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 DL72S951646Frame · crackedAT HMV, COMPLIED WITH SCHEDULED PERMANENT REPAIR TO RT MLG UPLOCK ATTACH FRAME AT FS 910. INSTALLED REPAIRS PER MM 53-11-0 PG 814.SDR DL72S951441Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION AT O/B GALLEY ATTACH TRACK LBL 56 BETWEEN STA 1070 AND STA 1115. REPLACED SEAT TRACK FROM STA 1070 TO STA 1110 PER SRM 53-10-5 FIG 7.SDR CAL950243Duct · rupturedEWR - FLT 0288 - THE NR 1 ENGINE FIRE LIGHT AND BELL ACTIVATED AT CLIMB POWER AND 6,000 FEET. THE NR 1 ENGINE THROTTLE WAS RETARDED AND THE WARNING CEASED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE SDR DL72S951450Angle · crackedFOUND ON CV2 CHECK, ONE INCH CRACK IN ATTACH ANGLE LOWER END OF NR 7 SPOILER ACTUATOR ATTACH FITTING. REPAIR: REPAIRED PER M/M 57-20-22 PAR 10.SDR DL72S951447Skin · crackedFOUND ON CV2 CHECK RT FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED .50 INCH. REPAIR: REPAIRED PER M/M 52-11-0 PG 808.SDR DL72S951446Angle · crackedFOUND ON CV2 NR 8 SLAT ANGLE CRACKED UNDER TELESCOPING TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S951443Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON RT INBD SEAT TRACK STA 380 TO 480. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7.SDR DL72S951442Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON RT CENTER SEAT TRACK STA 344 TO 480. CLEANED TREATED AND PAINTED FROM STA 460 TO 480 PER SRM 53-10-1, FROM STA 344 TO 460 REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7.SDR DL72K951356Slat · crackedCRACK BELOW ANTI-ICE TUBE NR 2 SLAT OPN 5535 AD. FOUND AT B-1 LETTER CHECK. REPAIRED PER MM 57-54-0 FIG 805A.SDR DL72K951355Web · crackedA ONE INCH CRACK ON LIGHTENING HOLE RT SIDE OF TORQUE BOX IN 48 SEC. FOUND AT B-1 LETTER CK. REPAIRED PER MM 53-11-0.SDR DL72K951354Skin · crackedA .5 INCH CRACK RT SIDE OF VERT STAB BELOW AND AFT OF SADDLE PANEL 9501. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3.SDR DL72K951353Skin · crackedA ONE INCH CRACK LT SIDE OF VERT STAB AT STR-6 APPROX FIN STA 160. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3.SDR DL72K951352Skin · crackedA .5 INCH CRACK RT SIDE OF VERT STAB BELOW PANEL 9501. FOUND DURING B-1 LTR CK. REPAIRED PER SRM 55-30-3.SDR DL72S951335Web · crackedVERT WEB CRACKED .625 INCH AT UPPER FASTENER ROW STA 1273, 48 SEC TORQUE BOX. FOUND AT E-2 LTR CK.SDR DL72S951334Skin · crackedA 1.25 INCH CRACK IN VERT STAB SKIN RT SIDE AT CUTOUT FOR PANEL 9501 SADDLE PLATE. FOUND DURING E-2 LR CK. REPAIRED PER SRM 55-30-3 PAMM.SDR DL72S951333Skin · dentedLOWER LEADING EDGE SKIN DENTED 26 INCHES FROM INBORD END. REPAIED LEADING EDGE AS PER THE 727 SRM 57-50-3. FLUSH REPAIR FIGURE ONE. DURING SHOP INSPECTION OF SLAT PANEL.SDR DL72S951579Skin · corrodedCORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN AT STA 950D PLUS 10 BETWEEN STR 28R AND 27R. A 1.625 INCH BY 3.125 INCH CUT OUT IN THE 0.150 INCH BONDED 2024-T3 CLAD SKIN WAS REQUIRED. AN EXTERNAL REPAIR DOUBLER AND TRIPLER WILL BE INSTALLED PER DL ERA 301441SDR DL72S951386Eel Battery · dischargedDURING PREFLIGHT INSP, EMERGENCY