# Service difficulty reports: N106FE, cancelled Jan 8, 2013 A list on [N106FE, cancelled Jan 8, 2013](https://openairdocs.org/deregistered/N106FE-2013-01-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 99FDEA00120](https://openairdocs.org/sdr/99FDEA00120.md): Skin · corroded · Mar 23, 1999 · N106FE · Boeing 72722C · Fuselage Main, Plate/Skin > NR 0562 011 - CORROSION (C53-100-01-5) ON EXTERIOR SURFACE OF SKIN AT BS 1180 BETWEEN STR 6R AND 7R. - [SDR 99FDEA00116](https://openairdocs.org/sdr/99FDEA00116.md): Fitting · corroded · Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > WHILE WORKING NR 310, FOUND CORROSION ON NET CASTING BS 365, LBL 60, WL 208 (MARKED). - [SDR 99FDEA00115](https://openairdocs.org/sdr/99FDEA00115.md): Spar · corroded · Mar 22, 1999 · N106FE · Boeing 72722C · Wing, Center Box > WHILE WORKING NR 654, FOUND VERTICAL FLANGE OF LWR WING CTR SECTION SPAR CHORD TO BE CORRODED RBL 55-LBL 55, BS 870. - [SDR 99FDEA00114](https://openairdocs.org/sdr/99FDEA00114.md): Bulkhead Web · corroded · Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Main, Bulkhead > WHILE WORKING NR 654, FOUND WING CENTER SECTION BULKHEAD WEB TO BE CORRODED 100 PERCENT AT RBL 4 TO LBL 4 BS 870. - [SDR 99FDEA00113](https://openairdocs.org/sdr/99FDEA00113.md): Spar · corroded · Mar 22, 1999 · N106FE · Boeing 72722C · Wing Spar > CORROSION (C53-132-02,1) ON VERTICAL FLANGE ON 870 CHORD UPPER LBL 47 TO 54. - [SDR 99FDEA00111](https://openairdocs.org/sdr/99FDEA00111.md): Web · corroded · Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > UPON 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. - [SDR 99FDEA00110](https://openairdocs.org/sdr/99FDEA00110.md): Sill · corroded · Mar 22, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > UPON REMOVAL OF SEAT TRACK ON NR 313 FOUND CORROSION ON MCD SILL CHORD AT BS 440 TO 660 LBL 65 WL 208.1. - [SDR 99FDEA00088](https://openairdocs.org/sdr/99FDEA00088.md): Skin · corroded · Mar 8, 1999 · N106FE · Boeing 72722C · Fuselage Main, Plate/Skin > PILLOWING SKIN AND DISHED RIVET HEADS BS 234, STR 23R AND 24R, (CORROSION C53-100-01). - [SDR 99FDEA00085](https://openairdocs.org/sdr/99FDEA00085.md): Strap · delaminated · Mar 5, 1999 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > BS 440 BONDED TEAR STRAP IS DELAMINATED FROM STR 4R TO STR 7R. - [SDR 96FDEA01594](https://openairdocs.org/sdr/96FDEA01594.md): Floorbeam · corroded · Oct 10, 1996 · N106FE · Boeing 72722C · Fuselage Main, Floor Beam > EXFOLIATION 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. - [SDR 96FDEA01593](https://openairdocs.org/sdr/96FDEA01593.md): Doubler · cracked · Oct 2, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > FINGER 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 MAT - [SDR 96FDEA01592](https://openairdocs.org/sdr/96FDEA01592.md): Fitting · corroded · Oct 2, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > MAIN 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. - [SDR 96FDEA01591](https://openairdocs.org/sdr/96FDEA01591.md): Web · corroded · Oct 1, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > CENTER 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. - [SDR 96FDEA01590](https://openairdocs.org/sdr/96FDEA01590.md): Frame · dented · Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, Frame > FRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6. - [SDR 96FDEA01589](https://openairdocs.org/sdr/96FDEA01589.md): Frame · dented · Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, Frame > FRAME DENTED STA 540 STR 6R. INSTALLED FRAME REPAIR STA 540 STR 6R PER SRM 53-10-6. - [SDR 96FDEA01545](https://openairdocs.org/sdr/96FDEA01545.md): Frame · dented · Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, Frame > FRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6. - [SDR 96FDEA01543](https://openairdocs.org/sdr/96FDEA01543.md): Frame · dented · Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, Frame > FRAME DENTED STA 540 STR 6R. INSTALLED FRAME REPAIR STA 540 STR 6R PER SRM 53-10-6. - [SDR 96FDEA01542](https://openairdocs.org/sdr/96FDEA01542.md): Frame · dented · Sep 26, 1996 · N106FE · Boeing 72722C · Fuselage Main, Frame > FRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6. - [SDR 96FDEA01548](https://openairdocs.org/sdr/96FDEA01548.md): Beam · corrosion · Sep 25, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR1052, 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. - [SDR 96FDEA01546](https://openairdocs.org/sdr/96FDEA01546.md): Beam · corrosion · Sep 25, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR1051 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. - [SDR 96FDEA01532](https://openairdocs.org/sdr/96FDEA01532.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0577, STR 2L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER 51-10-1. - [SDR 96FDEA01531](https://openairdocs.org/sdr/96FDEA01531.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0578, STR 3L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER 51-10-1. - [SDR 96FDEA01530](https://openairdocs.org/sdr/96FDEA01530.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0579, STR 4L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED, NO CRACK FOUND. - [SDR 96FDEA01529](https://openairdocs.org/sdr/96FDEA01529.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0580, STR 5L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* CHECKED BY NDT, NO CRACK FOUND. - [SDR 96FDEA01528](https://openairdocs.org/sdr/96FDEA01528.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0581 STR 6L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER SRM 51-10-1. - [SDR 96FDEA01527](https://openairdocs.org/sdr/96FDEA01527.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0582, STR 7L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED, NO CRACK FOUND. - [SDR 96FDEA01526](https://openairdocs.org/sdr/96FDEA01526.md): Fitting · cracked · Sep 24, 1996 · N106FE · Boeing 72722C · Fuselage Miscellaneous Structure > NR0853, STR 8L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED AND CRACK FOUND. - [SDR 96FDEA01547](https://openairdocs.org/sdr/96FDEA01547.md): Stringer · corroded · Sep 23, 1996 · N106FE · Boeing 72722C · Fuselage Main, Longeron/Stringer > NRO312, HEAVY CORROSION STA 1148 STR 19L. *S/D* REMOVED CORROSION AND INSTALLED REPAIR PER 53-30-3. - [SDR 95FDEA01094](https://openairdocs.org/sdr/95FDEA01094.md): Connector · loose · Aug 12, 1995 · N106FE · Boeing 72722C · Overheat Detection > LWR 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 LEAK ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N106FE-2013-01-08/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.