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 CALA9800056Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 4 SLAT OUTBOARD HOOK ATTACHES. A DOUBLER WAS INSTALLED IAW SRM 57-30-4.SDR CALA9800055Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 3 SLAT INBOARD HOOK ATTACHES. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4.SDR CALA9800054Skin · corrodedINSPECTION FOUND LT WING INBOARD MIDFLAP SKIN CORRODED OUTBOARD OF INBOARD CARRIAGE MOUNT AREA. A SKIN REPAIR WAS INSTALLED IAW SRM 57-50-4.SDR CALA9800053Brackets · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9800052Brackets · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9800051Gusset · crackedINSPECTION FOUND A .5 INCH CRACK AT TOP CORNER AND A .5 INCH CRACK AT LOWER CORNER OF GUSSET ON RT SIDE OF VERTICAL STABILIZER AT STRINGER 9 BETWEEN RIB NR 6 AND NR 7. THE GUSSET PLATE WAS REMOVED, A NEW GUSSET PLATE WAS FABRICATED AND INSTALLED IAW SRM 55-30SDR CALA9800050Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 996, RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.SDR CALA9800049Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.SDR CALA9800048Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN END OF STRINGER 15L AT STA 720C. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5.SDR CALA9800047Doubler · crackedINSPECTION FOUND THREE CRACKS AT HI-LOKS ON DOUBLER UPPER SIDE OF CARGO DOOR FRAME CUTOUT BETWEEN FS 604 TO 608, STRINGER 10R. THE CRACKS WERE .25 TO 1 INCH LONG. THE FASTENERS AND DOUBLER WERE REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-SDR CALA9800045Doubler · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT HI-LOK ON DOUBLER UPPER SIDE OF CARGO DOOR CUTOUT FRAME AT FS 576, STRINGER 18R. THE FASTENERS AND DOUBLER WERE REMOVED, A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800044Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK AT SCREW HOLE IN INTERCOSTAL AT FS 720 TO 720A, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9800043Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT FS 400 TO 420, BBL 0. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9800042Frame · crackedINSPECTION FOUND A .125 INCH CRACK AT HI-LOK IN FRAME AT STA 312 BETWEEN STRINGER 6R AND 7R. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-40-5, AND 53-10-4.SDR CALA9800038Clip · crackedINSPECTION FOUND A 1 INCH CRACK IN CLIPS ATTACHED TO BULKHEAD ON LT SIDE IN AFT STAIR COMPARTMENT AT STA 1183, WL 270 AND WL 273. THE CLIPS WERE REMOVED, NEW CLIPS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9800037Clip · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FRAME TO STRINGER CLIP IN AFT STAIR COMPARTMENT ON RT SIDE AT STA 1283. THE STRINGER CLIP WAS REMOVED AND A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9800036Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT ON LT SIDE AT STA 1263. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-30-2.SDR CALA9800035Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LEFT CIRCUMFERENTIAL FRAME REINFORCEMENT PLATE AT STA 804, STRINGER 14L. A 1.5 INCH CRACK WAS ALSO FOUND IN RIGHT CIRCUMFERENTIAL FRAME REINFORCEMENT PLATE AT STA 804, STRINGER 14R. FRAME REINFORCEMENT ANGLE REPAIRS WERE SDR CALA9800034Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 740. THE CORRODED ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IN THE UPPER INTERCOSTAL IAW SRM 51-10-1.SDR CALA9800033Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT AIRSTAIR WAY RIGHT LOWER TORQUE BOX ANGLE AT STA 1173. A NEW ANGLE WAS INSTALLED IAW SRM 53-10-10.SDR CALA9800032Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT AIRSTAIR WAY RIGHT LOWER TORQUE BOX ATTACH ANGLE AT FS 1263. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9800031Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR INNER SKIN. THE CRACK WAS LOCATED 4 FROM FORWARD EDGE AND 10 BELOW UPPER TORQUE TUBE. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2.SDR CALA9800030Panel · crackedINSPECTION FOUND TWO .125 INCH CRACKS IN TOP CENTER PANEL OF NOSE WHEEL WELL AT FS 289, RBL 51. THE FASTENERS WERE REMOVED AND CRACKED AREAS WERE CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.SDR CALA9800029Panel · crackedINSPECTION FOUND THREE .125 INCH CRACKS IN TOP RIGHT PANEL OF NOSE WHEEL WELL AT FS 264, RBL 10. THREE .125 INCH CRACKS WERE ALSO FOUND IN TOP LEFT PANEL OF NOSE WHEEL WELL AT FS 264, LBL 10. FASTENERS WERE REMOVED AND THE CRACKED AREAS WERE CUT OUT. REPAIRSDR CALA9800028Panel · crackedINSPECTION FOUND A .125 INCH CRACK IN TOP RIGHT PANEL OF NOSE WHEEL WELL AT FS 269, RBL 10. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. THE CRACKED AREA WAS CUT OUT IAW EA 5362-01016. DOUBLER, STRAP, AND FILLER WERE FABRICATED AND INSTALLED IAW EA 5362-0101SDR CALA9800027Frame · puncturedINSPECTION FOUND A HOLE THROUGH TOP OF FRAME AT STA 1050 ABOVE STRINGER 27R. THE DAMAGED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2, AND 51-10-2.SDR CALA9800026Intercostal · corrodedINSPECTION FOUND CORROSION ALONG BOTTOM SIDE OF UPPER FLANGE OF INTERCOSTAL BETWEEN STA 1050 AND 1070 ABOVE S27R. THE L-ANGLE WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9800025Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 970, S27L. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-2.SDR CALA9800024Skin · corrodedINSPECTION FOUND CORROSION AND DISHED RIVETS IN LT FUSELAGE SKIN JUST FORWARD OF NR 2 ENGINE FORWARD COWL, STA 1352, S20L. THE FASTENERS WERE REMOVED IAW SRM 53-30-3. THE CORRODED SKIN WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAWSDR CALA9800023Support · crackedINSPECTION FOUND A .5 INCH CRACK AROUND NUT PLATE HOLES IN FLOOR SUPPORT BETWEEN STA 950A AND 950B, RBL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-20-14.SDR CALA9800022Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 380, S17L. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-6.SDR CALA9800021Skin · damagedINSPECTION FOUND LEADING EDGE OF FORWARD UPPER FUSELAGE SKIN PEELED UP AT RADOME, STA 178. THE DAMAGED SKIN PANEL WAS REMOVED, A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.SDR 98FDEA00032Anti-Ice Duct · blownON CLIMBOUT AT 3000, LWR AFT BODY OVERHEAT LIGHT ILLUM. RAN CHECK LIST AND AFTER RETARD NR 2 THROTTLE LIGHT WENT OUT. ENG ANTI-ICE WAS OPENED JUST PRIOR TO ILLUM OF LWR AFT BODY OVERHEAT LIGHT. DECLARED EMERGENCY AND RETURN TO MEM. FOUND NR 2 ENG COWL THERMSDR TAOA019806Battery Base · shortedFLT 6521 - OVERNIGHT L/S CHECK - L-2 DOOR EMERGENCY EXIT DOOR SIGN INOPERABLE. REPLACED BATTERY PACK BASE, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50.SDR AALA980098Switch · defectiveTUL - DURING MAINTENANCE, CABIN EMERGENCY EXIT LIGHTS WOULD NOT OPERATE AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERGENCY EXIT LIGHT SWITCH AT AFT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR AALA980084Shear Tie · corrodedTUL - FOUND CORROSION ON SHEAR TIE STRINGER 26R AT STATION 720. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1. (M)SDR AALA980059Stringer · corrodedTUL - CORROSION ON STR 27R STA 1030 - STA 1040 AND SKIN UNDER STRINGER. REMOVED CORROSION, REPAIRED PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980044Light · inoperativeDFW - DURING OVERNIGHT CHECK, DISCOVERED COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR AALA980043Wire · defectiveDFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR LIGHTS IN FORWARD PASSENGER CABIN NOT OPERATING PROPERLY. REPLACED JUMPER WIRE AT FORWARD PASSENGER CABIN FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR AALA980082Floor Beam · corrodedTUL - APPROXIMATELY ONE-HALF DIAMETER OF DEEP CORROSION ON TOP OF FLOOR BEAM STA 1130 RBL 2411. REPAIRED AFFECTED AREA WITH STRAP DOUBLER PER ESO 11697 DATED 12-12-97. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980066Skin · corrodedTUL - AREA OF BULGED AND DISTORTED SKIN UPPER FIXED LEADING EDGE JUST ABOVE INBOARD END OF FUELING PANEL, POSSIBLE CORROSION. REMOVED DAMAGED AREA, INSTALLED FLUSH REPAIR PER SRM 57-30-4. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980056Stringer · corrodedTUL - CORROSION AT STR 23L, STA 720E TO 720F. REPAIRED STRINGER PER SRM 53-10-3, FIG 1, SHEET 4, DETAIL NR 1. TST: 67,236 HOURS. CYCLES: 44,034. (X)SDR AALA980036Light · defectiveDFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR 98ZZZM406Light · inoperativeDURING PREFLIGHT, THE EGRESS LIGHT WAS FOUND INOP, AT ROW 28 ABC. REPAIRED BY REPLACING EGRESS LIGHT HOLDER.SDR 98FDEA00009Anti-Ice Valve · leakingENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE GASKET ON TOP SIDE OF VALVE. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 ENGINE STRUT OVERHEAT SENSDR AALA980087Beam · crackedTUL - FOUND CRACK RIGHT SIDE 1183 BEAM FORWARD SIDE 24 INCHES OUTBOARD FROM VAULT DOOR FRAME STRINGER 13 AREA. INSTALLED SERVICEABLE BEAM PREVENT MOD AND REPAIR PER BOEING BWG 65C34406 (S/B 727-53-0192). (M)SDR AALA980086Web · corrodedTUL - RIGHT AFT LAV FLOOR WEB HAS SEVERAL AREAS OF CORROSION ON TOP SIDE. INSTALLED NEW FLOOR WEB PER SRM 51-10-1 PAGE 4. (M)SDR AALA980085Shear Tie · corrodedTUL - FOUND CORROSION AT SHEAR TIE STATION 680 BETWEEN STRINGER 26L AND STRINGER 27L. REPLACED SHEAR TIE PER SRM 51-10-1. (M)SDR AALA980083Floorbeam · corrodedTUL - FOUND STATION 328, 52LBL FLOORBEAM CORROSION. INSTALLED DOUBLER ON FLOORBEAM PER SRM 53-10-08 PAGE 49-53. (M)SDR AALA980081Shear Tie · crackedTUL - STA 720, ABOVE STR 18L, BELT FRAME SHEAR TIE IS CRACKED. REPAIRED PER SRM 51-40-3. TST: 67,236 HOURS. CYCLES: 44,034. (X)
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