# Service difficulty reports: N605LR

A list on [N605LR](https://openairdocs.org/aircraft/N605LR.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 3 · 115 reports

- [SDR REXA2026052800854](https://openairdocs.org/sdr/REXA2026052800854.md): Web · cracked · Nov 11, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION': CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER CRJ-900
- [SDR REXA2026052800862](https://openairdocs.org/sdr/REXA2026052800862.md): Intercostal · corroded · Oct 30, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00 DUE TO EXCESIVE CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00 WAS REPLACED PER CRJ900 SRM 53-21-23-101-002-A02, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2026052800855](https://openairdocs.org/sdr/REXA2026052800855.md): Stringer · corroded · Sep 24, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON STRINGER 26RH IN STA. FS= 295 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON STRINGER 26RH IN STA. FS= 295 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CR
- [SDR REXA2026052800848](https://openairdocs.org/sdr/REXA2026052800848.md): Intercostal · corroded · Sep 23, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON INTERCOSTAL AT STGR 20LH BTW FS333.00 TO FS 349.00 INTERCOSTAL AT STGR 20LH BTW FS333.00 TO FS 349.00 WAS EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER CRJ900 SRM 51-21-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42
- [SDR REXA2026052800850](https://openairdocs.org/sdr/REXA2026052800850.md): Rub Strip · worn · Sep 21, 2025 · N605LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > OUT OF SCOPE': WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE/LH ENGINE WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE AND UPPER FORWARD CORE COWL LH ENGINE WERE REPLACED PER CRJ-900 SRM 54-23-00-201-006-A01, RUB ST
- [SDR REXA2026052800849](https://openairdocs.org/sdr/REXA2026052800849.md): Rub Strip · worn · Sep 21, 2025 · N605LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > OUT OF SCOPE': WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE/LH ENGINE WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE AND UPPER FORWARD CORE COWL LH ENGINE WERE REPLACED PER CRJ-900 SRM 54-23-00-201-006-A01, RUB STR
- [SDR REXA2026052800863](https://openairdocs.org/sdr/REXA2026052800863.md): Stringer · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > IN REFERENCE TO NRC 00604: CORROSION ON STRINGER 19RH, 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT. (E/E) SUMMARY OF NRC 677 CORROSION ON STRINGER 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED O
- [SDR REXA2026052800861](https://openairdocs.org/sdr/REXA2026052800861.md): Hinge · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON BOTH HINGES OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (2 EAS) SUMMARY: BOTH HINGES OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (2 EAS) WERE REMOVED PER CRJ900 AMM 52-45-01 AND INSTALLED PER CRJ900 AMM 52-45-01 AND FABRICATED HINGE OF
- [SDR REXA2026052800860](https://openairdocs.org/sdr/REXA2026052800860.md): Frame · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 847.00+32 BTWN STGR 25LH TO 25RH CORROSION ON FRAME FS 847.00+32 BTWN STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-51-526 REV --
- [SDR REXA2026052800859](https://openairdocs.org/sdr/REXA2026052800859.md): Stringer · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > IN REFERENCE TO NRC 00604: CORROSION ON STRINGER 19RH, 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT. (E/E) SUMMARY OF NRC 677 CORROSION ON STRINGER 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED O
- [SDR REXA2026052800858](https://openairdocs.org/sdr/REXA2026052800858.md): Stringer · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN REFERENCE TO NRC 00604: CORROSION ON STRINGER 19RH, 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT. (E/E) SUMMARY OF NRC 677 CORROSION ON STRINGER 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED O
- [SDR REXA2026052800857](https://openairdocs.org/sdr/REXA2026052800857.md): Hinge · cracked · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACKED FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT REPLACED IAW SRM 51-42-06-001-001-A01 (FWD & AFT HINGES) WERE MANUFACTURED PER EA NO. CRJ953-20605 REV IR
- [SDR REXA2026052800856](https://openairdocs.org/sdr/REXA2026052800856.md): Hinge · cracked · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACKED FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 (FWD & AFT HINGES) WERE MANUFACTURED PER EA NO. CRJ953-20605
