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 96FDEA01265Fitting · crackedDISCREPANCY: STRINGER END FITTING CRACKED STA 740, AFT SIDE, AT STRINGER 5 RT. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER END FITTING PER SRM 51-10-01.Jul 18, 1996 · N116FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01264Rib · crackedDISCREPANCY: NR 1 FUEL TANK RIB AT WING STA 436.5 CRACKED AT LOWER ATTACHMENT POINT FOR STRINGER, JUST AFT OF ACCESS OPENING. CORRECTIVE ACTION: STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-5.Jul 18, 1996 · N116FE · Boeing 72725C · Wing, Rib/BulkheadSDR UPS96220962Chord · corrodedINSPECTION TYPE-C, NLG W/W RT UPPER CHORD OUT OF LIMITS AFTER CORROSION REMOVAL. FLAP PEENED AREA AFTER CORROSION REMOVAL, FABRICATED AND INSTALLED REPAIR ANGLE PER DHC SK-951-598 REV B AND OHM 20-10-03 AND APPLIED TOP COAT PER SRM 51-10-2.Jul 17, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220931Stringer · crackedINSPECTION TYPE-C, STRINGER CRACKED STA 1243 TO 1342, 12R. REMOVED AND REPLACED STRINGER PER UPS SRM 53-10-02, 51-30-02.Jul 17, 1996 · N951UP · Boeing 72725C · Fuselage Main, Longeron/StringerSDR UPS96221015Frame · corrodedINSPECTION TYPE: RE. BS 1183 FRAME OUT OF LIMITS AFTER CORROSION REMOVAL BETWEEN STR'S 10R AND 14R. REPAIRED PER DHC SK 951-947.Jul 16, 1996 · N951UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96220961Angle · corrodedINSPECTION TYPE-C, BL 0 SKIN SUPPORT ANGLE AND CLIP WAS FOUND TO HAVE HEAVY CORROSION BEYOND LIMITS. REMOVED AND FABRICATED REPLACEMENT ANGLE AND CLIP AND REPLACED PER SRM 51-10-01 AND 51-30-02.Jul 15, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220942Shear Tie · corrodedINSPECTION TYPE-C, SHEAR TIE HAS HEAVY CORROSION STA 590 BETWEEN STR 24R AND 25R. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-2 AND 51-10-01.Jul 12, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220933Angle · crackedINSPECTION TYPE-C, FWD LWR CARGO THRESHOLD SUPPORT ANGLE CRACKED STA 560 STR 26R TO 27R. REMOVED, FAB'D AND INSTALLED REPAIR ANGLE PER UPS SRM 53-10-2 AND 51-30-2.Jul 12, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220960Chord · corrodedINSPECTION TYPE-C, RT O/B CHORD IS CORRODED STA 1342 RBL 30 WL 250. REMOVED AND EPLACED RT O/B CHORD PER EO B727-5530-4601B AND SRM 51-10-01.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220958Frame · corrodedINSPECTION TYPE-C, RT LOWER FRAME CHORD RBL 24, WL 220, STA 1342 IS CORRODED. REMOVED AND REPLACED CHORD AT STA 1342 WL 220 PER SRM 51-30-02.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96220954Chord · corrodedINSPECTION TYPE-C, CHORD CORRODED ON FWD SIDE STA 1342. REMOVED AND REPLACED CHORD PER BOEING DWG 65-20981, SRM 53-30-2 AND EO B727-5530-4601B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220953Chord · corrodedINSPECTION TYPE-C, LT O/B CHORD CORRODED STA 1342 LBL 30 WL 250. REMOVED AND REPLACED CHORD PER SRM 51-10-1 AND EO B727-5530-4601B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220952Channel · corrodedINSPECTION TYPE-C, LT CHANNEL CORRODED ON AFT SIDE STA 1342 LBL 18 WL 247. REMOVED AND REPLACED CHANNEL PER BOEING DWG 65-93155 AND SRM 51-30-2.