N922EV

Service difficulty reports · 159

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 = 'N922EV' 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 SWIA202053515Floorbeam · damagedCOMPLY 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 10/18/2020. COMPLIED WITH REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. WEIGHT CHANGE OF +4.3 LBS. REFER TO ATTACHED CONJul 29, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202053514Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING Jul 28, 2020 · N922EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2017091943767Bulkhead Web · crackedCRACK INDICATION NOTED AT BS 621 REAR PRESSURE BULKHEAD FWD FACE AT RBL 27.5, WL 136. .250 IN LENGTH AND 100% FULL SCREEN HEIGHT FAILING NDT. REPAIRED THE PRESSURE BULKHEAD IAW REO.Aug 23, 2017 · N922EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2017091943769Skin · dentedLEFT INBOARD FLAP LOWER SKIN HAS A DENT .041 INCH DEEP AT THE INBOARD TRAILING EDGE. REPAIRED IAW REO.Jul 31, 2017 · N922EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2017091943768Skin · dentedRIGHT INBOARD FLAP LOWER SKIN HAS THREE DENTS ALONG INBOARD EDGE MEASURING .027 INCH DEEP, .072 INCH DEEP AND .041 INCH DEEP. REPAIRED IAW REO.Jul 31, 2017 · N922EV · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA201612121253Warning System · out of adjustOTBD COOL CAUTION MESSAGE AFTER TAKE OFF. QRH LED TO EMERGENCY DECOMPRESS. ADJUSTED SERVICE DOOR INDICATION SYSTEM IAW 52-70-06, OPS CHECKED GOOD.Dec 12, 2016 · N922EV · Cndair CL6002B19 · Door Warning SystemSDR ASOA2016061214922Landing Gear · malfunctionedHYDRALIC 3 CAUTION AND APU ON SELECTING GEAR DOWN LT AND MLG CAUTION MSG EMERGENCY ACTIONS, LANDING GEAR RETRACTION SYSTEM, PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYS IAW AMM 32-30-00. OPS CK GOOD AT THIS TIME. REMOVED AND STOWED GEARJun 12, 2016 · N922EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2015052212888Circuit Board · malfunctionedF/A NOTIFICATION LIGHT AT 11C & 11D AND ALSO EXIT SIGN ILLUMINATED MULTIPLE TIMES AT RANDOM. R & R PSU CIRCUIT BOARD IAW MM 25-28-54. OP'S CHECK GOOD.May 19, 2015 · N922EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015042712684Light · brokenWARDROBE FLOOR EMERGENCY FLOODLIGHT HAS BROKEN LENS AND BASE ASSEMBLY. DISCONNECTED THE ELECTRICAL LEADS TO THE WARDROBE EMERGENCY FLOODLIGHT. REMOVED THE BASE BY REMOVING 2 SCREWS. REMOVED THE LIGHT ASSY FROM THE WARDROBE. INSTALLED A NEW BASE BY SECURING Apr 19, 2015 · N922EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015042712683Angle · crackedCARGO DOOR SURROUND, CARGO SILL, FS 605.00 FLOOR ANGLE IS CRACKED. REMOVED CRACKED ANGLE AT FS 605 FLOOR CARGO DOOR STRUCTURE. TRANSFERED HOLES TO NEW ANGLE & DEBURRED IAW SRM 51-40-11 PG 1-2. INSTALLED NEW FLOOR ANGLE AT FS 605.00 IAW SRM 51-42-06, 51-42-10Apr 2, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712682Strap · corrodedFLOORBEAM STRAP FROM RBL 18 TO RBL 36 AT FS 559.00 IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-42-06. DRILLED NEW SERVICEABLE STRAP IAW SRM 51-40-11. INSTALLED STRAP IAW SRM 51-42-06.Apr 1, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042712681Skin · corroded2 EA FASTENERS, LOCATED AT JUST FWD OF FS 559+112, STR 23R ON EXTERNAL SKIN HAVE FILOFORM CORROSION AROUND FASTENER HEADS. FOUND CORROSION UNDER 6 MORE ROWS OF FASTENERS FWD OF FS 559+112. REMOVED 12 EA RIVETS AND REMOVED CORROSION IAW SRM 51-21-06. MAX MATApr 1, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015042712680Bracket · crackedAFT EQUIPMENT BAY RT SIDE DIRECTLY UNDER ACM HAS CRACKED BRACKET. REMOVED BRACKET IAW