N166PQ
Service difficulty reports · 155
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 = 'N166PQ' 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.
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 = 'N166PQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR REXA2020010726028Floor Support · corroded"INITIAL INSPECTION: CORROSION ON FLOOR SILL RH BTW FS.310 TO FS319 AT MAIN CABIN PASSENGER DOOR (SM)
"FLOOR SILL RH BTW FS. 280 TO FS319 AT MAIN CABIN PASSENGER DOOR WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 SDR REXA2020010725033Stringer · corroded"AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 18R BTW FS280/310 WAS FOUND IN REF EO: R25120 (SM)[E/E].
"SUMMARY OF NRC 00365 CORROSION LEVEL 2:STGR 18SDR REXA2020010725015Stringer · corroded"INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 27 BTW FS310/FS364 (SM)[E/E].
"SUMMARY OF NRC 00227 CORROSION LEVEL 2:STGR 27 BTW FS310/FS364 WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 ANDSDR REXA2020010750004Latch · damaged"INITIAL INSPECTION : ELONGATED HOLE ON COAMING LATCH DOOR AT UPPER HALF TRANSCOWL LH ENGINE ( MOT 1 )
""SUMMARY:ON NRC 00046: DOUBLER COAMING LATCH DOOR WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND SRM 51-42-06SDR REXA2020010740003Spigot · worn"INITIAL INSPECTION : WEAR ON SPIGOT AT LATCH DOOR ASSEMBLY OF UPPER HALF TRANSCOWL RH ENGINE ( MOT 2 )
"SUMMARY OF NRC 0040: SPIGOT AT LATCH DOOR ASSEMBLY OF UPPER HALF TRANSCOWL RH ENGINE WAS REPLACED PER CRJ-900 SRM 51SDR REXA2020010722039Angle · corroded"AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON ANGLES AT STGR 20R BTW FS310/364 WAS FOUND IN REF EO: R25120 (SM)[E/E].
""2 ANGLES WERE FABRICATED PER EA CRJ953-10066 SDR REXA2020010722024Door Sill · corroded"INITIAL INSPECTION: CORROSION ON LOWER SILL ANGLE AT GALLEY SERVICE DOOR SURROUND STRUCTURE (SM)(FUS)(TCI:53-20-219)
"SUMMARY OF NRC 00308: LOWER SILL ANGLE AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-0SDR REXA2020010720016Stringer · corroded"INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON STGR SPLICE 26R AT FS333 (SM)[E/E].
"SUMMARY OF NRC 00231: SPLICE 26R AT FS333 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 SDR REXA2020010719031Floorbeam · damaged"HIDDEN DAMAGE: ELONGATED HOLES ON STRIP UPPER SPLICE CROSSBEAM FS280 IN REF NRC 00178 (SM)[CPIL].
"SUMMARY OF NRC 00354: STRIP UPPER SPLICE CROSSBEAM FS280 WAS REPLACE PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-SDR REXA2020010719020Doubler · corroded"HIDDEN DAMAGE: IN REFERENCE JOB CARD 900-34-900-702, CORROSION ON SETTLEMENT DOUBLER AREA (4EAS) AT RADIO ALTIMETER ANTENNA (SM)
""SUMMARY: OF NRC 00264: REPAIR PARTS OF SETTLEMENT DOUBLER AREA (4EAS) AT RADIO ALTIMETER ANTENNA WERE FABRICATED PESDR REXA2020010729012Stringer · corroded"INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 25R FROM FS295/FS349 (SM)[E/E].
"SUMMARY: ON NRC. 00220, CORROSION LEVEL 2. STGR 25R FROM FS295/FS349 WAS REPLACED PER CRJ-900 SRM 51-21-06-001-001-ASDR REXA2020010718014Stringer · corroded"INITIAL INSPECTION: (DUE WET INSULATIONS) MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 25L FROM FS295/FS349 (SM)[E/E].
"SUMMARY: ON NRC. 00222 CORROSION LEVEL 2. STGR 25L FROM FS295/FS349 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-ASDR REXA2020010702030Floorbeam · damaged"HIDDEN DAMAGE: ELONGATED HOLES ON RIGHT ANGLE CAP CROSSBEAM FS280 IN REF NRC 00299 (SM)[CPIL].
"RIGHT ANGLE CAP CROSSBEAM FS280 WAS REPLACE PER CRJ/900 SRM 51-42-13-001-001-A01 SDR REXA20200107029Floorbeam · elongated"HIDDEN DAMAGE: ELONGATED HOLES ON LEFT ANGLE CAP CROSSBEAM FS280 IN REF NRC 00178 (SM)[CPIL].
