Boeing 727-232
Service difficulty reports · 6,539
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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 DL72L972681Blkhd Stiffener · crackedA 2 INCH CRACK WAS FOUND IN THE RBL 36.83 STIFFENER AND A 1 INCH CRACK WAS FOUND IN THE LBL 36.83 STIFFENER AT WL 238 ON THE FS 1183 BULKHEAD. THE STIFFENERS WERE REPAIRED PER BOEING S/B 727-53-0192 AS DOCUMENTED IN ER/A 363498-14.SDR EISA97283Actuator · failedNOSE GEAR WILL NOT EXTEND ON APPROACH TO BYH. REPLACED NOSE GEAR UPLOCK ACTUATOR, PER MM 37-32-11, PERFORMED GEAR RETRACTION, ALL OPS NORMAL PER MM 32-33-0. (X)SDR DL72S972694Torque Box · crackedWHILE ACCOMPLISHING THE TORQUE BOX INSPECTIONS PER B727 S/B 53-0129 AS MANDATED BY AD 94-07-08, THE FS 1273 BEAM AND GUSSET WERE FOUND CRACKED. THE DAMAGE PARTS WERE REPLACED PER THE S/B AND DOCUMENTED PER ER/A 363483-14AD.SDR DL72S972667Rib · crackedFOUND F2 LETTER CHECK, 1 IN CRACK NR 3 SLAT NOSE RIB AT SLAT ACT ROD END ATTACH I/B END. REPAIRED PER M/M 57-54-0 FIG 804.SDR DL72L972666Rib · crackedO/B ACTUATOR RIB CRACKED. REPAIRED RIB PER SRM 57-54-0.SDR DL72S972660Skin · crackedFOUND DURING B-2 LETTER CHECK, 1 IN CRACK NR 5 L/E FLAP SKIN AT I/B HINGE CUTOUT. REPAIRED PER M/M 57-53-0 AND ERA 363467-14.SDR DL72S972659Web · crackedFOUND ON B-2 CHECK, .5 IN CRACK AT RT TORQUE BOX VERT WEB LOWER LIGHTENING HOLE STA 1243. INSTALLED DOUBLER PER M/M 53-11-0 NR 16.SDR DL72S972658Web · crackedFOUND B-2 CHECK, .375 INCH CRACK AT LIGHTENING HOLE AT LT LOWER TORQUE BOX STA 1243. INSTALLED DOUBLER PER M/M 53-11-0 NR 16.SDR DL72S972661Skin · crackedSKIN, CRACKED THE FWD SECTION OF S DUCT FWD SKIN LIP AT THE 12:00 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN PER SRM. FABRICATED REPAIR PARTS PER SRM 54-10-3 FIG 13. TREATED AND PAINTED PER SRM 54-10-3. OK TO INSTALL REPAIR PER SRM 54-10-3. INSTALLSDR DL72S972652Skin · cracked.75 IN CRACK AT NR 2 LE FLAP SKIN AT INBD LIP HINGE CUTOUT. REPAIRED PER ERA 363453-14 AND M/M 57-30-0.SDR DL72S972639Power Supply · inoperativeR2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY.SDR DL72L972678Rib · crackedRIB NR 18 CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S972643Doubler · crackedFUSELAGE, FWD GALLEY DOOR SURROUND DOUBLER, UPPER HINGE: REPAIR FOR CRACK AT HINGE CUTOUT. THE FWD GALLEY DOOR SURROUND DOUBLER WAS FOUND WITH A 1.8 CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR INSTALLED PER BOEING S/B 727SDR DL72S972621Web · crackedFOUND DURING A-2 LETTER CHECK, .75 INCH CRACK LT LWR TORQUE BOX WEB STA 1227 UPPER EDGE OF VERT