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 20000511AP019Support Bracket · bentSUPPORT FOR CONDUIT CRACKED AND BENT BS 1110 TO 1130 LBL 33. REMOVED DAMAGED U CHANNEL SUPPORT AND ANGLE BRACKET IAW 51-30-2 PAGE 1/2. FABRICATED NEW U CHANNEL IAW 51-40-3 PAGE 3. TREATED, PRIMED AND PAINTED IAW 51-10-2 PAGE 2. INSTALLED U CHANNEL SUPPORT SDR 20000511AP018Angle · crackedCABIN FLOOR SUPPORT INTERCOSTAL TOP ANGLE CRACKED AT SCREWHEAD BL 0 BETWEEN BS 950A AND 950B. REMOVED ANGLE IAW 51-30-2 PAGE 2. FABRICATED NEW ANGLE IAW 51-40-2 PAGE 3. TREATED AND PRIMED IAW 51-10-2. INSTALLED ANGLE IAW 51-30-2 PAGE 12. (M)SDR 20000511AP017Retainer · corrodedFOUND SEAL RETAINER CHANNEL CORRODED, LOCATED AT TRAILING EDGE OF RIGHT OUTBOARD MID FLAP. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED NEW RETAINER CHANNEL IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNESDR 20000511AP016Skin · crackedVERTICAL STABILIZER LOWER LEADING EDGE FAIRING NR 9501 HAS .5 INCH CRACK IN SKIN AND CHAFED AROUND END. CUT OUT DAMAGED AREA IAW 51-40-2 FIG 1. FABRICATED DOUBLER IAW 51-40-2 FIG 1. INSTALLED REPAIR IAW 51-30-2 PAGE 2. (M)SDR 20000511AP015Angle · damagedCABIN FLOOR PANEL SUPPORT RIB BETWEEN STATION 720F AND 740 BL 0 TORN. REMOVED ANGLE SUPPORT BETWEEN STATION 720F TO 740 AT BL 0 IAW 51-30-2 PAGE 1. FABRICATED ANGLE SUPPORT IAW 53-10-4 PAGE 2. TREATED, PRIMED AND INSTALLED IAW 51-10-2 AND 51-30-2 PAGE 1. (SDR 20000511AP014Fairing · crackedFOUND .75 INCH CRACK AT TOP OF RIGHT INBOARD FLAP AFT TEARDROP FAIRING. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT TEARDROP FAIRING. (M)SDR 20000511AP013Fairing · crackedFOUND 1.5 INCH CRACK AT AFT MOUNT HOLE OF LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. (M)SDR 20000511AP012Bracket · crackedOUTBOARD BRACKET CRACKED .375 INCH AT INBOARD TRACK OF LET WING NR 3 SLAT WHERE SKIN ATTACHES. REMOVED DAMAGED BRACKET AND FASTENERS IAW 51-30-2 PAGE 6. FABRICATED BRACKET IAW 51-20-1 PAGE 8. TREATED, PRIMED AND INSTALLED IAW 51-30-2 PAGE, 51-20-1 PAGE 18, SDR 20000511AP011Seat Track · corrodedFOUND CABIN SEAT TRACK STATION 360 TO 440 RBL 48 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 12 FOUND OUT OF LIMITS IAW 51-10-1 PAGE 15. FABRICATED NEW SEAT TRACK IAW 53-10-5 PAGE 21. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW 53-10-5 PAGE 21. (M)SDR 20000511AP010Seat Track · corrodedFOUND CABIN TRACK STATION 360 TO 420 RBL 24 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 2 FOUND OUT OF LIMITS. FABRICATES SEAT TRACK IAW 51-10-1. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED TRACK IAW 51-30-2. (M)SDR 20000511AP009Seat Track · corrodedCABIN FLOORBEAM STATION 320 LBL 46 HAS CORROSION AT ANCHOR NOT. REMOVED CORROSION IAW 51-10-6 PAGE 12. ACCOMPLISHED UT THICKNESS CHECK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW 53-10-8 PAGE 49. FABRICATED ANGLES AND SPLICE, INSTALLED, TREATED IAW 53-10SDR 20000511AP008Seat Track · corrodedFOUND CABIN SEAT TRACK LBL 44 STATION 1110 TO 1070 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-10-6 PAGE 6. REMVOED SEAT TRACK IAW 51-30-2 PAGE 5. FABRICATED SEAT TRACK IAW 53-10-5 PAGE 4. TREATED AND PRIMED IAW 51-10-2 PAGE 6. INSTALLED TSDR 20000511AP007Seat