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220950Channel · corrodedINSPECTION TYPE-C, RT CHANNEL CORRODED AFT SIDE STA 1342 RBL 18 WL 247. REMOVED AND REPLACED CHANNEL PER SRM 51-10-01 AND EO B727-5530-4601B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220949Channel · corrodedINSPECTION TYPE-C, CENTER CHANNEL IS CORRODED STA 1342. REMOVED AND REPLACED CENTER CHANNEL PER SRM 51-10-01 AND EO B727-5530-46 01B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220948Frame · corrodedINSPECTION TYPE-C, LT LWR FRAME CHORD CORRODED STA 1342 LBL 24 WL 220. REMOVED AND REPLACED CHORD PER SRM 51-10-01 EO B727-5530-4601B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96220947Frame · corrodedINSPECTION TYPE-C, RT FRAME CHORD CORRODED STA 1342 RBL 20 WL 238. REMOVED AND REPLACED CHORD PER SRM 51-10-01 AND EO B727-5530-4601B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96220946Frame · corrodedINSPECTION TYPE-C, LT FRAME CHORD CORRODED STA 1342 LBL 20 WL 238. REMOVED AND REPLACED CHORD PER SRM 51-10-01 AND EO B727-5530-4601B.Jul 11, 1996 · N951UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96220932Engine Ring · corrodedINSPECTION TYPE-C, STA 1352 ENGINE RING CORRODED. REMOVED AND REPLACED (P/N 65-23687-23) IAW SRM 51-30-02.Jul 11, 1996 · N951UP · Boeing 72725C · Engine Cowling SystemSDR UPS96220955Channel · corrodedINSPECTION TYPE-C, AFT LOWER PIT STA 1046 RBL 20 FLOOR SUPPORT U-CHANNEL IS CORRODED HEAVY AT SPLICE. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED REPLACEMENT FLOOR SUPPORT IN LOWER AFT PIT STA 1046 RBL 20 PER SRM 51-30-2.Jul 10, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220937Seat Track · corrodedINSPECTION TYPE-C, LT SEAT TRACK AT STA 1160 LT HAS HEAVY CORROSION, AFT LWR CARGO. REMOVED AND REPLACED SEAT TRACK (P/N 65-22797-5) PER SRM 51-30-2 AND 51-10-01.Jul 10, 1996 · N951UP · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR UPS96220936Channel · crackedINSPECTION TYPE-C, FLOOR SUPPORT U-CHANNEL CORRODED AFT LWR CARGO PIT. REMOVED AND REPLACED U-CHANNEL PER UPS SRM 51-30-2 AND 51-10-01.Jul 10, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96221018Stiffener · crackedINSPECTION TYPE: C. RT WING L/E AT NR 6 SLAT INBD TRACK - OTBD VERTICAL STIFFENER FOR TRACK MOUNT IS CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER SRM'S 51-10-1, 51-30-2 AND SEALED PER SRM 50-20-4.Jul 8, 1996 · N951UP · Boeing 72725C · Wing Miscellaneous StructureSDR UPS96221017Stiffener · crackedINSPECTION TYPE: C. RT WING L/E AT NR 6 SLAT INBD TRACK - INBD VERTICAL STIFFENER FOR TRACK MOUNT IS CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER SRM'S 51-10-1, ,51-30-2 AND SEALED PER SRM 51-20-04.Jul 8, 1996 · N951UP · Boeing 72725C · Wing Miscellaneous StructureSDR UPS96220959Spar Chord · crackedINSPECTION TYPE-C, RT O/B AILERON AT CENTER I/B