N303PQ
Service difficulty reports · 80
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 = 'N303PQ' 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 = 'N303PQ' 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 REXA2026060400901Light · inoperativeFO SIDE MAP LIGHT SPARKED AND EMITTED SMOKE WHEN MOVED. REMOVED AND REPLACED FO SIDE MAP READING LIGHT IAW AMM 33-13-03. OPS CHECKS GOOD. NO SMOKE ODOR NOTED.SDR REXA2026041300284Overheat Sensor · inoperativeAT FL250 MLG BAY OVHT WARN RAN QRH WARN MSG DID NOT EXTINGUISH BTMS ALL 0000 LANDED W/O ISSUE WARN MSG PERSISTS AT GATE. R/R FIRE DETECTION CONTROL IAW AMM 26-14-01. MESSAGE DID NOT CLEAR. R/R L & R MLG BAY TEMPATURE SENSING ELEMENT IAW AMM 26-14-04. OPS TESDR REXA2025010300004Lamp · inoperativeRH REAR EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EXTERIOR EMEREGENCY LIGHT AT THE RIGHT AFT OVER WING SECTION OF THE FUSELAGE IAW AMM 33-51-15 OPS CHECK GOOD P/N ON/OFF:8GH002473-08SDR REXA2024092400722Battery Pack · inoperativeDURING INSP. FOUND ALL FOUR OVERWING EMER EXITS/ FORWARD FLOOR EMER EXITS AND MID CABIN FORWARD EMERGENCY LIGHTS INOP. TROUBLESHOT AND FOUND EMERGENCY BATTERY PS37 INCORRECTLY INSTALLED. R/R PS37 BATTERY AND WAS ABLE TO GET ONE O/W EXIT LIGHT WORKING AND BOSDR REXA2024040100319Door Frame · crackedLEFT FORWARD OVER-WING EMERGENCY EXIT 833 APPEARS TO BE CRACKED AT THE BASE OF THE AFT UPPER LUG. REQUIRES EVALUATION. REPAIRED AFT LH EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA NO: CRJ952-15922 REV IR DATED 3/6/2024SDR REXA2024032000289Door Frame · crackedAFT LH EMERGENCY EXIT DOOR POSSIBLE CRACK NEAR BASE OF UPPER LUG. REPAIRED AFT LH EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA NO: CRJ952-16063 REV IR DATED 3/4/2024SDR REXA2024103001120Panel · corrodedPAX DOOR FWD STAIR SIDE PANEL CORRODED AT APPROX DD7 AROUND HAND RAIL UPPER FWD POST ASSY. REPAIRED SIDE PANEL, FORWARD, PASSENGER DOOR STAIRS, P/N 601R317071-12 IAW ENDEAVOR AIR EA. CRJ952-16088 REV -- DATED 2-19-2024.SDR REXA2024102901121Floorbeam · crackedSTIFFENING ANGLE AT FS 280 RBL26 PN:CC670-34117-6 IS CRACKED AND REQUIRES REPLACEMENT. REMOVED STIFFENING ANGLE AT FS 280 RBL 26 PN: CC670-34117-6 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED NEW STIFFENING ANGLE PN CC670-31147-6 IAW CRJ900 SRM 51-42-06-001SDR REXA2024102901116Web · cracked"L/H FWD EQUIPMENT BAY FLOOR WEB APPEARS TO BE CRACKED AT F.S.193. REMOVED DAMAGED AREA IN BAY FLOOR WEB LH SIDE AT FS193 IAW CRJ900 SRM 53-11-43-201-001-A01. FABRICATED, LOCATED DRILLED, DEBURRED AND INSTALLED REPAIR PARTS, DOUBLER AND SHIM 2024T3 0.040"" PSDR REXA2024102901115Electrical Box · crackedEXTERNAL A/C POWER RECEPTICAL MOUNTING CHANNEL IS CRACKED. DISCONNECTED THE MAIN BATTERY IAW CRJ900 AMM 24-32-00-040-801-A01, CONNECTED MAIN BATTERY IAW CRJ 900 AMM 24-32-00-440-801-A01. REMOVED AND REINSTALLED EXTERNAL AC POWER RECEPTACLE USING PN NAS1149DDSDR REXA2024102901114Access Panel · chafedRH FLAP L/E ACCESS PANEL 684GB IS CHAFED. FOUND DAMAGE ON PANEL BEYOND REPAIR. LOCATED AND DRILLED NEW SERVICABLE PANEL 684GB IAW CRJ-900 SRM 51-40-11-001-001-A01.SDR REXA2024022600217Floorbeam · crackedRH COCKPIT FLOOR