Track · corrodedFOUND CABIN SEAT TRACK STATION 1070 LBL 50 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-30-2 PAGE 2. REMOVED HAT CHANNEL STATION 1070 LBL 50 IAW 51-30-2 PAGE 2. FABRICATED HAT CHANNEL IAW 51-10-1 PAGE 2. TREATED INSTALLED HAT CHANNEL IAW 51-1SDR 20000511AP006Strap · crackedFOUND .03125 INCH CRACK AT RIGHT WING FIXED LEADING EDGE AT AFT INBOARD END OF CUTOUT WHERE NR 5 SLAT INBOARD HOOK GOES INTO. REMOVED FASTENERS IAW 51-30-2 PAGE 1-2. STOP DRILLED CRACK IAW 51-10-1 PAGE 6. HFEC INSPECTION CONFIRMED CRACK CONTAINED IAW 51-00-SDR 20000511AP005Hinge · crackedFOUND .3125 INCH CRACK AT CUT OUT ON TOP OF LEFT WING FOR NR 4 SPOILER 2ND FROM OUTBOARD HINGE. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC INSPECTION CONFIRMED CRACK CONFINED IAW 51-30-2 PAGE 1. FABRICATED DOUBLER REPAIR IAW 57-30-4 FIG 10.8 PAGE 3. TREASDR 20000511AP004Seat Track · corrodedCABIN SEAT TRACK STATION 344 TO 400 LBL 44 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 53-10-1 FIG 3. FABRICATED SEAT TRACK IAW 51-30-5 PAGE 1. TREATED INSTALLED IAW 51-10-2 PAGE 1 AND 51-30-2. (M)SDR 20000511AP003Seat Track · crackedCABIN SEAT TRACK STATION 344-400 LBL 24 HAS CORROSION. REMOVED CORROSION AND FOUND SEAT TRACK OUT OF LIMITS IAW 51-10-6 PAGE 12. FABRICATED NEW SEAT TRACK STATION 344-400 LBL 24 IAW 53-10-5 PAGE 4. TREATED AND PRIMED IAW 51-10-2 PAGE 2-4. INSTALLED SEAT TRSDR 20000511AP002Angle · crackedFLAP FAIRING SUPPORT ANGLE HAS 1.125 INCH CRACK AT INBOARD SIDE OF LEFT WING NR 3 FLAP TRACK BELOW AFT FALSE SPAR AREA. REMOVED FAIRING, ACCOMPLISHED HFEC INSPECTION CONFIRMED ENDS OF CRACK IAW 51-00-00 PAGE 6. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC ISDR 20000511AP001Angle · crackedANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATED NEW ANGLE IAW 51-10-1 PAGE 2. INSTALLED ANGLE IAW 51-10-2 PAGE 1. (M)SDR 20000510AP007Skin · crackedFOUND .4374 INCH CRACK THROUGH FASTENER HOLE AT RIGHT OUTBOARD FOREFLAP LEADING EDGE ABOVE NR 7 FLAP TRACK AREA. STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 1. FABRICATED COUPLER REPAIR IAW 57-50-4 PAGE 17. HFEC INSPECTION OF CUTOUT CONFIRMED NO CRACKS. FABRICSDR 20000510AP006Rib · crackedFOUND .75 INCH CRACK AT RIGHT WING OUTBOARD MIDFLAP INBOARD MOST RIB AT LOWER AFT END. REMOVED JACKSCREW FAIRING. FABRICATED SINGLE REPAIR IAW 57-50-2 PAGE 5. HFEC CONFIRMED CRACK IS CONTAINED BY STOP HOLE IAW 51-00-00 PAGE 6. INSTALLED ANGLE REPAIR IAW 57SDR 20000510AP005Skin · crackedFOUND .5 INCH CRACK AT FASTENER HOLE AND TWO RIVETS CRACKED LOWER LEADING EDGE SKIN OF LEFT WING NR 3 SLAT BELOW UPSTOP PAD AREA. ACCOMPLISHED HFEC INSPECTION AND MARKED END OF CRACK IAW 51-00-00 PART 6. STOPPED DRILLED END OF CRACK IAW 51-10-1 PAGE 3. HFEC SDR 20000510AP004Web · crackedFOUND 1.75 INCH CRACK AT LEFT WING OUTBOARD MID FLAP INBOARD MOST RIB AT LOWER AFT END. STOP DRILLED CRACK IAW SRM 51-10-1. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. HFEC INSPECTION CONFIRMED CRACK WAS CONTAINED. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. SDR 2000ZZZM234Pump · failedUPON DEPARTURE FROM MCO, NR 1 ENGINE EPR DROPPED TO 1.4 AND N1 TO 80 PERCENT WITH A THROTTLE EVEN WITH NR 2 AND NR 3 AS WE CONTINUED CLIMBING THE ENGINE CONTINUED DECREASING.. BROUGHT ENGINE THROTTLE TO IDLE AND LOST CONTROL OF THE ENGINE WITH THE THROTTLE OISDR 20000609AP010Angle · crackedDURING C-CHECK, FOUND NR 1 ENGINE PYLON T/E RIB ATTACH ANGLE CRACKED AND RIB HOLES ELONGATED. REMOVED CRACKED ANGLE, FABRICATED NEW REPAIR PARTS PER SRM 51-40-2. INSTALLED NEW REPAIR PARTS AND SEALED AREA PER SRM 51-10-1 AND SRM 51-40-2. (M)SDR DL72S992607Seal · leakingAIRCRAFT WOULD NOT HOLD SCHEDULED CABIN PRESSURE WITH SINGLE PACK OPS AT FL 210. CABIN WAS 8000 FT, CLIMBING 500-700 FEET PER MIN. DESCENDED TO 15,000 TO HOLD LEVEL AT 8000 FEET CABIN PRESSURE. PRESSURIZED ACFT. FOUND AIR LEAKS AT L-1 AND R-1 DOOR SCUFF PLSDR DL72S992582Angle · crackedLOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 6 SLAT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812 & ERA 368813-14.SDR DL72S992579Angle · crackedCOVE SKIN ANGLE CRACKED NR 3 SLAT I/B OF ACTUATOR ROD END REPAIR PER MM 57-54-0.SDR DL72S992578Angle · crackedCOVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0.SDR 20000613AP007Beam · damagedDURING C-CHECK, FOUND J BEAM HAS ROUTED OUT SECTION AT TOP OF CUTOUT WITH PREVIOUS REPAIR ABOVE RIGHT WING NR 8 SPOILER ACTUATOR AREA. REMOVED AND REPLACED J BEAM PER SRM 51-30-2 PAGE 4. (M)SDR 20000522AP004Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM STATION 314 BL 0 HAS CORROSION. REMOVED CORROSION PER SRM 51-10-6, FOUND OUT OF LIMITS PER SRM 53-10-8, CUT OUT DAMGED FLOORBEAM IAW SRM 53-10-8, PERFORMED HFEC INSPECTION. NO CRACKS NOTED PER SRM 51-10-00. FABRICATED NSDR 20000522AP003Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM STATION 344 WALL TO WALL HAS SPOTS OF CORROSION. REMOVED AND FABRICATED NEW FLOORBEAM PER SRM 51-10-1 PAGE 14. TREATED AND PRIMED PER SRM 51-10-6 PAGE 2. INSTALLED FLOORBEAM PER SRM 53-10-1 PAGE 14. (M)SDR 20000522AP002Floorbeam · corrodedDURING C-CHECK, FOUND CABIN FLOORBEAM STATION 360 BL 24 TO 24 CORROSION AT ANCHOR NUT HOLES. NOTED 1 INCH CRACK AT RBL 5 UNDER FORWARD FLANGE. REMOVED CORROSION TO AFFECTED AREA IN ANCHOR NUT HOLES, WITHIN LIMITS IAW SRM 51-10-6. AT 1 INCH CRACK REMOVED CORSDR EISA99243Floorbeam · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON LOWER SURFACE OF UPPER FLOORBEAM CHORD AT BS 1166 LBL 28. REMOVED CORROSION AND MATERIAL LOSS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLES AND INSTALLED REPAIR PER SRM 53-10-8 AND SRM 5SDR EISA99221Floorbeam · corrodedACCOMPLISHEMNT OF A ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON FLOORBEAM UPPER AND LOWER CHORDS AT BS 1130 LBL TO RBL 16 MAIN CABIN. AFTER CORROSION REMOVAL, MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED UPPER AND LOWER CHORDS PER SRSDR DHL99742004Connector · looseON FLAP RETRACTION , NR 1 SLAT LIGHT AND L/E FLAPS LIGHT AMBER AT FLAPS 2. RESEATED CANNON PLUG ON NR 1 SLAT ACUATOR. CYCLED FLAPS SEVERAL TIMES, OPS CHECKED GOOD.SDR 20000615AP004Bracket · crackedDURNIG C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL 9503 LEFT AND RIGHT LOWER SECTION BRACKETS CRACKED. REMOVED BRACKETS, FABRICATED, TREATED AND INSTALLED PER SRM 51-30-3 APGE 14A. (M)SDR 20000615AP003Panel · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER L/E PANEL NR 9502, INNER AFT EDGE