HINGE, LWR SPAR CHORD IS CRACKED. REMOVED, FABRICATED AND INSTALLED LWR SPAR CHORD PER BOEING DWG 65-21766, SRM 51-30-02.Jul 8, 1996 · N951UP · Boeing 72725C · AileronsSDR UPS96220940Rib · crackedINSPECTION TYPE-C, FS 135 AND FIN STA 22.5 RT RIB IS CRACKED. CUT OUT DAMAGED AREA PER SRM 51-40-3, FAB'D AND INSTALLED ANGLE DOUBLER PER SRM 51-40-3 AND 51-30-2.Jul 8, 1996 · N951UP · Boeing 72725C · Vertical Stabilizer, Spar/RibSDR UPS96220941Stiffener · corrodedINSPECTION TYPE-C, LT KEEL BEAM VERTICAL STIFFENER EXFOLIATION CORROSION STA 940 WL 185. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS SRM 51-40-4 FIG 1 AND 51-30-2.Jul 6, 1996 · N951UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEAO1209Center Post · crackedFUSE CENTER POST BETWEEN PILOT AND COPILOTS NR 1 WINDOWS CRACKED RT 2RD SCREW DOWN PILOTS NR 4 WINDOW.Jul 2, 1996 · N116FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEAO1206Skin · crackedFUSE SKIN CRACKED I/B LWR CORNER OF PILOTS NR 4 WINDOW. DOUBLER INSTALLED AT LWR I/B CORNER OF PILOTS NR 4 WINDOW PER SRM 53-30-3.Jul 2, 1996 · N116FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 96FDEAO1205Skin · crackedFUSE AFT/LWR CORNER OF PILOTS NR 3 WINDOW SKIN CRACKED. DOUBLER INSTALLED PER SRM 53-30-3.Jul 2, 1996 · N116FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 96FDEA01302Casting · crackedUPPER LOBE MAIN CARGO STA 870 CASTING WL 190 LT HFEC INDICATES CRACK, AREA MARKED. CUT OUT CORROSION AND CRACK PER EA, INSTALLED REPAIR FITTING IAW EA 7-5310-28783.Jul 2, 1996 · N116FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01209Ctr Post · damagedFUSE CENTER POST BETWEEN PILOT AND COPILOT NR 1 WINDOWS CRACKED RIGHT 3RD SCREW DOWN, PILOTS NR 4 WINDOW. NDT VERIFIED NO CRACK FOUND WITH HFEC.Jul 2, 1996 · N116FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01090Bellframe · crackedSTR 9L IS CRACKED AT BELLFRAME 440L LWR RIVET. STR FLANGE CRACKED, VIEWED FROM UNDERSIDE AT RIVET BULKTAIL. REMOVED DAMAGED SECTION OF STR 9L FROM STA 430 TO 450. INSTALLED NEW SECTION OF STR 9L STA 430 TO 450 PER SRM 53-10-3 PGS 5, 6, 7 AND 8.Jun 11, 1996 · N120FE · Boeing 72725C · Fuselage Main, FrameSDR 96FDEA01055Hyd Line · leakingHYDRAULIC SYSTEM-A FAILURE, QTY DROPPED TO ZERO, MANUALLY CRANKED GEAR DOWN. FLUID SHUTOFF VALVES OFF FOR 30 MINUTES PRIOR TO ENGINE SHUTDOWN. PARTS CATALOG 27-60-00 FIG 20 PG 1, FOUND HYD FLUID LEAKING FROM B-NUT TO T-FITTING NR 60 AND A SMALLER LEAK AT T-FMay 30, 1996 · N118FE · Boeing 72725C · Hydraulic System, MainSDR 96FDEA01050Floor Web · corrosionCABIN CORROSION ON FLOOR WEB STA 1178 APPROX 55 INCHES LBL UPPER SURFACE UNDER CHORD ANGLE. CUT OUT DAMAGED FLOOR WEB AREA, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2.May 28, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01049Vert Angle · crackedVERT ANGLE CRACKED AT LIGHTENING HOLE AT BS 1183 RBL 26 TO 9 WL 253. PERFORMED 1183 VERTICAL BEAM MOD PER BOEING SERVICE BULLETIN 727-53-0182 PG 23 SRM 53-10-9.May 28, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01048Hinge