Boeing 727-277
Service difficulty reports · 627
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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 06FDEA03793Structure · misinstalledMISDRILLED HOLE ON REINFORCEMENT CHORD BS 1176 RBL 23 WL 208. REMOVED AND REPLACED BS 1176 REINFORCEMENT CHORD FROM LBL 65 TO RBL 65, WL 208 PER SRM 51-30-2, 53-10-1.SDR 06FDEA03784Floorbeam · corrodedFOUND CORROSION ON BS 1110 FLOORBEAM LOWER FLANGE AT NUT PLATE HOLE LBL 40 WL 200. REPAIRED BS 1110 FLOORBEAM AT LBL 40, WL 200 PER SRM 53-10-8 FIG 8.SDR 06FDEA03783Skin · delaminatedAFT AIR STAIRS, EXTERIOR SKIN AFT RT CORNER BENT AND DELAMINATING. REPAIRED EXTERIOR SKIN AT RT CORNER OF AFT AIRSTAIR PER SRM 51-40-2.SDR 06FDEA03745Stringer Clip · crackedFOUND CRACKED STR CLIP AT BS 720B STR 16R. REMOVED & REPLACED CRACKED STR CLIP AT BS 720B STR 16R IAW SRM 51-30-2.SDR 06FDEA03744Door Frame · crackedFOUND CRACK IN NR 3 DOOR FWD FRAME ABOVE LOWER CROSS BEAM IN THE RADIUS. REPLACED DOOR NR 3 PER MM 52-35-051-4.SDR 06FDEA03743Stringer Clip · crackedFOUND CRACKED STR CLIP AT BS 420 STR 3R. REMOVED & REPLACED CRACKED STR CLIP AT BS 420 STR 3R PER SRM 51-30-2.SDR 06FDEA03742Stringer Clip · bentFOUND BENT STR CLIP AT BS 680 STR 2L. REMOVED & REPLACED BENT STR CLIP AT BS 680 STR 2L IAW SRM 51-30-2.SDR 06FDEA03741Stringer Clip · crackedFOUND CRACKED STR CLIP AT BS 680 STR 9R. REMOVED & REPLACED STR CLIP AT BS 680 STR 9RT IAW SRM 51-30-2.SDR 06FDEA03740Stringer Clip · crackedFOUND CRACKED STR CLIP AT BS 680 STR 9R. REMOVED & REPLACED CRACKED STR CLIP AT BS 680 STR 9 RT IAW SRM 51-30-2.SDR 06FDEA03718Stringer Clip · crackedFOUND STRINGER CLIP CRACKED STA 783.95 STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 06FDEA03717Stringer Clip · crackedFOUND STRINGER CLIP CRACKED STA 848.95 STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 06FDEA03716Stringer Clip · crackedSTRINGER CLIP CRACKED STA 804.5 STR 5L . REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 06FDEA03715Stringer Clip · crackedFOUND STRINGER CLIP CRACKED STA 783.95 STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2, 51-30-5.SDR 06FDEA03719Link · corrodedEXPANSION LINK, BS 740-760, BL 0, CORRODED AROUND FWD ATTACH BOLT. REMOVED AND REPLACED EXPANSION LINK PER SRM 51-30-2.SDR 06FDEA03685Floorbeam · corrodedFOUND LONGITUDINAL FLOORBEAM CORRODED AT NUTPLATE HOLE, RBL 45, BS 782, WL 208. LONGITUDINAL FLOORBEAM WAS REPLACED ON N01170.SDR 06FDEA03684Floorbeam · corrodedFOUND LONGITUDINAL FLOORBEAM CORRODED AT NUTPLATE HOLES, RBL 45, BS 823 - 848, WL 208. FOUND CORROSION OUT OF LIMITS ON FLOOR BEAM IAW SRM 53-10-1 FIG 8 AND SRM 51-10-6. REMOVED AND REPLACED BEAM IAW SRM 51-30-2 AND SRM 51-30-5.SDR 06FDEA03683Floorbeam · corrodedFOUND CORROSION ON LONGITUDINAL FLOORBEAM AROUND NUTPLATE HOLES, LBL 25, BS 760 THROUGH 848, WL 208. REPLACED LONGITUDINAL FLOOR BEAM IAW SRM 53-10-1, 51-30-5 AND 51-30-2.SDR 06FDEA03646Stringer · gougedGOUGE ON STR 1 BS 565. REPAIRED STRINGER 1 AT BS 565 PER SRM 53-10-3 FIG 3.SDR 06FDEA03645Stringer · gougedFOUND GOUGE ON STR 1 BS 565. REPAIRED STRINGER 1 AT BS 565 PER SRM 53-10-3 FIG 3.SDR 06FDEA03635Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM UPPER TEE AND LOWER SURFACE STA 680 RBL 3-21. REPAIRED