Boeing 727-243
Service difficulty reports · 534
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 = '727243' 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 = '727243' 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 CALA9800114Angle · crackedINSPECTION FOUND A 6 INCH CRACK AT FASTENERS IN SUPPORT ANGLE INSIDE LT WING INBOARD LEADING EDGE AREA AFT OF NR 1 LEADING EDGE FLAP INBOARD END AT L/E STA 130. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9800113Skin · crackedINSPECTION FOUND A .625 INCH CRACK IN LT WING UPPER FIXED LEADING EDGE SKIN WHERE NR 3 SLAT OUTBOARD HOOK ATTACHES. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLER, BACK STRAP, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2.SDR CALA9800112Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON AND AROUND NUT PLATES IN E AND E COMPARTMENT UNDER GALLEY AT STA 380. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-4, AND 51-10-1.SDR CALA9800111Angle · corrodedINSPECTION FOUND Z-ANGLE CORRODED AT STA 616 ABOVE STRINGER 26R IN FORWARD BAGGAGE BIN. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9800110Support · corrodedINSPECTION FOUND RT FLOOR SUPPORT IN FORWARD BAGGAGE BIN CORRODED FROM DTA 616 TO 660. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9800109Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1030 BETWEEN STRINGERS 20-21L. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-6.SDR CALA9800092Frame · crackedINSPECTION FOUND A 3.5 CRACK IN UPPER AFT CORNER OF R-1 DOOR FRAME. A REPAIR WAS FABRICATED AND INSTALLED IAW DRAWING 69-69978, SRM 57-10-02, AND ECRA 5240-01223.SDR CALA9800091Lugs · corrodedINSPECTION FOUND HORIZONTAL STABILIZER LEFT AND RIGHT BEARING SUPPORT VERTICAL LUGS CORRODED. THE LT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01033. THE RT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01141.SDR CALA9800090Skin · corrodedINSPECTION FOUND RT WING INBOARD MID-FLAP UPPER SKIN PILLOWED WITH DISHED FASTENERS IN AREA ABOVE REAR SPAR UPPER CHORD APPROXIMATELY 21 INCHES FROM INBOARD END AND EXTENDING OUTBOARD 6.5 INCHES. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRSDR CALA9800083Torus · crackedINSPECTION FOUND A 5 INCH CRACK IN INBOARD WELD SEAM OF APU TORUS ASSEMBLY. THE APU WAS REMOVED AND REPLACED IAW MM 49-10-01. LEAK AND OPERATIONAL CHECKS WERE GOOD.SDR CALA9800082Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1060, STRINGER 27L. THE CORROSION WAS REMOVED AND THE SKIN WAS REPAIRED IAW SRM 53-30-3.SDR CALA9800081Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUTS, STA 380, RBL 24 TO RBL 62. TWO L-ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-30-8 FIGURE 8.SDR CALA9800080Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUT ON UPPER FORWARD FLANGE LOWER SURFACE AT STA 328, LBL 48. THE FLOORBEAM WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 53-10-8 AND 53-20-11.SDR CALA9701430Duct · brokenNUMBER 3 ENGINE FIRE WARNING LIGHT BELL ON AFTER TAKEOFF. RETARDED THROTTLE, LIGHT WENT OUT. FOUND NOSE COWL ANTI-ICE DUCT BROKEN. REPLACED DUCT ASSEMBLY.SDR CALA9701252Slide · low pressureTHE CREW FOUND L-1 DOOR EMERGENCY SLIDE PRESSURE LOW. THE L-1 DOOR SLIDE WAS REMOVED AND REPLACED PER MM 25-60-15.SDR CALA9701235Prbc · brokenTHE NR 3 ENGINE EGT HIT REDLINE ON TAKEOFF ROLL. REDUCING EPR TO 1.4 FAILED TO KEEP EGT OUT OF REDLINE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FITTING ON PRBC BROKEN. THE PRBC WAS REPLACED IAW MM 75-31-13. THESDR CALA9701189Lock Actuator · inoperativeTHE NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS SELECTED DOWN ON FINAL APPROACH. THE GEAR WAS CYCLED AND EXTENDED NORMALLY FOR A SAFE LANDING AT IAH. MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 3SDR CALA9701156Actuator · inoperativeTHE RT MLG WOULD NOT RETRACT WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION AFTER TAKEOFF. THE SECOND OFFICER'S ANNUNCIATOR PANEL INDICATED THAT THE RIGHT GEAR DOOR WAS DOWN. A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE AIRCRAFT WAS RETURNED TO IAH WHERESDR CALA9701141Battery · dischargedMAIN CABIN OVERHEAD AT STATION 520 LEFT SIDE ESCAPE PATH BATTERY PACK DEAD. REPLACED BATTERY PACK PER MM 33-00-00.SDR CALA9701140Battery · dischargedLEFT OVER WING EMERGENCY EXTERIOR LIGHTS ARE INOP. CLEANED AND RECHARGED BATTERY PACK PER MM 33-50-00.SDR CALA9701139Stringer · cracked2 CRACK ON UPPER WING STRINGER AT W/S 304 IN NR 1 FUEL TANK. CUT OUT DAMAGED AREA AND INSTALLED A 'J' STIFFENER AS PER SRM 57-10-4 FIG 6.SDR CALA9701106Stringer · gougedINSPECTION FOUND STRINGER GOUGED AT LT FUSELAGE STA 1213 ABOVE PANEL NR 3901. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 2.SDR CALA9701099Stringer · corrodedINSPECTION FOUND STRINGER SPLICE AND STRINGER 28L CORRODED IN FORWARD CARGO COMPARTMENT AT STA 480. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.SDR CALA9701135Angle · crackedLEFT AFT LAV FLOOR PANEL TO DITCH PAN ATTACH ANGLE AT LBL 50 HAS 3 FOOT LONG CRACK AT STA 1175. FABRICATED AND INSTALLED NEW ANGLE IN ACCORDANCE WITH SRM 51-30-2.SDR CALA9701105Frame · corrodedINSPECTION FOUND FORWARD SIDE OF AFT BAGGAGE BIN DOOR CORRODED AT UPPER STOP. THE CORRODED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9701097Frame · crackedINSPECTION FOUND A 2 INCH CRACK AT LOWER INBOARD FASTENER HOLE OF FRAME AT STA 783.5, RT SIDE. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FORMED, HEAT TREATED, AND INSTALLED IAW BOEING DRAWING NR 65C36280.SDR CALA9701116Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD END RIB OF RT OUTBOARD MID FLAP LOWER END AT FAIRING LOWER BOLT. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9701108Floorbeam · corrodedINSPECTION FOUND TOP OF FLOORBEAM CORRODED FROM BS 303-344, LBL 30 TO RBL 30. THE CORROSION WAS REMOVED. A T-CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701107Floorbeam · corrodedINSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 1070, RBL 40. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701104Web · corrodedINSPECTION FOUND DELTA BEAM CENTER BOTTOM WEB CORRODED AT BS 780. THE CORRODED SECTION OF WEB WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-40-2, FIGURE 1.SDR CALA9701098Floorbeam · corrodedINSPECTION FOUNDTOP OF FLOORBEAM CORRODED AT STA 380, RBL 24 TO RBL 45.5. THE FLOORBEAM UPPER CHORD WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701134Shear Tie · dentedFUSELAGE HAS DENT IN SHEAR TIE AT STA 380 STR 18L. CUT OUT, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IN ACCORDANCE WITH SRM 53-30-3 FIG 3.SDR CALA9701138Flap · delaminatedRIGHT INBOARD AFT FLAP IS DELAMINATED 32 THROUGH 54 FROM INBOARD END. REMOVED, REPAIRED AND REINSTALLED IN ACCORDANCE WITH MM 57-53-2.SDR CALA9701137Bracket · crackedLEFT WING NUMBER 1 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED BELOW INBOARD UPPER CORNER AREA INSIDE LEADING EDGE, LENGTH .75 FABRICATED AND INSTALLED NEW BRACKET IN ACCORDANCE WITH MM 27-81-1.SDR CALA9701136Bracket · crackedLEFT WING MOUNT BRACKETS CRACKED AT ALL FOUR CORNER AREAS WHERE NUMBER 2 LEADING EDGE FLAP ACTUATOR MOUNTS, INSIDE LEADING EDGE. LENGTH .75. FABRICATED AND INSTALLED NEW MOUNT BRACKET PER MM 27-91-1.SDR CALA9701109Tab · debondedINSPECTION FOUND LEFT OUTBOARD AILERON TAB INBOARD END DEBONDED AND END FILLER MISSING. