Boeing 727-277
Service difficulty reports · 627
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 = '727277' 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 = '727277' 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 AU960170Disc · corroded(AUS) ENGINE 9TH STAGE HIGH PRESSURE COMPRESSOR DISC CONTAINED CORROSION PITTING IN THE BLADE SLOT PRESSURE FACES AND BLADE SLOTSIDES IN EXCESS OF LIMITS - FOUND DURING INSPECTION IAW PWA SB 6038 AND AD/JT8D/29 - ENGINE HAD BEEN FITTED TO A LOW UTILISATIONAIRCSDR AU960707Chord · corroded(AUS) RH WING LEADING EDGE RIB 'T' AT STN 269.298 CORRODED ON THE BOTTOM FLANGE - FURTHER INVESTIGATION FOUND A SECTION OF THE CHORD APPROXIMATELY 152.4MM (6IN) FROM THE WING FRONT SPAR AND APPROXIMATELY 50.8MM (2IN) IN LENGTH COMPLETELY CORRODED AWAYSDR AU960722Skin · corroded(AUS) AIRCRAFT LOWER SKIN CORRODED AND SPLIT IN THE AREA OF THE LH RAM AIR INTAKE BETWEEN STRINGERS 27LH AND 28LH AT FRAME AT STN 700 - AREA OF CORROSION APPROXIMATELY 50.8MM BY 76.2MM (2IN BY 3IN) - INVESTIGATION FOUND THAT THE EXFOLIATION CORROSION WAS CAUSSDR AU960109Seal · failed(AUS) NO1 ENGINE DRIVEN HYDRAULIC PUMP DRIVE PAD SEAL FAILED - SYSTEM 'A' HYDRAULIC LEVEL DROPPED TO 1.8 GALLONS - CREW SHUT OFF FLUID SUPPLY TO PUMP CAUSING PUMP TO RUN DRY AND SELF DESTRUCTSDR 96FDEA00013Switch · inoperativeAFTER A NORMAL T/O AND FLAP RETRACTION, WE LEVELED AT 5,000 FT AND LEADING EDGE DEVICE LIGHT CAME ON 2 DEGREE SHOWED NR 5 LED UNSAFE. WING ANTI-ICE ON CHECKLIST COMPLETION EXTINGUISHED LIGHT BUT IT CAME ON AGAIN SEVERAL TIMES NO STRUCTURAL LIMITS EXCEEDED. ASDR AU960767Beam · corroded(AUS) AIRCRAFT CONTAINED LEVEL 2 CORROSION ON LOWER CHORD OF CABIN FLOOR BEAM IN SECTION 46 - AREA OF CORROSION 508MM BY 25.4MM BY2.032MM (20IN BY 1IN BY 0.80IN)SDR 95FDEA01695Closing Mech · out of adjustFORWARD ENTRY DOOR LIGHT ILLUMINATED IN-FLIGHT, DEPRESSURIZED AND DESCENT TO 5000 FEET MSL. A/C WAS DEPRESSURIZED FOR REMAINDER OF FLIGHT (15 MINUTES) AT 5000 FEET. REMOVED DOOR LINER AND ADJUSTED UPPER AND LOWER LATCH TORQUE TUBE CONTROL RODS. OPS CHECK NOSDR EISA95289Connector · damagedGEAR HANDLE WOULD NOT RETRACT PAST 'OFF' POSITION ON DEPARTURE. STRAIGHTENED PIN NR 24 ON D4654P PLUG. OPS CHECKS GOOD IAW MM 32-09-121. (M)SDR EISA95288Skin · delaminationLEFT INBOARD FORE FLAP LEADING EDGE SKIN DELAMINATED. REPAIRED FLAP PER SRM 57-50-4 AND SRM 51-60-6. (M)SDR EISA95287Skin · delaminationRIGHT WING NR 12 SPOILER SKIN DELAMINATED. REPAIRED SPOILER PANEL PER SRM 57-50-6. (M)SDR EISA95286Frame · corrosionHEAVY CORROSION ON BOLT FRAME, FS 1166, RIGHT AT FLOOR LINE. REPAIRED FRAME PER SRM 51-40-3. (M)SDR EISA95285Floor Beam · corrosionHEAVY CORROSION ON FLOOR BEAM FS 1130, LBL 