Boeing 727-25

Service difficulty reports · 827

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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 = '72725'
  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 DHL200070803CFrame · crackedCARGO CABIN CIRCUMFERENTIAL FRAME BS 480 CRACKED WHERE ATTACH TO FUS STR 16/17L CRACK ABOUT 6 INCHES LONG. REMOVED FASTENERS AT CIRC FRAME STA 480 PER SRM 51-30-2. CUT OUT DAMAGED AREA PER SRM 53-10-4. INSTALLED REPAIR PER SRM 53-10-4. TREATED AND PRIMED PSep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, FrameSDR DHL200070801CDuct · crackedEVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REMOVED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCT PER SRM 51-30-2. TREATED AND PRIMED AREA PER SRM 51-10-2. REPLACED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCTSep 8, 2000 · N708DH · Boeing 72725 · Leading Edge DevicesSDR DHL2000708026Strap · crackedEVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REPAIRED PER B727 SRM 51-10-2, 51-30-2. MATERIAL USED 12 X 20 INCH.Sep 8, 2000 · N708DH · Boeing 72725 · Leading Edge DevicesSDR DHL2000708014Seat Track · corrodedCORRODED CABIN SEAT TRACK AT LBL 25 BS 400. INSTALLED 40 INCHES OF NEW SEAT TRACK PER SRM 53-10-5.Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2000708011Floorbeam · corrodedLAVATORY AREA FLOORBEAM BS 328 AND BBL 54 AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER SRM 51-40-4. SIZE OF REPAIR 35 X 9 INCH.Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL2000708010Floorbeam · corrodedLAVATORY AREA FLOORBEAM BS 328 AND BBL 48 RIGHT AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER 51-40-4. SIZE OF REPAIR 35 X 9 INCH.Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL2000708009Floorbeam · corrodedLAVATORY AREA FLOORBEAM BS 328 AND BBL 36 RIGHT AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER B727 SRM 51-40-4. SIZE OF REPAIR 35 X 9 INCH.Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL2000708008Web · crackedWEB BENT AND CRACKED AT SEVERAL PLACES BETWEEN BS 1148 AND 1166 AT S-21R. INSTALL NEW INTERCOSTAL WEB PER SRM 53-10-1. SIZE OF REPAIR 16 X 4 INCH.Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL2000708013Panel · bentNR 2 CARGO DOOR AREA EXTERIOR PANEL 3610 AT REAR EDGE 2ND SUPPORT BRACKET BENT. REPLACED SUPPORT BRACKET PER SRM 51-30-2. SIZE OF REPAIR 7 X 2.5 INCH.Sep 7, 2000 · N708DH · Boeing 72725 · Cargo/Baggage DoorsSDR DHL2000708025Skin · crackedNOSE SECTION EXT LOWER AT BS 350 AND STR 27L SKIN CRACK ABOUT .5 INCH LONG. INSTALLED EXTERNAL DOUBLER PER B727 SRM 53-30-3. MATERIAL USED 11 X 8 INCH.Sep 6, 2000 · N708DH · Boeing 72725 · Fuselage Main, Plate/SkinSDR DHL2000708022Floor Support · damagedLOWER FWD CARGO COMPARTMENT SUPPORT ANGLE OVER STA.26 LT HAS APPROX 3 INCH SEPARATION. INSTALL NEW 6 INCH SECTION OF CHANNEL FLOOR SUPPORT AT FWD COMPARTMENT PER B727 SRM 51-40-3.Sep 6, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL2000708017Pressure Panel · crackedNOSE WHEEL WELL CEILING WEB PANEL SHOW CRACKS RUNNING FROM FASTENERS HOLES BS 290 BL 0. INSTALLED DOUBLER 9 X 6 INCH PER SRM 51-40-2.Sep 6, 2000 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR DHL2000708004Pressure Panel · crackedRIGHT MAIN WHEEL WELL PRESS WEB BS 950 SHOWS CRACK. INSTALL DOUBLER PER SR 53-10-9. SIZE OF REPAIR 