Boeing 727-247
Service difficulty reports · 2,669
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 = '727247' 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 = '727247' 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 DL72W960348Attach Box · crackedFOUND DURING F-1 LETTER CHECK, .25 INCH CRACK NR 1 L/E FLAP ACTUATOR ATTACH BOX O/B SIDE. REPAIRED PER MM 57-20-21.SDR DL72W960347Rib · crackedFOUND DURING F-1 LETTER CHECK, 2 INCH CRACK NR 8 L/E SLAT NOSE RIB AT I/B SIDE OF ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-00 PAR 9.SDR DL72W960366Skin · gougedSKIN GOUGED LOWER RUDDER EXT SKIN LT SIDE HAS SEVERAL NICKS AND GOUGES AT AREA OF LETTER 'A' L/E. BLENDED DAMAGE, CHECKED ALLOWABLE LIMITS OF GOUGE, FOUND DEPTH TO BE .019. DRILLED UP DOUBLER, INSTALLED REPAIR PER SRM 55-20-3.SDR DL72W960321Skin · wornDURING INSPECTION, LEFT WING AILERON LOWER OUTBOARD SKIN HAD SEVERAL OVERSIZED AND WORN FASTENER HOLES DUE TO FATIGUE. SPLICED IN NEW SECTION OF SKIN PER MM 57-51-00, FIG 801.SDR DL72W960320Web · crackedDURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 1.25 INCH CRACK AT STA 294.5, APPROXIMATELY AT WL 170. THE DAMAGED PORTION WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAPS WAS INSTALLED IN ACCORDANCE WITH B727-53-145.SDR DL72W960309Angle · crackedA 1.5 INCH CRACK AT NR 1 SLAT ACTUATOR O/B ATTACH ANGLE. REPAIRED PER MM 57 20-21.SDR DL72W960308Bracket · crackedFOUND AT LETTER CHECK, NR 6 L/E FLAP ACTUATOR MOUNT BOX CRACKED, I/B SIDE UPPER AND LWR CORNERS. REPAIRED PER MM 57-20-21.SDR DL72W960307Stringer · crackedA 1 INCH CRACK THROUGH HORIZ LEG OF STR 18A AND STA 950. REPAIRED PER MM 53-12-0, FOUND AT LETTER CHECK.SDR DL72W960306Angle · crackedSLAT ANGLE CRACKED UNDER NR 7 SLAT I/B STOP PAD AREA. FOUND DURING LETTER CHECK, NR 7 L/E SLAT. INSTALLED REPAIR PER MM 57-54-0.SDR DL72W960318Web · crackedDURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1.25 INCH CRACK BETWEEN STA 294.5 AND 285.5, APPROXIMATELY AT WL 170. THE REPAIR IS ACCOMPLISHED IN ACCORDANCE WITH S/B 727-53-145.SDR DL72W960270Angle · crackedFOUND ON C-2 LETTER CHECK, COVE SKIN SUPPORT ANGLE CRACKED .0625 INCH BELOW NR 7 SLAT ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.SDR DL72E960285Power Supply · inoperativeON PREFLIGHT, EMERGENCY TRACK LIGHTS INOP IN FWD CABIN. REPLACED POWER SUPPLY, OPS NORMAL.SDR DL72W960212Cooling Valve · failedDISPATCHED WITH ONE PACK, MIX VLV INOP. ACFT WOULD NOT HOLD THE CABIN WITH CARGO HEAT OUTFLOW CLOSED AND OUTFLOW VLV FULL CLOSED. REPLACED EQUIP COOLING VLV IN E/E COMP, PRESS ACFT TO 3 PSI AND OPERATION CKS OK.SDR UPS205316Indication Syst · malfunctionedCREW REPORTED, ON GEAR RETRACTION RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR, NORMAL DOOR INDICATION EXTENSION AND RETRACTION. THREE GROUND LIGHTS ON EXTENSION AND NO RED LIGHT ON RETRACTION. RED NOSE LIGHT CAME BACK ON AND FLUCTUATED IN INTENSITSDR DL72W960127Battery Pack · dischargedDURING INSPECTION, AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT RACK, OPS NORMAL.SDR DL72W961585Transverse Beam · crackedTHERE IS A 1 INCH CRACK IN THE ANGLE OF BOTH THE FWD AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THSDR DL72W960119Angle · crackedFOUND ON A1 LETTER CHECK, TWO .5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0.SDR DL72W960092Angle · crackedDURING C-1 LETTER CHECK, FOUND .5 INCH CRACK AT NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72E960086Rib · crackedSLAT NR 6, RIB NR 10 AND 12 CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72W960109Bushing · wornON CLIMBOUT FROM RIC AT 360 KTS, THE NOSE WHEEL DOORS WERE SLAMMING OPEN AND SHUT REPEATEDLY. FOUND NLG DOOR OUT OF RIG AND BUSHINGS WORN IN ROD ON FWD QUAD. REPLACED ROD AND RIGGED NLG DOORS.SDR DL72E960069Valve · malfunctionedON CLIMBOUT THROUGH 29,000 FT, THE CABIN CONTINUED TO CLIMB THROUGH THE PRESET 4,800 CABIN ALITITUDE. DESENCED TO 18,000 WHERE THE CABIN STABLIZED AT 10,000. PACK BLEEDS AND OUTFLOW APPEARED OK. REPLACED RT FLOW CONTROL VALVE, LEAK CKS GOOD. PRESSURIZED A/SDR UPS205183Light · inoperativeYHM - MAINTENANCE REPORTED, L-1 EMERGENCY LIGHT IS INOP. RESERVED L-1 EMERGENCY LIGHT ASSY AND ASSY CHECKED SERVICEABLE.SDR DL72W960302Seal · out of positionAFTER TAKEOFF, EXPERIENCED EXTREMELY LOUD NOISE FROM FWD ENTRY DOOR. ACFT RTN TO BLK AT 1331. FOUND L1 DOOR LOWER HINGE FLAPPER SEAL OUT OF POSITION. CYCLE DOOR, SEAL POSITION NORMAL.SDR DL72W960112Lanyard · brokenON PREFLIGHT, FOUND R-1 DOOR SLIDE GIRT BAR LANYARD BROKEN. REPLACED LANYARD, OPERATION NORMAL.SDR UPS205179Light · inoperativeYHM - MAINTENANCE REPORTED, L 1 EMERGENCY EXIT LIGHT WILL NOT TEST. LIGHT ASSY REMOVED AND REPLACED AND OPS CHECKED GOOD AS PER MM 33-50-01.SDR DL72W970015Battery Pack · dischargedLT OVERWING EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK, CHECKS NORMAL.SDR DL72W960654Frame · crackedDURING INSPECTION, FOUND L2 SERVICE DOOR WITH CRACKED FRAME AT UPPER FORWARD LATCH CUTOUT. ACCOMPLISHED REPAIRS PER SRM 52-40-02.SDR DL72W960023Skin · dentedTHE FUSELAGE SKIN WAS OIL CANNED BETWEEN FS 660 TO 680 STR 23R AND STR 26R. THE DAMAGED AREA OF THE SKIN WAS TRIMMED OUT FROM FS 680 BUTT JOINT FORWARD FOR 19.75 AND FROM THE SKIN LAP JOINT AT STR 26R UP 25.75. A REPAIR DOUBLER WAS INSTALLED PER 8110-3 12-28SDR DL72W954776Beaded Doubler · crackedDURING C/V, FOUND RT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BEADED DOUBLER LOWER PANEL CRACKED. REPAIRED PER SRM 55-20-3 FIG 3.SDR UPS205161Battery · dischargedMAINTENANCE FOUND CREW FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD.SDR DL72W954772Battery Pack · dischargedTWO AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CK GOOD.SDR DL72W954754Line · leakingLOSS OF B-SYSTEM QUANITITY DOWN TO ZERO - ON FINAL AFTER GEAR DOWN BRAKE PRESSURE ABOVE 1500 PSI, NR 1 B-SYSTEM PUMP OFF. NR 2 SYSTEM TURNED OFF AND FLICKER OF LOW PRESSURE LIGHT. CORRECTIVE ACTION - FOUND B-HYDRAULIC LINE LEAKING. REPLACED SAME, LEAK CKS ANSDR DL72W961618Skin · corrosionTHE SKIN AT FS 680 CL AND FS 690 STR 26R WAS FOUND TO HAVE CORROSION DAMAGE. THE DAMAGE CUTOUT AT STA 680 CL IS APPROXIMATELY 2 BY 3, LOCAL SKIN THICKNESS IS 0.050. THE DAMAGE CUTOUT AT FS 690 IS APPROXIMATELY 2 BY 2, WITH A LOCAL SKIN THICKNESS OF 0.050. TSDR DL72E954787Transducer · faultyIR - RT BRAKE EXTREMELY WEAK. NR 3 BRAKE AT FAULT, TURNED OFF ANTI-SKID BRAKES, OPS NORMAL. REPLACED NR 3 TRANSDUCEDR ANTI-SKID, OPS NORMAL.SDR DL72W961619Skin · corrosionTHE SUBJECT FUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE AT STR 26L LAP JOINT, FS 500, 520 TO 540 AND 560 TO 570. AT FS 500, THE DAMAGE CUTOUT IS APPROXIMATELY 8 BY 2 IN THE LOWER SKIN. AT FS 520 TO 540, THE DAMAGE CUTOUT IS APPROXIMATELY 7.75 BY 2 IN THE USDR DL72W954737Bulb · failedENGINE FIRE TEST CAUSES NR 1 ENG A/B FIRE DETECTION CIRCUIT BREAKER TO TRIP. REPLACED ENG FIRE TEST PANEL. REPLACED FIRE DET MOD. NO HELP. REPLACED FAULT BULB IN FIRE HANDLE. SYSTEM NOW CKS NORMAL.SDR DL72W954736Angle · crackedNR 2 SLAT COVE SKIN ATTACH ANGLE AT TAI DUCT. PREVIOUS REPAIR DOUBLER CRACKED .25 INCH. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER 57-54-0.SDR DL72E954786Battery · dischargedDURING STANDBY POWER CHECK, FIRST CLASS EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK OPERATION NORMAL.SDR DL72W962734Skin · crackedAFT LOWER SKIN CRACKED I/B END. REPAIRED PER M/M 57-54-0.SDR DL72W954720Seat Track · corrodedSEAT TRACK AT G-3 GALLEY INBOARD AFT MOUNT IS CORRODED. REPAIR PER M/M 53-20-11, PAGE 805.SDR UPS205140Battery Pack · dischargedMAINT REPORTED, FLIGHT DECK EMERGENCY EXIT LIGHT DIM DUE TEST. FOUND COCKPIT DOOR EMERGENCY LIGHT ASSY BAD. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES IAW MM 33-50-101 PAR 1 TO 3 PAGE 202 TO 203, GND OPS GOOD.SDR DL72E954676Trunnion · corrodedCORROSION ON ATTACH POINTS FOR NLG TRUNNION AT MATING SURFACE FOR CAPS AND SURFACE WHERE BEARINGS SET. REPAIRED PER MM 53-40-0.SDR UPS805130Eel · inoperativeWHILE ON GROUND IN YHM, MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT L1 CABIN ENTRY DOOR DOES NOT TEST. EMERGENCY EXIT LIGHT ASSY REMOVED AND REPLACED AS PER M/M 33-50-01, OPS CHK GOOD.SDR DL72E954634Act Bracket · crackedNR 6 L/E FLAP ACTUATOR BRACKET CRACKED OUTBOARD END. FOUND ON D-1 LTR CK TPA MM. REPAIRED PER 57-20-21.SDR DL72E954633Skin · crackedRIGHT ELEVATOR LOWER INBOARD SKIN IS CRACKED 2.50 INCHES AFT OF PREVIOUS REPAIR. FOUND DURING D-1 LTR CK TPA MM. REPAIRED PER SRM 55-20-3.SDR DL72W954635Skin · crackedLEFT FUSELAGE SKIN CRACKED TWO STRINGERS ABOVE THE 'E' IN 'DELTA', JUST FORWARD OF STA 580 AND UNDER STR 4. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLERS PER ERA 302855-14 ON NR 011.SDR DL72W954620Doubler · crackedFOUND ON F-1 LTR CHECK - DOUBLER CRACKED AT NR 7 SLAT INBOARD DOWNSTOP. REPLACED DOUBLER PER M/M 57-54-0.SDR DL72E954603Battery Pack · dischargedON LAYOVER, FOUND EMERGENCY LIGHTS INOP ABOVE FWD AND AFT OVERWING EMERGENCY EXITS LT SIDE. REPLACED M1090 BATTERY PACK, EMERGENCY LIGHTS OPS NORMAL.SDR DL72W954614Battery · dischargedUPON TRANSFER TO GROUND, EXTERNAL POWER FLIGHT ATTENDANTS FOUND EMERGENCY EXIT LIGHTS WERE INTERMITTENTLY, AT ROW 20 TO 22 ABC. REPLACED BATTERY PACK, OPS CKS GOOD.SDR DL72W954576Skin · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH FLOATING SKIN CRACKED AT FASTENERS BETWEEN RIBS NR 8 AND 9, 13 AND 14. REPAIRED PER MM 57-54-0.
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