- [SDR REXA2026052800853](https://openairdocs.org/sdr/REXA2026052800853.md): Bracket · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. CORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. WAS REMOVED PER CRJ900 SR
- [SDR REXA2026052800852](https://openairdocs.org/sdr/REXA2026052800852.md): Fitting · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON CLOSING FITTINGS (2EAS) BTW FS 314.00 AND FS 342.00 AND STGR 18L. CORROSION ON CLOSING FITTINGS (2EAS) BTW FS 314.00 AND FS 342.00 AND STGR 18L WERE REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, CLOSING FITTINGS FWD WAS EVALUAT
- [SDR REXA2026052800851](https://openairdocs.org/sdr/REXA2026052800851.md): Frame · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Frame
  > INITIAL INSPECTION: CORROSION ON FRAME FS= 310.00 BETWEEN STRG 24LH TO 24RH AT MAIN AVIONIC COMPARTMENT DUE TO EXCESIVE CORROSION ON FRAME IN STA. FS= 310 BETWEEN STRG 25RH TO STRG 24LH AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-21-06-101-0
- [SDR REXA2026052800845](https://openairdocs.org/sdr/REXA2026052800845.md): Drag Angle · cracked · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > INITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5
- [SDR REXA2026052800844](https://openairdocs.org/sdr/REXA2026052800844.md): Angle · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. CORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. WAS REMOVED PER CRJ900 SR
- [SDR REXA2026052800843](https://openairdocs.org/sdr/REXA2026052800843.md): Angle · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD, MID AND AFT ANGLE CAP (3 EAS) AT PASSENGER DOOR SURROUND STRUCTURE BTW FS 310.00 TO FS 349.00 OVER STGR 18L. DUE TO EXCESSIVE CORROSION ON MID AND AFT ANGLE CAP WERE EVALUATED OUT LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 51-21-06-001-00
- [SDR REXA2026052800842](https://openairdocs.org/sdr/REXA2026052800842.md): Angle · corroded · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD, MID AND AFT ANGLE CAP (3 EAS) AT PASSENGER DOOR SURROUND STRUCTURE BTW FS 310.00 TO FS 349.00 OVER STGR 18L. DUE TO EXCESSIVE CORROSION ON MID AND AFT ANGLE CAP WERE EVALUATED OUT LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 51-21-06-001-00
- [SDR REXA2026052800840](https://openairdocs.org/sdr/REXA2026052800840.md): Drag Angle · cracked · Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > INITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00) CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67
- [SDR REXA2026052800841](https://openairdocs.org/sdr/REXA2026052800841.md): Bracket · corroded · Sep 16, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON BRACKET OF THE AFT LAV WASTE LEVEL INDICATOR LIGHT (PRESS-TO-TEST INDICATOR). CORROSION ON BRACKET OF THE AFT LAV WASTE LEVEL INDICATOR LIGHT (PRESS-TO-TEST INDICATOR) WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATE
- [SDR REXA2026052800846](https://openairdocs.org/sdr/REXA2026052800846.md): Door Frame · cracked · Sep 12, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON UPPER FRAME AT AFT RH/LH & FWD RH OVERWING EMERGENCY EXIT DOOR. UPPER FRAME AT AFT RH/LH & FWD RH OVERWING EMERGENCY EXIT DOOR WERE REPAIRED PER REO 670-52-21-103 REV. - -
- [SDR REXA2024090600686](https://openairdocs.org/sdr/REXA2024090600686.md): Battery Pack · inoperative · Sep 3, 2024 · N605LR · Cndair CL6002D24 · Emergency Lighting
  > CENTER CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CENTER CEILING EMERGENCY LIGHT BATTERY PACK AND CHARGER IAW AMM 33-51-17. OPS CHECK GOOD. (PS 36). BATTERY PACK P/N: 2013-1ASMI
- [SDR REXA2022120202667](https://openairdocs.org/sdr/REXA2022120202667.md): Floor Support · corroded · Nov 30, 2022 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL IS CORRODED BETWEEN F.S. 280 TO F.S. 333. REMOVED AND REPLACED RH FLOOR SILL PN:SH670-32172-11 IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022120202666](https://openairdocs.org/sdr/REXA2022120202666.md): Support Angle · corroded · Nov 30, 2022 · N605LR · Cndair CL6002D24 · Galley Doors
  > GALLEY DOOR STEP PLATE AFT TWO SUPPORT ANGLES ARE CORRODED. REMOVED AND REPLACED THE TWO SUPPORT ANGLES IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022113002633](https://openairdocs.org/sdr/REXA2022113002633.md): Angle · corroded · Nov 28, 2022 · N605LR · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DOOR ANGLE IS CRACKED MIDDLE POINT OF DOOR. COMPLIED WITH SRM 52-11-01-201-002-A01.
