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 DL72S953147Frame · interferenceDURING INSTALLATION OF THE MODIFICATION TO THE LT STA 760.95 FRAME, AS REQUIRED PER AD 94-02-04 AND BOEING S/B 727-53-0197, A 0.125 INCH UNIDENTIFIED SHIM, BELOW WL 210 BETWEEN THE FRAME WEB AND THE 65-24546-3 LOWER CHORD OF THE FLOOR BEAM AND THE 69-18474-1 TSDR DL72S953053Angle · crackedA .5 AND .25 CRACK ON NR 7 SLAT SUPPORT ANGLE BELOW TAI DUCT. FOUND DURING D-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.SDR DL72S953052Angle · crackedNR 3 SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. FOUND DURING D-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.SDR DL72S953148Angle · crackedCRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND THE AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER ERA 302109-14AD.SDR DL72S953035Angle · crackedNR 7 SLAT COVE SKIN ANGLE DOUBLER CRACKED AT I/B STOP PAD. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0.SDR DL72S953034Angle · crackedNR 7 SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0.SDR DL72S953018Skin · crackedFOUND DURING A-2 LETTER CHECK, NR 6 SLAT COVE SKIN ANGLE, UNDER TAI DUCT CRACKED. REPAIRED PER SRM 57-54-0.SDR DL72S953017Skin · crackedFOUND DURING A-2 LETTER CHECK, CRACK IN LWR COVE SKIN SUPPORT ANGLE, BELOW TAI DUCT ON NR 3 SLAT. REPAIRED PER SRM 57-54-0.SDR DL72K953058Tube · crackedDURING CRUISE, HAD LOSS OF B-SYSTEM HYDRAULIC FLUID AND PRESSURE. FLIGHT DIVERTED TO JFK. FOUND CRACKED LINE FROM PUMP TO FILTER HOUSING. REPLACED LINE, PUMPS AND FILTERS, RETURNED TO SERVICE.SDR DL72K953019Skin · crackedA CRACK IN NR 3 L/E FLAP I/B EDGE, 1 INCH FROM LIP. FOUND DURING A-2 LTR CK TPAMM. REPAIRED PER MM 57-53-0 PG 804.SDR DL72S953337Skin · corrodedDURING CV-2 INSPECTION, THE SKIN WAS FOUND DAMAGED IN TWO PLACES ALONG STA 480 TO 500. ONE WAS FOUND AT STR 28L AND THE OTHER NEAR STR 27L. THE DAMAGE WAS REMOVED TO LEAVE TWO CUTOUTS MEASURING 17 BY 2.5 AND 16.375 BY 1.125. AN EXISTING REPAIR IS LOCATED JSDR DL72S953102Skin · crackedDURING HMV INSPECTION, FOUND THE FUSELAGE SKIN BEHIND STRINGER 18A HAD A .3750 INCH CRACK AT BS 948. THE CRACK EMANATES FROM THE LOWER FASTENER ROW OF THE STR 18A ATTACHMENTS AND PROGRESSES DOWNWARD TO EDGE OF THE SKIN. THERE WAS ALSO INDICATION OF A CRACK PSDR DL72S952982Skin · crackedCRACKS COMING OUT OF FASTENERS, FASTENER HOLES ON LEFT AND RIGHT SIDE OF SADDLE FAIRING NR 2 INTAKE VERTICAL STAB PANEL. FOUND DURING B-2 LTR CK. REPAIRED PER SRM 54-30-0.SDR DL72S952981Anti Ice Duct · crackedANTI-ICE DUCT CRACKED 22 INCHES FROM OUTBOARD END. REPAIRED PER SRM 57-50-03, FIG 12, AT HMV SHOP VISIT FOR WING L/E KRUGER FLAP.SDR DL72S953628Skin · dentedDURING A LAYOVER IN CMH, THE SKIN FROM FS 259.5 TO 294.5 WAS DENTED FROM CONTACT WITH A SERVICE TRUCK. THE PERMANENT REPAIR WILL BE INSTALLED IN ACCORDANCE WITH B727 SRM 53-10-4, FRAME STA 278, 53-10-3 FIG 2, STR 20R, 53-10-4 