N716EV

Service difficulty reports · 296

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N716EV' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA202055965Stringer · corroded*STGR27 CORRODED FS280.00 - FS295.00. (MARKED) (C-CHECK) RO 2/5/2021 STGR27 FROM FS280-FS313 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 DWG SH670-31630 REV K. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055964Stringer · corroded*STGR26R CORRODED FS295.00 €“ FS310.00. (MARKED) (C-CHECK) RO 2/5/2021 REPLACED STGR26R FS280-FS333.00 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 DWG SH670-31630 REV K COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055963Stringer · corroded*STGR25L CORRODED BETWEEN FS319.00 €“ FS333.00. (MARKED) (C-CHECK) RO 2/5/2021 REPLACED STGR 25L FROM FS280-FS333 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, DWG SH670-31630 REV K. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GNov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055962Stringer Splice · corroded*STGR26L STRINGER SPLICE CORRODED JUST FORWARD OF FRAME FS333.00. (MARKED) (C-CHECK) RO 2/5/2021 REPLACED STGR 26L STRINGER SPLICE AT FS333.00 WITH NEW REF CRJ-700 SRM 51-42-06-001-001-A01CRJ 700SRM 51-40-11-001-001-A01 AND DWG SH670-32429 REV A. COMPLIED Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055961Intercostal · corroded*INTERCOSTAL CORRODED FS310.00 €“ FS319.00, STGR20L. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED INTERCOSTAL (P/N- SH670-31822-1) AT FS 310.00 - FS 319.00, STGR 21LH. . REF CRJ-700 SRM 51-42-06-001-001-A01 & DWG SH670-31822 REV NC. SEE CONTINUE CARNov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055960Slat Track · corroded*RH SLAT TRACK 1-2 HAS 2 AREAS OF CORROSION (MARKED) (C-CHECK) RO 2/5/2021 BLENDED R/H SLAT TRACK 1-2 AND RESTORED AS REQUIRED PER REO 670-57-42-978 REV.-- DATE: 2020-12-17 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002 SKY.Nov 22, 2020 · N716EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202055959Slat Track · corroded*RH SLAT TRACK 2-2 HAS 2 AREAS OF CORROSION (MARKED) (C-CHECK) RO 2/5/2021 BLENDED R/H SLAT TRACK 2-2 AND RESTORED AS REQUIRED PER REO 670-57-42-979 REV. -- DATE: 20-12-17 WITHIN LIMITS, ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMNov 22, 2020 · N716EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202055958Slat Track · corrodedLH SLAT TRACK 1-2 HAS 1 AREA OF CORROSION. (C-CHECK) RO 2/5/2021 BLENDED L/H SLAT TRACK 1-2 AND RESTORED AS REQUIRED PER REO 670-57-42-976 REV. -- DATE:2020-12-18 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY.Nov 22, 2020 · N716EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202055957Slat Track · corrodedLT SLAT TRACK 2-2 HAS 2 AREAS OF CORROSION (MARKED) (C-CHECK) RO 2/5/2021 BLENDED AREA ON L/H SLAT TRACK 2-2 AND RESTORED AS REQUIRED. BLENDED DAREAS ARE STRUCTURALLY ACCEPTABLE REF. REO 670-57-42-977 REV. -- DATE: 20-12-18 ALL STEPS COMPLIED WITH. COMPLINov 22, 2020 · N716EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202055956Slider · wornR/H LWR TRANS COWL SLIDE HAS WORN AREA (FWD) (C-CHECK) RO 2/5/2021 REPAIRED DAMAGE TO RH LWR TRANSCOWL SLIDE PER MHIRJ REO 670-54-21-1410 REV -- DATED 2020-12-11 AND BOMBARDIER REO 670-78-34-384 REV D DATED 2018-11-27 / COMPLIED WITH SKYWEST TASK CARD 51-Nov 22, 2020 · N716EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202055955Skin · damagedRH FUSELAGE SKIN HAS HOLE BELOW STRINGER 11 AT APPROX FS 1151. VISABLE FROM WITHIN AEB (EXTERIOR SKIN IS COVERED BY RH PYLON). (C-CHECK) RO 2/5/2021 FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO # T-52592 AND FABRICATED SHIM FROM 2024-T3 .080 PO # T-55Nov 21, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202056005Panel · chafedL/H WING INBOARD FLAP L/E PANEL 584ET , HAS CHAFFING CONDITION (C-CHECK) RO 2/5/2021 REMOVED PNL 584ET, BLENDED DAMAGE, DETERMINED TO EXCEED LIMITS IAW CRJ700 SRM 57-52-01-101-001-A01, ORDERED AND RECIEVED NEW PANEL P/N CC670-14027-3, LOCATED,DRILLED AND Nov 20, 2020 · N716EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202056006Angle · corrodedANGLE CORRODED ON AIRCRAFT FOR PANEL 642 AZ (C-CHECK) RO 2/5/2021 INSTALLED NEW ANGLE CC670-10338-2 REF DWG CC670-10320 REV F DATE 2015 NOV 5. HI-LITE INSTALLATION REF CRJ-700 SRM TASK 51-42-21-001-001-A01 / COMPLIED WITH SKY CARD 28-900-100-SKY (CL600-Nov 19, 2020 · N716EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR SWIA202055997Bolt · corroded* CORROSION DETECTED ON (BOLT HEADS) ON L/H OTBD