# Service difficulty reports: N136EV

A list on [N136EV](https://openairdocs.org/aircraft/N136EV.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 · 149 reports

- [SDR REXA2025091500864](https://openairdocs.org/sdr/REXA2025091500864.md): Fitting · cracked · Aug 28, 2025 · N136EV · Cndair CL6002D24 · Fuselage Main, Structure
  > IN REF TO NRC 0087: AFTER AFT HANDRAIL SUPPORT FITTINGS REMOVAL, CRACK ON PASSENGER DOOR STAIR AFT SIDE PANEL WAS FOUND. PASSENGER DOOR STAIR AFT SIDE PANEL WAS REPAIRED PER CRJ 900 SRM 52-11-04-201-004-A01
- [SDR REXA2025091500863](https://openairdocs.org/sdr/REXA2025091500863.md): Fitting · cracked · Aug 28, 2025 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > IN REF TO NRC 0087: AFTER FWD HANDRAIL SUPPORT FITTINGS REMOVAL, CRACK ON PASSENGER DOOR STAIR FWD SIDE PANEL WAS FOUND. PASSENGER DOOR STAIR FWD SIDE PANEL WAS REPAIRED PER CRJ 900 SRM 52-11-04-201-004-A01
- [SDR REXA2025091500862](https://openairdocs.org/sdr/REXA2025091500862.md): Access Panel · corroded · Aug 19, 2025 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB. CORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITH
- [SDR REXA2025091500861](https://openairdocs.org/sdr/REXA2025091500861.md): Bracket · worn · Aug 19, 2025 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > INITIAL INSPECTION: WEAR AT FWD / AFT HANDRAIL SUPPORT FITTINGS AND ALSO MISSING BUMPERS. WEAR AT FWD / AFT HANDRAIL SUPPORT FITTINGS WAS EVALUATED DUE EXESSIVE DAMAGE AND WAS REPLACED ALSO MISSING BUMPERS WAS INSTALLED PER CRJ-900 SRM 53-00-00-101-001-A01 AND
- [SDR REXA2025091500858](https://openairdocs.org/sdr/REXA2025091500858.md): Fitting · worn · Aug 15, 2025 · N136EV · Cndair CL6002D24 · Wing Miscellaneous Structure
  > WEAR ON FLAP FITTING OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2025091500857](https://openairdocs.org/sdr/REXA2025091500857.md): Support · worn · Aug 15, 2025 · N136EV · Cndair CL6002D24 · Wing Miscellaneous Structure
  > WEAR ON PLATE SUPPORT OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF FLAP STUB FAIRING 171DL AT LH WING TRAILING EDGE (ROOT WING). WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2024103001216](https://openairdocs.org/sdr/REXA2024103001216.md): Door Frame · cracked · Apr 25, 2024 · N136EV · Cndair CL6002D24 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR SH670-36600 SN SB0938 HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16488 REV IR DATED 5/8/2024.
- [SDR REXA2024103001215](https://openairdocs.org/sdr/REXA2024103001215.md): Door Frame · cracked · Apr 25, 2024 · N136EV · Cndair CL6002D24 · Emergency Exits
  > R/H FWD EMERGENCY EXIT DOOR SH670-36600 SN SB0939 HAS A VISIBLE CRACK BELOW UPPER FWD AND AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16484 REV IR DATED 5/13/2024.
- [SDR REXA2024103001214](https://openairdocs.org/sdr/REXA2024103001214.md): Door Frame · cracked · Apr 25, 2024 · N136EV · Cndair CL6002D24 · Emergency Exits
  > L/H FWD EMERGENCY EXIT DOOR SH670-36600 SN SB0940 HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-164870 REV IR DATED 5/7/2024.
- [SDR REXA2024103001213](https://openairdocs.org/sdr/REXA2024103001213.md): Lug · cracked · Apr 25, 2024 · N136EV · Cndair CL6002D24 · Emergency Exits
  > L/H AFT EMERGENCY DOOR SH670-36600 SN SB0937 HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16486 REV IR DATED 5/7/2024.
- [SDR REXA2022032200490](https://openairdocs.org/sdr/REXA2022032200490.md): Mount · chafed · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Engine Mount Section
  > LH ENGINE MOUNT YOKE FOUND TO HAVE CHAFING IN ATTACHMENT PIN LADIUS MARKED WITH RED TAPE. - REPAIRED LH ENGINE YOKE IAW MHIRJ REO 670-71-21-057 REV-- DATED 2013- AND REO 690-71-21-035 REV-- DATED 2022-03-01.
