Boeing 727-51C
Service difficulty reports · 433
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 = '72751C' 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 = '72751C' 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 UPS96220498Angle · crackedINSPECTION TYPE: C. LT WING FRONT SPAR VERTICLE STIFFENER/RIB ATTACH ANGLE CRACKED AT NR 3 SLAT I/B TRACK I/B ROLLER MOUNTING RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW DWG 65-16200 AND SRM 57-10-2 AND 51-30-2.SDR UPS96220496Angle · crackedINSPECTION TYPE: C. LT WING FRONT SPAR VERTICAL STIFFENER/RIB ATTACH ANGLE IS CRACKED AT NR 3 SLAT O/B TRACK I/B ROLLER MOUNT RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW SRM 51-10-1 AND 51-30-2.SDR UPS96220495Angle · crackedINSPECTION TYPE: C. LT WING FRONT SPAR VERTICAL STIFFENER L/E RIB ATTACH ANGLE CRACKED AT NR 3 SLAT O/B TRACK O/B ROLLER MOUNT RIB. REMOVED VERTICAL STIFFENER ON NR 3 SLAT TRACK ATTACH ANGLE. REPLACED PER SRM 51-10-1, 51-30-2.SDR UPS96220494Stiffeners · crackedINSPECTION TYPE: C. LEFT WING AFT SPAR HOLES WORN IN VERTICLE STIFFENERS AT NR 2 SPOILER ACTUATOR FITTING LOWER ATTACH BOLTS. REMOVED AND REPLACED STIFFENERS IAW SRM 57-10-2 51-10-1, AND 51-30-2.SDR UPS96220490Torq Box Web · crackedINSPECTION TYPE: C. LOWER TORQUE BOX INBD WEB (RT) BS 1256 IS CRACKED AT THE LOWER LIGHTENING HOLE APPROXIMATELY .2 INCH LONG. REMOVED DAMAGE PER SRM 51-40-02, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-02 AND 51-30-02.SDR UPS96206052Batteries · dischargedMAINTENANCE REPORTED EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE. CHANGED BATTERIES IN BOTH UNITS, CHECK SATISFACTORY WITH REF TO MM 33-50-01.SDR 96ZZZM819Saddle Duct · rupturedFIRE WARNING SOUNDED ON NR 1 ENGINE AFTER TAKEOFF. DISCHARGED LEFT FIRE BOTTLE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED 13TH STAGE SADDLE DUCT ON NR 1 ENGINE. REPLACED LEFT FIRE BOTTLE.SDR 96ZZZX1649Pulley · bindingDURING DESCENT INTO INDY, THE NR 1 ENGINE THROTTLE HUNG AT APPROXIMATELY ONE-THIRD FORWARD TRAVEL AND WOULD NOT MOVE TO IDLE STOP. DURING APPROACH, THROTTLE CAME LOOSE AND WENT TO IDLE STOP. INSPECTED NR 1 ENGINE CONTROL RODS AT FUEL CONTROL, NO DEFECTS. INSDR UPS205609Seal · looseCREW REPORTED, LOUD FLAPPING SOUND HEARD AT 15,000 FT MSL 280 KTS AT TOP OF CAPT'S WINDSHIELD. REQUESTED PRIORITY LANDING, DECLARED EMERGENCY AND LANDED. AFTER SLOWING ASAP, FLAPPING SOUND WAS TOP OUTSIDE SEAL ON NEW WINDOW INSTALLED ON 2/20 IN SDF, DEFERREDSDR 96ZZZM250Switch · failedAFTER TAKEOFF DURING CLIMB, AS THE FLAPS WERE RETRACTED THE NR 4 LEADING EDGE FLAP INTRANSIT LIGHTS REMAINED ILLUMINATED. EXECUTED AIR TURN BACK TO IND. AIRCRAFT WAS LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP POSITION SWITCH PESDR 96ZZZM21Switch Wire · brokenDURING LANDING AT MKE, GEAR EXTENSION FAILED TO GET A DOWN INDICATION ON THE NOSE GEAR. CYCLED GEAR ONCE WITH SAME RESULTS. COMPLIED WITH GEAR MANUAL EXTENSION. MADE FLYBY AND MAINTENANCE VERIFIED GEAR APPEARED DOWN. AIRCRAFT WAS LANDED WITHOUT INCIDENT. SDR 96ZZZM24Valve · leakingON APPROACH INTO SAN, AS THE LANDING GEAR WAS EXTENDED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LEFT HYDRAULIC FLOW REGULATOR VALVE. INSPECTED A-SYSTEM HYDRAULIC PUMPS AND FILTERS. SERVICED HYDRAULIC SYSTSDR 95ZZZM689Bracket · brokenAS FLAPS WERE LOWERED TO 2 DEGREES FOR LANDING AT PHX ONLY INBOARD FLAPS EXTENDED, OUTBOARD FLAPS STAYED AT 0 DEGREES. ACCOMPLISHED SPLIT FLAPS CHECKLIST, HOWEVER, OUTBOARD FLAPS REMAINED AT 0 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT OUTBOARD FLSDR 95ZZZM663Switch · inopON GEAR RETRACTION ALL THREE GEAR UNSAFE LIGHTS REMAINED ON. GEAR DOOR LIGHTS OUT. REPLACED HORN AND WARNING CUT OUT SWITCH ON NR 