"SUMMARY: ON NRC. 00352, LEFTT ANGLE CAP CROSSBEAM FS280; WAS REPLACEDPER CRJ/900 SRM 51-42-13-001-001-A01 SDR REXA2020010716035Stringer · corroded"AWR HIDDEN DAMAGE: AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON STGR 20R BTW FS280/319 WAS FOUND IN REF EO: R25120 (SM)[E/E].
"SUMMARY OF NRC:00367; STGR 20RH BTW FS280/319 SDR REXA2020010716023Floorbeam · corroded"INITIAL INSPECTION: CORROSION ON CROSSBEAM FS280.00 AT RBL12 (SM)[CPIL].
""SUMMARY: ON NRC. 00299 CORROSION LEVEL 2. CROSSBEAM FS280.00 AT RBL12 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-00SDR REXA2020010714027Seat Track · corroded"INITIAL INSPECTION: CORROSION ON SEAT RAIL LBL 9 OF THE PASSENGER CABIN BTW FS.333 TO FS469 (SM)
"SUMMARY: ON NRC. 00324, CORROSION LEVEL 2. SEAT RAIL LBL 9 OF THE PASSENGER CABIN BTW FS.333 TO FS469 WAS REPLACEDSDR REXA2020010724026Seat Track · corroded"INITIAL INSPECTION: CORROSION ON SEAT RAIL RBL 9 OF THE PASSENGER CABIN BTW FS.333 TO FS469 (SM)
"SUMMARY: ON NRC. 00323, CORROSION LEVEL 2. SEAT RAIL RBL 9 OF THE PASSENGER CABIN BTW FS.333 TO FS469 WAS REPLACEDSDR REXA2020010740021Bracket · cracked"INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LHMAIN FUEL TANK. (SM)
"SUMMARY: ON NRC. 00297 CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER CRJ-900 REO 670-57-42-SDR REXA2020010724010Floorbeam · corroded"INITIAL INSPECTION: CORROSION ON CROSSBEAM FS280.00 AT LBL12 (SM)[CPIL].
"SUMMARY: ON NRC. 00178, CORROSION LEVEL 2. CROSSBEAM FS280.00 AT LBL12 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001SDR REXA2020010712022Bracket · cracked"INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT RHMAIN FUEL TANK. (SM)
"SUMMARY: CANISTER, WELDED NO.3 IN STA WS148 AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --SDR REXA2020010720009Floorbeam · corroded"INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE AT FS280.00 LBL9 TO RBL9 (SM)[CPIL].
"SUMMARY ON NRC 00177: CORROSION LEVEL 2, FLOOR PANEL SUPPORT ANGLE AT FS280.00 LBL9 TO RBL9 WAS REPLACED PER CRJ-900SDR REXA2020010721032Bulkhead Web · corroded"HIDDEN DAMAGE: CORROSION ON BULKHEAD WEB CROSSBEAM FS280.00 AT LBL12 IN REF NRC 00178 (SM)[CPIL].
"SUMMARY: ON NRC. 00356, CORROSION LEVEL 2. WEB CROSSBEAM FS280.00 AT LBL12 WAS REPAIRED PER CRJ-900 SRM 53-11-10-201SDR REXA2020010792019Intercostal · corroded"AWR: HIDDEN DAMAGE ; AFTER REMOVE INSULATION ON MAIN AVIONICS COMPARTMENT, CORROSION ON INTERCOSTAL AT STGR 21L AND FS310/319 WAS FOUND IN REF EO: R25120 (SM) [E/E].
"SUMMARY:INTERCOSTAL AT STGR 21L AND FS310/319SDR REXA2020010724025Seal · torn"AWR. HIDDEN DISCREPANCY: TORN SEAL IN APU TAILCONE EXHAUST CONE ASSY [IN REF NRC 187] (APU) (SM).
