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 95FDEA01636Door Frame · crackedFORWARD CARGO AFT CARGO DOOR FRAME STA 572 CRACKED FROM AROUND RIVET ON FRAME AFT DOOR STOP AREA. REMOVED RIVET AND STOP DRILLED. INSTALLED DOUBLER PER 51-10-4, PG 41.Oct 30, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01638Spar Chord · corrodedBS 740, LBL 40 - 46: WING CENTER SECTION FRONT SPAR LOWER CHORD TO LOWER TANK SKIN HAS HEAVY CORROSION. RIVET HEADS SHEARED AND SKIN BULGING. REPAIR PER EA NR 7-5710-26102 DATED 10-24-95.Oct 29, 1995 · N133FE · Boeing 72725C · Wing SparSDR 95FDEA01597Intercostal · crackedAFT CARGO CEILING CORROSION AROUND NUTPLATES STA 1110 AT BL 0. REMOVED CORROSION AND REPAIRED BOTTOM CAP OF BL 0 INTERCOSTAL STA 1110 PER ESO 11782 WITH FEDEX EA 7-5310-25785.Oct 24, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS204857Panel · crackedWHILE ON GROUND, MAINTENANCE FOUND NR 4 SPOILER PANEL CRACKED AT ACTUATOR ATTACH POINTS.Oct 23, 1995 · N937UP · Boeing 72725C · SpoilersSDR UPS204856Panels · crackedWHILE ON GROUND, MAINTENANCE FOUND 34 SPOILER PANEL CRACKED AT ACTUATOR ATTACH POINTS.Oct 23, 1995 · N937UP · Boeing 72725C · SpoilersSDR 95FDEA01634Spar Web · corrodedWING CENTER SECTION, RT SPAR LOWER PORTION OF WEB, SHOWS EVIDENCE OF BULGING AND CORROSION AT LBL 20, BS 870, WEB AND LOWER SPAR CHORD. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS, TRIPLERS AND REPAIR ANGLES PER ESO 11782 AND EA 7-5710-25952 AND 51-10-1.Oct 23, 1995 · N133FE · Boeing 72725C · Wing SparSDR 95FDEA01631Skin · corrodedLFEC INSPECTION INDICATES CORROSION EXCEEDING 10 PERCENT AT BS 441 BETWEEN STR 23-24R FWD LAP. REMOVED CORROSION AND INSTALLED 6.50 INCH BY 14 INCH DOUBLER PER SRM 53-30-4.Oct 23, 1995 · N133FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01582Skin · corrodedLFEC INSP INDICATES CORROSION EXCEEDING 10 PERCENT AT BS 441 BETWEEN STR 23 TO 24 RT FWD LAP. REMOVED CORROSION AND INSTALLED 6.5 INCH BY 14 INCH DOUBLER PER SRM 53-30-4.Oct 23, 1995 · N133FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01640Stringer · crackedSTR 8L IS CRACKED AT LOWER FLANGE ATTACH POINT TO FRAME AT STA 460 IN UPPER LOBE. REMOVED DAMAGED SECTION OF STR 8L STR 460 IN UPPER LOBE. REPAIRED PER SRM 53-10-3 PG 5 - 8.Oct 20, 1995 · N133FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 95FDEA01635Skin · crackedSKIN CRACKED JUST BELOW STR 6 AT FWD ENTRY CUT-OUT (MARKED). INSTALLED FWD ENTRY DOUBLER PER SB 727-53-18621 AND AGING AIRCRAFT AD 94-05-04.Oct 20, 1995 · N133FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01633Stringer · crackedMAIN CARGO STR 16R CRACK AT FRAME STA 500. REMOVED INTERCOSTAL, CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED REPAIR PER SRM 53-10-3.Oct 20, 1995 · N133FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 95FDEA1570Floorbeam · chippedSTA 920 FLOORBEAM IN UPPER LOBE, LOWER FLANGE CHIPPED OUT AT FASTENER HOLE RBL 28 (NR 0753). REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER ESO 11782 DATED 10-13-95.Oct 19, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA1569Stringer · crackedMAIN CARGO UPPER LOBE, STR 16R CRACKED AT STA 380 ATTACHMENT