPMENT COMPARTMENT. DOOR LANDING STRUCTURE AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FORWARD EQUIPMENT COMPARTMENT WAS REPAIRED PER EA CRJ953-19497
- [SDR REXA2025062600688](https://openairdocs.org/sdr/REXA2025062600688.md): Stiffener · cracked · Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON STIFFENER AT ACCESS PANEL 172CR. STIFFENER (P/N: SH670-39397-3) WAS FABRICATED PER EA NO: CRJ953-19538 REV: IR AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2026073001258](https://openairdocs.org/sdr/REXA2026073001258.md): Hinge Fitting · damaged · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Ailerons
  > FABRICATE BUSHINGS OVERSIZE FOR AILERON LT HINGE FITTING 2 & 3 WING TRAILING EDGE. BUSHINGS OVERSIZE FOR AILERON LT HINGE FITTING 2 & 3 WING TRAILING EDGE WERE FABRICATED PER REO 690-57-51-239 REV A.
- [SDR REXA2026073001257](https://openairdocs.org/sdr/REXA2026073001257.md): Fitting · damaged · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Ailerons
  > FABRICATE BUSHINGS OVERSIZE FOR AILERON LH HINGE FITTING 2 & 3 WING TE. BUSHINGS OVERSIZE FOR AILERON LT HINGE FITTING 2 & 3 WING T E WERE FABRICATED PER REO 690-57-51-239 REV. -A
- [SDR REXA2026073001256](https://openairdocs.org/sdr/REXA2026073001256.md): Hinge · corroded · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Ailerons
  > CORROSION WAS FOUND ON LUGS BORES R1, R2, R5 AND R6 AND WEAR AND CORROSION ON LUG FACE AND LUG EDGE R1, R2, R3, R4, R5 AND R6 AT RH AILERON CENTER FITTING LUGS BORES OF R1, R2, R5 AND R6 AND FACES R1, R2 AND R5 AT RH AILERON CENTER FITTING WERE REPAIRED REO 6
- [SDR REXA2026073001255](https://openairdocs.org/sdr/REXA2026073001255.md): Seat Track · corroded · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LOCATED ON 12LBL AND 12RBL BTW FS FS661.00+90/FS693.00. DUE TO EXCESIVE CORROSION ON SEAT TRACK LOCATED ON 12LBL AND 12RBL BTW FS FS661.00+90/FS693.00 WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND 53-31-49-101-001-A02 AND AMM 5
- [SDR REXA2026073001247](https://openairdocs.org/sdr/REXA2026073001247.md): Frame · corroded · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT FWD WATER WASTE SERVICE DOOR INTERNAL STRUCTURE, FWD & AFT FRAME. AFT FRAME AT FWD WATER WASTE SERVICE DOOR INTERNAL STRUCTURE WAS CLEANED IAW SRM 51-26-00-001-001-A01 AND NOT DAMAGE WAS FOUND, AND FRAME FWD BS 379 BTW STR 20R AND STR 25R WAS EVAL
- [SDR REXA2026073001245](https://openairdocs.org/sdr/REXA2026073001245.md): Skin · worn · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON SKIN IN BS 910 NEAR STR 27 AT FUSELAGE SKIN. SKIN WAS REPAIRED IAW EA CRJ953-19451, REV IR.
- [SDR REXA2026073001243](https://openairdocs.org/sdr/REXA2026073001243.md): Roller Guide · cracked · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Structure
  > IN REF TO TC 900-52-830-304: WEAR ON SUPPORT AFT ROLLER GUIDE ON AFT BAGGAGE BAY STRUCTURE DUE TO EXCCESIVE DAMAGE ON SUPPORT AFT ROLLER GUIDE ON AFT BAGGAGE BAY STRUCTURE WAS REPLACED IAW SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01.
