Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 95FDEA01499Clip · crackedCRACKED STRINGER CLIPS AT STA 950C, STR 6 AND 7R. REMOVED CRACKED STR CLIPS AT BS 950C, STR 6 AND 7R. BACK DRILLED NEW STR CLIPS AND INSTALLED WET WITH FAYING SURFACE SEALANT IAW FEDEX SRM 51-30-2, 51-10-1 AND FEDEX MM 51-30-0.SDR 95FDEA01498Clip · crackedCRACKED STR CLIP NR 1 AT BS 440. REMOVED CRACKED STR CLIP AT BS 440 STR 1. BACK DRILLED NEW CLIP AND INSTALLED WET WITH FAYING SURFACE SEALANT IAW FEDEX SRM 51-30-2, 51-10-1 AND MM 51-30-0.SDR 95FDEA01497Stringer · puncturedSTR 22R PUNCTURED BS 480 PLUS 8.5 INCHES. REMOVED DAMAGED SECTION OF STR 22R, BS 480 PLUS 8.5 INCHES. FABRICATED REPAIR PARTS AND INSTALLED WET WITH SEALANT IAW FEDEX 727 SRM 53-10-3, FIG 1.SDR 95FDEA01496Floor Beam · corrodedCORROSION (C53-224-01) AROUND FASTENER HOLES ON TOP CHORD OF BEAM BS 344, RBL 16-LBL 60, WL 208. REMOVED UPPER T-CHORD, FIXED NEW CHORD IN PLACE AND DRILLED, REMOVED DEBURRED, ALODINED, PRIMED AND INSTALLED WET WITH SEALANT. ALL WORK DONE IAW FEDEX SR 27-53-SDR 95FDEA01495Frame · crackedFRAME CRACKED UNDER FLOOR SUPPORT, BS 640, STR 27R, RBL 18. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-3.SDR 95FDEA01494Frame · crackedFRAME CRACKED UNDER FLOOR SUPPORT, BS 600 ABOVE STR 28L LBL 10. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-3.SDR 95FDEA01469Frame · crackedFRAME BENT AND CRACKED AT BS 500 STR 25L. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-03.SDR 95FDEA01445Sensor · failedDURING T/O WITH WEIGHT OFF LDG GEAR, LDG GEAR LEVER LATCH FAILED TO RELEASE, CB ON P6-3 WERE IN. UPON RETRACTING FLAPS IAW CHECKLIST FROM 5 TO 2 DEGREES, RECEIVED A T/O WARNING HORN. GEAR REMAIN DOWN ON THE GRD, RT MAIN IND LT FLASHES. REMOVED AND REPLACED SDR TAOA099512Eel Assy · failedESCAPE PATH EMERGENCY LIGHT AT ROW 7 INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (M)SDR 95FDEA01492Skin · crackedFORWARD LT FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. FS 303, STR 13L. CRACK LENGTH .480 INCH INITIAL MEASUREMENT. NDT VERIFIED CRACK END IN FASTENER HOLE. COUNTER BORED FUSELAGE OUTER SKIN AT FASTENER HOLE. ROUTED OUT CRACK AND INSTALLESDR AALA951716Eel Wire · brokenDFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN AND FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRE FOR EXIT LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 95FDEA01491Floor Beam · corrodedMAIN CARGO INTERIOR, CORROSION ON TOP OF STA 344 FLOOR BEAM UPPER CHORD, BETWEEN RBL 2 - 14. REMOVED CORROSION, INSTALLED REPLACEMENT CHORD AND SPLICE ANGLES PER STANDARD REPAIR DRAWING MANUAL SR 27-53-007.SDR 95FDEA01432Floor Beam · corrodedMAIN CARGO INTERIOR, CORROSION ON TOP OF STA 344 FLOOR BEAM UPPER CHORD BETWEEN RBL 2 - 14. REMOVED CORROSION, INSTALLED REPLACEMENT CHORD AND SPLICE ANGLES PER STANDARD REPAIR DRAWING MANUAL SR 277-53-007.SDR 95FDEA01490Stringer · crackedMAIN CARGO INTERIOR STRUCTURE. STR 16R CRACKED IN OUTER FLANGE, AFT OF STA 720B FRAME, FWD OF ICE LIGHT HOUSING. