N272PQ
Service difficulty reports · 81
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 = 'N272PQ' 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 = 'N272PQ' 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 REXA2026030900222Door Sill · corrodedCORROSION ON LOWER SILL ALSO ON SETTLEMENT AREA OF CARGO FLOOR 281JLF AT AFT BAGGAGE BAY DOOR CUT-OUT SURROUND STRUCTURE. DUE TO EXCESSIVE DAMAGE LOWER SILL OF AFT CARGO MUST BE REPLACE PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-1SDR REXA2026030900221Stringer · corrodedCORROSION ON STRINGER 25RH IN STA. FS=295.00 TO FS= 310.00 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 25RH IN STA. FS=295.00 TO FS= 310.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-SDR REXA2026030900216Hinge · excess playFREE PLAY ON HINGE & WEAR ON AFT FACE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT HINGE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT WAS REPLACED AND WEAR ON AFT FACE OF FLOATATION VALVE ON AFT ACCESSORIES COMPARTMENT WAS BLENDED OUT AND EVALUATESDR REXA2026030900214Attach Angle · crackedCRACK ON ATTACHMENT ANGLE INNER SKIN TO AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE (NEX TO MOTOR ASSIST PULLEY BRACKET) ANGLE INNER SKIN TO AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE (NEX TO MOTOR ASSIST PULLEY BRACKET) WAS REPLACED PER CRJ 9SDR REXA2026030900206Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LEFT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR REXA2026030900230Support · crackedCRACK ON BRACKET SUPPORT OF JB6 AT FORWARD EQUIPMENT COMPARTMENT. BRACKET SUPPORT OF JB6 AT FORWARD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2026030900158Skin · corrodedCORROSION ON INTERNAL SKIN BTW FS 677.00 AND FS693.00 STGR 26L TO 26R BELOW FLOOR. CORROSION ON INTERNAL SKIN BTW FS 677.00 AND FS693.00 STGR 26L TO 26R BELOW FLOOR WAS REPAIRED PER REO 690-53-31-1118 REV - -SDR REXA2026030900229Retainer · corrodedCORROSION ON INNER FACE SEAL RETAINER, AFTER REMOVAL AT FWR BAGGAGE DOOR DUE TO EXCESSIVE DAMAGE INNER FACE SEAL RETAINER WAS REPLACED PER SRM CRJ-900 SRM 51-10-06-001-001-A01 AND WILL BE INSTALLED UNDER NRC: 00101SDR REXA2026030900228Retainer · damagedREMOVE SEAL RETAINER AFT P/N: CC670-38662-5 OF MAIN AVIONICS COMPARTMENT DOOR TO BE INSTALLED ON A/C 921 THEN INSTALL SERVICEABLE PART. NEW SEAL RETAINER AFT P/N: CC670-38662-5S OF MAIN AVIONICS WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2026030900227Floorbeam · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50 CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STSDR REXA2026030900226Pressure Blkhd · corrodedCORROSION ON FWD CENTER PRESSURE BULKHEAD FS693.00 BTW STGR 26L AND STGR 26R. DUE EXCESSIVE DAMAGE ON FRAME FWD CENTER PRESSURE BULKHEAD WAS REPLACED PER CRJ900 SRM 53-41-10-101-001-A02, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01SDR REXA2026030900225Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RIGHT WING. MACHINED RIB OF LEADING EDGE SS57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV --SDR REXA2026030900224Support Angle · crackedCRACK LOWER FWD SUPPORT ANGLE OF EXTERNAL POWER SERVICE PANEL