TO FRAME (NR 1020). CUT OUT DAMAGED AREA, REPAIRED PER SRM 53-10-3 PG 3.Oct 19, 1995 · N133FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 95FDEA01721Floorbeam · damagedSTA 920 FLOORBEAM IN UPPER LOBE, LOWER FLANGE CHIPPED OUT AT FASTENER HOLE RBL 28. REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER ESO 11782 DATED 10-13-95 AND EA 7-5310-25946.Oct 19, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA1568Cargo Floor · crackedAFT CARGO FLOOR CRACK IN FRAME AROUND TOOLING HOLE STA 1090, JUST ABOUT STR 27 LT (NR 1020). FABRICATED FRAME REPAIR PER SRM 51-40-3, DOUBLER INSTALLED.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage Floor PanelSDR 95FDEA1567Doubler · crackedTOP FUSELAGE SKIN AT RADOME BULKHEAD STATION 178 CENTER, DOUBLER TOP OF SKIN IS CUT HAS SEVERAL CRACKS AT EDGE (NR 0704). REMOVED OLD DOUBLER, FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-3 PG 47.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA1566Clip · gougedSTR 4L GOUGED UNDER STR CLIP STATION 970, (NR 0707). INSTALLED STR SPLICE AND FILLER PER SRM 53-10-3 FIG 3 PG 5 TO 8.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA1565Press Deck · corrodedHEAVY CORROSION IN RT WHEEL WELL PRESSURE DECK LOCATED JUST O/B AND AFT OF VIEW WINDOW (NR 1036). FILE OPENOct 18, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA1564Floorbeam · corrodedCORROSION ON BOTTOM AND TOP OF UPPER FLANGE OF FLOORBEAM STA 480 LBL 24 RBL 24 IN UPPER LOBE (NR 0757). FILE OPENOct 18, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01719Tank · corrodedCTR FUEL TANK NR 3 BAY RIVET HEAD POPPED AND WEB BULGING AT STA 870, APPROX RBL 12 AT UPPER REAR CHORD ANGLE. INSTALLED REPAIR PER ESO 11782 DATED 10-12-95 AND INSPECTED RBL 12 STA 870 REPAIR IAW ESO 11782 AND REPAIRED PER EA 7-5710-25953.Oct 18, 1995 · N133FE · Boeing 72725C · Fuel StorageSDR 95FDEA01718Pin · corrodedLT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage, Wing Attach FittingsSDR 95FDEA01717Pin · corrodedLT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage, Wing Attach FittingsSDR 95FDEA01632Stringer · damagedSTR 41 GOUGED UNDER STR CLIP STA 970. INSTALLED STR SPLICE AND FILLER PER SRM 53-10-3, FIG 3, PG 5-8.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 95FDEA01600Floorbeam · corrodedCORROSION ON TOP AND BOTTOM OF UPPER FLANGE OF FLOORBEAM STA 480 LBL 24 RBL 24 IN UPPER LOBE. REMOVED CORROSION AND INSTALLED REPAIR IAW 53-10-8 AND EA 7-5310-2595.Oct 18, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01720Pin · corrodedR/W REAR SPAR TO BODY FITTING PIN CORRODED. REMOVED RUSTED CORRODED BODY FITTING PIN. INSTALLED NEW R/W REAR TO BODY FITTING PIN MM 57-41-1.Oct 17, 1995 · N133FE · Boeing 72725C · Wing, Fuselage Attach FittingsSDR 95FDEA01560Floorbeam · corrodedCORROSION ON LWR SIDE OF UPPER LOBE FLOORBEAM STA 480 LBL 24 TO 44. INSTALLED REPAIR IAW 53-10-8 FIG 5 OF SRM AND IAW ATTACHED JOB PROGRESS FORM.Oct 17, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01559Floor Web · corrodedUPPER LOBE FLOOR WEB CORRODED AT STA 540 LBL 44 TO 65. REMOVED CORROSION PER SRM 51-10-6 PG 4 AND INSTALLED DOUBLER PER SRM CHAPTER 