Boeing 727-225
Service difficulty reports · 4,226
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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 = '727225' 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 = '727225' 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 07FDEA00652Door · crackedFOUND NLG RT FWD DOOR INNER SKIN IS CRACKED AT INBD EDGE, FORWARD END CUT OUT DAMAGE. INSTALLED TYPICAL WEB REPAIR, REF SRM 51-40-2 FIG 1.SDR 07FDEA00651Stringer Clip · crackedFOUND MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 950D, SRT 9R. REPLACED STRINGER CLIP REF SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00650Stringer Clip · damagedFOUND MAIN CABIN FS 540, STR 3 R STRINGER CLIP HAS NO RADIUS AND HAS SHARP EDGES ON TOP SIDE. REPLACED STRINGER CLIP AT STA 540, STR 3R REFERENCE SRM 51-30-2. CLASSIFIED AS MAJOR REPAIR.SDR 07FDEA00648Skin · wornFUSELAGE AT LT WING LEADING EDGE ROOT AT BS 720D, 10" - 14" AT STRINGER 19L, LAP AREA IS WORN FROM PANEL CONTACT. BLENDED DAMAGED AREA REF 53-30-1 PAGE 2A. FOUND TO BE OUT OF LIMITS REF SRM 53-30-1 PG 2C. REPAIRED AREA WITH DOUBLER AND FILLER REF SRM 53-30SDR 07FDEA00647Stringer Clip · damagedFOUND MAIN CABIN STATION 620, STR 3R, STRINGER CLIP IS DAMAGED REPLACED STRINGER CLIP REF SRM 51-30-2.SDR 07FDEA00646Stringer Clip · crackedFOUND MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 970, STR 9R. REMOVED CRACKED STRINGER CLIP, DRILLED UP NEW CLIP AND INSTALLED REF SRM 51-30-2.SDR 07FDEA00628Stringer Clip · damagedFOUND MAIN CABIN STRINGER CLIP DAMAGED AT FS 540 STR 1. REPLACED STRINGER CLIP REF SRM 51-30-2 AND SRM 51-30-5. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00621Stringer Clip · crackedMAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 950C STR 9R. REPLACED STRINGER CLIP REFERENCE SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00620Skin · crackedFOUND LOWER FUSELAGE AT BS 178, LBL 0 - LBL 1 SKIN EDGE IS BENT, CRACKED AND KNIFE EDGED. REPAIRED DAMAGED LOWER FUSELAGE SKIN AT BS 178, LBL 0 - LBL 1 REF SRM 53-30-1, FIGURE 1.SDR 07FDEA00608Bushing · migratedNR 6 FLAP TRACK FWD ATTACH FITTING HAS MIGRATING BUSHING AND INBD FACE HAS CORROSION (BORE ALSO CORRODED) WBL 203. REMOVE BUSHING, REAMED BORE, MPI BORE, FABRICATE BUSHING, CAD PLATE BUSHING, ROTOPEEN BORE AND FACES, CAD PLATE LUG AND INSTALLED BUSHING REF FESDR C8GA20070003Blades · damagedFLT 1723 FROM BOS TO TOL, DURING CLIMB-OUT, NR 2 ENGINE BEGAN TO VIBRATE AND WAS CONFIRMED WITH THE THROTTLE. ENGINE BEGAN TO COMPRESSOR STALL, ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. POST FLIGHT INSPECTION REVEALED FOD DAMAGE TO THESDR CA070202005Duct · missing(CAN) UPON ARRIVAL, MAINTENANCE NOTICED AN APPROXIMATELY 6 INCH HOLE IN NR 1 ENGINE COWL. FURTHER INVESTIGATION DETERMINED THE CAP ON THE 6TH STAGE SADDLE DUCT MISSING, LOCATED IN COWL. CAP INSTALLED AND SECURED IAW MM AND COWL REPAIRED. (TC NR 20070202005)SDR DHL2007743505Floor Panel · corrodedBS 1178, RBL 18.0, AREA UNDER FLOOR PANEL (WEB), SHOWS CORROSION. CUT OUT DAMAGE, 5.5" BY 6", FABRICATED DOUBLER OUT OF 2024-T3, .050" BY 9.5" BY 10", PO NR 9004384; AND FILLER OUT OF 2024-T3, .040" BY 7.125" BY 8.75", PO NR 9004150, TREATED, PRIMED, AND INSTSDR DHL2007743503Bulkhead · crackedAFT CABIN, BS 1183 BULKHEAD SHOWS CRACK AT VERTICAL FLANGE APPROX BETWEEN RBL 36.8 AND WL 230. COMPLIED WITH REPAIR PROCEDURES PER B727 SB 727-53-0192, TO INCLUDE: TERMINATION OF CRACK END BY STOP DRILLING (.250" HOLE), AND INSTALLATION OF REPAIR PARTS FROM SDR DHL2007743504Bulkhead · crackedAFT CABIN, BS 1183 BULKHEAD SHOWS CRACK AT VERTICAL FLANGE ANGLE, APPROX BETWEEN BBL 36.8 AND WL 225. COMPLIED WITH REPAIR PROCEDURES PER B727 SB 727-53-0192, TO INCLUDE: TERMINATION OF CRACK END BY STOP DRILLING (.250" HOLE), AND INSTALLATION OF REPAIR PARTSSDR DHL2007743502Skin · delaminatedRT IB TE FOREFLAP LOWER SKIN PRESENTS DELAMINATION APPROX AT WBL 210.0. CUT OUT DELAMINATED AREA APPROX 13" BY 15.5". FABRICATED FILLER APPROX 13" BY 15.5" AND DOUBLERS 2EA APPROX 3" BY 15.5" FROM 2024T3 .016 PO NR 9003189. CLEANED, PREPPED, BONDED, TREATEDSDR CA070202004Wire · shorted(CAN) DURING CLIMB AT FL120, APU FIRE LIGHT AND BELL ILLUMINATED. APU FIRE DRILL CARRIED OUT, REMAINED (ON). DECLARED EMERGENCY, RETURNED TO AIRPORT WITHOUT INCIDENT. UPON INSPECTION NO FIRE DETECTED. MAINTENANCE FOUND (FIRE WARNING) WIRE NR W272-607-18 SHOSDR DHL2007743501Frame · corrodedREF ASTAR N/R'S 079970 AND 080116. AFT CARGO COMPT; CORROSION ON FLANGE ON FUSELAGE FRAME AT BS 1166 AND STR 29L. CORROSION OUT OF LIMITS. CUT OUT DAMAGE TO FRAME, 3.125 INCHES X 2.375 INCHES SRM 53-10-4 FIG 11. FABRICATED REPAIR PARTS: FILLER FROM 7075-TSDR CA070202003Seal · failed(CAN) DURING CRUISE AT FL320, CABIN RATE STARTED TO CLIMB AT 1500 FPM. CREW (CARGO FIT) DONED O2 MASKS. PRESSURIZATION CONTROLLER SELECTED TO (MANUAL) AND (STBY), NO CHANGE. CARGO HEAT OUTFLOW VALVE CLOSED, RECOVERED PRESSURE. O2 REMOVED, FLIGHT CONTINUED WITHSDR 07FDEA00092Unknown · unknownAFTER APPLICATION OF STANDARD TAKEOFF POWER AT APPROXIMATELY 60KTS A LOUD HIGH PITCH WHINE ACCOMPANIED WITH SOUND OF RUSHING AIR WAS HEARD. TAKEOFF WAS REJECTED AT 80KTS. CHECKED CARGO AND ENTRY DOOR SEALS FOR DAMAGE, NONE FOUND. PRESSURIZED AC IAW JRH CHAPSDR DHL2007743500Skin · delaminatedRT WING O/B