Boeing 727-228
Service difficulty reports · 1,323
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 = '727228' 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 = '727228' 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 DHL9872422CFairing · crackedAT C-CHECK, AFT CARGO FWD DOOR CUTOUT AFT CENTER AREA FAIRING LOWER CORNER TORN. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 3468.SDR DHL9872421CSkin · dentedAT C-CHECK, SKIN DENTED AT STA 423 BETWEEN STR 23L AND 24L. CUT OUT DAMAGED SECTION, INSTALLED DOUBLER PER SRM 53-30-3. DOUBLER 14 X 17, FILLER 1 X 1. N/R 3476.SDR DHL9872420CSkin · dentedAT C-CHECK, FS SKIN AT STA 420 STR 24L DENTED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 14 X 17. N/R 3487.SDR DHL9872406CClip · crackedAT C-CHECK, NR 1 SLAT OUTBD TRACK TO SLAT LOWER SKIN ATTACH CLIP IS CRACKED AT RADIUS. REPLACED CLIP PER SRM 51-30-2, N/R 1070.SDR DHL9872405CBracket · crackedAT C-CHECK, LEFT WING T/E CAVITY FOUND LOWER PANEL SUPPORT BRACKET CRACKED AND LOOSE BELOW NR 3 FLIGHT SPOILER. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-10-1, N/R 1049.SDR DHL9872404CRib · crackedAT C-CHECK, RT WING RIB CHORD AT BL 70.5 HAS HFEC CRACK INDICATION, HFEC HOLE, OVERSIZED. HFEC INSTALLED ATTACH TEE PER SRM 51-20-2, N/R 2288.SDR DHL9872403CAngle · crackedAT C-CHECK, RT WING NR 8 SPOILER UPPER SUPPORT BRACKET IS CRACKED, AFT BOTTOM AREA. ALSO, IN SAME BRACKET, OUTBD SIDE CRACKED AT TOP. REPLACED SUPPORT BRACKET AND ANGLE PER SRM 51-10-1, N/R 2333.SDR DHL9872470CSpar · corrodedAT C-CHECK, CORROSION ON LEFT WING FRONT SPAR LOWER CHORD O/B FLANGE UPPER SURFACE WS 399. REMOVED CORROSION, INSTALLED CHORD REPAIR PER AVITAS EO 98PMSI191D-1, 13 X 2.75. N/R 1024.SDR DHL9872429CSide Rail · gougedAT C-CHECK, MAIN CABIN RT SIDE RAIL AT BS 530 IS HEAVILY GOUGED. STOP DRILLED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 4.5 X 2.5. N/R 5039.SDR DHL9872425CSkin · dentedAT C-CHECK, DENT AT BS 259R AT STR 24R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 13 X 7.5. N/R 3424.SDR DHL9872424CSkin · dentedAT C-CHECK, DENT AT STR 24R BA 264R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 13 X 7.5. N/R 3425.SDR DHL98727003Fitting · brokenAIRFRAME VIBRATION AND BUFFETING DURING LEFT TURNS. REPLACED BROKEN CHANNEL FITTING COVE PANEL WING STA 521 I/B SIDE. REPLACED AND ADJUSTED BROKEN ROD END IN LT COVE PANEL ASSY STA 543. INSTALLED MISSING NUT, WASHER, IN RT I/B FLAP CARRIAGE TRACK ROLLER BEARSDR DHL9872454CRib · crackedAT C-CHECK, CRACK IN UPPER FLANGE OF RIB 13, R/W. STOP DRILL CRACK, HFEC, INSTALLED