N106FE, cancelled Jan 8, 2013

Service difficulty reports · 29

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 = 'N106FE' AND deregistration_id = 'N106FE-2013-01-08'
  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 99FDEA00120Skin · corrodedNR 0562 011 - CORROSION (C53-100-01-5) ON EXTERIOR SURFACE OF SKIN AT BS 1180 BETWEEN STR 6R AND 7R.Mar 23, 1999 · N106FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 99FDEA00116Fitting · corrodedWHILE WORKING NR 310, FOUND CORROSION ON NET CASTING BS 365, LBL 60, WL 208 (MARKED).Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 99FDEA00115Spar · corrodedWHILE WORKING NR 654, FOUND VERTICAL FLANGE OF LWR WING CTR SECTION SPAR CHORD TO BE CORRODED RBL 55-LBL 55, BS 870.Mar 22, 1999 · N106FE · Boeing 72722C · Wing, Center BoxSDR 99FDEA00114Bulkhead Web · corrodedWHILE WORKING NR 654, FOUND WING CENTER SECTION BULKHEAD WEB TO BE CORRODED 100 PERCENT AT RBL 4 TO LBL 4 BS 870.Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Main, BulkheadSDR 99FDEA00113Spar · corrodedCORROSION (C53-132-02,1) ON VERTICAL FLANGE ON 870 CHORD UPPER LBL 47 TO 54.Mar 22, 1999 · N106FE · Boeing 72722C · Wing SparSDR 99FDEA00111Web · corrodedUPON REMOVAL OF SEAT TRACK ON NR 313 FOUND MCD LWR VERTICAL WEB TO BE CORRODED FROM BS 480 TO 620, WL 200 TO 208, LBL 65.Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 99FDEA00110Sill · corrodedUPON REMOVAL OF SEAT TRACK ON NR 313 FOUND CORROSION ON MCD SILL CHORD AT BS 440 TO 660 LBL 65 WL 208.1.Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 99FDEA00088Skin · corrodedPILLOWING SKIN AND DISHED RIVET HEADS BS 234, STR 23R AND 24R, (CORROSION C53-100-01).Mar 8, 1999 · N106FE · Boeing 72722C · Fuselage Main, Plate/SkinSDR 99FDEA00085Strap · delaminatedBS 440 BONDED TEAR STRAP IS DELAMINATED FROM STR 4R TO STR 7R.Mar 5, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01594Floorbeam · corrodedEXFOLIATION CORROSION ON FLOORBEAM AT FS 344 FROM RBL 14 TO LBL 35. CUT AND SPLICED IN NEW SECTION OF UPPER FLOORBEAM CAP AT FS 344 FROM 14 RBL TO 70 LBL IAW SRM 53-10-8 FIG 9.Oct 10, 1996 · N106FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 96FDEA01593Doubler · crackedFINGER DOUBLER IS CRACKED AT DOOR REINFORCEMENT, STATION 600 BELOW STRINGER 2 RT. REMOVED CRACKED BENT SECTION, FABRICATED REPLACEMENT DOUBLER, ALODINED, PRIMED AND INSTALLED WET WITH SEALER. INSTALLED REPAIR IAW SRM 51-40-2. REPLACEMENT DOUBLER 3 BY 6 MATOct 2, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01592Fitting · corrodedMAIN CARGO COMPT 3RD FITTING BOX HAS HEAVY EXFOLIATION CORROSION, 3RD FITTING I/B FROM RT SIDE OF AIRCRAFT, FOR CARGO BARRIER NET 9G FITTING. FABRICATED NEW 9G FITTING BOX ON SHOP W/O AND YUB 2 ATTACHED. REMOVED AND REPLACED 9G FITTING BOX PER SRM 51-10-1.Oct 2, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01591Web · corrodedCENTER TANK, 2 BAD RIVETS ON BACK WEB RBL 40 TO 60 STA 870. REMOVED WEB TO GAIN ACCESS, REMOVED CORROSION, INSTALLED REPAIR PER SRM 51-40-2 AND EA 7-5710-28898 DATED OCT 1, L996.Oct 1, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01590Frame · dentedFRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6.Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01589Frame · dentedFRAME DENTED STA 540 STR 6R. INSTALLED FRAME REPAIR STA 540 STR 6R PER SRM 53-10-6.Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01545Frame · dentedFRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6.Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01543Frame · dentedFRAME DENTED STA 540 STR 6R. INSTALLED FRAME REPAIR STA 540 STR 6R PER SRM 53-10-6.Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01542Frame · dentedFRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6.Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, FrameSDR 96FDEA01548Beam · corrosionNR1052, 0104, LOWER LOBE CORROSION STA 540 BETWEEN C/L AND LB 25 BOTTOM SIDE OF MAIN DECK BEAM. *S/D* REMOVED CORROSION WITH LIMITS, PRIMED AND TREATED.Sep 25, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01546Beam · corrosionNR1051 AND 0104, LOWER LOBE FWD CARGO CORROSION STA 600 FROM LBL 25 TO RBL 25 BOTTOM SIDE OF MAIN DECK BEAM. *S/D* REMOVED CORROSION, TREATED, PRIMED AND INSTALLED DOUBLER REPAIR PER FEDEX EA NR 7-5310-28904 DATED 01 OCT 96.Sep 25, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01532Fitting · crackedNR0577, STR 2L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER 51-10-1.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01531Fitting · crackedNR0578, STR 3L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER 51-10-1.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01530Fitting · crackedNR0579, STR 4L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED, NO CRACK FOUND.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01529Fitting · crackedNR0580, STR 5L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* CHECKED BY NDT, NO CRACK FOUND.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01528Fitting · crackedNR0581 STR 6L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER SRM 51-10-1.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01527Fitting · crackedNR0582, STR 7L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED, NO CRACK FOUND.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01526Fitting · crackedNR0853, STR 8L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED AND CRACK FOUND.Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 96FDEA01547Stringer · corrodedNRO312, HEAVY CORROSION STA 1148 STR 19L. *S/D* REMOVED CORROSION AND INSTALLED REPAIR PER 53-30-3.Sep 23, 1996 · N106FE · Boeing 72722C · Fuselage Main, Longeron/StringerSDR 95FDEA01094Connector · looseLWR AFT BODY OVERHEAT ILLUMINATED IN FLT, COMPLIED WITH ABNORMAL PROCEDURES. LIGHT WENT OUT AND STAYED OUT AFTER TURNING OFF RIGHT PACK AND CLOSING NR 3 BLEED VALVE. RAN ENGINESAND APU LEAKED CHECK RIGHT PACK AND AIR CONDITION BAY. FOUND SEVERAL CLAMPS LEAKAug 12, 1995 · N106FE · Boeing 72722C · Overheat Detection
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