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 CALA9900479Support · crackedFORWARD CARGO COMPARTMENT OVERHEAD FLOOR BEAM SUPPORT SIDE BRACE BETWEEN STA 720 - 720A CRACKED IN THREE PLACES. REMOVED AND FABRICATED NEW ANGLE, TREATED PRIMED AND INSTALLED ANGLE PER SRM 51-30-2.SDR CALA9900478Hinge · crackedAPPROX .25 CRACK AT LEFT WING UPPER T/E AT 2ND FROM O/B CUT OUT FOR NR 4 SPOILER HINGE. STOP DRILLED CRACK PER SRM 57-30-4. FABRICATED REPAIR PER SRM 57-30-04 PAGE 29. TREATED PRIMED AND INSTALLED PER SRM 51-10-2 AND 57-30-04 PAGE 27.SDR CALA9900477Mount · crackedAPPROX .375 VISIBLE BRANCHING CRACK AT LEFT WING NR 2 SLAT WHERE INBOARD UP STOP PAD MOUNTS. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED EXTRUDED ANGLE REPAIR PER 51-4-4 FIG 3. INSTALLED PANELS PER 51-30-2.SDR CALA9900476Rib · crackedAPPROX 1.25 CRACK AT 3RD FROM INBOARD END RIB INSIDE LEFT WING NR 2 SLAT. STOP DRILLED CRACK. FABRICATED AND INSTALLED TYPICAL FORM DOUBLER FROM 2024 T3 PER SRM 51-40-3. INSTALLED ACCESS PANEL PER 51-30-2.SDR CALA9900475Intercostal · corrodedCABIN FLOOR INTERCOSTAL CRACKED (10) ON TOP FLANGE 0 BL FS 400 - 420. REMOVED DAMAGED FLANGE AND FABRICATED NEW FLANGE, TREATED, PRIMED, AND INSTALLED PER SRM 51-10-1, 51-30-2, AND 51-10-6.SDR GAIA9950Batteries · dischargedDURING ROUTINE 'B' CHECK MAINTENANCE, FOUND TWO, EACH FORWARD EMERGENCY EXIT LIGHTS WITH DEAD BATTERIES. REMOVED AND REPLACED TWO FORWARD ENTRY AREA "EMERGENCY EXIT' LIGHTS. NO ADDITIONAL PROBLEMS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR GAIA9948Accessory Box · malfunctionON FINAL APPROACH TO TOL, PUT GEAR DOWN AND 3 RED LIGHTS, AND 3 GREEN LIGHTS AND TAIL SKID LIGHT. RECYCLED GEAR AND GOT 3 GREEN LIGHTS, NORMAL INDICATIONS. AIRCRAFT MADE AN UNEVENTFUL LANDING AT TOL. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX. OPERATISDR MZZA99079Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO PLACES CRACKS WERE FOUND ON STRINGER 18A BETWEEN BS 940 AND BS 945. THE CRACKED STRINGER WAS CUT OFF AND REPAIRED PER ECRA 5310-03842. (M)SDR GAIA9947Battery · dischargedDURING P/S CHECK, FOUND L-1 EMERGENCY EXIT LIGHT BATTERY DEAD. CHARGED BATTERIES FOR EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR MZZA99080Fitting · brokenTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A BROKEN LUG WAS FOUND ON LEFT WING OUTBOARD AILERON TAB ROD ATTACHING FITTING. THE BROKEN LUG P/N 65-19620-13 WAS REMOVED AND REPLACED PER SRM 51-30-02. (M)SDR MZZA99083Stringer · corrosionTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON STRINGER 26L AT BS 720A. THE CORRODED AREA WAS REMOVED AND REPAIRED PER SRM 51-40-03. (M)SDR MZZA99078Rear Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CORROSION ON LEFT INBOARD WING MID FLAP REAR SPAR LOWER CHORD AT WBL 115. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER EC/RA 5750-03182. (M)SDR 99ZZZX1758Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1060 - STA 1110, LBL 45.SDR 99ZZZX1757Stringer · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STR 28R, STA 950F - STA 990.SDR 99ZZZX1756Channel · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON A SECTION OF HAT CHANNEL LEFT AFT LAVATORY STA 1137 - STA 1176.SDR 99ZZZX1755Hinge · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON R-1 DOOR'S LOWER HINGE.SDR 