Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72K971627Skin · puncturedLT OB AILERON SKIN PUNCTURED. REPAIRED PER MM 57-51SDR DL72S971756Bracket · crackedBRACKETS CRACKED THE NR 5 L/E FLAP I/B ACTUATOR BRACKET HAS PREVIOUS REPAIR STOP DRILL CRACKED BEYOND STOP DRILL. THE O/B NR 5 ACTUATOR BRACKET IS ALSO CRACKED AT LOWER RADIUS. REMOVED ACTUATOR REMOVED O/B BRACKET. STOP DRILLED CRACK. CRACK LENGTH AND REPASDR DL72S971659Stringer · crackedRIGHT WING STRINGER TO RIB AT WS 656.50 STR 5 HAS CRACK FROM HOLE AND ALONG ANGLE. STARTED DRILLING REPAIR PER M/M 57-13-0. DISCONNECTED LINE AT WS 686.5 AND COMPLETED DRILLING. REINSTALLED VENT LINE AND WIRE CLAMPS.SDR DL72S971646Floorbeam · corrodedCABIN FLOORBEAM CORRODED STA 400 RBL 30 AT NUTCLIP HOLE. REPAIRED FLOORBEAM PER MM 53-20-11 PG 802.SDR DL72S971722Skin · crackedR-1 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER ERA362243-14 REV. A.SDR DL72S971671Floorbeam · corrodedCORROSION ON FLOORBEAM STA 344 FROM LBL 47 TO LBL 62. REPAIRED PER SRM 53-10-8 FIG 11.SDR DL72S971670Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM STA 344 FROM LBL 30 TO LBL 45. REPAIRED PER SRM 53010-8 FIG 19.SDR DL72S971669Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM STA 344 FROM LBL3 TO LBL27. REPAIRED PER SRM53-10-8 FIG 11.SDR DL72S971647Frame · corrodedCORROSION AT ACCESS PANEL 3448R SUPPORT FRAME. REMOVED CORROSION AS PER SRM 51-10-6 ON WEB, WITHIN LIMITS AS PER SRM 53-10-1 FIG 1. TREATED AND PAINTED AS PER PS 900-2-5. REMOVED CORROSION AS PER SRM 51-10-6 FROM T-ANGLE. CORROSION OUT OF LIMITS AS PER SRMSDR DL72L971611Lens · missingEMERGENCY TRACK LIGHTS 2 BULBS INOP AND LENSES MISSING AT ROW 36. REPLACED LIGHT SOCKETS AND LENSES.SDR DL72S971599Web · crackedA .75 INCH CRACK IN UPPER LT TORQUE BOX WEB AT UPPER CHORD STA 1223. INSTALLED DOUBLER PER M/M 53-11-0.SDR DL72S971595Battery Pack · dischargedEMERGENCY EXIT FLOOR STRIP LIGHTING INOP 1ST CLASS SECTION WOULD NOT ILLUMINATE WHEN SWITCH TURNED ON OR WITH ESSENTIAL PWR IN STBY. REPLACED BATTERY PACK AND BATTERY.SDR DL72L971615Relay · failedEMERGENCY EXIT LIGHTS ILLUM DURING CRUISE WITH SW IN ARMED POSITION. REPLACED CHARGER CONTROL RELAY R70.SDR DL72L971614Battery · dischargedEMERGENCY EXIT LIGHTS INOP. CHARGED BATTERY PACKS, TESTS OK.SDR DL72K971600Battery Pack · dischargedEMERGENCY LIGHT ON NR 2 CARGO DOOR INOP. REPLACED BATT PACK, CKS NML.SDR DL72S971609Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED JUST AFT OF THE STA 480 BUTT SPLICE APPROX BETWEEN STA 482 TO 487, SEVERAL INCHES O/B OF STR 28R. THE CORRODED SKIN IS LOCATED NEXT TO ONE OF TWO REPAIR DOUBLERS INSTALLED PER E/RA 259873-14. AFTER THE CORROSION WAS REMOVSDR DL72S971593Switch · failedAFTER GEAR EXTENSION, RT MLG LIGHT FAILED TO ILLUMINATE SAFE CONDITION. LIGHT PRESSED TO TEST OK. CREW RAN CHECKLIST AND CYCLED DIM AND TEST CIRCUIT BREAKER AND LIGHT BEGAN OPERATING NORMAL. UNEVENTFUL LANDING. REPLACED RT MLG DOWN AND LOCKED SWITCH, LIGHTSDR DL72S971622Skin · out of contourTHE FUSELAGE SKIN BETWEEN STRINGERS 9R AND 10R AT STA 550 ABOVE THE 7TH WINDOW AFT OF THE R1 DOOR WAS FOUND WITH AN UNEVEN CONTOUR EXTENDING OUTWARD UP TO .25 