SUPPORT STRUCTURE LOWER FWD SUPPORT ANGLE OF EXTERNAL POWER SERVICE PANEL SUPPORT STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR REXA2026030900223Canister · crackedCRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 CRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV --SDR REXA2026030900220Support Angle · crackedCRACK ON FWD SUPPORT ANGLES (2EAS) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARMENT INTERNAL STRUCTURE FWD SUPPORT ANGLES (2EAS) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARMENT INTERNAL STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR REXA2026030900219Support Plate · corrodedCORROSION ON RH WHEEL WELL HYD. LINES SUPPORT PLATE (IB BK, LG EX, OB BK, LG DN AST AND LG RET) DUE TO EXCESIVE DAMAGE ON RH WHEEL WELL HYD. LINES SUPPORT PLATE IB BK, LG EX, OB BK, LG DN AST AND LG RET) WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, SRM 5SDR REXA2026030900218Bracket · damagedELONGATED BRACKET MOUNTING PULLEY OF PASSENGER DOOR BRACKET MOUNTING PULLEY OF PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-22-001-001-A01SDR REXA2026030900215Support · corrodedCORROSION ON LBL27.00 BTW FS977.00 / FS1051.00 AT AFT CARGO COMPARTMENT DUE TO EXCESSIVE DAMAGE ( CORROSION ) NO DAMAGE IS ALLOWED ON LONGITUDINAL BEAM UPPER FACE AT LBL27.00 BTW FS977.00 / FS1051.00 AFT BAGGAGE COMPARTMENT STRUCTURE WAS REPLACED PER CRJ900 SRSDR REXA2026030900213Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2136 RSDR REXA2026030900210Seat Track · corrodedCORROSION ON SEAT RAILS 4EA BTW FS 349.00 TO FS 677.00 RBL 9 AT FLOOR PASSENGER CABIN SEAT RAILS 4EA BTW FS 349.00 TO FS 677.00 RBL 9 AT FLOOR PASSENGER CABIN WERE EVALUATED OUT LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND AMM 53-00-SDR REXA2026030900209Angle · corrodedCORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX CORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE ANGLE AFT CAP AND ANGLE MID CAP WERE REPLACED AND CORROSION ON ANGLE FWD CAP WAS REMSDR REXA2026030900208Floor Support · corrodedCORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX CORROSION ON ANGLE FLOOR SUPPORT FS310 TO FS349 LBL=43 AT CPAX WAS REMOVED AND EVALUATED OUT OF LIMITS THEREFORE ANGLE AFT CAP AND ANGLE MID CAP WERE REPLACED AND CORROSION ON ANGLE FWD CAP WAS REMSDR REXA2026030900207Panel · crackedCRACK ON TOP PANEL EDGE MEMBER OF PASSENGER DOOR STAIR STEPS INTERNAL STRUCTURE, FWD & AFT EDGE SECTION. TOP PANEL EDGE MEMBER OF PASSENGER DOOR STAIR STEP WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01SDR REXA2026030900200Seat Track · corrodedCORROSION ON LH SIDE RAIL SEAT TRACK BTW FS437 TO FS445, FS501 TO FS517, FS597 TO FS613, FS629 TO FS645, FS661 TO FS661+16, FS661+46 TO FS661+50, FS669 TO FS677 AT CPAX CORROSION ON LH SIDE RAIL SEAT TRACK BTW FS437 TO FS445, FS501 TO FS517, FS597 TO FS613, FSSDR REXA2026030900157Seat Track · corroded" CORROSION ON SEAT RAILS 4EA BTW FS 374 TO FS 677 LBL 9 AT FLOOR PASSENGER CABIN. CORROSION ON SEAT RAILS (3EAS) BTW FS 374 TO FS 485 AND FS 581 TO 677 LBL 9 AT FLOOR PASSENGER CABIN WAS EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-SDR REXA2026030900205Seal · crackedBROKEN