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-0.SDR CALA9701100Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 188. THE DENTED AREA OF SKIN WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9701096Skin · debondedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD MOST TRAILING EDGE SPLIT/DEBONDED. THE AILERON TRAILING EDGE WEDGE WAS REMOVED. REPLACEMENT SKIN PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 51-30-2. THE AILERON WEDGE WAS REINSTALLED.SDR CALA9701095Skin · crackedINSPECTION FOUND A .3125 INCH CRACK IN LT WING LEADING EDGE SKIN CUTOUT ABOVE NR 3 SLAT INBOARD TRACK. THE CRACKED SECTION OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-30-4.SDR CALA9701115Skin · disbondedINSPECTION FOUND LEFT WING TRAILING EDGE INBOARD FOREFLAP DISBONDED AT INBOARD EDGE OF LOWER SURFACE. A HOT BOND REPAIR WAS ACCOMPLISHED IAW ENGINEERING WORK ORDER 97-0630.SDR CALA9700977Sequence Valve · leakingTHE SYSTEM-A HYDRAULIC FAILURE LIGHTS ILLUMINATED ON CO-PILOT PANEL AFTER GEAR RETRACTION. ALSO, THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ON SECOND OFFICER'S PANEL ILLUMINATED WITH THE ELEVATOR LOW PRESSURE LIGHT ILLUMINATING MOMENTARILY. THE GEAR WAS LOWESDR CALA9700820Hyd Line · leakingTHE 'A' SYSTEM HYDRAULIC FLUID WAS LOST WHEN LANDING GEAR WAS RAISED AFTER TAKEOFF FROM MCO. THE AIRCRAFT WAS RETURNED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MX FOUND THE LT MLG DOOR ACTUATOR PRESSURE LINE LEAKING. THE PRESSURE LINE WAS REMOVED AND REPLACSDR CALA9700796Hyd Module · crackedTHE AIRCRAFT WAS DIVERTED TO PHX, AFTER LOSING THE A-HYDRAULIC SYSTEM FLUID QUANTITY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC MODULE FITTING CRACKED. THE A-SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED. IN ADDITIONSDR CALA9700787Brake Housing · crackedACFT RETURNED TO THE GATE AFTER DRAGGING THE NR 3 BRAKE DURING TAXI. THE NR 3 TIRE CAUGHT ON FIRE, FOAM WAS USED TO EXTINGUISH THE FIRE. THE NR 3 AND 4 MAIN TIRE/WHEEL ASSEMBLIES AND BRAKES WERE REMOVED AND REPLACED. THE NR 3 BRAKE DEBOOST VALVE WAS ALSO RESDR CALA9700516Skin · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT INTERIOR SKIN CORRODED AT ANTENNA, STA 1030 TO 1050, STRINGER 29R TO 30. THE AREA WAS REPAIRED IAW SRM 51-40-3.SDR CALA9700581Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN VENTRAL STAIRWELL TORQUE BOX ANGLE AT STAIR ACTUATOR FITTING, STA 1272, RBL 22. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C27136.SDR CALA9700519Skin · disbondedINSPECTION FOUND LT INBOARD MIDFLAP UPPER SURFACE OF TRAILING EDGE WEDGE DISBONDED 24 INCHES FROM INBOARD END. THE DISBONDED AREA WAS CUT OUT, CORE AND DOUBLERS WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.SDR CALA9700515Skin · corrodedINSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 1130. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9700512Spar Web · crackedINSPECTION FOUND A .75 CRACK IN WEB AT FRONT SPAR JUST OUTBOARD OF LT FORWARD TERMINAL PIN FITTING. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-2.SDR CALA9700580Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD TRACK CUTOUT, STA 216. THE CRACK WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01489.
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