RIB REPAIR PER SRM 57-10-5. REPAIR 16 X 2 X 1. N/R 2257.SDR DHL9872440CRib · crackedAT C-CHECK, 1 CRACK NOTED AT UPPER FLANGE AT RIB 13. STOP DRILLED CRACK, HFEC STOP DRILL, INSTALLED RIB REPAIR AT WS 601.5 PER SRM 57-10-5, 16 X 2 X 1. N/R 2257.SDR DHL9872459CRib · crackedAT C-CHECK, LEFT WING RIB CHORD BL 70.5 HAS CRACK INDICATION AT FWD UPPER AND FWD LOWER HOLES. HFEC, CRACK VERIFIED. STOP DRILLED CRACK, HFEC, INSTALLED REPAIR PER S/B 57-0211. N/R 1030/1143.SDR DHL98727001Bulkhead Frame · crackedAT AFT BULKHEAD AFT ENTRY DOOR FRAME CRACKED AT NR 7 STOP LEFT AND RIGHT HAND. REPAIRED PER 727 S/B 53-0055.SDR DHL97720001Oil Press Switch · failedENGINE NR 3 OIL PRESSURE LIGHT FLICKERED CLIMBING THROUGH 8,000 ON T/O. ACCOMPLISHED ALT PROC AND DETERMINED AN IMPENDING OIL BYPASS. RETURNED TO DEN. WHEN THRUST RETARDED, OIL LIGHT WENT OUT. INSPECTED AND REPLACED OIL FILTER DUE TO CARBON, LIGHT FLICKERSDR DHL97722006Air Distribution · odorIRRITATING OIL BASED SMELL IN COCKPIT. SUSPECT TO BE FROM F/O SEAT. CLEANED EXCESS SEAT LUBRICANT FROM COCKPIT FLOOR AT F/E AND F/O SEAT PER BMM.SDR DHL97727006Oxy Bottle · leakingIN FLIGHT DURING SYSTEM CHECKS, CREW OXYGEN GAUGE READING 200 LBS. FOUND BOTTLE EMPTY, SERVICED O2 BOTTLE. FOUND LEAK, REMOVED AND REPLACED BOTTLE IAW 12-15-11, LEAKS CHECK GOOD.SDR DHL97724009Engine · malfunctionedCANNOT MAINTAIN MAX CONTINOUS THRUST THROUGH CLIMB-OUT ON NR 1 ENGINE. ENGINE RUNS APPROX 80 DEGREES HOTTER THAN NR 2 OR NR 3. REMOVED AND REPLACED ENGINE PER TASK MANUAL 71-01-17.SDR DHL97722005Fuel Control · failedNR 1 ENG EPR SPIKED TO 2.5 EPR FOR 1 SECOND DURING TAKEOFF, EPR THEN DECREASED TO APPROX 1.80 EPR ON CLIMB THRUST. ALL ENGINE GAUGES WERE THEN STEADY AT CLIMB THRUST. AFTER CLIMBOUT, THRUST LEVER MOVEMENT WOULD NOT CHANGE THRUST. REMOVED AND REPLACED NSDR DHL97721004Instrument Amp · failedCAPTAINS HSI PROCESSED EXCESSIVELY. OPERATES PROPERLY WHEN TRANSFERRED TO NR 2 DG, NR 1 RMI DOES NOT FOLLOW CAPTAINS HSI AFTER TRANSFER. REPLACED INST AMP, OPS CHECK OK.SDR DHL9772723CFloorbeam · crackedAT C-CHECK, MAIN CABIN CENTER SECTION FLOORBEAM CRACK THROUGH HOLE BS 825 LBL 51. REMOVED AND REPLACED WEB AT BS 825 LBL 45 TO LBL 70, 25 BY 12 PER SRM 51-30-2 AND SRM 53-10-2.SDR DHL9772722CFloorbeam · crackedAT C-CHECK, MAIN CABIN CENTER SECTION FLOORBEAM CRACKED AT BOTH THROUGH HOLES BS 804 LBL 51 AND LBL 55. REMOVED AND REPLACED WEB PER SRM 51-30-2 AND 53-10-2, 24.25 BY 9.SDR DHL9772716CCover · crackedAT C-CHECK, RT ELEVATOR BOB WEIGHTS HAVE CRACKED COVERINGS. REPLACED BOB WEIGHTS PER SRM 51-10-1.SDR