6 X 6 INCHES.Sep 6, 2000 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR DHL2000708018Pressure Panel · crackedNOSE WHEEL WELL CEILING PANEL SHOWS CRACKS AT BS 277 AND RBL 20. INSTALLED DOUBLER PER SRM 51-40-2.Sep 5, 2000 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR DHL2000708016Pressure Panel · crackedNOSE WHEEL WELL CEILING PRESS WEB SHOWING CRACKS RUNNING FROM RIVETS HOLES AT BS 268.5 AND RBL 20. INSTALLED DOUBLER 14 X 14 INCH PER SRM 51-40-2.Sep 5, 2000 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR DHL2000708015Pressure Panel · crackedNOSE WHEEL WELL CEILING WEB PANEL SHOWS CRACKS RUNNING FROM RIVET HOLES AT BS 268.5 AND RBL 10. INSTALL DOUBLER PER SRM 51-30-2. SIZE OF REPAIR 14 X 14 INCH.Sep 5, 2000 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR DHL200070811CBracket · crackedNR 2 CARGO COMPT AREA PANEL NR 3610 REAR EDGE SUPPORT BRACKET CRACKED (NR 3 POST). REMOVED BRACKET PANEL PER SRM 51-30-2. INSTALLED NEW BRACKET PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.Sep 3, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR 00FDEA00620Actuator · failedON FLAP RETRACTION TO 2 DEGREES NR 1 LEAD EDGE FLAP STAY AMBER BOTH ON UP. REMOVED AND REPLACED SLAP IND SWITCH (S202) PER MM 27-81-000-5. REMOVED AND REPLACED ACTUATOR PER MM 27-81-22.Sep 2, 2000 · N508FE · Boeing 72725 · Leading Edge Slat ActuatorSDR DHL200070804CBulkhead · corrodedFUSE FWD CARGO COMPT FWD BULKHEAD WEB CRACK AT LOWER LEFT CORNER. STOP DRILLED CRACK PER SRM 51-10-1. HEAT TREATED REPAIR DOUBLER PER SRM 51-10-3. TREATED AND PRIMED DOUBLER PER SRM 51-10-2. PERFORMED HFEC INSP OF AREA PER NDT MAN 51-00-00. INSTALLED DOUBSep 1, 2000 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR EISA20000132Switch · misalignedNOSE GEAR DOOR LIGHT ILLUMINATED. AIR TURNBACK TO (AUS). REMOVED AND REPLACED NOSE GEAR DOOR CABLES AND TESTED PER M/M 32-22-1. REMOVED AND REPLACED DOOR WARNING SWITCH PER M/M 32-62-11.Aug 31, 2000 · N290NE · Boeing 72725 · Landing Gear Position and WarningSDR DHL2000708023Angle · brokenAIR CONDITIONING COMPARTMENT AREA FAIRING MOUNT ANGLE ON DELTA BEAM BS 852 BROKEN. REPLACED 12 X 2 INCH ANGLE PER B727 SRM 51-30-2.Jul 15, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR 00FDEA00456Skin · corrodedFUSELAGE SKIN 65-18385-33 & DOUBLER 65-18385-53 CORRODED INTERIM REPAIRED PER EA 7-5330-51318. REMOVED CORRODED SKIN FROM FUSELAGE BS 1145 TO 1183 LONGERON L16 TO L20 LT FUSELAGE. FAB & INSTALL SKIN & DOUBLER REF EA 7-5330-51318 SRM 53-30-03 FIG 5.Jul 14, 2000 · N509FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR DHL2000708003Cdu · failedCAPT CDU FROZEN CENTERED TO/FROM, OPS NORMALLY ON SEVERAL FREQS. REMOVED AND REPLACED CAPTS CDU WITH SERVICEABLE UNIT, OPS CHECK OK PER M/M 34-62-01.Jun 14, 2000 · N708DH · Boeing 72725 · Directional Gyro and Indicating SystemSDR CA000621028Muffler · failed(CAN) DURING TROUBLESHOOTING OF AIRCRAFT FOR A PRESSURIZATION DEFECT, IT WAS NOTICED THAT THE RT ACCOUSTIC MUFFLER INTERIOR LINING HAD BECOME DETACHED. THE PIECES WERE FOUND BLOCKING THE PRIMARY HEAT EXCHANGER. THIS WAS DETERMINED TO BE THE CAUSE OF THE PRESSUJun 12, 2000 · Boeing 72725 · Air Distribution SystemSDR 00FDEA00363Actuator · leakingLOST A SYS QUANTITY ON LAND GEAR RETRACTION, LOST ALL A PRESSURE SHORTLY AFTER, COMPLIED WITH RED TABS. REMOVED