FLOOR BEAM UPPER CHORD AT STA 680 PER SRM 53-10-8.SDR 06FDEA03616Frame · dentedFOUND AFT CARGO BAY DENT ON FRAME AT BS 1110 BETWEEN STR 25L AND STR 26L. REPAIRED FRAME AT BS 1110 BETWEEN STR 25L AND STR 26L PER SRM 51-40-3.SDR 06FDEA03615Frame · dentedAFT CARGO BAY DENT ON FRAME AT BS 1050 BETWEEN STR 25L AND STR 26L. REMOVED DAMAGE ON FRAME AFT CARGO BAY BS 1050 BETWEEN STR 25L AND 26L AND REPAIRED IAW SRM 51-30-5, 51-40-3.SDR 06FDEA03614Frame · dentedAFT CARGO BAY DENT ON FRAME AT BS 990 BETWEEN STR 25L AND STR 26L. REPAIRED FRAME BS 990 BETWEEN STR 25L - 26L PER SRM 51-40-3.SDR 06FDEA03613Frame · dentedFOUND AFT CARGO BAY DENT ON FRAME AT BS 1030 BETWEEN STR 25R AND STR 26R. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3.SDR 06FDEA03612Frame · dentedFOUND DENT AFT CARGO BAY ON FRAME AT BS 1050 STR 23R. REMOVED DAMAGE REPAIREDWITH FASTENER PER SRM 53-10-1, SRM 51-30-2.SDR 06FDEA03611Frame · dentedFOUND AFT CARGO BAY DENT ON FRAME AT BS 950D STR 25L. REMOVED DAMAGE ON FRAME BS 950F STR 26L AND REPAIRED IAW SRM 53-10-1, 51-40-3.SDR 06FDEA03610Frame · dentedFOUND AFT CARGO BAY DENT ON FRAME AT BS 950B STR 26R. REPARIED FRAME AT BS 950B, STR 26R PER SRM 51-40-3.SDR 06FDEA03605Structure · vibrationIN CLIMB THRU FL190 (300 KNOTS) A-FRAME BUFFET. CYCLED SPEED BRAKE (NO HELP). DISCONNECTED A/P AND SLOWED TO 280 KNTS WITH CONTINUAL BUFFET. AT FL 240 A-FRAME BUFFET STOPPED, VIBRATION IN NR 1 THROTTLE.SDR AU510002077Guide Vane · fractured(AUS) NR 1 ENGINE FIRST STAGE NOZZLE GUIDE VANE (NGV) BURNED THROUGH. NGV WAS LOCATED ADJACENT TO NR 9 COMBUSTION CHAMBER. SUSPECT CAUSED BY CRACKING ON THE LEADING EDGE ALLOWING HOT AIR TO PENETRATE THE NGV. FOUND DURING INSPECTION OF THE COMBUSTION CHAMBERSDR AU510001985Spar · crackedLT ELEVATOR REAR SPAR CRACKED. FOUND DURING INSPECTION IAW AD/B727/100.SDR AU510001954Compressor · misrepairedNR 3 ENGINE FIRST STAGE COMPRESSOR BLADE BLENDED BEYOND LIMITS IN MAINTENANCE MANUAL. RECORDS GAVE NO INDICATION OF BLEND REPAIR BEING CARRIED OUT.SDR AU510001660Skin · crackedFUSELAGE SKIN LAP JOINTS CRACKED. JOINTS WERE LOCATED AT STRINGER 4R BETWEEN BS 480 AND BS 720B AND AT STRINGER 26L BETWEEN STN 560 AND STN 580. FOUND DURING MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION IAW AD/B727/160 AND SB727-53AO222.SDR AU510001646Hinge Pin · cracked(AUS) LT HORIZONTAL STABILIZER OUTER HINGE PIN CRACKED IN AREA OF THREAD ROOT ADJACENT TO SPLIT PIN HOLES. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW SB727-55A0090R1 PART 4 AND AD/B727/173.(AD/SB DESC: AD/B727/173, SB727-55A0090R1 ) (CASA# 510001646)SDR AU510001526Wheel · crackedMAIN WHEEL INNER HUB CRACKED APPROXIMATELY 35MM (1.377IN) BELOW THE MATING FACE AND EXTENDING THROUGH TO THE OUTSIDE OF THE HUB AT THE TIE BOLT HOLE SEAT RADIUS. CRACK LENGTH 18MM (0.708IN). CRACK IS LOCATED OUTSIDE OF AREAS LAID DOWN IN THE MAINTENANCE MANUSDR AU510001519Door Frame · crackedNR 3 CARGO DOOR LOWER FORWARD FRAME RADIUS AND `T` FRAME CRACKED THROUGH THREE FASTENER HOLES. FOUND DURING INSPECTION IAW SB 727-52-0149.SDR AU510001874Support Fitting · crackedLT AND RT ENGINE FORWARD SUPPORT FITTING ASSEMBLIES CRACKED. LT PYLON FITTING CRACKED AT HOLE `F`. RT PYLON FITTING CRACKED AT HOLE `P`. FOUND DURING INSPECTION IAW AD/B727/151 AND BOEING SB 727-54A0010.SDR AU510001461Line · damaged(AUS) HYDRAULIC PIPES PNO 65-17849-61 AND PNO 65-17849-4014 RUBBING TOGETHER CAUSING ONE PIPE TO BE HOLED. LOSS OF HYDRAULIC FLUID. INVESTIGATION FOUND A FAILED `P` CLIP ON ONE OF THE PIPES WHICH ALLOWED THE PIPES TO RUB TOGETHER.