Boeing 727-185C

Service difficulty reports · 425

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 = '727185C'
  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 UPS204536Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE ACCESSING 870 PRESSURE SEAL RETAINER, CORROSION UPPER SIDE OF TOP SKIN STA 870, LBL 45-65, WL 190. REMOVED CORROSION, REPAIRED SKIN PER USP E.O. 727-57-1648.Sep 28, 1995 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS204535Stringer · corrosionWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 STRINGER (LOWER) RWS 226-230, LOCATED ON TOP SIDE OF BOTTOM HORIZONTAL LEG OUT OF LIMITS. REMOVED AND REPLACED STRINGER PER E.O. 757-57-1641. UPON REMOVAL OF STRINGER, FOUND DAMGED SHEAR TIE AND ANGLESep 28, 1995 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS204534Spar Chord · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-01) LT WING LOWER SPAR CHORD IS CORRODED AT WS 180 TO 184 IN HEEL OF CHORD. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS, REPAIRED PER UPS E.O. B727-5710-7411-A.Sep 28, 1995 · N954UP · Boeing 727185C · Wing SparSDR UPS204533Spar Chord · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-02) RT WING UPPER SPAR CHORD IS CORRODED FROM WS 130 TO 224.5 AND GOING UNDER TRUNNION FITTING. REMOVED AND REPAIRED RT WING SPAR CHORD IAW UPS E.O. B727-5710-7410-A.Sep 28, 1995 · N954UP · Boeing 727185C · Wing SparSDR UPS204532Slat · corrosionWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP ATTACH LUGS ARE CORRODED AT LUG MOUNT BOLTS OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP PER MM 27-81-1 AND MM 27-81-00.Sep 28, 1995 · N954UP · Boeing 727185C · Leading Edge DevicesSDR UPS204531Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 1 ELEVATOR HINGE SUPPORT RIB CRACKED IN THREE PLACES ON UPPER CHORD. REMOVED AND INSTALLED NEW SUPPORT RIB. WORK DONE IAW SRM 51-30-2 MM 27-20-1, MM 27-30-05, MM 27-30-81, MM 27-30-61, MM 27-30-00.Sep 28, 1995 · N954UP · Boeing 727185C · Elevator, Spar/RibSDR UPS204530Spar Web · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REMOVED CENTER CELL REAR SPAR WEB FOR ACCESS OF 870 TENSION STRAP. AFTER WEB REMOVAL, FOUND CORROSION ON WEB TO BE OUT OF LIMITS PER SRM 57-10-1. REPLACED BS 870 WEB PER SRM 51-30-2, 51-10-1, 51-10-2, 51-10-6, 51-30-5, 51-20Sep 28, 1995 · N954UP · Boeing 727185C · Wing SparSDR UPS204529Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING UPPER SKIN HAS CORROSION AND AN 8 INCH CRACK FROM RWS 190 TO 224.5 AT AFT SPAR. CUTOUT DAMAGED SKIN, FABRICATED, INSTALLED REPAIR DOUBLERS, PER UPS E.O. B727-5730-7416.Sep 28, 1995 · N954UP · Boeing 727185C · Wing, Plate/SkinSDR UPS204528Load Beam · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SIDE LOAD BEAM STA 740, RBL 40 TO LBL 40, WL 170. REMOVED BEAM CHORD AND REPLACED WITH NEW CHORD IAW 727 SRM 51-10-2, 51-10-6, 51-30-2.Sep 28, 1995 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS204527Bracket · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON DELTA BEAM FORWARD ATTACH ANGLE BS 740 LBL 6 TO RBL 6, WL 155. REMOVED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW 727 SRM 51-10-01, 51-10-2, 53-10-1, 51-30-2.Sep 28, 1995 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS204500Upper Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE THE BOTTOM SIDE OF UPPER SKIN AT STATION 868 TO 870, RBL 63 LBL 63. MAINTENANCE COMPLIED WITH UPS EO 727-57-1648.Sep 22, 1995 · N954UP · Boeing 727185C · Wing, Plate/SkinSDR UPS204499Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE ON THE UPPER SIDE OF THE TOP SKIN AT STATION 870, RBL 45 TO 65 WL 190. MAINTENANCE BLENDED OUT THE CORROSION, FLAP PEENED AREA IAW OHM, TREATED AND INSTALLED REPAIR STRAP IAW UPS EO 727-57-1648.Sep 22, 1995 · N954UP · Boeing 727185C · Wing, Plate/SkinSDR UPS204498Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD AILERON, OUTBOARD CENTER BEARING SUPPORT FITTING ON THE AILERON. MAINTENANCE REMOVED AND INSTALLED NEW FITTING IAW SRM 51-30-2.Sep 22, 1995 · N954UP · Boeing 727185C · AileronsSDR UPS204497Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD AILERON, OUTBOARD BEARING SUPPORT FITTING ON THE AILERON. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING IAW SRM 51-10-1 AND 51-30-2.Sep 22, 1995 · N954UP · Boeing 727185C · AileronsSDR UPS204496Gate · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION IN THE FORWARD ENTRY DOOR LOWER GATE AT CENTER ROD ATTACHING POINT. MAINTENANCE REMOVED AND REPLACED THE FWD ENTRY DOOR LOWER GATE PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1 AND 51-20-1 AND MM 51-20-151.Sep 22, 1995 · N954UP · Boeing 727185C · Passenger/Crew DoorsSDR UPS204495Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD FRAME ON THE FORWARD ENTRY DOOR AT THE LOWER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR FORWARD FRAME PER SRM 51-10-1 AND 51-20-1.Sep 22, 1995 · N954UP · Boeing 727185C · Passenger/Crew DoorsSDR UPS204494Gate Beam · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR UPPER GATE BEAM IN THE OUTBOARD RADIUS. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR UPPER GATE BEAM PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1, 51-20-1 AND MM 51-20-151.Sep 22, 1995 · N954UP · Boeing 727185C · Passenger/Crew DoorsSDR UPS204493Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR AFT FRAME AT THE LOWER AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR AFT FRAME PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1 AND 51-20-1.Sep 22, 1995 · N954UP · Boeing 727185C · Passenger/Crew DoorsSDR UPS204492Seal Depressor · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOORWAY SEAL DEPRESSOR BELOW LOWER HINGE CUTOUT. MAINTENANCE REMOVED THE OLD SEAL DEPRESSOR, FABRICATED NEW SEAL DEPRESSOR AND INSTALLED PER SRM 51-10-2, 51-10-1 AND 51-30-2.Sep 22, 1995 · N954UP · Boeing 727185C · Passenger/Crew DoorsSDR UPS204491Bolts · shearedWHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 3 FLAP TRACK SPOILER BEAM BOLTS WERE SHEARED. MAINTENANCE REMOVED AND INSTALLED NEW BOLTS, FABRICATED NEW SHIM AND INSTALLED. ALL WORK DONE IAW MM 27-51-31-AND 51-30-2.Sep 22, 1995 · N954UP · Boeing 727185C · Wing, Control Surface Attach FittingsSDR UPS204468Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SURFACE OF THE RIGHT WING OUTBOARD FORE FLAP. MAINTENANCE REMOVED THE CORROSION AND TRAILING EDGE WEDGE, REPAIRED THE CORE AND INSTALLED NEW WEDGE PER SRM 51-40-6.Sep 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS204467Chord · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT MID-CHORD AT STATION 294.5 - 312, LBL 15 AND WL 170. MAINTENANCE REMOVED CORROSION BEYOND LIMITS, REMOVED AND REPLACED THE CHORD, FINAL INSTALLATION PER SRM 51-30-2, 53-10-1 AND 56-40-00.Sep 20, 1995 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS204466Doubler · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE ACCESS PANEL DOUBLER AT STATION 875, LBL 55 AND WL 165. MAINTENANCE REMOVED THE CORRODED DOUBLER, FABRICATED A NEW DOUBLER, AND INSTALLED PER SRM 51-10-2, 51-30-5 AND 51-30-2.Sep 20, 1995 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS204465Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE LEFT WING INBOARD FORE FLAP. MAINTENANCE REPAIRED THE UPPER AND LOWER SURFACES OF THE LEFT WING INBOARD FORE FLAP IAW SRM 51-40-6.Sep 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS204464Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SKIN ON THE RIGHT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED AREA, CLEANED AND REPAIRED AREA PER SRM 51-40-6.Sep 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS204463Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE RIGHT WING INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REPAIRED THE RIGHT WING INBOARD MID-FLAP TRAILING EDGE WEDGE IAW SRM 51-40-6.Sep 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS204462Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED SKIN ON THE UPPER AND LOWER SKINS, FINAL REPAIRS PER SRM 51-40-6.Sep 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS204461Te Wedge · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE OF THE LEFT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REPAIRED THE LEFT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE IAW SRM 51-40-6.Sep 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS204460Gate Beam · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR LOWER GATE BEAM AT THE LOWER AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE CRACKED LOWER GATE BEAM AND SECURED WITH FASTENERS IAW SRM 51-30-2 AND SRM 51-10-1.Sep 20, 1995 · N954UP · Boeing 727185C · Passenger/Crew DoorsSDR UPS204459Skin · delaminatedWHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE NR 5 SPOILER AT THE FORWARD OUTBOARD CORNER ON BOTH UPPER AND LOWER SKINS. MAINTENANCE REPLACED SPOILER IAW UPS NRC 364863.Sep 20, 1995 · N954UP · Boeing 727185C · SpoilersSDR UPS204458Fitting · pittedWHILE IN C-CHECK, MAINTENANCE FOUND THE AILERON PCU MOUNT FITTING PITTED AT THE ATTACH POINTS AND CONTROL LINKAGES. MAINTENANCE REMOVED