- [SDR REXA2022032200489](https://openairdocs.org/sdr/REXA2022032200489.md): Angle · cracked · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > POWER ASSIST MOTOR STIFFENING ANGLE CRACKED. - REMOVED AND REPLACED POWER ASSIST MOTOR STIFFENING ANGLE P/N: 601R317745-7 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022032200488](https://openairdocs.org/sdr/REXA2022032200488.md): Web · cracked · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CRACKED ON BOTTOM BY SUPPORT ANGLE - REMOVED ANGLES AND FITTINGS FROM UNSERVICEABLE WEB. LOCATED AND REINSTALLED SAME SERVICEABLE ANGLE AND FITTING ON SERVICEABLE WEB P/N: 601R317071-11 IAW CRJ900 SRM 51-40-11-001-001-A01 51-42-06-001-001-A01
- [SDR REXA2022032200487](https://openairdocs.org/sdr/REXA2022032200487.md): Sleeve · corroded · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR TENSION TIES BUSHINGS AND BUSHING SLEEVES CORRODED - REMOVED AND REPLACED TENSION TIE BEARINGS SLEEVE P/N MS17796-106 (2EA) AND SPACER SLEEVE P/N NAS43HT16-56 (2EA) IAW CRJ900 AMM 52-11-19-000/400-801-A01.
- [SDR REXA2022032200485](https://openairdocs.org/sdr/REXA2022032200485.md): Retainer · damaged · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND BOTTOM SEAL RETAINER P/N: 601R318722-1 DAMAGED - REPLACED BOTTOM SEAL RETAINER P/N: 601R318722-1 IAW CRJ900 SRM 51-42-06-001-001-A01 51-40-11-001-001-A01
- [SDR REXA2022032200484](https://openairdocs.org/sdr/REXA2022032200484.md): None · corroded · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND CLIP P/N: 601R319034-2 TO BE CORRODED TOWARDS THE HINGE - REPLACED CLIP P/N: 601R319034-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
- [SDR REXA2022032200474](https://openairdocs.org/sdr/REXA2022032200474.md): Frame · chafed · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FRAME, PN: MM670-36213-009, AT FS 1144 IN BETWEEN STGRS 9L & 10L HAS DAMAGE FROM HYD LINE CONTACT. - REPAIRED FARME @FS1144 BETWEEN STGR 9L & 10L IAW ENDEAVOR EA CRJ 952 12884 DATED 2-22-22 REV EA --REF JOB: 81522661 OP 525 FOR ACCUMULATOR INSTALLATION/REMOVAL
- [SDR REXA2022032200473](https://openairdocs.org/sdr/REXA2022032200473.md): Lug · damaged · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Wing Structure
  > RH AILERON HAS DAMAGE TO LUGS MARKED C AND E. - REPAIRED DAMAGE TO RH AILERON LUGS MARKED C AND E IAW BOMBARDIER REO 670-57-61-237 REV -- DATE 2017-07-25
- [SDR REXA2022032200472](https://openairdocs.org/sdr/REXA2022032200472.md): Lug · damaged · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Wing Structure
  > LH AILERON HAS DAMAGE TO LUGS MARKED D. - REPAIRED DAMAGE TO LH AILERON LUG MARKED IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25
- [SDR REXA2022032200471](https://openairdocs.org/sdr/REXA2022032200471.md): Skin · corroded · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN CORRODED AROUND PANEL CUTOUTS NUMEROUS LOCATIONS. TCI: 52-10-301 - REMOVED UNSERVICABLE PAX DOOR INNER SKIN AND INSTALLED SERVICABLE INNER SKIN IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01,51-42-21-001-001-A01, 51-40-11-001-00
- [SDR REXA2022032200470](https://openairdocs.org/sdr/REXA2022032200470.md): Web · corroded · Mar 7, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD WEB CORRODED AROUND ACCESS PANEL CUTOUTS AND NUTPLATES - REMOVED ANLGES AND FITTIGNS FROM UNSERVICABLE WEB. LOCATED AND REINSTALLED SAME SERVICEABLE ANGLE AND FITTING ON SERVICEABLE WEB P/N 601R317071-12 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42
- [SDR REXA2022032200440](https://openairdocs.org/sdr/REXA2022032200440.md): Frame · corroded · Mar 3, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 349 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 25L AND STGR 25R. - REPAIRED FRAME 349 LOWER SEGMENT STGR 25L-25R IAW ENDEAVOR EA CRJ953-12888, REV IR DATED 2/22/22.