BEAM (RBL12) IS CRACKED ON O/B AFT RADIUS. COMPLIED WITH MHIRJ REO# 690-53-11-1689 REV. -- DATED 2024-02-22 FOR RBL12 COCKPIT FLOOR BEAM.SDR REXA2024022600216Floorbeam · crackedLH COCKPIT FLOORBEAM IS CRACKED ON O/B AFT RADIUS. COMPLIED WITH MHIRJ REO# 690-53-11-1689 REV. -- DATED 2024-02-22 FOR RBL12 COCKPIT FLOOR BEAM.SDR REXA2024102901113Floor Support · corrodedRH FLOOR SILL BETWEEN FS 280 TO 319 IS CORRODED ON UPPER AND LOWER SURFACE. REMOVED AND REPLACED RH FLOOR SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01SDR REXA2024102901112Attach Angle · crackedRBL 9 FWD OB ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE RBL 9 FWD OB ATTACH ANGLE P/N CC670-34269-8 INSTALLED SERVICEABLE RBL 9 FWD OB ATTACH ANGLE P/N CC670-34269-8 IAW CRJ 900 SRM 51-42-21-001-001-A01.SDR REXA2024102901111Attach Angle · crackedRBL 12 FWD ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE RBL 12 FWD ATTACH ANGLE P/N CC670-34099-2.INSTALLED SERVICEABLE RBL 12 FWD ATTACH ANGLE P/N CC670-34099-2 IAW CRJ 900 SRM 51-42-21-001-001-A01.SDR REXA2024102901110Attach Angle · crackedLBL 12 FWD ATTACH ANGLE FOUND TO BE CRACKED. LOCATED AND DRILLED SERVICEABLE LBL 12 FWD ATTACH ANGLE P/N CC670-34099-1SB. INSTALLED SERVICEABLE LBL 12 FWD ATTACH ANGLE P/N CC670-34099-1SB IAW CRJ 900 SRM 51-42-21-001-001-A01.SDR REXA2024102901109Floorbeam · corroded"FS 280 ""J"" ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9 REMOVED FS 280 ""J"" ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW ""J"" ANGLE PN: CC670-34095-1 IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW FS 280 ""SDR REXA2024102901108Bulkhead Web · corrodedLH FS 280 BULKHEAD LOWER WEB IS CORRODED. REPAIRED LH FS 280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.SDR REXA2024102901107Bulkhead Web · corrodedRH FS 280 BULKHEAD LOWER WEB IS CORRODED. REPAIRED RH FS 280 BULKHEAD LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.SDR REXA2024102901106Floorbeam · corrodedRH FS 280 CROSSBEAM IS CORRODED REPLACED CROSS BEAM IAW SRM 51-40 AND 51-42SDR REXA2024040200327Floorbeam · crackedLH FS 280 CROSSBEAM IS CORRODED REMOVED AND REPLACED LH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-21-11-001-001-A01.SDR REXA2024030500234Post · corrodedFS 280 DOOR CORNER POST IS CORRODED AT LBL9 FLOOR LEVEL REPAIRED FS 280 DOOR CORNER POST AT LBL9 FLOOR LEVEL IAW CRJ 900 SRM 53-11-10-201-006-A01. REMOVED AND REINSTALLED INSTALLED SAME SERVICEABLE GUSSET AND INSTALLED NEW SERVICEABLE ATTACH ANGLE AT LH FS SDR REXA2022110402413Control Panel · inoperativeAT 29000 FT WE RECIEVED A CABIN ALT CAUTION THAT ESCALATED TO A CABIN ALT WARNING. THE CABIN ALT INCREASED TO 12,300 FT. WE RAN THE EMERGENCY CHECKLIST CARD WHICH DIRECTED US TO QRH 7-7. WE PREFORMED THE QRH PROCEDURE AS UNPRESSURIZED AND CONTINUED THE FLIGHT SDR REXA2020070600576Battery Pack · dischargedFA REPORTS FLOOR LEVEL EMRGENCY LIGHTED EXIT SIGNS ON BOTH SIDES IN ROW 13 ARE INOP. REMOVED AND REPLACED PS38 EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECK OK.SDR REXA2020040900438Piston · wornINITIAL INSPECTION: WEAR ON SETTLEMENT AREA OF THE WHEEL AT NLG PISTON/AXLE ASSEMBLY. (SM).IN REFERENCE NRC SN 461.