THE DAMAGED FITTING, INSTALLED NEW FITTING ONTO AIRCRAFT AND INSTALLED CABLES AND TORQUE TUBES PER MM 27-10-91.Sep 20, 1995 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS204457Angle · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE NR 3 SKATE ANGLE IN 2 PLACES ON INBOARD SIDE. MAINTENANCE STOP DRILLED THE CRACK NDI VERIFIED AND INSTALLED DOUBLER IAW SRM 51-40-2.Sep 20, 1995 · N954UP · Boeing 727185C · Wing Miscellaneous StructureSDR UPS204287Eel Batteries · dischargedWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS OVER FLIGHT DECK AND FWD ENTRY DOOR INOP. REPLACED BATTERIES, OPS CHECK OK.Aug 19, 1995 · N940UP · Boeing 727185C · Emergency LightingSDR UPS403898Skin · delaminatedWHILE ON GROUND MAINTENANCE FOUND DELAMINATION OF LT I/B T/E FLAP. REPAIRED IAW EO B727-5750-3081.Jul 20, 1995 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS202941Eel Battery Pack · dischargedMAINTENANCE REPORTED EMERGENCY EXIT LIGHTS INOP IN FLIGHT DECK. REPLACED BATTERY PACK PER MM 33-50-101. OPS CHECK OK.Apr 13, 1995 · N940UP · Boeing 727185C · Emergency LightingSDR UPS202101Frame · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND MID GALLEY DOORWAY FORWARD UPPER FRAME SEGMENT CRACKED TOP I/B CORNER STA 636. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-02, 51-30-2 AND MM 51-20-151.Jan 25, 1995 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS202091Stringer · crackWHILE IN 'C' CHECK, MAINT FOUND STR 15 AT BS 294.5 LEFT SIDE HAS A CRACK AT THE UPPER FLANGE ATTACH POINT LEFT SIDE. X-RAY NR 14-15 LEFT. INSTALLED REPAIR IAW EO 727-5310-1259F.Jan 24, 1995 · N940UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS202077Failsafe Strap · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND I/B AND O/B FAILSAFE STRAPS TO BE CRACKED AT BS 294, WL 215 APPROX. LBL 50. INSTALLED REPAIR IAW UPS FILE NR 727-53-1459.Jan 23, 1995 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS202063Frame · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT STA 760, LBL 65-70, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-10-6, 51-30-2, AND UPS ENGINEERING FILE NUMBER 727-53-1456.Jan 20, 1995 · N940UP · Boeing 727185C · Fuselage Main, FrameSDR UPS202062Skin · crackedDURING 'C' CHECK, MAINTENANCE FOUND SKIN CRACKED AT STA 1155 BETWEEN STR 20-21L. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-30-8, 53-30-3.Jan 20, 1995 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS202061Floor Support · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT NUT PLATE AT STA 848, LBL 40, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, 51-10-1.Jan 20, 1995 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS202060Floor Support · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT NUT PLATE AT STA 756, LBL 45-60. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2.Jan 20, 1995 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS202059Seat Track · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT STA 780-820, RBL 45, WL 208. REPLACED SEAT TRACK PER SRM 51-30-02, 51-10-1.Jan 20, 1995 · N940UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS202058Seat Track · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT STA 756-852, LBL 65. REPLACED SEAT TRACK PER SRM 51-30-02, 51-10-2, 51-20-4.Jan 20, 1995 · N940UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS202056Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7204. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.Jan 20, 1995 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS202055Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7207. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.Jan 20, 1995 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS202054Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7602. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.Jan 20, 1995 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS202053Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7603. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.Jan 20, 1995 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS202052Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7608. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.Jan 20, 1995 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS202051Skin · corrodedDURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7610. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074.Jan 20, 1995 · N940UP · Boeing 727185C · Wing, Plate/Skin
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