# Service difficulty reports: N901EV

A list on [N901EV](https://openairdocs.org/aircraft/N901EV.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 · 167 reports

- [SDR SWIA2018122145379](https://openairdocs.org/sdr/SWIA2018122145379.md): Bracket · bent · Dec 21, 2018 · N901EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > RETURN TO FIELD AFTER NOSE GEAR WOULD NOT RETRACT. (FLT#5714) FO: 12/21/2018 CLOSED NLG PROX SENSOR BENT. REMOVED AND REPLACE NLG PROX BRACKET IAW CMM AND AMM. PERFORMED SEVERAL GEAR SWINGS IAW AMM. OPS CHECK GOOD.
- [SDR SWIA2018060144742](https://openairdocs.org/sdr/SWIA2018060144742.md): Fairing · chafed · May 6, 2018 · N901EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP STUB FAIRING CHAFED. REPLACED THESTUB FARING IAW SRM. NO DEFECTS NOTED.
- [SDR SWIA2018060144741](https://openairdocs.org/sdr/SWIA2018060144741.md): Doubler · dented · May 2, 2018 · N901EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENTS FOUND ON THE DOUBLER ON THE RT AFT FUSELAGE AFT OF LOW PRESSURE AIR SERVICE DOOR. REMOVED AND REPLACED THE DOUBLER IAW REO.
- [SDR SWIA2018060144740](https://openairdocs.org/sdr/SWIA2018060144740.md): Floorbeam · corroded · May 2, 2018 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED ON THE UPPER CAP, RBL 27, BS 559. REMOVED AND REPLACED THE UPPER CAP IAW REO.
- [SDR SWIA2018060144739](https://openairdocs.org/sdr/SWIA2018060144739.md): Floorbeam · corroded · May 2, 2018 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED ON THE UPPER CAP, RBL 9, BS 559. REMOVED AND REPLACED THE CORRODED UPPER CAP IAW REO.
- [SDR SWIA2018060144738](https://openairdocs.org/sdr/SWIA2018060144738.md): Skin · dented · May 1, 2018 · N901EV · Cndair CL6002B19 · Ailerons
  > LT AILERON, TOP DENTED. CONTOURED THE AILERON SKIN IAW REO.
- [SDR SWIA2018060144737](https://openairdocs.org/sdr/SWIA2018060144737.md): Skin · dented · Apr 28, 2018 · N901EV · Cndair CL6002B19 · Spoilers
  > MULTIPLE DENTS ON THE UPPER SKIN PANEL OF LT INBD FLIGHT SPOILER. REPAIRED MULTIPLE DENTS ON THE LT INBD FLIGHT SPOILER IAW REO.
- [SDR SWIA201744082](https://openairdocs.org/sdr/SWIA201744082.md): Bracket · crushed · Dec 21, 2017 · N901EV · Cndair CL6002B19 · Nose/Tail Landing Gear
  > GEAR DISAGREE WARNING. REPLACED BRACKET ON NOSE GEAR SMASHED BY TOWBAR STRAP. OPS CHECKED GOOD.
- [SDR SWIA201743651](https://openairdocs.org/sdr/SWIA201743651.md): Bracket · bent · Aug 23, 2017 · N901EV · Cndair CL6002B19 · Main Landing Gear Attach Section
  > GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED THE NLG PROXIMITY SENSOR BRACKET IAW AMM. ALL INDICATIONS NORMAL.
- [SDR SWIA201743238](https://openairdocs.org/sdr/SWIA201743238.md): Servo Valve · malfunctioned · Apr 27, 2017 · N901EV · Cndair CL6002B19 · Landing Gear Steering System
  > NOSE WHEEL STEERING INOPERATIVE CAUTION ENROUTE. REMOVED AND REPLACED ELECTRO HYD SERVO VALVE IAW AMM. OK FOR SERVICE.
