# Service difficulty reports: N606LR

A list on [N606LR](https://openairdocs.org/aircraft/N606LR.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 6 · 288 reports

- [SDR REXA2026041600290](https://openairdocs.org/sdr/REXA2026041600290.md): Light · broken · Apr 10, 2026 · N606LR · Cndair CL6002D24 · Emergency Lighting
  > PART OF THE EMERGENCY PATH INDICATING LIGHT BY THE PASSENGER DOOR IS BROKEN. R/R EMERGENCY PATH INDICATING STRIP PER CMM 33-51-07.
- [SDR REXA2025022700234](https://openairdocs.org/sdr/REXA2025022700234.md): Fitting · cracked · Feb 25, 2025 · N606LR · Cndair CL6002D24 · Passenger/Crew Doors
  > DURING OVERNIGHT VISIT, MAINTENANCE FOUND MAIN PASSENGER DOOR AFT CAM FITTING FOR THE AFT PULL IN LEVER CRACKED. REMOVED AND REPLACED CAM FITTING, PERFROMED OPERATIONAL CHECK OF MAIN PASSENGER DOOR AND ADJUSTMENT CHECK OF THE MAIN PASSENGER DOOR IAW AMM 53-21-
- [SDR REXA2024120301550](https://openairdocs.org/sdr/REXA2024120301550.md): Fitting · obstructed · Nov 6, 2024 · N606LR · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND RH FITTING PN CC670-33562-001SB CANNOT BE INSTALLED PER SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING RIVET PATTERN ON FS202.75 BULKHEAD. TRIMMED FITTING AND OMITTED FASTENER IAW MHIRJ REO 690
- [SDR REXA2024111201472](https://openairdocs.org/sdr/REXA2024111201472.md): None · none · Nov 5, 2024 · N606LR · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE INCORPORATING SB 670BA-53-036/670SH-53-043 WE HAVE DISCOVERED THAT TWO FACTORY PILOT HOLES WILL NOT ALIGN WITH EXISTING HOLES FROM THE LH PRESSURE BOX @ FS 843 LBL18 AREA. OVERSIZED FASTENER HOLES AND INSTALLED ALTERNATE FASTENERS IAW MHIRJ REO 690-53-41
- [SDR REXA2024073000588](https://openairdocs.org/sdr/REXA2024073000588.md): Hinge · broken · Jan 29, 2024 · N606LR · Cndair CL6002D24 · Fuselage, Door Hinge
  > TOP FOLDING STEP HINGE PN: 601R31980-63 THAT ATTACHES THE PANEL WITH LOGO TO PAX DOOR IS BROKEN ON BOTH FORWARD AND AFT ENDS. REMOVED PAX DOOR TOP FOLDING STEP HINGE IAW CRJ900 SRM 51-42-06-001-001-A01, LOCATED, DRILLED, AND INSTALLED NEW PAX DOOR TOP STEP FO
- [SDR REXA2024073000573](https://openairdocs.org/sdr/REXA2024073000573.md): Stringer · corroded · Jan 28, 2024 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STGR BETWEEN FS 611+90-677 REMOVED CORRODED STRINGER 21R FROM F.S.661+74 TO F.S.693. FABRICATED, LOCATED AND DRILLED NEW SECTION STRINGER STR21R WITH S-MATERIAL P/N B0530020BF, PO# 5-8708 BETWEEN FS661+74Ï¿½ TO FS693, IAW CRJ-900 SRM 51-40-
- [SDR REXA2024030700246](https://openairdocs.org/sdr/REXA2024030700246.md): Stringer Splice · corroded · Dec 30, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 21R JOINT PLATE/WASTE DOOR SURROUND IS CORRODED BETWEEN FS 379 AND FS 394 REMOVED AND INSTALLED NEW SERVICEABLE STGR 21R JOINT PLATE BETWEEN FS 379 AND FS 394 PN SH670-32301-5 IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2024030700243](https://openairdocs.org/sdr/REXA2024030700243.md): Angle · corroded · Dec 30, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD LAV/WASTE CUTOUT LOWER SILL ANGLE IS CORRODED REMOVED AND INSTALLED NEW SERVICEABLE LOWER SILL ANGLE OF FWD LAV/WASTE DOOR CUTOUT IAW CRJ-900 SRM 51-42-06-001-001-A01 P/N SH670-32284-3
- [SDR REXA2024030700242](https://openairdocs.org/sdr/REXA2024030700242.md): Angle · corroded · Dec 30, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD LAV/WASTE DOOR CUTOUT UPPER SILL ANGLE IS CORRODED REMOVED AND INSTALLED NEW SERVICEABLE FWD LAV/WASTE DOOR CUTOUT UPPER SILL ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 P/N SH670-32285-15
