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.

SDR EISA99224Skin · delaminatedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED DELAMINATION OF LEFT OUTBOARD AFT FLAP TRAILING EDGE AT INBOARD CORNER. REPAIRED DELAMINATION WITH FIBERGLASS AND POTTING REPAIR PER SRM 57-50-4 AND SRM 51-40-6. TT: 65,345:17 HOURS. TC: 43,816. (X)Nov 12, 1999 · N353PA · Boeing 727225 · Trailing Edge FlapsSDR EISA99223Skin · gougedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A GOUGE ON LEADING EDGE OF LEFT INBOARD TRAILING EDGE FLAP. BLENDED GOUGE PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2. TT: 65,345:17 HOURS. TC: 43,816. (X)Nov 12, 1999 · N353PA · Boeing 727225 · Trailing Edge FlapsSDR EISA99222Skin · delaminatedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED AREA OF DELAMINATION ON LOWER RUDDER TAB, UPPER TRAILING EDGE, LEFT CENTER AND UPPER LEFT SIDE AND LOWER SURFACE. ACCOMPLISHED HONEYCOMB REPAIR TO ALL AREAS PER SRM 51-40-6. TT: 65,345:17 HOURS. TC: 4Nov 12, 1999 · N353PA · Boeing 727225 · Rudder Tab Control SystemSDR DHL99742003Actuator · looseNR 1 L/E SLAT WOULD NOT RETRACT. FOUND NR 1 L/E SLAT ACTUATOR LOOSE IN MOUNT. TIGHTENED 4 MOUNT BOLTS, PERFORMED SYSTEM ADJ AND TEST. LIGHTS OPS CHECK GOOD PER MM 27-82-0.Nov 12, 1999 · N742DH · Boeing 727225 · Leading Edge Slat ActuatorSDR 20000615AP007Slat Track · crackedDURING C-CHECK, FOUND .375 INCH CRACK AT LT WING FIXED L/E CUTOUT ABOVE NR 4 SLAT OUTBOARD TRACK. TRIMMED OUT DAMAGED SKIN AND FABRICATED DOUBLER AND FILLER, INSTALLED REPAIR PER SRM 57-30-4, PAGE 6. (M)Nov 11, 1999 · N802EA · Boeing 727225 · Leading Edge DevicesSDR 20000615AP006Rib · crackedDURING C-CHECK, FOUND RIGHT WING L/E RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M)Nov 11, 1999 · N802EA · Boeing 727225 · Wing, Rib/BulkheadSDR 20000615AP005Angle · crackedDURING C-CHECK, FOUND RIGHT WING RIB HAS 1 INCH CRACK WS 330. STOP DRILLED CRACK PER SRM 51-40-3 PAGE 1, FABRICATED ANGLE DOUBLER AND INSTALLED PER SRM 51-30-2 PAGE 2. (M)Nov 11, 1999 · N802EA · Boeing 727225 · Wing Miscellaneous StructureSDR 20000613AP008Beam · damagedDURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH IMPROPER PREVIOUS REPAIR ABOVE LEFT WING NR 7 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M)Nov 11, 1999 · N802EA · Boeing 727225 · Wing Miscellaneous StructureSDR SCNA99136Battery Charger · inopDURING A LINE MAINTENANCE CHECK, THE AFT CARGO DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK CHARGER. OPERATIONALLY CHECKS NORMAL.Nov 11, 1999 · N282SC · Boeing 727225 · Emergency LightingSDR EISA99226Floorbeam · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON BS 1030 FLOORBEAM T-CAP AT BL ZERO. REMOVED CORROSION AND MATERIAL LOSS OF LIMITS PER SRM 53-10-3. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8. TT: 65,345:17 HOURS. TC: 43,816. (X)Nov 11, 1999 · N353PA · Boeing 727225 · Fuselage Main, Floor BeamSDR DL72S992497Web · crackedVERT WEB OF LT LOWER TORQUE BOX IN 48 SECTION CRACKED AT STA 1235 AT UPPER RIVET ROW .25 INCH. INSTALLED DOUBLER PER M/M 53-11-0- NR 19, A-1 LETTER CHECK.Nov 11, 1999 · N8875Z · Boeing 727225 · Fuselage Miscellaneous StructureSDR EISA99240Seat Track · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON MAIN CABIN SEAT TRACK AT LBL 24 AT BS 990 TO BS 