N902XJ

Service difficulty reports · 185

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 = 'N902XJ' 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 REXA2025021900205Lug · corroded"FOUND BUSHING LUG BORE LABELED ""F"" TO HAVE PITTING REQUIRES TO GO TO FIRST OVER REPAIRED LH AILERON BUSHING LUG BORE LABELED ""F"" IAW REO 670-57-61-237 REV -- DATED 2017-07-25."Feb 7, 2025 · N902XJ · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2025020500129Seat Track · corrodedRBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 349 TO F.S. 379. REMOVED UNSERVICEABLE RBL9 SEAT TRACK BETWEEN FS349-FS483 IAW CRJ 900 AMM 53-00-49-000-801-A19.INSTALLED NEW SERVICEABLE SEAT TRACK P/N SH670-32159-1 IAW CRJ900 AMM 53-00-49-400-801-A19Feb 4, 2025 · N902XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2025020500128Angle · corrodedPAX DOOR UPPER MID SILL ANGLE IS CORRODED REMOVED UNSERVICEABLE PAX DOOR UPPER MID SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-41-02-001-001-A01.INSTALLED NEW PAX DOOR UPPER MID SILL ANGLEP/N SH670-31825-9S IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-41Feb 4, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025020500127Angle · corrodedPAX DOOR UPPER FWD SILL ANGLE IS CORRODED. REMOVED UNSERVICEABLE PAX DOOR UPPER FWD SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR UPPER FWD SILL ANGLE P/N SH670-31821-5S IAW CRJ900 SRM 51-42-06-001-001-A01.Feb 4, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025021900204Angle · corrodedFOUND PAX DOOR KICKPLATE ANGLE (P/N: SH670-31875-1) TO BE CORRODED. INSTALLED NEW SERVICEABLE PAX DOOR KICKPLATE ANGLE (P/N: SH670-31875-1) IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.Feb 1, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025020500126Angle · corrodedPAX DOOR UPPER AFT SILL ANGLE IS CORRODED. INSTALLED AND SEALED NEW SERVICEABLE ANGLE SUPPORT P/N SH670-33332-5, AND RESTORED SURFACE FINISH ON RIVETS IAW CRJ900 SRM 51-42-13-001-001-A01, SRM 51-23-00-001-001-A01, AND SRM 51-25-16-001-001-A01.Jan 26, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025021900203Door Frame · crackedL/H FWD. OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED REPAIRED LH FWD EMERGENCY EXIT DOOR IAW REO 690-52-21-182 REV -- DATED 2025-02-02 AND REO 670-52-21-103 REV -- DATED 2024-11-06Jan 23, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2025021300194Door Frame · cracked"L/H AFT OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED COMPLIED WITH REO 690-52-21-181 REV -- DATED 2025-02-02 FOR DEVIATION TO STEP 1 OF REO 670-52-21-103 REV -- DATED 2024-11-06. RESTORED TO FINISH IAW CRJ-900 Jan 23, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2025021300193Fitting · cracked"RIGHT AFT OVERWING EMERGENCY EXIT DOOR UPPER ALIGNMENT SPADE FITTING SURROUNDING STRUCTURE IS CRACKED COMPLIED WITH REO 690-52-21-180 REV -- DATED 2025-02-02 FOR DEVIATION TO STEP 1 OF REO 670-52-21-103 REV -- DATED 2024-11-06. INSTALLED THE R/H AFT OVER WJan 23, 2025 · N902XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024050300367Fan · inoperativeFUMES/SMOKE CAME OUT OF ECS VENTS IN THE COCKPIT AND CABIN AFTER TAKE OFF. FUMES/SMOKE MOSTLY DISSIPATED DURING LANDING. REMOVED AND REPLACED THE #1 AND #2 RECIRCULATION FAN FILTERS PER CRJ 900 AMM 21-22-12. PERFORMED OPERATIONAL CHECK PER AMM 21-22-10 AND PERMay 1, 2024 · N902XJ · Cndair CL6002D24 · Air Distribution FanSDR REXA2022040400560Light · inoperativeLIGHT DS101 PINS BROKEN OFF IN CONNECTER REPLACED LIGHT DS101 IAW AMM 33-51-15 AND ESPM 20-16-05 P/N ON/OFF:2LA006954-00Apr 2, 2022 · N902XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2021090200650Stringer · corrodedSTR 22R IS CORRODED