- [SDR ASOA2016041914720](https://openairdocs.org/sdr/ASOA2016041914720.md): Battery Pack · discharged · Apr 19, 2016 · N901EV · Cndair CL6002B19 · Emergency Lighting
  > FORWARD EMERGENCY FLOOR LIGHT AND EXIT SIGN ARE INOPERATIVE. R & R ELECTRICAL CONNECTOR IAW ESPM 20-11-00 20-17-10 ON WIRES LY6022 AND LY32A22. R & R EMERGENCY LIGHTS BATTERY NR 2 PACK IAW AMM 33-51-04-400-801, 33-51-04-000-801, IPC 33-51-04, ITEM 17. OPS T
- [SDR ASOA2016041414719](https://openairdocs.org/sdr/ASOA2016041414719.md): Structure · cracked · Apr 14, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CENTER LT LOWER CLIP AT 202 PRESSURE BULKHEAD IS CRACKED. REMOVED LT & RT LOWER CENTER POST CLIPS AT 202 PRESSURE BULKHEAD IAW SRM 51-42-21-00. LOCATED, DRILLED AND INSTALLED NEW LT & RT LOWER CENTER POST CLIPS AT 202 PRESSURE BULKHEAD IAW SRM 51-40-11 AND 5
- [SDR ASOA2016041114718](https://openairdocs.org/sdr/ASOA2016041114718.md): Skin · damaged · Apr 11, 2016 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > WHILE PERFORMING REO 601R-57-21-130, FOUND 1 EA OVERSIZE HOLE ON LT WING PLANK. RECEIVED AND COMPLIED WITH REO 601R-57-21-2436 AND ECTC 601R-57-21-2436.
- [SDR ASOA2016040714721](https://openairdocs.org/sdr/ASOA2016040714721.md): Shim · shifted · Apr 7, 2016 · N901EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > REFER TO EO 600-53-2650003, LT AND RT MLG SIDE BRACE FITTING BRACKET SHIMS ARE MIGRATED. COMPLIED WITH PERMANENT REPAIR IAW EC/TC REO 601R-53-41-101-01.
- [SDR ASOA2016040614717](https://openairdocs.org/sdr/ASOA2016040614717.md): Floor Support · corroded · Apr 6, 2016 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LBL 42.5 FLOOR SILL AT FS 559+32. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV, DATED 5/22/2013 AS WRITTEN.
- [SDR ASOA2016040614710](https://openairdocs.org/sdr/ASOA2016040614710.md): Floor Support · corroded · Apr 6, 2016 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AROUND 2 NUTPLATES ON RT FLOOR SILL. RBL 42.5 AND BETWEEN FS 559+32 TO 559+48. CORROSION AROUND 2 NUTPLATES ON RT FLOOR SILL. RBL 42.5 AND BETWEEN FS 559+32 TO 559+48. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV. DATED
- [SDR ASOA2016040414716](https://openairdocs.org/sdr/ASOA2016040414716.md): Battery Pack · discharged · Apr 4, 2016 · N901EV · Cndair CL6002B19 · Emergency Lighting
  > NR 2 BATTERY PACK INSIDE CABIN FOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY LIGHTS BATTER PACK IAW AMM 33-51-04-000-801/33-51-04-400-801, IPC 33-51-04, FIG 1, ITEM 17. R & R NR 2 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-04-000-801/33-51-04-400-801
- [SDR ASOA2016040414709](https://openairdocs.org/sdr/ASOA2016040414709.md): Floorbeam · corroded · Apr 4, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AROUND FLOORBOARD SCREW HOLE ON RBL9 AND AT FS 409+40. REMOVED CORROSION AT FS 409+40, RBL 9 INBD SIDE IAW SRM 51-21-06, AND FOUND TO HAVE COMPLETE MATERIAL LOSS. REPAIR FLOORBEAM SUPPORT STRUCTURE IAW SRM 53-00-43. REPAIRED FLOORBEAM AT 409+40 IAW
- [SDR ASOA2016040414708](https://openairdocs.org/sdr/ASOA2016040414708.md): Seat Track · corroded · Apr 4, 2016 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL SEGMENT ON RBL 9 AND BETWEEN FS 394 TO FS 409+112 CORRODED OUT OF LIMITS. FABRCIATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 394 TO FS 409+112, RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRCIATED SEAT RAIL AT RBL 9 F
- [SDR ASOA2016040414707](https://openairdocs.org/sdr/ASOA2016040414707.md): Bracket · corroded · Apr 4, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BOTTOM CORNER OF SERVICE DOOR CUTOUT AT FS 319.70, STR 17R AND RBL42 CORRODED. LOWER FRAME BRACKET AT FS 319.70 CORRODED OUT OF LIMITS IAW SRM 53-00-00. R & R BRACKET AT FS 319.70 IAW SRM 51-40-11 AND 51-42-21.