- [SDR REXA2024030700241](https://openairdocs.org/sdr/REXA2024030700241.md): Frame · corroded · Dec 30, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 379 FRAME IS CORRODED ON AFT SIDE AT LAV WASTE CUTOUT REMOVED AND INSTALLED NEW FRAME LOCATED AT FS 379 BETWEEN STR20R TO STR25R IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2024030700240](https://openairdocs.org/sdr/REXA2024030700240.md): Skin · corroded · Dec 30, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > MULTIPLE SPOTS OF CORROSION FOUND ON CLOSING SKIN AROUND FWD CARGO DOOR. REPAIRED IAW ENDEAVOR EA CRJ953-15863
- [SDR REXA2024021200180](https://openairdocs.org/sdr/REXA2024021200180.md): Frame · corroded · Dec 30, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 485, S20R-S26R REQUIRES REMOVAL FOR STRINGER 21R REPAIR ACCESS PERFORMED FRAME SPLICE REPAIR (TO FACILITATE NEARBY STRINGER REPAIRS) AT F.S. 485 FRAME FROM STGR 20R TO STGR 26R BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-15905 REV IR DATE
- [SDR REXA2024030700239](https://openairdocs.org/sdr/REXA2024030700239.md): Angle · corroded · Dec 29, 2023 · N606LR · Cndair CL6002D24 · Service Doors
  > LAV DOOR CUTOUT IMPACT ANGLE IS CORRODED. REMOVED AND INSTALLED NEW LAV. DOOR CUTOUT IMPACT ANGLE P/N SH670-32310-1 IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2024030700238](https://openairdocs.org/sdr/REXA2024030700238.md): Stringer · corroded · Dec 29, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R BETWEEN F.S.409 TO F.S.437 IS CORRODED. REMOVED AND INSTALLED NEW STRINGER IAW CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, AND CRJ900 SRM 51-42-13-001-001-A01
- [SDR REXA2024030700237](https://openairdocs.org/sdr/REXA2024030700237.md): Bracket · cracked · Dec 29, 2023 · N606LR · Cndair CL6002D24 · Wing, Attach Fittings
  > RH SLAT TRACK1-3 CANISTER ATTACHMENT TAB IS CRACKED (INSIDE FUEL TANK) REPAIRED IAW BOMBARDIER REO 670-57-42- 577
- [SDR REXA2024031300264](https://openairdocs.org/sdr/REXA2024031300264.md): Intercostal · corroded · Dec 20, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 21L FROM F.S.333 TO F.S.349 IS CORRODED. INSTALLED NEW SERVICEABLE INTERCOSTAL/BACKUP SILL P/N SH670-31823-1 IAW CRJ-900 SRM 51-40-11-001-001-A01.
- [SDR REXA2024012200105](https://openairdocs.org/sdr/REXA2024012200105.md): Bracket · corroded · Dec 20, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MACHINE FITTING AT F.S.565 STGR 26R IS CORRODED. REMOVED CORRODED FITTING AND INSTALLED NEW SERVICABLE MACHINE FITTING IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024012200101](https://openairdocs.org/sdr/REXA2024012200101.md): Seat Track · corroded · Dec 20, 2023 · N606LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 847+48 TO F.S. 969. REMOVED RBL9 SEAT TRACK BETWEEN FS847+48 - 969 IAW CRJ900 AMM 53-00-49-000-801-A07 CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE RBL9 SEAT TRACK PN 670-53-00-692-1 BETWEEN FS847+48 - 969 IAW C
- [SDR REXA2024012200100](https://openairdocs.org/sdr/REXA2024012200100.md): Seat Track · corroded · Dec 20, 2023 · N606LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 847+48 TO F.S. 985. REMOVED LBL9 SEAT TRACK BETWEEN FS847+48 - 985 IAW CRJ900 AMM 53-00-49-000-801-A07 CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE LBL9 SEAT TRACK PN 670-53-00-692-1 BETWEEN FS847+48 - 985 IAW C
- [SDR REXA2024012200099](https://openairdocs.org/sdr/REXA2024012200099.md): Fitting · corroded · Dec 20, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CROSSBEAM ATTACH FITTING AT F.S.349, LBL36 IS CORRODED. REMOVED FLOOR BEAM FITTING AT FS 349, LBL 36, IAW CRJ 900 SRM 51-42-21-001-001-A01. INSTALLED NEW FLOOR BEAM FITTING PN:SH670-31942-3 AT FS 349, LBL 36, IAW CRJ 900 SRM 51-42-21-001-001-A01
- [SDR REXA2024012200098](https://openairdocs.org/sdr/REXA2024012200098.md): Floor Panel · cracked · Dec 20, 2023 · N606LR · Cndair CL6002D24 · Fuselage Floor Panel
  > RH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IS CRACKED JUST O/B OF THE ADG RETRACTION PUMP. REPAIRED RH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IAW CRJ 900 SRM 53-11-43-201-001-A01.
