Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 05FDEA03772Repair · improperFOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 720 10" - BS 720B 15", S27R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED EXISTING REPAIR STR 27R BS 720B 15 AND DETERMINSDR 05FDEA03771Repair · undamagedEXISTING FLUSH REPAIR ON FWD SERVICE DOOR BS 380 STR 9R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND NOT TO BE WITHIN COMPLIANCE WITH FAA APPROVED DATA, REMOVED FASTENERS FABSDR 05FDEA03753Repair · improperEXISTING SPLICE REPAIR ON STR 15L BS 385, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AT BS 385 STR 15L. INSTALLED NEW REPAIR BS 385 STR 15L PER SRM 53-10-3 FIGSDR 05FDEA03752Repair · damagedEXISTING EXTERNAL REPAIR ON AFT CARGO DOOR BS 950E STR 26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR ON AFT CARGO DOOR PER SRM 52-00-3.SDR 05FDEA03739Skin · unknownEXISTING EXTERNAL REPAIRS ON NR 5 K-FLAP INNER TAI SKIN, 14 EACH 2" ROUND REPAIRS. REPAIRS REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FASTENERS, INSTALLED WASHERS AND INSTALLED FASTENSDR 05FDEA03734Flap Track · corrodedNR 6 FLAP TRACK, AFT MOUNTING SURFACE IS CORRODED. RECEIVED NR 6 FLAP TRACK INSTALLED ON FED EX WC 27X5708-03.SDR 05FDEA03733Flap Track · corrodedNR 6 FLAP TRACK, FWD MOUNT BUSHINGS ARE CORRODED. NR 6 FLAP TRACK REPLACED ON FED EX WC 27X5708-03.SDR 05FDEA03721Floor Support · corrodedFOUND SEAT TRACK SUPPORT CORRODED BS 760-848 LBL45. REMOVED AND REPLACED UPPER CHORD SUPPORT BEAM AND SEAT TRACK IAW BAC DWG 65-16279 AND FX B727 SRM 53-10-5 FIG 2. ALODINED AND PRIMED IAW FX B727 SRM 51-10-2.SDR 05FDEA03719Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM STA 344,BL0-LBL30. REMOVED, FABRICATED, ALODINED. PRIMED AND PAINTED FLOORBEAM REPAIR AT STA 344 AT BL0-LBL30 ALL IAW FX SRZ 27-53007 AND B727 SRM'S 51-30-2,53-10-2 FIG 7 AND 51-20-151.SDR 05FDEA03712Stringer · unknownFOUND EXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 705 - BS 720 15", S26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED STRINGER IAW SRM 53-10-3. DETERMINED TO BE A MAJOR REPASDR 05FDEA03695Repair · improperFOUND EXISTING EXTERNAL REPAIR ON FUSELAGE BS 1120-1133 STR 18-20R. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED REPAIR AT BS 1120-1133 STR 18R-20R PER SRM 53-30-3 FIG 3.SDR 05FDEA03643Stringer · crackedFOUND LT W/W, 18A SHELF IS CRACKED, STA 915, LBL 63, WL 189. REMOVED AND REPLACED LEFT MLG W/W 18A SHELF STA 870-940 LBL 63 WL 189 PER SRM 51- 30-2SDR 05FDEA03642Repair · improperFOUND EXISTING FLOORBEAM REPAIR AT BS 1110, RBL 16 - LBL 35, WL 208. