# Service difficulty reports: N902EV

A list on [N902EV](https://openairdocs.org/aircraft/N902EV.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 · 182 reports

- [SDR SWIA2020040149822](https://openairdocs.org/sdr/SWIA2020040149822.md): Unknown · smoke · Apr 1, 2020 · N902EV · Cndair CL6002B19 · Air Distribution System
  > RECEIVED A SMOKE TOILET CAUTION MESSAGE IN FLIGHT. BOTH PILOTS AND THE FLIGHT ATTENDANT SMELLED SMOKE. THE ALARM WAS SOUNDING. PERFORMED QRH PROCEDURE AND DIVERTED TO KSGU. FLIGHT 5261 - FILED CLOSED FOLLOWED PROCEDURES AS OUTLINED IN FIM DUE TO SMOKE TOILET
- [SDR SWIA2019082746226](https://openairdocs.org/sdr/SWIA2019082746226.md): Landing Gear · failed · Aug 27, 2019 · N902EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE AFTER TAKEOFF DURING GEAR RETRACTION. NOSE LANDING GEAR WOULD NOT RETRACT. DURING LANDING GEAR MECHANICAL AND HYDRAULIC HEALTH CHECK, FOUND NGWOFW2 OUT OF LIMITS. READJUSTED NGWOFW2 SENSOR IAW AMM. CYCLED LANDING GEAR IAW AMM MULTIPLE TIMES WIT
- [SDR SWIA2019082746229](https://openairdocs.org/sdr/SWIA2019082746229.md): Selector Valve · failed · Aug 26, 2019 · N902EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON DEPARTURE OUT OF ORD. NOSE GEAR SHOWED RED. RETURNED TO FIELD. ADJUSTED NGWOFW2 SENSOR IAW AMM. REMOVED AND REPLACED 3A & 3B ACMP AND SELECTOR VALVE IAW AMM. CYCLED LANDING GEAR MULTIPLE TIMES IAW AMM NO DEFECTS NOTED. OPS CHECK GOOD.
- [SDR SWIA2019032845669](https://openairdocs.org/sdr/SWIA2019032845669.md): Landing Gear · slow · Mar 28, 2019 · N902EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING AFTER TAKEOFF DURING GEAR RETRACTION. LEVELED AT SAFE ALT TO RUN QRH. JUST AFTER WE STARTED QRH GEAR WENT UP ON ITS OWN. COMPLETED QRH AND CONTINUED. GEAR OPERATED NORMALLY DURING EXTENSION. (FLT#3134) CLOSED PERFORMED FULL STRUT SERVICE
- [SDR SWIA2018100245117](https://openairdocs.org/sdr/SWIA2018100245117.md): Light · malfunctioned · Oct 2, 2018 · N902EV · Cndair CL6002B19 · Flight Compartment Lighting
  > ON DEPARTURE OUT OF ICT AREA, CAPTAIN SIDE YOKE LIGHT STARTED SPARKING AND POPPING WITH SUBSEQUENTLY SMOKING. SMOKE PERSISTED FOR ABOUT 5-10 MINUTES WITH SMOKE/ELECTRICAL SMELL. (FLT#3113) CLOSED DEFERRED CAPT YOKE CHART HOLDER IAW MEL.
- [SDR SWIA2018091445078](https://openairdocs.org/sdr/SWIA2018091445078.md): Selector Valve · failed · Sep 13, 2018 · N902EV · Cndair CL6002B19 · Landing Gear Selector
  > GEAR DISAGREE ON TAKEOFF. NOSE GEAR WOULD NOT RETRACT. FLIGHT 3130. FO: 9/14/2018. CLOSED REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. PERFORMED FULL SWINGS OF LANDING GEAR (NOSE AND MAIN). OPS CHECKS AND LEAK CHECKS GOOD.
- [SDR SWIA201844413](https://openairdocs.org/sdr/SWIA201844413.md): Floorbeam · corroded · Feb 20, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND THE FLOORBEAM ANGLE TO HAVE EXFOLIATING CORROSION AT LBL 40, BS 349. INSTALLED A NEW ANGLE IAW SRM.
