N103FE, cancelled Jan 31, 2006

Service difficulty reports · 19

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 = 'N103FE' AND deregistration_id = 'N103FE-2006-01-31'
  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 03FDEA01262Skin · crackedCRACK INDICATED AT BS 441 BETWEEN STR 1L AND 2L.Jul 30, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 03FDEA01263Tab · delaminatedLOWER RUDDER TAB 2FH SIDE UPPER END IS DELAMINATED AT AFT END.Jul 21, 2003 · N103FE · Boeing 727100 · Rudder, Tab StructureSDR 03FDEA01264Tab · delaminatedLOWER RUDDER TAB 2FH SIDE IS DELAMINATED 13 22 ABOVE PUSH ROD ATTACH FITTING.Jul 21, 2003 · N103FE · Boeing 727100 · Rudder, Tab StructureSDR 03FDEA01267Skin · crackedL 2FH NLG 2F SKIN CRACKED AT STA 242 BELOW PANEL CUTOUT.Jul 19, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 03FDEA01266Flange · crackedE AND E COMPT STA 420 STR 26R CRACKED AT LWR FLANGE AND BENT AT STA 422. REPAIRED CRACKED STRINGER IAW BOEING 727-100 SRM 53-10-3Jul 19, 2003 · N103FE · Boeing 727100 · Fuselage Main, StructureSDR 03FDEA01269Skin · crackedL 2FH NLG 2F SKIN CRACKED AT STA 242 BELOW PANEL CUT OUT.Jul 19, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 03FDEA01265Skin · crackedAFT CARGO COMPT DOOR LOWER BEAM 22 FOR INTERIOR SKIN IS CRACKED BEYOND STOP DRILL AT FWD END.Jul 18, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 00FDEA00412Flap · malfunctionedWHILE CONFIGURING FOR LANDING, FLAP HANDLE AT 25 DEGREES, INBD FLAP INDICATOR (FWD ONE) READ 0. DURING GO-AROUND WHEN FLAPS CONFIGURED TO 15, FWD INBD INDICATOR 15 & ALL INDICATORS WORKED NORMAL. RAN FLAPS THRU SEVERAL CYCLES OPS CHECK GOOD PER 27-52-000-0. Jun 27, 2000 · N103FE · Boeing 72722C · Trailing Edge Flap Control SystemSDR 99FDEA00359Control Valve · failedBURNING SMELL IN COCKPIT AREA AND IN BULKHEAD AREA NEXT TO LAVATORY. REPLACED FLOW CONTROL VALVE PER B727 MM 21-58-021-4. NO FURTHER SMELLS DETECTED. A/C OK FOR SERVICE.Sep 1, 1999 · N103FE · Boeing 72722C · Air Distribution SystemSDR 97FDEA00649Computer · failed97-0177 ON T/O UPON ROTATION, THE STALL WARN STICK SHAKER ACTIVATED. USED FIREWALL PWR ON ALL 3 ENG FOR APPROX 45 SEC. ALL ENG PARAMETERS AT RED LINE (N1,EGT). REDUCED ENG POWER AND CONTINUED AROUND FOR A NORM LANDING WITH THE STALL WARN STICK SHAKER ACTIVASep 11, 1997 · N103FE · Boeing 72722C · Stall Warning SystemSDR 96FDEA00771Floor Beam · corrodedUPPER LOBE, CORROSION BEYOND LIMITS IN DEPTH ON TOP SURFACE OF FLOOR BEAM BS 480, RBL 26 TO 35. CUT OUT AREA OF CORROSION AND INSTALLED FLOOR BEAM REPAIR PER SRM 51-10-6, 51-10-8 FIG 6 AND 8, ESO 11782 DATE 3-20-96 AA AND EA 7-5310-28846 DATED 3-20-96 FEDEX.Apr 4, 1996 · N103FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA00770Stringer · crackedFUSE STR 25R CRACKED AROUND FASTENER STA 365. FABRICATED AND INSTALLED REPAIR SECTION OF STR 25R, STR 365 PER SRM 53-10-3 PAGE 4C AND E.Apr 2, 1996 · N103FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 96FDEA00769Bulkhead · ripplesFUSE RIPPLES IN 1183 BULKHEAD AT BOTTOM INSIDE TAIL SKID COMP. REPAIRED RT 1183 BULKHEAD AT TAIL SKID AREA PER ESO 11782 DATED 03-18-96 AND EA NR 7-5310-28179 DATED 3-26-96.Mar 28, 1996 · N103FE · Boeing 72722C · Fuselage Main, BulkheadSDR 96FDEA00713Bellframe · dentUPPER LOBE BS 580 STR 6R DENT IN BELLFRAME. REMOVED DAMAGED SECTION OF BELLFRAME, FABRICATED SECTION OF BELLFRAME, INSTALLED BELLFRAME REPAIR PER SRM 53-10-4 FIG 1.Mar 26, 1996 · N103FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA00712Bellframe · crackedAFT CARGO COMP FS 1090 BELLFRAME CRACKED IN FLANGE AND INTO WEB IN AREA BETWEEN STR 26 AND 27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-3.Mar 25, 1996 · N103FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA00711Bulkhead · crackedAFT CARGO COMPARTMENT FS 1183 BULKHEAD IS CRACKED BL 30 RT, 10 ABOVE STR 26L COMING OUT BEHIND HORIZ STIFFENER. CRACKED AREA OF BULKHEAD REMOVED AND FILLER AND DOUBLER INSTALLED PER BOEING SB 727-53-0215.Mar 20, 1996 · N103FE · Boeing 72722C · Fuselage Main, BulkheadSDR 96FDEA00709Floor Beam · corrosionUPPER LOBE SLAT BS 344 FLOOR BEAM HAS CORROSION FROM RBL 2 TO LBL 54. REMOVED CORRODED BEAM CAP OF FLOOR BEAM AND INSTALLED NEW REPAIR PER SRM 53-10-8.Mar 19, 1996 · N103FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 95FDEA00446Engine · failedDURING FLT HAD NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT WITH 46 PSI OIL PRESS NR 1 ENG SHUTDOWN AS PER RED TABS. LIGHT CAME ON AT START OF DESCENT. MINOR VIBRATION NOTED DURING FLIGHT, BUT ALL INDICATIONS NORMAL UNTIL LIGHT CAME ON. FOUND METAL IN THE OIL SYSMay 2, 1995 · N103FE · Boeing 72722C · Engine (Turbine/Turboprop)SDR 95FDEA00074Support · corroded2 CORRODED FASTENERS RBL 40, BS 320, WL 208 UNDERSIDE OF BEAM AND CHORD. ALSO, FOUND FLOOR SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT PER BOEING DRAWING 65-26173, FEDEX SRM 51-10-02, 51-30-2 AND MM 51-20-21.Jan 23, 1995 · N103FE · Boeing 72721C · Fuselage Miscellaneous Structure
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