FIG 11, FRAME 294, 53-30-3 FIG 24SDR DL72S953150Frame · crackedFORWARD FRAME OF C-2 CARGO OPENING FOUND CRACKED. REPAIRED PER DL ERA 302087-14AD.SDR DL72S952955Fitting · crackedLEFT WING - REF OPN 5522. HFEC INSP ON BORE OF AFT TERMINAL FITTING SHOWS CRACK INDICATION AT 6 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7, FIG 1.SDR DL72S952944Stiffener · crackedFOUND DURING F-1 LETTER CHECK - L/E WING SPAR STIFFENER CRACKED AT NR 3 SLAT O/B TRACK O/B LEG. REPLACED WING SPAR STIFFENER PER M/M 57-20-21.SDR DL72S952943Stiffener · crackedFOUND DURING F-1 LETTER CHECK - I/B L/E SPAR STIFFENER CRACKED AT NR 5 SLAT TRACK. REPLACED WING SPAR STIFFENER PER M/M 57-20-21, PG 813.SDR DL72S952942Slat · crackedFOUND DURING F-1 LETTER CHECK - .75 INCH CRACK BELOW NB 8 SLAT O/B STOP PAD. REPAIRED PER MM 75-54-0.SDR DL72S952941Skin · crackedFOUND DURING F-1 LETTER CHECK - LWR LT TORQUE BOX SKIN CRACKED .1250 INCH AT LWR FWD LIGHTNING HOLE STA 1223, LWR RT TORQUE BOX SKIN CRACKED .3750 INCH AT LWR FWD LIGHTNING HOLE STA 1223. REPAIRED PER MM 53-11-0.SDR DL72L953205Skin · dentedDURING ROUTINE INSPECTION, NR 7865 WAS WRITTEN FOR A DENT IN LT OUTBOARD AILERON UPPER SKIN. DENT WAS REPAIRED PER SRM 57-50-5.SDR DL72S953051Skin · corrodedCORROSION ON FUS SKIN AT STR 28R STA 495 FWD B/B. REPAIRED PER SRM 53-30-3 FIG 3. FOUND AT HMV.SDR DL72L952919Angle · crackedDURING LETTER CHECK, A 1 INCH CRACK WAS FOUND IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. REPLACED DAMAGED PART IN ACCORDANCE WITH S/B 727-53-0129, REV. 4.SDR DL72S952921Skin · corrodedDURING HMV, CORROSION DAMAGE TO THE SKIN AND STR 27L WAS FOUND IN SEVERAL LOCATIONS BETWEEN STATIONS 600 AND 660. THE SKIN WAS CRACKED AND CORRODED AT APPROX FS 627 AND STR 27L. THERE WAS AN EXISTING EXTERNAL REPAIR AT APPROX FS 620 AND STR 27L. REPAIRED PSDR DL72S952980Blkhd Skin · misdrilledMISDRILLED HOLE AFT SIDE STA 1183 BULKHEAD, RBL 36.83 APPROX 38 INCHES ABOVE FLOOR LINE. HOLE IS DRILLED THROUGH THE SKIN BUT NOT THROUGH THE FRAME. HOLE IS DRILLED NEXT TO AN EXISTING FASTENER AND WAS DRILLED WHILE ACCOMPLISHING EO 4-59821-3. REPAIRED PER SDR DL72S952968Stringer · corrodedFOUND ON CV2 CHECK, CORROSION AT STR 28R, OUTBOARD SIDE JUST FORWARD OF STA 1070. REPAIR: REPAIRED PER ERA 302065-14.SDR DL72S952967Intercostal · corrodedFOUND ON CV2 CHECK, CORROSION AT SKIN FORWARD OF STA 1070 OUTBOARD STR 28R, INBOARD OF INTERCOASTAL. REPAIR: REPAIRED PER ERA 302065-14.SDR DL72S952909Floorbeam · corrodedDURING HMV, FOUND FLOORBEAM CORRODED AT STA 1030 RBL 12 LBL 12. REPAIRED PER SRM 53-10-8.SDR DL72S952863Skin · damagedFOUND DURING B-2 LETTER CHECK - HOLE BURNED THROUGH RT O/B ELEVATOR STATIC WICK BASE. REPAIRED PER SRM 55-20-3, FIG 2 SHT 1.SDR DL72S952856Angle · crackedCOVE SKIN ANGLE CRACKED UNDER NR 3 SLAT TAI DUCT. FOUND DURING B-2 LTR CK. REPAIRED PER 57-54-0, PAR 2.SDR DL72S953238Le Skin · wornDURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT O/B END OF FLAP. REPAIRED PER SRM 57-52-0 PG 808.SDR DL72S953237Le Skin · wornDURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT INBD EDGE OF FLAP. REPAIRED PER SRM 57-52-0 PG 808.SDR DL72S953101Le Skin · damagedNR 4 FOREFLAP LEADING EDGE WAS FOUND WORN 46 INCHES FROM INBOARD END. THE LEADING EDGE WAS REPAIRED PER SRM 57504 BY INSTALLING A DOUBLER.SDR DL72S953100Le Skin · damagedNR 4 FOREFLAP WAS FOUND WITH A TEMPORARY REPAIR ON THE LEADING EDGE 47 INCHES FROM OUTBOARD END. THE DOUBLER WAS REMOVED AND LEADING EDGE REPAIRED PER SRM 57-50-4.SDR DL72S952979Rib · crackedAT HMV, NR 4 SLAT, NR 18 RIB WAS FOUND CRACKED, REPAIRED PER MM 57-54-0, PG 807.SDR DL72S952969Skin · crackedFOUND ON CV2 CHECK, LEFT AFT SERVICE DOOR S/N 506 HAS .75 INCH CRACK AT UPPER HINGE CUTOUT. REPAIR: REPAIRED PER SRM 52-40-2, FIG 4.SDR DL72S952957Skin · crackedSKIN CRACKED, L1 DOOR. THE L1 MAIN ENTRY DOOR HAS EXT SKIN CRACK AT THE LWR FWD CORNER. REPAIRED PER SRM5 2-11-01, FIG 804. FOUND AT HMV.SDR DL72S952954Skin · crackedFRAME CRACKED. THE LOWER FWD CORNER OF THE L1 MAIN ENTRANCE DOOR HAS A 2 INCH CRACK (VIEWED FROM LWR FWD LIGHTING HOLE). REPAIRED PER MM 52011091, PAGE 805.SDR DL72S952935Fitting · corrodedAT HMV, LT FWD TERMINAL PIN BODY FITTING IS CORRODED IN SEVERAL AREAS. REPAIRED PER SRM 57-10-7.SDR DL72S952908Beam · corrodedDURING HMV, FOUND LT MLG WALKING BEAM WITH CORROSION IN BORES OF HOLES FOR MLG ATTACH FITTING. REPAIRED PER SRM 57-40 FIG 1 PG 6 AND 7.SDR DL72S952872Attach Fitting · corrodedLT MLG BEAM HAS CORROSION IN HOLES WHERE O/B ATTACH FITTING BUSHINGS WERE REMOVED. REPAIRED PER SRM 57-40 FIG 1 PG 6 AND 7.SDR DL72S952871Bushing · tornLT MLG BEAM FABROID TORN IN BUSHINGS FOR O/B ATTACH FITTING. REPAIRED PER SRM 57-40, FIG 1.SDR DL72L952840Skin · corrodedCORROSION/RIVET SHEARED STA 1075 STRINGER 27L, FOUND DURING B-2 LTR CK TPAMM. INSTALLED TIME LIMITED REPAIR PER SRM 53-30-3.SDR DL72L952839Angle · crackedNR 2 SLAT COVE SKIN ANGLE BELOW TAI DUCT CRACKED, FOUND AT B2 LTR CK. REPAIRED PER MM 57-54-0.SDR DL72S953048Structure · crackedLIGHTENING HOLE, CRACKED AND BENT ABOVE AND TO THE LEFT OF THE ELEVATOR FEEL COMPUTER. REPAIRED PER SRM 55-10-4 PAGE 3 FIG 2. FOUND AT HMV.SDR DL72S952973Stringer · corrodedFOUND ON CV2 CHECK CORROSION ON OUTBOARD SIDE OF STR 28L BETWEEN STA 480-500. REPAIR: REPAIRED PER ERA 302043-14.SDR DL72S952972Skin · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN OUTBOARD SIDE OF STR 28L BETWEEN STA 480 AND STA 500. REPAIR: REPAIRED PER ERA 302043-14.SDR DL72S952971Stringer · corrodedFOUND ON CV2 CHECK, CORROSION INSIDE STR 27L BETWEEN STA 480-500. REPAIR: REPAIRED PER ERA 302043-14.SDR DL72S952904Stringer · corrodedFOUND ON CV2 CHECK, CORROSION AT STR 28R AFT OF STA 1148 O/B SIDE. REPAIRED AS PER SRM 53-10-3 FIG 1, IDENTIFIED AS PERMANENT REPAIR PER PS 900-5-1 NR 4.
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