MAX FROM NORMAL CONTOUR, OVER A 10 BY 10 SIZE AREA. ACCOMPLISHED PERMANENT REPAIR PER ERA 361950-14.SDR DL72S971587Web · crackedVERTICAL WEB CRACKED ABOVE 'S' DUCT STA 1303 RT LWR CORNER. REPAIR PER M/M 53-11-0.SDR DL72L971579Light · inoperativeFOUND ON S/C 21D EMERGENCY TRACK LIGHT INOP AND LIGHT COVER MISSING. RELAMPED 21D, OPS CKS GOOD. INSTALLED LIGHT COVER, CKS OK.SDR DL72S971562Control Mech · malfunctionedON APPROACH OUTBD FLAPS WOULD NOT EXTEND. MADE MISSED APPROACH. FLAPS EXTENDED NORMAL ON SECOND ATTEMP. FLAP OPERATIONAL TEST NORMAL ON GROUND AND VISUALLY INSPECTED NO DEFECT FOUND.SDR DL72S971551Battery Pack · dischargedLT FWD AND AFT OVERWING EXIT UPPER EXIT LIGHTS INOP. REPLACED BATTERY PACK.SDR DL72S971535Relay · inoperativeON DESCENT FOR LANDING, EMERGENCY EXIT LIGHTS CAME ON AND STAYED ON. REPLACED R-70 CHARGER CONTROL RELAY. EXIT LIGHTS CHECKED NML.SDR CALA9701160Hyd Line · leakingTHE AIRCRAFT LOST B-SYSTEM HYDRAULIC QUANTITY WHILE IN FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAKAGE IN B-SYSTEM HYDRAULIC RETURN LINE AT CASE DRAIN TEE FITTING. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LISDR DL72L971678Skin · corrosionCORROSION WAS FOUND ON THE SKIN AND STRINGER BELOW THE C2 DOOR BETWEEN STA 950-F-970 AT STR 28R. THE CORROSION IN THE SKIN WAS TRIMMED OUT LEAVING A CUTOUT MEASURING 12.75 BY .75 STRINGER 28R WAS CUT AT STA 950F PLUS 10 AND STA 980 TO ORDER TO REMOVE CORROSIOSDR DL72S971509Stiffener · crackedWING L/E SPAR STIFFENER CRACKED NR 4 SLAT INBD TRACK INBD SIDE. REPLACED ANGLE PER M/M 57-20-21.SDR DL72S971508Angle · crackedFOUND ON B1 LETTER CK, .5 INCH CRACK FWD LOWER RT INBD VERTICAL KEEL BEAM ANGLE AT STA 870. REPAIRED PER SRM 53-10-9.SDR DL72S971496Bulb · failedEMER TRACK LIGHTS INOP AT ROW 21 AND ROW 25. REPLACED BULBS AND LENSES.SDR DL72S971481Battery Pack · dischargedEMER EXIT LIGHT AFT OF F/C BULKHEAD INOP. REPLACED BATT PACK.SDR 97FDEA00478Receiver · failed97-0142, NR 2 VOR FAILED IN FLIGHT (NO IDENT ON VHF NAV NR 2 ANY STATION). REMOVED AND REPLACED NR 2 VOR/ILS RECEIVER PER MAINTENANCE MANUAL 34-31-21, OPERATIONAL CHECKED GOOD.SDR DL72S971475Fire Loop · malfunctionedON CLIMBOUT, NR 3 ENGINE FIRE LIGHT ILLUMINATED. FIRE DETECTOR SWITCH IN A-MODE AS PER MCO. ALL OTHER ENGINE INDICATIONS NORMAL. SHUTDOWN ENGINE AS PER POM, FIRED BOTH BOTTLES AS PER POM AND FIRE LIGHT REMAINED ON UNTIL LANDING. TESTED FIRE LIGHT AFTER ISDR CALA9701186Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER AREA OF RT WING STRINGER, SECOND FROM AFT AT STA 686.5. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050 AND SRM 51-30-2.SDR CALA9701183Rib · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING FUEL TANK RIB AT WS 760. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 57-10-5.SDR DL72S971470Battery · dischargedEMERG LIGHT O/H ROW 13 DID NOT TEST. REPLACED BATTERY, CKS OK.SDR CALA9701257Frame · puncturedINSPECTION FOUND LOWER OUTBOARD EDGE OF FORWARD PIT DOOR FRAME PUNCTURED. THE LOWER FRAME WAS REMOVED AND A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9701187Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER AREA OF STRINGER, THIRD FROM AFT AT RT WING RIB STA 519. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050 AND BOEING SERVICE BULLETIN 57A159.SDR DL72S971464Controller · failedSMOKE IN THE CABIN WITH SMOKE DETECTORS GOING OFF. EMERGENCY RETURN INITIATED. SMOKE IN THE CABIN WITH TWO PACKS OPERATING. COMPRESSOR DISCHARGE TEMP LESS THAN 150 DEGREES, FLAPS UP AND LANDING GEAR DOWN. MAINTENANCE REPLACED 35 DEG CONTROLLER AND ACCOMPLISDR CALA9701258Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED AT STA 740. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A NEW STRINGER SECTION AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.SDR CALA9701179Bulkhead Web · crackedINSPECTION FOUND A 3 INCH CRACK IN BULKHEAD WEB PLATE AT STRINGER 7 AND RIB 8 OF LT SIDE OF VERTICAL STABILIZER INTERIOR. THE CRACKED PLATE WAS REMOVED, A REPLACEMENT PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9701176Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 FROM BL 0 TO RT WALL. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR DL72S971483Skin · crackedTHE LT AND RT SKINS OF THE VERTICAL STABILIZER WERE FOUND CRACKED AT THE FRONT SPAR JUST ABOVE THE FUSLEAGE CREASE. ON THE LT SIDE, A TOTAL OF FOUR FASTENER HOLES HAVE CRACKS EMANATING FROM THEM. TWO ARE IN THE TYPICAL LOCATION OF THE SRM 55-30-3, FIGURE 7 RSDR CALA9701185Hinge Fitting · crackedINSPECTION FOUND A .25 INCH CRACK IN HINGE FITTING FORWARD OF OUTBOARD AILERON, SECOND HINGE FROM OUTBOARD END. THE HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9701184Skin · corrodedINSPECTION FOUND LT WING OUTBOARD FOREFLAP LOWER TRAILING EDGE SKIN CORRODED AND FIBERGLASS WAS DEBONDED. THE CORRODED SKIN AND CORE WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.SDR CALA9701182Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING UPPER LEADING EDGE SKIN AT CUTOUT WHERE NR 4 SLAT OUTBOARD HOOK INSERTS. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4.SDR CALA9701181Skin · crackedINSPECTION FOUND LT WING LOWER LEADING EDGE SKIN BENT WITH A .25 INCH CRACK AT CUTOUT DIRECTLY OVER NR 2 SLAT ACTUATOR PISTON. THE CRACKED OUTER SKIN WAS CUT OUT, THE CRACKED INNER SKIN WAS STOP DRILLED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRSDR CALA9701175Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 25 TO 45. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701174Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 480, RBL 25. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701173Bulkhead · crackedINSPECTION FOUND A .25 AND .375 INCH CRACK AT FASTENER HOLES IN NLG WHEEL WELL RIGHT SIDEWALL BULKHEAD STA 286. THE CRACKS WERE STOP DRILLED, A DOUBLER AND STRAP REPAIR WERE FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-53-0145.SDR CALA9701172Pressure Panel · crackedINSPECTION FOUND A .25 AND .375 INCH CRACK IN NLG WHEEL WELL TOP LEFT PANEL AT STA 280. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-53-0145.SDR CALA9701171Panel · crackedINSPECTION FOUND THREE CRACKS AT FASTENER HOLES IN TOP CENTER PANEL AT STA 286, NLG WHEEL WELL. THE CRACKS MEASURED .25 TO .375 INCH LENGTH. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-53-0145.
Back to Boeing 727-232