SRM 51-42-06. INSTALLED NEW BRACKET, IAW SRM 51-42-06.Apr 1, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712679Floor Support · corrodedLBL 27, FLOORBEAM IN CARGO COMPARTMENT HAS AREAS OF EXFOLIATION CORRSION FS 559+80- FS 559+112. COMPLIED WITH EC/TC REO:601R-53-00-005.Mar 31, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712678Intercostal · crackedRIGHT FS 621-625 INTERCOSTAL 601-35012-52 CRACKED AT STR 14R. REMOVED CRACKED INTERCOSTAL AT FS 621-FS 625 STR 14R IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL AT FS 621-FS 625, STR 14R IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM Mar 31, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712677Intercostal · crackedLEFT FS 621-625 INTERCOSTAL 601-35012-51, CRACKED AT STR 14L. REMOVED CRACKED INTERCOSTAL AT FS 621-FS 625, STR 14L IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL AT FS 621-FS 625, STR 14L IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRMMar 31, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712676Post · crackedFS 409+128, RBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RAD II AT WL 69 .250" LONG X 50 PERCENT FSH. BOTH FAILED NDT INSP. REMOVED VERTICAL POST ASSY AT FS 409+128, RBL 18. INSTALLED RBL 18 FS 409 POST IAW REO 601R-53-41-88Mar 30, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712675Post · crackedFS 409+128, BL 0, VERT POST RT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250" LONG X 50 PERCENT FSH. FAILED NDT INSP. REMOVED FS 409+128, BL 0 VERTICAL POST IAW SRM 51-42-06, 51-42-22. LOCATED, DRILLED AND SUBASSEMBLED NEW SERVICEABLE RMar 30, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712674Post · crackedFS 409+128, LBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RAD II AT WL 69 BOTH APPROX .250" LONG X 50 PERCENT FSH. BOTH FAILED NDT INSP. REMOVED FS 409+128, LBL 18 VERTICAL POST IAW SRM 51-42-06 AND 51-42-22. INSTALLED NEW POMar 30, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712673Seat Track · corrodedRT SIDE SEAT RAIL FS 549 AFT HAS SEVERAL AREAS OF HEAVY INTERGRANULAR CORROSION. COMPLIED WITH EC/TC REO 601R-53-00-055 REV A DATED 11/18/2011 AS WRITTEN. R & R SEAT TRACK.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712672Seat Track · corrodedRBL 27, CARGO FLOOR SEAT TRACK FS 559+80-FS 559+96 CORRODED AROUND SCREW HOLES. REMOVED RBL 27 CARGO FLOOR SEAT TRACK FS 559+80-FS 559+96 IAW SRM 51-41-2. REPLACED RBL 27 FLOOR SEAT TRACK W/601R38779-9 IAW AMM 53-01-05.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712671Seat Track · corrodedRBL 9 CARGO FLOOR SEAT TRACK FS 559+110 - FS 567 CORRODED AROUND SCREW HOLES. REMOVED CORRODED SEAT TRACK AT RBL 9 CARGO FLOOR AT FS 559+110 - FS 567 IAW SRM 51-41-04. LOCATED, DRILLED AND INSTALLED NEW CARGO SEAT TRACK PT 601R38779-49 AT RBL 9, FS 559+110 -Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712670Seat Track · corrodedRBL 9 FLOOR SEAT TRACK, CARGO, FS 559+84 - FS 559+96 CORRODED AROUND MOUNT SCREW HOLES. REMOVED RBL 9 FLOOR SEAT TRACK FS 559+84 -FS 559+96 IAW SRM 51-41-02. REPLACED RBL 9 SEAT TRACK W/601R38779-13 IAW SRM 51-40-11 AND AMM 53-01-05.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712669Floor Support · corrodedRBL 27, FLOORBEAM IS CORRODED AROUND SCREW HOLES FS 559+82-FS 559+104. COMPLIED WITH EC/TC REO 601R-53-00-005.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712668Floor Support · corrodedRIGHT CARGO FLOOR SILL HAS CORROSION AROUND SCREW HOLES FS 559+87-FS 562. COMPLIED WITH ECTC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV DATED 05/22/2013 AS WRITTEN.