- [SDR SWIA201844412](https://openairdocs.org/sdr/SWIA201844412.md): Frame · corroded · Feb 12, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 310 HAS CORROSION ON THE FLANGE BETWEEN STRINGERS 3L & 4L. BLENDED THE CORROSION IAW SRM, AND REO.
- [SDR SWIA201844411](https://openairdocs.org/sdr/SWIA201844411.md): Doubler · corroded · Feb 11, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Structure
  > DOUBLER AT SERVICE DOOR FRAME BS 349, STRINGER 18R AND DOUBLER AND LOWER FRAME BRACKET AT BS 319.7, STRINGER 18R CORRODED. REPLACED THE DOOR FRAME BRACKETS AND RESTORED FINISH TO DOUBLERS IAW SRM.
- [SDR SWIA2018031644410](https://openairdocs.org/sdr/SWIA2018031644410.md): Skin · scratched · Feb 11, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE EXTERIOR SKIN HAS SEVERAL SCRATCHES AT THE LT AND RT DME ANTENNA LOCATIONS. REPAIRED THE SKIN IAW REO.
- [SDR SWIA2018031644409](https://openairdocs.org/sdr/SWIA2018031644409.md): Floorbeam · corroded · Feb 10, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AROUND MULTIPLE FASTENER HOLES ON THE FLOORBEAM, LBL 9 TO RBL 9, BS 589. INSTALLED A NEW CAP STRIP ON THE FLOORBEAM IAW SRM.
- [SDR SWIA2018031644408](https://openairdocs.org/sdr/SWIA2018031644408.md): Floorbeam · corroded · Feb 10, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AROUND MULTIPLE FASTENER HOLES ON FLOORBEAM, LBL 9 TO RBL 40, BS 574. INSTALLED A NEW CAP STRIP ON THE FLOORBEAM IAW SRM.
- [SDR SWIA201844407](https://openairdocs.org/sdr/SWIA201844407.md): Rub Strip · chafed · Feb 8, 2018 · N902EV · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER AND LOWER L/E EDGES RUB STRIPS ARE CHAFED AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE RUB STRIPS IAW SRM AND REO.
- [SDR SWIA2018031644406](https://openairdocs.org/sdr/SWIA2018031644406.md): Skin · dented · Feb 1, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO DENTS FWD OF SERVICE DOOR AT BS 310, STRINGER 12R. REPAIRED IAW SRM.
- [SDR SWIA2018031644405](https://openairdocs.org/sdr/SWIA2018031644405.md): Skin · dented · Feb 1, 2018 · N902EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ONE DENT FWD OF SERVICE DOOR AT BS 310, STRINGER 16R. REPAIRED IAW SRM.
- [SDR SWIA201743650](https://openairdocs.org/sdr/SWIA201743650.md): Plate · gouged · Aug 2, 2017 · N902EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP INBOARD ROLLER GUIDE PLATE IS GOUGED. REPLACED THE ROLLER GUIDE PLATE IAW SRM.
- [SDR SWIA2017082143649](https://openairdocs.org/sdr/SWIA2017082143649.md): Vane · chafed · Aug 2, 2017 · N902EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OTBD FLAP VANE HAS CHAFING NEAR OTBD ACTUATOR. INSTALLED A REPAIR IAW REO.
- [SDR ASOA2016081715272](https://openairdocs.org/sdr/ASOA2016081715272.md): Proximity Switch · out of adjust · Aug 17, 2016 · N902EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKE OFF SELECTED GEAR UP GOT NOSE GEAR DISAGREE WARNING FOLLOWED QRH PROCEDURE TO EXTEND LANDING GEAR. ACFT DIVERTED. ADJUSTED NLG CENTERING PROXMITY SWITCH IAW AMM 32-61-05 OPS CHECKED GOOD.