- [SDR ASOA2016040414706](https://openairdocs.org/sdr/ASOA2016040414706.md): Placard · cracked · Apr 4, 2016 · N901EV · Cndair CL6002B19 · Placards and Markings
  > SERVICE DOOR INNER OPEN/CLOSE HANDLE PHOTOLUMINESCENT "EXIT" PLASTIC PLACARD CRACKED. REMOVED SERVICE DOOR INNER PHOTOLUMINCENT "EXIT" PLACARD BY REMOVING 2 SCREWS WITH A SCREW DRIVER. INSTALLED A SERVICABLE EXIT PLACARD IAW AMM 20-21-00-910-801.
- [SDR ASOA2016033114715](https://openairdocs.org/sdr/ASOA2016033114715.md): Skin · dented · Mar 31, 2016 · N901EV · Cndair CL6002B19 · Trailing Edge Flaps
  > DENT ON LT FLAP LOWER SKIN OTBD OF OTBD HINGE. REPAIRED IAW SRM 57-52-00 TO LT FLAP LWR SKIN OTBD OF OTBD HINGE AREA. RECEIVED AND COMPLIED WITH EC/TC EO 600-57-0476.
- [SDR ASOA2016033114714](https://openairdocs.org/sdr/ASOA2016033114714.md): Skin · cracked · Mar 31, 2016 · N901EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FWD FUSELAGE SKIN CRACKED AT LT FWD HYDRAULIC BAY DOOR SURROUND JUST BELOW LT AFT LATCH. REMOVED CRACKED SKIN AT LT FORWARD HYD BAY DOOR SURROUND IAW SRM 51-42-06 & 51-42-13. INSTALLED NEW SKIN AT LT FWD HYDRAULIC BAY IAW SRM 51-42-06 & 51-42-13 & DWG 600-370
- [SDR ASOA2016033114690](https://openairdocs.org/sdr/ASOA2016033114690.md): Angle · cracked · Mar 31, 2016 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 625 ANGLE CRACKE. R & R THE ANGLE IAW SRM 51-42-21-00.
- [SDR ASOA2016033114689](https://openairdocs.org/sdr/ASOA2016033114689.md): Handle · lack of lube · Mar 31, 2016 · N901EV · Cndair CL6002B19 · Emergency Exits
  > RT OVERWING EMERGENCY EXIT HANDLE FAILS OPS FORCE CHECK. PERFORMED LUBRICATION OF THE RT OVERWING EMERGENCY EXIT HANDLE IAW AMM 12-20-52-640-802, FUNCTIONAL TEST OF HANDLE GOOD REF AMM 52-21-00-720-801.
- [SDR ASOA2016012414390](https://openairdocs.org/sdr/ASOA2016012414390.md): Skin · cracked · Jan 24, 2016 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK FOUND AT RT LOWER WING PLANK, WS 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-131. REMOVED UPPER PIE PANEL IAW SRM 51-42-06 & 51-42-13. INSTALLED UPPER PIE PANEL IAW CRJ 200 SRM 51-42-06, 51-42-13. COMPLIED WITH ECTC REO 601R-5
- [SDR ASOA2016012414389](https://openairdocs.org/sdr/ASOA2016012414389.md): Skin · cracked · Jan 24, 2016 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK FOUND AT LT LOWER WING PLANK WS 148.019 CRACK LENGTH IS.7170. COMPLIED WITH ECTC REO 601R-57-21-130 AND REO 601R-57-21-131. REMOVED UPPER AND LOWER PIE SKIN PANELS IAW SRM 51-42-06 AND 51-42-15 AND 511-42-21. INSTALLED PIE PANELS IAW SRM 51-41-02 AND
- [SDR ASOA2015050812775](https://openairdocs.org/sdr/ASOA2015050812775.md): Lens · missing · May 5, 2015 · N901EV · Cndair CL6002B19 · Emergency Lighting
  > WARDROBE LOWER EMERGENCY LIGHT COVER MISSING. REPLACED WARDROBE LOWER EMERGENCY LIGHT LENS COVER IAW AMM 33-51-19.