SETTLEMENT AREA OF THE WHEEL AT NLG PISTON/AXSDR REXA2020042300542Seal · tornEDV AIR: LH ENGINE TR COWL LOWER SEAL TORN.(MOT1)(AYP)
SUMMARY: SEAL (P/N: G50483) LOWER TR COWL LH ENGINE WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01.SDR REXA2020042300541Hinge Fitting · corrodedAWR IN REF NRC S/N 00523, AFTER BUSHING REMOVAL CORROSION WAS FOUND ON PCU HINGES FITTING LUGS (4EAS) OF LH AILERON .
HINGES FITTING LUGS (4EAS) OF LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV.--SDR REXA2020042300540Hinge Fitting · corrodedAWR IN REF NRC S/N 00524, AFTER BUSHING REMOVAL CORROSION WAS FOUND ON PCU HINGES FITTING LUGS (4EAS) OF RH AILERON .
HINGES FITTING LUGS (4EAS) OF RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV. --SDR REXA2020042300539Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL 15RH BETWEEN FS847+16 TO FS897.70, FS897.70 TO FS913, FS913 TO FS969 AT PASSENGER CABIN.(SM)(CPAX)(TCI 53-20-301)
SUMMARY. SIDE SEAT RAILS 15RH BETWEEN FS847+16SDR REXA2020040900437Canister · crackedINITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. (AI)
CANISTER, WELDED NO. 3 IN WS148 AT LH MAIN FUESDR REXA2020040900436Seal Depressor · wornINITIAL INSPECTION. WEAR ON SEAL DEPRESSURE FS 517 AND 565, BTW STRG 23L-24L AT FWD CARGO BAY SURROUND.