EXIT LIGHT AT AF AIRSTAIR INOP. REPLACED BATTERIES OPERATION NORMAL.SDR DL72S951583Skin · corrodedAT CV2 VISIT, CORROSION WAS FOUND JUST AFT OF FS 700 BETWEEN S-28L AND S-28R. CORROSION REQUIRES A 12.5 INCH BY 3.25 INCH CUT OUT AT THIS AREA. REPAIRED SKIN PER DL ERA 301443-14AD.SDR DL72S951582Stringer · corrodedAT THE CV2 VISIT, THE SKIN ON THE LOWER O/B FUSELAGE STR 28R AT STA 1040 THROUGH STA 1052 WAS FOUND CORRODED. REPAIRED PER DL ERA 301444-14.SDR DL72S951326Spar · crackedTHE NR 3 MID FLAP DAMAGED FROM BLOWN TIRE. AFT SPAR RAIL CRACKED IN TWO PLACES AT I/B QUADRANT CUTOUT. REPAIRED PER MM 57520 FIG 802. SPLICED IN NEW RAIL SECTION.SDR DL72S951312Rib · crackedTHE NR 4 L/E SLAT RIB CRACKED .5 INCHES O/B SIDE. FOUND DURING A-2 LTR CHECK. REPAIRED PER MM 57-54-0 PG 803.SDR DL72S951311Skin · crackedA FIVE INCH CRACK AT LOWER SKIN OF LT ELEV SKIN O/B SIDE. FOUND DURING A-2 LTR CK, TPAMM 3/28/95. REPAIRED PER SRM 55-20-3 FIG 5.SDR DL72S951310Skin · crackedFOUND DURING E-2 LETTER CHECK, BOLT SHEARED AND UPPER SKIN WEDGE CRACKD 1 INCH NR 6 SLAT I/B GUIDE HOOK. REPAIRED PER SRM 57-50-3 FIG 10.SDR DL72S951339Skin · corrodedFOUND DURING CV-2 CHECK, CORROSION ON BELLY SKIN FROM STA 580 TO 600 BETWEEN STR 8R AND O/B INTERCOSTAL. REPAIRED PER SRM 53-30-3 FIG 3.SDR DL72S951259Doubler · crackedDURING SHOP INSPECTION, DOUBLER ON RIB NR 11 AND 12 WERE FOUND CRACKED INSIDE SLAT PANEL. REPAIRED PER MM 57-54-00.SDR DL72L951257Slat · crackedA .375 INCH CRACK EMANATING FROM I/B STOP PAD NR 7 SLAT. FOUND DURING C-1 LETTER CHECK, TPAMM 3-24-95. REPAIRED PER MM 57-54-0 PG 816.SDR DL72S951785Skin · wornNR 2 AFT FLAP, UPPER L/E SKIN WORN AT I/B END. REPAIRED PER SRM 575004, MFG'D AND INSTALLED FILLER AND DOUBLER.SDR DL72S951246Web · crackedFOUND DURING A-2 LETTER CHECK, CRACK IN LT TORQUE BOX SKIN .5 INCH LONG AT UPPER RIVET ROW ABOVE FWD LIGHTENING HOLE. ALSO,A .125 INCH CRACK AT UPPER FWD LIGHTENING HOLE LT SIDE VERT STAIRWAY. REPAIRED PER B727 MM 53-11-0 PG 832.SDR DL72S951679Nose Cowl · crackedOUTER FRAME AND BULKHEAD DAMAGED UNDER TEMP. REPAIR AT 3 O'CLOCK POSITION. DAMAGE WAS REPAIRED PER B-727 SRM 54-10-3 FIG 3 FOR NR 3 ENGINE NOSE COWL, DURING SHOP INSPECTION.SDR DL72S951357Skin · crackedDURING THE INITIAL INSPECTION, THE NR 5 LEADING EDGE SLAT, THE AFT HOLE ON THE OUTER SKIN WHERE THE FENCE IS MOUNTED WAS FOUND TO HAVE A .5 INCH LONG CRACK BESIDE IT. THE SKIN WAS REPAIRED PER MM 57-54-0 FIG 813.SDR DL72S951322Angle · crackedDURING INITIAL INSPECTION, OF THE NR 5 LEADING EDGE SLAT, THE LOWER AFT ANGLE AT THE O/B END WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED PER MM 57-54-0 FIG 805A.SDR DL72S951221Bullnose · crackedCRACK AT I/B BULLNOSE HINGE ATTACH POINT, NR 4 KRUGER FLAP. REPAIRED PER SRM 57-50-3 PG 32.SDR DL72K951306Skin · dentedDURING A SHOP INSPECTION, A DENT IN THE LEADING EDGE WAS FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS. A REPAIR WAS INSTALLED PER SRM 57-50-3. RT WING NR 6 L/E SLAT.SDR DL72K951305Rib · crackedDURING A SHOP INSPECTION, TWO RIBS WERE FOUND TO BE CRACKED. ITEM NR 1 RIB NR 16 RIB CRACKED, A REPAIR WAS