N133FE, cancelled Aug 26, 2004

Service difficulty reports · 38

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N133FE' AND deregistration_id = 'N133FE-2004-08-26'
  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 99FDEA00104Window · crackedPILOTS WINDOW CRACKED IN FLIGHT. INSTALL SERVICEABLE L-1 WINDOW, REFERENCE B727-100 MM 56-11-011-4.Mar 16, 1999 · N133FE · Boeing 72725C · Flight Compartment WindowsSDR 99FDEA00026Computer · malfunctioned99-002O - ELEVATOR HAS 5 TO 6 INCH OF FREEPLAY IN THE YOKE (I.E.) MOVING THE YOKE AND NO RESPONSE FROM THE ELEVATOR. REMOVED AND REPLACED ELEV FEEL COMPUTER, ADJUSTED AND TEST PER 727-100 MM 27-30-101-2. ADJUSTED AND TEST OF STAB TRIM POTENTIOMETER C/W PER 7Jan 23, 1999 · N133FE · Boeing 72725C · Elevator Control SystemSDR 98FDEA00742Feel Unit · inopAFTER DEPARTURE AT 2000 TO 3000 FT MSL, 200 PLUS KNOTS, ELEVATOR FEEL WENT LIMP FOR 3 TO 5 SEC. THEN WITHOUT WARNING FEEL RETURN. *S/D* REMOVED AND REPLACED PNL 9777, 9778 AND ELEV FEEL CONTROL UNIT PER MM 27-30-112. PERFORMED FEEL FORCE SYS MM 27-30-00-05Dec 11, 1998 · N133FE · Boeing 72725C · Elevator Control SystemSDR 98FDEA00499Socket · malfunctioned98-200 - ON SHORT FINAL, NOSE GEAR MAIN GREEN LIGHTS BOTH WENT OUT. AFTER GO AROUND RECYCLED GEAR AND BOTH LIGHTS KEPT FLICKERING. BULBS TESTED GOOD. INSPECTED LIGHT SOCKET, FOUND THAT MOVEMENT ON LENS CAUSE LIGHT TO FLICKER THEN GO OUT. REMOVED AND REPLACAug 11, 1998 · N133FE · Boeing 72725 · Landing Gear Position and WarningSDR 98FDEA00405Windshield · cracked98-0155 - STA-IAD - SAW FLAME AND ARCING ON COPILOTS FROM WIND SCREEN RIGHT NR 1 FROM WINDOW HEAT. WINDOW HEAT WAS SECURED ON RIGHT SIDE, MINUTES LATER WIND SCREEN ON OUTER PANEL BEGAN CRACKING. REMOVED RIGHT NR 1 WINDOW AND INSTALLED SERVICEABLE WINDOW ANDJun 17, 1998 · N133FE · Boeing 72725C · Flight Compartment WindowsSDR 98FDEA00115Door · blown offAIRCRAFT HYDRAULIC SERVICE ACCESS DOOR BLOWN OFF IN FLIGHT. CANNIBALIZED DOOR FROM AIRCRAFT 146 AND INSTALLED ON AIRCRAFT 133, OPS CHECK GOOD.Feb 18, 1998 · N133FE · Boeing 72725C · Hydraulic Compartment DoorsSDR 97FDEA00298Position Switch · malfunctionWHEN GEAR PLACED DOWN, NOSE WHEEL GREEN LIGHT WOULD NOT ILLUMINATE. PRESS TO TEST GOOD. CYCLED GEAR AND GOT A GREEN DOWN AND LOCKED LIGHT. AFTER TROUBLESHOOTING SYS, SUSPECT NOSEGEAR POS SWITCH AS BEING BAD. ORDERED PT AND PT N.I.S. REMOVED ARM FROM LOCK May 21, 1997 · N133FE · Boeing 72725 · Landing Gear Position and WarningSDR 95FDEA01753Fitting · corrodedLT STA 740 WING TERMINAL FITTING ON FUSELAGE, BORE IS CORRODED. REMOVED CORROSION BY BORING HOLE TO 3500 PER SRM 57-10-7 PAGE 3, MADE SLEEVE PER SRM 57-10-7 PART 9 AND 10. INSTALLED TERMINAL SLEEVE PER SRM 51-10-1.Nov 14, 1995 · N133FE · Boeing 72725C · Wing Miscellaneous StructureSDR 95FDEA01722Floorbeam · corrodedSTA 380 FLOORBEAM FOUND TO BE TOO THIN AFTER CORROSION REWORK AT APPROX LBL 54 UPPER AFT FLANGE. REPAIRED FLOORBEAM PER EA 7-5310-25983 DATED 10-26-95.Nov 13, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 95FDEA01723Trunnion · crackedL/W FRONT SPAR BOTTLE BOLT TRUNNION FS 740 CRACKED INSIDE PIN HOLE, 3 PLACES. REMOVED AND REPLACED TRUNNION IAW BOEING DRAWING NR 65C29064.Nov 9, 1995 · N133FE · Boeing 72725C · Wing, Landing Gear Attach FittingsSDR 95FDEA01637Floor Beam · corrodedMAIN CARGO - CORROSION ON BOTTOM OF UPPER FLANGE OF FLOOR BEAM AT STA 640 BETWEEN NR 5 AND NR 6 SEAT TRACK. REMOVED CORROSION PER SRM 51-10-06. REPAIRED FLOOR BEAM PER ESO 11782 AND FEDEX EA 7-5310-25944.Oct 30, 1995 · N133FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 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 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 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 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, Frame
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