AND REPLACED NR 6 LEAD EDGE FLAP ACTUATOR PER 727-100 MM 27-81-22. NO LEAK, RE-SAFETY ALL SWITCHES IN COCKPIT WITH BREAK-AWAY WIRE.Jun 1, 2000 · N154FE · Boeing 72725 · Leading Edge Slat ActuatorSDR 00FDEA00125Hinge · crackedLEFT WING OTBD ATTACH FITTING (HINGE HALF) FOR THE INBD AILERON IS CRACKED. REMOVED AND REPLACED PER IAW SRM 51 -30-2.Feb 29, 2000 · N155FE · Boeing 72725 · Wing, Control Surface Attach FittingsSDR DHL2000708002Pin · shearedMAIN CARGO DOOR FORWARD HINGE PIN SHERAED OFF AT FIRST LUG. REPLACED FWD HALF OF MAIN CARGO DOOR HINGE PIN PER AEI CARGO DOOR MAINTENACE MANUAL. OPERATIONAL CHECK OK.Feb 12, 2000 · N708DH · Boeing 72725 · Cargo/Baggage DoorsSDR EISA2000013Detector · defectiveDURING CRUISE, CARGO SMOKE LIGHT ILLUMINATED, REFERRED TO CHECKLIST, VERIFIED NO SMOKE. RECYCLED ON AND OFF SWITCH AND LIGHT EXTINGUISHED. FOUND NR 2 SMOKE DETECTOR DEFECTIVE. REMOVED AND REPLACED PER MM 26-10-1. SYSTEM CHECKS GOOD. (M)Feb 8, 2000 · N290NE · Boeing 72725 · Smoke DetectionSDR EISA2000010Tube · cloggedCARGO SMOKE LIGHT CAME ON IN FLIGHT, RESET TWICE CAME BACK ON AFTER EACH RESET COULD NOT VERIFY THE SMOKE. DIVERTED INTO (MEM). SUSPECT MOISTURE IN SENSOR TUBES BLEW OUT SENSORS WITH NITROGEN. SYSTEM TEST NORMAL. NO EVIDENCE OF SMOKE. (M)Feb 3, 2000 · N290NE · Boeing 72725 · Smoke DetectionSDR 00FDEA00049Unknown · smoke00-29 SMOKE COMING FROM LWR RT SIDE OF COCKPIT NEAR 1ST OFFICER'S FEET. CK APU AREA. WHEEL WELL & AC PACKS ALL OK. SUSPECT DE-ICE FLUID FROM HEAVY SPRAY AT PREV. STA. RAN #2 ENG & SHUT OFF APU. CK OK.Feb 2, 2000 · N509FE · Boeing 72725 · Air Distribution SystemSDR DHL2000708001Skin · corrodedLEFT WING HAS INTERGRANNULAR CORROSOIN STA 464 UPPER SURFACE. CUT OUT CORRODED SECTON, FABRICATED FILLER AND REPAIR DOUBLERS PER SRM 57-30-3. N/R ITEM 15.Jan 13, 2000 · N708DH · Boeing 72725 · Wing, Plate/SkinSDR 99FDEA00508Indicator · malfunctioned99-291 - OIL PRESS ON NR 3 ENG DROP BELOW 30 PSI. MAIN OIL FILTER WAS REMOVED AND CK PER 727 MM 79-00-000-2. FOUND CLEAN, REINSTALL. NO LEAKS NOTED. COULD NOT DUPLICATE ON GRD. OK FOR SERVICE.Dec 22, 1999 · N508FE · Boeing 72725 · Engine Oil Indicating SystemSDR 99FDEA00502Control Valve · failed99-285 - ON FLAP RETRACT UP TO FLAPS 2, BOTH INBD AND OTBD NEEDLES STUCK BETWEEN 2 AND 5. ALL LED'S IND EXT. REMOVED AND REPLACED O/B FLAP CONTROL VALVE PER MM 27-51-00. LUBED I/B FLAP CONTROL DRUM RIGGED CK GOOD PER 27-51-00-5.Dec 17, 1999 · N154FE · Boeing 72725 · Trailing Edge Flap Control SystemSDR 99FDEA00489Light · inopWHEN LANDING GEAR LOWERED NORM THERE WAS NO LT MAIN DOWN & LOCK IND. GEAR LIGHT TEST LT MAIN LIGHT INOP.Nov 26, 1999 · N152FE · Boeing 72725 · Landing Gear Position and WarningSDR EISA99215Smoke Detector · will not testNUMBER FOUR SMOKE DETECTOR WOULD NOT TEST. REMOVED AND REPLACED NUMBER 4 SMOKE DETECTOR. OPERATIONS CHECK GOOD. (M)Nov 22, 1999 · N290NE · Boeing 72725 · Smoke DetectionSDR DHL99708009Floorbeam · misrepairREPAIR AT BS 560 FLOORBEAM RBL 3 TO RBL 21 HAD BOTH REPAIR ANGLES OF MATERIAL NOT IN CONFORMANCE. REPLACED BOTH SUPPORT ANGLES PER SRM 53-10-8 BAC 1490-2785 AND 2831.Nov 17, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708008Floorbeam · misrepairREPAIR AT BS 560 FLOORBEAM LBL 44 BOTH ANGLES, MATERIAL NOT IN CONFORMANCE. REPLACED BOTH SUPPORT ANGLES PER SRM 53-10-8 MATERIAL 1490-2831 