N584NN

Service difficulty reports · 64

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 = 'N584NN' 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 VNAA2026010811101Mcu · faultedSTAB TRIM RUNAWAY ON APPROACH / INTERROGATED MDC FOUND B1 CODE 007955 UNDER DIRECTION FROM MOC AND TROUBLESHOOTING IAW FIM 27-42-07-810-809-A01. REMOVED AND REPLACED MCU IAW AMM 27-42-07-000/400-801-A01. OPS CHECKS GOOD. MCU REMOVED PN 7074-5 SN 1002Jan 6, 2026 · N584NN · Cndair CL6002D24 · Stabilizer Control SystemSDR VNAA2025031911101Elec Connector · unserviceableANTI SKID INBD CAUTION MSG/ WITH IND GRND SPOILER FAULT STAUS MSG. / DISASSEMBLED CONNECTOR AT WHEEL SPEED TRANSDUCER AND FOUND TO BE UNSERVICEABLE. REMOVED AND REPLACED CONNECTOR IAW CRJ900 AMM 32-61-05-000/400-803. OPS CHECK GOOD AND BITE TEST GOOD.Mar 17, 2025 · N584NN · Cndair CL6002D24 · Landing Gear System WiringSDR VNAA202407110030Intercostal · corrodedSECONDARY NRC: AFTER FRAME REMOVAL IN REF NRC 00130, CORROSION ON INTERCOSTAL STGR 27 BLW FS1031.00 AND FS1047.00. CORROSION ON INTERCOSTAL STGR 27 BLW FS1031.00 AND FS1047.00 WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED, THEREFORE IT IS WHIJun 20, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407110019Doubler · wornIN REF TO JOBCARD 275000·218_R/H.JIC: WEAR ON FLAP VANE ACTUATOR #3 AREA (INNER SKIN) WEAR ON FLAP VANE ACTUATOR #3 AREA (INNER SKIN) WAS REPAIRED PER REO 670-57-52-352 REV --Jun 20, 2024 · N584NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202407110027Unknown · corrodedSECONDARY NRC FROM NRC 00128': AFTER REMOVAL, CORROSION ON STRAY ASSY FS 280.00. LH SIDE. CORROSION ON STRAY ASSY FS 280.00. LH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED UNDER NRC 00128.Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407110026Frame · corrodedCORROSION ON FRAME FS 1047.00 BTW STGR 27 TO STGR 26 LH. CORROSION ON FRAME STA 1051.30 BTW STGR 27 TO STGR 26 LH WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PER CRJ900 SRM 53-61-06-101-003-A02 THEREFORE WAS REPLACED PER CRJ90Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202407110016Seat Track · corrodedCORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS1002.00. (3EA). SEAT RAILS OF RBL9 BTW FS693.00 TO FS1002.00. (3EA) ARE OUT OFF LIMITS PER CRJ-900 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110015Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL27 BTW FS485.00 TO FS581.00 (2EA). DUE TO ONLY ONE TYPE OF DAMAGE IS ALLOWED AT ANY TYPICAL CROSS-SECTION, SEAT RAILS OF LBL27 BTW FS485.00 TO FS581.00 (2EA) ARE OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 THEREFORE WERE REJun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110014Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS379.00 TO FS693.00 (5EA). SEAT RAIL OF LBL9 BTW FS379.00 TO FS693.00 (5EAS) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49(CONFIG A12 )Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110011Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA). LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 CONF(A12)Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110010Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BLW FS485.00 TO FS720.85.00 (4EA). LH SIDE SEAT RAIL BLW FS485.00 TO FS720.85.00 (4EA) WERE EVALUATED, ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACE PER Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110008Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 (A12)Jun 5, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110024Floorbeam · corrodedSECONDARY NRC FROM NRC 00084': AFTER REMOVAL, CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ-900 SRM 5Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202407110023Floorbeam · corrodedCORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-10-001-Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202407110022Bracket · crackedDURING INSPECTION, CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, RH MAIN FUEL TANK. PER REO 670-57-42-577. REV.--Jun 4, 2024 · N584NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202407110021Bracket · crackedDURING INSPECTION, CRACK AT SLAT TRACK CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. CANISTER WELDED BRACKET NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577. REV.