SEAL NEXT TO ACCESS PANEL 591JB UPPER, LH WING BROKEN SEAL NEXT TO ACCESS PANEL 591JB UPPER, LH WING WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A07SDR REXA2026030900217Attach Angle · crackedCRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ ON MLG SHOCK STRUT BAY DUE TO EXCESSIVE DAMAGE ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2026030900204Web · crackedCRACK ON LH ELECTRICAL BAY WEB FLOOR FS 193.00 AT FWD EQUIPMENT COMPARTMENT LH ELECTRICAL BAY WEB FLOOR FS 193.00 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A01 CHARGE VALVE AND GAUGE WERE REMOVED/INSTALLED, SERVICING OF HYDRAULSDR REXA2026030900212Fitting · wornWEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING (2EAS) OF FLAP STUB FAIRING 171DL AND 172DR AT RT & LT WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01, CRJ900 SRM 51-42-SDR REXA2026030900203Retainer · crackedCRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34) BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND RBL 34) WAS REPLACED PER CRJ 900 SRM 51-41-02-001-001-A01SDR REXA2026030900202Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRSDR REXA2025111000983Stringer · chafedCHAFE DAMAGE TO STGR 6L AND 7L AT FS 1144 TO 1162 PERFORMED PERMANENT REPAIR TO STGRS 6L AND 7L PER REO 690-53-61-1698 REF EA CRJ953-20703 AND CRJ953-20704SDR REXA2025111000982Frame · chafedCHAFE DAMAGE TO FRAME SECTOR AT FS 1162 PERFORMED TEMPORARY REPAIR TO FRAME SECTOR AT FS 1162 PER REO 690-53-71-098SDR REXA2025102900968Engine · contaminatedAFTER ROTATION CA AND FO STARTED TO SMELL SMOKE . VERY FAINT WHITE SMOKE SEEN BY PILOTS AND FAS WITH CHEMICAL ODOR. RAN CHECKING CARD AND QRH SMOKE AND FUMES REMOVAL PROCEDURE. TURNING PACKS AND RECIRC FAN OFF REDUCED ODOR SIGNIFICANTLY. FIRE RESCUE DID NOT NSDR REXA2022101702278None · corrodedRH SIDE FLOOR SILL AT F.S. 310.00 CORRODED COMPLIED WITH REO 690-53-21-1549 REV -- DATED 2022-10-03SDR REXA2020082000626Charger · not groundedDURING MX NOTED EMER. LIGHT JUST AFT OF THE SERVICE DOOR (EXTERIOR FUSELAGE) DOES NOT ILLUMINATE. FOUND EPSU BATTERY CHARGER NOT GROUNDING CORRECTLY AT PS36 REMOVED & REPLACED EPSU BATTERY CHARGER & BATTERY AT PS36 IAW CRJ 900 AMM 33-51-17 OPS CHECK GOOD ALL ESDR REXA2020082000625Battery Pack · failedCREW REPORTED FWD(4) OVERHEAD CENTER LIGHTS CAME ON IN FLIGHT, WILL NOT EXTINGUISH. ALL OTHER EMERGENCY LIGHTS OPERATE AS PRESCRIBED. REMOVED & REPLACED EPSU BATTERY PACK AT PS36&EPSU BATTERY CHARGER IAW CRJ900 AMM 33-51-17. OPS CHECK GOOD ALL LIGHTS ILLUMISDR REXA2019052800741Floorbeam · corrodedINITIAL INSPECTION: CORROSION ON FLOORBEAM LBL9.00 BTW FS1015.00 - FS1051.30 AFTER BAGGAGE BAY (C3)[SM]. SUMMARY: CORROSION LEVEL 2. FLOORBEAM LBL9.00 BTW FS1015.00 - FS1051.30 AFTER BAGGAGE BAY, WAS REPAIRED PER SRM 53-00-41-201-001-A03. NEW BEAM WAS DRILLED SDR REXA2019052700744Support · corrodedINITIAL INSPECTION: CORROSION ON FLOOR FITTING SUPPORT BTW FS=565 / FS=629 AND STGR 22L / 27L (4 EAS) AT INTERNAL STRUCTURE OF FWD CARGO COMPARTMENT (C1) (SM) (TCI 53-20-306). SUMMARY:CORROSION LEVEL 2, FLOOR FITTING SUPPORTS BTW FS=565 / FS=629 AND STR 22L / SDR REXA2019052700743Angle · corroded"AWR