Boeing 727-222
Service difficulty reports · 1,723
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 = '727222' 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 = '727222' 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 2003F00453Fitting · corrodedAT C-CHECK, FOUND VERTICAL STAB AT FIN STATION 316, HORIZONTAL STAB HINGE FITTING BEARING HOLE, LT SIDE, HAS CORROSION ON INSIDE DIAMETER. REWORK VERTICAL STAB, HORIZONTAL STAB HINGE FITTING BEARING HOLE AT LEFT SIDE AND INSTALLED NEW BEARING. (M)SDR 2003F00466Support Angle · crackedAT C-CHECK, FOUND CRACK ON SUPPORT ANGLE, FUSELAGE BODY FAIRING, STATION 720, STRINGER 29L. REPAIRED SUPPORT ANGLE BELOW FUSELAGE BODY FAIRING AT INBOARD END, STATION 720 STRINGER 29L. (M)SDR 2003F00464Bearing · crackedAT C-CHECK, FOUND CRACK ON VERTICAL STAB, LEFT HORIZONTAL STAB HINGE BEARING. REMOVED AND REPLACED VERTICAL STAB, LEFT HORIZONTAL STAB HINGE BEARING. (M)SDR 2003F00452Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, RIGHT OUTER HINGE PIN IS GALLED AND PITTED. REMOVED AND REPLACED HORIZONTAL STAB RIGHT OUTER HINGE PIN. (M)SDR 2003F00450Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, LEFT INNER HINGE PIN, HAS CORROSION ON THREADED END. REMOVED AND REPLACED HORIZONTAL STAB LEFT INNER HINGE PIN. (M)SDR 2003F00438Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, RIGHT INNER HINGE PIN, HAS CORROSION ON THREADED END. REMOVED AND ERPLACED RIGHT INNER HINGE PIN. (M)SDR 2003F00437Hinge Pin · corrodedAT C-CHECK, FOUND HORIZONTAL STAB, LEFT OUTER HINGE PIN, IS CRACKED AND CORRODED. REMOVED AND REPLACED HORIZONTAL STAB RIGHT OUTER HINGE PIN. (M)SDR 2003F00266Bearing · crackedAT C-CHECK, FOUND CRACK ON VERTICAL STAB, RIGHT HORIZONTAL STAB HINGE BEARING. REMOVED AND REPLACED VERTICAL STAB, RIGHT HORIZ STABILIZER HINGE BEARING. (M)SDR 2003F00467Structure · crackedAT C-CHECK, FOUND CRACK ON NR 4 KRUEGER FLAP, INBOARD EDGE. (M)SDR 2003F00465Floorbeam · corrodedAT C-CHECK, FOUND CORROSION, FORWARD CARGO PIT, MAIN FLOORBEAM, LOWER FLANGE AT STATION 575, RBL 0, BENEATH NUTPLATE. CUTOUT DAMAGED AREA. FABRICATED ANGLE REPAIR AND FILLER. TREATED AND PRIMED. INSTALLED FABRICATED ANGLE ON FORWARD CARGO PIT, MAIN FLOORBESDR 2003F00463Torque Box · crackedAT C-CHECK, FOUND CRACK ON AIRSTAIR TORQUE BOX, STATION 1263. CUTOUT CRACKED AREA AND INSTALLED DOUBLER. (M)SDR 2003F00462Structure · crackedAT C-CHECK, FOUND CRACK ON UPPER TRAILINGE EDGE, NR 6 SLAT WS 629. TRIMMED OUT DAMAGED AREA OF TRAILING EDGE. FOUND TO BE WITHIN LIMITS. ALODINED BARE METAL AT NR 6 SLAT TRAILING EDGE WL 629. (M)SDR 2003F00461Floorbeam · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBEAM, STATION 328 RBL 10, UNDERNEATH NUTPLATE. REMOVED CORROSION. MATERIAL LOSS OTU OF LIMITS. FABRICATED ONE EACH END CAP AND 4 ANGLES. TREATED, PRIMED AND INSTALLED REPAIRED PARTS. (M)SDR 2003F00456Seat Track · crackedAT C-CHECK, FOUND CRACKED SEAT TRACK AT STATION 948C, LBL 25. REPLACED SEAT TRACK AT STATION 950B TO 950D. (M)SDR 2003F00268Floorbeam · corrodedAT C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT STATION 1130, RBL 45. REMOVED UPPER T-CAP FROM LBL 60 TO RBL 60. FABRICATE, TREAT, PRIME AND INSTALLED NEW T-CAP. (M)SDR 2003F00267Floorbeam · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 