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER SRM 53-10-3 FIG 2.SDR SCNA95190Eel · faultyTHE OVERHEAD EMERGENCY LIGHT NEAR THE R-1 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-01, LIGHT TESTED GOOD.SDR 95FDEA01395Floor Beam · corrodedCORROSION ON TOP OF UPPER LOBE FLOOR BEAM STA 344, RBL 2-6.SDR 95FDEA01394Stringer · crackedNR 0398 (PATTERN CARD 72C235-02) CRACK IN STR 15L AT FASTENER. FORWARD SIDE OF ICE LIGHT BETWEEN FUSELAGE STA 720B - 720C. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-10-3, FIG 2.SDR CAL950821Hyd Pump · inoperativeMSY - FLT 1528 - THE NR 1 HYDRAULIC B-PUMP LOW PRESSURE LIGHT ILLUMINATED IN-FLIGHT. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 B-SYSTEM HYDRAULIC ELECTRIC DRIVEN PUMP HAD FAILED. THE PUMP WAS RESDR 95FDEA01489Stringer · crackedCRACK IN STR 15L AT FASTENER AFT OF ICE LIGHT BOX BETWEEN STA 720B AND 720G. STOP DRILLED CRACK IN STR 15L AT FASTENER AFT OF ICE LIGHT. HFEC AROUND STOP DRILL, NO CRACKS FOUND PER NDT MANUAL. INSTALLED REPAIR PER SRM 53-10-3 / 7075-T6 .040 INCH, SRM 53-10-SDR 95ZZZM736Outlet Duct · crackedNR 1 ENGINE FAILED, NR 9 COMBUSTION CAN INSPECTED. INNER OUTLET DUCT AFT OF NR 9 COMBUSTION CAN CRACKED BEYOND LIMITS OF MM 72-44 PAGE 201 TO 206. REMOVED AND REPLACED NR 1 ENGINE IAW J771-00-01. LEAK AND OPS CHECKS GOOD. ENGINE LAST SHOP VISIT, 10875 HOURSDR TAOA099505Eel Battery Pack · dischargedRIGHT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK ASSEMBLY. OPS CHECK OK PER MM 33-50-0. (X)SDR 95ZZZM734Rod · disconnectedIND - FLT NR 428 - THE L-2 (GALLEY DOOR) IS HARD TO OPEN AND CLOSE. IT WAS FOUND THAT THE L-2 DOOR WAS HARD TO OPEN DUE TO THE LOWER GATE ON L-2 NOT RAISING. REMOVED DOOR LINING AND FOUND THE ROD TO THE LOWER GATE DISCONNECTED. REATTACHED ROD, REINSTALLED DSDR 95FDEA01233Circuit Card · failedT/O ABORTED AT 110 KTS, BECAUSE OF WARNING LIGHT, ALT ALERT, 3 REVERSERS, ALL GEAR WARNING LIGHTS GEAR PANEL. REMOVED AND REPLACED MASTER DIM AND TEST MODULE CARD.SDR 95FDEA01223Stringer · corrosionFWD CARGO BAY HAD CORROSION ON STR 27R AT BS 625. REMOVED AND REPLACED DAMAGED AREA OF STA 625 STR 27R PER FEDEX SRM 53-10-3.SDR 95FDEA01215Floorbeam · damagedWHILE WORKING NR O652 DISCOVERED DAMAGE