SEAL DEPRESSURE FS 517 BTW STRG 23L-24L AT FWDSDR REXA2020042300538Stringer · corrodedINTIAL INSPECTION: CORROSION ON STRINGER 26RH BETWEEN FS 349 AND FS364 AT MAIN AVIONICS COMPARTMENT. (SM)(E/E)(CI 100-09E5)
SUMMARY: STRINGER 26RH BTW FS=333 TO FS=364 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.SDR REXA2020042300537Retainer · wornINITIAL INSPECTION : WEAR ON RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL (MOT 2)
SUMMARY: RETAINER 8E/A OF LOWER AND UPPER RH ENGINE TRASCOWL WERE REPLACED PER CRJ900 SRM 51-42-20-001-001-A01.SDR REXA2020042300536Baffle · crackedINITIAL INSPECTION: CRACK ON BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS.(MOT2)
BAFFLES 2E/A ON RH ENGINE LOWER THRUST REVERSER CASCADE FITTINGS WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
ADDSDR REXA2020042300534Support Angle · corrodedAWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICEDOOR LOWER SILL,FWD WET AREA. (W1) (CPAX)
SUMMARY: CORROSION ON ANGLE, LOWER SILL REMOVED PER CRJ900 SRM 51-21-0
6-001-00SDR REXA2020042300533Support Angle · corrodedAWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)
PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-42-21-001-SDR REXA2020042300532Support Angle · corrodedAWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)
SUMMARY: PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ900 SRM 51-4SDR REXA2020042300531Support Angle · corrodedAWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)
SUMMARY:CORROSION ON ANGLE, LOWER SILL WAS REMOVED PER CRJ900 SRM SDR REXA2020042300529Support Angle · corrodedAWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)
SUMMARY:PROTECTION PLATE SUPPORTS ANGLE WAS REPLACESDR REXA2020042300528Support Angle · corroded"AWR; [TASK R53520 STEP 7]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "
"SUMMARY: PROTECTION PLATE SUPPORTS ANGLE WAS REPLACED PER CRJ90SDR REXA2020042300527Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTION FS847+16 TO FS913, FS913 TO FS969 LH SIDE RAIL AT PASSENGER CABIN. (SM) (CPAX) (TCI 53-20-301)
SEAT SIDE RAIL SECTION FS847+16 TO FS913, FS913 TO FS969 LH SIDE RAIL AT PASSENGER CABIN WERE REPLACED PER CSDR REXA2020042300526Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTIONS FS677 TO FS720.85, FS744.15 TO FS761.85, FS785.15 TO FS847+FS8.40, FS847+8.40 TO FS847+16 SIDE RAIL LH/RH SECTIONS AT PASSENGER CABIN.(SM)(CPAX)(TCI 53-20-301) SDR REXA2020042300525Seat Track · corrodedINITIAL INSPECTION: CORROSION ON SEAT SIDE RAIL SECTIONS FS485 TO FS565, FS565 TO 661+16, FS 661+16 TO FS661+90 LH SIDE ALSO FS661 TO FS661+16,FS661+16 TO FS661+90 SECTION RH SIDE AT PASSENGER CABIN. (SM) (CPAX) (TCI 53-20-301)
SEAT SIDE RAIL SECTIONS FS485 TSDR REXA2020042300523Seat Track · corrodedINITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 349 TO FS= 485, 9RBL/LBL ] [FS485 TO FS581 9RBL][ FS= 661+32 TO FS= 847+8.40, 9LBL/9RBL ] ALSO [27LBL FS954 TO FS 985 AND 9LBL FS977 TO FS 985] AT PAX CABIN. (CPAX) (TCI: 53-20-243) SDR REXA2020042300522Hinge · corroded"PARTS RACK: CORROSION ON HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY
DOOR CUTOUT. (CCT). "
"HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPLACED
FOR NEW ONES PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6A."SDR REXA2020040900435Frame · corrodedINITIAL INSPECTION. CORROSION ON FRAME FS 549, STRG 18 AT FWD CARGO BAY. (TCI 53-20-333).
FRAME FS 549, STRG 18 AT FWD CARGO BAY WAS REPSDR REXA2020040900430Retainer · wornINITIAL INSPECTION : BENT SEAL RETAINER LOWER EDGE OF AFT CARGO COMPARTMENT DOOOR (PTAS)
SEAL RETAINER LOWER EDGE OF AFT CARGO COMPARTMENT DOOOR WAS REPAIRED PER EA NO: CRJ952-10646 REV. IRSDR REXA2020042300521Channel · crackedINITIAL INSPECTION: CRACK ON CHANNEL OF AFT CARGO DOOR SURROUND STRUCTURE. (CCT)
"CHANNEL OF AFT CARGO DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ-900
SRM 51-41-02-001-001-A01."SDR REXA2020042300519Channel · crackedPARTS RACK: . CRACK ON CHANNEL 1E/A OF WING TO FUSELAGE FAIRING 196DR. (FUS)
DAMAGED CHANNEL WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01
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