INSTALLED PER SRM 57-50-3. ITEM NR 2 RIB NR 17 CRACKED. A REPAIR WAS INSTALLED PER 57-50-3. RT WING NR 6 L/E SLAT.SDR DL72K951304Rib · crackedDURING SHOP INSPECTION, A RIB WAS FOUND TO BE CRACKED IN RT WING NR 6 L/E SLAT. REPAIRED PER MM 57-54-00.SDR DL72K951284Rib · crackedDURING SHOP INSPECTION, ITEM NR 1 AND NR 2 CRACKS WERE FOUND IN RIBS OF NR 6 SLAT. REPAIRS WERE INSTALLED PER MM 57-54-0.SDR DL72S951584Anti-Ice Duct · crackedWHILE IN SHOP 380, THE NR 4 KRUEGER FLAP ANTI-ICE DUCT TORQUE TUBE WAS FOUND WITH TWO CRACKS EXTENDING FROM AN EXISTING CUT OUT LOCATED 22.5 INCH FROM THE I/B EDGE OF THE FLAP. REPAIRED PER DL ERA 270445-14.SDR DL72S951338Seat Track · corrodedFOUND DURING CV-2 CHECK, CORROSION ON LT CENTER SEAT TRACK STA 1040 TO 1137. FOUND WITHIN LIMITS FROM 1190 TO 1137 PER SRM 53-10-1. REPLACED SEAT TRACK FROM 1030 TO 1090 PER SRM 53-10-5 FIG 7.SDR DL72S951337Seat Track · corrodedFOUND DURING CV-2 CHECK, CORROSION AT GALLEY ATTACH TRACK BETWEEN STA 344 AND 460 RBL 44. REPLACED SEAT TRACK FROM STA 344 TO 360 AND STA 410 TO 460. FOUND WITHIN LIMITS FROM 360 TO 440 PER SRM 53-10-1.SDR CAL950224Hyd Coupling · brokenIAH - FLT 0650 - BOTH B-HYDRAULIC SYSTEM PUMP LOW PRESSURE LIGHTS ILLUMINATED WITH A DROP IN HYDRAULIC QUANTITY WHILE IN-FLIGHT TO IAH. HYDRAULIC QUANTITY LOSS CHECK LIST WAS COMPLIED WITH AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND QUICK DISCONNSDR DL72S951315Skin · crackedLOWER SKIN TO RIB ATTACH ANGLE CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED PER SRM 57-54-0. DURING SHOP INSPECTION, OF NR 7 L/E SLAT.SDR DL72S951314Rib · crackedA CRACK IN RIB NR 13. REPAIRED PER MM 57-54-0 PG 819.SDR DL72S951179Stiffener · crackedFOUND DURING A-1 LETTER CHECK - .50 INCH CRACK AT NR 6 SLAT STIFFENER AT COVE PANEL BELOW ANTI-ICE T-DUCT. REPAIRED PER M/M 57-54-0 PG 807A.SDR DL72S951177Skin · crackedFOUND DURING A-1 LETTER CHECK - 48 SEC TORQUE BOX SKIN CRACKED .3750 INCH AT A LIGHTNING HOLE RT SIDE STA 1323. INSTALLED DOUBLER PER M/M 53-11-0.SDR DL72S960394Web · crackedDURING INSPECTION, FOUND THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL CRACKED BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. THE CRACK IS APPROXIMATELY 1.75 INCH IN LENGTH. IN ACCORDANCE WITH S/B 727-53-145, THE WEB WAS TRIMMED OUT AND A REPAIR DOUBLER ASDR DL72S951303Rib · crackedA CRACK IN NR 10 RIB LOWER AFT CORNER. REPAIRED PER MM 57-54-0. ALSO, A CRACK IN NR 11 RIB LOWER FWD CORNER. REPAIRED PER MM 57-54-0. DAMAGE FOUND AT SHOP INSPECTION, OF NR 7 SLAT.SDR DL72S951139Skin · crackFOUND DURING E-1 LETTER CHECK, SKIN CRACKED .5 INCH VERTICAL STAB LT SIDE BELOW ACCESS PNL 9501. REPAIRED PER SRM 55-30-3 FIG 1.SDR DL72S951138Web · crackFOUND DURING E-1 LETTER CHECK, 3 LIGHTNING HOLES CRACKED VERTICAL WEB LT TORQUE BOX STA 1223, 1 EA LIGHTNING HOLE CRACKED VERTICL WEB RT TORQUE BOX 48 SEC STA 1323. REPAIRED PER M/M 53 -11 - 0 PG 828.SDR DL72S951137Slat · crackFOUND DURING E-1 LETTER CHECK, 2 INCH BY .25 INCH CRACKS BELOW ANTI-ICE TUBE ON NBR 2 L/E SLAT. REPAIRED PER MM 57-54-0 PG 807A.
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