FLAP, (INBD) HINGE BOX, (FWD) SUPPORT FITTING (WING PLANK SIDE), ATTACHING HARDWARE (MARKED). (C-CHECK) RO 2/5/2021 - INSTALLED 6 NEW BOLTS AND ATTACHING HARDWARE ON TO FLAP HINGE BOX SUPPORT FITTING AT WS17Nov 19, 2020 · N716EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202055954Skin · damagedEVALUATE CREASE @ FS 409 ABOVE STGR 20L. (C-CHECK) RO 2/5/2021 INSTALLED REPAIRED DOUBLER-1 AND REPAIR SHIM-2. REF: REO 670-53-21-1888 REV. -- DATE: 2020-12-14. PRESSURE CHECK GOOD. / COMPLIED WITH ALL STEPS OF REO 670-53-21-1888 REV -- DATED 2020-12-14. CNov 16, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2018051645127Light · inoperativeDURING MX INSPECTION THE OVERHEAD EMERGENCY LIGHT AT ROW 4 IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-09, CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 14, 2018 · N716EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201712045244Diaphragm · crackedAFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE FORWARD DIAPHRAGM P/N SH670-39241-3 AT FS 909.00 LBL 17.63 IS CRACKED AT JOGGLE. REPAIRED WING TO FUSELAGE AFT FAIRING SUP FS 909.00, LBL 17.63 & (OR) RBL 17.63 IAW REO 670-53-82-478 REV A. REO 670-53-82-519 HAS BDec 4, 2017 · N716EV · Cndair CL6002C10 · Aerodynamic FairingsSDR ASOA201712045243Crossbeam · crackedRT FS280 CROSSBEAM CRACKED APPROX 4" AT RBL 45. REO 670-53-21-1471 HAS BEEN ACCOMPLISHED.Dec 4, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201711305241Floor Support · corrodedREF: CO# 10084617 JOB# 71008468 OP# 29: RIGHT CABIN FLOOR SILL RBL45 F.S.280-F.S.300 IS CORRODED. C/A: REMOVED AND REPLACED RIGHT CABIN FLOOR SILL IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND EXPRESNov 30, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201711305240Drag Angle · crackedREF: CO# 10084617 JOB# 71008461 OP# 41: PAX DOOR AFT DRAG ANGLE IS CRACKED NEAR POWER ASSIST PULLEY FITTING. C/A: REPAIRED PAX DOOR AFT DRAG ANGLE IAW EXPRESS JET EC/TC REO 670-52-11-072 AND 670-52-11-985.Nov 30, 2017 · N716EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201711305239Striker · corrodedREF: CO# 10084617 JOB# 71008468 OP# 28: SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. C/A: REMOVED AND REPLACED SERVICE DOOR LOWER SEAL STRIKER IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 AND BOMBARDIER REO 670-53-21-146Nov 30, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201711295238Lug · chafedREF: CO# 10084617 JOB# 71008467 OP# 16: RIGHT AILERON OUTBOARD PCU HINGE LUG IS CHAFED. C/A: REPAIRED RIGHT AILERON HINGE LUG IAW BOMBARDIER REO 670-57-61-107 REV A AND EXPRESS JET EC/TC EO700-57-60-00007.Nov 29, 2017 · N716EV · Cndair CL6002C10 · Wing, Attach FittingsSDR ASOA201711245236Hinge · gougedPASSENGER DOOR HINGE ON DOOR SIDED IS GOUGED AT 2(EA) LOCATIONS ON FORWARD SIDE OF ATTACHMENT LUG. REPAIRED PASSENGER DOOR HINGE IAW REO 670-52-11-511 REV E DATED 2017-08-02 AND EC/TC REO 670-52-11-511 REV E.Nov 24, 2017 · N716EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201711245235Seat Track · corrodedLEFT SIDEWALL NR 5 SEAT TRACK FROM FS 715-FS 761 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.Nov 24, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711195231Support · crackedMAIN LANDING GEAR FAIRING 194AB CENTER SUPPORT FWD AND AFT ANGLE BRACKETS ARE CRACKED. BROKEN WHERE PANEL MOUNTS. REMOVED AND REPLACED FWD AND AFT ANGLE BRACKETS IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01Nov 19, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201711185227Seat Track · corrodedFLOOR SEAT TRACK AT RBL 9 BETWEEN FS847-FS969 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.Nov 18, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711185226Seat Track · corrodedFLOOR SEAT TRACK AT LBL 9 BETWEEN FS693-FS847 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.Nov 18, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711185225Seat Track · corrodedFLOOR SEAT TRACK AT LBL 9 BETWEEN FS485-FS581 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.Nov 18, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711165224Seat Track · corrodedRT SEAT TRACK AT RBL 9..00 IS CORRODED BETWEEN FS 693 AND FS 847.00. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, DATED 2015-10-22 AND REO 670-53-00-343 REV M, DATED 2015-10-19.Nov 16, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711155223Intercostal · corrodedINTERCOSTAL FROM FS 364-349 BETWEEN STRINGER 27 AND 26L IS CORRODED AT FRONT OF AVIONICS BAY DOOR CUTOUT. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 364 TO 349 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01.Nov 15, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201711155222Frame · corrodedFS 349 LOWER FRAME SEGMENT IS CORRODED BETWEEN STRINGER 27 AND 26L. REPAIRED FRAME FS 349 IAW REO 670-53-21-1281 DATED 2016-04-11 AND EC/TC REO 670-53-21-1281.Nov 15, 2017 · N716EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201711145230Seat Track · corrodedLEFT SIDEWALL NR 6 SEAT TRACK FROM BS 785 TO 853 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, AND EC/TC REO 670-53-00-343, REV K.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145229Seat Track · corrodedRIGHT SIDEWALL NR 8 SEAT TRACK FROM BS 861 TO 961 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV.M, AND EC/TC REO 670-53-00-343 REV.K,Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145228Seat Track · corrodedRIGHT SIDEWALL NR 6 SEAT TRACK FROM BS 784 TO 855 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145221Seat Track · corrodedLEFT SIDEWALL NR 3 SEAT TRACK FROM BS 570 - 670 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145220Seat Track · corrodedLEFT SIDEWALL NR 2 SEAT TRACK FROM BS 485 - 570 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145219Seat Track · corrodedRIGHT SIDEWALL NR 5 SEAT TRACK FROM BS 713 TO 763 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145218Seat Track · corrodedRIGHT SIDEWALL NR 4 SEAT TRACK, BS 675 TO 713 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K,Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145217Seat Track · corrodedLEFT SEAT TRACK AT LBL 9 IS CORRODED BETWEEN BS 847 AND 985. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145216Seat Track · corrodedSEAT TRACK, RBL 27 IS CORRODED BETWEEN BS 985 AND 1000. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711145215Floorbeam · corrodedBS 280 FLOORBEAM ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-25-00-001-001-A01.Nov 14, 2017 · N716EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201711135214Frame · corrodedBS 310 LOWER FRAME SEGMENT IS CORRODED BETWEEN STRINGERS 25 AND 27L. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EC/TC REO 670-53-21-799, REV A.Nov 13, 2017 · N716EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201711135213Seat Track · corrodedLEFT SIDEWALL NR 8 SEAT TRACK FROM BS 861 - 961 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, REO 670-53-00-343, REV M, AMM 53-00-49-000-801-A17, AND 53-00-49-400-801-A17.Nov 13, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711115212Seat Track · corrodedLEFT SIDEWALL NR 4 SEAT TRACK FROM FS677-FS715 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.Nov 11, 2017 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201711095211Floor Support · corrodedAVIONICS BAY FLOORBOARD SUPPORT AT FS 280.00 IS CORRODED. REMOVED AND REPLACED WITH NEW SERVICEABLE FLOORBOARD SUPPORT P/N CC670-34256-3 IAW SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Nov 9, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201711095210Plate · corrodedSERVICE DOOR STEP PLATE HAS CORROSION ON THE BOTTOM OF THE STEP PLATE. REPLACED CORRODED STEP PLATE P/N SH670-31407-7 WITH NEW SERVICEABLE STEP PLATE P/N SH670-31407-7. DRILLED AND LOCATED STEP PLATE IAW SRMS 51-40-11-001-001-A01 AND 51-45-00-001-001-A01.Nov 9, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201708061822Control Panel · malfunctionedUNCOMMANDED RUDDER DEFLECTION TO RIGHT. ACFT RETURNED TO DEPARTURE AFTER T/O. REMOVED AND REPLACED THE ALIERON-RUDDER CONTROL PANEL IAW AMM 27-12-10. OPS TESTED AILERON TRIM SYSTEM IAW AMM 27-11-00. OPS TESTED RUDDER TRIM SYSTEM IAW AMM 27-22-00. OPS TESTEDAug 6, 2017 · N716EV · Cndair CL6002C10 · Flight Control SystemSDR ASOA201705131572Skin · dentedFUSELAGE DAMAGE BETWEEN FS 265 AND FS 280 BETWEEN STR 15R AND 16R. REPAIRED DAMAGED AREA OF FUSELAGE SKIN IAW REO 670-53-11-1277 REV O.May 13, 2017 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201704071453Stringer · crackedFS 280 STRINGER 3L WAS FOUND TO BE CRACKED. REO 670-53-21-493 AND SERVICE BULLETIN 670BA-53-040 PART A & B INCORPORATED.Apr 7, 2017 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201704071452Post · crackedFS 202 LBL 30 POST, HAS A CRACK INDICATION NOTED AT THE UPPER EDGE OF FLANGE, .250 INCHES LONG. FAILED NDT. REPAIRED FS 202 LBL 30 POST IAW SRM 53-11-10-201-005-A01.Apr 7, 2017 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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