Boeing 727-2H3
Service difficulty reports · 547
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 = '7272H3' 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 = '7272H3' 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 K11A2008111772201Web · corrodedE AND E BAY WALKWAY WEB CORRODED AT STA 312 TO 340 AND LBL 38. CORROSION 4 BY 6 INCHES.SDR K11A2008103172202Stiffener · crackedLT FORWARD EDGE ON NLG TRUNNION SUPPORT VERTICAL STIFFENER IS CRACKED 3 INCHES STA 320, LBL 16, WL 149.SDR K11A2008103172201Frame · corrodedCORROSION ON BS 1110 FUSELAGE FRAME BETWEEN STR 17R AND STR 18R. CORROSION 2 X 2 INCHES.SDR K11A2008103072202Structure · crackedAFT AIRSTAIRS LT WING BS 1250 APPROX WL 190 CRACKED AT LIGHTENING HOLE .5 INCH CRACK.SDR K11A2008102372201Structure · corrodedLOWER TEE CHORD FLANGE CORRODED, VIEWED THRU ACCESS HOLE ON NLG WHEEL WELL.SDR K11A2008102372208Intercostal · corrodedINTERCOSTAL CORROSION UNDER F/S SEAT TRACK (CORROSION OUT OF LIMITS).SDR K11A2008102372205Stringer · crackedCRACKED FUSELAGE STRINGER (NOSE WHEEL WELL) AT STA 270.SDR K11A2008102372202Frame · crackedFRAME 1110 LT SIDE AT LBL 30 CRACKED AND DENTED.SDR K11A2008102372207Panel · corrodedNOSE WHEEL WELL PANEL 1104 HAS CORROSION ON ATTACH UNDER NUT PLATES.SDR K11A2008111772202Tee Fitting · corrodedLOWER TEE CHORD OTBD FLANGE UPPER SURFACE CORRODED BETWEEN FRAME WEBS AT STA 302-312, LBL 16, WL 149. CORROSION 1 BY 2 INCHES.SDR K11A2008111272205Frame · corrodedSTA 312 FRAME UPPER CHORD ASSY UPPER AND LOWER SURFACE CORRODED WHERE NLG STEERING CABLE PULLEY BRACKET ATTACHES AT LBL 32. CORROSION 2 X 2 INCHES.SDR K11A2008111272204Web · corrodedNLG WHEEL WELL WEB INNER SURFACE HAS CORROSION AT STA 292, LBL 148-153. CORROSION 1 X 1 INCH.SDR K11A2008111272202Frame · corrodedFRAME WEB HAS CORROSION ON AFT SIDE ABOVE STRINGER 24L AT STA 303.9 LBL 37. CORROSION 2 X 2 INCHES.SDR K11A2008102372213Floorbeam · corrodedFLOORBEAM HAS CORROSION ON UPPER CHORD, UPPER SURFACE.SDR K11A2008110472201Floorbeam · corrodedMAIN DECK, CORROSION ON BS 1110 FLOORBEAM UPPER CHORD AT RBL 62. CORROSION 2 X 1 INCHES.SDR K11A2008102472201Intercostal · corrodedMAIN DECK FLOOR INTERCOSTAL UPPER CHORD AND WEB CORRODED (INTERCOSTAL FRAME).SDR K11A2008120372214Doubler · corrodedAFT LAV SERVICE PANEL SKIN DOUBLER CORRODED ON INSIDE LOWER CORNER.SDR K11A2008102372212Mount Bracket · corrodedAPU INLET SCREEN DRAIN ASSY HORIZONTAL MOUNT BRACKET (CHORD) CORRODED ON INSIDE OF KEEL BEAM.SDR K11A2008102372211Floor Support · corrodedCOCKPIT FLOOR PANEL SUPPORT RAIL HAS SURFACE CORROSION TO BE OUT OF LIMITS.SDR K11A2008102372206Floor Support · corrodedSURFACE CORROSION FOUND ON COCKPIT FLOOR PANEL SUPPORT RAIL TO BE OUT OF LIMITS.SDR K11A2008102772201Shear Tie · corrodedFRAME SHEAR TIE 2 INCHES BY 2 INCHES CORROSION STA 