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 DHL2007748013Seat Track · corrodedSEAT TRACK BS 1050-1130 LBL 45 CORRODED. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 1070 TO 1090 LBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION MATERIAL USED BAC 1520-792-7178-T616 PO NR 9005692 DIMENSION 69" LONG, 2 EACH ANGLE MATERIASDR DHL2007748005Seat Track · corrodedMAIN CABIN STATION 848.95 TO 870 LBL 24 SEAT TRACK FLANGE HAS CORROSION BOTH SIDES. REMOVED SEAT TRACK SECTION AT MAIN CABIN STATION 848.95 TO 870 LBL 24 IAW B-727 SRM 51-30-2. FABRICATED SECTION SEAT TRACK MATERIAL USED BAC 1520-1466 7178-T6511 PO NR 730788SDR DHL2007748004Seat Track · corrodedMAIN CABIN STATION 848.95-870 LBL 45 SEAT TRACK FLANGES HAS CORROSION ON BOTH. REMOVED SECTION OF SEAT TRACK IAW SRM 51-30-2. FABRICATED SECTION SEAT TRACK IAW SRM 53-10-2 FIGURE 7 AND 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SECTION SEAT TRASDR DHL2007748006Frame · dentedFRAME DENTED IN MAIN CABIN BS 540 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 540 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW FRAME REPAIR MATERIAL USED 7075-T6 0.063" PO NR 9005713 DIMENSION (9.25 BY 4.875") IAW B-727 SRM 53-10-2 FIGURE 3 SDR DHL2007748010Frame · dentedFRAME DENTED IN MAIN CABIN BS 580 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 580 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 7075-T6 0.063" PO NR 9005773 DIMENSION 10" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3.SDR DHL2007748003Frame · dentedFRAME DENTED IN MAIN CABIN BS 520 AT STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 520 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW REPAIR MATERIAL USED 7075-T6 0.063" PO NR 9005773 DIMENSION 9" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2SDR DHL2007748011Frame · dentedFRAME DENTED IN MAIN CABIN BS 560 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 560 STRINGER 17R IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 2. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. DOUBSDR DHL2007748009Frame · dentedFRAME DENTED IN MAIN CABIN BS 600 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 600 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 7075-T6 0.063" PO NR 9005773 DIMENSION 10" BY 5" IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3.SDR DHL2007748008Frame · dentedFRAME DENTED IN MAIN CABIN BS 640 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 640 STRINGER 17R IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 3. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. DOUBSDR DHL2007748007Frame · dentedFRAME DENTED IN MAIN CABIN BS 660 STRINGER 17R. REMOVED PREVIOUS REPAIR AT MAIN CABIN BS 660 STRINGER 17R IAW B-727 SRM 51-30-2. FABRICATED DOUBLER IAW SRM 51-40-3 FIGURE 1 AND 53-10-2 FIGURE 2. PART AND AREA TREATED AND PRIMED IAW SRM 51-10-2. DOUBLER INSSDR CA071010006Turbine Wheel · failed(CAN) AT THE RUNWAY THRESHOLD THE FLIGHT CREW ADVANCED THE THROTTLES TO 1.2 EPR, STABLE ENGINES WERE CALLED. ADVANCED THRUST LEVERS AND APPROACHING TAKEOFF THRUST, BEFORE REACHING APPROXIMATELY 20 KTS, A LOUD BANG AND VIBRATION OCCURRED. THE FLIGHT CREW REJECTSDR K11A2008112572406Spar · corrodedHORIZONTAL STABILIZER CORROSION ON LOWER CHORD RT HORIZONTAL REAR SPAR.SDR 07FDEA04138Wire · damagedAFT AIRSTAIR LIGHT ILLUMINATED AT ROTATION. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 30SEP07 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT, INOP. PLEASE WORK IN CONJUNCTION WITH TSI: 52-62 9704. REPAIRED WIRE AT SW S273 (UPLOCSDR 07FDEA03458Door Frame · corrodedCORROSION FOUND BELOW LOWER DOOR STOP FITTING ON LT FWD DOOR, FRAME 14 LT, T1. REPAIR WAS PERFORMED BY SMOOTH BLEND OUT OF CORROSION IAW EA 6-5312-95915 AND RAS/043491/005/2006 ISSUE A.SDR 07FDEA03387Duct · damagedNR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE AND LIGHT EXTINGUISHED. AFTER LIGHT EXTINGUISHED, NORMAL POWER SETTINGS USED, LIGHT NEVER CAME BACK ON. REMOVED AND REPLACED 8TH STAGE DUCT DUE TO FLANGE AND NUT LEAKING. GROUND RAN NR 1 ENSDR DHL2007742013Skin · crackedL1 DOOR FORWARD LOWER HINGE CUTOUT IS CRACKED AT FORWARD EDGE BS 303 BETWEEN STR 12/14. CONTINUED ON N/R 138192. REMOVED FASTENERS AT L1 DOOR LOWER HINGE CUTOUT IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM 301 1/2 HARD .063 PO NR 9004843 APPROXIMATESDR 07FDEA03227Beam · corrodedHORIZONTAL WALKWAY BEAM L/SIDE HAS EVIDENCE OF CORROSION AT APPROX STA 320. REMOVED CORROSION ON TOP OF LT WALKWAY BEAM FROM STA 320 TO STATION 330 AND ACCOMPLISHED ULTRASOUND THICKNESS TEST (ACCEPTABLE) IAW 727 200 SRM 53-10-4 FIG 7. MECHANICS WROTE ITEM ASSDR 07FDEA03200Beam · corrodedHORIZONTAL WALKWAY BEAM R/SIDE STATION 320 HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON TOP OF RT WALKWAY BEAM FROM STA 328 TO STATION 336 AND ACCOMPLISHED ULTRASOUND THICKNESS TEST (ACCEPTABLE) REFERENCE 727-200 SRM 53- 10-4 FIG 7.SDR C8GA20070007Connector · dirtyFLT 738 FROM SLW TO GDL, DURING CLIMB-OUT FROM SLW, THE INBOARD FLAPS WOULD NOT RETRACT BEYOND 15 DEGREES. APPROPRIATE CHECKLIST WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SLW WHERE IT LANDED WITHOUT INCIDENT. ON POST FLIGHT PERFORMED THOROUGH INSPECTION CHECSDR CA070717017Nut · loose(CAN) ON APPROACH, CREW SELECTED FLAPS FROM 2 TO 5 AND HAD AN AMBER LIGHT INDICATION FOR THE NR 1 KRUGER FLAP INDICATING STILL RETRACTED. FELT MODERATE VIBRATION AND DECLARED AN EMERGENCY. UNEVENTFUL LANDING. MAINTENANCE CYCLED SYSTEM AND COULD NOT FAULT. FUSDR DHL2007742512Splice Plate · crackedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN "A"CHECK REF N/R 138282,138287,138292. MCD LWR SILL BEAM BS 560 TO BS580 SPLICE PLATE CRACKED AT SLOT RADIUS. REMOVED LOCK FITTINGS AND SPLICE PLATES AT BS 560 AND BS 580. FABRICATED NEW SPLICE PLATES AT BS 560 ASDR DHL2007742009Support Angle · crackedDURING AN "A" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, CRACK INDICATION ON RT AIRSTAIR ACTUATOR SUPPORT ANGLE INSIDE TORQUE BOX WEB AT BS 1273. REMOVED CRANKED ANGLE AT RT TORQUE BOX BS 1273 IAW B727 SRM 51-30-2 FIG 7. FABRICATED NEW SUPPORT ANGLE, MATSDR DHL2007742008Splice Plate · crackedDURING AN "A" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES THE FOLLOWING DISCREPANCIES WERE NOTED, MCD LOWER SILL BEAM AT BS 600 AND 620, SPLICE PLATES ARE CRACKED AT SLOT RADIUS (2 EA.) NDT FINDING. REMOVED LOCK FITTING AND SPLICE PLATES AT BS 640 AND 660 IAW B727 SDR DHL2007742007Splice Plate · crackedDURING AN "A" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES THE FOLLOWING DISCREPANCIES WERE NOTED; MCD LOWER SILL BEAM AT BS 640 AND 660, SPLICE PLATES ARE CRACKED AT SLOT RADIUS (2 EA.) NDT FINDING. REMOVED LOCK FITTING AND SPLICE PLATES AT BS 640 AND 660 IAW B727 SDR DHL2007742005Shear Tie · crackedDURING AN "A" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED: FUSELAGE INTERIOR FRAME AT BS 480 AND STR 17L FRAME SHEAR TIE