CRACKED. REMOVED INNER SKIN PER SRM 51-30-2 PAGE 1, FABRICATED NEW INNER SKIN PER SRM 55-10-2. INSTALLED PER SRM 55-10-2. (M)SDR 20000615AP014Angle · crackedDURING C-CHECK, FOUND TWO RIVETS PULLING, AND .375 INCH CRACK AT DOUBLER AT LT WING LOWER FAIRING SUPPORT ANGLE AFT FALSE SPAR AREA, OUTBOARD OF NR 3 FLAP TRACK. REMOVED DOUBLER FOR CRACK AND TWO RIVETS PULLING AS PER SRM 51-30-2 PAGE 1. FABRICATED NEW DOUBLSDR 20000615AP013Channel · crackedDURING C-CHECK, FOUND 1.5 INCH CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT CHANNEL. INSTALLED NEW CHANNEL IAW SRM 51-30-2 PAGE 1. (M)SDR 20000613AP010Rib · crackedDURING C-CHECK, FOUND NR 3 ENGINE PYLON T/E INNER COMPARTMENT, AFT OF AFT ENGINE MOUNT SUPPORT RIB CRACKED. FABRICATED NEW MOUNT SUPPORT RIB PER SRM 51-10-2 PAGE 1 AND INSTALLED PER SRM 51-30-2 PAGE 1. (M)SDR USAA020002Switch · inoperativeFLT6311 - BOS-LGA - HEAVY SMOKE SEEN FROM RUNWAY TURNOFF LIGHT SWITCHES WHEN PLACED TO O. SMOKE STOPPED WHEN SWITCH PLACED TO OFF. CI NR M849917 ASSIGNED FOR LEFT RUNWAY TURNOFF LIGHT SWITCH PER MEL SEQ 33-12. CI NR M849918 ASSIGNED FOR RT RUNWAY TURNOFF LISDR USAA119903Switch · failedFLT 6311 - BOS-LGA - SMOKE SEEN FROM RUNWAY TURNOFF LIGHT SWITCHES, WHEN SWITCHES PLACED TO ON POSITION. INSPECTED WIRING AT SWITCHES, FOUND ALL WIRES OK. REPLACED LEFT AND RIGHT RUNWAY TURNOFF LIGHT SWITCHES, OPERATIONAL CHECK NORMAL. (M)SDR 20000615AP012Rib · crackedDURING C-CHECK, FOUND TWO EACH 1 INCH CRACKS INSIDE LEFT WING FIXED L/E AT TOP AFT END OF NOSE RIB-SLAT STATION 0, SEEN FROM OUTBOARD SIDE. FABRICATED NEW RIB AND INSTALLED IAW 51-10-1, PAGE 4. (M)SDR 20000615AP011Rib · crackedDURING C-CHECK, FOUND RIGHT WING FIXED L/E RIB AFT END HAS TWO .75 INCH CRACKS THROUGH BOLT HOLES WHERE IT MOUNTS TO FRONT SPAR. CUT OUT CRACK AREAS AT R/W L/E INTERIOR WEB STATION 130-599 IAW SRM 51-40-2 FIG 1. FABRICATED FILLER AND REPAIR DOUBLER AND INSTASDR 20000615AP010Bracket · crackedDURING C-CHECK, FOUND BRACKET HAS 1 INCH CRACK WHERE RT WING NR 8 SLAT LOWER SKIN EXTENSION ATTACHES TO BOTTOM OF INBOARD TRACK. REPLACED BRACKET IAW SRM 51-10-1 AND 51-30-2 PAGE 1 AND PAGE 4. (M)SDR 20000615AP009Channel · crackedDURING C-CHECK, FOUND RIGHT WING LOWER TRAILING EDGE SUPPORT INBOARD CHANNEL CRACKED APPROX 1 INCH. REPLACED CHANNEL IAW SRM 51-10-1 PAGE 4. (M)SDR 20000615AP008Angle · crackedDURING C-CHECK, FOUND .375 INCH CRACK AT ANGLE ON BOTTOM OF RIGHT WING UPPER T/E PANEL AT WEB 5 INCHES FORWARD OF INBOARD AILERON L/B LEADING EDGE. FABRICATED NEW ANGLE PER SRM 51-10-1 PAGE 4. INSTALLED ANGLE PER SRM 51-30-2 PAGE 1. (M)SDR EISA99241Skin · crackedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED INTERIOR SKIN ON FORWARD ENTRY DOOR IS BENT AND CRACKED AT TORQUE TUBE CUTOUT. STOP DRILLED CRACK PER SRM 51-10-1, RESHAPED DEFORMED AREA PER SRM 51-30-10. FABRICATED AND INSTALLED WEB REPAIR PER SRM'S 51-SDR EISA99237Skin · crackedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A CRACK IN FUSELAGE EXTERNAL SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUT-OUT. TRIMMED DAMAGED AREA PER SB 727-53-0198. FABRICATED AND INSTALLED DOUBLER PER SB 727-53-0198. TT: 65,345:17 HOURS. TC: 43,
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