- [SDR REXA2024011600072](https://openairdocs.org/sdr/REXA2024011600072.md): Intercostal · corroded · Dec 19, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 21L FROM F.S.310 TO F.S.333 IS CORRODED. INSTALLED NEW SERVICEABLE WEB FLOOR PROTECTOR ANGLES 2EA (PN SH670-32040-4S) AND 1EA (PN SH670-32040-3S) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2024011600073](https://openairdocs.org/sdr/REXA2024011600073.md): Bracket · corroded · Dec 19, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S. 333 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 26L AND STGR 27. INSTALLED NEW SERVICEABLE WEB FLOOR PROTECTOR ANGLES 2EA (PN SH670-32040-4S) AND 1EA (PN SH670-32040-3S) IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR REXA2024010900056](https://openairdocs.org/sdr/REXA2024010900056.md): Bracket · corroded · Dec 19, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND HEAVY CORROSION ON WEB FLOOR PROTECTOR ANGLES (3EA), LOCATED BETWEEN FS 319.00 TO FS 349.00. AT SERVICE DOOR SILL AREA. INSTALLED NEW SERVICEABLE WEB FLOOR PROTECTOR ANGLES 2EA (PN SH670-32040-4S) AND 1EA (PN SH670-32040-3S) IAW CRJ900 SRM 51-42-06-001-0
- [SDR REXA2024031300261](https://openairdocs.org/sdr/REXA2024031300261.md): Bracket · cracked · Dec 18, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR, BRACKET CRACKED AT FS335, UNDER PANEL 832AB. REMOVED CRACKED PAX DOOR AFT COUNTERBALANCE BEAM. LOCATED, MATCH DRILLED, INSTALLED NEW SERVICEABLE COUNTERBALANCE MOUNT BEAM PN 601R318011-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.
- [SDR REXA2024031300260](https://openairdocs.org/sdr/REXA2024031300260.md): Beam · cracked · Dec 18, 2023 · N606LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT GAS SPRING BEAM CRACKED. REMOVED CRACKED PAX DOOR AFT COUNTERBALANCE BEAM. LOCATED, MATCH DRILLED, INSTALLED NEW SERVICEABLE COUNTERBALANCE MOUNT BEAM PN 601R318011-1 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.
- [SDR REXA2024071600539](https://openairdocs.org/sdr/REXA2024071600539.md): Floor Skin · cracked · Dec 13, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Structure
  > LH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IS CRACKED JUST O/B OF THE BRAKE ACCUMULATOR GAUGES REPAIRED LH FLOOR WEB IAW CRJ900 SRM 53-11-43-201-001-A01. MATERIAL USED FOR DOUBLER AND SHIM 2024-T3 0.040Ï¿½ PO# 5-5501, CLEAT 2024-T3 0.032Ï¿½ PO# W89584. COMPL
- [SDR REXA2024100300820](https://openairdocs.org/sdr/REXA2024100300820.md): Intercostal · corroded · Dec 11, 2023 · N606LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 (PN: 601R318067-3) IS CORRODED. REMOVED INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.LOCATED AND DRILLED NEW SERVICEABLE PART 601R318067-5 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALL
- [SDR REXA2024031300259](https://openairdocs.org/sdr/REXA2024031300259.md): Former · corroded · Dec 11, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR FORMER FS 320 FOUND CORRODED BETWEEN DD5 AND DD7. INSTALLED NEW SERVICEABLE FORMER PN 601R318032-5 IAW CRJ 900 SRM 51-40-11-001-001-A01, 52-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2024110101374](https://openairdocs.org/sdr/REXA2024110101374.md): Angle · corroded · Dec 10, 2023 · N606LR · Cndair CL6002D24 · Wing Miscellaneous Structure
  > RH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER (BLOW OUT PANEL) ANGLE CORRODED INSTALLED NEW SERVICEABLE RH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER ANGLE (P/N CC670-10338-2) IAW CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-15-001-001-A01
- [SDR REXA2024011600071](https://openairdocs.org/sdr/REXA2024011600071.md): Stringer · corroded · Dec 10, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 20R IS CORRODED BETWEEN FS 379 AND FS 477 AT APPROX. FS 453. REPLACED CORRODED SECTION OF STGR 20R BETWEEN F.S. 421 - F.S. 477 BY COMPLYING WITH ALL STEPS OF ENDEAVOR AIR EA CRJ953-15975 REV IR DATED 1/9/2024.