FOREFLAP HAS DELAMINATION DAMAGE. REMOVED DELAMINATED AREA APPROX 4.8" BY 2". CLEANED AND PREPPED REPAIR AREA TO BOND IAW B727 SRM 51-40-20 PAR 7 FIG 3. FABRICATED LOWER FILLER AND DOUBLER FROM .016" 2024T3 PO NR 9003189, REPAIR CORE FROM HRP-3/SDR G8GA20060021Fire Detector · contaminatedFLT 740 FROM TOL TO BNA, DURING CRUISE OPERATION AT 30000 FEET , THE APU FIRE WARNING CAME ON INDICATING AN APU FIRE. APU FIRE BOTTLE WAS FIRED AND THE FIRE WARNING LIGHT EXTINGUISHED. AIRCRAFT LANDED IN BNA WITHOUT INCIDENT. ON POST FLIGHT INSPECTED APE ANSDR DHL2006742002Battery · dischargedON WALK AROUND, FOUND EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED BATTERIES IAW MM 33-50-71, OPS CK GOOD.SDR 06FDEA04136Steering Sys · malfunctionedDURING TAKEOFF ROLL, A/C DRIFTED LEFT OF CENTERLINE WITH NO ABILITY TO CONTROL, TAKEOFF ABORTED. SUSPECTED ICY RUNWAY. DURING TAXI IN, NOTICED THAT THE RUDDER PEDALS WOULD NOT STEER A/C TO RIGHT, TILLER WAS REQ'D TO EFFECT RIGHT TURN. RIGHT RUDDER PEDAL DOESDR CA061219001Duct · disconnected(CAN) LOWER AFT BODY HEAT WARNING LIGHT ILLUMINATED IN FLIGHT. FLIGHT CREW FOLLOWED EMERGENCY CHECKLIST AND LIGHT EXTINGUISHED WHEN NR 3 BLEED AND THRUST LEVER CLOSED. UPON INVESTIGATION MAINTENANCE DISCOVERED SUPPLY DUCT FORWARD OF STA 1183 DISCONNECTED AND SDR C8GA20060020Rod · brokenFLT 713 FROM BOS TO ROC, AFTER TAKEOFF AND CLIMBING, THE RIGHT MAIN GEAR DOOR LIGHT REMAINED ON. CYCLED THE GEAR AND THE LIGHT REMAINED ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN BOS. ON POST FLIGHT INSP NOTED THAT THSDR C8GA20060019Switch · shortedFLT 716 FROM TOL TO MEM, ON TAKEOFF ROLL AT 100 KTS TAKEOFF WARNING HORN SOUNDED, TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE RAMP WITHOUT INCIDENT. ON POST FLIGHT, FOUND STABILIZER TAKEOFF SWITCH NR S532 SHORTED TO GND. REMOVED AND REPLACED NR S532, OPSDR 06FDEA04010Striker · wornAFT AIRSTAIR LIGHT ILLUMINATED PASSING F220 CLIMBING LEVELED AT F230 PER ATC AND RETURNED TO MEMPHIS, UNEVENTFUL LANDING. RELEASED FOR SERVICE PER MEL/CDL: 52-06-BCATEGORY: C EXPIRATION: 23NOV06. DISCREPANCY HAS BEEN REASSIGNED TO WRI 52-70/9033. DURING INSSDR DHL2006748004Connector · dirtyNR 3 ENGINE FIRE INDICATION ON SHORT FINAL (LIGHT AND BELL) PHASE 1 HEMS COMPLETED FIRE LIGHT WENT OUT WITHOUT BOTTLE DISCHARGE. RESET SYSTEM, CLEANED CONNECTORS ON FIRE LOOP, CHECKED FOR LEAKS ON ENGINE NONE FOUND. PERFORMED TEST PER M/M 26-10-10, OPS CHECKSDR C1HA200676003Duct · disconnectedAT 3000' IN CLIMB, LOWER AFT BODY OVERHEAT LT ILLUMINATED. RAN COM 2, 3, 6, 5, AND LT EXTINGUISHED. RETURNED TO IND. FOUND DISCONNECTED AIR DUCT IN AFT BAG BIN. REPLACED COUPLER. FUNCTIONAL