N2824W
Service difficulty reports not matched to an aircraft · 34
They name N2824W, 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 = 'N2824W' 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.
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 = 'N2824W' AND registry_match IS NULL 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 DL72E954603Battery Pack · dischargedON LAYOVER, FOUND EMERGENCY LIGHTS INOP ABOVE FWD AND AFT OVERWING EMERGENCY EXITS LT SIDE. REPLACED M1090 BATTERY PACK, EMERGENCY LIGHTS OPS NORMAL.SDR DL72E954266Doubler · crackedTHE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK WAS FOUND WITH A PREVIOUS MODIFICATION DOUBLER INSTALLED FOR A CRACK AT LBL 55 AND STA 938. THE PREVIOUS DOUBLER WILL BE REMOVED AND A NEW DOUBLER INSTALLED PER REVISION 4 OF THE SERVICE BULLETIN E0 4.61537-3ASDR DL72E954027Bushing · looseAT HMV, FOUND BUSHING LOOSE IN LT MLG PORK CHOP FTG IN AFT HOLE FOR NR 4 FLAP TRACK. REPAIRED AND INSTALLED NEW BUSHING PER MM 57-42-0.SDR DL72E953991Fitting · corrodedFOUND AT HMV, FRETTING CORROSION ON I/B FACE OF LT MLG PORK CHOP FITTING AT FLAP TRACK ATTACH HOLE. REPAIRED PER MM 57-42-0 PG 814.SDR DL72E953977Rib · crackedAT HMV, NR 4 SLAT RIB NR 18 CRACKED. REPAIRED PER MM 57-54-00.SDR DL72E953945Stringer · crackedDURING A HANGAR INSPECTION, A CRACK WAS DISCOVERED IN THE FWD STRINGER OF THE NR 1 ENGINE LWR COWL. A REPAIR WAS INSTALLED PER THE S.R.M. 51-40-3.SDR DL72E954116Skin · corrosionAT HMV IN ATLANTA, MTC FOUND CORROSION IN FUSELAGE SKIN AT STA 950 PLUS 10 INCHES JUST OUTBOARD OF STR 30. FINAL CUT-OUT DIMENSIONS ARE 2.75 INCHES BY 3.75 INCHES. THE SKIN IS FABRICATED FROM 2024-T3 CLAD AND HAS A NOMINAL THICKNESS OF 0.183 INCH AT THE FWD SDR DL72E954117Vent Access Hole · mislocatedDURING ACCOMPLISHMENT OF THE LT WING UPPER STRINGER 13/14 TAB ONLY REPAIR AT WS 656.5 RIB, THE VENTB OX ACCESS HOLE WAS INADVERTENTLY CUT INBD OF THE RIB INSTEAD OF OTBD. THIS REPAIR WAS BEING ACCOMPLISHED PER B727 M/M 57-13-0 FIG. 804, REPAIR FOR TAB CRACKS SDR DL72E954025Skin · crackedAT HMV, FOUND VERT STABILIZER SKIN STOPPED DRILLED 3 TIMES AT RT FS 1333 AT BOTTOM OF VERT FIN. REPAIRED PER MM 55-30-0 PG 801.SDR DL72E953976Angle · crackedNR 1 L/E FLAP ACTUATOR ATTACH ANGLE CRACKED I/B SIDE. WORKED AT HMV, REPAIRED ANGLE PER M/M 57-20-21.SDR DL72E954069Frame · crackedAT HMV, FOUND FUSELAGE FRAME CRACKED AT REPAIR DOUBLER, UPPER FASTENER HOLE FS 930 RT SIDE. REPAIRED PER SRM 53-10-04 FIG 25 TYP B.SDR DL72E954023Web · crackedAT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E954022Web · crackedAT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E953974Vent Box Tab · crackedREF OPN 8602 AD HFEC INSP OF RT OUTER WING UPPER STRINGER-TO-RIB CRACK INDICATED FWD VENT BOX AFT TAB W.S. 686.5, MARKED NR 2.SDR DL72E953973Rib · crackedNR 5 SLAT-RIB NR 20 CRACKED UNDER LEADING EDGE AT NUTPLATE. WORKED AT HMV. REPAIRED PER M/M 57-54-00.SDR DL72E953972Heat Shield · crackedNR 6 SLAT-INTERIOR HEAT SHIELD CRACKED BETWEEN RIBS 11 AND 12. WORKED AT HMV. REPAIRED PER M/M 57-54-00, PG 804A.SDR DL72E953971Stringer · crackedHFEC CHECKED ON