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 DL72S952903Stringer · corrodedFOUND ON CV2 CHECK, CORROSION AT STR 28L STA 1050. REPAIRED PER SRM 53-30-3 FIG 1, IDENTIFIED AS A PERMANENT REPAIR PER PS 900-5-1 NR 4.SDR DL72S952885Web · crackedWEB CRACKED AT STR 16L STA 360. REPAIRED PER SRM 53-10-4 PG 14.SDR DL72S952870Skin · crackedRT HORIZONTAL STABILIZER I/B EDGE OF UPPER SKIN BENT AND CRACKED WHERE SEAL ATTACHES AT CENTER BOX AREA, BETWEEN FWD AND AFT SPAR. REPAIRED PER SRM 55-10-3 FIG 4.SDR DL72S952860Floorbeam · corrodedFOUND ON CV2 CHECK, CORROSION AT FLOORBEAM STA 312 LBL 25. REPAIRED AS PER ERA 302020-14.SDR DL72S952859Floorbeam · crackedFOUND ON CV2 CHECK, FLOORBEAM CRACKED AT FLOOR PANEL SCREW HOLE STA 344 8 INCHES OUT LBL 25. REPAIRED PER SRM 53-10-8 FIG 8.SDR DL72S952846Eel Wire · shortedDURING CRUISE, HAD EMERGENCY LIGHTS COME ON WHEN SWITCH IN ARMED POSITION. THE EMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER TRIP. FOUND WIRES 9004-20 AND 9010-20 SHORTED. REPAIRED WIRES AND REPLACED LITGHT SWITCH AND BATTERY IN 9027. OPERATION NORMAL.SDR DL72S952844Valve · failedON CLIMBOUT, HAD NR 2 ENGINE START VALVE LIGHT ILLUMINATE. PER CHECKLIST, ENGINE WAS SHUTDOWN. FOUND NR 2 ENGINE START VALVE WITH SOLENOID SEPARATED FROM HOUSING. REPLACED VALVE, OPERATION NORMAL.SDR DL72S953269Connector · looseDURING CRUISE, WIRING CONNECTION AT TOP LEFT CORNER OF L-1 WINDSHIELD BEGAN TO SPARK AND BURN. SHUT OFF POWER ARCING STOPPED. FOUND TERMINAL CONNECTION VERY LOOSE. REPLACED TERMINAL DUE TO ARCING DAMAGE. OPERATION NORMAL.SDR DL72S953081Skin · crackedDURING HMV, FOUND CRACK IN SKIN INSIDE NR 2 ENG INLET S-DUCT. REPAIRED PER SRM 54-10-3 FIG 13.SDR DL72S953049Stringer · crackedSTR 15L CRACKED AT FWD SIDE OF LT WING L/E ILLUMINATION LIGHT. REPAIRED PER SRM 53-10-3 FIG 2. FOUND AT HMV.SDR DL72S953047Skin · damagedAT HMV, FOUND TIME LIMITED REPAIR ON FUSELAGE SKIN AT RT FWD CORNER OF VENTRAL STAIR CUTOUT. INSTALLED NEW REPAIR PER MM 53-30-0 PG 803-804 FIG 802.SDR DL72S953046Skin · gougedSKIN GOUGED FS 682 BETWEEN STR 21R AND 22R. REPAIRED PER SRM 53-30-3 FIG 3A.SDR DL72S952970Foreflap · crackedFOUND ON CV2 CHECK, CRACK RIGHT WING OB FOREFLAP AT FLAP TRACK. REPAIR: REPAIRED PER SRM 57-50-4.SDR DL72S952961Skin · crackedSKIN CRACKED, .50 INCH CRACK IN VERT STAB SKIN RT SIDE AT FRONT SPAR AREA BELOW PANEL 9501. REPAIRED PER SRM 55-30-3 FIG 2, AT HMV.SDR DL72S952907Stringer · crackedDURING HMV, FOUND AFT TAB OF VENT BOX STR 11 CRACKED AT WS 519.00. REPAIRED PER M/M 57-13-0.SDR DL72S952869Skin · damagedAT HMV, FOUND TIME LIMITED REPAIR RT SIDE VERTICAL STAB SKIN AT TORQUE BOX AREA. INSTALLED PERMANENT REPAIR PER MM 55-30-0 FIG 801.SDR DL72S952868Skin · damagedREPAIR UNIDENTIFIED RT O/B AILERON UPPER SKIN HAS PREVIOUS TIME LIMITED REPAIR. INSTALLED PERMANENT REPAIR PER SRM 57-50-5 PG 2.SDR DL72S952821Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S952820Rib · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT L/E RIB CRACKED, .5 INCH I/B OF ACTUATOR MOUNT. REPAIRED PER MM 57-54-0 PAR 3.SDR DL72S952819Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.SDR DL72S952818Web · crackedFOUND DURING A-1 LETTER CHECK, 1 INCH CRACK IN RT WEB OF 48 SEC LOCATED AT STA 1226 LWR LIGHTNING HOLE. A .25 INCH CRACK IN RT WEB OF 48 SEC LOCATED AT STA 1233. REPAIRED PER M/M 53-11-0 PAR 16.SDR DL72S953050Stringer · corrodedCORROSION ON STR 28R STA 495 FWD B/B. REPAIRED PER SRM 53-10-3 PG 3. FOUND AT HMV.SDR DL72S953590Spar Rail · crackedFASTENER ELONGATED ON LOWER SURFACE T/E SEAL RETAINER ATTACH ANGLE, LOWER AFT SPAR ANGLE. REPAIR DOUBLER CRACKED, APPROX 2 INCH CRACK IN AFT SPAR RAIL, 56 INCHES FROM I/B END OF FLAP. ALL THREE AREAS WERE REPAIRED BY REPLACING SPLICING IN NEW SPAR RAIL AS PESDR DL72S953430Spar · crackedTHE NR 2 MIDFLAP AFT LOWER SPAR RAIL CRACKED 56 FROM I/B END OF FLAP. REPAIRED PER M/M 575200 P807, SPLICED IN NEW SECTION OF SPAR RAIL. FOUND AT SHOP VISIT.SDR DL72S953890Heat Shield · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACK IN HEAT SHIELD AT RIVETS BETWEEN RIBS NR 5, 6, 7, 10 AND 11. REPAIRED PER MM 57-54-0 FIG 814.SDR DL72S953889Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKING IN THE I/B AND O/B SUPPORT RIBS, FOR BOTH I/B AND O/B SLAT TRACK ATTACH FITTINGS. ACCOMPLISHED REPAIRS PER MM 57-54-0.SDR DL72S953888Ribs · crackedDURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH RIBS NR 11 AND NR 13 CRACKED. REPAIRED PER MM 57-54-0.SDR CAL950531Regulator · inoperativeLAX - FLT 0418 - AIRCRAFT LOST CABIN PRESSURE WHILE AT 33,000 FEET EN ROUTE FROM SFO TO LAX. CABIN PRESSURE COULD NOT BE CONTROLLED IN STAND-BY A.C. OR D.C. MODES AND RT PACK COULD NOT BE RESET. OXY MASKS DEPLOYED AND AIRCRAFT WAS DIVERTED TO LAX WHERE IT LASDR DL72S953143Angle · cracked1.0 CRACK IN ANGLE OF FWD BEAM OF THE RT TORQUE BOX, FS 1263. REPAIRED PER DL ERA 301959-14.SDR DL72S952738Stiffener · crackedFOUND DURING E-1 LETTER CHECK, WING SPAR STIFFENER AT NR 6 LE SLAT I/B TRACK O/B SIDE HAS 1 INCH CRACK FROM BOTTOM. REPAIRED PER M/M 57-20-21.SDR DL72L954126Skin · crackedDURING SHOP INSPECTION, RIGHT WING OUTBOARD AILERON WAS FOUND WITH DENTED UPPER SKIN AT 37 INCHES FROM I/B END AND OVERSIDE HOLE SKIN TO RIB FASTENER HOLE AT 2ND FROM I/B RIB. REPAIRED PER SRM 57-50-5, FIG 2.SDR DL72S953754Panel · crackedTHE INBOARD AFT PUSHROD CUT-OUT HAS A CRACK AT INBOARD AFT CORNER. REPAIRED PER M/M 57-52-0, PAGE 819. FOR NR 3 MID-FLAP PANEL DURING SHOP INSPECTION.SDR DL72S952910Skin · damagedDURING A SHOP INSPECTION, THE SKIN ON THE LOWER INBD SECTION WAS FOUND TO HAVE SEVERAL DENTS AND ELONGATED HOLES, IN WHICH RIVETS WERE PULLING THROUGH. A SKIN SPLICE REPAIR WAS INSTALLED PER THE M/M 57-51-0 FOR THE LEFT OUTBOARD AILERON.SDR DL72S952852Skin · damagedDURING A SHOP INSPECTION, THE LOWER OUTBOARD SKIN WAS FOUND TO HAVE SEVERAL FASTENERS PULLING THROUGH THE