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INSTALLED FLOORBEAM REPAIR AT B.S. 1110 RBL 16-LBL 35 WL 208 PER SRMSDR 05FDEA03641Frame · crackedFOUND CRACK IN STUB FRAME UPPER FLANGE IN FWD CARGO BAY BILGE AT BS 613, STR 26R. REPLACED STUB FRAME AT BS 613 STR 26R PER SRM 51-30-2.SDR 05FDEA03592Door Frame · gougedAFT FRAME IS GOUGED NEXT TO THE CRANK ARM FITTING OF THE LEFT AFT EMERGENCY ESCAPE DOOR. REPAIRED FRAME AT LEFT AFT EMERGENCY ESCAPE DOOR PER SRM 51-40-3.SDR 72400026Skin · corrodedTHREE 2 INCH DIAMETER AREAS OF CORROSION ON INNER SKIN.SDR 72400025Attach Angle · corrodedA .5 X .5 INCH AREA OF CORROSION ON ATTACH ANGLE.SDR 72400024Web · corrodedA 3 X 1 INCH AREA OF CORROSION ON WEB.SDR 72400023Fitting · crackedA .5 INCH CRACK IN FITTING.SDR 72400022Stringer Clip · crackedA .5 INCH CRACK IN STRINGER CLIP.SDR 72400021Stop Fitting · crackedA 5 INCH CRACK IN DOOR STOP FITTING.SDR 72400020Stop Fitting · crackedA 5 INCH CRACK IN DOOR STOP FITTING.SDR 72400019Stringer Clip · crackedA 1 INCH CRACK IN STRINGER CLIP.SDR 05FDEA03587Stringer Clip · corrodedFOUND CORROSION ON STRINGER CLIP IN FWD CARGO BAY AT BS 560, STR 26L. REPLACED STRINGER CLIP AT BS 560 STR 26L PER SRM 51-20-1.SDR DHL2005742532Shear Tie · corrodedAFT PIT STA 1170 SHEAR TIE BETWEEN STR 28R AND 29R HAS EXFOLIATED CORROSION. REMOVED SHEAR TIE ANGLE. FABRICATED AND INSTALLED SHEAR TIE ANGLE 12 X 2.75 X 2.5 INCHES FROM 60-12480 - 7075-T6 6511 IAW SRM 51-30-2, 51-20-01, 51-10-2 AND B727 MM 51-20-11, 21-32-SDR DHL2005742531Stringer · unknownAFT CARGO COMPT AT STR 28R BETWEEN STA1166 THRU STA 1148 NEED REMOVED FOR FRAME REPAIR. CUT AND REMOVED STR 28R STA 1166 TO 1148 TO FOM S/M REPAIR. FABRICATED STRINGER SPLICE 10.0 INCHES FROM BAC1498-131 TREATED, PRIMED AND TOPCOATED REPAIR PARTS AND INSTALLSDR 05FDEA03506Skin · dentedFOUND SIX INCH DENT IN SKIN AT BS 330 STR 20R. REMOVED DAMAGE ON SKIN BS 330 BETWEEN STR 20R & 21R FABRICATED REPAIR DOUBLER AND FILLER. ALODINE, PRIME INSTALLED AND PAINTED AT BS 330 BETWEEN STR 20R & 21 R IAW SRM 53-30-3 FIG 1.SDR CA051103008Turbine Blades · missing(CAN) IN CRUISE, LOST EGT INDICATION UPON DESCENDING AND POWER REDUCTION NR1 ENGINE RESULTED IN VIBRATION REQUIRING NR1 ENGINE TO BE SHUTDOWN. INITIAL INSPECTION INDICATED SOME VISIBLE T4 BLADE DAMAGE WHEN VIEWED THROUGH TAILPIPE.SDR CA051027004Bolt · sheared(CAN) DURING A ROUTINE WHEEL CHANGE, IT WAS FOUND THAT 2 OF THE 3 BRAKE RETAINING BOLT HEADS HAD SHEARED. THE BROKEN BOLT HEADS HAD BECOME TRAPPED BETWEEN THE BRAKE AND WHEEL INNER HALF CAUSING SCORING DAMAGE TO THE WHEEL. IT IS SUSPECTED THAT THE COUNTERSUNKSDR 72400007Tee Fitting · corrodedSEVERAL AREAS OF CORROSION ON NOSE T-CHORD.SDR DHL2005742530Structure · corrodedCORROSION ON CENTER WING BOX APPROX 830 AT RBL 10.0. MECHANICALLY REMOVED CORROSION ON CENTER WING BOX STA 830 RBL 10 IAW B727 SRM 51-10-6. ULTRASONIC INSPECTION OF BLEND AREA IAW ASTM E797-95, HIGH READING .209" LOW READING .128" MATERIAL LOSS .082" FOUND OSDR DHL2005742529Web · corrodedCORROSION ON SUBDECK FLOOR UPPER SURFACE AT LBL 16 STA 1166 - 1170 AT AFT ENTRY DOORWAY. CUT OUT CORROSION ON SUBDECK FLOOR UPPER SURFACE AT LBL 1166 - 1170 AT AFT ENTRY DOORWAY. FABRICATED AND INSTALLED REPAIR DOUBLER 12.25 X 14.5 INCHES FROM 2024-T3 .050 ISDR DHL2005743003Light · dislodgedEMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR HAS FALLEN OFF. RESECURED EMERGENCY EXIT LIGHT