JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer Structure, 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 jasc_code = '5510' 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 jasc_code = '5510' 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 95ZZZW518Bolt · corrodedNR 4 'A' FRAME BOLT UPPER, LEFT STABILIZER SCRAPPED DUE TO CORROSION. REMOVED AND REPLACED BOLT AS REQ'D IAW MM.SDR 95ZZZW517Bolt · corrodedNR 2 'A' FRAME UPPER BOLT LEFT STABILIZER SCRAPED DUE TO CORROSION. REMOVED AND REPLACED BOLT AS REQ'D IAW MM.SDR 95ZZZW693Lugs · corrodedDURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-701-02, CORROSION FOUND AT THE LEFT HORIZONTAL STABILIZER AFT, UPPER CENTER SECTION LUG AROUND THE BUSHINGS. THE BUSHINGS WERE REPLACED PER BOEING SB 737-55-1033 AND 737-55-1055.SDR 95ZZZW692Bolt · galledDURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-701-02, THE RT HORIZONTAL STABILIZER AFT, LOWER BOLT WAS EXTREMELY DIFFICULT TO LOOSEN/REMOVE. ONCE REMOVED, THE BOLT AND BUSHINGS WERE FOUND GALLED. EVIDENCE OF CORROSION AROUND BUSHING TO FITTING LUG MATINGSDR 95ZZZW691Bolt · galledDURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-701-02, THE LEFT HORIZONTAL STABILIZER AFT, LOWER BOLT WAS EXTREMELY DIFFICULT TO LOOSEN/REMOVE. ONCE REMOVED, THE BOLT AND BUSHINGS WERE FOUND GALLED. EVIDENCE OF CORROSION AROUND BUSHING TO FITTING LUG MATISDR DL72S950851Support · crackedAT HMV FOUND SUPPORT STRIP CRACKED ON T/E OF STAB BELOW O/B ELEV ATTCH HNGE POINT. INSTALLED NEW T/E BEAM.SDR UP202227Beam · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LT HORIZ. STAB. LOWER T/E BEAM AT ELEVATOR STA 169-157, STA 142 AND STA 125-121. INSTALLED REPAIR IAW SRM 51-30-2.SDR DLL10950575Fairing · crackedON CLIMB-OUT, HEARD UNUSUAL RUMBLE AS AIRCRAFT ACCELERATED, RUMBLE INCREASED WITH SPEED. FOUND RIGHT LOWER STAB TO FUSELAGE FAIRING LEADING EDGE UNFAIRED WITH SUBSTRUCTURE CRACKED. REPLACED FAIRING PER MM 55-16-00.SDR 95ZZZX819Hinge · corrodedUPON ANNUAL INSPECTION, FOUND SEVERE EXFOLIATION CORROSION ON RT HORIZONTAL STABILIZER HINGE. NOTE: ACFT USED ON FLOATS.SDR TSAA9555041Beam · corrodedDURING HEAVY MAINTENANCE VISIT, RT HORIZONTAL STABILIZER UPPER T/E BEAM - SURFACE CORROSION AT ES 213. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA9555040Beam · corrodedDURING HEAVY MAINTENANCE VISIT, RT HORIZONTAL STABILIZER UPPER T/E BEAM - SURFACE CORROSION AT ES 195.0. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA9555039Beam · corrodedDURING HEAVY MAINTENANCE VISIT, LT HORIZONTAL STABILIZER LOWER T/E BEAM - SURFACE CORROSION AT ES 195.0. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA9555038Beam · corrodedDURING HEAVY MAINTENANCE VISIT, LT HORIZONTAL STABILIZER LOWER T/E BEAM - CORROSION AT ES 50.0. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X)SDR UPS202075Web · corrosionDURING 'D' CHECK, MAINTENANCE FOUND CORROSION IN WEB AT STA 68.92 INSIDE RT HORIZONTAL STAB. INSTALLED REPAIR IAW SRM 55-10-2, 55-10-1, AND 51-30-2.SDR UPS201938Te Beam · corrosionWHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON RT HORIZIZONTAL STAB UPPER T/E BEAM, LOWER SURFACE OF FWD FLANGE AT APPROX STAB STA 118.00. INSTALLED REPAIR IAW SRM 51-30-2.SDR 9500449947Bracket · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN BOTH LEFT AND RIGHT HORIZONTAL STABILIZER 'A' BRACKETS UPPER FASTENER BORES. OVERSIZED BORES AND INSTALLED BUSHINGS PER EA 99-094108 AND -094107 RESPECTIVELY.
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