- [SDR REXA2024030700236](https://openairdocs.org/sdr/REXA2024030700236.md): Floorbeam · cracked · Dec 9, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RBL 12 FLIGHT COMPARTMENT FLOOR BEAM IS CRACKED AT THE FWD SIDE OF F.S. 280. REPAIRED FLIGHT COMPARTMENT FLOOR BEAM AT F.S. 280 RBL 12 IAW CRJ 900 SRM 53-11-43-201-003-A01.
- [SDR REXA2022121201047](https://openairdocs.org/sdr/REXA2022121201047.md): Stringer · corroded · Dec 9, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R IS CORRODED BETWEEN FS 280 AND FS 333 REMOVED AND REPLACED STRINGER 21R FS 280 TO 333 IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2022121201033](https://openairdocs.org/sdr/REXA2022121201033.md): Stringer · corroded · Dec 9, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R BETWEEN F.S.333 TO F.S.364 IS CORRODED REMOVED AND REPLACED STRINGER 26R FROM F.S. 333 TO F.S. 364 IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2024100300818](https://openairdocs.org/sdr/REXA2024100300818.md): Stringer Splice · corroded · Dec 8, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT STGR 24R F.S. 333 IS CORRODED. LOCATED AND DRILLED NEW STGR 24R SPLICE PN SH670-32429-4S AT FS 333 IAW CRJ900 SRM 51-40-11-001-001-A01INSTALLED STGR 24R SPLICE AT FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022121201046](https://openairdocs.org/sdr/REXA2022121201046.md): Stringer · corroded · Dec 8, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN FS 280 AND FS 333 REMOVED AND REPLACED STRINGER 26R BETWEEN FS 280 AND FS 333 IAW CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2022121201034](https://openairdocs.org/sdr/REXA2022121201034.md): Stringer · corroded · Dec 8, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L BETWEEN F.S.280 TO F.S.333 IS CORRODED. REMOVED AND REPLACED STRINGER 25L FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022121201031](https://openairdocs.org/sdr/REXA2022121201031.md): Stringer · corroded · Dec 8, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R BETWEEN F.S.379 TO F.S.333 IS CORRODED. REMOVED AND INSTALLED NEW STRINGER 21R FROM FS 333 TO FS 379 IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2024061100418](https://openairdocs.org/sdr/REXA2024061100418.md): Handle · inoperative · Dec 7, 2023 · N606LR · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR HANDLE HOUSING FAILED NDT WITH A 100% F.S.H INDICATION AROUND 1/2 THE CIRCUMFERENCE OF THE HOUSING. REMOVED AND REPLACED AVIONICS BAY DOOR HANDLE HOUSING IAW CRJ 900 SRM 51-42-21-001-001-A01
- [SDR REXA2024021600191](https://openairdocs.org/sdr/REXA2024021600191.md): Angle · corroded · Dec 7, 2023 · N606LR · Cndair CL6002D24 · Wing Miscellaneous Structure
  > LH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER (BLOW OUT PANEL) ANGLE CORRODED. MARKED WITH ORANGE TAPE. REPLACED FOR NEW SERVICEABLE LH MLG ELECTRICAL /HYDRAULICS PROTECTIVE COVER ANGLE (P/N CC670-10338-1) IAW CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-15-
- [SDR REXA2022121201032](https://openairdocs.org/sdr/REXA2022121201032.md): Stringer Splice · corroded · Dec 7, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 21R AT F.S.477 IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE ON F.S. 477 STGR 21R P/N SH670-33252-1, IAW CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022121201029](https://openairdocs.org/sdr/REXA2022121201029.md): Door Sill · corroded · Dec 7, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR LOWER SILL CORRODED BETWEEN FS1000 AND FS1047 MULTIPLE AREAS. REMOVED AND REPLACED LOWER SILL WITH PN MM670-35655-003 BETWEEN FS1000 