ON AFT SIDE OF F.S. 333.00. REQUIRES EVALUATION. R/R UNSERVICEABLE STGR 22R, STGR 22R SPLICE, AND STGR 22R CLEAT FS 333 TO 349 WITH SERVICEABLE STGR, SPLICE, AND CLEAT IAW SRM 51-42-06-001-001(A01), 51-40-11-001-001(A01).Sep 2, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200657Angle · corroded"RH IB FLAP LOWER SKIN CHAFED FROM CONTACT WITH IB CANOE FAIRING (683BB). FOUND CHAFE TO BE OUT OF LIMITS PER SRM 37-52-01-001-001-A01. REMOVED UNSERVICEABLE SKIN AND INSTALLED SERVICEABLE SKIN IAW SRM 57-52-01-201-005-A01. R & R SAME SERVICEABLE R/H I/B FAug 20, 2021 · N902XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2021090200655Stringer · corroded"STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJAug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200654Stringer · corrodedSTR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ 9Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200653Cleat · corroded"STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW SRAug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA2021090200652Stringer · corroded"STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED, AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ 9Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200651Stringer · corroded"STR 21R HAS MULTIPLE AREAS OF CORROSION FROM F.S. 333.00 TO 453.00. REMOVED STR 21R FROM FS 394 - FS 477 AND FROM FS 333 - FS 379. LOCATED, DRILLED AND INSTALLED NEW STR 21R FROM FS 333-379 AND 394-477 AND INCLUDING NEW STR SPLICES AND JOINT PIECES IAW CRJ Aug 17, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200678Stringer · corrodedSTRINGER 22R HAS CORROSION BTW BS 437 TO 453. CUT & REMOVED FROM SECTION FS 469 FOR ACCESS. REMOVED AND REPLACED STRINGER 22R FROM 394-477 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. REINSTALLED FROM SECTION FS 469 AND REPAIR SPLICE IAW CAug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200677Stringer · corrodedSTRINGER 22R HAS CORROSION BTW BS 437 TO 453. CUT & REMOVED FROM SECTION FS 469 FOR ACCESS- REMOVED AND REPLACED STRINGER 22R FROM 394-477 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. REINSTALLED FROM SECTION FS 469 AND REPAIR SPLICE IAW CRJAug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200674Frame · corrodedFRAME BS 379 HAS CORROSION BTW STR 20R TO STR 21R. REMOVED STR 22R AND 3 CLEATS AT ST 21, 22, AND 24R, REMOVED SPLICE FRAME AND ANGLE AT FS 379. REMOVED AND REPLACED RH REINFORCING ANGLE AND FRAME SECTION AT FS 379 BTW ST 20R-21R IAW CRJ 900 SRM 51-42-06-001Aug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2021090200673Frame · corrodedFRAME BS 379 HAS CORROSION BTW STR 20R TO STR 21R. REMOVED STR 22R AND 3 CLEATS AT ST 21, 22, AND 24R, REMOVED SPLICE FRAME AND ANGLE AT BS 379. REMOVED AND REPLACED RH REINFORCING ANGLE AND FRAME SECTION AT FS 379 BTW ST 20R-21R IAW CRJ 900 SRM 51-42-06-00Aug 16, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2021090200672Stringer · corrodedSTRINGER 20R HAS MULTIPLE AREAS OF CORROSION FROM BS 364 TO 409. REMOVED, LOCATED, DRILLED AND REPLACED STR 20R AT FS 364-469 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.Aug 15, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021090200679Frame · corrodedFOUND CORROSION AT BS 942, STRINGER 22R ON FRAME. REPAIRED THE BS 942 FRAME IAW CRJ 900 SRM 53-00-06-201-001-A03, 51-42-06-001-001-A01, 51-40-11-001-001-A01 & 53-51-06-101-003-A04.Aug 13, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2021090200675Joint · corrodedANGLE JOINT PIECE LOCATED BTW FS 379 TO FS 394 AT LEVEL STR 21R HAS CORROSION. REMOVED, LOCATED, DRILLED, DEBURRED, AND REPLACED ANGLE JOINT/STRINGER BETWEEN FS 379-394 