Boeing 727-225
Service difficulty reports · 4,226
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 = '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 SCNA00305Web · corrodedDURING HEAVY MAINTENANCE CHECK, ALL MOUNT HOLES FOR THE L1 DOOR TORQUE BOX WERE FOUND CORRODED OUT OF LIMITS. REMOVED CORROSION IAW B727 OHM 521601. REMOVED AND REPLACED L1 DOOR TORQUE BOX IAW B727 OHM 521601. RIGGED L1 DOOR IAW B727 MM 521100 OPS AND LEAK SDR EISA2000031Engine · failedNR 3 ENGINE FAILED DURING TAKEOFF ROLL. RETURNED TO BLOCKS (DAL). REMOVED AND REPLACED NR 3 ENGINE IAW EXPRESS ONE CARD NR 001, AND BOEING MM 71-0. (M)SDR EISA2000034Stringer · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND INTERNAL STRUCTURE OF RIGHT ELEVATOR CRACKED AT STATION 80.56 AS SHOWN IN X-RAY SHOT NR 5R ON REAR STRINGER. STOP DRILLED CRACK. DYE PENETRANT CONFIRMS CRACK TERMINATED. FABRICATED DOUBLER PER SRM 55SDR GAIA00102Light · inoperativeFLT 1850 - SEA-FWA - THE EMERGENCY EXIT LIGHTS DO NOT COME ON WITH SWITCH TURNED ON. THE FLIGHT CONTINUED TO FWA AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULITES. OPERATIONALLY CHECKED SYSTEM AND COULD NOT DUPLICATE. SYSTEM OPS CHECKS GOOD. THE AIRCRAFT SDR EISA2000036Floorbeam · misrepairedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND FLOORBEAM UPPER T-CAP SPLICE REPAIR NOT IN COMPLIANCE WITH VENTURA AEROSPACE STC 00848 LA AND DRW NR 2919 REV C AT FS 344. REMOVED T-CAP FROM FLOORBEAM. FABRICATED NEW T-CAP PER SAMPLE FROM BAC 1505SDR EISA2000037Floorbeam · corrodedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON FLOORBEAM UPPER T-CAP AT FS 1110 LBL 50 TO LBL 57. MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS PER SRM 53-10-8SDR EISA2000028Seal · dirtyAPPROACHING 17,000 FT UNABLE TO CONTROL CABIN PRESSURE DESCENDED TO 10,000 FT TO HOLD 8,500 FT CABIN. AIRTURN BACK TO (CVG). TROUBLESHOT SYSTEM, FOUND DEBRIS AROUND AFT AIRSTAIR ENTRY DOOR SEAL, CLEANED SAME. PRESSURIZED AIRCRAFT WITH APU. OPERATIONS CHECKSDR USAA020006Clamp · brokenFLT 6358 - DCA - AIRCRAFT ON GROUND AT GATE, WITH CREW IN COCKPIT. OCCURRED PRIOR TO PUSHBACK. APU DEACTIVATED PER MEL SEQ 49-1, APU FIRE DETECTION DEACTIVATED PER MEL SEQ 26-11. FOUND APU INNER EXHAUST STACK SEPARATED AT TURBINE OUTLET. REPLACED INNER EXHSDR EISA2000019Warning Light · illuminatedNR 3 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON ASCENT. AIR TURN BACK TO (MTY). (M)SDR SCNA00018Battery Pack · inoperativeDURING A LINE MAINTENANCE CHECK, THE FORWARD AFT FACING EMERGENCY BULL NOSE LIGHT ROW 5 WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE FORWARD AFT FACING BULL NOSE EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS GOOD.SDR DL72S000331Web · crackedFOUND ON F2 LETTER CK, TWO .25 INCH CRACKS ON RT VERTICAL TORQUE BOX WEB AT UPPER LIGHTENING HOLE STA 1288. REPAIRED PER MM 53-11-0.SDR