Casting · brokenLARGE HINGE ASSEMBLY FOR LEFT HAND O/B AILERON HAS BAR BROKEN OFF. REMOVED HINGE CASTING AND INSTALLED A SERVICEABLE CASTING PER DRAWING NR 65-19260 SHEET 1.May 28, 1996 · N136FE · Boeing 72725C · AileronsSDR UPS96220585Floor Beam · corrodedINSPECTION TYPE-C, FLOOR BEAM CORRODED AT STA 480 FROM BL 0 TO RBL 48. CUT OUT DAMAGED AREA AT STA 480, FROM LBL 12 TO RBL 65 PER SRM 53-10-8, FAB'D AND INSTALLED UPPER CAP REPAIR PER SRM 53-10-8 FIG 5 AND SRM 51-30-2.May 21, 1996 · N946UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96220586Skin · crackedINSPECTION TYPE-C, RT AFT EMERGENCY EXIT HAS TWO OPEN HOLES AND ONE HOLE IS CRACKED OUT TO THE EDGE OF SKIN. CUT OUT DAMAGE ON RT AFT EXIT DOOR PER SRM 52-40-2 FIG 1, FAB'D DOUBLER AND INSTALLED IAW SRM 52-40-11, 52-40-2 FIG 1 AND SRM 51-30-2.May 20, 1996 · N946UP · Boeing 72725C · Emergency ExitsSDR UPS96220135Engine · failedNR 2 ENGINE FAILED INFLIGHT. REMOVED AND REPLACED NR 2 ENG PER T/C 1202 (P/N JT8D-7B) (S/N 68500). REMOVED MAIN ENGINE OIL STRAINER, FOUND LARGE AMOUNTS OF METAL.May 17, 1996 · N950UP · Boeing 72725C · Engine (Turbine/Turboprop)SDR UPS96220132Light · inoperativeCOCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OP CHECKS GOOD (P/N 10-0067-9), OFF (S/N 19703), ON (S/N 26798).May 16, 1996 · N947UP · Boeing 72725C · Emergency LightingSDR UPS96220118Light · inoperativeINSPECTION TYPE: EMERGENCY EXIT LIGHT FAILED TO TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY.May 15, 1996 · N947UP · Boeing 72725C · Emergency LightingSDR UPS96220589Fitting · corrodedINSPECTION TYPE-C, RT FUSELAGE TERMINAL FITTING BS 870 HAS A 1 INCH CRACK EXTENDING BETWEEN TWO FASTENERS FWD, OUTER FLANGE, SIX INCHES ABOVE STR 13R. REMOVED AND REPLACED RT 870 TERMINAL FITTING PER BOEING DWG 65C-23231 AND UPS EO 727-5310-3056.May 9, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220588Spar Web · crackedINSPECTION TYPE-C, LT O/B AILERON SPAR WEB IS CRACKED AT O/B TAB ROD AREA THROUGH HOLE. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-2 FIG 1.May 9, 1996 · N946UP · Boeing 72725C · AileronsSDR UPS96220587Spar · crackedINSPECTION TYPE-C, LT O/B AILERON SPAR UPPER CHORD IS CRACKED O/B OF NR 2 HINGE. REMOVED AND REPLACED UPPER CHORD IAW SRM 51-10-1, 51-30-2 AND BOEING DWG 65-21723.May 8, 1996 · N946UP · Boeing 72725C · AileronsSDR UPS96220186Stringer Tie · crackedINSPECTION TYPE: C. STA 990 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220185Stringer Tie · crackedINSPECTION TYPE: C. STA 970 AT STR 7R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220184Stringer Tie · crackedINSPECTION TYPE: C. STA 970 AT STR 2R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220183Stringer Tie · crackedINSPECTION TYPE: C. STA 970 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220182Stringer Tie · crackedINSPECTION TYPE: C. STA 970 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous Structure
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