- [SDR ASOA2016030114546](https://openairdocs.org/sdr/ASOA2016030114546.md): Shim · shifted · Mar 1, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Structure
  > MIGRATING SHIM BETWEEN FS 513.00 FRAME AND RT AND LT MCG SIDE BRACE FITTING BRACKETS. COMPLIED WITH ECTC REO 601R-53-41-101-01 PERMANENT REPAIR. COMPLIED WITH ECTC EO 600-53-26-50003. COMPLIED WITH EC/TC REO 601R-53-41-101 01. VERIFIED COMPLIANCE OF ECTC RE
- [SDR ASOA2016022314543](https://openairdocs.org/sdr/ASOA2016022314543.md): Stiffener · cracked · Feb 23, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > STIFFENER ON REAR PRESSURE BULKHEAD AT LBL 36, FS 621 IS CRACKED. REMOVED CRACKED STIFFNER ANGLE ON RT PRESSURE BULKHEAD AT LBL36, FS621.00 IAW SRM 51-42-06. LOCATED, DRILLED NEW STIFFNER ANGLE IAW SRM 51-40-11. INSTALLED FASTENERS AT LBL36 FS621, REF SRM 5
- [SDR ASOA2016022114544](https://openairdocs.org/sdr/ASOA2016022114544.md): Skin · damaged · Feb 21, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TEMP REPAIR ON FUSELAGE SKIN AT FS 589-605, STRINGERS 21-26R. REPAIR BECOMES PERMENANT AT REV A OF REO 601-53-61-5212.
- [SDR ASOA2016022014542](https://openairdocs.org/sdr/ASOA2016022014542.md): Floorbeam · corroded · Feb 20, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > OTBD NUTPLATE AREA CORRODED ON FLOORBEAM CAP AT 559+80 & RBL 27. REMOVED SEAT TRACK TRACK TO FOM IAW AMM 53-01-11. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. UPON FURTHER INVESTIGATION FLOORBEAM CAP AT FS 559.00, RBL27 WAS EXTREMELY EXFOILATED AROUND NU
- [SDR ASOA2016022014541](https://openairdocs.org/sdr/ASOA2016022014541.md): Crossbeam · corroded · Feb 20, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON CROSSBEAM 559 + 80 AND RBL 9. REMOVED CORROSION IAW SRM 51-21-06. REWORKED WITH THE ALLOWABLE DAMAGE LIMITS OF SRM 53-51-15-01 AND SRM 53-00-00-01, FIG 102.
- [SDR ASOA2016021814540](https://openairdocs.org/sdr/ASOA2016021814540.md): Fitting · cracked · Feb 18, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT WINDSHIELD CENTER POST LOWER FITTING CRACKED FS 202.75, WL 110.00. R & R CRACKED RT WINDSHIELD CENTER POST LOWER FITTING AT FS 202.75 AND WL 110.00 IAW SRM 51-42-21.
- [SDR ASOA2016021714539](https://openairdocs.org/sdr/ASOA2016021714539.md): Bulkhead · cracked · Feb 17, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT BL 0.00 - 36.20 BETWEEN WL 73.50 AND WL 137.50 FS 621.00 AREA IS MARKED. COMPLIED WITH ECTC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, DATED: 10/31/2011. COMPLIED WITH REO 601R-53-61-5659. RECEIVED AND CO
- [SDR ASOA2016021714538](https://openairdocs.org/sdr/ASOA2016021714538.md): Bulkhead · cracked · Feb 17, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT LBL 36.20 JUST ABOVE WL 73.50, BS 621. COMPLIED WIHT EC/TC REO 601R-53-61-1285, REV D.