STGR 21R IAW CRJ 900 SRM 51-47-06-001-001-A01 AND 51-40-11-001-001-A01.Aug 13, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021090200681Floor Support · corrodedFLOOR BEAM AT LBL27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000.00 TO FS 1098.00. REMOVED AND REPLACED FLOORBEAM AT LBL 27 FS 1000-1098 IAW CRJ 900 SRM 53-00-41-201-001-A03. RESTORED FINISH IAW SRM 51-25-00-001-001-A01.Aug 11, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021090200671Intercostal · corrodedINTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN FS. 349 TO 364. R & R UNSERVICEABLE INTERCOSTAL WITH A SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001(A01), 51-40-11-001-001-(A01) & 51-42-21-001-001-A01.Aug 10, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021090200680Frame · corrodedFRAME AT BS 954 CORRODED BETWEEN STRINGERS 25R AND 26R. PERFORMED CUT OUT OF FRAME AT STGR 27 AND REMOVED FRAME SECTION FROM STGR 20 TO 27 @ 954 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 53-00-06-201-001-A03. PERFORMED EDDY CURRENT OFAug 8, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2021090200667Fitting · corrodedRIGHT AILERON CENTER FITTING, INBD BUSHING LUGS FOUND TO BE CORRODED UPON REMOVAL OF BUSHINGS. REPAIRED RH AILERON CENTER FITTING INBD BUSHING LUGS IAW REO 670-57-61-237 REV-.Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Elevator StructureSDR REXA2021090200664Angle · corrodedPAX DOOR ACCESS HOLES 832 AL, 832 BL, 83 DL, 832 EL, AND 832 FL HAVE INTERNAL SKIN CORROSION. LOCATED, DRILLED, AND INSTALLED NEW PAX DOOR FWD DRAG ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 38.Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200662Skin · corrodedPAX DOOR ACCESS HOLE 832 JR HAS A CORRODED FASTNER HOLE. AFTER FURTHER INVESTIGATION FOUND PAX DOOR INNER SKIN TO REQUIRE REPLACEMENT R/R PAX DOOR INNER SKIN IAW CRJ 900 SRM 51-40-11-001-001(A01) & 51-42-06/13/21/22-001-001(A01).Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200658Web · crackedPAX DOOR FWD WEB BOTTOM FASTNER FLANGE FOR PNL 832 CT IS CRACKED. LOCATED AND DRILLED NEW PAX DOOR FWD STAIR WEB P/N 601R317071-12 AND INSTALLED SUPPORT ANGLES ONTO NEW WEB IAW CRJ 900 SRM 51-40-11-001- 001-A01 AND 51-42-06-001-001-A01 REV 38.Aug 6, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200666Fitting · chafedFLAP STUB FAIRING 172 DR FWD MOUNTING BRACKET CHAFED. R & R UNSERVICABLE FLAP STAB FAIRING BRACKET WITH SERVICABLE BRACKET IAW CRJ 900 SRM 51-42-21-001-001(A01) & 51-25-06/16-001-001(A01).Aug 5, 2021 · N902XJ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2021090200663Angle · corrodedPAX DOOR ACCESS HOLE 832DR HAS INTERNAL SKIN CORROSION. LOCATED, DRILLED AND INSTALLED NEW PAX DOOR AFT DRAG ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 38.Aug 4, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200661Panel · corrodedPAX DOOR AFT WEB BOTTOM FASTNER FLANGE FOR STEP PNL 832 BT IS CORRODED. LOCATED AND DRILLED NEW PAX DOOR AFT STAIR WEB AND INSTALLED SUPPORT ANGLES ONTO NEW WEB IAW SRM 51-40-11-001- 001-A01 AND 51-42-06-001-001-A01 REV 38.Aug 4, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200668Former · corrodedUPON REMOVAL OF PAX DOOR INNER SKIN FOUND FWD FORMER P/N 601R318031-5 TO BE CORRODED BEYOND LIMITS. FORMER REQUIRES REPLACEMENT. REMOVED MID AND LOWER TENSION TIES IAW AMM 52-11-19-000-801-A01 REV 67. REF MWC 81513131/301 FOR TENSION TIE INSTALL. REMOVED FAug 2, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200665Seat Track · damagedLEFT AND RIGHT SIDE SEAT TRACKS BETWEEN BS 744.15 AND 761.85 HAVE SCRATCHES AND GOUGES AT THE FWD ENDS.Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021090200660Panel · corrodedPAX DOOR AIRSTAIR TOP COVER PLATE FASTNER HOLES ARE CORRODED. FOUND PAX DOOR TO HAVE SEVERAL AREAS OF CORROSION. REMOVED, LOCATED, DRILLED AND INSTALLED STIFFENERS IAW SRM (51-45-00-001-001-A01), (51-42-06-001-001-A01), (51-40-11-001-001-A01 (51-40-11-0Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200659Stiffener · corrodedPAX DOOR AIRSTAIR TOP COVER PLATE FASTNER HOLES ARE CORRODED. FOUND PAX DOOR TO HAVE SEVERAL AREAS OF CORROSION. REMOVED, LOCATED, DRILLED AND INSTALLED STIFFENERS IAW SRM CRJ 900 (51-45-00-001-001-A01), (51-42-06-001-001-A01), (51-40-11-001-001-A01, (5Aug 2, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200670Angle · crackedPAX DOOR POWER-ASSIST MOTOR UPPER ATTACH ANGLE P/N 601R317745-7 IS CRACKED. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW CRJ 900 SRM 51-40-4-001-001-A01. REV 38. REF MWC 81513131/200 FOR ANGLE INSTALL.Aug 1, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200669Cleat · corrodedUPON REMOVAL OF PAX DOOR INNER SKIN FOUND FWD MID CLEAT P/N 600-31902-269 CORRODED BEYOND LIMITS. REMOVED AND REPLACED WITH NEW P/N 600-31902-269 CLEAT IAW SRM 51-42-06-001-001-A01 REV 38.Aug 1, 2021 · N902XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021090200656Angle · corroded"FWD WING TO FUSELAGE FAIRING SUPPORT INTERCOSTAL BETWEEN F.S. 661.00+62 AND F.S. 661.00+90 BELOW THE FWD KEEL BEAM HAS CORROSION IN FASTENER HOLES. R & R UNSERVICEABLE INTERCOSTAL WITH A SERVICEABLE INTERCOSTAL BETWEEN FS 661+62 AND 661+90 IAW CRJ900 SRM 51-Aug 1, 2021 · N902XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020071400595Light · inoperativeEMERGENCY EXIT SIGN ON G1 NEXT TO SVC DOOR HAS BULBS INOP. RELAMPED EMERGENCY EXIT SIGN ON G1 NEXT TO SVC DOOR IAW AMM 33-51-05.Jul 7, 2020 · N902XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2019072901142Light · inoperativeEMERGENCY LIGHT NEAR SERVICE DOOR INOP. (CREW NOTED) RELAMPED EXIT LAMP SIGN BULB # 'S OL3071BPE/GPL.Jul 29, 2019 · N902XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2019070901112Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 333 BETWEEN STR 25L TO 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. FRAME IN STA. FS= 333 BETWEEN STR 25L TO 25R AT INTERNAL STRUCJul 9, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019070801116Stringer · corrodedINITIAL INSPECTION: CORROSION STR 25R BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STR 25R BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICSJul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019070801115Stringer · corrodedINITIAL INSPECTION: CORROSION STR 26L BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGER 26L BTW FS=280 AND FS=333 ATINTERNAL STRUCTURE OF MAIN AVIONICSJul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019070801114Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 319 BETWEEN STR 25L TO 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. FRAME IN STA. FS= 319 BETWEEN STR 25L TO 25R AT INTERNAL STRUCJul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019070801113Stringer · corrodedINITIAL INSPECTION: CORROSION STR 27 BTW FS=295.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGERS 27 BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIOJul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019070801111Stringer · corrodedINITIAL INSPECTION: CORROSION STR 26R BTW FS=280.00 / FS=333.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00084 TASK 900-53-140-300 APPENDIX A ]. NEW STRINGER 26R BTW FS=280 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICJul 8, 2019 · N902XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
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