WEB. REPAIRED PER M/M 53-11-0.SDR DL72S972620Frame · wornFOUND DURING A-2 LETTER CHECK, ANGLE WORN THROUGH 11 INCHES, 6 O'CLOCK POSITION FS 1352 FRAME. REPAIRED PER ERA 363434.SDR DL72S972619Skin · crackedFOUND DURING A-2 LETTER CHECK, 1.75 INCH CRACK IN RT ELEVATOR UPPER SKIN AT DOUBLER BETWEEN O/B 2 ELEVATOR HINGES. REPAIRED PER ERA 363435-14.SDR DL72L972642Skin · gougedFUSELAGE, SKIN FS 340-380 STRINGER 20L-21L : REPAIR FOR SKIN GOUGE AND DENT CUTOUTS. THE FUSELAGE SKIN BETWEEN FS 340 AND 380 AND BETWEEN STRINGER 20L AND 21L WAS BADLY GOUGED AND DENTED. THE DAMAGED AREAS WERE CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER ANSDR CALA9701752Relay · inoperativeTHE NR 1 ENGINE FIRE DETECTION FAULT LIGHT AT B POSITION ILLUMINATED INTERMITTENTLY WHILE IN FLIGHT. TROUBLESHOOTING THE NR 1 ENGINE FIRE DETECTION SYSTEM FOUND R147 TEAT RELAY FAULTY. THE R147 RELAY WAS REMOVED AND REPLACED. THE NR 1 ENGINE B FIRE DETECTIONSDR DL72S972646Rib · crackedWING, RIB, BL 70.5, STA 760.95, UPPER RIB CHORD, REPAIR FOR CRACKED FASTENER HOLES. WHILE ACCOMPLISHING AND MANDATED INSPECTIONS OF THE BL 70.5 RIB CHORD AT STA 760.95, SEVERAL FASTENER HOLES SHOWED CRACK INDICATIONS. THE CRACKED HOLES WERE OVERSIZED TO ELIMSDR DL72S972742Rib · crackedTHE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED DURING SHOP VISIT. THE RIB WAS REPAIRED BY INSTALLING A DOUBLER PER 727 M/M 57-52-0.SDR DL72S972645Structure · damagedFUSELAGE, SKIN, FRAME, AND STRINGER FS228-252, S24R. REPAIR FOR DENTED AND CRACKED SKIN, STRINGERS, AND FRAMES. THE FUSELAGE SKIN BETWEEN FS 228 AND 252 AT S-24R WAS DAMAGED BY GROUND EQUIPMENT. THE SKIN DAMAGE WAS CUTOUT AND A DOUBLER REPAIR INSTALLED. THSDR DL72S972594Light · inoperativeAFT OUTBOARD EMERGENCY FLASHLIGHT IS NOT FLASHING. REPLACED FLASHLIGHT ASSY AND BREAKAWAY BAND.SDR DL72L972597Actuator · leakingPILOT REPORTED, CLIMBING THROUGH 18,000 FT 'A' SYS QTY DECREASED TO ZERO. ALL PROCEDURES ACCOMPLISHED PER CHECKLIST. BOTH 'A' SYSTEM LOW PRESS LIGHTS WERE BLINKING AS PRESS WAS DROPPING. MAINTENANCE FOUND NR 4 L/E FLAP ACTUATOR LEAKING AT SWIVEL END. REPLASDR DL72L972591Batteries · dischargedEMERGENCY LIGHTS ABOVE BOTTOM OF AFT AIRSTAIRS INOP. REPLACED BATTERIES.SDR DL72S972586Spar · crackedHORIZONTAL STABILIZER, RT ELEVATOR, REAR SPAR, REPAIRED FOR LOOSE HINGE FITTING AND SPAR CRACKS. THE RT ELEVATOR WAS FOUND WITH ONE HINGE FITTING LOOSE. THREE (3) .125 INCH LONG CRACKS WERE FOUND IN THE REAR SPAR WEB EXTENDING FROM THE CORNERS OF THE SHEAR SDR CALA9701744Skin · dentedINSPECTION FOUND RT WING FORWARD