- [SDR REXA2025062600687](https://openairdocs.org/sdr/REXA2025062600687.md): Handle · cracked · Jun 2, 2025 · N601LR · Cndair CL6002D24 · Passenger/Crew Doors
  > INITIAL INSPECTION': CRACKED OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026073001263](https://openairdocs.org/sdr/REXA2026073001263.md): Support Bracket · corroded · May 30, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT BRACKET LOCATED BTW BS 280 AND STR 26LT - 26RT DUE TO EXCESSIVE DAMAGE SUPPORT BRACKET LOCATED BTW BS 280 AND STR 26LT - 26RT WAS REPLACED IAW SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-06-001-001-A01.
- [SDR REXA2026073001242](https://openairdocs.org/sdr/REXA2026073001242.md): Beam · worn · May 30, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Structure
  > WEAR ON BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE). WEAR ON BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE WAS REPAIRED PER EA CRJ953-19464 REV. IR.
- [SDR REXA2024102501011](https://openairdocs.org/sdr/REXA2024102501011.md): Door · cracked · Jan 7, 2024 · N601LR · Cndair CL6002D24 · Emergency Exits
  > FOUND AFT LUG CRACKED ON L/H FWD EMERGENCY EXIT DOOR. REPAIRED IAW MHIRJ REO 690-52-21-150 REV -- DATED 2024-01-15.
- [SDR REXA2024102500975](https://openairdocs.org/sdr/REXA2024102500975.md): Door · cracked · Jan 7, 2024 · N601LR · Cndair CL6002D24 · Emergency Exits
  > FOUND L/H AFT EMERGENCY DOOR FWD. DOOR LUG MOUNT CRACKED. REPAIRED IAW MHIRJ REO 690-52-21-147A DATED 1/14/2024.
- [SDR REXA2024032100299](https://openairdocs.org/sdr/REXA2024032100299.md): Door Frame · cracked · Jan 7, 2024 · N601LR · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FWD EMERGENCY EXIT DOOR HAS A VISIBLE CRACK ON THE UPPER FWD LUG FRAME, REPAIRED IAW MHIRJ REO 690-52-21-149 REV--1/15/2024,
- [SDR REXA2024102500974](https://openairdocs.org/sdr/REXA2024102500974.md): Support · corroded · Jan 5, 2024 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON R/H SILL AT RBL 36 FS 801. REPAIRED IAW MHIRJ REO# 690-53-41-442, REV--, DATED 2024-01-08.
- [SDR REXA2024102500973](https://openairdocs.org/sdr/REXA2024102500973.md): Support · corroded · Jan 5, 2024 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON L/H SILL AT LBL 36 FS 792. REPAIRED IAW MHIRJ REO# 690-53-41-442, REV--, DATED 2024-01-08.
- [SDR REXA2021122001178](https://openairdocs.org/sdr/REXA2021122001178.md): Lamp · inoperative · Dec 14, 2021 · N601LR · Cndair CL6002D24 · Emergency Lighting
  > AFT RH OVERWING EXTERIOR EMERGENCY LIGHT INOP. FOUND WIRE AT DS93 (YAH8493-22) TO BE BROKEN AT CONNECTOR DS93 AND BULB INOP. FOUND GROUND WIRE GS1612, GJG6080N BROKEN AT LIGHT DS56. REPAIRED BROKEN WIRES TO CRJ 900 ESPM 20-33-00. REPLACED UNSERVICEABLE BULB AT
- [SDR REXA2021122001148](https://openairdocs.org/sdr/REXA2021122001148.md): Frame · corroded · Dec 13, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME 349 CORRODED ON LOWER / AFT FACE AT STGR 27. C/A: REMOVED CORRODED FRAME SECTOR AT F.S.349 STGR 27 AND INSTALLED NEW SERVICABLE FRAME SECTOR IAW CRJ 900 SRM 51-42-21-001-001-A01 & 51-42-06-001-001-A01..