99ZZZX1754Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON NR 1 NOSE FLAP OF NR 1 KREUGER FLAP AT BUSHING FLANGE ATTACH POINT.SDR 99ZZZX1753Beam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM.SDR 99ZZZX1752Strap · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON STRAP IN C-1 PIT FLOOR AREA JUST FORWARD OF STA 540 THAT CROSSES FLOORBEAM.SDR 99ZZZX1751Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED AT STA 720L, STR 27.SDR MZZA99075Plate · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH DIAMETER CORROSION WAS FOUND ON RIGHT INBOARD MIDFLAP INNER SPLICE PLATE AT WBL 242. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 51-30-02, 51-10-02. (M)SDR MZZA99081Track · rustedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RUST WAS FOUND ON NR 4 FLAP TRACK FORWARD MOUNTING PAD A UPPER SURFACE AND HOLES. THE RUSTED TRACK, P/N 65-19269-20 WAS REMOVED AND REPLACED WITH P/N 65-19269-13 PER B727 MM 27-51-31 AND OPERATIONAL CHESDR MZZA99076Rear Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY 5 INCH AREA CORROSION WAS FOUND ON RIGHT OUTBOARD MIDFLAP REAR SPAR LOWER CHORD FORWARD FLANGE AT WBL 431. THE CORROSION WAS REMOVED AND REPAIRED PER ECRA 5750-03184 DATED ON APR 6, 1999. (SDR MZZA99074Angle · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A .25 INCH LONG CRACK WAS FUOND ON RIGHT INBOARD MIDFLAP T/E LOWER CLOSURE ANGLE AT WBL 108. THE CRACKED AREA WAS CUT OFF AND REPAIRED PER SRM 51-40-04, 51-30-02. (M)SDR MZZA99072Floorbeam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON NR 6A GALLEY FLOORBEAM BETWEEN RBL 32 AND RBL 44 AT BS 1130. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 53-10-08 AND 51-10-02. (M)SDR MZZA99071Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON LEFT AFT LAVATORY FORWARD SUPPORT HAT CHANNEL BETWEEN LBL 28 AND LBL 34 AT BS 1138. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 53-10-02 AND 51-40-04. (M)SDR MZZA99077Pulley · frozenTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FROZEN BEARING WAS FOUND ON NR 4 SPOILER ACTUATOR PULLEY. THE DAMAGED PULLEY P/N BACP3QJ4 WAS REMOVED AND REPLACED WITH A NEW ONE PER MM 27-61-41. (M)SDR MZZA99070Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY .5 INCH AREA IG CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 798 AND STRINGER 10L. THE CORROSION WAS REMOVED AND REPAIRED PER SRM 53-30-03 FIG 15A 51-10-02. (M)SDR MZZA99084Stringer · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON STRINGER 27R TEE CHORD AT C2 DOOR CUT OUT OUTBOARD HORIZONTAL FLANGE UPPER SURFACE BETWEEN 950E PLUS 12.5 AND BS 979.5. THE CORRODED AREA WAS REMOVED AND REPAIRED PER EC/RA 5310-0SDR MZZA99069Pulley · frozenTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A FROZEN PULLEY WAS FOUND ON NR 12 SPOILER. THE FROZEN PULLEY P/N BACP30K-2D WAS REMOVED AND REPLACED PER B727 MM 27-61-00 AND OPERATIONAL CHECK FOUND NORMAL. (M)SDR MZZA99073Skin · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH LONG CRACK WAS FOUND ON AFT BILGE SKIN AT BS 1184. THE CRACK AREA WAS CUT OFF AND REPAIRED PER SRM 53-30-03. (M)SDR CALA9900188Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 5 FLAP TRACK CARRIAGE LOWER FORWARD ROLLER I/B YOKE FITTING. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 27-51-3.SDR CALA9900187Acoustic Panel · tornINSPECTION FOUND NR 2 ENGINE INLET ACOUSTIC PANEL TORN. THE TORN AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 54-10-3.SDR CALA9900186Skin · corrodedINSPECTION FOUND LT O/B MIDFLAP UPPER TRAILING EDGE SKIN CORRODED AND SEPARATING I/B TO O/B END. INSTALLED NEW TRAILING EDGE IAW SRM 51-30-2.SDR CALA9900184Skin · delaminatedINSPECTION FOUND LT TRAILING EDGE O/B AFT FLAP UPPER SURFACE DELAMINATED. THE LT O/B AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-12.SDR CALA9900183Skin · corrodedINSPECTION FOUND THE LT WING NR 10 SPOILER CORRODED WITH SCREWS PULLING THROUGH SKIN AT TOP CENTER HINGE. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1.SDR CALA9900182Skin · delaminatedINSPECTION FOUND THE LT WING NR 13 SPOILER UPPER TRAILING EDGE DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-00.SDR CALA9900181Skin · corrodedINSPECTION FOUND LT WING NR 6 L/E SLAT O/B END UPPER AND LOWER SURFACES CORRODED AT SCREWS. THE SLAT WAS REMOVED AND REPLACED IAW MM 27-80-00.SDR CALA9900180Skin · delaminatedINSPECTION FOUND RT TRAILING EDGE O/B AFT FLAP LOWER SURFACE DELAMINATED. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-50-02.SDR CALA9900179Skin · corrodedINSPECTION FOUND RT O/B FOREFLAP CORRODED ON LOWER AND UPPER SURFACE I/B TO O/B. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.SDR CALA9900178Skin · debondedINSPECTION FOUND THE LT WING NR 2 SPOILER DEBONDED AT TRAILING EDGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-81.SDR CALA9900177Spar Chord · corrodedINSPECTION FOUND TOP SURFACE OF LT WING FRONT SPAR LOWER CHORD CORRODED AT FS 355 TO 367. THE FASTENERS AND RIB WERE REMOVED FOR ACCESS. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-1, 51-20-2, AND ECRA 5710-01945.SDR CALA9900174Wire · failedINSPECTION FOUND FORWARD AISLE EMERGENCY CEILING LIGHT INOPERATIVE. MAINTENANCE FOUND EMERGENCY AISLE LIGHT FORWARD SECTION WIRING SPLICE AT FAULT. THE WIRING SPLICE WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-5, PAGE 501.SDR CALA9900173Fitting · brokenINSPECTION FOUND RT O/B AILERON TAB SUPPORT FITTING (SECOND FROM O/B END) BROKEN OFF INSIDE AILERON. THE TAB SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-2.SDR CALA9900172Skin · delaminatedINSPECTION FOUND LT WING I/B AFT FLAP DELAMINATED. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-50-2.SDR CALA9900171Wire · failedINSPECTION FOUND LT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND POWER WIRE AT BATTERY PACK AT FAULT. THE WIRING SPLICE WAS REPAIRED IAW MM 33-51-01.SDR CALA9900170Wire · looseINSPECTION FOUND L-2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE AT POWER SUPPLY CONNECTOR. THE WIRING WAS SECURED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-22, PAGE 201.SDR CALA9900160Skin · debondedINSPECTION FOUND LT WING NR 4 SPOILER UPPER SURFACE OB T/E DEBONDED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9900159Spoiler · delaminatedINSPECTION FOUND NR 11 SPOILER SPLIT AND DELAMINATED AT CENTER T/E TOP SURFACE AREA. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.SDR CALA9900158Beam · crackedINSPECTION FOUND A .25 CRACK IN J BEAM ABOVE LT WING NR 7 SPOILER ACTUATOR. THE J BEAM WAS REMOVED IAW SRM 51-30-2. A NEW J BEAM WAS INSTALLED WITH NUT PLATE IAW SRM 51-30-2 AND 51-10-2.
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