--Jun 4, 2024 · N584NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202407110017Seat Track · corrodedCORROSION ON SEAT RAILS OF LBL9 BTW FS693.00 TO FS1002.00. (3EA) SEAT RAILS OF LBL9 BTW FS693.00 TO FS1002.00. (3EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49 CONF(A12Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110009Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ-900Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407110007Angle · corrodedCORROSION ON ANGLE MID CAP AT LOWER PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON ANGLE MID CAP AT LOWER PASSENGER DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PER CRJ 900 SRM 53-21-23-101-001-A02, THEREFOJun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407100010Bracket · corrodedCORROSION ON PLATES (02 EAS) AND BRACKETS, MACHINED (07 EAS) OF INTERNAL STRUCTURE AT FWD & CTR CARGO COMPARTMENT. PAINT ON PLATES (02 EAS) AND BRACKET MACHINED (49 P) FS.517.00 STGR.23LH OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS REMOVED PER SRM 51-2Jun 4, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407110025Bulkhead Web · corrodedSECONDARY NRC FROM NRC 00084': AFTER REMOVAL, CORROSION ON RH LOWER WEB AT BULKHEAD FS 280.00 RBL 12 ABOVE FLOOR. CORROSION ON RH LOWER WEB AT BULKHEAD FS 280.00 RBL 12 ABOVE FLOOR WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPAIREDJun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, BulkheadSDR VNAA202407110013Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS720.85. (6EA). SEAT RAILS OF RBL9 BTW FS349.00 TO FS720.85. (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49(CONFIG A12)Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202407110006Rib · crackedIN REFERENCE TO RC TRFKE001TV3L': AFTER INTERNAL ZONAL INSPECTION, CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-359 REV -.Jun 3, 2024 · N584NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202407110005Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-1Jun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202407110004Post · corrodedDURING INSPECTION OF THE TASK CARD 53-10-219B, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00. CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00 WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS PEJun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, BulkheadSDR VNAA202407100002Skin · damagedLIGHTNING STRIKE ON EXTERNAL SKIN OF FWD/CTR BAGGAGE-BAY DOOR (REAR LOWER CORNER). REPAIRED PER REO 690-52-35-420. REV. -- AND PER REO 690-52-35-421. REV. --Jun 3, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA202407090005Skin · damagedIN REF. TRFKE00BFL7B:REO 690-53-00-532.1500FH PERM REPAIR - TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS BTW FS379.00-FS437.00 & STR25L-STR27 AND FS897.00- FS913.00 & STR2L-STR3L WITHIN 1500FH ACCOMPLISH APERMANENT REPAIR IAW APPROVED PROCEDUJun 3, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202407110003Floor Support · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00, DUE EXCESSIVE CORROSIÓN ON FLOOR SUPPORT ANGLE UPPER FACE AT FS 280 BTW RBL 9.00 AND LBL 9.00 ITS OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01. PER SRM 51-42-06-001Jun 2, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407110002Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS=333.00 TO FS= 364.00 AT MAIN AVIONICS COMPARTMENT. SUMMARY:EVALUATED, DUE TO EXCESIVE DAMAGE ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS=333.00 TO FS= 364.00 PER CRJ-900Jun 1, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407110001Skin · corrodedINITIAL INSPECTION: CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. DOOR CUT-OUTINNER SKIN AT E/E MAIN COMPARTMENT WAS REPAIRED PER REO 690-53-21-032 REV--.Jun 1, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202407100004Skin · dentedDENT BTW FS310.00 TO FS319.70 AND STGR27 TO STGR26 RH SIDE AT EXTERNAL FUSELAGE SKIN. DENT BTW FS310.00 TO FS319.70 AND STGR27 TO STGR26 RH SIDE AT EXTERNAL FUSELAGE SKIN WAS REPAIRED PER REO 670-51-00-085 REV-A AND PER REO 690-53-21-1784 REV--May 31, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202407100009Door Sill · corrodedINITIAL INSPECTION: CORROSION ON LOWER SILL OF AFT BAGGAGE-BAY DOOR CUT OUT. LOWER SILL OF AFT BAGGAGE-BAY DOOR CUT OU WAS EVALUATED, THE BLEN DEPTH EXCEEDED 0.016,THEREFORE IS OUT OF LIMITS PER CRJ900 SRM 53-61-23-201-001-A01 AND REPLACED PER CRJ900 SRM 51May 30, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407100008Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER REO 690-53-11-1775 REV.