- [SDR REXA2022113002604](https://openairdocs.org/sdr/REXA2022113002604.md): Door Sill · corroded · Nov 28, 2022 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED CORRODED LOWER SILL ANGLE WITH NEW IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022113002605](https://openairdocs.org/sdr/REXA2022113002605.md): Angle · corroded · Nov 27, 2022 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER SILL ANGLE IS CORRODED. REMOVED UPPER SILL (KICK PLATE) AT PAX DOOR IAW CRJ-900 SRM 51-41-02-001-001-A01. INSTALLED NEW PAX DOOR UPPER SILL ANGLE IAW SRM 51-42-06-001-001-A01
- [SDR REXA2022052601036](https://openairdocs.org/sdr/REXA2022052601036.md): Light · missing · May 22, 2022 · N605LR · Cndair CL6002D24 · Emergency Lighting
  > FOUND FLOOR LIGHTING MISSING AT 13 D/C INSTALLED FLOOR LIGHTING IAW CMM 33-51-07
- [SDR REXA2020103000733](https://openairdocs.org/sdr/REXA2020103000733.md): Trunnion · damaged · Oct 25, 2020 · N605LR · Cndair CL6002D24 · Wing, Landing Gear Attach Fittings
  > LT MLG TRUNNION HAS TOOLING GOUGES ON INNER SURFACE BETWEEN HOLES 5 AND 11. SIX DISCREPANT AREAS, LARGEST APPROXIMATELY.250L Z.010D. C/W MHIRJ REO 690-57-21-3672, REV- DATED 10/22/20.
- [SDR REXA2019021000150](https://openairdocs.org/sdr/REXA2019021000150.md): Seat Track · corroded · Feb 10, 2019 · N605LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS IN SECTIONS [FS=785 TO FS= 847+16, STR 15L] [FS=847+16 TO FS=913, STR 15L] AT PAX CABIN. SEAT RAILS WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2019020500145](https://openairdocs.org/sdr/REXA2019020500145.md): Stringer Splice · corroded · Feb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE 25L AND 25R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. CORROSION ON STRINGER SPLICE WAS REMOVED PER SRM 51-21-06-001-001-A01 ITEM 5. REWORKED AREA ON STRINGER SPLICE 25L WAS MEASURE AND ORIGINAL THIC
- [SDR REXA2019020500143](https://openairdocs.org/sdr/REXA2019020500143.md): Stringer · corroded · Feb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26L AND 26R IN STA FS= 295 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. STRINGER REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.
- [SDR REXA2019020500142](https://openairdocs.org/sdr/REXA2019020500142.md): Stringer · corroded · Feb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 26L AND 26R IN STA FS= 339 TO FS= 364 AT MAIN AVIONIC COMPARTMENT. CORROSION LEVEL 2. CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 ITEM 5. STRINGER 26R WAS MEASURE ORIGINAL THICKNESS IS 0.050" AND MAXIMUM DEPTH REMOVED IS 0.012" TH
- [SDR REXA2019020500141](https://openairdocs.org/sdr/REXA2019020500141.md): Stringer · corroded · Feb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 24R IN STA FS= 295 TO FS=333 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. STRINGER WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.
- [SDR REXA2019013000146](https://openairdocs.org/sdr/REXA2019013000146.md): Stringer Splice · corroded · Jan 30, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE 26L AND 26R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. CORROSION ON STRINGER SPLICE WAS REMOVED PER SRM 51-21-06-001-001-A01 PAR 5D, REWORKED AREAS ON STRINGER SPLICE, MEASURE AND MAXIMUM DEPTH REMOV
- [SDR REXA2019012700149](https://openairdocs.org/sdr/REXA2019012700149.md): Seat Track · corroded · Jan 27, 2019 · N605LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAILS IN SECTIONS [FS= 485 TO FS= 581, 9RBL] [FS=581 TO FS=661+32, 9RBL] [FS=661+32 TO FS=693, 9 RBL] [FS=693 TO FS=830, 9LBL/9RBL] AT PAX CABIN. FLOOR SEAT RAILS WERE REPLACED PER AMM 53-00-49.
- [SDR REXA2019012500148](https://openairdocs.org/sdr/REXA2019012500148.md): Seat Track · corroded · Jan 25, 2019 · N605LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SIDE SEAT RAILS IN SECTIONS [FS= 485 TO FS= 572, STR 15L/R] [FS= 572 TO FS= 661+16, STR 15L/R] [FS= 661+16 TO FS= 661+90, STR 15L] AT PAX CABIN. SIDE SEAT RAILS AT PAX CABIN WERE REPLACED FOR A NEW ONES PER AMM 53-00-49.
