Boeing 727-224
Service difficulty reports · 2,252
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 = '727224' 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 = '727224' 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 CALA9801556Bolt · corrodedINSPECTION FOUND RT WING FLAP TRACK NR 5 CORRODED AT FORWARD ATTACH BOLT. THE NR 5 FLAP TRACK AND ATTACH BOLT WERE REMOVED AND REPLACED IAW MM 57-50-0.SDR CALA9801555Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT OUTBOARD AILERON LEADING EDGE RIB JUST OUTBOARD OF NR 3 HINGE. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4.SDR CALA9801554Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN JUST FORWARD OF CAPTAIN'S WINDSHIELD WIPER AREA. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1. A DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 51-30-2, 51-20-4, AND ECRA 5330-02698.SDR CALA9801553Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J BEAM AT CUTOUT AREA ABOVE NR 7 SPOILER. THE J BEAM WAS REPAIRED IAW ECRA 5780-02914.SDR CALA9801552Skin · delaminatedINSPECTION FOUND RT ELEVATOR CONTROL TAB INBOARD TRAILING EDGE DELAMINATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9801551Skin · delaminatedINSPECTION FOUND RT WING INBOARD AFT FLAP LOWER SURFACE DELAMINATED AT MID OUTBOARD AREA. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-10.SDR CALA9801550Skin · debondedINSPECTION FOUND LT INBOARD FOREFLAP DEBONDED ON LOWER SURFACE ABOVE NR 4 CARRIAGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-2.SDR CALA9801549Skin · debondedINSPECTION FOUND LT OUTBOARD AILERON TAB TRAILING EDGE DEBONDED 41.5 INCHES FROM INBOARD END. THE OUTBOARD AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.SDR CALA9801546Angle · crackedINSPECTION FOUND LT WING INBOARD NR 7 SPOILER ACTUATOR SUPPORT FITTING LOWER ANGLES (TWO EACH) RIB PANEL SUPPORTS CRACKED. THE CRACKS WERE .5 INCH LONG. THE INBOARD AND OUTBOARD ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9801545Skin · tornINSPECTION FOUND LEFT WING UPPER TRAILING EDGE SKIN TORN AT ALL THREE HINGES OF NR 6 SPOILER. THE TORN AREAS WERE CUT OUT IAW SRM 57-30-4. A DOUBLER WAS INSTALLED AT EACH OF THE THREE HINGES IAW SRM 57-30-4, FIGURE 10, SHEET 3.SDR CALA9801544Bulkhead Beam · crackedINSPECTION FOUND TWO 1.5 CRACKS IN AFT BULKHEAD VERTICAL SUPPORT BEAM AT AFT CARGO COMPARTMENT, BS 1183, RBL 46.93. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5310-03758.SDR 98ZZZX3504Seat Track · corrodedDURING C-CHECK, CORROSION WAS NOTED FORWARD LAVATORY/GALLEY AREA SEAT TRACK RBL 24 - FS 420 - FS 460.SDR 98ZZZX3503Strap · corrodedDURING C-CHECK, CORROSION WAS NOTED AFT GALLEY AREA ON FLOORBEAM LOWER T-CHORD STRAP APPROXIMATELY 45 RBL STA 1050 - 1070.SDR 98ZZZX3502Strap · corrodedDURING C-CHECK, CORROSION WAS NOTED AFT RT LAVATORY AREA BOTTOM T-CHORD OF FLOORBEAM ATTACH STRAP FS 1130 APROXIMATELY RBL 20.SDR 98ZZZX3501Web · corrodedDURING C-CHECK, CORROSION WAS NOTED ON SHEAR WEB AROUND SINK DRAIN AFT RT LAVATORY.SDR 98ZZZX3500Strap · corrodedDURING C-CHECK, CORROSION WAS NOTED AFT