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 DL72S952397Trunnion · corrosionLEFT NLG UPPER TRUNNION FITTING LOWER SURFACE IS CORRODED (CAP MATING SURFACE). REPAIR PER M/M 53-40-0.SDR DL72S952395Trunnion · corrosionNOSE LG TRUNNION LT FWD AND AFT BOLT HOLES CORRODED. REPAIR PER M/M 53-40-0.SDR DL72S952344Bearing · frozenAT HMV, FOUND ELEV TO STAB BEARING FROZEN, NR 1 ELEV TO STAB MOUNT WORN. REPAIRED PER MM 55-50-0.SDR DL72S952343S Duct · bentAT HMV FOUND S-DUCT LE RIM BENT AND WORN. REPAIRED PER SRM 54-10-3 FIG 13.SDR DL72L952364Eel Battery Pack · dischargedRIGHT OVERWING EMERGENCY EXIT SIGN LIGHTS INOP. REPLACED BATTERY, CHECKS GOOD.SDR DL72S952398Trunnion · corrosionNLG LT/RT TRUNNION BEARING FITTINGS CORRODED IN THE BORES AND ON THE FACES. REPAIR PER M/M 53-40-0.SDR DL72S952396Trunnion · corrosionNLG RT UPPER TRUNNION BEARING FITTING CORRODED IN LINE UP PINHOLE. REPAIR PER ERA 301860-14.SDR DL72S952394Trunnion · corrosionNLG RT UPPER TRUNNION BEARING FITTING IS PITTED ON THE I/D OF FITTING, FWD HOLE IN UPPER FITTING IS PITTED. REPAIR PER E.O. 4-57751-3.SDR DL72S952393Trunnion · corrosionNOSE L/G UPPER TRUNNION FITTING LOWER SURFACE IS CORRODED (CAP MATING SURFACE). REPAIR PER M/M 53-40-0.SDR DL72S952392Trunnion · corrodedRIGHT GEAR - FWD TRUNNION ATTACH FITTING IS CORRODED ON BOTH LEGS. REMOVED SEALANT, NO CORROSION FOUND. INSTALL SHIMS PER M/M 57-43-0.SDR DL72S952427Trunnion · corrosionTHE LEFT AND RIGHT NLG TRUNNION BEARING FITTINGS HAD CORROSION ON THE FACES AND THE BORES. CORROSION REMOVAL RESULTED IN THE LT BORE ID 2.608, RT BORE ID 2.5885, UPPER FITTING SPOT FACED THICKNESS IS 1.506, CAP SPOT FACED THICKNESS IS 1.460. ALL CORROSION RESDR DL72S952413Skin · corrodedCORROSION ON SKIN AFT OF STA 720 BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-30-3 FIG 1, FOUND AT HMV.SDR DL72S952298Skin · crackedNR 6 L/E FLAP HAD A PREVIOUS REPAIRED CRACK WHICH CRACKED FURTHER. REPAIRED PER SRM 57-50-3, FOUND AT HMV.SDR DL72S952297Skin · crackedNR 6 L/E FLAP HAD A CRACK AT I/B HINGE FITTING AFT END. REPAIRED PER SRM 57-50-03 PG 32.SDR DL72L952294Rib · crackedUPON INSPECTION, RIB NR 11 FOUND CRACKED IN LWR FWD CORNER. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952293Rib · crackedUPON INSPECTION, A CRACK WAS FOUND IN THE LOWER FWD CORNER OF NR 10 RIB. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952292Heat Shield · crackedUPON INSPECTION, A CRACK WAS FOUND IN HEAT SHIELD BETWEEN RIBS 11 AND 12, AND BETWEEN RIBS 12 AND 13. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72S952502Doubler · crackedDOUBLER CRACKED AT AFT CHORD ANGLE 19 INCHES FROM I/B END. REMOVED AND REPLACED DOUBLER PER MM 57-52-0, NR 3 MIDFLAP AT HMV, SHOP VISIT.SDR DL72S952266Le Skin · damagedFOUND DURING D-2 LETTER CHECK - NR 3 T/E FOREFLAP LEADING EDGE SKIN DAMAGED. REPAIRED PER SRM 57-50-4 FIG 1.SDR DL72S952265Skin · crackedFOUND DURING D-2 LETTER CHECK - 1 INCH CRACK AT SKIN WHERE NR 4 JACKSCREW FAIRING BUTTS. REPAIRED PER SRM 53-50-3 FIG 2.SDR DL72L952262Rib · crackedUPON INSPECTION BY MAINT. RIB NR 11 IN NR 7 L/E SLAT WAS FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S952250Spar · oversized holesOVERSIZED HOLES WERE FOUND IN THE REAR SPAR AND SKIN. THE SPAR WAS REPAIRED PER SRM 55-20-1 AND THE SKIN WAS REPAIRED PER SRM 55-20-3, FOR THE RIGHT ELEVATOR AT HMV.SDR CAL950418Hyd Pump · inoperativeFLT NR 0774 - IAH - THE 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO AND WAS ACCOMPANIED BY LOSS OF 'A' SYSTEM PRESSURE WHLE IN FLIGHT. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESDR DL72S952507Stringer · corrodedFWD B/B STR 28R CORRODED ON UPPER FLANGE, JUST FWD OF STA 540. REPAIRED PER SRM 53-10-3 PG 4C, FOUND AT HMV.SDR CAL950412Actuator · leakingFLT NR 0209 - IAH - THE 'A' HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP WHILE EN ROUTE TO IAH. THE FLUID LOSS WAS STABILIZED BY THE CREW AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 LEADING EDGE SLAT ACTUATOR LEAKING. THE SLAT ACTUATOR WSDR DL72S952216Eel Battery Pack · dischargedR-2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL.SDR DL72S952215Eel Battery · dischargedL-2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPERATION NORMAL.SDR DL72S952237Exchanger · failedON CLIMBOUT FL 2,900 CABIN WARNING HORN CAME ON, CABIN ALT ROSE 12,000 TO 13,000 FT. MADE EMEMERGENCY DESCENT, RETURNED TO ATL. FOUND RIGHT PACK HEAT EXCHANGER BURST AND LEAKING. REPLACED HEAT EXCHANGER OPERATION NORMAL.SDR DL72K952200Skin · crackedA 6 INCH BY .25 INCH CRACKS FROM RIVETS ON LT VERT SPAR SKIN, JUST FWD AND BELOW BOTTOM CORNER OF SADDLE PANEL 9501. ALSO, 2 INCH BY .25 INCH CRACKS ON RT SIDE SAME LOCATION AS ITEM 1 ABOVE, AT NR 2 INTAKE STRUCTURE. REPAIRED PER MM 54-30-0.SDR DL72S952596Channel · crackedDURING LETTER CHECK INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM CHANNEL AT FS 1263 WAS FOUND CRACKED. IN ACCORDANCE WITH BAC S/B 727-53-0129 REV 4, THE CHANNEL WAS REPLACED.SDR DL72S952172Angle · crackedOUTBD ATTACH CASTING CRACKED 1.75 INCH NR 3 SPOILER AT ACTUATOR. CRACK REPAIR TO BE ACCOMPLISHED WITHIN 30 DAYS PER SRM 57-50-6.SDR DL72S952171Angle · crackedDOUBLER CRACKED COVE SKIN ATTACH ANGLE NR 2 SLAT INBD STOP PAD, FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 57-54-0.SDR DL72S952170Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED NR 4 SLAT OUTBRD TRACK .25 INCH, FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.SDR DL72L952253Skin · corrodedFOUND ON CV 2 CHECK, REMOVED 7 INCH BY 8 INCH SECTION OF FUSELAGE SKIN TO FACILITATE MTC. REPAIRED AREA PER SRM 53-30-3, FIG 1.SDR DL72S952195Stringer · crackedDURING HMV, FOUND