INITIAL INSPECTION: CORROSION ON ANGLE MID CAP, BTW FS=310 / 349 AND LBL 40 AT INTERNAL STRUCTURE OF FWD WET AREA (W1) (SM) IN REFERENCE EO NBR R53520 STEP 7. SUMMARY OF NRC: 00231 CORROSION LEVEL: 2 DUE TO EXCESSIVE CORROSION ON ANGLE MID CAP BTW FS=310 SDR REXA2019052700740Floorbeam · corrodedINITIAL INSPECTION: CORROSION ON FLOORBEAM LBL27.00 BTW FS1000.00 - FS1051.30 AFTER BAGGAGE BAY (C3)[SM]. SUMMARY OF NRC 306: LEVEL CORROSION 2. FLOORBEAM LBL27.00 BTW FS1000.00 - FS1051.30 AFTER BAGGAGE BAY, WAS REPAIRED PER SRM 53-00-41-201-001-A03.SDR REXA2019052400733Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 669 TO FS= 720, STGR 15L/R ] [ FS= 744 TO FS= 761, STR 15L/R ] [ FS=785 TO FS= 847+8, STR 15L/R], [ FS= 847+8 TO FS= 847+16, STR 15L/R], [ FS= 847+16 TO FS= 913, STR 15L/R] AND [ FS= 913 TO FS=SDR REXA2019052100742Angle · corrodedINITIAL INSPECTION: CORROSION ON ANGLE, BTW FS=310 / 349 AND LBL 40 AT INTERNAL SURROUND STRUCTURE OF PASSENGER DOOR (CPAX) (SM) (TCI 53-20-216). SUMMARY: ON NRC. 00234 CORROSION LEVEL 2. ON ANGLE, BTW FS=310 / 349 AND LBL 40 AT INTERNAL SURROUND STRUCTURE OF SDR REXA201905190739Angle · corrodedINITIAL INSPECTION: CORROSION ON ANGLE, BTW FS=319 / 349 AND RBL 40 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR (CPAX) (SM) (TCI 53-20-215). SUMMARY: SUMMARY OF NRC: 00235 CORROSION LEVEL: 2. CORROSION ON ANGLE BTW FS= 319/ FS= 349 AND RBL 40 AT INTSDR REXA2019051900738Canister · crackedINITIAL INSPECTION : CRACK IN CANISTER, WELDED NR 3 IN STA. WS=148 AT LT MAIN FUEL TANK. (AI) SUMMARY OF NRC 00188: CANISTER WELDED NR 3 IN STA. WS=148 AT LT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV. --.SDR REXA2019051900736Intercostal · corrodedAWR HIDDEN DAMAGE: CORROSION ON INTERCOSTALS BTW FS=310.00 / FS=333.00 AND STR 20R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE JOBCARD NRB R25120. "SUMMARY OF NRC 00213 CORROSION LEVEL 2 ON INTERCOSTALS BTW FS=310.00 / FS=333.00SDR REXA2019051900734Seat Track · corroded"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTION [ FS= 661+16 TO FS= 669, STR 15L ] AND [ FS= 661+16 TO 661+90, STR 15R ] AT PAX CABIN. (CPAX) (TCI: 53-20-217) "SUMMARY: OF NRC 00139, CORROSION LEVEL 2. SECTION SEAT RAILS IN SECTION [ FS= 661+16 TOSDR REXA2019051900728Seat Track · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 847+16, 9LBL/RBL ] AND [FS= 846+16 TO FS= 977, 9LBL/9RBL ] AT PAX CABIN. (CPAX) (TCI: 53-20-233) SUMMARY OF NRC 00136, CORROSION LEVEL-2: SECTION IN SEAT RAIL SECTIONS [ FS= 677 TSDR REXA2019051700737Panel · crackedINITIAL INSPECTION: CRACKS ON AFT SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). SUMMARY OF NRC 00166: CRACK ON AFT SIDE PANEL OF STEPS AT PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-004-A01, ZONE 5 DETAIL X AND Y; FIGURE 52-11-04-995-802.SDR REXA2019051700735Panel · cracked"INITIAL INSPECTION: CRACKS ON FWD SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). "SUMMARY OF NRC. 00165: CRACKS ON FWD SIDE PANEL OF STEPS AT PASSENGER DOOR (PTAS) (SM). WERE REPAIRED PER SRM 52-11-04-201-004-A01 PAR. 5.B.(1) ZONE 4 DETAIL V AND W FIGURE
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