3 ENGINE THROTTLE PER MM 31-26-13 AND 32-61-01. GEAR INDICATIONS AND HORN OPS CHECK NORMAL. (M)SDR 95ZZZX5916Ind Lamp · failedPHX - ON APPROACH, THE NOSE GEAR GREEN DOWN AND LOCKED INDICATOR FAILED TO ILLUMINATE ON GEAR EXTENSION. TOWER VISUALLY VERIFIED GEAR DOWN. ON GO-AROUND, FLIGHT CREW RE-LAMPED INDICATOR AT WHICH TIME IT ILLUMINATED. CYCLED GEAR, INDICATIONS NORMAL. AIRCRAFSDR UPS204350Bullnose · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP BULLNOSE CRACKED AT OUTBOARD LUG ATTACH POINT, INBOARD FASTENERS HOLES. REMOVED CRACKED BULLNOSE AND INSTALLED NEW BULLNOSE PER SRM 51-30-2, 51-30-8, M.M. 27-81-00.SDR UPS204340Te Wedge · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE HAS ONE DELAMINATION ON UPPER SURFACE 23 INCHES FROM INBOARD END. CUT OUT DAMAGE AREA, APPLIED FIBERGLASS, AND COMPLETED REPAIRS PER SRM 51-40-6, MM 51-20-151.SDR UPS204346Stringer · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND 20 PERCENT MATERIAL LOSS AT BS 360, 3 INCHES TO THE RIGHT ON STR 1 MARKED BY NDI. REPAIRED PER E.O. B727-5310-1371E, SRM'S 51-10-2, 51-30-8, 51-20-4, AND 51-30-2.SDR UPS204345Bonding Jumper · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP OUTBOARD BONDING JUMPER UPPER ATTACH POINT IS PITTED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-50-1, CUT OUT DAMAGE AND REPAIRED PER SRM 57-50-3.SDR UPS204344Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK INDICATION NOTED LT WINDSHIELD, UPPER SILL, LOWER AFT RIVET APPROX 8 O'CLOCK POSITION. CUT OUT DAMAGE AND REPAIRED PER SRM 53-30-3.SDR UPS204343Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 HINGE BEARING BLOCK ON LT WING, OUTBOARD AILERON TO BE WORN AND HAVE EXCESSIVE PLAY, BACK AND FORTH, SIDE TO SIDE. (NOTE UPON REMOVAL OF BEARING BLOCK FOUND FITTING CORRODED). REMOVED AND INSTALLED NEW FITTING. WSDR UPS204342Lower Chord · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBOARD MID-FLAP, INBOARD AFT FLAP ACTUATING CUT-OUT LOWER CHORD IS CRACKED. REMOVED AND INSTALLED NEW FABRICATED PARTS. WORK DONE I/A/W SRM 51-30-2, 51-40-4.SDR UPS204341Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND LEADING EDGE INBOARD AFT FLAP, INBOARD CENTER TRACK CUT-OUT IS CRACKED. CONTAINED CRACK BY STOP DRILLING AND VERIFIED BY NDI. FABRICATED REPAIR PARTS AND INSTALLED. WORK DONE I/A/W SRM 57-50-4, 51-30-2.SDR UPS204339Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 1 SPOILER HAS 2 AREAS OF DELAMINATION ON LOWER SURFACE AT THE INBOARD FORWARD CORNER AND ON THE OUTBOARD EDGE OF THE CENTER FITTING. REMOVED DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER SRM 57-50-1, SDR UPS204338Hat Channel · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON PANEL SUPPORT AT FORWARD LAV STA 344, RBL 18, WL 208-UNDERSIDE. REMOVED AND INSTALLED NEW FABRICATED HAT CHANNEL. WORK DONE I/A/W SRM'S 53-10-1, 51-30-2.SDR UPS203834Eel Battery · dischargedWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT WILL NOT ILLUMINATE WHEN TURNED ON. REPLACED BATTERIES IN BOTH EMERGENCY EXIT LIGHTS. OPS CHECK GOOD.SDR UPS203664Floorbeam · crackWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON FLOORBEAM ATTACH FLANGE NEAR BS 940. REPAIRED IAW B727-5310-5596.SDR 95ZZZX3384Fuel Control · failedLAX - NR 3 ENGINE WOULD NOT RESPOND TO THROTTLE ON APPROACH INTO LAX. MINIMUM FUEL FLOW 2500 POUNDS/HOUR WAS ALL IT WOULD PRODUCE, AT IDLE IT SPOOLED DOWN. IN-FLIGHT, ENGINE SHUT-DOWN PERFORMED; RYAN CHECKLIST AND PROCEDURES COMPLIED WITH. REMOVED AND REPLASDR UPS203660Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT 70.5 RIB CHORD HAS CRACK. REPAIRED IAW B727-5710-7142.SDR UPS203659Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND LT 70.5 RIB CHORD HAS CRACK. REPAIRED