CRACKED, (NDT) FINDING. REMOVED FASTENERS AT SHEAR TIE AND CUT OUT CRACKED SECTION (2" BY 8") OF SHEAR TIE IAW B727 SRM 53-10-4 FIG 11. SDR DHL2007742004Shear Tie · crackedDURING AN "A" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED: FUSELAGE INTERIOR FRAME AT BS 480 AND STR 17L FRAME SHEAR TIE CRACKED (NDT) FINDING. REMOVED FASTENERS AT SHEAR TIE AND CUT OUT CRACKED SECTION (2" BY 8") OF SHEAR TIE IAW B727 SRM 53-10-4 FIG 11. FSDR DHL2007740011Nose Cowl · damagedNR 1 ENG NOSE COWL AT O/B SIDE 9 O`CLOCK POSITION HAS EXISTING REPAIR PULLING LOOSE AND CHAFF MARK. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2 FABRICATED NEW REPAIR USING 2024-T3 .040 PO#9005138 DIM 9" BY 4" AND FILLER USING 2024T3 .032 PO NR 9005049 DIM 5"SDR DHL2007742010Floor Support · crackedA CHECK REF N/R 138248 DISCREPANCY, CRACKED INDICATION ON LT AIRSTAIR AREA UPPER FLOOR SUPPORT INSIDE TORQUE BOW WEB BS 1263. STOPPED DRILLED CRACK TERMINATED CRACK PER B727 SRM 51-10-1. NDT CONFIRMED. FABRICATED REPAIR PART 7075-T6, .063 PO NR 9005314 11 BYSDR DHL2007742003Skin · dentedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN A CHECK, RT O/B FLAP, AFT FLAP LOWER AREA HAS 2 DENTS. REMOVED DAMAGED AREA APPROX 3.2" BY 4" CLEANED AND PREPPED AREA TO ALODINED, FABRICATED FILLER 3.2 BY 4 AND DOUBLER 6.2" BY 5.5 FROM .016" 2024-T3 PO NR 920031SDR DHLA200700031Battery Pack · inoperativeFLIGHT DECK EMERGENCY EXIT LIGHT INOP ON STBY PWR CHECK. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-71, OPS CK NORMAL.SDR CA070530006Warning System · activated(CAN) AFTER DEPARTURE, WHEN AT 13,000 FEET ALT WARNING HORN SOUNDED AND COULD NOT BE SILENCED WITH THE HORN CUTOUT. CREW TRIED SWITCHING TO STBY WITH NO RESULTS. HORN CONTINUED ON APPROACH. AT TIME OF INITIAL HORN, CABIN PRESSURE WAS 5000 FT AND 5PSI DIF. THE SDR C8GA20070005Line · leakingFLT 2819 FROM DFW TO TOL. DURING DESCENT INTO TOL, THE NR 1 ENGINE WAS UNRESPONSIVE TO THROTTLE MOVEMENT. AS PRECAUTIONARY NR 1 ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THE FUEL INLSDR 07FDEA01986Rod · unknownAFTER TAKE OFF FROM MEM, GEAR WAS RET AND THE FWD RED GEAR DOORS LT REMAINED ILLUM WITH ASSOC NOSE GEAR DOOR LT ILLUM ON S/O'S PANEL. C/W QRH, RECYCLED GEAR AND IND REMAINED. CONT'D FLT WITH APPROPRIATE RESTRICTIONS. UPON LDG IN ICT WITH NORM TOUCHDOWN, THESDR 07FDEA01985Stringer · corrodedFWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS- 720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/NSDR 07FDEA01984Stringer · corrodedFWD CARGO A/C DISTRIBUTION BAY LT FLOOR STR-26L BADLY CORRODED APPROXIMATELY FS-720F-740. JUST O/B OF DUCT. REMOVED CORRODED SECTION OF STRINGER AT STA 720C TO 740 AND SPLICED IN A NEW SECTION OF STRINGER ON 26L IAW 727 SRM-53-10-3 FIG 1, STRINGER ORIG P/N#6SDR 07FDEA01980Skin · misrepairedEXTERNAL REPAIR ON FUSELAGE SKIN STA 1111-1127 AND STR 21R-23R DOES NOT COMPLY PER SRM. REMOVED OLD REPAIR IAW SRM 51-30-2. FABBED NEW DOUBLER IAW SRM 53-30-3 FIG 1 FROM MAT.2024T3 0.05, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW DOUBLER IAW SRM 53-3SDR 07FDEA01979Seat Track · corrodedCABIN FLOOR SEAT TRACK HAS CORROSION FS 640 LBL 1". REMOVED CORROSION IAW 727 SRM 51--10-2 FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL IAW SR 53-10-1. FABBED NEW SEAT TRACK IAW SRM 51-30-2 ,TREATED AND PRIMED IAW SRM 51-10-1. REMOVED AND INSTALLED SEASDR 07FDEA01978Stringer · corrodedFWD CARGO COMPT FS 720D-720E STR-26L HAS CORROSION. CUT OUT DAMAGE