950D, BETWEEN STR 26L AND 27L FRAME SHEAR TIE.SDR K11A2008102372204Floorbeam · corrodedCORROSION AROUND FASTENER HOLE ON FLOORBEAM BOTTOM CHORD.SDR K11A2008102372214Fitting · corrodedFRAME TIE CORRODED, 9 INCHES IN LENGTH.SDR K11A2008111272203Frame · corrodedUPPER CHORD OF FRAME CORRODED BELOW SUB FLOOR AT STA 304, ABOVE STR 24L, LBL 38. CORROSION 2 X 1 INCHES.SDR K11A2008102372210Frame · corrodedUPPER WEB FRAME BELOW SUB FLOOR CORROSION (WHERE CABLES PASS THRU).SDR K11A2008102372209Stringer · corrodedSTRINGER ANGLE CORROSION OUT OF LIMITS.SDR K11A20080817001Floorbeam · gougedFLOORBEAM STA 380, RBL 45 HAS GOUGES ON BOTH SIDES ON LOWER SURFACE OF UPPER CHORD AND ON UPPER WEB.SDR K11A2008102372203Floorbeam · corrodedFLOORBEAM ON THE LOWER SURFACE OF THE UPPER CHORD AT WEB HAS GRINDING MARKS AND CORROSION BEYOND LIMITS.SDR K11A2008111272201Frame · corrodedEVIDENCE OF CORROSION ON LOWER WEB OF SUB FLOOR FRAME ON AFT SIDE BETWEEN STRINGERS 26L AND 27L BY NOSE GEAR WELL BULKHEAD AT STA 304, LBL 16, WL 146.SDR K11A2008120372213Window Post · crackedTHE E-H WINDOW POST CRACKED 4 INCHES ABOVE LOWER CORNER.SDR K11A2009010272303Stringer · corrodedSTRINGER CORROSION.SDR K11A2009010172301Shear Tie · crackedSHEAR TIE CRACKED.SDR K11A2009010272306Skin · dentedDENT IN FUSELAGE.SDR K11A2008123172309Stringer · corrodedSTRINGER HAS CORROSION.SDR K11A2008112072303Skin · corrodedSKIN CORROSION, 4 INCHES ABOVE NR 2 ENG RT SIDE.SDR K11A2008123172310Skin · damagedL1 DOOR HAS INTERIOR SKIN DAMAGE.SDR K11A2008112072305Frame · corrodedFRAME, CORROSION OUT OF LIMITS STA 227R 16 INCHES OFF CABIN FLOOR.SDR K11A2009010272304Fitting · corrodedDOOR BACK UP FITTING CORRODED.SDR K11A2009010272302Stringer · corrodedSTRINGER CORROSION.SDR K11A2008123172308Support Frame · corrodedCOCKPIT SLIDING WINDOW SUPPORT FRAME HAS AREA OF CORROSION.SDR K11A2008112072302Frame · corrodedFRAME, CORROSION TO BE OUT OF LIMITS STA 211 APPROX 19 INCH FROM CABIN FLOOR.SDR K11A2008112072301Skin · gougedEXTERNAL FUSELAGE SKIN, SKIN GOUGED OUT OF LIMITS.SDR K11A2008123172307Fastener · looseC-3 DOOR HAS LOOSE FASTENERS.SDR K11A2009010272305Frame · damagedHOLES IN FRAME ELONGATED, L 1 DOOR.SDR K11A2008123172311Beam · corrodedLT MLG BEAM LOWER SURFACE CORROSION HAS CORROSION IN AND AROUND FASTENER HOLES.SDR K11A2008120372210Spar · corrodedELEVATOR REAR SPAR CORRODED.SDR K11A2008112872203Skin · damagedC-3 BULKPIT DOOR EXTERIOR SURFACE WIDE ARRAY OF DAMAGE, INCLUDING CORROSION, DING/DENTS AND EDGE DAMAGE.SDR K11A2008120272211Skin · damagedPREVIOUSLY BLENDED AREA IN SKIN WITH QUESTIONABLE LIMITS.SDR K11A2008112672213Skin · damagedAPPROX STA 300 STR 18R SKIN DAMAGE AT LAV SERVICE CUTOUT FWD UPPER CORNER.SDR K11A2008120372212Angle · corrodedCORROSION IN THE NOSE LANDING GEAR WHEEL WELL, LT ANGLE.
Back to Boeing 727-2H3