(OTHER CAUSE: AGE ) (CASA# 510SDR 05FDEA02141Floorbeam · corrodedFLOORBEAM AT STA 620 RBL 0-24.5 HAS CORROSION ON UPPER CAP. REMOVED DAMAGED AREA IAW SRM 53-10-8. FAB REPAIR PARTS, T-ANGLE, SUPPORT ANGLE, STRAP, IAW SRM 53-10-3 FG 3 PG 18. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 53-10-8 FIG 3 PSDR AU510001965Engine · bird ingestionNR 1 ENGINE BIRDSTRIKE. INVESTIGATION FOUND THE REMAINS OF THREE FLYING FOXES. THOROUGH INSPECTION OF THE ENGINE FOUND NO OBVIOUS DEFECTS. A WATER WASH WAS CARRIED OUT AND THE AIRCRAFT RELEASED TO SERVICE.SDR AU510001545Duct · brokenNR 2 ENGINE INLET ANTI-ICE DUCT FLANGE COUPLING LIP FRACTURED AND SEPARATED. EVIDENCE OF A PRE-EXISTING CRACK.SDR AU510001960Nut · separated(AUS) NR 2 ENGINE POWER CONTROL LEVER CONTROL CRANK RETAINING NUT LOCATED ON THE MAIN ACCESSORY GEARBOX CROSS SHAFT ADRIFT. THE CRANK MOVED OFF THE CROSS SHAFT AND POWER LEVER CONTROL WAS LOST. THE RESULT OF THE UNCONTROLLED POWER LEVER ALLOWED AN UNCOMMANDED SDR 04FDEA03394Stringer · corrodedDURING "B" CHECK VISIT, LOWER AFT FUSELAGE FWD OF STATION 1183 HAS HI LOCK AND RIVETS MISSING. FURTHER INVESTIGATION REVEALED STRINGER 28R, STA 1166 HAD EXFOLIATION CORROSION OUT OF SRM LIMITS. SPLICED IN NEW SECTION OF STRINGER PER B727 SRM 53-10-3, FIG 1SDR 04FDEA02842Channel · corrodedFWD LWR CARGO A/C COMPT STR 27L BETWEEN F/S 720F TO 740, PROTECTIVE FINISH PEELING AND MINOR SURFACE CORROSION IN HAT CHANNEL. REMOVED CORROSION IAW SRM 51-10-6 PG 6, PARG 4. ORIG MAT .095, AFTER REWORK .075 .020 MAT LOSS, FOUND TO BE OUT OF LIMITS IAW SRMSDR 04FDEA02840Floorbeam · corrodedBFM CLOSER C/W WITH EA7-5321-82044 FUSELAGE, FLOORBEAM UPPER CORD REPAIR STA 950 AT BL 21.0 ENT BY: 497236 RPT BY: 497236 FACT 28SEP04 23:10. BFM U COMPLIED WITH EA 7-5321-82044. REMOVED CORROSION, TREATED AREA AND INSTALLED REPAIR ANGLE ENT BY: 497236 RPT SDR 04FDEA02839Support Beam · corrodedCLOSER COMPLY WITH EA NR 7-5710-82041 WINGS, LEFT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. BFM U COMPLIED WITH EA7-5710-82041 REAMED HOLE, FLAP PEENED AREA , INSTALLED REPAIR BUSHING AND WASHER ENT BY: 497236 RPT BY: 497236.SDR AUS20040438Door Frame · cracked(AUS) NR 1 CARGO DOOR FRAME CRACKED IN AREAS ADJACENT TO DOOR STOP NR 5 AND NR 6. FOUND DURING INSPECTION IAW AD/B727/165 AND MFG SB727-53A0219.SDR AUS20040376Bearing · seized(AUS) IB FLAP SELECTOR VALVE INPUT ROD SELF ALIGNING BEARING BINDING DUE TO LACK OF LUBRICATION.SDR AUS20040211Nut · missing(AUS) RT IB FLAP CARRIAGE DEAD WEIGHT ROLLER NUT AND LOCK WASHER MISSING. BOLT WAS STARTING TO MIGRATE FROM POSITION. SUSPECT CAUSED BY FAILURE OF LOCK WASHER TAB.SDR AUS20040179Panel · faulty(AUS) SMOKE AND BURNING ODOR COMING FROM TOP SECTION OF P18 CIRCUIT BREAKER PANEL.SDR AUS20040157O-Ring · failed(AUS) HYDRAULIC SYSTEM A PRESSURE MODULE SUPPLY LINE O-RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.
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