DL72S000310Skin · wornINSTALLED REPAIR PER B727 MM 57-54-0, FIG 813. SLAT WORN.SDR RIVA0000001Feel Unit · bindingEXCESSIVE ELEVATOR CONTROL INPUT REQUIRED DURING LANDING FLARE. MAINTENANCE VISUALLY INSPECTED CABLES AND PULLEYS, NO DAMAGE NOTED. FERRIED AIRCRAFT TO MAINTENANCE BASE. REMOVED AND REPLACED ELEVATOR FEEL UNIT AND ELEVATOR PACK FILTERS. PERFORMED ALL OPERATSDR 00FDEA00060Angle · corrodedCORROSION (C53-100-01,1) ON UPPER PORTION OF HORIZONTAL L ANGLE AT BS 294.5, RBL 11 IN NLG W/W. *S/D* REMOVED AND REPLACED IAW FEDEX SRM 51-30-2 & FEDEX DRAWING 65-18415.SDR 00FDEA00059Skin · corrodedNR 598 - CORROSION (C53-224-05) ON UPPER LEVEL CELL SKIN BS 817, LBL 12, WL 195. REMOVED CORROSION PER FEDEX SRM 51-10-6. REPLACED FASTENERS PER FEDEX SRM 51-30-2 AND FEDEX EA NR 7-5730-47895 AND PERF LEAK CK MM 28-11-00, CK GOOD.SDR 00FDEA00058Skin · dentedDENT IN EXTERNAL SKIN BS 406, STR 17L. *S/D* CUT OUT DAMAGE AND REPAIRED SKIN PER FEDEX SRM 53-30-3 FIG 3.SDR 00FDEA00057Skin · lightning strikeLIGHTNING STRIKE FASTENER HOLE BS 400, 3 INCHES BELOW STR 21 L. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 13A.SDR 00FDEA00056Skin · damagedOUTER SKIN SCRATCHED BS 1031 FROM STR 29L TO STR 29R. *S/D* REPAIRED SKIN PER FEDEX SRM 53-30-3 FIG 3.SDR 00FDEA00055Intercostal · corrodedCORROSION EMANATING FROM FWD END OF DELTA BOX BS 740 FRAME LBL 4 & LBL 9, WL 148. *S/D* REMOVED AND REPLACED INTERCOSTAL PER FEDEX 57-30-2, 57-20-4 SRM & FEDEX DRAWING NR 65-23555.SDR 00FDEA00054Seat Track · corrodedSEAT TRACK AT BS 1030 TO BS 1030+11, LBL 45, WL 208 WAS CORRODED. *S/D* REMOVED FLOOR PNLS BS 990-1110, LBL 45-65, BS 997-1068 LBL 25-45, PER FEDEX 727 SRM 51-30-2 & 51-20-4.SDR 00FDEA00053Angle · corrodedCORROSION (C53-100-01,1) ON LWR END OF VERTICAL L ANGLE AT BS 294.5, LBL 23 IN NLG W/W TORQUE BOX. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-4.SDR DL72S000245Battery · dischargedEMERGENCY EXIT LIGHT ABOVE R2 PASSINGER DOOR INOP. REPLACED BULBS AND BATTERY PACK.SDR DL72S000215Indicator · malfunctionedAFTER T/O UPON SELECTION/RETRACTION OF FLAPS TO 2 DEG. O/B FLAPS RETRACTED TO 4 DEG I/B FLAPS TO 2 DEG. STARTED APPROACH CHECK LIST. O/B FLAPS THEN RETRACTED TO THE SELECTED POSITION 2 DEG. DISCONTINUED CHECK LIST. FLAPS OPERATED NORMAL FOR REMAINDER SDR DL72S000201Fuel Cap · wornAIR TURNBACK, FUEL LEAK FROM THE OVERWING REFUELING CAP LEFT WING. REPLACED CAP, LEAK CHECKED OK.SDR DL72S000204Fuel Port · corrodedFUEL LEAK FROM OVERWING REFUEL CAP ON LEFT WING. REPLACED OVERWING FUEL PORT ASSY.SDR EISA2000009Duct Seal · wornNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AT CLIMB POWER. AIR TURN BACK TO (AEX). REMOVED AND REPLACED 13TH STAGE BLEED DUCT SEAL. (M)SDR 20000425SH022Floorbeam · corrodedFOUND DURING SCHEDULED C-CHECK, CABIN FLOORBEAM STA 344 WALL-TO-WALL HAS SPOTS OF CORROSION. POSSIBLY CAUSED