AND 2785.Nov 17, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708004Floorbeam · misrepairedREMOVED AND REPLACED WEB AT BS 804.5 OF FLOORBEAM RBL 51 PREV REPAIRED. REMOVED AND INSTALLED NEW WEB PER SRM 53-10-1, 24 X 9.Nov 15, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708007Floorbeam · misrepairedFLOORBEAM STABILITY STRAP REPAIR AT BS 380 BL 0 DID NOT CONFORM TO SRM. REPLACED SECTION OF STRAP PER SRM 53-10-8, 3 X 63.Nov 11, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708006Strap · misdrilledFLOORBEAM STABILITY STRAP FROM BS 420 TO BS 400 BL 0 HAD NUMEROUS HOLES DRILLED IN TO IT. REPLACED STRAP 3 X 63 PER SRM 53-10-8.Nov 11, 1999 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL99708005Seat Track · corrodedCABIN SEAT TRACK AT BS 708 LBL 24.5 CORRODED BEYOND LIMITS ON I/B FLANGE. REPLACED SECTION OF SEAT TRACK FROM BS 680 TO 740 PER SRM 51-30-2.Nov 11, 1999 · N708DH · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR DHL99708015Strap · misdrilledSTABILITY STRAP HAS DRILL MARKS BL 0 BS 1090 AND 1070. INSTALLED PLUG FASTENERS PER SRM 51-30-2. REMOVED SECTION OF STAB STRAP AT BOTTOM OF FLOORBEAM BETWEEN STA 1070 AND 1090. INSTALLED NEW SECTION PER SRM 53-10-8.Nov 10, 1999 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL99708014Floorbeam · corrodedBS 480 FLOORBEAM CORROSION LOWER SIDE OF UPPER CAP FWD SIDE OF LBL 45. CUT OUT DAMAGED AREA AT STA 480 RBL 35, INSTALLED FLOORBEAM REPAIR FROM RBL 35 TO 65 PER SRM 53-10-8.Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708013Floorbeam · misrepairBS 680 FLOORBEAM REPAIR UPPER CHORD OF LBL 6 TO 30 DID NOT CONFORM TO SRM. CUT OUT DAMAGED AREA. INSTALLED FLOORBEAM REPAIR BETWEEN LBL 36 AND 12 PER SM 53-10-8.Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708012Floorbeam · misrepairBS 660 FLOORBEAM REPAIR UPPER CHORD OF RBL 14 TO RBL 22 DID NOT CONFORM TO SRM. CUT OUT DAMAGED AREA FROM RBL 16 TO 36. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8.Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708011Floorbeam · corrodedBS 360 FLOORBEAM CORRODED ON UPPER CHORD FLANGE RBL 30. CUT OUT DAMAGED AREA FROM RBL 24 TO RBL 68. INSTALLED FLOORBEAM PER SRM 53-10-8.Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708010Floorbeam · misrepairBS 620 FLOORBEAM REPAIR UPPER CHORD FROM LBL 2 TO 31 DID NOT CONFORM PER SRM. CUT OUT DAMAGED UPPER CHORD, INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8.Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708003Strap · misrepairedSTABILITY STRAP AT RBL 23 HAS PREVIOUS REPAIR LOCATED FWD SIDE OF BS 1110 FLOOR NOT IN CONFORMANCE WITH SRM. REPLACED REPAIR PER SRM 53-10-8 3 X 26.Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL99708002Floorbeam · corrodedBS 560 FLOOR BEAM UPPER CHORD HAS FLOOR BEAM REPAIR AND CORROSION FROM LBL 4 TO LBL 14.REMOVED OLD REPAIR AND INSTALLED NEW REPAIR PER SRM 53-10-8 , SUPPORT ANGLE 11 , AND 7 N/R 3885Nov 9, 1999 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL99708001Trunnion · corrodedLEFT AND RIGHT NOSE LANDING GEAR TRUNNION HAD CORROSION AND PITTING AT BEARING MATING SURFACES. MACHINED LEFT AND RIGHT TRUNNIONS, CORROSION REMOVED AND WITHIN LIMITS PER SRM 53-40-1.Nov 9, 1999 · N708DH · Boeing 72725 · Nose/Tail Landing Gear Attach Section
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