"B-SEAL AFT WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND AMM 49-81-00-960-802. SDR REXA2018031600194Clamp · looseFA REPORTED THAT GALLEY HEAT HAS A BURNED ODOR. REMOVED AND REPLACED THE GALLEY HEATER IAW AMM 21-23-64. OPS CHECKED, THERE WAS NO FLOW OF AIR FROM THE GALLEY VENT. REMOVED DEBRIS FROM THE DUCT, PERFORMED AN OPS CHECK IAW 21-23-64. AIR FLOW AND HEAT OPERATSDR ASOA20161106125Seat Track · corrodedSEAT TRACK AT BS 744 - 761 IS CORRODED. REPAIRED IAW REO670-53-00-343 REV K., AND REO 670-53-00-343 REVM. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106124Seat Track · corrodedSEAT TRACK AT BS 661+46 - 661+90 IS CORRODED. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07, REO 670-53-00-343 AND EC/TC REO 670-53-00-343. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106123Seat Track · corrodedSEAT TRACK AT BS 661+16 - 667 IS CORRODED. COMPLIED WITH EC/TC REO670-53-00-343 REV M. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106122VCrossbeam · corrodedAFTER REMOVAL OF CORRODED PACKER BS 333 RBL 9, FOUND CORROSION ON CROSSBEAM. COMPLIED WITH EC/TC EA 32-2016-189 AND EA 32-2016-189. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106121Floor Support · corrodedFLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND DWG SH670-31810. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106120Floor Support · corrodedRT FLOOR SUPPORT HAS CORROSION FROM BS 280 - 319. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-41-11-001-001-A01, 51-42-13-001-001-A01, AND DWG SH690-32170. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA201611061190Floor Support · corrodedRT FLOOR SUPPORT HAS CORROSION AT BS 349+8.0 COMPLIED WITH EC/TC EA 05-2016-135 AND EA 05-2016-135. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106118Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN BS 333 - 349. REPAIRED THE STRINGER IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32429 REV C. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106117Frame · corrodedFRAME AT BS 319 CORRODED BETWEEN STRINGERS 24 AND 25R. REPAIRED THE FRAME IAW SRM 53-00-06-201-001-A03 AND DWG SH670-31355. AIRRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA201611061160Doubler · corrodedTCAS ANTENNA DOUBLER CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 AND DWG SH670-32364. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106115Floorbeam · corrodedFLOORBEAM AT FS 1031 RBL 9 IS CORRODED. COMPLIED WITH EC/TC REO 690-53-61-631 REV A. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106114Structure · corrodedPACKER CORRODED AT BS 333 RBL 9. REMOVED CORRODED PACKER AND INSTALLED NEW PACKER IAW SRM 51-42-06-001-001-A01. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106113Angle · corrodedPAX DOOR KICKPLATE ANGLE CORRODED. REMOVED AND REPLACED ANGLE AND FABRICATED AND INSTALLED NEW KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG SH670-31810. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106112Stringer · corrodedSTRINGER 25R IS CORRODED FROM BS 280 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG SH670-31212. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106111Bracket · damagedBRACKET AT STRINGER 7L BETWEEN BS 1144-1162 ARE DAMAGED. COMPLIED WITH EC/TC REO 670-53-61-292 AND REO 670-53-61-292 REV D. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20161106110Sleeve · corrodedALL FOUR INBD MLG PISTON AXLES ARE CORROCED. REMOVED AND REPLACED THE SLEEVE IAW SB 49200-32-85 SECTION 11 STEPS 3(A-C). AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20160914126Crossbeam · corrodedDURING C CHECK FOUND CROSSBEAM CORRODED AT FS 333 RBL9. MTC C/W EC/TC EA 32-2016-189 & EA 32-2016-189.SDR ASOA20160914125Angle · corrodedDURING C CHECK FOUND PAX DOOR UPPER FLOOR SILL CORRODED. MTC R & R FLOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-012-001-001-A01, & DRAWING SH670-31810. ALL DEFECTS CORRECTED.SDR ASOA20160914123Door Sill · corrodedDURING C CHECK FOUND RT FLOOR SILL CORRODED AT FS 349.00+8. MTC C/W EC/TC EA 05-2016-135 & EA 05-2016-135.SDR ASOA20160914120Doubler · corrodedDURING C CHECK FOUND TCAS ANTENNA DOUBLER CORRODED. MTC R & R DOUBLER, REMOVED STR 27 FROM FS280-295 FOR ACCESS AND REINSTALLED. WORK IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, & DWG SH670-32364.SDR ASOA20160914076AAngle · corrodedPAX DOOR SILL CORRODED. REMOVED AND REPLACED UPPER DOOR SILL CAP ANGLE IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01 AND DRAWING SH670-31810.SDR ASOA20160913124Door Sill · corrodedDURING C CHECK RT FLOOR SILL CORRODED AT FS280-319. MTC R & R RT FLOOR SILL IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-41-13-001-001-A01, & DRAWING SH690-32170.SDR ASOA20160910118Angle · corrodedDURING C CHECK FOUND PAX DOOR KICK PLATE ANGLE CORRODED. MTC REMOVED, FABRICATED, & INSTALLED KICK PLATE ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & DWG SH670-31810.SDR ASOA20170910117Structure · corrodedDURING C CHECK FOUND PACKER CORRODED AT FS 333 RBL 9. MTC R & R PACKER IAW SRM 51-42-06-001-001-A01.
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