BY LIQUID SPILLS OR DISSIMILAR METAL CONDITION. (X)SDR 20000425SH021Beam · misrepairedFOUND DURING SCHEDULED C-CHECK, J-BEAM HAS ROUTED OUT SECTION AT TOP OF CUT OUT WITH PREVIOUS REPAIR ABOVE LEFT WING NR 7 SPOILER ACTUATOR AREA. (X)SDR 20000425SH020Floorbeam · corrodedFOUND DURING SCHEDULED C-CHECK, CABIN FLOORBEAM STA 360 BL 24 TO 24 CORROSION AT ANCHOR NUT HOLES. POSSIBLY CAUSED BY LIQUID SPILLS OR DISSIMILAR METAL CONDITION. (X)SDR 20000425SH019Beam · misrepairedFOUND DURING SCHEDULED C-CHECK, J-BEAM HAS ROUTED OUT SECTION AT TOP OF CUT-OUT WITH PREVIOUS REPAIR ABOVE RT WING NR 8 SPOILER ACTUATOR AREA.SDR 20000425SH018Floorbeam · corrodedFOUND DURING SCHEDULED C-CHECK, CABIN FLOORBEAM STA 314 BL ZERO HAS CORROSION. POSSIBLY CAUSED BY LIQUID SPILLS OR DISSIMILAR METAL CONDITION. (X)SDR 20000428AP001Relief Valve · failedDURING TAKEOFF AND CLIMB-OUT FROM MIA, NR 3 ENGINE OIL PRESSURE INCREASED TO 85 PSI. REDUCED THROTTLE TO IDLE AND PRESSURE DECREASED THEN INCREASED TO 90 PSI. SHUTDOWN NR 3 ENGINE THEN FOLLOWED AOM ABNORMAL PROCEDURES AND DECLARED EMERGENCY. RETURNED TO MIASDR MYWA000004O-Ring · damagedLOG PAGE 37837. ON TAKEOFF ALL NORMAL, THEN NR 3 ENGINE OIL PRESSURE WENT TO 65 PSI CONSTANT. RETURNED TO MIAMI, DID NOT SHUT DOWN ENGINE AND NO EMERGENCY DECLARED. CANCELLED FLIGHT. FOUND O-RING ON PRESSURE RELIEF VALVE DAMAGED, REPLACED O-RING. AS PRECASDR EISA2000007Arm · out of adjAFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE, DUE TO L1 DOOR NOT BEING CLOSED. RETURNED TO IND. ADJUSTED GUIDE ARM IAW MM 52-11, OPS CHECK GOOD. (M)SDR USAA010004Actuator · fracturedDCA/LGA - FLT 6378 - LOST A-SYSTEM HYDRAULICS ON FLAP EXTENSION. DIVERTED TO EWR. FOUND AFT END OF NR 8 L/E SLAT ACTUATOR BROKEN. REPLACED NR 8 L/E SLAT ACTUATOR. CHECKED RETURN AND CASE DRAIN FILTERS.SDR SCNA99158Sign · inoperativeDURING A LINE MAINTENANCE CHECK, THE EMERGENCY EXIT IDENTIFIERS AT THE RT OVERWING DOORS WERE FOUND INOPERATIVE. REPAIRED SPLICES FOR RT OVERWING EXIT IDENTIFIERS PER WPM 203012. LIGHTS OP CHECKED GOOD PER MM 33590.SDR SCNA99779Fitting · crackedDURING A HEAVY MAINTENANCE CHECK, THE LEFT MAIN LANDING GEAR BEAM OUTBOARD SUPPORT FITTING WAS FOUND TO BE CRACKED. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR BEAM SUPPORT FITTING IAW SB 72757167.SDR DL72S992786Battery Pack · dischargedEMERGENCY LIGHT ABOVE R2 DOOR INOP. REPLACED BATTERY PACK, OPS NORMAL.SDR SCNA99778Seat Track · corrodedDURING A HEAVY MAINTENANCE CHECK, THE RIGHT FORWARD GALLEY INBOARD SEAT TRACK TIE DOWNS WERE FOUND TO BE CORRODED OUT OF LIMITS. FABRICATED NEW SEAT TRACK FROM STA 1070 TO STA 1110. TREATED, PRIMED AND INSTALLED NEW SEAT TRACK PER SRM 51302 AND 51202.SDR SCNA99777Seat Track · corrodedDURING A HEAVY MAINTENANCE CHECK THE LEFT AFT GALLEY OUTBOARD SEAT TRACK TIE DOWNS WERE FOUND TO BE CORRODED OUT OF LIMITS. FABRICATED