Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72S971237Skin · crackedAT HMV, A CRACK WAS FOUND AT NR 3 SLAT AT RIB 4. THIS WAS REPAIRED PER MM 57-54-0 PG 801.SDR DL72S971171Floorbeam · corrosionCORROSION FOUND AT NUTPLATE HOLE ON FLOORBEAM STA 344 AND LBL 45. REPAIRED PER SRM 53-10-8, FIG. 11.SDR DL72S971167Rib · crackedFOUND ON A1 LETTER CK, .75 IN CRACK IN RADIUS OF NR 6 SLAT RIBS I/B AND O/B SIDES OF ACTUATOR AT COVE SKIN ATTACH. REPAIRED PER MM 57-54-0.SDR CALA9701036Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 480 FROM RBL 46 TO SIDEWALL. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3.SDR CALA9700961Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 720F, BL 0. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR DL72S971131Web · cracked.5 INCH CRACK IN TORQUE BOX LIGHTENING HOLE RT SIDE APPROX STA 1230. REPAIRED PER M/M 53-11-0 PG 828.SDR CALA9700960Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN WEB BELOW CABIN FLOOR TRACK AREA AT BS 885, RBL 45. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700959Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 277, RBL 12. A REPAIR WAS INSTALLED IAW SRM 51-10-1.SDR DL72S971115Battery Pack · dischargedAFT STAIRWAY EMERGENCY LIGHT INOP. REPLACED BATTERIES IN PACK. CKS NORMAL.SDR DL72S971111Accessory Unit · failedBOTH PACKS OVERHEATED AND SMOKED CABIN. PACK FAN CONTROL C/B POPPED AND WOULD NOT RESET. REPLACED LANDING GEAR ACCY UNIT.SDR DL72S971110Fan · shortedSTRONG ELECTRICAL FUMES IN ACFT, COINCIDING WITH GASPER FAN C/B POPPED. REPLACED GASPER FAN, CKS OK.SDR DL72K971106Hyd Syst · leakingA-SYSTEM HYDRAULICS OVERHEAT CAME ON. FOLLOWED ABNORMAL PROCEDURE, LIGHT STAYED ON.SDR CALA9701035Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 BETWEEN RBL 25 AND RBL 46. THE CORROSION WAS REMOVED. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9701034Floorbeam · corrodedINSPECTION FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 344, LBL 30. THE CORRODED SECTION WAS CUT OUT. A BEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700958Floor Track · corrodedINSPECTION FOUND FLOOR TRACK CORRODED AT BS 400 TO 440, RBL 46. THE FLOOR TRACK WAS REMOVED, A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9700957Floor Track · corrodedINSPECTION FOUND FLOOR TRACK CORRODED AT STA 1110 RBL 25. THE TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9700947Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 8 AND STRINGER 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.SDR CALA9700946Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 2 AND STRINGER NR 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.SDR DL72S971149Skin · corrosionTHE FUSELAGE SKIN HAS A 2.3 BY 2.6 CUTOUT FOR A CORROSION REPAIR AT STA 535 BETWEEN STR 26R AND 27R. THE CUTOUT IS NEXT TO STR 27R BELOW THE LAP JOINT. THE REPAIR WAS APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DTD 6-5-97.SDR DL72S971098Skin · crackedA .5 INCH CRACK EMPENNAGE SKIN LT SIDE FWD OF SADDLE PLATE 9501. REPAIRED PER M/M 54-30-0 FIG 801, TIME LIMITED REPAIR.SDR CALA9701039Skin · crackedINSPECTION FOUND THREE 1 CRACKS AT LT WHEEL WELL KEEL BEAM SKIN AT FORWARD END OF APU CUTOUT, JUST AFT OF BS 870. THE CRACKED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND ECRA 5310-03522.SDR CALA9701037Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN MID UPPER AFT LT WING STRINGER AT RIB STATION 629. THE CRACK WAS STOP DRILLED. THE STRINGER WAS REPAIRED IAW BOEING SERVICE BULLETIN 57A159.SDR CALA9700962Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING STRINGER JUST FORWARD OF FUEL DUMP LINE AT STA 656.50. A REPAIR WAS FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-57A159.SDR CALA9700951Stringer · corrodedINSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED AT STA 720E. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A STRINGER AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.SDR CALA9700949Floorbeam · crackedINSPECTION FOUND A .5 INCH CRACK COMING FROM LIGHTENING HOLE IN FLOORBEAM AT BS 825, LBL 54. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700948Floorbeam · crackedINSPECTION FOUND A .5 AND .3125 INCH CRACK OUT OF LIGHTENING HOLE OF FLOORBEAM AT BS 825, RBL 49. THE CRACK WAS STOP DRILLED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700956Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 720A BETWEEN STRINGER 27R AND 28R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9701032Skin · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT SKIN BETWEEN STRINGER 27 AND 28 AT STA 720D CORRODED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700963Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 424, RBL 45. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.SDR CALA9700955Stringer · corrodedINSPECTION FOUND STRINGER S28R IN FORWARD CARGO COMPARTMENT CORRODED AT STA 620. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 1.SDR CALA9700954Clip · crackedINSPECTION FOUND A .5 INCH CRACK IN S28L TIE CLIP AND A .5 INCH CRACK IN S28R TIE CLIP AT STA 460. REPLACEMENT TIE CLIPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-30-2, AND 51-10-3.SDR DL72S971109Floorbeam · corrosionCORROSION ON FLOORBEAM AT STA 344 AND RBL 1. REPLACED SECTION OF BEAM PER SRM 53-10-8 FIG 11.SDR CALA9701038Spar · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING FRONT SPAR UPPER CHORD AT STA 335. THE CRACKED SECTION WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5710-01819 AND SRM 57-10-6.SDR CALA9701033Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT BOTTOM OF WINDOW POST AREA BETWEEN FIRST OFFICER'S WINDSHIELD AND SLIDING WINDOW. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 8.SDR CALA9701031Skin · dentedINSPECTION FOUND A DENT IN RT FUSELAGE SKIN AT STA 1086 TO 1093 BETWEEN STRINGER 21R AND 22R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9701030Bulkhead · crackedINSPECTION FOUND A 2.5 INCH CRACK IN BULKHEAD AT APU LOAD CONTROL CUTOUT, BS 870. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01544.SDR CALA9700953Skin · crackedINSPECTION FOUND A .1875 INCH CRACK IN FUSELAGE SKIN WITH CORROSION AT LAP SEAM BS 600, STRINGER 26L. THE CORROSION WAS REMOVED AND THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700952Skin · crackedINSPECTION FOUND .0625 INCH CRACKS AROUND RIVET HEADS OF FUSELAGE SKIN AT LAP SEAM 26L BETWEEN BS 575 TO 588. THE CRACKED AREA OF SKIN WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700950Skin · corrodedINSPECTION FOUND FUSELAGE SKIN BULGING WITH TWO FASTENERS POPPED AT LEFT LAP SEAM 26L BETWEEN BS 700 TO 715. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR DL72S971223Spar Web · crackedTHE CENTER SPAR WEB WAS FOUND CRACKED IN TWO PLACES. THE FIRST LOCATION IS APPROX .75 INCH LONG LOCATED APPROX 25 INCHES FROM I/B END AT THE FOREFLAP CUTOUT NEAR THE UPPER I/B CORNER. THE OTHER CRACK WAS 51 INCHES FROM THE I/B END AT THE I/B CARRIAGE SUPPORTSDR DL72K971051Battery · dischargedRIGHT OVERWING EMERGEMCY EXIT SIGNS INOP. REPLACED BATTERY PACK, CHECKS NORMAL.SDR DL72K971050Battery · dischargedR1 EMERGENCY OVHD EXIT LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.SDR DL72S971043Spar · wornRT O/B AILERON REAR O/B SPAR WORN. INSTALLED REPAIR DOUBLER PER SRM 51-40-03.SDR DL72S971042Skin · loose rivetsRT O/B AILERON SKIN HAD LOOSE RIVETS ON UPPER SKIN. INSTALLED NEW SKIN SECTION REPAIR PER SRM 57-50-5.SDR DL72S971040Uplock Actuator · malfunctionedAFTER GEAR EXTENSION, 'A' HYD QTY WENT TO ZERO (NOSE GEAR REQUIRED MANUAL EXTENSION). POM PROCEDURES COMPLIED WITH AND A FLAP 15 LDG ACCOMPLISHED. REPLACED NOSE GEARLOCK ACTUATOR PER M/M. SERVICED HYD FLUID, RETRACTED NOSE GEAR SEVERAL TIMES AND OPS NORMAL.SDR DL72L971034Batteries · dischargedF/C MEGAPHONE INOP. REPLACED BATTERYS, CK NORMAL.SDR 97FDEA00312Fire Detection · failed97-0097 13 MINS INTO FLT, ENG NR 1 FIRE DETECTION FAULT IND LIGHT ILLUMINATED WITH NO OTHER FIRE INDICATIONS. IAW RED TABS, FOUND LOOP A FAULTY AND COMPLETED REMAINDER OF FLT IN LOOP B. REPEAT GRIPE AGAIN. AC RELEASED FOR SERV PER MEL/COL:26-6B CATEGORY: C SDR DL72S971004Brakes · damagedNUMBER 3 BRAKE OVERHEATED AND CAUGHT FIRE AFTER LANDING. REPLACED BRAKE AND WHEEL ASSY NO DAMAGE TO LANDING GEAR OR ANY OTHER PART OF AIRCRAFT.SDR DL72S971013Vertical Web · crackedFOUND VERTICAL WEB CRACKED AT STA 1303 ON LT SIDE OF S-DUCT VIEWED FROM 48 SECTION. REMOVED CROSS SECTION REPAIRED PER SRM 58-10-4, FIG 17.SDR 97FDEA00307Fire Detector · failed97-0094, NR 1 ENGINE FIRE LIGHT BELL AND DETECTOR FAULT LIGHT ILLUMINATED IN FLIGHT FOR 5 SECONDS. DETECTOR SYSTEM WAS IN LOOP-A AS PER MINIMUM EQUIPMENT LIST. LOOP-B FAILED TEST, NO OTHER ABNORMAL ENGINE INDICATIONS. REMOVED AND REPLACED FIRE DETECTOR ELEM
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