IAW SRM 53-30-3 FIG 5. FABBED REPAIR DOUBLERS AND FILLER IAW SRM 53-30-3 FIG 5. INSTALLED DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA01841Web · corrodedAFT CARGO STA 970 S-28R WEB HAS CORROSION. REMOVED CORROSION ON WEB AT STA 970 STR 28R CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-6, FABED NEW WEB ON MAE TR T7/679785. INSTALLED THE NEW WEB IAW SRM 51-30-2. INSTALLED STIFFENERS THAT WERE REMOVED PREVIOUSLYSDR 07FDEA01840Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED UPPER SURFACE FROM FSTA 848 - 870, LBL 45 BLENDED SEAT TRACK AT 848 - FS870 LBL 45 FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-30-1 (FIG 1); ORDERED NEW SEAT TRACK PART NR BAC1520-841 BATCH NR 3370-1 AND LOCATED AND DRILLED SDR CA070515003Tube · chafed(CAN) IB, HYDRAULIC A SYS PRESSURE WAS NORMAL ON APPROACH AND QUANTITY REPORTED APPROXIMATELY ZERO. UPON SELECTION OF FLAPS, QUANTITY READ ZERO AND LOW PRESSURE LIGHTS ILLUMINATED. FLIGHT CREW DECLARED AN EMERGENCY AND THE HYDRAULIC FAILURE CHECKLIST WAS CARRISDR 07FDEA01712Bracket · crackedNR 3 PYLON HOLE "P" BRACKET CRACKED FWD OUTBD SEEN INSIDE PYLON AS PER STEP4. 2 ON W/C 7-5410-7-3304. REMOVED AND REPLACED ANGLE( 69-16917-2) IAW SRM 51-30-2 AND 51-10-4. NDT CHECKED "P" HOLE FOR CRACK AND NO CRACK NOTED IAW NTM 51-00-11.SDR 07FDEA01711Spar Cap · crackedRT WING UPPER SURFACE AT SPOILER PANEL NR 11 AREA SPAR CAP HAS CRACK AROUND 3RD HINGE FITTING. NDT NOTED NO CRACKED PER NTM 51-00-00 PT6 (AFTER STOP DRILL). STOP DRILLED 0.025" HOLE AT THE END OF CRACKED IAW SRM 57-30-4 FIG10 SHEET 1/3. TREATED AND PRIMED ISDR C1HA200779001Switch · malfunctionedAFTER EXTENDING LANDING GEAR THE LT AND RT MAIN GEAR GREEN LTS ILLUMINATED AND THE RED NOSE GEAR LT REMAINED ILLUMINATED WITHOUT A GREEN INDICATION. AFTER 2 TO 3 MINUTES THE NOSE GEAR GREEN LIGHT ILLUMINATED AND THE RED LT EXTINGUISHED. REPLACED NOSE GEAR LOSDR CA070427006Attach Bracket · cracked(CAN) DURING A AND B5 INSPECTION NR 7 SLAT ATTACH BRACKET UPPER MOUNT ON FRONT SPAR CRACKED. P/N TO BE DETERMINED FROM MFG ENGINEERING DRAWINGS. RDA ISSUED BY DECA ENGINEERING TO REPAIR. (TC NR 20070427006)SDR 07FDEA01374Support · corrodedDURING PANEL CLOSE UP ON AFT BULKHEAD IN AFT PIT, CENTER LOWER PANEL, UPPER ANGLE CORRODED AROUND FASTENER HOLES. REMOVED CENTER BULKHEAD PANEL SUPPORT ANGLE, REPAIRED BY INSTALLING 2 ANGLES AND A FILLER. RE-INSTALLED PANEL SUPPORT ANGLE REF SRM 51-40-4/FIG SDR DHL2007743506Spar · crackedDISCOVERED WHILE IN "A" CHECK A/C 743DH AT MCO, THEN FERRIED TO VQQ REF ASTAR NR 078282 AND NR 078290. LT WING AFT FALSE SPAR ANGLE JUST FWD OF NR 7 SPOILER FITTING CRACKED IN ANGLE APPROX 2 1/2" LONG STARTING FROM INBD AND RUNNING BELOW FASTENERS. CUT OUT DSDR 07FDEA01370Angle · crackedRT WING, TE LOWER PANEL, BELOW NR 12 SPOILER PANEL, OTBD ATTACH ANGLE, OF THE OTBD SET IS CRACKED AT SUPPORT ROD. REMOVED DAMAGE ANGLE, VERIFIED REPAIR MATERIAL AS 7075-T6 .050 REF IPC 57-30-00 FIG 16 AND DWG 65-21658. FABRICATED REPLACEMENT ANGLE REF FED EXSDR 07FDEA01369Channel · crackedAFT CARGO PIT RT "Z" CHANNEL CRACKED AT RIVET HEAD AT STA 1040 FRAME REPLACED Z-ANGLE REF SRM 51-30-2.SDR 07FDEA01368Attach Fitting · corrodedLT WING NR 1 KRUGER FLAP ALL 3 HINGES, HARDWARE HAS RUST CENTER CASTING AT ACTUATOR ATTACH, 1 HOLE IS CORRODED EDGE DAMAGED. REPLACED NR 1 KRUGER FLAP REFERENCE MM 27-81-001-4 ADJUSTMENT AND CHECK PERFORMED REF W/C70C007-00.
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