N601LR

Service difficulty reports · 198

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026042100295Display · inoperativeWHEN 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 PApr 17, 2026 · N601LR · Cndair CL6002D24 · Central DisplaySDR REXA2026073001251Angle · corrodedCORROSION 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 Jun 19, 2025 · N601LR · Cndair CL6002D24 · Service DoorsSDR REXA2026073001250Skin · corrodedCORROSION 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 Jun 19, 2025 · N601LR · Cndair CL6002D24 · Service DoorsSDR REXA2026073001249Angle · corrodedCORROSION 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.Jun 19, 2025 · N601LR · Cndair CL6002D24 · Fluid Service DoorsSDR REXA2025062600699Drag Angle · crackedCRACK 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 DATUMJun 19, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026073001253Hinge Fitting · corrodedCORROSION 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 51-41-02-001-0Jun 17, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2025071500696Step · crackedCRACK 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-A01Jun 17, 2025 · N601LR · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2025062600698Support Angle · crackedCRACK 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-A01Jun 17, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025062600697Diaphragm · crackedCRACK 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. IRJun 17, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025062600694Angle · crackedCRACK 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 (Jun 17, 2025 · N601LR · Cndair CL6002D24 · Vertical StabilizerSDR REXA2026073001246Angle · crackedAFTER 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.Jun 9, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001248Floorbeam · corrodedAFTER 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--.Jun 7, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2025062600693Bracket · crackedAFTER 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 51-42-21Jun 6, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073001254Hinge Fitting · corrodedCORROSION 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.Jun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026073001252Hinge · corrodedCORROSION 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.Jun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026073001244Plate · corrodedAFTER 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.AJun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025062600692Canister · crackedCRACK 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. - -Jun 5, 2025 · N601LR · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2025062600691Angle · crackedAFTER 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 SURROJun 5, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001259Support Plate · crackedCRACK 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-A01Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025062600690Web · crackedINITIAL 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-A01Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025062600689Door Sill · crackedCRACK 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 Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2025062600688Stiffener · crackedCRACK 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-A01Jun 3, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001258Hinge Fitting · damagedFABRICATE 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.Jun 2, 2025 · N601LR · Cndair CL6002D24 · AileronsSDR REXA2026073001257Fitting · damagedFABRICATE 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. -AJun 2, 2025 · N601LR · Cndair CL6002D24 · AileronsSDR REXA2026073001256Hinge · corrodedCORROSION 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 6Jun 2, 2025 · N601LR · Cndair CL6002D24 · AileronsSDR REXA2026073001255Seat Track · corrodedCORROSION 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 5Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073001247Frame · corrodedCORROSION 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 EVALJun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001245Skin · wornWEAR ON SKIN IN BS 910 NEAR STR 27 AT FUSELAGE SKIN. SKIN WAS REPAIRED IAW EA CRJ953-19451, REV IR.Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2026073001243Roller Guide · crackedIN 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.Jun 2, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2025062600687Handle · crackedINITIAL 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-A01Jun 2, 2025 · N601LR · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026073001263Support Bracket · corrodedCORROSION 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.May 30, 2025 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001242Beam · wornWEAR 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.May 30, 2025 · N601LR · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024102501011Door · crackedFOUND AFT LUG CRACKED ON L/H FWD EMERGENCY EXIT DOOR. REPAIRED IAW MHIRJ REO 690-52-21-150 REV -- DATED 2024-01-15.Jan 7, 2024 · N601LR · Cndair CL6002D24 · Emergency ExitsSDR REXA2024102500975Door · crackedFOUND L/H AFT EMERGENCY DOOR FWD. DOOR LUG MOUNT CRACKED. REPAIRED IAW MHIRJ REO 690-52-21-147A DATED 1/14/2024.Jan 7, 2024 · N601LR · Cndair CL6002D24 · Emergency ExitsSDR REXA2024032100299Door Frame · crackedR/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,Jan 7, 2024 · N601LR · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024102500974Support · corrodedFOUND CORROSION ON R/H SILL AT RBL 36 FS 801. REPAIRED IAW MHIRJ REO# 690-53-41-442, REV--, DATED 2024-01-08.Jan 5, 2024 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024102500973Support · corrodedFOUND CORROSION ON L/H SILL AT LBL 36 FS 792. REPAIRED IAW MHIRJ REO# 690-53-41-442, REV--, DATED 2024-01-08.Jan 5, 2024 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001178Lamp · inoperativeAFT 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 ATDec 14, 2021 · N601LR · Cndair CL6002D24 · Emergency LightingSDR REXA2021122001148Frame · corrodedFRAME 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..Dec 13, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001135Frame · corrodedAFT 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.Dec 12, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001176Stringer · corrodedSTRINGER 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.Dec 7, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001134Frame · corrodedAFT 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-Dec 7, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001147Stringer · corrodedSTRINGER 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 CRJ953-12425Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001146Stringer · corrodedSTRINGER 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 CRJ953-12425Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001145Bracket · corrodedSTRINGER 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.Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001144Angle · corrodedSTRINGER 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.Dec 5, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001136Frame · corrodedAFT 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.Dec 4, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022011100005None · corrodedAFT 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.Dec 2, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001171None · corrodedSEAT 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.Nov 29, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021122001162None · corrodedRH 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."Nov 29, 2021 · N601LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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