- [SDR ASOA2014101711436](https://openairdocs.org/sdr/ASOA2014101711436.md): Unknown · odor · Oct 13, 2014 · N901EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WILL NOT OPEN AND ELECTRICAL ODOR. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-08. OPS CHECK IS GOOD. PERFORMED INSPECTION OF DOOR ASSIST MOTOR IAW AMM 52-11-08. NO DEFECTS ARE NOTED AT THIS TIME, DOOR OPERATES CORRECTLY. ACFT IS OK FOR SERVI
- [SDR ASOA2014090511182](https://openairdocs.org/sdr/ASOA2014090511182.md): Fuel Sys · malfunctioned · Sep 2, 2014 · N901EV · Cndair CL6002B19 · Aircraft Fuel Distribution System
  > 400 LB IMBALANCE DURING CLIMBOUT, LT TANK, DURING FLIGHT, LEFT TANK IMBALANCE INCREASED TO AROUND 900 LBS WITH PUMPS WORKING, FOLLOWED QRH, DIVERTED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED OPS CHECK OF FUEL TRANSFER EJECTOR PUMP IAW AMM 28
- [SDR ASOA2014042910439](https://openairdocs.org/sdr/ASOA2014042910439.md): Connector · corroded · Apr 4, 2014 · N901EV · Cndair CL6002B19 · Light System Wiring
  > CONNECTOR FOR LT FWD FUSELAGE EMERGENCY LIGHT IS CORRODED. R & R CONNECTOR IAW ESPM 20-17-10 AND WIRING DIAGRAM MANUAL 33-52-00. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.
- [SDR ASOA2014042910438](https://openairdocs.org/sdr/ASOA2014042910438.md): Access Panel · cracked · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL ACCESS PANEL 650EB HAS 2 INDICATIONS ON THE OTBD FWD & AFT SIDES 50 PERCENT FCH FAILED NDT. PERFORMED ROTOPEEN IAW SRM 51-24-11 IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2014042910437](https://openairdocs.org/sdr/ASOA2014042910437.md): Access Panel · cracked · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL ACCESS PANEL 550DB HAS 1 INDICATIION ON THE FWD, INBD SIDE 50 PERCENT FCH FAILED NDT. PERFORMED ROTOPEEN IAW SRM 51-24-11 REO 601R-57-21-030, REV L.
- [SDR ASOA2014042910436](https://openairdocs.org/sdr/ASOA2014042910436.md): Access Panel · cracked · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT FUEL ACCESS PANEL 540DB HAS ONE INDICATION ON THE INBD SIDE 60 PERCENT FCH FAILED NDT. COMPLIED WITH REO 601R-57-21-030. PERFORMED ROTOPEEN IAW SRM 51-24-11 IAW REO 601R-57-21-030, REV L.
- [SDR ASOA2014042910435](https://openairdocs.org/sdr/ASOA2014042910435.md): Vertical Beam · cracked · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, VERTICAL BEAM IS CRACKED AT RBL 27 INBD SIDE BOTTOM FASTENER HOLE. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056, REV F.
- [SDR ASOA2014042910434](https://openairdocs.org/sdr/ASOA2014042910434.md): Vertical Beam · cracked · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, VERTICAL BEAM IS CRACKED AT RBL 36 INBD SIDE BOTTOM FASTENER HOLE. C/W REO 601R-53-41-189 AT INBD SIDE OF RBL 36, VERTICAL POST AT FS 409+128. C/W REO 601R-53-41-189 AT INBD SIDE OF RBL 36 VERTICAL POST AT FS 409+128. C/W EC/TC REO 601R-53-41-18
- [SDR ASOA2014042910433](https://openairdocs.org/sdr/ASOA2014042910433.md): Skin · cracked · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND LT AFT DRAIN VALVE HOLE INBD SIDE AFT LOWER PLANK BETWEEN STR 7 AND 5 MULTIPLE INDICATIONS APPROX.5" IN LENGTH 70 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EA 25-2014-113. EA 25-2014-113 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTE
- [SDR ASOA2014042910432](https://openairdocs.org/sdr/ASOA2014042910432.md): Bulkhead · damaged · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 9.50 REQUIRES REPAIR. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO LBL 9.50 IAW REO 601R-53-61-5250 & REO 601R-53-6
- [SDR ASOA2014042910431](https://openairdocs.org/sdr/ASOA2014042910431.md): Bulkhead · damaged · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 36.20. REQUIRES REPAIR. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO LBL 36.2 IAW REO 601R-53-61-5250 & REO 601