--May 30, 2024 · N584NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202407090002Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) REPAIRED PER CRJ 900 SRM 55-31-00-201-001-A01May 30, 2024 · N584NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202407090001Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01May 30, 2024 · N584NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202407100007Skin · nickedINITIAL ISPECTION:SEVERAL NICKS ON INBD FLAP FLS 15.00 TO FLS 75.60 AT LH WINGSEVERAL NICKS ON INBO FLAP FLS 15.00 TO FLS 75.60 AT LH WING WERE BLENOEO OUT PER CRJ900 SRM 51-12-00-001-001-A01 ANO WERE EVALUATEO BTW FLS15 TO FLS45 OUT OF LIMITS ANO BTW FLS45 TOMay 29, 2024 · N584NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202407100006Panel · wornINITIAL INSPECTION: WEAR ON LEADING EDGE PANEL 622AR, 622BR AND 631AR AND 531AL AT RH/LH WING. WEAR ON LEADING EDGE PANEL 622AR, 622BR AND 631AR AND 531AL AT RH/LH WING WERE REPAIRED PER REO 690-57-41-432 REV- -AND REO 690-57-41-431 REV- -May 29, 2024 · N584NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202407100005Skin · nickedINITIAL INSPECTION: SEVERAL NICKS BTW FS1000.00 TO FS1051.30 AND STGR#27 TO STGR#24RH SIDE AFT FUSELAGE. SEVERAL NICKS BTW FS1000.00 TO FS1051.30 AND STGR#27 TO STGR#24RH SIDE AFT FUSELAGE WERE REPAIRED PER REO 690-53-61-1410 REV -May 29, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202407100003Skin · wornIN REFERENCE TO RC TRFKE000YNZV': WEAR ON INNER SKIN IN FWD/CTR BAGGAGE BAY DOOR. WEAR ON INNER SKIN IN FWD/CTR BAGGAGE BAY DOOR REPAIRED PER REO 690-52-35-428 REV--AND REO 690-52-35-427REV -May 29, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA202407100001Arm · wornIN REFERENCE TO RC TRFKE001RPE1': WEAR ON FWD/AFT COUNTERBALANCE ARMS AT FWD/CTR BAGGAGE BAY DOOR. WEAR ON FWD/AFT COUNTERBALANCE ARMS AT FWD BAGGAGE BAY DOOR AND WEAR ON AFT COUNTERBALANCE ARMS AT CTR BAGGAGE BAY DOOR WERE REPAIRED PER REO 690-52-35-418 REV.May 29, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA202407090009Skin · damagedIN REF. TRFKE00C9EWX:EA A1-690-55-00012. 526.07FH PERM REPAIR- RH ELEVATOR UPPER SKIN TRAILING EDGE LIGHTNING STRIKE DAMAGE 1. WITHIN 526.07 FH'S. (BEFORE 19,075.19 FH) FROM SECTION I REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURESMay 29, 2024 · N584NN · Cndair CL6002D24 · Elevator, Plate/SkinSDR VNAA202407090008Skin · damagedIN REF. TRFKE00C9ELU:REO 690-57-21-456. 560FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED LIGTHNING STRIKE DAMAGE TO LH WING LOWER PLANK BETWEEN WS264.00-WS274.00 AND STR22-STR23 WITHIN 560FH, PERFORM A PERM REPAIR IAW APPROVED PROCEDURES. NOTE: ROTO/SHOT May 29, 2024 · N584NN · Cndair CL6002D24 · Wing, Plate/SkinSDR VNAA202407090007Fireshield · chafedIN REF. TRFKE00BY829:670-54-23-1164. 1500FH PERM REPAIR - SPEED TAPE APPLIED - CHAFE DAMAGE TO FWD CORE COWL FIRESHIELD PERMANENT REPAIR CORE COWL DUE TO DENT/CHAFE DAMAGE, SEE W.O. OR L.B. AND 670-54-23-1164 FOR DETAILS. CHAFE DAMAGE TO FWD CORE COWL FIRESHMay 29, 2024 · N584NN · Cndair CL6002D24 · Nacelle/Pylon, Bulkhead/FirewallSDR VNAA202407090006Fireshield · chafedIN REF. TRFKE00BMX8D:EA A1-690-54-00008.1265FH PERM REPAIR - RH CORE COWL FIRE SHIELD CHAFE DAMAGE WITHIN 1265 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. RH CORE COWL May 29, 2024 · N584NN · Cndair CL6002D24 · Nacelle/Pylon, Bulkhead/FirewallSDR VNAA202407090004Arm · wornIN REF. TRFKE009EULT:EA 22-C9-52-1205. PERM REPAIR - CENTER BAGGAGE BAY DOOR WITHIN 3,927.79 FHS FROM IR (BEFORE 19,075.19 FH), REPAIR, OR REPLACE THE DISCREPAN! ÍTEM IN ACCORDANCE WITH APPROVED PROCEDURES, WEAR ON FWD COUNTERBALANCE ARMS AT CENTER BAGGAGE BAYMay 29, 2024 · N584NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA202407090003Fireshield · wornIN REF. TRFKE0095XD2:EA22-C9-54-0939. PERM REPAIR - LH ENGINE FWD CORE COWL FIRE SHIELD WITHIN 4270.48 FLIGHT HOURS FROM IR (BEFORE 19,075.18 FH'S) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. REPAIRED PER REO.NO .690-54-23-3May 29, 2024 · N584NN · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR VNAA202407110029Fitting · corrodedCORROSION ON CENTER FITTING BORE LUGS L1, L2, L5 AND L6 AT LH AILERON. CORROSION ON CENTER FITTING BORE LUGS L1, L2, L5 AND L6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV --May 14, 2024 · N584NN · Cndair CL6002D24 · AileronsSDR VNAA202407110028Fitting · corrodedCORROSION ON CENTER FITTINGS AT RH AILERON LUG HOUSING R1,R2,R3,R4,R5 AND R6. CORROSION ON CENTER FITTINGS AT RH AILERON LUG HOUSING R1,R2,R3,R4,R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV --May 14, 2024 · N584NN · Cndair CL6002D24 · AileronsSDR VNAA202407110020Floorbeam · crackedAFTER REMOVAL, CRACK ON FWD FLOOR SUPPORT ANGLE AT 280 FLOOR STRUCTURE. FLOOR SUPPORT ANGLE AT FS280 FLOOR STRUCTURE CRJ900 SRM 53-11-43-001-001-A01 ITEM 137May 14, 2024 · N584NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202407110018Hinge Fitting · wornAFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL #2103 REV.B.May 14, 2024 · N584NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
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