LT WING STRINGER 8 AT STA 546.5 CRACKED. REPAIRED PER M/M 57-13-0 PG 801.SDR DL72S952148Le Skin · wornDURING SHOP INSPECTION, NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO L/E AT 86 FROM THE I/B END. REPAIRED PER SRM 57-50-4 FIG 1.SDR DL72L952291Lip · damagedFORWARD COWLING LIP DAMAGED AT 6 O'CLOCK POSITION NR 2 ENG CUTOUT. FOUND DURING CV-2 CHECK. REPAIRED PER M/M 53-11-0 PG 801.SDR DL72S952169Le Skin · damageRT WING NR 4 FORE FLAP FLAP L/E DAMAGE DUE TO HITTING T/E BRACKETS IN UP POSITION. REPAIRED PER SRM 57-50-4 FIG 1.SDR DL72S952134Stringer · crackedAT HMV, RT WING STA 656.5, FOUND STR 9 CRACKED JUST OUTBOARD OF BOLT HOLE. REPAIRED PER MM 57-13-0 FIG 802.SDR DL72S952592Skin · corrodedDURING HMV INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN STA 570 AND STA 590 UNDER STRINGER 27L REQUIRING A 5 BY 9 CUTOUT. THE CUTOUT WAS REPAIRED IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3.SDR DL72S952506Inlet · crackedNR 2 ENGINE INLET AFT LWR EDGE, BENT AND CRACKING IN SEVERAL PLACES. REPAIRED PER SRM 54-10-3.SDR DL72S952482Skin · damagedAT HMV, FOUND NUMEROUS TEMP REPAIRS ON FWD B/B LWR SKIN STA 480 TO 680. INSTALLED AND FABRICATED NEW SKIN PANELS PER SRM 53-30-3.SDR DL72S952162Window · smokingCLIMBING THROUGH FL 320, HAD VISIBLE SMOKE AND FUMES COMING FROM CONDUIT BETWEEN R-2 AND R-3 COCKPIT WINDOWS ON F/O SIDE. SMOKE CLEARED WHEN WINDOW HEAT TURNED OFF. REPLACED R-2 WINDOW AND CONTROLLER.SDR DL72S952149Skin · damagedWIND BLEW BAG CART INTO A/C FWD OF LT WING. REMOVED FWD BAG BIN SIDEWALL PANELS AT STA 720A, FABRICATED AND PAINTED REPAIR DOUBLER AND STRINGER SPLICE INSTALLED. COMPLETED REPAIR PER SRM 53-30-3 AND 53-10-3.SDR DL72S952133Angle · crackedDOUBLER CRACKED FOR FLANGE UNDER ANTI ICE DUCT FOR NR 2 SLAT. FOUND DURING A-2 LTR CK. REPAIRED PER MM 57-54-0.SDR DL72S952132Rib · crackedONE-HALF INCH CRACK NR 2 SLAT NOSE RIB ANGLE O/B OF ACTUATOR ATTACH. REPAIRED PER MM 57-54-0. FOUND AT A-2 LETTER CHECK.SDR DL72L952275Stringer · corrodedFOUND ON CV2 CHECK, CORROSION INSIDE OF STR 28L AND OUTBD SIDE AFT OF STA 1010. REPAIRED PER ERA 301845-14.SDR DL72L952219Stringer · corrodedFOUND ON CV2 CHECK, CORROSION ON STR 27L BETWEEN STA 580 AND 600. REPAIRED PER SRM 53-10-3 FIG 1, IDENTIFIED AS PERMANENT REPAIR PER PS 900-5-1 NR 4.SDR MZZA95033Hyd Pump · failedGUM - FLT 965 - AIRCRAFT LOST 'A' SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM OSAKA, JAPAN TO SAIPAN, CNMI. FLIGHT WAS DIVERTED TO GUAM. MAINTENANCE FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP FAILED. MECHANIC REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULICSDR DL72S952542Frame · corrodedAT HMV FOUND FORWARD LOWER FLANGE OF FRAME 1070 CORRODED LOC BETWEEN STR 30 AND 29R. INSTALLED NEW CLIP PER MM 53-11-0.
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