- [SDR ASOA2016021014537](https://openairdocs.org/sdr/ASOA2016021014537.md): Cargo Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED RBL27, FS 559+78-559+95. EVALUATED CARGO TRACK RBL27 FS 559+78-559+95 OUT OF LIMITS IAW SRM 53-61-49. REMOVED CARGO TRACK RBL27, 559+78-559+95 IAW AMM 53-00-49-000-801. FABRICATED NEW CARGO TRACK IAW EC/TC REO 601R-53-00-485. INSTALLED
- [SDR ASOA2016021014536](https://openairdocs.org/sdr/ASOA2016021014536.md): Cargo Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 3 EA CARGO TRACKS CORRODED ON LBL 27 FROM FS 559+96-574.00. REMOVED 3 EA DISCREPANT CARGO TRACKS, ANCHOR PLATES REF: AMM 53-00*-49-000-801. INSTALLED 3 EA SERVICEABLE CARGO TRACKS IAW AMM 53-00-49-400-801. EVALUATED CORROSION DAMAGE FOR ALLOWABLE DAMAGE AND
- [SDR ASOA2016021014535](https://openairdocs.org/sdr/ASOA2016021014535.md): Cargo Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 2 EA CARGO TRACKS CORRODED FROM FS 559+86-559+112, RBL9. EVALUATED 2 EA CARGO TRACKS. TRACKS AT DISCREPANT LOCATION AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-51-49 AND SRM 53-61-49, FIG 101. REMOVED 2 EA CORRODED CARGO TIE DOWN TRACKS AS NEEDED SRM
- [SDR ASOA2016021014534](https://openairdocs.org/sdr/ASOA2016021014534.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 2 EA CARGO FLOOR TRACKS CORRODED FROM FS 559+86-559+122, LBL9. EVALUTED 2EA CARGO FLOOR TRACKS AT DISCREPANT LOCATIONS AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-51-49-01 AND 53-61-49-01, FIG 101. REMOVED 2EA CORRODED CARGO TIE DOWN TRACKS AS NEEDED
- [SDR ASOA2016021014533](https://openairdocs.org/sdr/ASOA2016021014533.md): Floor Support · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO RT FLOOR SILL CORRODED BETWEEN FS 574-589. REMOVED CORROSION ON RT FLOOR SILL TW FS 574-589 IAW SRM 51-21-06-00. ACCOMPLISHED CORROSION REMOVAL, BLEND OUT IAW REO 601R-53-61-5654. UPON FURTHER EVALUATION, FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS OF
- [SDR ASOA2016021014531](https://openairdocs.org/sdr/ASOA2016021014531.md): Cargo Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACKS CORRODED ON LBL 9 AT FS 584 AND FS 600. FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-61-49, FIG 101. REMOVED THE CARGO TRACK IAW AMM 53-00-49-000-801. INSTALLED IAW AMM 53-00-49-400-801.
- [SDR ASOA2016021014530](https://openairdocs.org/sdr/ASOA2016021014530.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK SEGMENT, BS 612 - 616, LBL9. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW EC/TC REO 601R-53-00-485. INSTALLED NEW FABRICATED SEAT TRACK FS 612-616 LBL9 IAW AMM 5
- [SDR ASOA2016021014529](https://openairdocs.org/sdr/ASOA2016021014529.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK SEGMENT CORRODED BS 559+86, LBL9. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT TRACK FS 559+5-559+86, LBL9.
- [SDR ASOA2016021014528](https://openairdocs.org/sdr/ASOA2016021014528.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK SEGMENT CORRODED BS 559+5 - 559+86, RBL9. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49, SRM 53-00-49. REMOVED SEAT TRACK IAW AMM 53-01-000-802. FABRICATED NEW SEAT TRACK IAW EC/TC REO 601R-53-00-485. INSTALLED NEW FABRICATED SEAT TRACK IAW
- [SDR ASOA2016021014527](https://openairdocs.org/sdr/ASOA2016021014527.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK SEGMENT, BS 409+16 - 409+112 CORRODED SEVERAL AREAS. REMOVED LT SIDE SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED LT SIDE SEAT TRACK IAW AMM 53-01-11-420-802. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV B.
- [SDR ASOA2016021014526](https://openairdocs.org/sdr/ASOA2016021014526.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK SEGMENT FS 409+112 - 449.85 CORRODED SEVERAL AREAS. REMOVED LT SIDE SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED LT SIDE SEAT TRACK IAW AMM 53-01-11-420-001. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV B.
- [SDR ASOA2016021014525](https://openairdocs.org/sdr/ASOA2016021014525.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK SEGMENT, FS 409+112-449.85 CORRODED SEVERAL AREAS. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SIDE SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-055.
- [SDR ASOA2016021014524](https://openairdocs.org/sdr/ASOA2016021014524.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK SEGMENT BS 409+16 - 409+112 CORRODED SEVERAL AREAS. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SIDE SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-055.
- [SDR ASOA2016021014523](https://openairdocs.org/sdr/ASOA2016021014523.md): Seat Track · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK SEGMENT FS 364-409+16 CORRODED SEVERAL AREAS. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT TRACK IAW REO 601R-53-00-485. INSTALLED NEW FABRICATED RT SIDE SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/T
- [SDR ASOA2016021014522](https://openairdocs.org/sdr/ASOA2016021014522.md): Floorbeam · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED RBL9 BETWEEN 559+16 - 559+112. UPON FURTHER EVALUATION FOUND FLOORBEAM CAP TO BE OUT OF LIMITS IAW SRM 53-00-00 WITH SEVERE HEAVY CORROSION. COMPLIED WITH ECTC REO 601R-53-51-274.