SKIN. A REPAIR WAS INSTALLED PER THE M/M 57-51-0, FOR LEFT OUTBOARD AILERON.SDR DL72S952718Pack · overheatON SHORT FINAL AND LANDING, HAD LEFT PACK OVERHEAT WITH SOME BURNING ODOR IN CABIN. FOUND COOLING FAN C/B TRIPPED. RESET C/B OPERATION TEST, NO TROUBLE FOUND, RETURNED TO SERVICE.SDR DL72S952713Fitting · pittedDURING SCHEDULED TRIPLE LANDING GEAR CHANGE FOUND LT AND RT NOSE GEAR TRUNNION CAPS AND BEARINGS WORN AND PITTED. REPAIRED PER M/M 53-40-0.SDR DL72K952654Angle · crackedFOUND DURING A-2 LETTER CHECK, ANGLE AT STA 910 CRACKED. REPAIRED PER M/M 53-11-0 PAR 20.SDR DL72K952653Angle · crackedFOUND DURING A-2 LETTER CHECK, NR 4 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72K952652Skin · crackedFOUND DURING A-2 LETTER CHECK, NR 2 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72K952651Skin · crackedFOUND DURING A-2 LETTER CHECK, NR 1 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 12.SDR DL72K952650Web · crackedFOUND DURING A-2 LETTER CHECK, 2 CRACKS TORQUE BOX WEB UPPER ROW OF RIVETS FWD SIDE RT. REPAIRED PER MM 53-11-0 PAR 19.SDR CAL950493Sensor Wire · brokenIAH - FLT 0775 - OVERRIDE WAS REQUIRED TO RETRACT THE LANDING GEAR AFTER TAKEOFF FROM SJO. REPLACING THE LANDING GEAR LEVER LOCK SOLENOID DID NOT HELP. MAINTENANCE FOUND A BROKEN WIRE TO THE LEFT GEAR SAFETY SENSOR. THE WIRE WAS REPAIRED. AN OPERATIONAL CHSDR DL72S952646Skin · crackedCOVE SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT NR 2 SLAT, FOUND DURING E-1 LETTER CHECK. REPAIRED PER M/M 57-54-0 PG 80.SDR DL72S952645Angle · crackedFOUND DURING E-1 LETTER CHECK, COVE SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT AT NR 3 SLAT. REPAIRED PER M/M 57-54-0 PG 807A.SDR DL72S953914Fairing · crackedAFT MOUNT HOLES ENLARGED, WELDED AS PER MM 57-52-0 2. CRACK IN CLOSEOUT PANEL UNDER GUIDE PIN. REPAIRED PER SRM 51-40-2. REPAIRS FOUND AT SHOP INSP FOR AFT O/B FLAP TRACK FAIRING.SDR DL72S952612Skin · crackedFOUND ON A2 LTR CK, 1.125 INCH CRACK VERTICAL STABILIZER SKIN LT SIDE STA 110.400 S-9. REPAIR INSTALLED DOUBLER PER SRM 55-30-3.SDR DL72S952605Nose Cowl · crackedFOUND DURING A-2 LETTER CHECK, NOSE COWL AFT WEB CRACKED 6 INCHES AT 5 O'CLOCK POS/AFT WEB DOUBLER CRACKED 2 INCHES 5:30 POS. REPAIRED PER SRM 54-10-3 FIG 3.SDR DL72S952604Skin · crackedFOUND DURING A-2 LETTER CHECK, 7.25 INCH CRACK LT ELEVATOR UPPER SKIN ELEVATOR STA 120.00. REPAIRED PER SRM 55-20-3 AND ID PER PS 900-5-1 NR 4.SDR DL72S952587Spar · crackedDURING SHOP INSPECTION, THE LOWER FORWARD SPAR CAP WAS FOUND CRACKED 8 FEET FROM THE INBOARD EDGE. THE SPAR WAS REPAIRED PER SRM 55-20-5.SDR DL72K952948Blkhd Web · crackedSEVERAL CRACKS WERE FOUND IN FS 1183 BULKHEAD WEB AND STIFFENERS AFTER AIRCRAFT FAILED TO PRESSURIZE IN BOS. A 4 INCH LONG L-SHAPED CRACK WAS FOUND IN FS 1183 BLKHD WEB AT LBL 46.9 AND WL 213.67. THE LBL 46.93 VERTICAL STIFFENER HAD MULTIPLE CRACKS WITH MAXI
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