N919EV

Service difficulty reports · 253

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 = 'N919EV' 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 SWIA202053547Floorbeam · corrodedPRESS FLOOR 9R SUPPORT BEAM HAS CORROSION IN MULTIPLE AREAS, AS MARKED. C-CHECK RO 10/20/2020. REMOVED MULTIPLE AREAS OF CORROSION FROM FLOOR BEAM FLANGE AT RBL 9 ABOVE PRESSURE FLOOR, IAW CRJ-200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS OF REO. SUBMITSep 15, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202053546Skin · corrodedEXTERIOR SKIN CORRODED BETWEEN STGRS 26L AND 25R AT FS 559+112, AS MARKED. C-CHECK RO 10/20/2020. BLENDED OUT EXTERIOR CORROSION ON EXTERIOR SKIN BETWEEN STGRS 26L AND 25R AT FS 559+112, AS MARKED, REF CRJ 200 SRM. REPAIRED EXTERIOR SKIN BETWEEN STGRS 26L ASep 15, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053545Doubler · wornLT INBOARD FLAP VANE HAS WEAR ON DOUBLER AT WS 104 FROM FLAP STOP. C-CHECK RO 10/20/2020. REMOVED EXISTING LT INBOARD FLAP (OUTBOARD CENTER) LEADING EDGE. FIT AND INSTALLED NEW LT INBOARD FLAP (OUTBOARD CENTER) LEADING EDGE P/N 601R14303-51 WITH SEALANT, RESep 14, 2020 · N919EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202053544Doubler · wornRT INBOARD FLAP VANE HAS WEAR ON DOUBLER AT WS 55 FROM FLAP STOP. C-CHECK RO 10/20/2020. REMOVED INBOARD RT FLAP VANE AT WS 55 AND WET INSTALLED NEW FLAP VANE P/N 601R14303-54, REF CRJ 200 SRM AND DWG. INSTALLATION OF REPAIR DOUBLER TITANIUM CAPS ON INBOARDSep 14, 2020 · N919EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202053543Skin · dentedFS 559+112 TO FS 755.0 EXTERIOR BELLY SKIN HAS SEVERAL DENTS. C-CHECK RO 10/20/2020. REPAIRED FS 559+112 TO FS 755.0 EXTERIOR BELLY SKIN, REF MHI RJ REO AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.Sep 14, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053569Bolt · corrodedRT OUTBOARD GROUND SPOILER HAS CORRODED HARDWARE ON PCU LINK ASSEMBLY. C-CHECK RO 10/20/2020. REPLACED RT OUTBOARD GROUND SPOILER CORRODED HARDWARE ON PCU LINK ASSEMBLY, PER CRJ 200 AMM. OPERATION TEST GOOD.Sep 13, 2020 · N919EV · Cndair CL6002B19 · SpoilersSDR SWIA202053568Bolt · corrodedLT ELEVATOR ATTACH HARDWARE, BONDING WIRE AND SAFETY TAB HARDWARE SEVERAL PLACES HAS CORROSION. C-CHECK RO 10/20/2020. REMOVED AND REPLACED ALL LT ELEVATOR HINGE ATTACH HARDWARE, BONDING WIRES, AND SAFETY TABS, REF CRJ200 AMM. REPLACED 25 BOLTS, 6 SCREWS, Sep 13, 2020 · N919EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202053567Nut · corrodedRT ELEVATOR ATTACH HARDWARE, BONDING WIRE AND SAFETY TAB HARDWARE SEVERAL PLACES HAS CORROSION. C-CHECK RO 10/20/2020. REMOVED AND REPLACED RT ELEVATOR INBOARD AND OUTBOARD FLUTTER DAMPENER AFT MOUNTING HARDWARE, REF CRJ200 AMM TASK. REMOVED MINOR SURFACE CSep 13, 2020 · N919EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202053542Intercostal · crackedIN AFT EQUIPMENT BAY, INTERCOSTAL BETWEEN FS 621 AND FS 625, STR 13R IS CRACKED. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED "NEW" AFT EQUIPMENT BAY INTERCOSTAL LOCATED BETWEEN FS 621-FS 625 STRG 14L, AS REQUIREDD REF REO. SEE CONTINUATION CARD FOR DETAILSSep 13, 2020 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053541Intercostal · crackedIN AFT EQUIPMENT BAY, INTERCOSTAL BETWEEN FS 621 AND FS 625, STR 13L IS CRACKED. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NERW AFT EQUIPMENT BAY, INTERCOSTAL BETWEEN FS 621 AND FS 625, STR 14L, REF REO, DWG & CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILSep 13, 2020 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202053540Bulkhead · damagedEVALUATE OR REPAIR LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. C-CHECK RO 10/20/2020. REPAIRED LT 9G BULKHEAD, PER MHIRJ EO. COMPLIED WITH SKYWEST TASK CARD.Sep 13, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202053539Bulkhead Web · damagedEVALUATE OR REPAIR CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS. C-CHECK RO 10/20/2020. REPAIRED CENTER 9G BULKHEAD, PER MHIRJ EO. COMPLIED WITH SKYWEST TASK CARD.Sep 13, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202053538Bulkhead Web · damagedEVALUATE OR REPAIR RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS. C-CHECK RO 10/20/2020. REPAIRED RT 9G BULKHEAD, PER MHIRJ REO. COMPLIED WITH SKYWEST TASK CARD.Sep 13, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202053602Attach Fitting · gougedLEFT OUTBOARD FLAP INBOARD HINGE BOX AFT ATTACH FITTING ON WING INBOARD ATTACH POINT OUTBOARD LUG GOUGED. C-CHECK RO 10/20/2020. BLENDED OUT GOUGE ON LEFT OUTBOARD FLAP INBOARD HINGE BOX AFT ATTACH FITTING ON WING INBOARD ATTACH POINT OUTBOARD LUG, IAW CRJ20Sep 12, 2020 · N919EV · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA202053537Skin · chafedWING LOWER PLANK UNDER PANEL 193AB CHAFED AT RBL 45. C-CHECK RO 10/20/2020. BLENDED OUT CHAFE ON WING LOWER PLANK UNDER PANEL 193AB AT RBL 45, IAW CRJ200 SRM. ORIGINAL MATERIAL THICKNESS OF LOWER WING PLANK AT REWORKED AREA ZONE A .300. REMAINING MATERIAL Sep 12, 2020 · N919EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202053536Skin · dentedFUSELAGE DENT AT APPROXIMATELY FS 220 BETWEEN STR 22R AND STR 23R. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 220 BETWEEN STR 22R AND STR 23R, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053535Skin · dentedFUSELAGE DENT BETWEEN FS 250 AND FS 265 BETWEEN STR 24R AND STR 25R. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 250 AND FS 265 BETWEEN STR 24R AND STR 25R, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053534Skin · dentedFUSELAGE DENT BETWEEN FS 235 AND FS 250 BETWEEN STR 25L AND STR 26L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 235 AND FS 250 BETWEEN STR 25L AND STR 26L, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053533Skin · dentedFUSELAGE 2 DENTS BETWEEN FS 250 AND FS 265 BETWEEN STR 24L AND STR 25L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 250 AND FS 265 BETWEEN STR 24L AND STR 25L, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053532Skin · dentedFUSELAGE DENT BETWEEN FS 250 AND FS 265 BETWEEN STR 23L AND STR 24L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 250 AND FS 265 BETWEEN STR 23L AND STR 24L, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053531Skin · dentedFUSELAGE DENT BETWEEN FS 265 AND FS 280 BETWEEN STR 23L AND STR 24L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 265 AND FS 280 BETWEEN STR 23L AND STR 24L, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053530Skin · dentedFUSELAGE DENT BETWEEN FS 265 AND FS 280 BETWEEN STR 24L AND STR 25L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 265 AND FS 280 BETWEEN STR 24L AND STR 25L, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053529Skin · dentedFUSELAGE DENT BETWEEN FS 265 AND FS 280 BETWEEN STR 25L AND STR 26L. C-CHECK RO 10/20/2020. REPAIRED FUSELAGE SKIN BETWEEN FS 265 AND FS 280 BETWEEN STR 25L AND STR 26L, REF REO. SEE CONTINUATION CARD FOR DETAILS.Sep 12, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053528Hinge Arm · chafedLEFT OUTBOARD FLAP CENTER HINGE ARM CHAFED ON OUTBOARD SIDE NEAR ATTACHMENT TO HINGE BOX. C-CHECK RO 10/20/2020. BLENDED OUT CHAFE ON LEFT OUTBOARD FLAP CENTER HINGE ARM ON OUTBOARD SIDE NEAR ATTACHMENT TO HINGE BOX, IAW CRJ200 SRM. BLENDED AREA FOUND TO BESep 11, 2020 · N919EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202053527Fitting · damagedRT WING OUTBOARD FLAP OUTBOARD HINGE BOX AFT FITTING ON WING OUTBOARD ATTACH POINT INBOARD LUG HAS EDGE DAMAGE. C-CHECK RO 10/20/2020. BLENDED OUT CHAFING ON RT WING OUTBOARD FLAP OUTBOARD HINGE BOX AFT FITTING ON WING OUTBOARD ATTACH POINT INBOARD LUG, IAW Sep 11, 2020 · N919EV · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA202053598Fitting · chafedPASSENGER DOOR SURROUND AT AFT UPPER PIN FITTING HAS CHAFE DAMAGE. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT UPPER PIN STOP FITTING, REF CRJ 200 AMM (TESTS GOOD).Sep 10, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053597Cam · chafedPASSENGER DOOR SURROUND AT STOP ABOVE FORWARD PULL IN LEVER CAM CHAFED AND HIGH METAL. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW PASSENGER DOOR PULL IN LEVER STOP ABOVE FWD PULL IN LEVER CAM, REF CRJ 200 SRM.Sep 10, 2020 · N919EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053596Cam · chafedPASSENGER DOOR SURROUND AT FORWARD PULL IN LEVER CAM ON FUSELAGE CHAFED THROUGH PROTECTIVE COATING. C-CHECK RO 10/20/2020. EVALUATED, REMOVED, AND REPLACED PASSENGER DOOR FWD DOOR CAM P/N 600-31688-17 P/O T56322, REF CRJ 200 SRM (TEST GOOD). SEE CONTINUTIONSep 10, 2020 · N919EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202053595Stop Fitting · chafedAVIONICS BAY DOOR SURROUND AT RT STOP FITTING AT STR 25R STOP PAD CHAFED. C-CHECK RO 10/20/2020. REMOVED AND REPLACED NEW 1 EA STOP FITTING AT STR 25R AVIONICS BAY DOOR SURROUND, PER REF CRJ 200 SRM.Sep 10, 2020 · N919EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202053594Stop Fitting · chafedAVIONICS BAY DOOR SURROUND AT LT STOP FITTING AT STR 25L STOP PAD CHAFED. C-CHECK RO 10/20/2020. REMOVED AND REPLACED 1 EA. A-BAY DOOR LT STOP FITTING AT STGR 25L WITH NEW PART, REF CRJ200 SRM.Sep 10, 2020 · N919EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202053563Guide · crackedAVIONICS BAY DOOR SURROUND AFT RT PLASTIC GUIDE CRACKED. C-CHECK RO 10/20/2020. REMOVED AND REPLACED NEW 1 EA PLASTIC GUIDE AFT RT AVIONICS BAY DOOR SURROUND, PER REF CRJ 200 SRM.Sep 10, 2020 · N919EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202053526Window Post · crackedLEFT SIDE WINDSHIELD POST LOWER OUTBOARD CLIP CRACKED. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW LT SIDE WINDSHIELD POST LOWER CLIP, REF CRJ-200-SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.Sep 9, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053525Window Post · crackedRIGHT SIDE WINDSHIELD POST LOWER OUTBOARD CLIP CRACKED. C-CHECK RO 10/20/2020. REMOVED AND INSTALLED NEW RT SIDE WINDSHIELD POST LOWER CLIP, REF CRJ-200-SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.Sep 9, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053524Skin · wornRT WING AILERON LEADING EDGE LOWER SHROUD SKIN HAS WEAR. C-CHECK RO 10/20/2020. BLENDED OUT CHAFING ON RT WING AILERON LEADING EDGE LOWER SHROUD SKIN AT 2 EA LOCATIONS, AS MARKED, IAW REO 1 EA. BLENDED PANEL IS FOUND TO BE WITHIN LIMITS & 1 EA, BLENDED PANESep 9, 2020 · N919EV · Cndair CL6002B19 · AileronsSDR SWIA202053523Skin · chafedLT AILERON, LOWER INBOARD FIXED LEADING EDGE SKIN IS CHAFED. C-CHECK RO 10/20/2020. BLENDED OUT CHAFE ON LT AILERON, LOWER INBOARD FIXED LEADING EDGE SKIN, IAW REO. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE LOWER SKIN LEADING EDGE ON LT AILERON WSep 6, 2020 · N919EV · Cndair CL6002B19 · AileronsSDR SWIA202053522Floor Skin · crackedTRU BAY FLOOR IS CRACKED, LEFT SIDE APPROXIMATELY FS 191.00, MARKED. C-CHECK RO 10/20/2020. PERFORMED REPAIR OF THE TRU BAY FLOOR, LEFT SIDE APPROXIMATELY FS 191.00 USING REF REO. OPERATIONS CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.Sep 5, 2020 · N919EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA202053521Angle · weakCOMPLY WITH REO 601R-53-41-1116. REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. C-CHECK RO 10/20/2020. COMPLIED WITH BOMBARDIER REO. REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. PRESSURE CHAug 21, 2020 · N919EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019111846769Fan · failedDISPLAY COOL CAUTION MESSAGE IN CRUISE. DID NOT CLEAR WITH QRH. FLIGHT # 3638 CLOSED MSG HAD CLEARED. CHECKED FOR OPERATION OF THE FLIGHT FAN AND GROUND FAN. BOTH FANS CHECKED GOOD. CHECKED DISPLAY COOL FILTER FOR EXCESSIVE DUST. FOUND TO RELATIVELY CLEAN.Nov 17, 2019 · N919EV · Cndair CL6002B19 · Central DisplaySDR SWIA2019061145969Actuator · failedGEAR DISAGREE ON FINAL APPROACH. LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN, AUDIBLE CLUNK WAS HEARD WHEN LEFT MAIN LANDING GEAR DID FINALLY INDICATE DOWN. COMPLIED WITH QRH AND LANDED WITH NO FURTHER ISSUE. (FLT#3912) REMOVED AND REPLACED LT SIDESTAY MLG AJun 11, 2019 · N919EV · Cndair CL6002B19 · Landing Gear ActuatorSDR SWIA2018112745270Uplock · contaminatedLEFT MAIN GEAR DIDN'T COME UP WHEN LANDING GEAR WAS SELECTED UP. GEAR DISAGREE WARNING, (FLT#7360) CLOSED REMOVED ICE/SNOW BUILD UP AROUND THE LT MLG UPLOCK. PERFORMED NUMEROUS CYCLES OF THE LANDING GEAR EXTENSION/RETRACTION. OPS CHECK GOOD.Nov 27, 2018 · N919EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018062644803Strut · dischargedNOSE DOOR WARNING AFTER TAKE OFF. PERFORMED NOSE STRUT SERVICE, ADJUSTMENT OF WEIGHT OFF WHEEL SENSORS IAW AMM. COMPLIED WITH A GEAR EXTENSION IAW AMM. OPS CHECKED GOOD. NO DEFECTS.Jun 19, 2018 · N919EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2018040444331Proximity Sensor · out of adjustGEAR DISAGREE, NOSE WOULD NOT RETRACT AFTER TAKE OFF WHEN LEVER SELECTED UP. ADJUSTED THE NLG PROXIMITY SENSOR IAW AMM. NLG SWUNG SEVERAL TIMES. OPS GOOD.Feb 26, 2018 · N919EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018022744331Not Reported · malfunctionedGEAR DISAGREE, NOSE WOULD NOT RETRACT AFTER T/O WHEN LEVER SELECTED TO UP. (FLT 4870) FO: 02/26/2018 WORK IN PROGRESS.Feb 26, 2018 · N919EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201743550Skin · damagedPERMANENT REPAIR REQUIRED TO FUSELAGE SKIN AT BS 700, STRINGER 6R. REPAIRED THE SKIN IAW REO.Jul 15, 2017 · N919EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201743549Floor Support · corrodedRT FLOOR SUPPORT BS 559+85 TO 559+116 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.Jun 10, 2017 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743548Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN BS 559+112 - 569 AT LBL 27. REMOVED AND REPLACED THE FLOOR SUPPORT SECTION IAW SRM AND REO.Jun 9, 2017 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743547Strap · corrodedFLOOR SUPPORT STRAP AT BS 559, BETWEEN RBL27 TO RT FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED IAW SRM.Jun 9, 2017 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743546Floor Support · corrodedRBL 27 FLOOR SUPPORT HAS CORROSION AT BS 559. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.Jun 9, 2017 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743545Floor Support · corrodedFLOOR SUPPORT RBL 9 AT BS 559+80 HAS CORROSION UNDER SEAT TRACK. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW SRM.Jun 9, 2017 · N919EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743544Floorbeam · corrodedBS 559 FLOORBEAM AT BS 559+112 HAS VARIOUS SPOTS OF CORROSION BTW RBL 27 TO RT FLOOR SUPPORT. REMOVED AND REPLACED FLOORBEAM SHIM IAW REO AND SRM.Jun 8, 2017 · N919EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
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