DHL9772713CShroud · corrodedAT C-CHECK, RT LOWER FUEL LINE SHROUD IS HEAVILY CORRODED ON OUTBD FWD SIDE. REMOVED SHROUD, REPLACED GUIDE ASSY PER SRM 51-10-1, 19 BY 2. REPLACED LATCH, INSTALLED SHROUD AND SEALED.SDR DHL9772709CSkin · crackedAT C-CHECK, LEFT INBD FLAP MIDFLAP FWD SKIN PANEL O/B OF NR 3 TEAR DROP CRACKED. CUT OUT DAMAGED AREA, ACCOMPLISHED HFEC, FOUND NO CRACKS BEYOND CUT OUT. INSTALLED DOUBLER PER SRM 57-50-4, 5.5 BY 4.5.SDR DHL9772719CSkin · gougedAT C-CHECK, FUSELAGE SKIN GOUGED BELOW NR 1 ENGINE STRUT FWD END. BURNISHED SKIN, OUT OF LIMITS. CUT OUT DAMAGED AREA 1.5 BY .75. INSTALLED REPAIR PER SRM 53-30-3.SDR DHL9772718CChannel · corrodedAT C-CHECK, CORROSION ON HORIZ SUPPORT CHANNEL STA 1135 LBL 19 UNDER ANCHOR NUT. REMOVED CORRODED CHANNEL AND INSTALLED NEW CHORD PER SRM 51-10-1, 10 LONG.SDR DHL9772717CCover · crackedAT C-CHECK, LT ELEVATOR TAB BOB WEIGHTS HAVE CRACKED COVERINGS. REPLACED BOB WEIGHTS PER SRM 51-10-1.SDR DHL9772712DBracket · crackedAT C-CHECK, 37 SLAT ACTUATOR MOUNT BRACKET CRACKED I/B SIDE. ACCOMPLISHED REPAIR PER S/B 57-130.SDR DHL9772704CDoor · crackedAT C-CHECK, FWD CARGO DOOR FWD LOWER CORNER CRACKED. REPLACED CORNER PER SRM 51-30-2.SDR DHL9772720CFloorbeam · corrodedAT C-CHECK, STA 328 FLOORBEAM UPPER CHORD TO FLOOR PANEL BLEEDING CORROSION FROM APPROX RBL 12 TO LBL 12. CUT OUT DAMAGED AREA, INSTALLED ANGLES, REPAIR PER BOEING SRM 53-1-8. ANGLE 15 BY 1 BY 1.25, 13 BY 1 BY 1 AND FILLER 1.75 BY 1.SDR DHL9772715CWeb · crackedAT C-CHECK, LEFT STAIRWELL LOWER TORQUE BOX LIGHTENING HOLE CRACKED JUST AFT OF STA 1323. STOP DRILLED CRACK, HFEC INSP, INSTALLED WEB REPAIR DOUBLER PER SRM 51-40-2. REPAIR 5 BY 3.SDR DHL9772714CSkin · dentedAT C-CHECK, RT LOWER FUSELAGE SKIN HAS A DENT FWD PANEL 3332. ROUND OUT DAMAGED AREA, OUT OF LIMITS. INSTALLED DOUBLER REPAIR PER SRM 53-30-3, REPAIR 4.SDR DHL9772711CBracket · crackedAT C-CHECK, NR 6 SLAT I/B UP STOP HAS BOTH LT AND RT SUPPORT BRACKETS CRACKED. REMOVED AND REPLACED SUPPORT BRACKETS AND STOPS PER SRM 51-10-1. ADJUSTED STOPS, BRACKETS 3 BY 5.SDR DHL9772710CRib · corrodedAT C-CHECK, L/E RIB HAS CORROSION AT FWD END ABOVE NR 5 L/E FLAP AT STA 234. CUT OUT CORROSION, INSTALLED REPAIR PER SRM 57-10-6, REPAIR 3 BY 5.SDR DHL9772708CSkin · dentedAT C-CHECK, RT SIDE OF LOWER FUSELAGE SKIN HAS A DENT FWD OF PANEL 3332. DENT OUT OF LIMITS. INSTALLED DOUBLER REPAIR PER SRM 53-30-3.SDR DHL9772707CSkin · crackedAT C-CHECK, FWD GALLEY DOOR EXTERNAL SKIN PREVIOUS REPAIR IS BENT AND CRACKED. REMOVED REPAIR, INSTALLED DOUBLER AND FILLER PER SRM 