- [SDR REXA2021122001135](https://openairdocs.org/sdr/REXA2021122001135.md): Frame · corroded · Dec 12, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE AT FS 847+32, BETWEEN STR 26R AND 26L, FRAME IS CORRODED. C/A: SPLICE REPAIRED FRAME SECTOR IAW CRJ 900 SRM 53-00-06-201-001-A03.
- [SDR REXA2021122001176](https://openairdocs.org/sdr/REXA2021122001176.md): Stringer · corroded · Dec 7, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 21R CORRODED AT MULTIPLE FASTENER LOCATION BETWEEN FS340 TO FS348. C/A: REMOVED AND REPLACED STRINGER 21R BETWEEN FS340 AND FS348 IAW CRJ 900 SRM 53-00-03-995-806, 53-00-03-201-001-001-A02, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2021122001134](https://openairdocs.org/sdr/REXA2021122001134.md): Frame · corroded · Dec 7, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE AT FS 847+16 BETWEEN STR 26L AND 26R HAS EVIDENCE OF CORROSION AROUND FITTING FASTENERS. C/A: SPLICE REPAIRED FRAME SECTOR @ FS847+16 BETWEEN STR26L AND STGR26R IAW CRJ 900 SRM53-00-06-201-001-A03, 51-21-06-001-001-A01 AND ENDEAVOR AIR EA #CRJ953-
- [SDR REXA2021122001147](https://openairdocs.org/sdr/REXA2021122001147.md): Stringer · corroded · Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER AT 20R IS CORRODED FS 280 TO FS 319. C/A: REMOVED & REPLACED STRINGER IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 & ENDEAVOR AIR EA CRJ953-12425
- [SDR REXA2021122001146](https://openairdocs.org/sdr/REXA2021122001146.md): Stringer · corroded · Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER AT 20R IS CORRODED FS 319 TO FS 349. C/A: REMOVED & REPLACED STRINGER IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 & ENDEAVOR AIR EA CRJ953-12425
- [SDR REXA2021122001145](https://openairdocs.org/sdr/REXA2021122001145.md): Bracket · corroded · Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 20R BRACKET IS CORRODED FS 280 TO FS 349. C/A: REMOVED & REPLACED BRACKET IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 & ENDEAVOR AIR EA CRJ953-12425.
- [SDR REXA2021122001144](https://openairdocs.org/sdr/REXA2021122001144.md): Angle · corroded · Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 20R ATTACH ANGLES ARE CORRODED FS 280 TO FS 349. C/A: REMOVED & REPLACED ANGLES (2) IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 & ENDEAVOR AIR EA CRJ953-12425.
- [SDR REXA2021122001136](https://openairdocs.org/sdr/REXA2021122001136.md): Frame · corroded · Dec 4, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE UNDERFLOOR FS 969 BETWEEN STR 25 AND 26R AND FLOOR SKIN HAS CORROSION C/A: SPLICE REPAIRED FRAME SECTOR @ FS969 BETWEEN STR 25R AND 26R IAW CRJ 900 SRM53-00-06-201-001-A03 AND 51-21-06-001-001-A01.
- [SDR REXA2022011100005](https://openairdocs.org/sdr/REXA2022011100005.md): None · corroded · Dec 2, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SILL IS CORRODED BETWEEN FS1000 AND FS1047. REMOVED AND REPLACED AFT CARGO DOOR LOWER SILL IAW CRJ 900 SRM 51-42-13-001-001-A01 & 51-42-20-001-001-A01.
- [SDR REXA2021122001171](https://openairdocs.org/sdr/REXA2021122001171.md): None · corroded · Nov 29, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT TRACK CORRODED AT FS988-FS1005, LBL9. C/A: REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A07 AND CRJ 900 SRM 53-00-49-201-001-A01.
- [SDR REXA2021122001162](https://openairdocs.org/sdr/REXA2021122001162.md): None · corroded · Nov 29, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED BETWEEN FS280-286 "CORRECTIVE ACTION: REMOVED & REPLACED SILL IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01."

Next page: https://openairdocs.org/aircraft/N601LR/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 = 'N601LR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N601LR/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.