- [SDR REXA2022032200445](https://openairdocs.org/sdr/REXA2022032200445.md): Frame · corroded · Mar 2, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS333 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 25L AND STGR 25R. - FOUND TO BE BEYOND REPAIRABLE LIMITS IAW CRJ 900 SRM 53-00-06-201-005-A01, REPAIRED FRAME IAW CRJ 900 SRM 53-00-06-201-006-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01 AND 51-21-11-001-0
- [SDR REXA2022032200438](https://openairdocs.org/sdr/REXA2022032200438.md): Angle · cracked · Feb 28, 2022 · N136EV · Cndair CL6002D24 · Vertical Stabilizer
  > LH VERTICAL STAB DRAG ANGLE HAS SUSPECTED CRACK. - REMOVED AND REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01
- [SDR REXA2022032200486](https://openairdocs.org/sdr/REXA2022032200486.md): Cleat · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND CLEAT P/N: 600-31902-269 CORRODED AT FS313.56 DD4. - REMOVED AND REPLACED CLEAT P/N 600-13902-269 AT FS 313.56 DD4 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-0A1.
- [SDR REXA2022032200483](https://openairdocs.org/sdr/REXA2022032200483.md): Angle · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > TOP ANGLE CLOSEST TO HINGE AND CLIPS CORRODED - REMOVED AND REPLACED ANGLE P/N 601R317052-1 AND CLIP (1EA) P/N 601R318058-1 AT CODDER CENTER OF PAX DOOR CLOSEST TO HINGE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022032200480](https://openairdocs.org/sdr/REXA2022032200480.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL AT DD6 CORRODED - REMOVED AND REPLACED INTERCOSTAL PN 601R318057-APO BRACKET P/N 601R31902-461 AT DD6 IAW CRJ900 SRM 51-42-06-001-001-A01 51-40-11-001-001-A01 51-42-21-001-001-A01
- [SDR REXA2022032200469](https://openairdocs.org/sdr/REXA2022032200469.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD5 IS CORRODED. - REMOVED AND REPLACED INSTERCOSTAL P/N 601R318091-5 AND BRACKET P/N 601R31902-461 AT DD5 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022032200468](https://openairdocs.org/sdr/REXA2022032200468.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 IS CORRODED. TCI: 52-10-301. - REMOVED AND REPLACED INTERCOSTAL P/N 601T318093-1 AND BRACKET P/N 601R31902-461 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 (DD4).
- [SDR REXA2022032200453](https://openairdocs.org/sdr/REXA2022032200453.md): None · none · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 581.00 AND FS 661.00+32 IS CORRODED. - REMOVED, FABBED & INSTALLED SEAT TRACK IAW CRJ 900 SRM 51-40-11-001-001-A01 & AMM 53-00-49-000/400-801-A01.
- [SDR REXA2022032200449](https://openairdocs.org/sdr/REXA2022032200449.md): None · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL BETWEEN FS 280.00 TO FS 319.00 IS CORRODED IN MULTIPLEL LOCATIONS - REMOVED AND REPLACED FLOOR SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-10-001-001-A01
- [SDR REXA2022032200448](https://openairdocs.org/sdr/REXA2022032200448.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 21L IS CORRODED BETWEEN FS310 AND FS349. TCI: 53-20-304 - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 53-21-23-101-001-A02, 51-21-06-001-001-A01, 51-21-11-001-001-A01 INSTALLED AVIONICS SHELF
- [SDR REXA2022032200447](https://openairdocs.org/sdr/REXA2022032200447.md): Angle · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVI BAY FLOORBOARD SUPPORT ANGLE ON FS 280 LOWER FRAME SEGMENT IS CORRODED. - BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-21-06-001-001-A01, 53-00-00-101-001-A01, 51-21-11-001-001-A01
- [SDR REXA2022032200444](https://openairdocs.org/sdr/REXA2022032200444.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 27R CORRODED BETWEEN FS 394 AND FS 409. - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-21-11-001-001-A01
- [SDR REXA2022032200443](https://openairdocs.org/sdr/REXA2022032200443.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 27L CORRODED BETWEEN FS 394 AND FS 409. - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-00-001-001-A01, 51-23-00-001-001-A01, 51-21-11-001-001-A01
- [SDR REXA2022032200441](https://openairdocs.org/sdr/REXA2022032200441.md): Intercostal · corroded · Feb 27, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 27L CORRODED BETWEEN FS 349 AND FS 364. - REMOVED AND REPLACED INTERCOSTAL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01 AND 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022032200481](https://openairdocs.org/sdr/REXA2022032200481.md): Intercostal · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT DD7A CORRODED - REMOVED AND REPLACED INTERCOSTAL P/N 601R318083-1 AND CUP P/N 601R318058-1 AT DD7A IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022032200479](https://openairdocs.org/sdr/REXA2022032200479.md): Intercostal · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT DD7 CORRODED - REMOVED AND REPLACED INTERCOSTAL P/N 601R318826-1 AND CUP P/N 601R318824-1 AT DD7 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022032200467](https://openairdocs.org/sdr/REXA2022032200467.md): Seat Track · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SIDE SEAT TRACK AT FS744.15-761.85 HAS MULTIPLE SPOTS OF CORROSION. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A11. PN SH690-36285-1.