FOREFLAP DENTED ON BOTTOM SURFACE ABOVE NR 5 FLAP TRACK. THE FOREFLAP WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-00.SDR CALA9701743Stringer · crackedINSPECTION FOUND A .75 CRACK IN AFT TANG AT FORWARD VENT BOX STRINGER WHERE IT MOUNTS TO TOP OF LT WING RIB, WS 686.50, TANK CUTOUT NR 7218. THE FASTENERS WERE REMOVED. CUTOUT ACCESS HOLE TO ACCESS REPAIR IAW EA 5762-01050. REPAIR ANGLE AND SHIMS WERE FABRISDR CALA9701742Stringer · crackedINSPECTION FOUND A .75 CRACK IN AFT TANG AND A .75 CRACK IN FORWARD TANG AT AFT VENT BOX STRINGER WHERE IT MOUNTS TO TOP OF LT WING RIB, WS 686.50, TANK CUTOUT NR 7218. THE FASTENERS WERE REMOVED. CUTOUT ACCESS HOLE TO ACCESS REPAIR IAW EA 5762-01050. REPAISDR CALA9701741Stringer · crackedINSPECTION FOUND A .75 CRACK IN LT WING THIRD FROM REAR SPAR UPPER STRINGER AT WS 629, ACCESS CUTOUT NR 7216. THE STRINGER WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 5, AND ECRA 5710-01859.SDR CALA9701740Angle · crackedINSPECTION FOUND A .75 CRACK IN J ANGLE AT LT WING T/E AREA JUST ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE TOP PANEL WAS REMOVED. A J ANGLE BRACKET REPAIR WAS INSTALLED AND THE PANEL WAS REINSTALLED. WORK WAS PERFORMED IAW SRM 51-10-2, 51-10-1, 51-30-SDR DL72S972567Roller · bindingAFTER TAKEOFF, THE LEFT FORWARD ENTRY DOOR DID NOT SEAL PROPERLY. DAYLIGHT COULD BE SEEN THROUGH THE DOOR SEAL. FOUND DOOR NOT CLOSED PROPERLY. INSPECTED DOOR, FOUND CAMPLATE ROLLER BINDING. REPLACED ROLLER, FOUND UPPER DOOR GUIDE HINGE GUIDE ARM OUT OF ADSDR DL72L980218Frame · partFS FRAME 1352 FRAME WORN AT THE 6 O'CLOCK POSITION. FRAME WAS REPAIRED PER MM 53-11-0.SDR DL72L980121Web · crackedAT MV-2/DFW, FOUND A CRACK AT A LIGHTENING HOLE AT FS 870 IN WEB AND DBLR. REPAIRS WHERE COMPLETED PER SRM 53-10-9 FIG 5. CRACK WAS LOCATED AT THE 5 O'CLOCK POSITION.SDR DL72S972555Duct · rupturedNR 2 ENG 8TH STAGE DUCT RUPTURED, DAMAGED FIREWALL AND FIRE LOOP. REPLACED DUCT AND FIRE LOOP, MADE TEMPORARY REPAIR TO FIREWALL. A/C MTC FAIRY TO SLC.SDR DL72S972627Beam · crackedRT WING SPOILER SUPPORT BEAM CRACKED IN O/B BOLT HOLE FOR NR 5 FLAP TRACK. REMOVED DAMAGED SECTION OF SPOILER BEAM PER M/M 57-55-0 FIG 805. REMOVED SUPPORT BETWEEN SPOILERS 7 AND 8. FABRICATED EXTRUDED CHORD IAW M/M 57-55-0 PG 810. DRILLED CHORD, DOUBLER TSDR DL72S972587Beam · crackedTHE AFT GUSSET AND HORIZONTAL BEAM AT FS 1273 ON THE VENTRAL STAIRWAY TORQUE BOX WERE FOUND CRACKED PER INSPECTIONS OF S/B 53-0129 AS MANDATED BY AD 94-07-08. THE CRACKED PARTS WERE REPLACED PER S/B 53-0129 AS DOCUMENTED IN ER/A 363353-14AD.SDR