STR-TO-RIB HOLES SHOWS CRACK INDICATION ON STRINGER NR 10 AND NR 14 AT W.S. 656.5. WORKED AT HMV. INSTALLED REPAIR DOUBLER PER M/M 57-13-00.SDR DL72E953970Support · crackedRT ELEVATOR-HINGE SUPPORT FRAME CRACKED AT BOLT, INSIDE 3RD BALANCE BAY FROM O/B END, WORKED AT HMV. REPAIRED PER SRM 55-10-04, FIG 6.SDR DL72E953969Rib · crackedNR 4 SLAT-RIB NR 2 CRACKED. WORKED AT HMV. REPAIRED PER M/M 57-40-00, FIG 805.SDR DL72E953968Vent Box Tab · crackedTAB CRACKED. VENT BOX TAB CRACKED STA. 686.5 AT HOLE MARKED NR 4. WORKED AT HMV. REPAIRED TAB PER M/M 57-13-00.SDR DL72E954067Stringer · crackedAT HMV, FOUND STRINGER CRACKED VERTICAL STAB INTERIOR STR 8R LOC IN 5TH BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-00 FIG 803.SDR DL72E954024Skin · crackedAT HMV, FOUND SKIN CRACKED NR 2 ENG INLET AT 3 O'CLOCK POS, 10 INCHES AFT OF LIP. FABRICATED AND INSTALLED NEW REPAIR PER MM 54-30-0 PG 801.SDR DL72E954020Skin · crackedAT HMV, FOUND .375 CRACK AT AFT INBD CORNER OF PNEU AIR CONNECTION ACCESS DOOR CUOUT. REPAIRED PER MM 53-30-0 PG 803.SDR DL72E954017Web · crackedAT HMV, FOUND .5 INCH CRACK IN LT TORQUE BOX WEB IN 48 SECT STA 1223 AT UPPER RIVET ROW. FABRICATED AND INSTALLED REPAIR PER MM 53-11-0 PG 833.SDR DL72E954016Web · crackedAT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 RT SIDE ABOVE S-DUCT. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-10-4 FIG 17.SDR DL72E954015Web · crackedAT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 LT ABOVE S-DUCT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17.SDR DL72E953975Stringer · crackedSTRINGER CRACKED VERT STAB INTERIOR STR 8R CRACKED, LOCATED IN 3RD BAY UP FROM ACCESS HOLE. WORKED AT HMV, REPAIRED PER M/M 55-30-00.SDR DL72E953967Web · crackedWORKED AT HMV. PERFORM PERMANENT REPAIR, CRACK STA 913.5 LT, PER M/M 53-11-00, PG 816. REMOVED AND INSTALLED REPAIR PER M/M 53-11-00.SDR DL72E953965Skin · dentedDEFERRED FROM NR 15. WORKED AT HMV, 6 INCHES LONG BY 2 INCHES WIDE, DENTED/SCRATCHED AREA LWR RT FUSELAGE SKIN STA 1148 BETWEEN STR 19R AND 20R. REPAIRED PER SRM 53-30-03.SDR DL72E953943Spar · crackedNR 3 MID FLAP DURING HMV INSPECTION FOUND A CRACKED AFT SPAR CORD 19 INCHES FROM I/B END AND A CRACKED DOUBLER 37 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0 NRC38851 (2) AFT SPAR CORD WAS CRACKED 41 INCHES FROM O/B END. REPAIRED PER M/M 57-52-0. NRC 8852SDR DL72E953854Eel Power Supply · failedFLOOR EMERGENCY EXIT LIGHTS INOP AFT OF ROW 26. FOUND PWR SUPPLY BAD FOR AFT EMERGENCY TRACK LIGHTING. REPLACED SAME EMERGENCY LIGHTS, NOW TEST NORMAL.SDR DL72E952526Windshield · shorted/arcingDURING CRUISE, COPILOTS WINDSHIELD SHORTED WITH SPARKS BEING EMITTED. SHUT-OFF WINDOW HEAT, NO FURTHER ARCING. REPLACED WINDSHIELD AND CONTROLLER.SDR DL72E950992Flap · crackedFOUND ON LETTER CHECK NR 4 FORE FLAP L/E CRACKED .25 INCH ABOVE NR 7 FLAP TRACK. REPAIRED PER SRM 57-50-4 FIG 1.SDR DL72E950989Web · crackedFOUND ON LETTER CHECK STA 1235 LT LIGHTENING HOLE DAMAGED AT 7:00 POSITION AIR STAIR VERTICAL WEB. REPAIR INSTALLED DOUBLER PER MM 53-11-0 PG 828.
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