N922

Service difficulty reports not matched to an aircraft · 37

They name N922, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N922' AND registry_match IS NULL
  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 MASA20210625239Skin · dentedFUS FWD LH FS437 AREA NEAR STR 22L IS DENTED|REPAIRED SKIN STA 437 NEAR STR 27L IAW SRM 53-00-01Jun 25, 2021 · N922 · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR MASA20210625238Intercostal · corrodedFORWARD E&E BAY INTERCOSTAL CORRODED AT STGR 27L FS 349|R&R INTERCOSTAL IAW SRM 51-42-06Jun 25, 2021 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210618236Intercostal · corrodedINTERCOSTAL IN E+E BAY CORRODED AT STGR 27L AT FS364 |REMOVED CORROSION ON INTERCOSTAL IN E+E BAY AT STGR 27L AT FS364 IAW SRM 51-42-06Jun 18, 2021 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210614235Stringer · corrodedSTGR 27 FWD CORRODED AT FS284| R&R STGR 27 FWD AT FS284 IAW SRM 51-42-06 AND SRM 51-42-21Jun 14, 2021 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR MASA20210614234Intercostal · corrodedFWD E&E BAY INTERCOSTAL CORRODED RH SIDE FS319-FS333 STGR 20R|R&R INTERCOSTAL IAW SRM 51-42-06Jun 14, 2021 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210614233Track · damagedAFT BAGGAGE BAY FWD DOOR TRACK HAS DAMAGE AND BARE METAL|R&R AFT BAGGAGE BAY DOOR TRACK IAW REO 670-53-62-102Jun 14, 2021 · N922 · Cndair CL6002D24 · Cargo/Baggage DoorsSDR MASA20210611232Intercostal · corrodedFWD E&E BAY INTERCOSTAL CORRODED RH SIDE FS319-FS333|R&R INTERCOSTAL IAW SRM 51-42-06Jun 11, 2021 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210608229Post · corrodedR/H FLIGHT COMPARTMENT DOOR POST CORRODED|R&R FABRICATED REPAIR PARTS IAW SRM 53-00-00Jun 8, 2021 · N922 · Cndair CL6002D24 · Aerodynamic FairingsSDR MASA20210608228Floor Support · corrodedR/H FLIGHT COMPARTMENT FLOOR PANEL SUPPORT GUSSET CORRODED|R&R FLOOR SUPPORT GUSSET IAW SRM 51-42-06Jun 8, 2021 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR MASA20210607227Frame · corrodedFORWARD E&E BAY FRAME AT FS310 STGR 26L AND 26R |REMOVED AND REPAIRED FRAME SECTOR FS310 BETWEEN STGR 25R AND 25L IAW SRM 53-00-06Jun 7, 2021 · N922 · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019060431801Floorbeam · corroded"AWR; HIDDEN CRACK: [ DURING 280 RH FLOOR BEAM REMOTION RELATED WITH NR C 00141, A STIFFENER OF COCKPIT BULKHEAD, FWD FACE WAS FOUND CRAKED ]: CRACKED STIFFENER IN STA. FS= 280 AND 26RBL AND WL= 70 AT PAX CABIN F WD WET AREA. (W1) (CPAX) May 31, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019060431800Seal · torn"INITIAL INSPECTION: TORN SEAL ON FLAP FAIRING NBR. 597BB AT LH WING. AI) " "SUMMARY: SEAL ON FLAP FAIRING NBR. 597BB AT LH WING WAS CLEANED PER C RJ900 SRM 51-26-00-001-001-A01. AFTER OF May 31, 2019 · N922 · Cndair CL6002D24 · Emergency ExitsSDR REXA2019060429799Fitting · corroded"INITIAL INSPECTION: FREE PLAY ON BOTH LOWER ROD END LINKS [LH/RH ] AT NLG AFT DOOR. (FYT) " "SUMMARY OF NRC 163: HARDWARE ON NLG AFT DOOR WERE REPLACED PER CRJ 900 AMM 32-22-05 AND ALTERNATE EXTENSION TMay 29, 2019 · N922 · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2019060424798Stiffener · corroded"AWR; HIDDEN CRACK: [ DURING 280 RH FLOOR BEAM REMOTION RELATED WITH NR C 00141, A STIFFENER OF COCKPIT BULKHEAD, FWD FACE WAS FOUND CRAKED ]: CRACKED STIFFENER IN STA. FS= 280 AND 26RBL AND WL= 70 AT PAX CABIN F WD WET AREA. (W1) (CPAX) May 24, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060422797Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON MIDDLE C AP ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LO WER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. MIDDLE CAP ANGLE INMay 22, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060419795Support · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTI ON PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SER VICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: PROTECTION PLATE SUPPORT IN STMay 19, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060419794Support · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON CAP ANGL E IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SI LL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. CAP ANGLE IN STA. FSMay 19, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060419793Support · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER S RIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOW R SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. LOWER STRIKER IN STA. FMay 19, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060419792Support · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPORT M OUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE D OOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. SUPORT MOUNTING ANGLMay 19, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060419791Support · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTI ON PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERV ICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. PROTECTION PLATE SUPMay 19, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060419790Floorbeam · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTI ON PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERV ICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. PROTECTION PLATE SUPMay 19, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019060417788Floorbeam · corroded"INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS P ANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT. (CPIL) TCI 53-10-219 " "SUMMARY: AREA WAS MEASURED AND FOUND WIMay 17, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019060414787Stringer · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION. CORROSION ON STRINGER 26 RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TA SK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. STRINGER 26RH IN STMay 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019060414786Stringer · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION. CORROSION ON STRINGER 25 RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TA SK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. STRINGER 25RH IN STAMay 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019060414785Intercostal · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060414784Intercostal · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060414783Intercostal · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060414782Intercostal · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019060414781Stringer · corrodedCORROSION ON STRINGER 25RH IN STA. FS= 280 TO FS= 327 BETWEEN AT MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01.May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019060414780Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. THE PRODUCTION DOUBLER WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 PAR. 6.May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2019060414779Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 25LH AT MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01. "May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019060414778Stringer Splice · corroded[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09. STRINGER SPLICE WAS REPLACED PER S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA201906040777Stringer · corrodedCORROSION ON STRINGER SPLICE 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09. STRINGER SPLICE 25RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01.May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019060414776Stringer Splice · corroded"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 24RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09. STRINGER SPLICE 24RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-0May 14, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019051200775Frame · corrodedCORROSION ON FRAME FS= 349 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TAS K 900-53-140-300 APPENDIX A ] TCI: 100-09, CORROSION ON FRAME FS= 349 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 53-00-06-201May 12, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019060427773Tripler · gougedINITIAL INSPECTION: GOUGE ON PREVIOUS REPAIR TRIPLER IN STA. FS= 917 TO FS= 919.5 NEAR STGR 27 AT FUSELAGE SKIN. (FUS) SKIN TO STA. FS= 917 TO FS= 919.5 NEAR STGR 27 AT FUSELAGE SKIN WAS REPAIRED, PER CRJ-900 REO 670-53-00-290 REV.FMar 27, 2019 · N922 · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2019060470772Plate · corrodedWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 4RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2; PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41 RBMar 27, 2019 · N922 · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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