Boeing 727-173C

Service difficulty reports · 436

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 = '727173C'
  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 UPS202141Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT, 7TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01.Feb 2, 1995 · N938UP · Boeing 727173C · Leading Edge DevicesSDR UPS202140Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND LT NR 4 SLAT I/B END RIB CRACKED IN FWD RADIUS. INSTALLED REPAIR IAW SRM 51-30-02 AND OHM 57-51-61.Feb 2, 1995 · N938UP · Boeing 727173C · Leading Edge DevicesSDR UPS202139Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT FIRST RIB ON O/B END CRACKED. INSTALLED REPAIR IAW 51-10-1 AND DWG 65-16223.Feb 2, 1995 · N938UP · Boeing 727173C · Leading Edge DevicesSDR UPS202138Skin Lap · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INNER SKIN LAP BS 683-685 STRINGER 4 RT. INSTALLED REPAIR IAW SRM 53-30-3.Feb 2, 1995 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS202137Clip · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER CLIP AT BS 1166 STRINGER 18R. INSTALLED REPAIR IAW SRM 53-10-3, 51-10-02, 51-30-2 AND MM 51-20-151.Feb 2, 1995 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS202136Skin · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON SKIN AT STR 4L STA 110. INSTALLED REPAIR IAW SRM 53-30-2, 53-30-1, 53-30-3.Feb 2, 1995 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS202135Support · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON RT WING MID FLAP O/B FLAP CARRIAGE BEARING SUPPORT. INSTALLED REPAIR IAW MM 27-51-13.Feb 2, 1995 · N938UP · Boeing 727173C · Wing, Control SurfacesSDR UPS202134Shear Tie · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SHEAR TIE AT BS 1130, WL 186, STRINGERS 19R AND 20R. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-02, 53-10-2.Feb 2, 1995 · N938UP · Boeing 727173C · Fuselage Internal Mounting StructureSDR UPS202119Rib Mount Tab · crackedWHILE IN 'D' CHECK, MAINT FOUND VENT BOX STR 12 RIB MOUNT TAB CRACKED AT WS 656.5 (KIT P/N 65C26139-16), LT WING. INSTALLED REPAIR IAW SRM 57-10-4 AND SB 57A159.Jan 30, 1995 · N938UP · Boeing 727173C · Wing, Rib/BulkheadSDR UPS202118Support Block · corrosionWHILE IN 'D' CHECK, MAINT FOUND CORROSION ON LT WING O/B FLAP, I/B AFT SUPPORT BLOCK. INSTALLED REPAIR IAW MM 27-51-13.Jan 30, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202117Support Block · corrosionWHILE IN 'D' CHECK, MAINT FOUND CORROSION O/B FLAP O/B AFT SUPPORT BLOCK CORRODED AND WORN ON LEFT WING. INSTALLED REPAIR IAW MM 27-51-13.Jan 30, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202116Skin Lap · corrosionWHILE IN 'D' CHECK, MAINT FOUND CORROSION ON SKIN LAP STR 4 LT AT STA 927, 940. INCLUDED STA 954-958 AT STR 4 LT.Jan 30, 1995 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS202115Stringer · corrosionWHILE IN 'D' CHECK, MAINT FOUND CORROSION ON STR NR 23R BS 410 WL 164 RBL 42. INSTALLED REPAIR IAW SRM 53-10-3.Jan 30, 1995 · N938UP · Boeing 727173C · Fuselage Main, Longeron/StringerSDR UPS202114Upper Gate · corrosionWHILE IN 'D' CHECK, MAINT FOUND CORROSION ON FORWARD ENTRY DOOR UPPER GATE. INSTALLED REPAIR IAW SRM 51-10-2, 51-30-2, 51-30-8 AND MM 51-20-151.Jan 30, 1995 · N938UP · Boeing 727173C · Passenger/Crew DoorsSDR UPS202113Transverse Beam · corrosionWHILE IN 'D' CHECK, MAINT FOUND AFT CARGO DOOR NR 1 TRANSVERSE BEAM CORRODED. INSTALLED REPAIR IAW SRM 51-30-2.Jan 30, 1995 · N938UP · Boeing 727173C · Cargo/Baggage DoorsSDR UPS202112Transverse Beam · crackedWHILE IN 'D' CHECK, MAINT FOUND AFT CARGO DOOR HAS 2 CRACKS ON THE NR 3 TRANSVERSE BEAM AND WEB. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-30-2.Jan 30, 1995 · N938UP · Boeing 727173C · Cargo/Baggage DoorsSDR UPS202082Rib · crackedWHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING RIB CHORD WAS CRACKED AT WING STA 656.5, LOWER CHORD S-8. