Boeing 727-21C
Service difficulty reports · 217
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '72721C' 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 aircraft_model_key = '72721C' 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 95FDEA00092Web · corrodedCORROSION ON FRAME WEB BS 760 RBL 65-70 WL 204-208. REPAIRED PER FEDEX EA 7-5310-7-23668.SDR 95FDEA00091Strap · corrodedFRAME STRAP HAS CORROSION AT BS 760, RBL 65, WL 205. REPAIRED PER FEDEX EA 7-5310-7-23668.SDR 95FDEA00090Chord · corrodedCORROSION ON STUB BEAM LOWER ANGLE AT BS 761 WL 204 RBL 60. REMOVED AND REPLACED LOWER CHORD PER FEDEX SRM 51-10-1.SDR 95FDEA00089Strap · corrodedCORROSION (71C708-02) BS 1057-1110, WL 149, RBL 20 ON SCUFF PLATE T-STRAP. REMOVED AND REPLACED T-STRAP PER DRAW NR 65-20732-4.SDR 95FDEA00088Threshold · corrodedCORROSION (71C708-02) BS 1057-1110, WL 148, RBL 25 ON SUBTHRESHOLD PLATE. REMOVED AND REPLACED SUBTHRESHOLD PLATE.SDR 95FDEA00087Angle · corrodedCORROSION ON L ANGLE AT BS 259 WL 150 RBL 20. REMOVED AND REPLACED ANGLE AT BS 259 WL 150 RBL 20 PER FEDEX SRM 51-40-1.SDR 95FDEA00101Stiffener · corrosionSTIFFENER ON TOP OF DOG HOUSE, AT BS 303, RBL 10, WL 181 HAS CORROSION. REMOVED AND REPLACED STIFFENER PER FEDEX SRM 53-10-01.SDR 95FDEA00100Sill Web · crackedIN AFT CARGO AT STA 1050-1057 WL 146, RBL 20 THE SILL WEB IS CRACKED. REMOVED CRACKED WEB, FABRICATED NEW WEB AND INSTALLED SILL WEB PER FEDEX SRM 51-20-1.SDR 95FDEA00099Skin · damageFASTENERS PULLED THROUGH SKIN AT BS 1342, STR 20R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND FORMER SKIN REPAIR PER FEDEX SRM 53-30-3 AT BS 1342 STR 20R.SDR 95FDEA00083Frame · corrosionCORROSION AT BS 1110, WL 154, RBL 25 UNDER TOP FLANGE OF FRAME. REPAIRED FLANGE OF FRAME PER FEDEX SRM 51-40-3 FIG 1 AND 3.SDR 95FDEA00081Stringer · damagedTOOLING MARKS BS 441.5, STR NR 1 LT AND RT. REMOVED SECTION OF STR, AND CUT OUT A REPLACEMENT SECTION. FABRICATED AND SPLICED IN PER SRM FEDEX 53-10-3 AT STR NR 1 STA 430-450.SDR 95FDEA00080Skin · gougedGOUGE IN SKIN BS 1345 STR 11L. CUT OUT DAMAGE AT BS 1345, STR 11L. FABRICATED, INSTALLED DOUBLER AND FILLER PER FEDEX SRM 54-30-3.SDR 95FDEA00076Expansion Link · corrodedEXPANSION LINK BETWEEN STA 848-87, LBL 25, WL 208 IS CORRODED BEYOND LIMITS. REMOVED CORROSION, TREATED AND PRIMED ALL PER SRM 51-10-6, 53-10-1 AND FEDEX EA 7-5310-23666.SDR 95FDEA00074Support · corroded2 CORRODED FASTENERS RBL 40, BS 320, WL 208 UNDERSIDE OF BEAM AND CHORD. ALSO, FOUND FLOOR SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT PER BOEING DRAWING 65-26173, FEDEX SRM 51-10-02, 51-30-2 AND MM 51-20-21.SDR 95FDEA00084Angle · crackedWEB AT LBL 42 BETWEEN BS 294 AND 312 HAS CRACK ON EXISTING REPAIR ANGLE, WL 207. REMOVED WEB, FABRICATED, ALODINED, PRIMED AND PAINTED. INSTALLED FABRICATED WEB AT LBL 42 BETWEEN BS 294 AND 312, WL 207 PER FEDEX SRM 51-20-1 AND PER FEDEX MM 51-20-2.SDR 95FDEA00077Bracket · crackedWHILE WORKING CARD NR 0278 FOUND BRACKET STA 303, LBL 32 CRACKED WL 208. REMOVED AND REPLACED BRACKET PER SRM 51-20-1.SDR 95FDEA00075Seat Track · corrodedSEAT TRACK CORRODED WL 208, LBL 25, STA 870-1070. REMOVED AND REPLACED NEW SEAT TRACK BS 870-1070, LBL 25, WL 208 IAW FEDEX 727 SRM 53-10-5.
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