IAW B727-5710-7142-A.SDR UPS203645Wedge · disbondedWHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W O/B MID FLAP T/E WEDGE UPPER SURFACE DISBONDED. REPAIRED IAW SRM 57-40-6, 51-40-6.SDR UPS203644Frame · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FRAME ON STA 760, LBL 72, WL 205. REPAIRED IAW B727-5310-7117-A.SDR UPS203643Angle · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SUPPORT ANGLE AT B.S. 920, LBL 65, WL 189 AROUND LOWER FASTENERS. REPAIRED IAW SRM 51-10-2, 51-30-5, 51-30-2, 51-20-1, M/M 51-20-31.SDR UPS203642Angle · brokenWHILE IN C-CHECK MAINTENANCE, FOUND BROKEN ANGLE SUPPORT BRACKET AT WING BASE LINE STA 120, BEHIND THE NR 8 SPOILER ACTUATOR FITTING. REPAIRED IAW SRM 51-20-1, 51-30-2.SDR UPS203641Stiffener · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKED STIFFENER R/W L/E NR 6 SLAT I/B TRACK I/B SIDE LOWER END SLAT STA 135.5. REPAIRED IAW SRM 51-30-2, 51-10-2, M/M 28-11-21, 36-00-01, OHM 20-50-01.SDR UPS203640Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DISBONDED R/W I/B MID FLAP T/E WEDGE UPPER SURFACE AND WATER IN HONEY COMB. REPAIRED IAW SRM 51-40-6.SDR UPS203639Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER RUDDER TAB ON LOWER RT SIDE. REPAIRED IAW SRM 51-40-9.SDR UPS203638Floor Beam · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION UNDER UPPER FLOOR BEAM FLANGE, FORWARD SIDE STA 344, RBL 2, WL 208. REPAIRED IAW SRM 51-20-1, 51-10-1, 53-10-8, 51-30-2.SDR UPS203637Strap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRAP B.S. 351, RBL 30, WL 172. REPAIRED IAW SRM 51-40-4.SDR UPS203636Windshield Sill · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL RT SIDE AT B.S. 269. REPAIRED IAW SRM 53-30-3, 51-30-2.SDR UPS203635Windshield Sill · crackedWHILE IN C-CHECK MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL LT SIDE AT B.S. 267. REPAIRED IAW SRM 727-53-1620.SDR UPS203634Box Fairing · crackedWHILE IN C-CHECK MAINTENANCE FOUND CRACK EXTRUDING PAST STOP DRILL IN NOSE WHEELWELL SIDE BOX FAIRING. B.S. 277, RBL 23.5, WL 168. REPAIRED IAW SRM 51-10-2, 51-30-2, 51-21-1.SDR UPS203633Skin · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN SKIN AT BLOWOUT DOOR CUTOUT, B.S. 1333, LBL 48, WL 217. REPAIRED IAW SRM 51-10-2, 53-30-3, 51-30-2, 51-20-4, 51-10-1, 51-10-2, M/M 51-20-151.SDR UPS203632Web · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON B.S. 351 WEB AT RBL 217, WL 172. REPAIRED IAW SRM 51-40-2.SDR 95ZZZM187Connector · corrodedTHE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NOSE GEAR POSITION SWITCH CONNECTOR, OPS CHECKED GOOD. (M)SDR UPS203082Chord · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE VERTICAL FLANGE OF THE LOWER CHORD AT STATION 870, WL 160, LBL 27 AND RBL 25. MAINTENANCE REMOVED THE CORRODED CHORD, FABRICATED NEW CHORD AND INSTALLED IAW UPS EO 727-5710-6912A.SDR UPS203081Fitting · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE LEFT HAND TERMINAL FITTING AT STATION 870. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW UPS EO 727-5310-6913.SDR UPS203080Spar Chord · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE CENTER WING TANK UPPER SPAR CHORD AT STATION 870 AND LBL 37 TO 40. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-10-7, 51-30-2 AND 51-10-2.SDR UPS203079Rib Chord · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE RIB CHORD ON THE RIGHT HAND SIDE AT 12 AND 6 O'CLOCK POSITION AT STATION 759, BL 70.5. MAINTENANCE REPAIRED THE CRACKS IAW UPS EO 727-5710-1271G.SDR UPS203078Rib Chord · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIB UPPER CHORD AT BL 70.5. MAINTENANCE REPAIRED AND MODIFIED THE CHORD IAW UPS EO 727-5710-1271G.
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