GALLEY AREA. LOWER T-CHORD STRAP FS 1050 - FS 1070 APPROXIMATELY RBL 24.SDR 98ZZZX3498Floorbeam · corrodedDURING C-CHECK, CORROSION WAS NOTED ON FLOORBEAM BOTTOM T-CHORD AROUND NUTPLATES FS 1110 APPROXIMATELY RBL 50.SDR 98ZZZX3497Support · corrodedDURING C-CHECK, CORROSION WAS NOTED ON LT AFT LAVATORY ON FLOORBOARD SUPPORT LBL 15 FS 1130 - FS 1148.SDR 98ZZZX3496Frame · corrodedDURING C-CHECK, CORROSION WAS NOTED IN E/E COMPARTMENT FRAME 440 AT STR 27R.SDR 98ZZZX3495Skin · corrodedDURING C-CHECK, CORROSION WAS NOTED UNDER L1 DOOR RAIN GUTTER.SDR 98ZZZX3494Skin · corrodedDURING C-CHECK, CORROSION WAS NOTED ON SKIN OF 42 DOOR (LOWER HINGE).SDR 98ZZZX3493Skin · corrodedDURING C-CHECK, CORROSION WAS NOTED ON EXTERIOR SKIN OF R-2 DOOR (PILLOWING MANY AREAS AND POPPED RIVETS).SDR 98ZZZX3492Support · corrodedDURING C-CHECK, CORROSION WAS NOTED ON FLOOR SUPPORT FORWARD LAVATORY INBOARD WALL APPROXIMATELY RBL 15 STA 312 - STA 344. (X)SDR 98ZZZX3491Fuselage Skin · corrodedDURING C-CHECK, CORROSION WAS NOTED ON SKIN OF R2 DOOR FORWARD OF UPPER HINGESDR 98ZZZX3490Support · corrodedDURING C-CHECK, CORROSION WAS NOTED ON FORWARD LAVATORY FLOOR SUPPORT APPROXIMATELY FS 312 JUST UNDER LAVATORY SINK CABINET.SDR 98ZZZX3489Splice · corrodedDURING C-CHECK, CORROSION WAS NOTED ON STRINGER SPLICE STR 30 STA 1148 - STA 1166.SDR 98ZZZX3488Hinge · corrodedDURING C-CHECK, CORROSION WAS NOTED ON AFT LAVATORY SERVICE DOOR UPPER AND LOWER HINGES.SDR 98ZZZX3487Stringer · corrodedDURING C-CHECK, CORROSION WAS NOTED ON STRINGER 22L STA 1148.SDR CALA9801548Skin · debondedINSPECTION FOUND LT WING NR 4 SPOILER DEBONDED AT LOWER SKIN. THE NR 4 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9801547Skin · debondedINSPECTION FOUND THE LT WING NR 6 SPOILER LOWER SKIN DEBONDED AT FORWARD END. THE NR 6 SPOILER WAS REMOVED AND REPLACED IAW MM 57-00 AND 27-60-1.SDR CALA9801543Bolts · corrodedINSPECTION FOUND FOUR VERTICAL STABILIZER TENSION TIE BOLTS CORRODED AT TOP OF STABILIZER. THE FOUR BOLTS WERE REMOVED AND REPLACED IAW SRM 55-20-00.SDR CALA9801542Sidewall · crackedINSPECTION FOUND A .125 INCH CRACK IN LEFT SIDEWALL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-20-1. DOUBLER AND FITTINGS WERE INSTALLED IAW ECRA 5310-03759.SDR CALA9801541Skin · delaminatedINSPECTION FOUND AREAS OF DELAMINATED SKIN ON TOP AND BOTTOM OF LT WING OUTBOARD AILERON OUTBOARD TRAILING EDGE WEDGE PANEL. THE WEDGE PANEL WAS REMOVED AND REPAIRED IAW SRM 57-50-5. THE PANEL WAS REINSTALLED IAW SRM 51-10-1.SDR CALA9801540Skin · crackedINSPECTION FOUND A .875 INCH AND .25 INCH CRACK IN LT OUTBOARD FOREFLAP LEADING EDGE CUTOUT ABOVE NR 1 FLAP TRACK. THE FLAP WAS REPAIRED IAW SRM 57-50-4, FIGURE 1.SDR CALA9801539Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 SLAT AT OUTBOARD HOOK. A REPAIR WAS ACCOMPLISHED IAW SRM 57-50-3, FIGURE 10.SDR CALA9801538Beam · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING TRAILING EDGE J BEAM JUST ABOVE NR 8 SPOILER MOUNT. REPAIR PARTS WERE INSTALLED IAW ECRA 5720-01676.SDR CALA9801534Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN L-ANGLE OF LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-30-2.SDR CALA9801533Chord · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LOWER FORWARD CHORD OF LT WING BELOW NR 7 SPOILER ACTUATOR. THE CRACKED SECTION WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5720-01675.SDR CALA9801532Fitting · corrodedINSPECTION FOUND NOSE GEAR LT TRUNNION FITTING AND CAP CORRODED IN AREAS OF BUSHING RECESS. THE FACES AND BORE OF LT NLG TRUNNION AND CAP ASSEMBLY WERE MACHINED IAW SRM 53-40-1 AND ECRA 5340-01323.SDR CALA9801531Fitting · corrodedINSPECTION FOUND NOSE GEAR RT TRUNNION FITTING AND CAP CORRODED. THE STIFFENERS AND FITTING WERE REMOVED AND THE AREA WAS REPAIRED IAW SRM 51-10-2 AND 51-10-6.SDR CALA9801530Chord · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT WING TRAILING EDGE LOWER CHORD AT NR 8 SPOILER ACTUATOR CASTING. THE CRACKED SECTION OF CHORD WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND ECRA 5720-01675.SDR CALA9801519Bracket · crackedINSPECTION FOUND A 0.4 INCH CRACK IN RT WING LEADING EDGE FLAP NR 6 ACTUATOR MOUNT BRACKET. THE MOUNT BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.SDR CALA9801518Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J-BEAM APPROXIMATELY 1.5 INCHES ABOVE NR 7 SPOILER ACTUATOR AT CUTOUT ABOVE INBOARD END OF AFT FALSE SPAR. PANELS AND A FITTING WERE REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5740-02914 AND SRM 51-10-2, AND 51-10-6. THE SDR CALA9801509Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LT FUSELAGE SKIN BETWEEN WINDOWS NR 16 AND NR 17 AT STA 680. THE CRACKED AREA WAS REPAIRED IAW SRM 51-40-00, 51-10-6, AND 51-10-2.SDR CALA9801508Web · corrodedINSPECTION FOUND CORROSION ON TOP OF AFT CABIN FLOOR SUPPORT WEB AT BS 1148 TO 1183, RBL 25 TO LBL 25. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1.SDR CALA9801507Web · corrodedINSPECTION FOUND LT LAV FLOOR WEB CORRODED AT STA 1130, LBL 27. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, SHEET 6.SDR CALA9801506Bracket · crackedINSPECTION FOUND A .0781 INCH CRACK AT UPPER FORWARD LEG OF LT GEAR UPLOCK SUPPORT BRACKET WHERE IT MOUNTS TO FUSELAGE BS 910 BETWEEN STRINGER 18A LEFT AND 18L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4.SDR CALA9801505Skin · corrodedINSPECTION FOUND FORWARD LOWER C-3 DOOR CUTOUT CORRODED IN AFT CARGO COMPARTMENT BETWEEN LONGERON 25R AND 26R. THE CORRODED AREA WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 53-10-1, PAGE 5, FIGURE 1.SDR CALA9801504Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT ATTACH BOLT IN STRINGER 9R AT VERTICAL STABILIZER INNER COMPARTMENT NR 9 RIB. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-4. A REPAIR WAS INSTALLED IAW SRM 55-20-4, FIGURE 1, SHEET 5, AND SRM 51-10-2.SDR CALA9801503Plate · crackedINSPECTION FOUND A 4 INCH CRACK IN VERTICAL STABILIZER INNER COMPARTMENT NR 1 RIB LOWER LT CORNER PLATE JUST AFT OF S-DUCT. THE RIVETS WERE REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 51-30-2.
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