Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 SCNA97195Batteries · dischargedTHE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN AFT AIRSTAIR LIGHT, LIGHT CHECKED GOOD.SDR CALA9700898Web · crackedINSPECTION FOUND A .5 INCH CRACK IN NOSE GEAR WELL HORIZONTAL WEB ON RT SIDE AT STA 290. THE WEB WAS REMOVED, A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700897Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1012, STRINGER 29L. THE CORROSION WAS REMOVED, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-30-3.SDR AALA970981Stringer · corrodedAFW - CORROSION ON STAND-OFF BRACKET FOR WIRING FS 720F AT STR 28R. REMOVED AND INSTALLED NEW PART, STAND-OFF BRACKET. TST: 65,866.18 HOURS. CYCLES: 43,812. (X)SDR AALA970980Bracket · corrodedAFW - CORROSION ON BLEED AIR SUPPORT BRACKET, STA 1040. INSTALLED NEW BRACKET PER MM 52-10-6. TST: 65,866.18 HOURS. CYCLES: 43,812. (X)SDR SCNA97172Battery Pack · dischargedL-1 AND R-1 DOOR EMERGENCY EXIT LIGHT (EXTERIOR) INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY, LIGHTS TESTED GOOD.SDR SCNA97173Wire · damagedTHE FORWARD LAVATORY SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. FOUND DAMAGED WIRES. REPAIRED WIRES, DETECTOR CHECKED NORMAL.SDR EISA97109Epr Indicator · failedON TAKEOFF, EPR NR 3 ROSE TO 2.9 WITH NORMAL N1. NR 1 AND NR 2 NORMAL INDICATION. REMOVED AND REPLACED INDICATOR. OPS CHECK GOOD. (M)SDR SCNA97171Battery Pack · dischargedRIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT (EXTERIOR) FLICKERS DIM. REMOVED AND REPLACED M665 BATTERY PACK, LIGHT TESTED GOOD.SDR SCNA97170Battery Pack · dischargedLEFT LOWER OVERWING EMERGENCY EXIT LIGHT (EXTERIOR) FLICKERS DIM. REMOVED AND REPLACED M955 BATTERY PACK, LIGHT TESTED GOOD.SDR SCNA97169Battery Pack · dischargedLEFT FORWARD OVERWING EMERGENCY EXIT LIGHT (EXTERIOR) FLICKERS DIM. REMOVED AND REPLACED M654 BATTERY PACK, LIGHT TESTED GOOD.SDR SCNA97168Battery Pack · dischargedRIGHT CENTER OVERWING EMERGENCY EXIT LIGHT (EXTERIOR) FLICKERS DIM. REMOVED AND REPLACED M956 BATTERY PACK, LIGHT TESTED GOOD.SDR CALA9700878Stringer · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN STRINGER 26L AT STA 720E TO 720F. THE CRACKED SECTION OF STRINGER WAS CUT OUT. A NEW STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.SDR TAOA059706Fuel Pump · failedFLT 6171 - BOS-LGA - NR 1 ENGINE FAILED EARLY IN THE TAKEOFF ROLL. ACCOMP APPROPRIATE CHECK LISTS AND RETURNED TO GATE. REPLACED FUEL PUMP PER MM 73-11-1 AND REPLACED FUEL CONTRO PER MM 73-11-57. ALL OPERATIONAL CHECK NORMAL. (M)SDR TAOA059705Switch · failedNORMAL START TAXI, WHEN POWER WAS APPLIED FOR TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. THE TAKEOFF WAS REJECTED AT APPROXIMATELY 20 KNOTS GROUND SPEED. FOUND UPPER TAEKOFF WARNING SWITCH BROKEN INTERNALLY. REPLACED PER MM CHAPTER 31-20-24. (M)SDR CALA9700877Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT CIRCUMFERENTIAL FRAME AT BS 480 BETWEEN STRINGER 25R AND 26R. A FRAME SPLICE WAS INSTALLED AND FLOOR SUPPORT SPLICE WERE INSTALLED IAW SRM 53-10-4 AND 51-30-2.SDR CALA9700876Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN LT MLG UPLOCK SUPPORT FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-10-1.SDR TAOA059704Battery Pack · dischargedFLT 6141 - BOS-LGA - FOUND L/S CHECK, ROW 3 EMERGENCY EXIT CEILING LAMP INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL IAW MM CHAPTER 33-50-0. (M)SDR TAOA059703Battery Pack · dischargedFLT 6141 - BOS-LGA - FOUND ON L/S CHECK, LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL IAW MM CHAPTER 33-50-0. (M)SDR CALA9700888Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING UPPER STRINGER AT CUTOUT NR 7618, WS 686.5. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW EA 5762-01050.SDR CALA9700887Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING UPPER STRINGER AT WS 629.0 CUTOUT NR 7616. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050.SDR CALA9700886Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING UPPER STRINGER WHERE IT ATTACHES TO RIB AT WS 656.50 TANK CUTOUT NR 7217. THE CRACKED SECTION WAS REMOVE, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9700871Support · corrodedINSPECTION FOUND FORWARD LAV FLOOR SUPPORT CORRODED AT STA 340, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-1.SDR CALA9700870Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 400, RBL 30. THE CORRODED AREA WAS CUT OUT, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700869Support · corrodedINSPECTION FOUND MAIN CABIN FLOOR PANEL SUPPORT CORRODED AT STA 420, RBL 10 TO 62. THE FLOOR SUPPORT WAS REMOVED, A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700885Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN UNDERSIDE LEADING EDGE OF RT OUTBOARD FOREFLAP. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-50.SDR CALA9700868Angle · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD ANGLE CORRODED AT BS 380, RBL 12. THE CORRODED AREA WAS REMOVED, A SUPPORT CHANNEL STRAP AND UPPER CHORD WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700652Motor · leakingAIRCRAFT LOST THE 'A' HYDRAULIC SYSTEM FLUID QUANTITY WHILE EN ROUTE FROM EWR TO TPA. THE FLUID LOSS WAS ACCOMPANIED BY NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LOSS. THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND THE RT OUTBOARD FLAP MOTSDR CALA9700884Flap · disbondedINSPECTION FOUND THE RT OUTBOARD MIDFLAP OUTBOARD TRAILING EDGE DISBONDED. THE DISBONDED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-6.SDR CALA9700864Frame · corrodedINSPECTION FOUND END OF FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 600, STRINGER 27R. REPAIRED IAW SRM 53-10-4.SDR CALA9700883Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 12 SPOILER OUTBOARD SPAR ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9700881Skin · crackedINSPECTION FOUND A 1.5 CRACK IN SKIN OF LT WING INBOARD MIDFLAP INBOARD SPINDLE CUTOUT NR 8443. THE CRACKED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700879Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT AFT STAIR TORQUE BOX WEB AT STA 1263 BELOW ACTUATOR FITTING. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-0 AND 51-30-2.SDR CALA9700874Ceiling Panel · crackedINSPECTION FOUND A .75 INCH CRACK AT FASTENER OF NLG WHEEL WELL CEILING PANEL FORWARD OF STA 273, LBL 14. A REPAIR WAS INSTALLED IAW SRM 51-40-2.SDR CALA9700872Panel · crackedINSPECTION FOUND THREE CRACKS AT FASTENERS OF NLG WHEEL WELL CEILING PANEL AT BS 286, BL 0. THE CRACKS WERE .5 TO 1 INCH LONG. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700865Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD CARGO COMPARTMENT AT STA 580 TO 600, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700863Skin · corrodedINSPECTION FOUND FORWARD CARGO SKIN CORRODED AT STA 560 TO 580, STRINGER 28R. THE CORROSION WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, PAGE 8.SDR CALA9700862Frame · corrodedINSPECTION FOUND BOTTOM OF FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 540, STRINGER 28L TO 26R. THE FRAME WAS REPAIRED IAW SRM 53-10-4.SDR CALA9700867Support · corrodedINSPECTION FOUND FORWARD LAV FLOOR SUPPORT CORRODED AT STA 320 TO 340, RBL 15. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9700866Support · corrodedINSPECTION FOUND FORWARD LAV FLOOR SUPPORT CORRODED AT STA 315 TO 340, RBL 35. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1.SDR TAOA059702Flush Motor · smokingFLT 6401 - LGA-DCA - FORWARD LAVATORY SMOKE DETECTOR ACTIVATED WHILE AIRCRAFT ON GROUND, DUE TO SMOKE FROM MALFUNCTIONING FLUSH MOTOR. REPLACED LAVATORY WASTE PUMP, OPERATIONAL CHECK NORMAL IAW MM CHAPTER 38-32-21. (M)SDR CALA9700889Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT INBOARD AND OUTBOARD ENDS OF NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9700882Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN LOWER LEADING EDGE OF RT INBOARD TRAILING EDGE FLAP SKIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW 57-40-4.SDR CALA9700875Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WHEEL WELL ANGLE BELOW LOAD CONTROL VALVE. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.SDR CALA9700873Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WHEEL WELL ANGLE FORWARD OF APU LOAD CONTROL VALVE DUCT AT KEEL BEAM. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9700880Wedge · disbondedINSPECTION FOUND LT WING TRAILING EDGE INBOARD AFT FLAP DISBONDED IN FIVE AREAS. LOWER SURFACE: 15-20 AND 54-69 FROM INBOARD EDGE. UPPER SURFACE: 73-80, 112-116, AND 142-146 FROM INBOARD EDGE. THE FLAP WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-2.SDR SCNA97143Chord · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON REINFORCEMENT CHORD NEAR AFT ENTRY STATION 1183, WL 208, LBL 5. REMOVED AND INSTALLED NEW CHORD IAW B727 SRM 51-40-01.SDR SCNA97100Sill Plate · corrodedDURING HEAVY MAINTENANCE, FOUND CORROSION ON LOWER SILL PLATE SKIN AT LEFT AFT GALLEY DOOR CUTOUT. REMOVED PLATE, FABRICATED AND INSTALLED NEW PLATE IN ACCORDANCE WITH B727 SRM 51-40-3 AND 51-30-2.SDR SCNA97096Panel · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND HEAVY CORROSION ON BOTH SIDES OF THE NUMBER 3 TRANSITION PANEL AT BS 1060 TO 1183. REMOVED PANEL, FABRICATED NEW PARTS, AND INSTALLED IN ACCORDANCE WITH B727 SRM 51-40-2.SDR SCNA97108Rib · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND ON THE RIB CHORD LOCATED AT STATION 760, LBL 70.5 AND RBL 70.5. REPAIRED CRACKS IAW B727 SERVICE BULLETIN 57-112, ENGINEERING ORDER 57-5127-1, AND DRAWING 65C21524, 65C33202, AND 65C37221.
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