- [SDR ASOA2016021014521](https://openairdocs.org/sdr/ASOA2016021014521.md): Door Sill · cracked · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER SILL CRACKED AT FS 589. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-21-433, REV C, DATED 11/23/2012 AS WRITTEN.
- [SDR ASOA2016021014520](https://openairdocs.org/sdr/ASOA2016021014520.md): Floorbeam · corroded · Feb 10, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT RBL9 SCREW HOLES CORRODED BETWEEN FRAME BS 409+9 - 409+35. BLENDED CORROISON DAMAGE IAW SRM 51-21-06. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-00 WITH NO MATERIAL REMAINING. REMOVED FASTENERS IN FLOORBEAM COMMON TO REPAIR IAW SRM 53-0
- [SDR ASOA2016020814519](https://openairdocs.org/sdr/ASOA2016020814519.md): Rib · cracked · Feb 8, 2016 · N902EV · Cndair CL6002B19 · Fuselage Main, Structure
  > INSIDE LT WHEEL WELL, LT BATTERY RIB CRACKED AT WS 53.60. REPAIRED BATTERU RIB ASSY IAW REO 601R-57-51-046, REV B. RECEIVED AND COMPLIED WITH ECTC REO 601R-57-51-046.
- [SDR ASOA2016020814518](https://openairdocs.org/sdr/ASOA2016020814518.md): Angle · cracked · Feb 8, 2016 · N902EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT FS 621-625.00 AND STR 14, LT AND RT SIDE. R & R CRACKED ANGLE AT FS 621-625.00 AND STR14 LT AND RT IAW SRM 51-42-21.
- [SDR ASOA2016020814509](https://openairdocs.org/sdr/ASOA2016020814509.md): Fitting · gouged · Feb 8, 2016 · N902EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS COMPARTMENT FWD RT DOOR FITING ON FUSELAGE IS GOUGED. NO ALLOWABLE DAMAGE. BLENDED DAMAGE IAW IAW SRM 51-12-00 BLEND AREA IS.5" WIDE X.2" TALL MATERIAL REMOVED IS.019" MEASURED USING MACT 3100. SUBMITTED TO ENGINEERING FOR PERMANENT DISPOSIT
- [SDR ASOA2016020814508](https://openairdocs.org/sdr/ASOA2016020814508.md): Fitting · gouged · Feb 8, 2016 · N902EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS COMPARTMENT FWD LT DOOR FITTING ON FUSELAGE IS GOUGED. BLENDED DAMAGE IAW SRM 51-12-00 BLEND AREA IS.5" WIDE X.2" T. ALL MATERIAL REMOVED IS.017" MEASURED USEING MACT 3100. SUBMITTED TO STS ENGINEERING FOR PERMANENT DISPOSITON REF SRM 51-13
- [SDR ASOA2015101513894](https://openairdocs.org/sdr/ASOA2015101513894.md): Bulb · burned out · Oct 15, 2015 · N902EV · Cndair CL6002B19 · Emergency Lighting
  > OUTSIDE FWD EMERGENCY LIGHT BURNED OUT. R & R OUTSIDE FWD EMERGENCY LIGHT BULB IAW AMM 33-51-21.
- [SDR ASOA2015081013476](https://openairdocs.org/sdr/ASOA2015081013476.md): Bulb · burned out · Aug 10, 2015 · N902EV · Cndair CL6002B19 · Emergency Lighting
  > SECOND AFT CABIN EMERGENCY CEILING FLOOD LIGHT IS INOPERATIVE. R & R CABIN EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.
- [SDR ASOA2015073113417](https://openairdocs.org/sdr/ASOA2015073113417.md): Sign · damaged · Jul 31, 2015 · N902EV · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED EXIT SIGN ABOVE SERVCE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-13. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Next page: https://openairdocs.org/aircraft/N902EV/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 = 'N902EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N902EV/reports

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