Boeing 727-25C

Service difficulty reports · 2,007

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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 = '72725C'
  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 UPS96205972Stringer · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RWS 629.0 STR 12 HAS A CRACKED VENT STR TAB. REPAIRED STR 12 RWS 629.0 IAW UPS EO B727-5710-0314 APP 8.3.Apr 6, 1996 · N933UP · Boeing 72725C · Wing, Longeron/StringerSDR UPS96205970Frame · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION AFT SIDE OF FRAME WEB BS 720 BL 0 WL 159. REPAIRED IAW SRM 53-10-1, 51-40-2, 51-10-2, 51-30-2.Apr 4, 1996 · N933UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96205914Chord · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FIN STA 13.74 CHORD FOUND TO BE CRACKED. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-2.Mar 25, 1996 · N948UP · Boeing 72725C · Vertical StabilizerSDR UPS96205713Battery Pack · out of positionWHILE IN MEX CREW REPORTED, ON T/O ROLL THE COCKPIT EMERGENCY EXIT LIGHT FELL OFF THE BULKHEAD AND HIT THE FLOOR. LIGHT IS NOW INOP. REPOSITIONED BATTERIES AND LAMPS. CHECKS NORMAL.Mar 18, 1996 · N949UP · Boeing 72725C · Emergency LightingSDR 96FDEA00655Skin · corrosionSKIN LAP UPPER PANEL, 65-18386-107, CORRODED, AND TRIMMED AWAY FUSE SKIN BETWEEN STR 21-22L FROM THE PRODUCTION SPLICE AT BS 1080.45 TO THE PRODUCTION SPLICE AT BS 1183 CORRODED. CUT DAMAGED SKIN FROM BS 1080.45 TO BS 1183 AND SPLICED NEW SKIN PER EA 7-5330-2Mar 18, 1996 · N119FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 96FDEA00654Skin · corrosionFUSELAGE PLATES CORRODED. REPAIR TO LT SKIN ASSY STA 1130 - STA 1183, STR 14 - STR 20L. REPETITIVE ULTRASONIC INSPECTION. SKIN REMOVED AND REPLACED PER EA 7-5330-22692, DATE 11-16-94.Mar 18, 1996 · N119FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 96FDEA00657Floor Beam · corrodedCABIN FLOOR BEAM AT STA 312, BL ZERO WAS FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL, BUT NO REPAIR WAS INSTALLED. REMOVED CORRODED AREA, FABRICATED FILLER AND INSTALLED REPAIR PER SRM 53-10-8.Mar 17, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96205913Spar Web · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 WL 260 VERT FIN SPAR WEB IS CRACKED. CUT OUT DAMAGED CENTER WEB, FABRICATED REPLACEMENT SECTION AND REPAIRED PER SRM 55-30-6.Mar 16, 1996 · N948UP · Boeing 72725C · Horizontal Stabilizer, Spar/RibSDR UPS96205908Stiffener · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 351 STA 19L, FRAME TEE STIFFENER HAS HEAVY CORROSION. REMOVED AND FABRICATED AND INSTALLED FRAME TEE STIFFENER AT FS 351, STR 19L PER SRM 51-10-1 AND 51-30-2.Mar 16, 1996 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA00656Floor Beam · corrosionFLIGHT DECK FLOOR BEAM, STA 268, UPPER CHORD CORRODED AND PREVIOUS REPAIR NOT PER SRM LBL 2. REMOVED AND REPLACED FITTING IAW SRM 51-10-1.Mar 15, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00653Floor Beam · corrosionSTA 312 - STA 328, BL ZERO, LBL 22, FLOOR BEAM CORRODED ON UPPER SURFACE. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.Mar 15, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96220046Shear Web · corrodedINSPECTION TYPE: C. STA 1185, LBL 65 SHEAR WEB CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA IAW SRM 51-40-2 AND FABRICATED AND INSTALLED REPAIR DOUBLER IAW 51-40-2 AND 51-30-2.Mar 14, 1996 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220045Skin · corrodedINSPECTION TYPE: C. LFEC INSPECTION REVEALED MATERIAL LOSS OF GREATER THAN 10 PERCENT, BUT LESS THAN 20 PERCENT ON AFT SIDE BS 360, BETWEEN STR 25L AND STR 26L. CUT OUT DAMAGED AREA AT AFT STA 360 BETWEEN STR 25L AND STR 26L. REPAIRED SKIN PER DRAWING NR 6Mar 14, 1996 · N948UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS96220044Angle · crackedINSPECTION TYPE: C. LEFT SKIN SUPPORT ANGLE IS CRACKED AT FS 1345 AND FIN STA 22.5. REMOVED DAMAGED AREA IAW SRM 51-40-3 AND FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3.Mar 14, 1996 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA00652Floor Beam · corrosionUPPER LOBE CORROSION ON FLOOR BEAM STA 640, BL ZERO - RBL 65. REPAIRED IAW SRM 53-10-8.Mar 14, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00643Frame · crackedFRAME CRACKED AT STA 480, STR 9L. INSTALLED FUSELAGE CROWN FRAME REPAIR, STA 440, STR 9L, PER SRM 53-10-4, PG 18.Mar 14, 1996 · N119FE · Boeing 72725C · Fuselage Main, FrameSDR UPS96205909Stringer · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 300 AT STR 23R HAS CORROSION AT FRAME ATTACH POINT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2, 53-10-3 AND 51-30-2.Mar 13, 1996 · N948UP · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 96FDEA00651Floor Beam · corrosionCABIN, FS 480, FLOOR BEAM HAS CORROSION AROUND FASTENER NUTPLATES, BOTTOM FLANGE BL 45 - BL 60R. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8.Mar 13, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00650Floor Beam · corrosionCABIN, FS 740, FLOOR BEAM HAS CORROSION DEVELOPING IN SCREW HOLE AND NUTPLATES (BOTTOM SIDE) BETWEEN BL 8 RT TO BL 53 RT. INSTALLED FLOOR BEAM REPAIR PER ESO AND EA NR 7-5310-27774.Mar 11, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00649Floor Beam · corrosionCABIN, FS 740, FLOOR BEAM HAS HEAVY INTERGRANULAR CORROSION AT SCREW HOLE AND NUTPLATE 3.50 INCHES TO THE RT OF BL ZERO FLOOR TRACK, BOTTOM SIDE FLANGE. INSTALLED FLOOR BEAM REPAIR PER ESO AND EA NR 7-5310-27774.Mar 11, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96205661Light · inoperativeMAINTENANCE REPORTED EMERGENCY LIGHT IN COCKPIT FAILED. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL.Mar 10, 1996 · N931UP · Boeing 72725C · Emergency LightingSDR 96FDEA00646Casting · corrodedRIGHT WING PIVOT BOLT HOLE FOR OUTBOARD AILERON QUAD CORRODED AT BOTTOM. REPLACED OUTBOARD AILERON LOCK-OUT SUPPORT CASTING PER 51-10-1.Mar 8, 1996 · N119FE · Boeing 72725C · AileronsSDR UPS96205912Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 7 SPOILER I/B HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-10-1 AND 51-30-2.Mar 5, 1996 · N948UP · Boeing 72725C · SpoilersSDR UPS96205911Floor Beam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 312, LBL 26 FLOOR BEAM UPPER FLANGE AFT BOTTOM SIDE FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED PER SRM 53-10-8, FIG 7.Mar 5, 1996 · N948UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96205910Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 351 LT SIDE 2 INCHES AFT OF FWD AIR STAIR CUTOUT AT STR 18L, FRAME HAS LARGE AREA OF CORROSION AND LARGE CRACK. REMOVED DAMAGED AREA PER SRM 51-40-2, FABRICATED PARTS AND INSTALLED PER SRM 51-40-2. INSTALLED ATTMar 5, 1996 · N948UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96205907Web · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOG HOUSE TUNNEL AREA RT SIDE APPROX STA 279, WALL OF NOSE W/W CUTOUT HAS 4 INCH CRACK IN WEB. REMOVED DAMAGED SECTION PER SRM 51-40-2 AND FAB DOUBLER AND FILLER AND INSTALLLED PER SRM 51-40-2.Mar 5, 1996 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA00647Floor Beam · crackedCABIN FLOOR BEAM CRACKED/CORRODED ON UPPER FLANGE, BS 480, LBL 28. REPAIRED CRACKED/CORRODED FLOOR BEAM, STA 480, LBL 28, PER SRM 53-10-8, FIG 5.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00645Stringer · crackedCABIN UPPER LOBE STRINGER NR 1 IS CRACKED HALF WAY THROUGH FS 1080. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 51-10-3.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 96FDEA00644Stringer · crackedCABIN UPPER LOBE STRINGER NR 1 CRACKED THROUGH AT FS 1045. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 51-10-3.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 96FDEA00400Floor Beam · corrodedCABIN FLOOR BEAM CORRODED ON UPPER FLANGE STA 480 LBL 28. *S/D* REPAIRED CRACKED/CORRODED FLOOR BEAM STA 480 LBL 28 FIG 5.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00399Floor Beam · corrodedCABIN FLOOR BEAM TOP AFT FLANGE CORRODED ON UPPER AND LWR SURFACE STA 420 LBL 0 TO 24. *S/D* REMOVED CORRODED SECTION FAB AND INSTALLED REPAIR PER SRM 53-10-8 FIG 8.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00398Floor Beam · corrodedCABIN FLOOR BEAM CORRODED ON UPPER SURFACE STA 640 BL 0 TO RBL 65. *S/D* REPAIRED IAW SRM 53-10-8 NR0781.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA00394Stringer · crackedCABIN UPPER LOBE STRINGER NR 1 CRACKED THROUGH AT FS 1045. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 51-10-3.Mar 3, 1996 · N119FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 96FDEA00397Spar Chord · crackedWS 304 RT WING 3RD STR AFT OF FWD UPPER SPAR CHORD CRACKED. *S/D* REPAIRED STRINGER AT WS 304 RT WING 3RD TOP FRONT SPAR CHORD PER SRM 7-10-4.Feb 29, 1996 · N119FE · Boeing 72725C · Wing SparSDR 96FDEA00648Skate Angle · corrosionRIGHT FWD SKATE ANGLE NOSE COMPARTMENT HAS CORROSION ON FWD END. REMOVED AND REPLACED RT FWD SKATE ANGLE PER SRM 51-10-1.Feb 28, 1996 · N119FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205608Stringer · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRINGER 18A LT HAS NO EDGE DISTANCE AT STA 940, DUE TO CORROSION IN FASTENER HOLES. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EWO 96-2090.Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Main, Longeron/StringerSDR UPS205607Forging · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED WHILE WORKING FUSELAGE CUST NR 433165, FOUND A CRACK ON THE BS 950 FORGING AT THE FWD SIDE OF PRESSURE WEB ATTACH FITTING. DRILLED CRACK AND VERIFIED CRACK CONTAINMENT, INSTALLED NEW FITTING AND REPAIRED IAW EO 96-20Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205606Floorbeam · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER FLANGE BS 1110 RBL 50 TO 56 LBL 3 TO 20 AND 40 TO 44. REMOVED CORROSION, OUT OF LIMITS REPAIRED PER EWO 96-2087.Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205605Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INNER SKIN BS 640 TO 660 BETWEEN STR 2 TO 3 LT. REMOVED CORROSION, OUT OF LIMITS PER SRM 53-30-2 FABRICATED REPAIR PARTS AND INSTALLED IAW 96-2089.Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS205604Forging · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT AFT 870 TERMINAL FORGING IS CRACKED AT BS 870 WL 188 LBL 67. REMOVED CRACKED AREA AND NDT VERIFIED CRACK CONTAINMENT, REPAIRED IAW EO 96-2060.Feb 27, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96UPS20561Forging · crackedDURING 'C' CHECK MAINTENANCE REPORTED, BS 940 FORGING CRACKED AT STRINGER 18A, WL 208. REPLACED FORGING IAW EO B727-5310-4501C.Feb 26, 1996 · N931UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA00396Skate Angle · corrosionRT FWD SKATE ANGLE NOSE COMPARTMENT HAS CORROSION ON FWD END. *S/D* REMOVED AND REPLACED RT FWD SKATE ANGLE PER SRM 51-10-1.Feb 26, 1996 · N119FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205598Gate · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR LOWER GATE EXTERNAL SURFACE CORRODED CORROSION (C53-224-01.06-01). REMOVED AND REPLACED FWD ENTRY DOOR LOWER GATE IAW UPS SRM 51-30-2, 51-10-1, 51-10-2 AND UPS MM 52-11-00.Feb 24, 1996 · N931UP · Boeing 72725C · Passenger/Crew DoorsSDR UPS205597Gate · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD ENTRY DOOR UPPER GATE CORRODED AROUND LOWER RIV-NUTS AND EXTERNAL EDGES CORROSION (C53-224-01.06-01). REMOVED AND REPLACED FWD ENTRY DOOR UPPER GATE IAW UPS SRM 51-10-1, 51-10-2, 51-10-3 AND UPS MM 52-11-00.Feb 24, 1996 · N931UP · Boeing 72725C · Passenger/Crew DoorsSDR UPS205603Bonding Jumper · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 5 K-FLAP I/B UPPER LUG CORRODED AT BONDING JUMPER. REMOVED AND REPLACED NR 5 K-FLAP NRC 432723.Feb 23, 1996 · N931UP · Boeing 72725C · Leading Edge DevicesSDR UPS205602Floorbeam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01), ON FLOORBEAM STA 312 LBL 48 TO LBL 0 WL 208 AROUND NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM IAW UPS SRM 53-10-8, 51-10-6, 53-10-1.Feb 23, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205601Seat Track · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK AT STA 870 TO 1000 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK FROM STA 870 TO 1060 LBL 45 IAW UPS SRM 51-30-2.Feb 23, 1996 · N931UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR 96FDEA00312Forging · crackedHFEC IND A CRACK IN LT STA 870 FORGING AT INTEGRAL RIB, BELOW CABIN FLOOR WL 190 ON TOP SIDE AT LOWER AFT FASTENER CRACK. ALSO, RUNNING UNDER RIB EXTENDING AFT. REMOVED INTEGRAL RIB FLUSH WITH WEB, PER ESO 11782. HFEC CONFIRMED NO CRACKS AFTER DAMAGE REMOVAFeb 23, 1996 · N118FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS205594Floorbeam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01), ON FLOORBEAM UPPER CHORD STA 640, LBL 60 TO RBL 60, WL 208 AROUND NUTPLATE HOLES. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED PERFeb 22, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS205591Floorbeam · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01-05-03), ON FLOORBEAM UPPER FLANGE BS 1030, RBL 10 AND LBL 0 TO 58, WL 208. CORROSION REMOVAL ON FLOORBEAM UPPER FLANGE WAS OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INFeb 22, 1996 · N931UP · Boeing 72725C · Fuselage Main, Floor Beam
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