53-10-9.Oct 17, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01551Rib · crackedFWD UPPER HOLE AT 12 O'CLOCK ON THE RT RIB CHORD AT STA 760 IS CRACKED. REPAIRED PER EA 7-5710-25838 DATED 10-11-95.Oct 17, 1995 · N135FE · Boeing 72725C · Wing, Rib/BulkheadSDR 95FDEA01550Angle · crackedFWD 2 HOLES IN LT CHORD ANGLE AT STA 760 SHOW CRACKS. REPAIR COMPLETED PER EA 7-5710-25838.Oct 17, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS204809Eel · malfunctionedWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT ASSY AS YOU ENTER CABIN, WOULD NOT WORK WHEN LIGHTS ARMED AND POWER SHUTDOWN. ASSY WOULD ONLY WORK WITH SWITCH ON, ON THE ASSY ITSELF. REMOVED AND REPLACED ASSY USING ORIGINAL BATTERIES, OPS CHECKED NOROct 16, 1995 · N933UP · Boeing 72725C · Emergency LightingSDR 95FDEA01547Sill · corrodedMCD THRESHOLE SILL PLATE CORRODED AT STA 560. REMOVED CORROSION PER 51-10-6 PG 4 TO 5, INSTALLED DOUBLER AT STA 560 PER SRM 53-10-9 PG 11, REF NR 0098.Oct 16, 1995 · N133FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01548Fitting · crackedLT WING FRONT SPAR FWD TERMINAL PIN JOINT HOLE CRACKED AFT END. LEVELED AND SHORED A/C IAW SRM 51-50-1, CUT LOWER CHORD ANGLE AND WEB IAW BOEING DRWG NR 65C29064, REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGOct 15, 1995 · N135FE · Boeing 72725C · Fuselage, Wing Attach FittingsSDR 95FDEA01531Frame · corrodedTHE AREA ABOVE CARGO DOOR, CORROSION ON FRAME BETWEEN STA 1070 TO 1090 RT BELOW STR 18R.Oct 10, 1995 · N133FE · Boeing 72725C · Fuselage Main, FrameSDR 95FDEA01530Frame · crackedAFT CARGO FLOOR CRACK IN FRAME AROUND TOOLING HOLE STA 1090 JUST ABOVE STR 27L. BELT FRAME REPAIR ACCOMPLISHED PER SRM 51-40-3 AND DOUBLER INSTALLED.Oct 10, 1995 · N133 · Boeing 72725C · Fuselage Main, FrameSDR 95FDEA01510Hyd Line · brokenDURING CRUISE FL 290, A/C LOST SYS A-HYD, NO APPARENT REASON. FOUND NR 2 SPOILER PRESS LINE BROKE. REMOVED AND REPLACED PRESS LINE, REMOVED CASE DRAIN FILTERS AND PRESS FILTERS, NO CONTAMINATION FOUND. INSTALLED NEW CASE DRAIN FILTERS PER MM 29-11-41, PRESSOct 7, 1995 · N136FE · Boeing 72725C · Hydraulic System, MainSDR UPS204759Floorbeam · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 328 LBL 33 WL 208. ALSO, HAS MECHANICAL DAMAGE LBL 54 WL 208. REPAIRED FLOORBEAM PER 727 SRM 53-10-8 FIGURE 7 AND EO 727-53-1686.Oct 4, 1995 · N933UP · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01488Fitting Pin · corrodedRIGHT WING REAR SPAR BODY FITTING FWD AND REAR BUSHINGS WORN, BODY FITTING PIN FLANGE CORRODED. INSTALLED NEW RT WING REAR SPAR BODY FITTING PIN PER SRM 51-10-1 PG 4, REPLACED FWD AND REAR BUSHINGS PER 51-10-1 PG 4, ESO 11782 AND FEDEX EA NR 7-5310-25827.Oct 4, 1995 · N135FE · Boeing 72725C · Wing, Fuselage Attach FittingsSDR 95FDEA01487Floor Beam · corrodedCORROSION IN AFT CARGO COMP FS 1110 FLOOR BEAM LOWER FLANGE BL 16L TO 30L. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED FILLER AND DOUBLER PER ESO 11782, INSTALLED FILLER AND DOUBLER PER ESO 11782 AND SRM 51-10-6, 51-40-2. EA NR 7-5310-25810.Oct 3, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01486Floor Beam · corrodedCORROSION IN LOWER FLANGE OF FLOOR BEAM BS 1110, BL 0 - 48 RT, IN AFT CARGO COMP. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED ANGLES AND STRAP PER ESO 11782, INSTALLED SAME PER ESO 11782, EA NR 7-5310-25188.Oct 3, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01485Skin · crackedDOUBLER CRACKED AT RIVET STA 1160 O/B OF STR 26R. REMOVED DAMAGED SKIN AT SKIN LAP STA 1149 - 1163, STR 26R PER SRM 53-30-3 FIG 5. INSTALLED REPAIR DOUBLER FROM STA 1140 - 1167 STR 26R PER SRM 53-30-3, PAGES 20-25.Oct 3, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS204647Eel Batt Pack · looseWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT OVER COCKPIT DOOR MUST BE BANGED ON TO MAKE WORK. FOUND BATT PACK LOOSE. CLEANED DOOR CONTACT PINS AND RESECURED BATT PACK. OPS CK NORMAL MM 33-50-00.Sep 30, 1995 · N933UP · Boeing 72725C · Emergency LightingSDR 95FDEA01463Floorbeam · corrodedCORROSION TOP SIDE OF FLOORBEAM STA 312 LBL 35. REPAIR PER SRM 53-10-2.Sep 29, 1995 · N135FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01462Stringer · damagedFASTENERS PULLED THROUGH SIDE OF STR 24R STA 460 TO 484. REMOVED FASTENERS AND REPAIRED STR PER SRM 51-10-3.Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR 95FDEA01461Skin · corrodedCORROSION BETWEEN SKINS IN CORNER OF FWD ENTRY DOOR CUTOUT, FWD UPPER CORNER APPROX STA 310 TO 318, CORNER OF DOOR AND PROCEEDS FWD TO APPROX STA 303 AREA. REPAIRED PER EA 7-5330-25765 DATED 9-18-95.Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 95FDEA01455Casting · corrodedTHE 9G NET CASTING HAS HEAVY CORROSION, JUST I/B OF RBL 45 SEAT TRACK AND CRACKED STA 460 TO 487. FABRICATED NEW SUPPORT PER EA 7-5320-25815 DATED 9-25-95. INSTALLED FITTING 9G AT RBL 45 IAW ESO 11782 DATED 9-15-95 AND SRM 51-10-1.Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01454Casting · corrodedUPPER LOBE FLOOR, FOUND CORROSION ON 9G NET FLOOR ANCHOR STA 360 LT LBL 24. INSTALLED NEW NET ANCHOR CASTING PER SRM 51-10-1 EA 7-5320-25815 DATED 9-25-95.Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 95FDEA01453Skin · crackedCRACK IN SKIN AT FWD EDGE OF ENTRY DOOR CUTOUT JUST BELOW STR 7L. REPAIRED PER ESO 11782 DATED 9-15-95 AND EA 7-5330-25765 DATED 9-18-95.Sep 28, 1995 · N135FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS204579Te Skin · delaminatedWHILE ON GROUND, MAINTENANCE FOUND NR 6 SPOILER LT WING DELAMINATED ON TRAILING EDGE. REMOVED AND REPLACED NR 6 GROUND SPOILER (P/N 65-17348-108A) (S/N 5758) ON, (P/N 65-17348-55) (S/N 6307) OFF.Sep 27, 1995 · N931UP · Boeing 72725C · SpoilersSDR UPS204578Eel Battery Pack · dischargedWHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT BATTERY PACK DIM. REMOVED AND REPLACED BATTERY LIGHT PACK.Sep 27, 1995 · N933UP · Boeing 72725C · Emergency LightingSDR 95FDEA01456Frame · crackedBS 870 TERMINAL FITTING AFT ROW 2ND FASTENER HOLE ABOVE STR 10R HAS CRACK IND, AT 12 O'CLOCK ON O/B SIDE OF O/B FLANGE, RT SIDE FUSELAGE. CRACK IN FRAME STA 870 RT JUST ABOVE STR 10R CRACK IND IS BETWEEN THE 3RD AND 4TH FASTENER ABOVE STR 10R. INSTALLED DOUBSep 27, 1995 · N135FE · Boeing 72725C · Fuselage Main, Frame
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