TO FLOORBEAM WEB AT BS 1110 BL 0 WL 207. PREVIOUSLY CAUSED DURING INSTALLATION OF HAYES CARGO MOD. REPAIRED FLOORBEAM PER FEDEX EA 7-5310-25620.SDR 95FDEA01213Skin · corrodedCORROSION (71C209-02), ON SKIN BS 950F PLUS 12 TO 974, BETWEEN STR 29 AND 30R AFT CARGO BAY. CUT OUT DAMAGED AREAS OF SKIN FROM BS 950F PLUS 12 TO 974, BETWEEN STR 29 AND 30R. REPAIRED CUT OUT AREAS IAW FEDEX SRM 53-30-3.SDR 95FDEA01205Frame · crackIN THE FWD CARGO BAY THE UPPER FLANGE OF FRAME IS CRACKED AT BS 560 RBL 2, WL 154. REPAIRED UPPER FLANGE OF FRAME AT BS 560 RBL 2 WL 154 IAW SRM 51-40-3.SDR 95FDEA01206Splice · corrosionCORROSION ON STR 26R BS 648-664 AND ON STR SPLICE HAT AT BS 680. REMOVED CORROSION WITHIN DAMAGE LIMITATION ON STR AND REPLACED STR SPLICE HAT AT BS 680 STR 26R ALL WORK IAW SRM 51-40-3.SDR 95FDEA01214Keel Beam · crackedCORROSION ON O/B FLANGE OF STR 29R BS 950E KEEL BEAM. DURING CORROSION REMOVAL DISCOVERED A CRACK RUNNING CLEAR THROUGH KEEL BEAM LOWER FLANGE FROM RADIUS TO RADIUS, AT BS 950E PLUS 3.5 STR 29R CRACK WAS 1.5 LONG. CUT OUT SKIN FOR ACCESS AND REMOVED KEEL BEASDR TAOA089507Eel Battery Pack · dischargedRIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK FOR RT FORWARD OVERWING EMERGENCY EXIT LIGHT - OPS CHKS OK. (X)SDR CAL950752Hyd Module · leakingFLT NR 0299 - EWR - THE 'A' HYD SYSTEM OVERHEAT LIGHT ILLUMINATED IN FLIGHT. THE 'ABNORMAL' PROCEDURES WERE COMPLIED WITH, BUT HAD NO EFFECT. A RETURN TO EWR WAS INITIATED AND ON FINAL APPROACH THE 'A' SYSTEM PRESSURE WENT TO 500 PSI ACCOMPANIED BY ILLUMINATSDR 95FDEA01199Switch Wire · failedRT MLG DOOR LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT, 3 TIMES. REMOVED AND REPLACED WIRING FROM D752 TO SPLICES SP578 AND SP576. REMOVED AND REPLACED D752 FOR RT MLG DOOR LOCK SW. FUNCTIONAL CHECKS GOOD PER FEDEX MM 32-62-11.SDR 95FDEA01197Floor Beam · corrodedTHE UPPER CHORD OF THE BS 480, FLOOR BEAM IS CORRODED OUT OF LIMITS AT RBL 12, WL 208.5. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-10-08, FIG 3.SDR 95FDEA01184Skin · corrodedBS 480-500 STR 28R-26R. THERE ARE DEEP GOUGES, DENTS AND A SMALL BULGE ON EXTERIOR SKIN. REPAIRED CORRODED SKIN AT BS 496, RBL 7 PER FEDEX SRM 53-30-5.SDR 95FDEA01183Shear Tie · corrodedCORROSION (71C709-02) ON SHEAR TIE LOWER FLANGE BS 970, RBL 3, FWD AND AFT SIDE OF FRAME AFT CARGO BAY. INSTALLED NEW SHEAR TIE OR BS 970 PER SRM 53-10-2.SDR 95FDEA01182Stringer · corrodedCORROSION IN FWD CARGO BAY. THERE IS CORROSION ON STR 28R AT BS 496. REPAIRED CORRODED STR 28R AT BS 496 PER FEDEX SRM 53-10-3. REPAIRED CORRODED SKIN FROM NRO 067 AT BS 496 , RBL 7 PER FEDEX SRM 53-30-3.SDR 95FDEA01181Seat Track · corrodedSEAT TRACK CORRODED ALONG FLANGES BS 495-535 AND BS 615, BL 0, WL 208.5. REMOVED, FABRICATED AND INSTALLED SEAT TRACK BS 480-630 PER SRM 53-10-5.SDR 95FDEA01180Rib · crackFLOOR BEAM CORRODED AT BS 460, RBL 12 - 23, WL 208.5. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1 AND 53-10-08.SDR 95FDEA01164Stringer · crackedNR 8R STR IS CRACKED IN VERTICAL FIN BAY NR 8 FIN STA 180 WHERE STR ATTACHES TO WEB. REPAIRED NR 8R STR IN VERTICAL FIN, BAY NR 8, FIN STA 180. FEDEX SRM 55-30-4 FIG 1.SDR 95FDEA01163Skin · corrosionCORROSION ON (INTERIOR) SKIN AT BUTT JOINT BS 680-688 BETWEEN STR 26-27R. REPAIRED CORROSION ON SKIN AT BUTT JOINT BS 680-688 BETWEEN STR 26-27R AS PER FEDEX SRM 53-30-3.SDR 95FDEA01162Stringer · crackedSTR NR 8R IS CRACKED IN VERTICAL FIN BAY NR 8 AT FIN STA 151.2. REPAIRED STR NR 8R IN VERTICAL FIN BAY NR 8 AT FIN STA 151.2 IAW FEDEX SRM 55-30-4.SDR 95FDEA01161Spar · crackedNR 6 SLOT CRACKED IN SPAR AT TAI TUBE CUTOUT. STOP DRILLED CRACK AND INSTALLED REPAIR PARTS IAW SRM 57-20-1, 51-30-2 AND FEDEX EA 7-5710-25579.SDR 95FDEA01157Skin · chafedUPON REMOVAL OF LT WING PIE SECTION. FOUND CHAFING SPOT 2 INCHES LONG BY 1 INCH WIDE AND .081 DEEP ON STR 19L AT LAP SEAM, STA 720D PLUS 11. REPAIRED DAMAGE PER FEDEX SRM 53-30-3.SDR 95FDEA01155Track · corrodedSEAT TRACK CORRODED OUT OF LIMITS BS 344 TO 423 LBL 25 WL 208.5. REMOVED, FABRICATED AND REPLACED SEAT TRACK FROM BS 344 TO 480, WORK PER SRM 51-10-1.SDR 95FDEA01154Seat Track · corrodedSEAT TRACK CORRODED ALONG RT FLANGE BS 538 TO 550 RBL 25 WL 208.5. REMOVED, MACHINE SHOP FABRICATED AND INSTALLED SEAT TRACK FROM BS 480 TO 550.SDR 95FDEA01153Chord · double drilledDOUBLE HOLE IN LOWER CHORD OF FLOORBEAM BS 720F LBL 46 WL 201. OVERSIZED HOLE AND INSTALLED HI-LOC PER ENGINEERING REQUEST.SDR 95FDEA01152Shear Tie · corrodedCORROSION ON SHEAR TIE BS 720 BETWEEN STR 27 LT AND RT. REMOVED, FABRICATED AND REPLACED SHEAR TIE SRM 53-10-4.SDR 95FDEA01151Frame · crackedIN THE FWD CARGO BAY, THE UPPER FLANGE OF FRAME IS CRACKED AT BS 520 LBL 2 WL 154 AND RBL 14 WL 154. FABRICATED DOUBLER, CUT OUT DAMAGE, REPAIRED FRAME PER SRM 51-40-3.SDR 95FDEA01150Web · corrosionAREA OF CORROSION ON LOWER WEB OF DELTA BEAM, OUTER SURFACE AT BS 791 LBL 5. REPAIRED AREA OF CORROSION ON LOWER WEB OF DELTA BEAM, OUTER SURFACE AT BS 791 PER FEDEX SRM 51-40-2 FIG 1.SDR SCNA95174Eel Batteries · dischargedTHE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE AFT AIRSTAIR EMERGENCY LIGHT BATTERIES AND THE LIGHT CHECKED GOOD IAW MM 33-50-61.
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