- [SDR REXA2018080300668](https://openairdocs.org/sdr/REXA2018080300668.md): Light · inoperative · Aug 1, 2018 · N605LR · Cndair CL6002D24 · Emergency Lighting
  > RT OVERWING EXTERIOR EMERGENCY LIGHT (FWD) INOP. R&R RT FWD OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-51-15. OPS CHECK GOOD.
- [SDR REXA2018070600612](https://openairdocs.org/sdr/REXA2018070600612.md): Knob · missing · Jul 6, 2018 · N605LR · Cndair CL6002D24 · Emergency Equipment
  > MEGAPHONE VOLUME KNOB MISSING. REMOVED AND REPLACED MEGAPHONE IAW AMM 25-61-14. PERFORMED OPS TEST. OPS TEST GOOD. A/C OK FOR SVC.
- [SDR REXA2018052700423](https://openairdocs.org/sdr/REXA2018052700423.md): Battery · discharged · May 27, 2018 · N605LR · Cndair CL6002D24 · Emergency Lighting
  > DURING LINE CHECK FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY ASSY IAW AMM 33-51-17 OPS CHECK GOOD LIGHTS WORK P/N ON 2013-1A S/N ON 119621, P/N OFF AD-2013-1A S/N OFF 105626.
- [SDR REXA2018012100042](https://openairdocs.org/sdr/REXA2018012100042.md): Light · missing · Jan 21, 2018 · N605LR · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT STRIP MISSING, NEXT TO 1A SEAT. REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-51-01.
- [SDR REXA2018010300006](https://openairdocs.org/sdr/REXA2018010300006.md): Seal · broken · Jan 3, 2018 · N605LR · Cndair CL6002D24 · Emergency Equipment
  > EMK KIT SEAL BROKEN. REMOVED AND REPLACED EMK KIT IAW AMM 25-61-04.
- [SDR REXA2017082000896](https://openairdocs.org/sdr/REXA2017082000896.md): Seal · missing · Aug 20, 2017 · N605LR · Cndair CL6002D24 · Emergency Equipment
  > SEAL MISSING ON FWD FA PBE. INSTALLED A NEW SEAL ON FWD FA PBE.
- [SDR REXA2017073100844](https://openairdocs.org/sdr/REXA2017073100844.md): Pbe · unserviceable · Jul 31, 2017 · N605LR · Cndair CL6002D24 · Portable Oxygen System
  > FLIGHT DECK PBE OTS SOFT TO THE TOUCH HAS LOST VACCUM SEAL. R&R CAPT PBE IAW AMM 35-31-06.
- [SDR REXA2017052600643](https://openairdocs.org/sdr/REXA2017052600643.md): Flashlight · inoperative · May 26, 2017 · N605LR · Cndair CL6002D24 · Emergency Equipment
  > AFT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW CMM 25-60-02, OPS CHECKED GOOD. "
- [SDR REXA2017031200405](https://openairdocs.org/sdr/REXA2017031200405.md): Light · burned out · Mar 12, 2017 · N605LR · Cndair CL6002D24 · Flight Compartment Lighting
  > INTERMITTENT FUMES IN FLIGHTDECK ONLY. CAN ONLY DESCRIBE IT AS HOT ELECTRICAL APPLIANCE SMELL, ON FINAL CRUISE INTO DESCENT. COMPLIED WITH FIM 21-21-00. RAN ENGINES AS WELL 21-00-00. NO SMELL REPORTED. ALL INDICATIONS REPORTED NORMAL. A/C OK FOR SVC. CONFIRMED
- [SDR REXA2017011700047](https://openairdocs.org/sdr/REXA2017011700047.md): Flashlight Assy · inoperative · Jan 17, 2017 · N605LR · Cndair CL6002D24 · Emergency Equipment
  > COPILOT`S FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT AND HOLDER IAW AMM 25-61-02. OP CHECKED GOOD IAW AMM 25-61-00.
- [SDR REXA2017010600010](https://openairdocs.org/sdr/REXA2017010600010.md): Lamp · inoperative · Jan 6, 2017 · N605LR · Cndair CL6002D24 · Emergency Lighting
  > FORWARD LEFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-15. OPSCHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N605LR/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 = 'N605LR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N605LR/reports

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