ASSY IAW 727 MM 33-50-71, OPS GOOD.SDR DHL2005742519Floorbeam · corrodedCABIN FLOORBEAM CORRODED ON FLOWER FLANGE LOWER SURFACE BS 1010 LBL 24. CUT OUT CORRODED PORTION OF LOWER LEG OF FLOORBEAM AT BS 1010 LBL 24. FABRICATED AND INSTALLED FLOOR BEAM REPAIRS 18.0 INCH X 1.95 INCH FROM BAC1505-10097, 29.50 INCH X 1.95 INCH FROM 707SDR 72400006Web · corrodedA 2 X 10 INCH AREA OF CORROSION ON WEB.SDR 724000018Stringer · crackedCRACK IN STRINGER SPLICE.SDR 724000017Angle · crackedCRACK IN ANGLE.SDR 724000016Structure · crackedCRACK IN LOWER CHORD.SDR 724000015Doubler · nickedNICK IN DOUBLER.SDR 724000014Doubler · nickedNICK IN DOUBLER.SDR 724000013Brace · crackedCRACK IN BRACE.SDR DHL2005743002Switch · out of adjustAFT AIRSTAIR AMBER LIGHT ON S/O PANEL ILLUMINATES INTERMITTENTLY. ADJUSTED AFT AIRSTAIR UP SWITCH, OPS CHECK GOOD IAW M/M 52-62-01.SDR 05FDEA03244Seat Track · corrodedSEAT TRACK AT LBL 45 STA 690-740 IS CORRODED. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED NEW SEAT TRACK FROM STA 680-740 AT LBL45 ALL IAW FX B727-200 SRM 53-10-5,53-10-1 FIG 3, 51-30-2 AND 51-10-2.SDR DHL2005742518Floorbeam · corrodedAFT PIT CEILING, CABIN FLOORBEAM BS 1120 UPPER SURFACE HAS CORROSION AT RBL 44. REMOVED CORROSION IAW B727 SRM 51-10-6, UT INSPECTED. CUT OUT CORROSION, FABRICATED AND INSTALLED FLOORBEAM REPAIR 9-3/4" BY 2.9" BY .300" FROM 7075-T6 .050 AND 8.0" BY 2.0" BY 1SDR DHL2005742521Floorbeam · corrodedAFT PIT CEILING, CABIN FLOORBEAM STA 1130 UPPER SURFACE HAS CORROSION AT LBL 60. REMOVED FLOOR PANEL AT BS 1130. CUT OUT CORRODED AREA ON FLOORBEAM UPPER STA 1130 LBL 60. FABRICATED AND INSTALLED REPAIR 10.0" BY 2.0" BY 1.0" BY .30" FROM 7075-T6 .050, AND SSDR DHL2005742510Web · corrodedCLOSE OUT WEB LEFT AT STA 354 S-15 - 17L HAS ELONGATED HOLES, GOUGES AND EXFOLIATED CORROSION. REMOVED WEB, FABRICATED AND INSTALLED SHEAR WEB 15 X 4.2 INCHES FROM 7075-T6 .040 SRM 51-40-2, 51-20-1 AND 51-10-2.SDR DHL2005742517Floorbeam · corrodedAFT PIT CEILING, CABIN FLOORBEAM BS 1070 LOWER SURFACE HAS CORROSION AT LBL 14. REMOVED CORROSION IAW SRM 53-10-8. CORROSION REMOVAL INTO TANGENT OF RADIUS. FABRICATED AND INSTALLED REPAIR STRAP 13.3 INCHES FROM 7075-T6 .100 AND TEE FILLER FROM BAC1505-100797SDR DHL2005742509Floorbeam · corrodedAFT PIT CEILING, CABIN FLOORBEAM BS 1070 LOWER SURFACE HAS CORROSION AT RBL 16. REMOVED CORRODED FLOORBEAM STA 1070 RBL 16 IAW B727 SRM 53-10-8. FABRICATED 2 EACH ANGLES 18 X .9 X .8 INCHES AND 12 X .8 X 1.2 INCHES FROM BAC 1490-2888 AND 1 EACH FILLER FROM 7SDR 05FDEA03185Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BETWEEN STA 560 AND 600 AT LBL 24. REMOVED AND REPLACED SEAT TRACK FROM STA 480 TO 630 AT LBL, 24 IAW FX B727 SRM 53-10-5 FIG 1, 51-10-2 AND 51-30-2.SDR 05FDEA03183Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER SURFACE STA 560 LBL 24-62. REMOVED, FABRICATED, AND REPLACED T-CAP, WEB AND STIFFENER IAW B727 SRM 53-10-8 FIG 3, 51-10-2 AND 51-30-2.
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