DL72S972540Stiffener · crackedA 1.5 INCH CRACK IN 2 EA SPAR STIFFENERS AT NR 6 SLAT OUTBD TRACK. REPAIRED PER MM 57-20-21.SDR DL72S972539Angle · crackedNR 1 SLAT I/B ACTUATOR MOUNT ANGLE CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S972538Skin · crackedA .25 INCH VISIBLE CRACK IN COVE SKIN ANGLE AT NR 1 SLAT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.SDR DL72S972515Battery · dischargedON PREFLIGHT, FWD EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED BATT.SDR CALA9701707Power Supply · inoperativeINSPECTION FOUND L-2 DOOR INTERIOR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED.SDR DL72S972520Torque Box · crackedTHE TORQUE BOX WAS FOUND WITH A CRACKED UPPER CHORD AND A CRACKED FS 1263 UPPER BEAM ANGLE AND CHANNEL. THE CRACKED MEMBERS WERE REPLACED OR REPAIRED PER S/B 53-0129. ER/A 363340-14AD WAS ISSUED TO DOCUMENT THE DAMAGE AND CONTROL THE REPAIR METHOD.SDR DL72S972514Skin · crackedFOUND ON D1 LETTER CK, ONE 3 AND ONE 3.5 INCH CRACK IN SLAT LOWER SKIN OF NR 6 L/E SLAT AT O/B T/E. REPAIRED PER MM 57-54-0.SDR DL72S972506Spar Web · crackedTHE CENTER WING REAR SPAR WEB WAS FOUND WITH A 3.75 INCH LONG CRACK IN THE CHEM-MILL TRANSITION AREA OF THE WEB JUST BELOW THE REAR SPAR CAP AT RBL 17. THE CRACK WAS CUTOUT AND A REPAIR DOUBLER INSTALLED PER ER/A 363301-14, REV A.SDR DL72S972505Spar Web · crackedTHE CENTER WING REAR SPAR WEB WAS FOUND WITH A 3 INCH LONG CRACK IN THE CHEM-MILL TRANSITION JUST BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT AND A REPAIR DOUBLER INSTALLED PER ER/A 363296-14, REV A.SDR DL72S972497Battery · dischargedFRONT CABIN FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY PACK.SDR DL72L972489Light · corrodedLT AFT ENTRY DOOR SLIDE LIGHT INOP ON LAYOVER CHECK. REPLACED REFLECTOR ASSY DUE TO CORRODED CENTER ELECTRODE.SDR DL72S972508Stringer · corrodedCORROSION WAS FOUND ON THE BASE FLANGE OF STRG 28R AT STA 720A +10 COMMON TO THE SKIN. A SECTION OF THE STRINGER WAS CUTOUT AND THE SKIN WAS CUTOUT TO REMOVE THE CORROSION. A NEW SECTION OF STRINGER WAS SPLICED IN AND A SKIN DOUBLER INSTALLED PER ER/A 363SDR DL72S972507Skin · corrodedTHE FUSELAGE SKIN BETWEEN STA 580 AND 640 WAS FOUND CORRODED BETWEEN S-26L AND 27L. THE DAMAGED SKIN WAS CUTOUT AND A NEW SECTION OF SKIN WAS SPLICED IN WITH TWO SPLICE STRAPS PER ER/A 363277-14, REV A.SDR DL72S972485Skin · crackedA .1875 INCH CRACK IN SKIN RT LOWER FWD CORNER OF VERTICAL STAB SADDLE PLATE CUTOUT (PANEL 9501). INSTALLED DOUBLER PER M/M54-30-0 FIG 802.
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