- [SDR REXA2022032200466](https://openairdocs.org/sdr/REXA2022032200466.md): Seat Track · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT TRACK AT FS847+16-905 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ900 AMM 53-00-49-000/400-801-A01
- [SDR REXA2022032200465](https://openairdocs.org/sdr/REXA2022032200465.md): Seat Track · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT TRACK AT FS 785-847+16 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ900 SRM 53-00-49-201-002-A01, 51-40-11-001-001-A01 AND AMM 53-00-49-000/400-801-A11
- [SDR REXA2022032200460](https://openairdocs.org/sdr/REXA2022032200460.md): Seat Track · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT TRACK OF FS570-661+16 HAS MULTIPLE SPOTS OF CORROSION - REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A11
- [SDR REXA2022032200457](https://openairdocs.org/sdr/REXA2022032200457.md): Seat Track · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SEAT TRACK FROM FS 847+16-985 RBL 9 HAS MULTIPLE SPOTS OF CORROSION - REMOVED, FABED, AND INSTALLED SEAT TRACK F/S 847+16 - 985 @ RBL9 IAW CRJ900 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A11
- [SDR REXA2022032200451](https://openairdocs.org/sdr/REXA2022032200451.md): Seat Track · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 485.00 AND FS 581.00 IS CORRODED. - REMOVED FASTENERS & CORRECTED COUNTERSINKS & REINSTALLED FASTENERS IAW CRJ 900 SRM 51-40-11-001-001-A01 & 53-00-49-400-801 (CONFIG A11).
- [SDR REXA2022032200442](https://openairdocs.org/sdr/REXA2022032200442.md): Intercostal · corroded · Feb 26, 2022 · N136EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 27R CORRODED BETWEEN FS 349 AND FS 364. - REMOVED AND REPLACED INTERCOSTAL 27R IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2022032200475](https://openairdocs.org/sdr/REXA2022032200475.md): Crossbeam · corroded · Feb 23, 2022 · N136EV · Cndair CL6002D24 · Fuselage Main, Structure
  > FOUND LH FS 280 CROSSBEAM CORRODED AT MULTIPLE LOCATIONS. - REMOVED UNSERVICEABLE, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE PN CC670-34094J P-18. INSTALLED NEW SERVICEABLE FS 280 LH CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01,
- [SDR REXA2022032200458](https://openairdocs.org/sdr/REXA2022032200458.md): Angle · corroded · Feb 23, 2022 · N136EV · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280.00 CROSS BEAM J ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9. - REMOVED UNSERVICEABLE, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE FS 280 J ANGLE PN CC670-34095-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND 51-
- [SDR REXA2022032200446](https://openairdocs.org/sdr/REXA2022032200446.md): Stringer · corroded · Feb 23, 2022 · N136EV · Cndair CL6002D24 · Nacelle/Pylon Structure
  > STRINGER 25R IS CORRODED BETWEEN FS280 AND FS 338. - REPAIRED STRINGER IAW ENDEAVOR AIR EA CRJ953-12914.
- [SDR REXA2022032200482](https://openairdocs.org/sdr/REXA2022032200482.md): Angle · corroded · Feb 22, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > FWD SUPPORT ANGLE CORRODED. - LOCATED AND DRILLED NEW FWD FORMER SUPPORT ANGLE P/N 601R318737-3 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW SUPPORT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20.
- [SDR REXA2022032200478](https://openairdocs.org/sdr/REXA2022032200478.md): Angle · corroded · Feb 22, 2022 · N136EV · Cndair CL6002D24 · Passenger/Crew Doors
  > AFT FORMER SUPPORT ANGLE CORRODED. - LOCATED AND DRILLED NEW AFT FORMER SUPPORT ANGLE P/N 601R318732-3 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE CRJ 900 SRM 51-42-06-001-001-A01 REV 38 07/25/20.

Next page: https://openairdocs.org/aircraft/N136EV/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 = 'N136EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N136EV/reports

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