Boeing 727-230
Service difficulty reports · 181
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 = '727230' 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 = '727230' 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 C8GA20090045Skin · delaminatedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING INBOARD AFT FLAP UPPER SURFACE HAS 2 SPOTS OF DELAMINATION WBL 80-90. REMOVED DAMAGED SKIN AND CORE DIM 7.5 INCH BY 9.5 INCH. FABRICATED NEW CORE FROM 5052-44-3/16. FABRICATED FILLER DIM 7.5 INCH BY 9SDR C8GA20090044Panel · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 11 SPOILER PANEL 2ND HINGE CUTOUT HAS 1 CRACK WS 460. STOP DRILLED CRACKS HFEC INSPECTED AND FABRICATED REPAIR DOUBLER. FABRICATED BACKING PLATE. INSTALLED DOUBLER REPAIR. NO OTHER DEFECTS NOTED. AIRCRAFSDR C8GA20090043Skin · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 11 SPOILER PANEL HINGE CUTOUT HAS 2 EA CRACKS WS. 470. STOP DRILLED CRACKS HFEC INSPECTED AND FABRICATED REPAIR DOUBLER FROM 7075 T6 .071 INCH DIM 6.5 INCH BY 5 INCH. FABRICATED BACKING PLATE FROM 7075 T6 .SDR C8GA20090042Web · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT TRAILING EDGE FALSE SPAR, AFT WEB IS CRACKED AT LOWER RIVET AT WBL 130. REMOVED SPOILER ACTUATOR FITTING AND DOUBLER TRIM WEB. FABRICATED NEW LOWER CHORD FROM P/N BAC 1514-14377075T6511 DIM 20.5 INCH LONG ASDR C8GA20090041Skin · debondedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT INBD AFT FLAP UPPER SURFACE APPROX 64 INCHES FROM OTBD END IS DIS-BONDED. DAMAGED AREA REMOVED DIM 9 INCH BY 4.5 INCH. FABRICATED FILLER DIM 9 INCH BY 4.5 INCH AND DOUBLER DIM 12 INCH BY 6 INCH FROM 2024 T3SDR C8GA20090040Skin · debondedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT INBD AFT FLAP APPROX 30 INCHES FROM THE INBD END UPPER SURFACE IS DIS-BONDED. DAMAGED AREA REMOVED DIM 6.0 INCHES BY 2.5 INCHES. FABRICATED FILLER DIM 6 INCH BY 2.5 INCH AND DOUBLER DIM 9.5 INCH BY 4 INCH SDR C8GA20090039Skin · debondedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT INBD AFT FLAP LOWER SURFACE OTBD END DIS-BONDED. DAMAGED AREA REMOVED DIM 3.5 INCH BY 2 INCH. FABRICATED DOUBLER FROM 2024 T3 .016 INCH HOT BONDED REPAIR. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SDR C8GA20090038Mount · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 6 K-FLAP UPPER MOUNT IS CRACKED AT THE OUTBOARD UPPER CORNER. REMOVED ASSY MOUNT, FABRICATED TWO WEB'S INBD AND OTBD. INSTALLED REPAIR PARTS IAW DWG NR 65-16275. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURSDR C8GA20090037Vent Line · chafedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RIGHT WING TANK VENT TUBE AT WS 686.50 IS CHAFED. FABRICATED DOUBLER FROM 2024-0 DIM 3.5 INCH BY 3 INCH. INSTALLED REPAIR IAW COTNEY DWG NR EDAG91-1. LEAK CHECK GOOD, NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETSDR C8GA20090036Vent Line · chafedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RIGHT WING TANK VENT TUBE AT WS. 629.00 IS CHAFED. FABRICATED DOUBLER FROM 2024-0 DIM 3.5 INCH BY 3 INCH. INSTALLED REPAIR IAW DWG NR EDAG91-1. LEAK CHECK GOOD, NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNEDSDR C8GA20090035Rib · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 3 SLAT HAS AN INTERNAL ATTACH FITTING CRACKED. THE SLAT ACTUATOR INBD AND OTBD RIBS WERE REMOVED AND REPLACED. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090034Hinge · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING DTA EVALUATION IT WAS NOTED THAT THE L1 DOOR LOWER HINGE REPAIR FASTENERS DID NOT COMPLY WITH SB 727-53A0198. FASTENERS WERE REMOVED, HOLES NDT AND OVER SIZED. INSTALLED NEW FASTENERS IAW 727-53A0198. NO OTHER DEFECTS WSDR C8GA20090032Vent Line · chafedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE LEFT WING TANK VENT TUBE AT WS. 656.50 IS CHAFED. FABRICATED DOUBLER FROM 2024-O .040 INCH DIM 4.5 INCH BY 3 INCH. INSTALLED REPAIR IAW COTNEY DWG NR EDAG91-1. LEAK CHECK GOOD, NO OTHER DEFECTS WERE NOTED. ASDR C8GA20090031Vent Line · chafedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE LEFT WING TANK VENT TUBE AT WS. 629.00 IS CHAFED. FABRICATED DOUBLER FROM 2024-O .040 INCH DIM 4.0 INCH BY 3 INCH. INSTALLED REPAIR IAW DWG NR EDAG91-1. LEAK CHECK GOOD, NO OTHER DEFECTS WERE NOTED. AIRCRAFTSDR C8GA20090030Vent Line · chafedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE LEFT WING TANK VENT TUBE AT WS. 601.50 IS CHAFED. FABRICATED DOUBLER FROM 2024-O .040 INCH DIM 4.5 INCH BY 3 INCH. INSTALLED REPAIR IAW COTNEY DWG NR EDAG91-1. LEAK CHECK GOOD NO OTHER DEFECTS WERE NOTED. AISDR C8GA20090029Structure · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE LT OUTBOARD AFT FLAP AT WBL. 485 IS DELAMINATED. REMOVED DAMAGED AREA DIM 5.5 INCHES BY 22 INCHES. FABRICATED REPAIR FILLER FROM 2024 T3 .016 INCH DIM 5.5 INCH BY 22 INCH AND DOUBLER FROM 2024SDR C8GA20090028Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE LT OUTBOARD AFT AT WBL 445 IS DELAMINATED. REMOVED DAMAGED AREA DIM 5.5 INCH BY 6.5 INCH. FABRICATED REPAIR FILLER AND DOUBLER FROM 2024 T3 .016 INCH AND HOT BONDED REPAIR. NO OTHER DEFECTS WSDR C8GA20090027Bulkhead · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WHEEL WELL BS 870 BULKHEAD WEB CRACKED AT LOCK FASTENER LOAD CONTROL VALVE CUTOUT RBL 10. REMOVED DAMAGE, FABRICATED FILLERS FROM 2024 T3 .063 INCH AT AFT UPPER DIM 1.425 INCH BY .5SDR C8GA20090026Skin · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS A GOUGE WAS NOTED ON THE LT SIDE OF THE FUSELAGE AT BS 1352 STR 17L. DAMAGED AREA WAS REMOVED 1 INCH BY 1 INCH FABRICATED FILLER FROM 2024 T3 .050 INCH AND DOUBLER FROM 2024 T3 .063 INCH DIM 9.5 INCH BY 3.5 INSDR C8GA20090025Skin · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE SKIN IN FRONT OF THE RIGHT RAM AIR INLET DOOR HAS EXFOLIATED CORROSION AT BS 720. DAMAGE WAS REMOVED DIM 2 INCH BY 1.75 INCH. FABRICATED 2 EA INTERNAL DOUBLERS FROM 2024 T3 .050 INCH DISDR C8GA20090024Floorbeam · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE FUSELAGE UPPER LOBE WING CENTER SECTION OVERWING FLOORBEAM IS CRACKED UNDER SEAT TRACK SECTION BS 760.9 RBL 24.75. CRACKED FLOORBEAM WAS REMOVED AND REPLACED WITH NEW CHORD FROM BS 760.9. SDR C8GA20090023Floorbeam · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE FUSELAGE UPPER LOBE WING CENTER SECTION OVERWING FLOORBEAM CRACKED UNDER SEAT TRACK SECTION BS 760.9 RBL 45.50. CRACKED FLOORBEAM WAS REMOVED AND REPLACED WITH NEW CHORD FROM BS 760.9. NOSDR C8GA20090022Floorbeam · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE FUSELAGE UPPER LOBE WING CENTER SECTION OVERWING FLOORBEAM CRACKED UNDER SEAT TRACK SECTION BS 760.9 LBL 24.75 CRACKED FLOORBEAM WAS REMOVED AND REPLACED WITH NEW CHORD FROM BS 740-850 IAW SDR C8GA20090021Floor Support · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION, IT WAS NOTED THAT THE FUSELAGE UPPER LOBE WING CENTER SECTION OVERWING FLOORBEAM CRACKED UNDER SEAT TRACK SECTION BS. 760.9 LBL. 45.50. CRACKED FLOORBEAM WAS REMOVED AND REPLACED WITH NEW CHORD FROM BS 740-850SDR C8GA20090020Tab · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LEFT ELEVATOR TAB TRAILING EDGE WAS DELAMINATED. DAMAGE WAS REMOVED, FABRICATED FILLER, DOUBLER AND BONDED REPAIR. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090019Tab · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT ELEVATOR TAB WAS DELAMINATED. DAMAGE WAS REMOVED, FABRICATED FILLER 3 INCH BY 3.5 INCH AND DOUBLER 4.5 INCH BY 5.5 INCH FROM .010 INCH 2024 T3 AND HOT BONDED REPAIR. NO OTHER DEFECTSDR C8GA20090018Structure · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING DTA EVALUATION IT WAS NOTED THAT EXISTING REPAIR AT BS 309 STR 26L IS NON-COMPLIANT WITH SRM. REMOVED DOUBLER REPAIR. FABRICATED NEW DOUBLER, TRIPLER, AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETSDR C8GA20090017Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE FLOORBEAM AT BS 277 BL 14L HAS CORROSION. CUT OUT DAMAGED AREA 13 INCH. FABRICATED REPAIR CHORD FROM BAC 1505-39042 7075 T65N DIM 13 INCH AND FILLER FROM 7075 T6 .050 INCH DIM 6.125 INCH BY 9.00 INCH. INSTALSDR C8GA20090016Frame · dentedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE FRAME WAS DENTED AT BS 680 ABOVE STR 23R. CUT OUT DAMAGED AREA 1.4 INCH BY 1.5 INCH. FABRICATED REPAIR FROM 7075-0 .063 INCH DIM 9.2 BY 3.3, HEAT TREATED TO T6 AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTSDR C8GA20090015Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT SHEAR TIE AT BS 1130 STR 30 HAS CORROSION. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGED SHEAR TIE WAS REMOVED AND FABRICATED NEW, HEAT TREATED TO T6. INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2,53-10-4. SDR C8GA20090014Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT SHEAR TIE AT BS 970 STR 28R TO 29R HAS CORROSION. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGED SHEAR TIE WAS REMOVED AND FABRICATED NEW. HEAT TREATED TO T6. INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2,53SDR C8GA20090013Shear Tie · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE BOTTOM OF FRAME AND SHEAR TIE AT STR 27L TO 27R HAS CORROSION BS 990. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGED SHEAR TIE WAS REMOVED AND FABRICATED NEW FROM 7075-0, .071 DIM 4 BY 4. HEAT TREATED SDR C8GA20090012Stringer · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT STR 29R HAS CORROSION AT BS 950E AND 950F. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGE WAS REMOVED AND 4 NEW REPAIR DOUBLER'S WERE FABRICATED AND 5 EXTERNAL DOUBLER'S. INSTALLED REPAIR PARTS. NO OTHER DSDR C8GA20090011Stringer · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT STR 27R HAS CORROSION AT BS 950A. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGE WAS REMOVED AND 2 NEW REPAIR ANGLES WERE FABRICATED FROM 7075-0 .063 INCH DIA 18 INCHES AND 1 3 3/8 INCH BY 3 7/8 INCH HEAT TRSDR C8GA20090010Stringer · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT STR 24R HAS CORROSION AT BS 740. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGED STRINGER WAS REMOVED FROM BS 740. FABRICATED NEW STRINGERS 8 INCHES IN LENGTH FROM BAC1498-132 7075 T6. FABRICATED NEW SPLICSDR C8GA20090009Stringer · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT STR 28L HAS CORROSION AT BS 540 AND 560. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGED STRINGER WAS REMOVED FROM BS 540-560. FABRICATED NEW STRINGERS 19 INCH IN LENGTH FROM BAC1498-143 7075 T62. FABRICATSDR C8GA20090008Stringer · corrodedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT STR 28L HAS CORROSION AT BS 520 AND 540. CORROSION WAS DETERMINED TO BE OUT OF LIMITS. DAMAGED STRINGER WAS REMOVED FROM BS 500-540. FABRICATED 2 NEW STRINGERS 19 INCHES IN LENGTH FROM BAC1498-143 7075 T62. FABRSDR C8GA20090007Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STR. 25L HAS CORROSION AT BS 580. CORROSION TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF STRINGER FROM BS 532-570, FABRICATED 2 NEW STRINGERS 19 INCH LONG FROM BAC1498-139, 7075-T6 .036 INSDR C8GA20090006Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE FORWARD CARGO LOWER LOBE STR 24L HAS BULGING AND CORROSION AT BS 560-582. REMOVED DAMAGED SECTION OF STRINGER FROM BS 563-606, FABRICATED 2 NEW STRINGERS 20 INCH LONG FROM BAC 1498-132, 70SDR C8GA20060002Door · not closedFLT 707 FROM PHX TO MCI, DURING CLIMB OUT AIRCRAFT WOULD NOT PRESSURIZE ABOVE 1.5 PSID. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND L1 DOOR NOT FULLY CLOSED. OPENED, CYCLED AND RESET DOOR, CONFIRMED L1 DOOR FULLY CLOSED AND LOSDR C8GA20050002Switch · malfunctionedFLT 738 FROM TOL TO MIO, AFTER TAKEOFF, THE LEADING EDGE FLAP AMBER LIGHT ILLUMINATED. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT INCIDENT. ADJUSTED THE NR 2 LEADING EDGE FLAP POSITION INDICATING SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR C8GA20040022Duct · looseFLT 705 CLEARED FOR TAKEOFF, A LOUD BANG WAS HEARD AT 1.4 EPR CHECK. TAXI CLEAR OF RUNWAY AND PERFORMED A SECOND CHECK ON THE DE-ICE PAD WITH SAME RESULTS. AIRCRAFT RETURNED TO RAMP AND UPON INSPECTION FOUND THE PRESSURE RELIEF VALVE ON PACK DISTRIBUTION DUCT SDR C8GA20040018Compressor · stalledFLT 707 FROM KPHX TO KMCI. AFTER SETTING MAX POWER, THE NR 2 ENGINE COMPRESSOR STALL TRIPPING THE PACKS OFF. ABORTED TAKEOFF AND RETURNED TO RAMP WITH NO FURTHER INCIDENT. INSPECTED NR 2 ENGINE FOR DAMAGE WITH NO DEFECTS NOTED IAW B727 MM 71-00 AND THE AIRCSDR 2004F00115Actuator · faultyAFTER TAKEOFF FROM ELP, DURING SLAT RETRACTION, NR 7 LEADING EDGE SLAT REMAINED EXTENDED WITH SLAT HANDLE AT 0 DEGREES. AMBER LEADING EDGE SLAT LIGHT WAS ILLUMINATED AND NR 7 INDICATED EXTENDED ON FLIGHT ENGINEERS LEADING EDGE PANEL. AIRCRAFT RETURNED TO ELPSDR C8GA20030019Clamp · failedAFTER TAKEOFF, NR 3 BLEED AIR TRIP LIGHT ON, FOLLOWED BY NR 3 ENGINE STRUT OVERHEAT LIGHT ON. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST, AIR TURN BACK AND AC LANDED WITHOUT INCIDENT. A/C WAS INSPECTED AND FOUND CLAMP ON NR 3 BLEED RIGHT SIDE AIR STAIRS AREA SDR 2003F00261Smoke Detector · defectiveON APPROACH INTO DAY, A MOMENTARY ACTIVATION OF MAIN CARGO FIRE SYSTEM, FOLLOWED IMMEDIATELY BY THE GREEN SYSTEM NORMAL LIGHT AND THEN YELLOW MAINTENANCE LIGHT. NO ACCOMPANING FIRE OR SMOKE NOTED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SMOKESDR 20000801SH010Shear Tie · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE AT STA 1150, STR 26R AND STR 29L. (X)SDR 20000801SH009Web · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON CARGO COMP FLOOR SUPPORT WEB FROM STA 950A - STA 950B, APPROXIMATELY STR 29L AND STR 29R. (X)SDR 20000329SH009Frame · corrodedDURING A C-CHECK, CORROSION WAS NOTED R-1 DOOR SILL MOUNT FRAME. (X)SDR 2000ZZZX248Duct · crackedKXAS/KAUS - FLT 311 - DURING TAKEOFF AND JUST AFTER ROTATION, NR 1 ENGINE FIRE WARNING CAME ON. NR 1 ENGINE THRUST LEVER WAS RETARDED TO FLIGHT IDLE. FIRE WARNING LIGHT WENT OUT. RETURNED TO KLAX WITHOUT FURTHER INCIDENT. FOUND 13TH STAGE DUCT WITH CRACK A
Back to Boeing 727-230