AND FS1047 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024100300817](https://openairdocs.org/sdr/REXA2024100300817.md): Support Angle · cracked · Dec 5, 2023 · N606LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO AFT TIE DOWN SUPPORT ANGLE IS CRACKED. LOCATED AND DRILLED SERVICEABLE BEAM PN MM670-35328-003 IAW CRJ900 SRM 51-40-11-001-001-A01.INSTALLED SERVICEABLE BEAM WITH PN MM670-35328-003 AT TIE DOWN PLATE IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024012200097](https://openairdocs.org/sdr/REXA2024012200097.md): Stringer · corroded · Dec 5, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R CORRODED ON UPPER SURFACE OF ATTACHED FLANGE BETWEEN FS597.00 AND FS613.00. NO DAMAGE ALLOWED ON STR 21R BETWEEN FS 597 AND FS 613, IAW CRJ-900 SRM 53-31-03-101-003-A04, STRINGER STR21R P/N: SH690-33211-3 MUST BE REPAIR OR REPLACEMENT. FABRICATED
- [SDR REXA2024100300816](https://openairdocs.org/sdr/REXA2024100300816.md): Stringer · corroded · Dec 4, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R IS CORRODED BETWEEN FS 280 AND FS 333 LOCATED AND DRILLED NEW STGR 24R PN SH670-31212-2U FROM FS 280 TO FS 333 IAW CRJ900 SRM 51-40-11-001-001-A01INSTALLED STGR 24R FROM FS 280 TO FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01 AD 51-42-21-001-001-A01
- [SDR REXA2024110101373](https://openairdocs.org/sdr/REXA2024110101373.md): Seat Track · corroded · Dec 3, 2023 · N606LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "FLOOR SEAT TRACK AT LBL9 BETWEEN FS 349.00 AND 485.00 IS CORRODED FABRICATED REPLACEMENT LBL9 SEAT TRACK PN 670-53-00-692-1 IAW REPAIR ""B"" STEP 1A OF REO 670-53-00-589 REV -C, DATED 2022-12-19 AND INSTALLED NEW SERVICEABLE LBL9 SEAT TRACK PN 670-53-00-692-
- [SDR REXA2024012400114](https://openairdocs.org/sdr/REXA2024012400114.md): Frame · corroded · Dec 2, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 364 LOWER FRAME SECTOR IS CORRODED ON LOWER FLANGE BETWEEN STGR 26R AND STGR 27. INSTALLED NEW FS 364 SEGMENT (P/N-SH670-32090-9) THROUGH THE SKIN IAW CRJ 900 SRM 51-42-06-001-001-A01.
- [SDR REXA2024100300813](https://openairdocs.org/sdr/REXA2024100300813.md): Seat Track · corroded · Nov 29, 2023 · N606LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "CORROSION FOUND ON SEAT TRACK LBL 9 BETWEEN FS 661+32-693 FABRICATED,LOCATED AND DRILLED NEW PART P/N 670-53-00-692-1 / SH690-33405-1 IAW MHIRJ REO 670-53-00-589 REV-C DATE 2023-02-08 REPAIR ""B"" 3.B REMOVED AND REPLACED FLOOR SEAT TRACK P/N SH690-33405-1 I
- [SDR REXA2024010800051](https://openairdocs.org/sdr/REXA2024010800051.md): Frame · corroded · Nov 26, 2023 · N606LR · Cndair CL6002D24 · Fuselage Main, Frame
  > "FS 533 FRAME IS CORRODED AT STGR 17L TO 18L. FABRICATED AND DRILLED ALL REPAIR PARTS IAW CRJ900 SRM 53-00-06-201-001-A03 STEP 6E-D-G FROM 7075-0.080"" PO W91683, S1710-4, AND REPAIR FRAME SEGMENT P/N SH690-33121-5. INSTALLED A NEW SERVICEABLE FS 533 FRAME FR
- [SDR REXA2024010800049](https://openairdocs.org/sdr/REXA2024010800049.md): Bracket · cracked · Nov 26, 2023 · N606LR · Cndair CL6002D24 · Wing, Attach Fittings
  > "LH SLAT TRACK 1-3 CANISTER ATTACHMENT TAB IS CRACKED (INSIDE FUEL TANK). FABRICATED, LOCATED, DRILLED AND INSTALLED SERVICEABLE SUPPORT BRACKET P/N CC670-12942-1 IAW BOMBARDIER DWG NO: CC670-12942 REV. NC, BOMBARDIER REO 670-57-42-577 REV-- DATED 2016-12-02.

Next page: https://openairdocs.org/aircraft/N606LR/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 = 'N606LR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N606LR/reports

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