1130, LBL 0. REMOVED CORROSION FROM FLOORBEAM AT FUSELAGE STATION 1130 BL 0. REMOVED UPPER T-CAP LBL 60 TO RBL 60, STATION 1130. FABRICATED NEW T-CAP. TREATED, PRIMED AND INSTALLED NEW UPPER T-CAP LBL 60 SDR 2003F00280Floorbeam · corrodedAT C-CHECK, FOUND CORROSION ON TOP OF BEAM IN CABIN FLOOR AREA AT STATION 950, RBL 30 TO RBL 42. REMOVED CORROSION. MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED DAMAGED AREA. TREATED AND PRIMED AREA. (M)SDR 2003F00282Stringer · crackedAT C-CHECK, FOUND FLOOR STRINGER CRACKED AT STATION 950D, ABOVE STRINGER 29R. STOPPED DRILL FOR CRACK TERMINATION. FABRICATED ANGLE REPAIR. TREATED, PRIMED AND INSTALLED AT FUSELAGE STATION 950D, STRINGER 29R. (M)SDR 2003F00281Restraint · crackedAT C-CHECK, FOUND RBL 60, FUSELAGE STATION 680 HAS CRACKED SIDE RESTRAINT. FABRICATED DOUBLER REPAIR. TREATED, PRIMED AND INSTALLED AT FUSELAGE STATION 680, RBL 60. (M)SDR 2003F00451Seat Track · corrodedAT C-CHECK, FOUND CORROSION ON SEAT TRACK AT STATION 1100, RBL 48. REPLACED SEAT TRACK AT FUSELAGE STATION 1070-1136, RBL 48. TREATED AND PRIMED. (M)SDR 2003F00292Stringer · crackedAT C-CHECK, FOUND STRINGER, 8L AT FUSELAGE STATION 380 CRACKED. REMOVED DAMAGED AREA FROM FRAME AT FUSELAGE STATION 380, STRINGER 8L. FABRICATE REPAIR DOUBELR. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M)SDR 2003F00291Panel · crackedAT C-CHECK, FOUND STRINGER 5L, FUSELAGE STATION 360, SUPPORT PANEL 6F, CRACKED. REMOVED AND REPLACED PANEL STATION 360, STRINGER 5L. (M)SDR 2003F00284Frame · crackedAT C-CHECK, FOUND NR 2 ENGINE BULKHEAD AT FUSELAGE STATION 1342 ENGINE COWL LIP SEAL IS CRACKED AT 10 O'CLOCK TO 11 O'CLOCK POSITION. INSTALLED NEW COWL SEAL LIP RETAINER NR 2 ENGINE AT STATION 1342 FROM STRINGER 6L TO STRINGER 6R. (M)SDR 2003F00279Seat Track · corrodedAT C-CHECK, FOUND SEAT TRACK CORRODED AT STATION 1110 TO 1120, RBL 45. REMOVED CORROSION ON SEAT TRACK FLANGE. MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK. TREATED AND PRIMED. (M)SDR 2003F00278Panel · crackedAT C-CHECK, FOUND STRINGER 5L, FUSELAGE STATION 350, SUPPORT PANEL IS CRACKED. REMOVED AND REPLACED PANEL STATION 350, STRINGER 5L. (M)SDR 2003F00277Stringer Clip · crackedAT C-CHECK, FOUND STRINGER 4L, STATION 720D, HAS CRACKED CLIP. FABRICATED, TREATED, PRIMED AND INSTALLED NEW CLIP AT STATION 720D, STRINGER 4. (M)SDR 2003F00276Stringer · crackedAT C-CHECK, FOUND STRINGER 9R, FUSELAGE STATION 950C HAS CRACKED STRINGER. FABRICATED, TREATED, PRIMED AND INSTALLED FLANGE AT FUSELAGE STATION 950, STRINGER 9R. (M)SDR 2003F00275Stringer Clip · crackedAT C-CHECK, FOUND STRINGER 8R, FUSELAGE STATION 460 RIGHT SIDE, HAS CRACKED CLIP. REMOVED AND REPLACED CLIP. TREATED AND PRIMED AREA AT STARINGER 8R, FUSELAGE STATION 460. (M)SDR 2003F00270Frame · crackedAT C-CHECK, FOUND NR 2 ENGINE FORWARD BULKHEAD, ENGINE COWL LIP SEAL, CRACKED AT FUSELAGE STATION 1342, 6 O'CLOCK POSITION. INSTALLED NEW COWL SEAL RETAINER, NR 2 ENGINE, STRINGER 6L TO STRINGER 6R. (M)SDR 2003F00269Frame · crackedAT C-CHECK, FOUND NR 2 ENGINE BULKHEAD AT FUSELAGE STATION 1342, ENGINE COWL LIP SEAL CRACKED FROM 1 O'CLOCK TO 4 O'CLOCK POSITION. INSTALLED NEW COWL SEAL RETAINER NR 2 ENGINE AT FUSELAGE STATION 1342, STRINGER 6L TO STRINGER 