1130. REMOVED CORROSION AND MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED TRACK SECTION AND FABRICATED NEW SECTION PER SAMPLENov 10, 1999 · N353PA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR EISA99230Seat Track · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND CORROSION ON MAIN CABIN SEAT TRACK AT BS 680 TO BS 740, RBL 45. REMOVED CORROSION PER SRM 51-10-6. MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED TRACK SECTION AND FABRICATED NEW SECTION PER SAMPLE. INov 10, 1999 · N353PA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000613AP009Seat Track · corrodedDURING C-CHECK, FOUND CABIN SEAT TRACK STATION 680 TO 740 LBL 24 HAS CORROSION OUT OF LIMITS PER SRM 53-10-1, PAGE 16. REMOVED AND FABRICATED SEAT TRACK, INSTALLED PER SRM 51-30-2 PAGE 1. (M)Nov 9, 1999 · N802EA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR USAA020003Battery Pack · dischargedFOUND ON L/S - R-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKS OK. (M)Nov 6, 1999 · N919TS · Boeing 727225 · Emergency LightingSDR SCNA99132Light · inopDURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRES AT AISLE BY LIGHT ASSEMBLY IAW MM 33501.Nov 6, 1999 · N282SC · Boeing 727225 · Emergency LightingSDR SCNA99133Light · inopDURING A LINE MAINTENANCE CHECK, AN EMERGENCY FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT SEAT ROW 16. REMOVED AND REPLACED THE LIGHT LAMP HOOLDER ASSEMBLY. LIGHT OPERATIONALLY CHECKS GOOD REF MM 335900.Nov 5, 1999 · N283SC · Boeing 727225 · Emergency LightingSDR EISA99242Skin · delaminatedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED DELAMINATION ON TOP SURFACE OF NR 2 SPOILER PANEL. REPAIRED TOP LEFT CORNER OF PANEL WITH FIBERGLASS REPAIR PER SRM 57-50-6 PAGE 611. TT: 65,345:17 HOURS. TC: 43,816. (XNov 4, 1999 · N353PA · Boeing 727225 · SpoilersSDR EISA99236Skin · crackedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A CRACK IN FUSELAGE SKIN AT UPPER HINGE CUT-OUT AT FORWARD ENTRY DOOR. TRIMMED DAMAGED AREA PER SB 727-53-0198. FABRICATED AND INSTALLED DOUBLER PER SB 727-53-0198. TT: 65,345:17 HOURS. TC: 43,816. (XNov 4, 1999 · N353PA · Boeing 727225 · Fuselage Main, Plate/SkinSDR EISA99235Seat Track · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON MAIN CABIN SEAT TRACK AT LBL 45 FROM BS 950 AFT TO BS 1030. REMOVED CORROSION AND MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED SEAT TRACK AND REPLACED WITH NEW SECTION FABRICATED PER SNov 4, 1999 · N353PA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR EISA99234Floorbeam · gougedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION OF FLOOR SUPPORT IN MAIN CABIN BETWEEN BS 1166 AND AND BS 1183 LBL 19. REMOVED DAMAGED AREA PER SRM 51-10-6, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-50-2. TT: 65,345:17 HOURS. Nov 4, 1999 · N353PA · Boeing 727225 · Fuselage Main, Floor BeamSDR EISA99233Skin · gougedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED LEFT OUTBOARD FOREFLAP WS 417 GOUGED UNDER LEADING EDGE. REMOVED DAMAGED AREA PER SRM 51-10-1, FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4. TT: 65,345:17 HOURS. TC: 43,816. (X)Nov 4, 1999 · N353PA · Boeing 727225 · Leading Edge DevicesSDR EISA99232Skin · delaminatedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED AREA OF DELAMINATION