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-2, 51-20-1, 51-30-2.Jan 23, 1995 · N938UP · Boeing 727173C · Wing, Rib/BulkheadSDR UPS202081Flap · delaminationWHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 72 INCHES FROM O/B END ON T/E. INSTALLED REPAIR IAW ARM 51-40-06.Jan 23, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202080Flap · delaminationWHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 31 INCHES FROM I/B END LOWER SURFACE. INSTALLED REPAIR IAW ARM 51-40-06.Jan 23, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202079Flap · delaminationWHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 57 INCHES FROM I/B END. INSTALLED REPAIR IAW ARM 51-40-06.Jan 23, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202078Butt Joint · corrosionWHILE IN 'D' CHECK, MAINTENANCE FOUND STA 441, STR 6L TO 10L CORROSION EMANATING FROM FWD SIDE OF BUTT JOINT. INSTALLED REPAIR IAW EO B727-5310-1371E, APP. 8.5.Jan 23, 1995 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS202076Skin · corrosionDURING 'D' CHECK, MAINTENANCE FOUND CORROSION AT SKIN LAP AT BS 1020, WL 188, RBL 55. INSTALLED REPAIR IAW SRM 53-30-3.Jan 20, 1995 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS202075Web · corrosionDURING 'D' CHECK, MAINTENANCE FOUND CORROSION IN WEB AT STA 68.92 INSIDE RT HORIZONTAL STAB. INSTALLED REPAIR IAW SRM 55-10-2, 55-10-1, AND 51-30-2.Jan 20, 1995 · N938UP · Boeing 727173C · Horizontal Stabilizer StructureSDR UPS202074Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND L/W RIB CHORD IS CRACKED WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5.Jan 20, 1995 · N938UP · Boeing 727173C · Wing, Rib/BulkheadSDR UPS202073Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND R/W RIB CHORD IS CRACKED AT WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5.Jan 20, 1995 · N938UP · Boeing 727173C · Wing, Rib/BulkheadSDR UPS202072Support Roller · pittedDURING 'D' CHECK, MAINTENANCE FOUND R/W O/B FLAP I/B CARRIAGE (NR 5) AFT SUPPORT ROLLER IS PITTED. INSTALLED REPAIR IAW 51-10-6.Jan 20, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202070Hinge · corrosionDURING 'D' CHECK, MAINTENANCE FOUND L/W, O/B AILERON, AFT I/B HINGE HALF IS CORRODED. INSTALLED REPAIR IAW MM 27-10-41.Jan 20, 1995 · N938UP · Boeing 727173C · AileronsSDR UPS202069Skin · delaminatedDURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP T/E HAS EDGE DELAMINATION AT O/B CORNER. INSTALLED REPAIR IAW SRM 51-40-6.Jan 20, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202068Skin · delaminatedDURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 86 INCHES FROM O/B END LOWER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6.Jan 20, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202067Skin · delaminatedDURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 60 INCHES FROM I/B END UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6.Jan 20, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202066Skin · delaminatedDURING 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B FORE FLAP HAS DENT WITH DELAMINATION 12 INCHES FROM O/B END UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6 AND 51-20-151.Jan 20, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202065Skin · delaminatedDURING 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B FORE FLAP HAS AREA OF DELAMINATION ON I/B T/E CORNER LOWER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6 AND MM 51-20-151.Jan 20, 1995 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS202064Frame · crackedDURING 'D' CHECK, MAINTENANCE FOUND FLOURESCENT LIQUID PENETRANT INSPECTION OF FASTENER HOLES ON BS 660 FRAME AT OR NEAR STRINGER 19R EXHIBIT A CRACK INDICATION FROM SCREW HOLE TO FASTENER HOLE. INSTALLED REPAIR IAW SRM 51-40-3, 51-30-2, AND 51-10-2.Jan 20, 1995 · N938UP · Boeing 727173C · Fuselage Main, FrameSDR UPS201955Web · crackWHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1226 WL 188 RBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND 51-20-151.Jan 9, 1995 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS201935Web · crackWHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1290 WL 180 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151.Jan 9, 1995 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS201934Web · crackWHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1226 WL 188 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 53-10-2 AND MM 51-20-151.Jan 9, 1995 · N938UP · Boeing 727173C · Fuselage Miscellaneous Structure
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