NEW SEAT TRACK FROM STA 1070 TO STA 1110. TREATED, PRIMED AND INSTALLED NEW SEAT TRACK PER SRM 51302 AND 51202.SDR 20000511AP029Beam · crackedFOUND J BEAM HAS TWO .375 INCH CRACKS AT LEFT WING TRAILING EDGE AREA ABOVE NR 7 SPOILER ACTUATOR AREAS. REMOVED WALKING BEAM PANEL AND SMALL SKIN PANEL IAW 51-30-2 PAGE 2. REMOVED J BEAM IAW 51-30-2 PAGE 1. INSTALLED J BEAM IAW 51-30-2 PAGE 4. INSTALLED RSDR 20000511AP028Beam · crackedFOUND J BEAM HAS .375 INCH CRACK AT RIGHT WING ABOVE NR 8 SPOILER ACTUATOR AREA. REMOVED RIGHT WING TOP SKIN AND WALKING BEAM PANEL IAW 51-30-2 PAGE 2. REMOVED J BEAM AT RIGHT WING ABOVE NR 8 SPOILER. INSTALLED NEW J BEAM IAW 51-30-2 PAGE 1. INSTALLED REMOSDR 20000511AP027Retainer · crackedSEAL RETAINER CRACKED ABOVE RIGHT ELEPHANT EAR FAIRING ON AFT SEGMENT. REMOVED SEAL RETAINER, DRILLED HOLES IN NEW RETAINER IAW 51-30-2 PAGE 5. INSTALLED RETAINER IAW 51-30-2 PAGE 5. (M)SDR 20000511AP026Web · crackedVERTICAL FIN LEADING EDGE PANEL 9602 INNER CURVED WEB HAS 1 INCH CRACK AT CORNER. STOP DRILLED CRACK IAW 51-10-1 PAGE 613. FABRICATED DOUBLER IAW 51-40-2 PAGE 2, 3, 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED DOUBLER AND WEB IAW 51-30-2 PAGE 1. (MSDR 20000511AP025Web · tornVERTICAL LEADING EDGE CENTER SECTION INTERIOR WEB IS DAMGED AT THREE CORNERS. CUT OUT DAMAGED AREAS IAWS 51-40-2 PAGES 2/3. HFEC SHOWS NO CRACKS IAW 51-00-00 PAR 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED REPAIR IAW 51-40-2. (M)SDR 20000511AP024Bracket · crackedFOUND NR 7 SPOILER OUTBOARD HINGE SUPPORT CRACKED. REMOVED CRACKED HINGE SUPPORT BRACKET. DRILLED NEW SUPPORT BRACKET IAW 51-10-1 PAGE 14. INSTALLED NEW HINGE SUPPORT BRACKET IAW 51-10-1 PAGE 1. (M)SDR 20000511AP023Floorbeam · corrodedTOP OF FLOORBEAM BS 1110 BL 0 - LBL 12 AND BL 0 - RBL 12. REMOVED CORROSION IAW 51-10-6 PAGE 2. AREA OUT OF LIMITS. CUT OUT DAMAGED AREA IAW 53-10-8 FIG 8. FABRICATED ANGLE AND FILLER REPAIR IAW 53-10-8 FIG 8 SHEET 4-5. ACCOMPLISHED HFEC AROUND EDGES OF CSDR 20000511AP022Flap Track · corrodedRIGHT OUTBOARD MID FLAP INBOARD TRAILING EDGE FLAP TRACK CORRODED. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED RETAINER IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNEL IAW 51-30-3 PAGE 2. (M)SDR 20000511AP021Floor Support · corrodedFOUND FLOOR SUPPORT BS 1110 TO 1130 LBL 12 CORRODED. REMOVED FLOOR SUPPORT IAW 51-30-2 PAGE 1. FABRICATED SUPPORT IAW 51-10-1 PAGE 2. TREATED AND PRIMED IAW 51-10-2. INSTALLED FLOOR SUPPORT IAW 51-30-2 PAGE 1. (M)SDR 20000511AP020Floorbeam · groovedFOUND FLOORBEAM BS 1110 LBL 45 HAS 2.5 INCH GROOVE CENTER OF TOP FLANGE. REMOVED WEB, SIDE WALLS AND SEAT TRACK. CUT OUT DAMAGED AREA IAW 53-10-2 FIG 3. ACCOMPLISHED HFEC INSPECTION AROUND EDGES OF CUTOUT IAW 51-00-00. NO CRACKS NOTED. FABRICATED FLOORBEA
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