ON RIGHT WING OUTBOARD FOREFLAP, INBOARD TRAILING EDGE. REPAIRED TRAILING EDGE WITH FIBERGLASS REPAIR PER SRM 51-40-6. TT: 65,345:17 HOURS. TC: 43,816. (X)Nov 4, 1999 · N353PA · Boeing 727225 · Leading Edge DevicesSDR 2000ZZZM85Fitting · crackedJFK - ON FINAL APPROACH, AIRCRAFT LOST 'A' SYSTEM HYDRAULICS. MADE UNEVENTFUL LANDING, UNABLE TO TAXI A/C DUE LOSS OF FLUID IN NOSE STEERING SYSTEM. ON INSPECTION FOUND NLG DOWNLOCK ACTUATOR HYDRAULIC LINES DAMAGED AND DOWNLOCK SUPPORT CHANNEL FLANGE ON AFT Oct 31, 1999 · N804MA · Boeing 727225 · Hydraulic System, MainSDR 20000505AP026Bracket · crackedRT MLG DEBOOSTER VALVE BRACKET CRACKED AT TOP CENTER EDGE. STOP DRILLED CRACK, HFEC TO VERIFY CRACK CONTAINMENT. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 SHEET 4. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Main Landing GearSDR 20000505AP025Rib · crackedFOUND .625 INCH CRACK IN INBOARD MOST RIB OF THE LEFT OUTBOARD MIDFLAP. STOP DRILLED CRACK, HFEC TO VERIFY CRACK CONTAINMENT. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 SHEET 4. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Trailing Edge FlapsSDR 20000505AP024Skin · crackedNR 6 SLAT INNER SKIN CRACKED AT FASTENER. INSTALLED REPAIR PER SRM 57-50-3 FIG 1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Leading Edge DevicesSDR 20000505AP023Skin · crackedNR 6 SLAT OUTBOARD, HOOK CUTOUT CRACKED. INSTALLED REPAIR PER SRM 57-30-4 FIG 9. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Leading Edge DevicesSDR 20000505AP022Fairing · crackedNR 5 FLAP TRACK MOVEABLE FAIRING, FORWARD RIB CRACKED AT LOCK BOLT SAFETY WIRE HOLE. INSTALLED REPAIR PER SRM 51-40-3 PAGE 3. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Aerodynamic FairingsSDR 20000505AP021Flange · corrodedAPU AIR INLET SCREEN MOUNTING FLANGE CORRODED ALONG BOTTOM FLANGE. FABRICATED REPLACEMENT FLANGE (ANGLE) PER SRM 51-10-1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 20000505AP020Bracket · crackedFOUND 3 INCH CRACK IN NR 8 JACKSCREW FARING AT AFT MOUNT. REMOVED DAMAGED BRACKET AND FABRICATED REPLACEMENT PART. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing Miscellaneous StructureSDR 20000505AP019Skin · crackedFOUND .375 INCH CRACK IN LOWER SURFACE OF RIGHT OUTBOARD FORE FLAP AT THE OUTBOARD ATTACHMENT AREA. INSTALLED REPAIR PER SRM 57-50-4 FIGURE 7. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Leading Edge DevicesSDR 20000505AP018Skin · crackedFOUND .5 INCH CRACK AT LEADING EDGE OF RIGHT OUTBOARD FORE FLAP ADJACENT TO NR 7 FLAP TRACK. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED PER SRM 57-50-4 FIG 7. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Leading Edge DevicesSDR 20000505AP017Rib · crackedFOUND NR 1 INCH CRACK AT BOTTOM OF RIB NR 6 SLAT ADJACENT TO INBOARD SIDE OF ACTUATOR ROD END ATTACHMENT. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 51-40-3. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing, Rib/BulkheadSDR 20000505AP016Rib · crackedFOUND .5 INCH CRACK AT LEFT WING TRAILING EDGE RIB, FROM AFT END TO RIVET HOLE, JUST FORWARD OF OUTBOARD AILERON OUTBOARD HINGE AREA. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE, TREATED, PRIMED AND PAINTED. INSTALLED IAW 51-40-3. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing, Rib/BulkheadSDR 20000505AP015Angle · crackedFOUND 1.25 INCH CRACK AT ANGLE INSIDE LEFT WING TRAILING EDGE AT OUTBOARD END OF AFT FALSE SPAR ACCESS THROUGH PANEL 8407. REMOVED ANGLE AND FABRICATED REPLACEMENT ANGLE AND INSTALLED IAW 51-10-1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing Miscellaneous StructureSDR 20000505AP014Skin · crackedFOUND .3125 INCH CRACK AT LEFT WING, UPPER SURFACE AT NR 4 OUTBOARD HOOK CUTOUT, AT AFT OUTBOARD CORNER. STOP DRILLED CRACK, PERFORMED HIGH FREQUENCY EDDY CURRENT TO ENSURE CRACK CONTAINMENT. REPAIR INSTALLED PER SRM 57-30-4. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing, Plate/SkinSDR 20000505AP012Wire · shortedFORWARD E-PATH LIGHT STRIP INOPERATIVE ON TEST. REPLACED SHORTED WIRING CABLE LEAD ASSY. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Light System WiringSDR 20000505AP011Frame · crackedWING TRAILING EDGE CHORD ANGLE CRACKED BELOW NR 8 SPOILER (WBL 125.0). REPAIRED CRACK PER BOEING SERVICE BULLETIN 727-57-158 R1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing Main, Frame StructureSDR 20000505AP010Skin · corrodedLEFT WING LOWER SKIN HAS CORROSION IN SEVEN LOCATIONS BETWEEN WING STATION 165 AND WING STATION 270 BELOW FRONT SPAR. REMOVED CORROSION FROM SEVEN LOCATIONS BLENDED DAMAGE, COLD WORKED HOLES, FLAP PEENED SURFACE AND REPLACED FASTENERS PER BOEING INSTRUCTION MOct 27, 1999 · N887MA · Boeing 727225 · Wing, Plate/SkinSDR 20000505AP009Floorbeam · corrodedFOUND CABIN FLOORBEAM AT STATION 1130, RBL 36, CORROSION AROUND SCREW HOLES. REPAIRED FLOORBEAM PER JOSSAIR DWG NR 72R5371137 FROM LBL 65 TO RBL 65. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage Main, Floor BeamSDR 20000505AP008Skin · puncturedFOUND SKIN PUNCTURED NEAR FORWARD JACK PAD. REPAIRED SKIN PER BOEING INSTRUCTION MIA-99-00029H. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage Structure (General)SDR 20000502AP012Bracket · crackedFOUND BRACKET CRACKED AT RIGHT WING LOWER TRAILING EDGE SUPPORT, OUTBOARD OF NR 6 FLAP TRACK. REMOVED DOUBLER FABRICATED NEW DOUBLER PER SRM 51-40-2 FIG 1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing Miscellaneous StructureSDR 20000502AP011Support Bracket · corrodedFOUND CABIN R1 DOOR SILL 4 EACH SUPPORT BRACKETS CORRODED. FABRICATED NEW BRACKETS AND REPLACED PER SRM 51-10-1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 20000502AP010Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 480 TO STATION 690 LBL 24. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000502AP009Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 480 TO STATION 690 LBL 45. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000502AP008Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 680 TO STATION 740 LBL 24. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000502AP007Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990, RBL 45. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000502AP006Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990, RBL 45. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000502AP005Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990 RBL 24. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 1 SHEET 4. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
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