TEST WING ANTI-ICE SYS CHECKS NORMAL REF MM 30-13-00.SDR C1HA200675005Switch · malfunctionedTAKEOFF FROM MSP WHEN RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES ON CLIMB-OUT, THE LE FLAP AMBER LIGHT REMAINED ILLUMINATED AND THE NR 3 LE FLAP AMBER LIGHT ON THE FLAP AND SLAT INDICATOR PANEL REMAINED ILLUMINATED. RAN THE COM 2.27.12 PROCEDURE. LIGHT REMASDR C8GA20060016Circuit Card · dirtyON TAKE OFF, TAKE OFF WARNING HORN SOUNDED. CREW CYCLED TRIM, SPEED BRAKES, AND FLAPS. NO HELP. AIRCRAFT RETURNED TO BLOCKS. FOUND E-6 CARD CONNECTOR DIRTY. CLEANED AND RESEATED E-6 CARD. TAKE OFF WARNING OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA060918010Start Valve · malfunctioned(CAN) THE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED DURING CLIMB OUT. A/C RETURNED TO BASE. A/C INSPECTED AND THE START VALVE REPLACED DUE CRACKED. A/C RETURNED TO SERVICE. FAULT REOCCURRED DURING CLIMB. A/C RETURNED TO BASE. THE FUEL HEAT DUCT WASSDR CIHA200675002Web · corrodedAFT AIRSTAIR 6TH FROM BOTTOM WEB CORRODED. FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED WEB ON AFT AIRSTAIR 6TH STEP IAW B727 SRM 52-10-1 FIG 1 AND 51-30-2.SDR C1HA200675003Web · corrodedAFT AIRSTAIR STEP WEB CORRODED (3RD STEP FROM BOTTOM). FABRICATED AND INSTALLED NEW SHEAR TIE AT RISER IAW B727 SRM 52-10-1 FIG 3 AND 51-30-2 FIG 1 AND 15.SDR CIHA200675001Web · corrodedAFT AIRSTAIR 5TH FROM BOTTOM WEB CORRODED. FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED WEB ON AFT AIRSTAIR 5TH STEP IAW B727 SRM 52-10-1 FIG 1 AND 51-30-2.SDR C1HA200675004Channel · corrodedFUSELAGE LWR LOBE STA 205 HAS MID-CHORD CORRODED FWD OF TRUNNION FITTING RT SIDE. REMOVED AND REPLACED MID-CHORD P/N 65-19862-20 IAW B727 SRM 51-30-2 FIG 1,11 AND 15.SDR CIHA200676001Support Angle · corrodedCOCKPIT R-5 WINDOW FRAME CORRODED. REMOVED AND REPLACED COCKPIT R-5 WINDOW FRAME SUPPORT ANGLE IAW SRM 51-30-2 FIG 1.SDR C1HA200676002Attach Angle · corrodedFWD LWR FUSELAGE (DOG HOUSE) LT HORIZ WALKWAY AT BS 328 AT WL 169- UNDERSIDE IB SIDE OF WALKWAY SKIN WEB AT CHORD ATTACHMENT ANGLE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED CHORD PN 65-19862-19 IAW SRM 51-30-2 FIG 7,11,15.SDR DHL2006743523Coupling · crackedWHILE VISUALLY INSPECTING THE MAIN CARGO DOOR FOUND A COUPLING CRACKED ON THE HOOK TORQUE SHAFT. THE COUPLING IS NR 2 FROM FRONT END OF DOOR. THE CRACK RUNS FROM EDGE TO THROUGH BOLT HOLE. THE CRACK IS APPROX 1/2" LONG, THE DOOR IS A PEMCO STC.SDR DHL2006743524Coupling · crackedWHILE VISUALLY INSPECTING THE MAIN CARGO DOOR A CRACK WAS FOUND ON A HOOK TORQUE SHAFT COUPLING, 2ND FROM FORWARD END. THE CRACK IS FROM EDGE OF