- [SDR ASOA2014042910430](https://openairdocs.org/sdr/ASOA2014042910430.md): Bulkhead · unknown · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00, BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, RBL 27.50. REQUIRES REPAIR. C/W REO 601R-53-61-5250, P1 AT RBL 27.5. ADDED WEIGHT OF REPAIR PARTS & FIELD FASTENERS IS 4.10 LBS. C/W REO 601R-53-61-5250, REV. RECEIVED AND VERIFIED FINAL REO 6
- [SDR ASOA2014042910429](https://openairdocs.org/sdr/ASOA2014042910429.md): Bulkhead · unknown · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00, BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 27.50 REQUIRES REPAIR. REMOVED ANGLE 601R36008-39, FS 621, BULKHEAD AFT SIDE LBL 27.50 IAW SRM 51-42-06 AND 51-42-21. INSTALLED ANGLE 601R36008-39 AFT SIDE OF FS 621, BULKHEAD LBL 27.50 IAW
- [SDR ASOA2014042910428](https://openairdocs.org/sdr/ASOA2014042910428.md): Bulkhead · unknown · Apr 2, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 18.00. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS AND FINAL REAMED ALL HOLES FOR REPAIR TO LBL 18 IAW REO:601R-53-61-5250. PERFORMED CUT ON BULKHEAD
- [SDR ASOA2014042910427](https://openairdocs.org/sdr/ASOA2014042910427.md): Bulkhead Web · cracked · Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROXIMATELY.5" IN LENGTH, 100 PERCENT FSH, FAILED NDT INSPECTION. REMOVED CARGO COMPARTMENT DOOR FOR ACCESS IAW AMM 52-31-00-000-801. REMOVED AFT CARGO BALANCE SPRING BOX IAW AMM 5
- [SDR ASOA2014042910426](https://openairdocs.org/sdr/ASOA2014042910426.md): Bulkhead Web · cracked · Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 112-WL 107.5 APPROX 4.5" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. REMOVED STIFFENER ANGLE FROM FS 621.00, BULKHEAD AT WL 120.43 IAW SRM 51-42-06. INSTALLED STIFFENER ANGLE IAW CJR
- [SDR ASOA2014042910425](https://openairdocs.org/sdr/ASOA2014042910425.md): Bulkhead Web · corroded · Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB, RBL 9.50, WL 103 HAS INDICATION NOTED APPROX 1.0" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. LOCATED AND DRILLED IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO RBL 9.5 IAW R
- [SDR ASOA2014042910424](https://openairdocs.org/sdr/ASOA2014042910424.md): Bulkhead Web · cracked · Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB RBL 18.00, WL 107 HAS INDICATION NOTED APPROX 1.0" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. PERFORMED CUTOUT OF BULKHEAD WEB IAW REO: 601R-53-61-5250. COMPLIED WITH REO:601R-53-61-5250 IAW NDTM PT 1 51-20-06. C/W RE
- [SDR ASOA2014042910423](https://openairdocs.org/sdr/ASOA2014042910423.md): Bulkhead Web · cracked · Apr 1, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB, RBL 36.20, WL 82-WL 85 HAS INDICATIONS NOTED APPROX 3.0" IN LENGTH, 70 PERCENT FSH, FAILED NDT INSPECTION. LOCATED AND DRILLED REPAIR IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO
- [SDR ASOA2014042910422](https://openairdocs.org/sdr/ASOA2014042910422.md): Floorbeam · corroded · Mar 31, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM CAP AT FS 589.00, RBL 27. REMOVED DAMAGED CAP IAW SRM 51-42-06. INSTALLED CAP IAW SRM 51-40-11, 51-42-06 AND 51-42-15.
- [SDR ASOA2014042910421](https://openairdocs.org/sdr/ASOA2014042910421.md): Attach Angle · cracked · Mar 30, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STRINGER 3L FWD UPPER AND LOWER ATTACH ANGLES CRACKED JUST AFT OF FS 280 BULKHEAD. REMOVED 2 ATTACH ANGLES AT FS 280 STGR 3L IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ATTACH ANGLES AT FS 280, STGR 3L IAW SRM 51-42-06 AND 51-42-02.
- [SDR ASOA2014042910420](https://openairdocs.org/sdr/ASOA2014042910420.md): Isolator · cracked · Mar 30, 2014 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD ISOLATOR LOCATED SECOND UP FROM BOTTOM AT RBL 9 IS CRACKED. REMOVED CRACKED ISOLATOR IAW SRM 51-42-13. INSTALLED NEW ISOLATOR IAW SRM 51-42-13.

Next page: https://openairdocs.org/aircraft/N901EV/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 = 'N901EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N901EV/reports

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