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 MZZA96109Sign Cover · brokenTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON FORWARD GALLEY AREA 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-103 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFSDR MZZA96108Sign Cover · brokenTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON R1 GALLEY SERVICE DOOR 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-106 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATSDR MZZA96107Sign Cover · brokenTNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON L2 SERVICE DOOR 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-105 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTOSDR MZZA96106Batteries · dischargedTNN - DURNIG 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AFT AIRSTAIR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. THE BATTERIES, P/N S106, WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF, HANGAR NON ROSDR CALA9601492Fire Warning · activatedTHE APU FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED, BUT CAME BACK ON. THE AIRCRAFT WAS DIVERTED TO PIT. THE LIGHT EXTINGUISHED AGAIN AFTER 10 MINUTES AND THE AIRCRAFT LANDED AT PIT WITHOUT FUSDR 97ZZZX1442Skin · corrodedDURING C-10 INSPECTION, LEVEL 2 CORROSION WAS NOTED ON AIRCRAFT SKIN AT BELT FRAME TIE AT STA 1172 AT S17L.SDR 97ZZZX1441Skin · corrodedDURING C-10 INSPECTION, LEVEL 2 CORROSION WAS NOTED ON AIRCRAFT SKIN BETWEEN STA 580 AND STA 720 AT S9R.SDR 97ZZZX1440Skin · corrodedDURING C-10 INSPECTION, LEVEL 2 CORROSION WAS NOTED ON AIRCRAFT SKIN BETWEEN STA 328 AND STA 344 AT S24R.SDR 97ZZZX1439Skin · corrodedDURING C-10 INSPECTION, LEVEL 2 CORROSION WAS NOTED ON AIRCRAFT SKIN BETWEEN STA 1130 AND STA 1150 BETWEEN S24R AND S25R.SDR 97ZZZX1438Tee Fitting · corrosionDURING C-10 INSPECTION, LEVEL 2 CORROSION WAS NOTED ON COCKPIT FLOOR SUPPORT BEAM TRIPLE TEE FITTING AT STA 265.SDR 97ZZZX1489Stringer Tie · corrosionDURING C-10 INSPECTION, CORROSION WAS NOTED ON STR TIE S19R AT FS 560.SDR 97ZZZX1437Frame · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON FRAME 219.8 AT S25L.SDR 97ZZZX1436Frame · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON FRAME FS 380 BETWEEN S6R AND S7R.SDR CALA9601389Skin · corrodedINSPECTION LT FUSELAGE SKIN BULGED AT STA 430. THE BULGED AREA WAS CUT OUT, A REPAIR PLATE WAS FABRICATED AND INSTALLED IAW SRM 53-30-2.SDR CALA9601421Rib · crackedINSPECTION FOUND NR 3 LEADING EDGE SLAT INBOARD END CLOSURE RIB CRACKED. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9601411Angle · corrodedINSPECTION FOUND CORROSION ON BOTTOM SIDE OF SPLICE ANGLE ABOVE STRINGER 27R AT STA 620 TO 630. THE OLD SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-10-2.SDR CALA9601410Skin · corrodedINSPECTION FOUND CORROSION ON SKIN UNDER STRINGER 28L BETWEEN STA 480 AND 500. THE CORRODED AREA WAS CUT OUT, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-30-2 AND 53-30-3.SDR MZZA96071Skin · corrosionGUM - DURING B-CHECK, FOUND CORROSION AT LOWER FUSELAGE SKIN BS 720B RAM AIR DOOR CUTOUT AREA. ITEM CLASSIFIED AS MAJOR REPAIR PER ENGINEERING. EC/RA 5330-02438 WAS INITIATED AND AUTHORIZED BY BOEING AND FAA DER. MAINTENANCE REPAIRED CORROSION AREA AS PER ESDR CALA9601442Floor Beam · corrodedINSPECTION FOUND LOWER HORIZONTAL LEG AT CABIN FLOORBEAM CORRODED FROM BL ZERO TO RBL 56, STA 1070 (AFT CARGO). A STRAP AND ANGLE REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9601313Duct · blownTHE NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF. THE EMERGENCY CHECKLIST WAS COMPLIED WITH AND THE WARNING LIGHT WENT OUT. THE AIRCRAFT WAS RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 13TH STAGE BLEED AIRSDR CALA9601438Rib · crackedINSPECTION FOUND LOWER FORWARD END OF NINE RIBS CRACKED AT INTERIOR OF NR 5 SLAT. THE CRACKS RANGED IN LENGTH FROM .1250 INCH TO 1 INCH. THE CRACKS WERE STOP DRILLED. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3.SDR CALA9601430Angle · crackedINSPECTION FOUND A HOLE BROKEN THROUGH CAP ANGLE OF CABIN FLOOR INTERCOSTAL BETWEEN STA 720 AND 720A, BL ZERO. THE CAP WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9601439Floor Beam · corrodedINSPECTION FOUND EXFOLIATION CORROSION ON FLOORBEAM AT STA 1130, LBL 18. THE CORROSION WAS REMOVED IAW SRM 51-10-6. REPAIR STRAPS WERE INSTALLED IAW SRM'S 51-10-2, 51-30, 51-40-5, AND 53-30-4.SDR CALA9601429Angle · corrodedINSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT LBL 35, STA 1034. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM'S 51-10-1, 51-30-2, 51-10-2, AND 51-40-5.SDR CALA9601428Angle · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN RBL 24 AND RBL 48 AT STA 1067. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM'S 51-10-1, 51-10-2, AND 51-30-2.SDR CALA9601427Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9601422Support · corrodedFLOOR SUPPORT AND INTERCOSTAL CORRODED AT STATION 1130 TO 1142 RBL 12 TO 16. REMOVED AND REPLACED FLOOR SUPPORT AND INTERCOSTAL IAW SRM 51-10-1 AND 51-10-2.SDR CALA9601420Stringer · crackedINSPECTION FOUND LT WING FUEL TANK STRINGER CRACKED AT STA 686.50. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050.SDR CALA9601417Angle · crackedINSPECTION FOUND A 2.25 INCH CRACK ON INBOARD FLANGE, JUST BELOW CABIN FLOORBOARD ATTACH ANGLE, OF LEFT FRAME AT BS 760.95. THE AREA WAS REPAIRED IAW BOEING DRAWING NR 65C36279-1.SDR CALA9601416Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1070, RBL 48 TO 57. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9601415Sub Floor · corrodedINSPECTION FOUND RT AFT LAV SUBFLOOR CORRODED AT STA 1134 TO 1140, RBL 19. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-2.SDR CALA9601308Floor Support · corrodedINSPECTION FOUND TRANSVERSE FLOOR SUPPORT CORRODED AT BS 1130, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-00.SDR CALA9601307Floor Support · corrodedINSPECTION FOUND TRANSVERSE FLOOR SUPPORT CORRODED AT BS 1070, RBL 20 TO RBL 32. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA9601437Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN LOWER AFT END OF INBOARD RIB OF RT OUTBOARD MID FLAP. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM'S 51-10-0, 51-10-2, AND 51-40-3.SDR CALA9601436Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN CHORD FITTING AT AFT UPPER INBOARD CORNER OF RT WING INBOARD MID FLAP REAR SPAR, WBL 124.2. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9601414Floorbeam · corrodedINSPECTION FOUND CORROSION AT NUTPLATE HOLES OF FLOORBEAM FLANGE AT STA 344, LBL 40. THE FLANGE WAS CUT OFF AND REPLACED IAW SRM 53-10-8.SDR CALA9601413Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE ON TOP AFT FLANGE OF STA 344 FLOORBEAM AT LBL 26. THE UPPER FLANGE WAS CUT OFF AND A REPLACEMENT FLANGE WAS INSTALLED IAW SRM 53-10-8.SDR CALA9601412Floorbeam · corrodedINSPECTION FOUND FORWARD FLANGE OF FLOORBEAM AT STA 344 AND LBL 21 CORRODED. THE FLANGE WAS REMOVED AND A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9601441Floor Beam · corrodedINSPECTION FOUND HORIZONTAL LEG OF AFT CARGO FLOORBEAM CORRODED AT STA 1130, RBL ZERO TO RBL 56. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE FLOORBEAM WAS REPAIRED IAW ECRA 5330-03333.SDR CALA9601440Floor Beam · corrodedINSPECTION FOUND THE AFT CARGO HORIZONTAL FLOORBEAM CORRODED AT STA 1130, RBL 30 TO RBL 53.SDR CALA9601435Rib · groovedINSPECTION FOUND OUTBOARD RIB OF NR 5 SLAT DEEPLY GROOVED. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9601434Angle · crackedINSPECTION FOUND A .50 INCH CRACK BETWEEN BOLTS OF UPPER RIB CAP ANGLE AT RT WING LEADING EDGE, STA 332. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 51-40-3, 51-8-0, AND 51-30-2.SDR CALA9601419Web · crackedINSPECTION FOUND LATERAL WEB CRACKED AT UPPER AND LOWER RADIUS INSIDE LEFT WING TIP, FORWARD OF FLUX VALVE COMPARTMENT. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-40-5.SDR CALA9601409Floorbeam · corrodedINSPECTION FOUND CORROSION ON CABIN FLOORBEAM AT STA 1068, RBL 48. THE FLOORBEAM WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-1.SDR CALA9601408Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO COMPARTMENT ABOVE STRINGER 26L FROM STA 480 TO 720D. THE CORROSION WAS REMOVED, REPLACEMENT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 51-40-5, 51-10-0, 51-10-2 AND SDR CALA9601407Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO COMPARTMENT ABOVE STRINGER 26R FROM STA 480-720D. THE FLOOR SUPPORT WAS REMOVED AND THE CORROSION WAS CLEANED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-SDR CALA9601406Floorbeam · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 1110, RBL 16 TO RBL 52. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9601405Stringer · corrodedINSPECTION FOUND STRINGER 26L IN FORWARD CARGO COMPARTMENT CORRODED AT STA 580. THE CORROSION WAS REMOVED AND THE STRINGER WAS REPAIRED IAW SRM 53-10-3.SDR CALA9601401Support · crackedINSPECTION FOUND CENTER SUPPORT FOR FLOORBOARD IN FORWARD CARGO COMPARTMENT CRACKED AT STA 580 TO 600. ALSO, THE WEB BELOW WAS CRACKED. THE CRACKS WERE STOP DRILLED, REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-40-3.SDR CALA9601400Angle · crackedINSPECTION FOUND A CRACK PROTRUDING PAST STOP DRILL IN ANGLE BELOW FLOOR SUPPORT AT STA 580 ABOVE STRINGER 28L. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
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