52-00-3. FILLER 1.5 BY 2 AND DOUBLER 5 BY 5.SDR DHL9772706CFrame · crackedAT C-CHECK, FRAME WEB CRACKED BETWEEN FASTENERS AT BS 1050 AT STR 30. HFEC, INSTALLED WEB REPAIR PER SRM 51-40-2, 5 BY 6.SDR DHL9772705CFrame · dentedAT C-CHECK, FRAME I/B FLANGE HAS DEEP DENT AT BS 1090 AND 26L. CUT OUT DAMAGED AREA ON FRAME 2.75 BY 1.25. INSTALLED FRAME REPAIR PER SRM 53-10-4 DOUBLER 14.5 BY 2.375 BY 1.SDR DHL9772703CSkin · crackedAT C-CHECK, NR 7 SLAT UPPER SKIN AT L/E IS DENTED AND TWO CRACKS RADIATING FROM RIVET HOLES. PERFORMED HFEC, ONE CRACK ONLY. STOP DRILLED CRACK, HFEC, INSTALLED REPAIR PER SRM 57-50-3, 4 BY 4.SDR DHL9772702CSkin · damagedAT C-CHECK, NR 5 SLAT PREVIOUS REPAIR ON LOWER SKIN IS NOT WITHIN SRM LIMITS. INSTALLED REPAIR PER SRM 57-50-3, 4 BY 6.SDR DHL9772701CSkin · chafedAT C-CHECK, LEFT WING O/B FLAP HAS CHAFING ON UPPER SURFACE O/B END. BURNISHED AREA, OUT OF LIMITS. CUT OUT DAMAGED AREA, INSTALLED DOUBLER 8.5 BY 4.5 AND FILLER 5.75 BY 1.5 PER SRM 57-50-4.SDR DHL9772721CSkin · dentedAT C-CHECK, C-3 CARGO DOOR EXT SKIN DENTS AT 10 AND 18 ABOVE CONTROL HANDLE. CUT OUT DAMAGED AREA AT 18 ABOVE DOOR HANDLE. INSTALLED REPAIR DOUBLER PER SRM 52-00-3. DOUBLER 7 BY 8 AND FILLER 2 BY 2. DENTS AT 10 WITHIN LIMITS. NDT FOR CRACKS, NONE FOUND.SDR DHL97724008Fitting · crackedFS 740 RT STR 18R TO 20 RT, CRACK IN FWD FLANGE OF THE 740 FITTING ALONG ROW FASTENERS. REMOVED FASTENERS, ACCOMPLISHED HFEC, STOP DRILLED CRACKS, ACCOMPLISH HFEC OF STOP DRILL. AREA PREVIOUSLY REPAIRED.SDR DHL97724007Door · corrodedC-3 DOOR EXTERIOR SKIN BULGED AND OIL CANNED APPROX 14 FROM TOP OF AFT CORNER. CUT OUT DAMAGED SKIN AT C-3 DOOR, AREA 1.5 BY 7. INSTALLED DOUBLER PER SRM 52-00-3 ON 14 FROM TOP AFT CORNER. REPAIR 7 BY 10.SDR DHL97724006Skin · corrodedBULGED FUSELAGE SKIN PANEL AT BS 1030 JUST BELOW RIGHT AFT SERVICE DOOR LOWER HINGE. REMOVED AND REPLACED SKIN PANEL 8 BY 8. REMOVED SURFACE CORROSION FROM SKIN AT LAP SEAM (.002) AND PRESSURE STOP FITTING, O/B SIDE APPROX .022, WITHIN LIMITS PER SRM 53-10-1SDR DHL97724005Flap Indicator · malfunctionedON CLIMBOUT, DURING FLAP RETRACTION, OUTBOARD FLAPS STAYED AT 15 DEG WHEN 5 DEG WAS SELECTED. ACCOMPLISHED ALTERNATE PROCEDURE, RESET CBS, RECYCLED FLAPS, WITH NO RESULTS. ON LANDING THE OUTBOARD FLAPS EXTENDED TO 30 DEG. REMOVED AND REPLACED FLAP INDICATORSDR DHL97722004Connector · brokenNR 1 ENGINE OIL TEMP 135 TO 140 IN CRUISE, PRESS 46 PSI, 4.2 GAL OIL QUANTITY. FOUND PIN F ON CONNECTOR D356 BROKEN. REPAIRED PER 79-34-01, OPS CHECK OK.
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