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712667Frame · corrodedFS 589 FRAME HAS LIGHT CORROSION ON LOWER FLANGE STR 27-25L. REMOVED FLOORBEAM AT FS 589 TO GAIN ACCESS IAW AMM 21-22-01-000-801. INSTALLED FLOORBEAM AT FS 589 IAW AMM 21-22-01-400-801. BLENDED FRAME 589 BETWEEN STR 27-25L SMOOTH REMOVING CORROSION IAW SRM Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015042712666Seat Track · corrodedLBL 27 FLOOR SEAT TRACK FS 559+80-FS 559+96 CORRODED AROUND SCREW HOLES. REMOVED LBL 27 FLOOR SEAT TRACK FS 559+80 - 559+86 IAW SRM 51-42-02. REPLACED LBL 27 FLOOR SEAT TRACK W/601R38779-9 IAW AMM 53-01-11-400-802.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712665Seat Track · corrodedLBL 9, FLOOR SEAT TRACK FS 559 - 559+88 IS CORRODED AROUND MOUNT SCREWS. REMOVED LBL 9 FLOOR SEAT TRACK FS 559+96-FS 559+88 IAW SRM 51-41-02. REPLACED LBL 9, FLOOR SEAT TRACK FROM FS 559+96 -559+88, W/601R38779-13 IAW AMM 53-01-05.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712664Floor Support · corrodedLBL 9 FLOORBEAM HAS SEVERAL AREAS EXFOLIATION AROUND SCREW HOLES FS 568-FS 621. REMOVED FLOORBEAM LBL 9, FS 568-FS 621. REMOVED, 3 FILLERS, 2 SEAT TRACK LUGS AND 1 SEAT TRACK SECTION AND INBD RIVETS ON FLOORBEAM LBL 9, FS 568-FS 621 IAW SRM 51-41-02 AND 51-4Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712663Seat Track · corrodedLBL 9, FLOOR SEAT TRACK, FS 559+4 - 559+80 CORRODED AROUND SCRW HOLES. REMOVED FLOOR SEAT TRACK AT LBL 9, FS 559+4 TO 559+80 IAW AMM 53-01-11-000-802. DRILLED UP NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. INSTALLED SERVICEABLE SEAT TRACK AT LBL 9 FS 559+4Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712662Seat Track · corrodedRBL 9, FLOOR SEAT TRACK FS 559+4 - 559+80 CORRODED AROUND SCREW HOLES. REMOVED RBL 9 FLOOR SEAT TRACK BETWEEN FS 559+4 - 559+80 IAW SRM 51-41-02. LOCATED AND DRILLED NEW SEAT TRACK IAW REO 601R-53-00-485. INSTALLED SERVICEABLE SEAT TRACK AT RBL 9, FS 559+4 Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712661Seat Track · corrodedLBL 9 FLOOR SEAT TRACK FROM FS 559+110-FS 569 CORRODED AROUND SCREW HOLES. R & R LBL 9 FROM FS 559+110-FS 569 W/601R38779-5 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042712660Floor Support · corrodedLBL 27 FLOORBEAM IN CARGO COMPARTMENT HAS AREAS OF EXFOLIATION CORROSION FS 621-FS 559+96. REMOVED FLOORBEAM CAP AT LBL 27 FOR REPLACEMENT IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW FLOORBEAM CAP AT LBL 27, PN 601R35031-263 IAW SRM 51-42-21 AND 5Mar 29, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712659Door Sill · corrodedCARGO DOOR SILL HAS SEVERAL AREAS OF CORROSION AROUND, +1 BETWEEN, NUTPLATE HOLE. REMOVED DAMAGED FLOOR SILL IAW SRM 51-42-02 AND 51-42-21. LOCATED AND DRILLED CARGO DOOR SILL IAW SRM 51-40-11. INSTALLED FABRICATED DOOR SILL IAW REO 601R-53-61-1574 AND SRM Mar 28, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712658Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .500 IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO:601R-53-61-1230 AND GREO:601R-53-61-1230, REV F, DATED 10/31/2011 AS WRITTENMar 28, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015042712657Bulkhead Web · crackedFS 280 WEB IS CRACKED OTBD OF RBL 9 IN RADIUS OF LOWER FLANGE. C/W ECTC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.Mar 28, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015042712656Floorbeam · crackedFS 621, LEFT FLOOR SUPPORT ANGLE CRACKED AT LBL 36. LOCATED AND DRILLED NEW FLOOR SUPPORT ANGLE, PN 601R53-61-117-1 IAW SRM 51-40-11. REPAIRED FS 621 LT FLOOR SUPPORT IAW REO 601R-53-61-5465. REO 601R-53-61-5465 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEENMar 28, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042712655Floor Support · corrodedLEFT PRESSURE FLOOR SILL HAS FILIFORM CORROSION IN MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559.00. C/W ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN. REO 601R-53-41-1892 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCMar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712654Floor Support · corrodedRIGHT PRESSURE FLOOR SILL HAS FILIFORM CORROSION IN MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. AREA AT FS 559, RBL 39 FOUND TO BE OUT OF LIMITS GREO 601R-53-4-666. COMPLETED CORROSION REMOVAL IAW GREO 601R-53-41-666.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042712653Seat Track · corrodedSEAT TRACK RAIL AT RBL 9 BETWEEN FS 364.0 TO FS 409+32 HAS PITTING AND INTERGRANULAR CORROSION IN MULTIPLE LCOATONS. REMOVED SEAT TRACK AT RBL 9 BETWEEN FS 364.00 TO FS 409+32 IAW AMM TASK 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK, 601R31032-15,Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042412652Seat Track · corrodedSEAT TRACK RAIL AT LBL 9 BETWEEN FS 364. TO FS 409+32 HAS PITTING AND INTERGRANULAR CORROSION IN MULTIPLE LOCATIONS. REMOVED SEAT TRACK AT LBL 9 BETWEEN FS 364.00 TO FS 409+32 IAW AMM TASK 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL 9 BETWEMar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015042412651Attach Angle · crackedANGLE ATTACHING TO INTERCOSTAL AT FS 484.0 AND LBL 27 IS CRACKED. REMOVED DAMAGED ANGLE AT FS 484, LBL 27 AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015042412650Attach Angle · crackedANGLE ATTACHING TO INTERCOSTAL AT FS 484.0 AND RBL 27 IS CRACKED. REMOVED DAMAGED ANGLE AT FS 484 AND RBL 27 AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015042412649Floorbeam · crackedFS 280.00 INBD AND OTBD FLOOR SUPPORT CLIP AT RBL 9 ARE CRACKED IN RADIUS. R & R INBD RBL 9.0 FLOOR SUPPORT CLIP AT FS 280.00, PN:601R31113-58 IAW SRM 51-42-21.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042412648Floorbeam · crackedFS 280.0 INBD FLOOR SUPPORT CLIP AT LBL 9 IS CRACKED IN UPPER RADIUS. R & R FLOOR SUPPORT CLIP AT LBL 9 IAW SRM 51-42-21.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042412647Attach Bracket · crackedPAX DOOR 3L LINTEL, ATTACH BRACKET JUST AFT OF FS 280 BULKHEAD IS CRACKED. REMOVED UNSERVICEABLE ANGLE AND LOCATED, DRILLED AND INSTALLED SERVICEABLE ANGLE PT 600-31057-19 IAW SRM 51-40-11, 51-42-06 AND 51-42-21.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015042412646Isolator · crackedFS 621 BULKHEAD, PANEL MOUNT ISOLATORS, 4, ARE CRACKED AT: LBL 27 BOTTOM, RBL 27 BOTTOM AND RBL 43 1ST AND 3RD FROM BOTTOM. IN ADDITION FOUND 6 MORE ISOLATORS CRACKED. R & R 10 ISOLATORS IAW SRM 51-42-10.Mar 27, 2015 · N922EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014072510968Fuse · blownMAIN CABIN ENTRANCE EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. R & R FUSES ON BATTERY PACK 2 IAW AMM 33-51-04, OPS CK GOOD.Jul 22, 2014 · N922EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014072510966Fuse · blownCABIN EXIT SIGN 50 PERCENT INOPERATIVE ABOVE ROW 8. R & R FUSES ON BATTERY PACK NR 2 IAW AMM 33-51-04. OPS CK GOOD, DEFER CLEARED PLACARD REMOVED.Jul 21, 2014 · N922EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014032510182Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT LBL 27.50, WL 132. CRACK APPEARS TO EXTEND UNDER DOOR TRACK. INSTALLED REPAIR IAW REO 601R-53-61-1541, REV E. MAJOR REPAIR IAW GMM 5-3.Mar 21, 2014 · N922EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
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