36, LOWER SIDE. REPAIRED BEAM PER DALFORT AVIATION XEA 1-53-688, REVISION 1. (M)SDR EISA95284Floor Beam · corrosionHEAVY CORROSION ON CHORD, FLOOR BEAM STATION 1176-1179, LBL 65 (UPPER SIDE). REPAIRED CHORD PER BOEING DRAWING 6563357. (M)SDR EISA95283Skin · crackedFOUND 2 CRACKS .5 INCH LONG, FS 700, LBL3, AT RBL 3 EXTERNAL SKIN. REPAIRED SKIN PER SRM 53-30-3. (M)SDR EISA95282Angle · crackedFOUND 5 CRACKS AT FASTENER HOLES INBOARD END OF LEFT WING LEADING EDGE STATION 130.7 LOWER WEB ANGLE. REPLACED ANGLE PER SRM 51-30-2. (M)SDR EISA95281Skin · crackedFUSELAGE SKIN HAS AN 1.25 INCH LONG CRACK AT TOP HINGE CUTOUT FOR FORWARD ENTRY DOOR. REPAIRED SKIN PER SERVICE BULLETIN 727-53-0198, FIG 3 AND 4. (M)SDR EISA95280Angle · crackedFOUND RIGHT WING LEADING EDGE UPPER REPAIR ANGLE CRACKED, AFT SIDE OF WING STATION 350. REPLACED ANGLE PER SRM 51-30-2. (M)SDR EISA95279Stiffener · crackedFOUND RIGHT WING LEADING EDGE RIB INBOARD STIFFENER LOWER END CRACKED AT WS 93. REPAIRED STIFFENER PER SRM 51-40-3. (M)SDR EISA95278Beam · corrosionFLOOR BEAM HAS HEAVY CORROSION FORWARD SIDE FS 1140, RBL 60. REPAIRED BEAM PER SRM 53-10-8, FIG 8. (M)SDR EISA95277Angle · corrosionLEFT WING LEADING EDGE ANGLE FORWARD OF FRONT SPAR HAS HEAVY CORROSION AT WING STATION 320. SPLICE ANGLE PER SRM 51-40-4. (M)SDR EISA95276Fitting · corrosionHEAVY CORROSION ON FITTING, FS 1183 END OF STRINGER 23L. REPLACED FITTING PER SRM 51-30-2. (M)SDR EISA95275Stringer · corrosionHEAVY CORROSION ON STRINGER 23L, FS 1166-1183. REPAIRED STRINGER SECTION PER SRM 53-10-3. (M)SDR EISA95274Rib · crackLEFT WING STATION 738 RIB TO STRINGER ATTACH HOLE CRACKED 1 INCH LONG AT FORWARD LOWER HOLE, REPAIRED. REPAIRED RIB PER SRM 57-10-5, FIG 2. (M)SDR EISA95273Doubler · corrosionHEAVY CORROSION AT CENTER WING BOX UPPER SKIN OUTBOARD OF FUEL CONNECTION, STATION 770, RT. REPLACED DOUBLER PER SRM 51-30-2. (M)SDR 95FDEA00445Door · missingACFT ARRIVED AT JFK WITH HYD SERVICE DOOR MISSING AND SLIGHT FAIRING DAMAGE. REPLACED MISSING HYD SERVICE DOOR AND MADE TEMPORARY REPAIR ON FAIRINGS.SDR 95FDEA00164Stiffener · corrodedMCM - LT WING FRONT SPAR STIFFENER CORRODED AND EXFOLIATED UNDER HYD LINE CLAMP STANDOFFS. LOCATED JUST OUTBD OF BOOST PUMP PRESSURE SWITCHES APPROX. FRONT SPAR STA 260. REMOVED HYD LINES LT WING F.O.M. INSTALLED SPAR STIFFENER REF EA 7-5710-3813 REV A. SDR 95FDEA00010Accessory Unit · false warningAFTER T/O FROM MEM AT GEAR RETRACTION, THE L/MAIN GEAR RED LIGHT WOULD NOT EXTINGUISH. CHECKLIST PROCEDURE ACCOMPLISHED. ALL GREEN ALL GEAR DOOR LIGHTS AND THE NOSE AND R/MAIN RED LIGHT EXTINGUISHED. THE L/MAIN RED LIGHT STILL WOULD NOT EXTINGUISH. FLT CON
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