COUPLING TO A THROUGH BOLT HOLE. THE DOOR WAS MANUFACTURED BY PEMCO. THE CRACK EXTENDS APPROX 1/2" IN LENGTH.SDR DHL200674352Coupling · crackedWHILE VISUALLY INSPECTING THE MAIN CARGO DOOR FOUND A COUPLING CRACKED ON THE HOOK TORQUE SHAFT. THE COUPLING IS NR 2 FROM FRONT END OF DOOR. THE CRACK RUNS FROM EDGE TO THROUGH BOLT HOLE. THE CRACK IS APPROX 1/2" LONG. THE DOOR IS A PEMCO STC.SDR DHL2006743Coupling · crackedWHILE VISUALLY INSPECTING THE MAIN CARGO DOOR FOUND A COUPLING CRACKED ON THE HOOK TORQUE SHAFT. THE COUPLING IS NR 2 FROM FRONT END OF DOOR. THE CRACK RUNS FROM EDGE TO THROUGH BOLT HOLE. THE CRACK IS APPROX 1/2" LONG THE DOOR IS A PEMCO STC.SDR CA060728002Switch · out of rig(CAN) DURING CLIMB THROUGH FL210 AND 6.0 PSID CABIN DIFFERENTIAL THE CARGO DOOR UNSAFE LIGHT INDICATION ILLUMINATED. AIRCRAFT DUMPED FUEL AND RETURNED TO STATION, DURING APPROACH THE CARGO DOOR UNSAFE LIGHT EXTINGUISHED. UPON INSPECTION MAINTENANCE FOUND DOOR SDR 06FDEA2675Actuator · faultyNR 4 SLAT W/N RETRACT AFTER T/O. RAN QRH CK LIST W/NEGATIVE RESULTS. RETURNED TO MEM. EXPERIENCED UNCOMMANDED ROLLING INPUT), CREW REPORTED DURING DEBRIEF THAT THEY CYCLED FLAPS TO 5 DEGREES AND BACK TO FLAPS 2 WITH NO HELP. A/C STILL EXPERIENCED UNCOMMANDSDR CA060724001O-Ring · swollen(CAN) ON DESCENT STABILIZER OUT OF TRIM LIGHT ILLUMINATED, STABILIZER WOULD NOT RESPOND TO COMMANDS FROM AUTOPILOT, MAIN ELECTRIC TRIM OR MANUAL TRIM. FLIGHT CREW ACCOMPLISHED THE STABILIZER JAM EMERGENCY CHECK LIST AND LANDED UNEVENTFULLY. UPON INSPECT MAINTESDR DHL2006743002Downlock Sensor · looseON INITIAL ATTEMPT TO LOWER LANDING GEAR RIGHT MAIN GEAR UNSAFE LIGHT -RED- REMAINED ILLUMINATED WITH NO GREEN SAFE LIGHT. INITIATED GO AROUND AND COMPLIED WITH AOM ABNORMAL PROCEDURE. SECOND ATTEMPT TO CYCLE GEAR PRODUCED NORMAL INDICATIONS. FOUND RT DOWNLSDR CA060630003Actuator · inoperative(CAN) SHORTLY AFTER TAKEOFF, CREW NOTICED THAT THE #8 LEADING EDGE SLAT WAS NOT INDICATING THAT IT WAS RETRACTED. THE CREW REQUESTED FUEL DUMP AND TURN BACK TO DEPARTURE. MAINTENANCE TESTED THE SLAT AND FOUND THE INDICATION SWITCH IN THE ACTUATOR WAS AT FAULT.SDR CA060626001Rib · cracked(CAN) DURING SCHEDULED INSPECTON, MAINTENANCE FOUND THE NR 1 LEADING EDGE SLAT ACTUATOR WING RIB ATTACH POINT CRACKED. CRACKED MOUNT SUPPORT REPLACED.SDR DHL2006743009Skin · crackedL1 DOOR HINGE UPPER CUTOUT BS306 HAS 1 INCH CRACK EXTENDING FWD FROM RADIUS. TRIM-OUT DAMAGE AREA DIM. 1X 1.250 IAW SB727-53-A0198 REV 2 VERIFIED CRACK REMOVAL WITH HFEC IAW B727 NDT M PT6 51-00-00 FIG 23. FABBED DOUBLER MAT USED 301 1/2 HD .063 PO 9001442 D
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