6R. (M)SDR 2003F00293Door · crackedAT C-CHECK, FOUND NR 2 AFT CARGO DOOR, LOWER AFT CORNER IS CRACKED. REMOVED AND REPLACED LOWER AFT DOOR CORNER, NR 2 CARGO DOOR. (M)SDR 2003F00289Support · corrodedAT C-CHECK, FOUND CORROSION IN E/E BAY, FUSELAGE STATION 328, RBL 50, FLOOR SUPPORT. REMOVED CORROSION AT FUSELAGE STATOIN 328 RBL 50 PER B727 SRM 51-10-06. FOUND TO BE OUT OF LIMITS. FABRICATE FILLER AND TWO ANGLES PER B727 SRM 53-10-8. TREATED AND PRIMEDSDR 2003F00295Mount Bracket · crackedAT C-CHECK, FOUND NR 2 ENGINE CASCADE VANE HAS CRACKED MOUNT BRACKET. WELDED CRACKED MOUNT BRACKET PER AMS STD-1595 AND BAC5975. (M)SDR RYN2003F00005Fitting · crackedDURING B CHECK, LT AND RT MAIN GEAR BEAM FITTING SAFETY BOLT LUGS FOUND CRACKED.SDR RYN2003F00002Splice · crackedAT B CHECK, CRACK FOUND AT FUSELAGE INTERIOR FLOOR SPLICE PLATE TO LOWER SILL BEAM, BS 640.SDR RYN2003F00004Skin · crackedDURING B CHECK, FOUND SKIN CRACKED AT FUSELAGE INTERIOR, LT SIDE, BS 480, FRAME TO LOWER SILL BEAM FROM TIE TO FUSELAGE.SDR RYN2003F00003Floorbeam · crackedAT B CHECK, CRACK FOUND IN FUSELAGE INTERIOR AT FLOORBEAM LOWER CHORD ANGLE BS295, LBBL30.SDR RYN2003F00001Frame · crackedAT B CHECK, CRACK FOUND ON FORWARD AND AFT SIDES OF FUSELAGE INTERIOR, LT FRAME AT BS 680 ATTACHMENT TO SKIN LOWER SILL BEAM.SDR 02FDEA00942Duct · blownAFTER TAKEOFF NR 3 ENGINE HAD FIRE INDICATOR, IAW FLIGHT MANUAL QRM SHUTDOWN ENGINE, FIRELIGHT EXTINGUISHED BY ITSELF AND TESTED GOOD. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. AFTER ENGINE SHUTDOWN WINDMILLED FOR APPROXIMATELY 10 MIN. NR 3 OIL PRESS APPRSDR RYN76391ASkin · crackedDURING A SCHEDULED INSPECTION, FOUND BULGE IN SKIN AND APPROXIMATELY 2.5 INCH HORIZONTAL CRACK AT STA 1020, STRINGER 26R.SDR RYN76392AIntercostal · crackedDURING A SCHEDULED INSPECTION, FOUND RT AFT FUSELAGE TAIL HAS 1 INTERCOASTAL WITH A CRACK RUNNING FROM THE UPPER AFT CORNER APPROXIMATELY 1.125 INCH IN LENGTH.SDR RYN76393ASupport Beam · crackedDURING SERVICE CHECK, FOUND CRACK ON LT MAIN LANDING GEAR SUPPORT BEAM, OB ATTACH LUGS AT UPPER LOCK BOLT LUG.SDR 2002F01042Stringer Clip · crackedAT C-CHECK, FOUND FUSELAGE UPPER LOBE STRINGER SHEAR CLIP, BS 950B STRINGER 9L, CRACKED. (M)SDR 2002F01041Shear Tie · crackedAT C-CHECK, FOUND CABIN SHEAR TIE CLIP CRACKED AT BS 970 STRINGER 4R. (M)SDR 2002F01040Doubler · crackedAT C-CHECK, FOUND PREVIOUS REPAIR WITH SEVERAL CRACKS AT MAIN CARGO, STATION 400-420 BL 0.0. (M)SDR 2002F01032Attach Fitting · crackedAT C-CHECK, FOUND RIGHT LANDING GEAR SUPPORT BEAM OUTBOARD ATTACH FITTING CRACKED. (M)SDR 2002F01031Skin · damagedAT C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN HAD 1 DENT WITH CREASE AND 1 DENT WITH CHERRY MAX RIVET IN CENTER OF DENT AT STABILIZER STATION 4 AND APPROXIMATELY 10 INCHES FORWARD AT STATION 14 IS 2 CREASES WITH A DENT AT DRAIN HOLE. (M)SDR 2002F01039Fitting · crackedAT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 950F STRINGER 4L. (M)SDR 2002F01038Fitting · crackedAT C-CHECK, FOUND CRACKS IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 1050 STRINGER 4L. (M)SDR 2002F01037Fitting · crackedAT C-CHECK, FOUND CRACK IN TIE FITTING, INTERIOR STRUCTURE OF FUSELAGE, UPPER LOBE, FS 1070 STRINGER 4L. (M)
Back to Boeing 727-222