# Service difficulty reports: N147FE, cancelled Mar 6, 2003 A list on [N147FE, cancelled Mar 6, 2003](https://openairdocs.org/deregistered/N147FE-2003-03-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 01FDEA00238](https://openairdocs.org/sdr/01FDEA00238.md): Control Unit · malfunctioned · Mar 30, 2001 · N147FE · Boeing 72722 · Smoke Detection > WHILE HOLDING FOR T/O DURING CROSSBLEED START OF NR 3 ENG. AFT CARGO SMOKE WARNING AND BELL ACTIVATED. FIRED NR 1 FIRE BOTTLE INTO AFT CARGO COMPARTMENT. WARNING STAY ON. INPS AFT CARGO COMP. NO FIRE OR SMOKE. *S/D* REMOVED AND REPLACED AFT CARGO COMP C - [SDR 00FDEA00644](https://openairdocs.org/sdr/00FDEA00644.md): Frame · gouged · Sep 8, 2000 · N147FE · Boeing 72722 · Fuselage Main, Frame > DURING ROUTINE INSP, BS 1342 FRAME FOUND GOUGED BEYOND ALLOWED LIMITS ABOVE STR 20R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW B727 SRM 51-40-3 AND B727 SRM 51-30-2. - [SDR 00FDEA00643](https://openairdocs.org/sdr/00FDEA00643.md): Frame · worn · Sep 8, 2000 · N147FE · Boeing 72722 · Fuselage Main, Frame > DURING ROUTINE INSP, APPROX 4 IN OF FRAME AT BS 1342 FOUND WORN BEYOND LIMITS AT STR 15R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW B727 SRM 51-40-3 AND B727 SRM 51-30-2. - [SDR 00FDEA00638](https://openairdocs.org/sdr/00FDEA00638.md): Cover · cracked · Sep 8, 2000 · N147FE · Boeing 72722 · Escape Slide > DURING ROUTINE INSP, THE EMERGENCY ESCAPE SLIDE COVER FOUND CRACKED IN SEVERAL PLACES. REPAIRED COVER PER IAW B727 SRM 51-40-8. - [SDR 00FDEA00641](https://openairdocs.org/sdr/00FDEA00641.md): Frame · worn · Sep 7, 2000 · N147FE · Boeing 72722 · Fuselage Main, Frame > DURING ROUTINE INSP, APPROX 5 IN OF THE FRAME AT BS 1342 WAS FOUND WORN BEYOND LIMITS AT STR 20R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW SRM 51-40-3 AND B727 SRM 51-30-2. - [SDR 00FDEA00642](https://openairdocs.org/sdr/00FDEA00642.md): Skin · worn · Sep 7, 2000 · N147FE · Boeing 72722 · Fuselage Main, Plate/Skin > DURING ROUTINE INSP, FUSELAGE SKIN WAS FOUND WORN BEYOND LIMITS AT BS 1342 UNDER RAIN GUTTER. REMOVED AND REPLACED, FAB PER IAW B727 SRM 53-30-3. - [SDR 00FDEA00640](https://openairdocs.org/sdr/00FDEA00640.md): Skin · corroded · Sep 6, 2000 · N147FE · Boeing 72722 · Fuselage Main, Plate/Skin > DURING ROUTINE INSP, THE FUSELAGE SKIN FOUND CORRODED BEYOND ALLOWED LIMITS BETWEEN SKIN LAP AT BS 1338, STR 10L. REMOVED AND REPLACED, FAB DOUBLER AND FILLER PER IAW B727 SRM 53-30-3. - [SDR 00FDEA00639](https://openairdocs.org/sdr/00FDEA00639.md): Stiffener · cracked · Sep 6, 2000 · N147FE · Boeing 72722 · Fuselage Miscellaneous Structure > DURING ROUTINE INSP, A VERTICAL STIFFENER FOUND CRACKED AT BS 1070, BETWEEN STR 28R AND 29R. REMOVED, FAB AND INSTALLED PER IAW B727 SRM 51-20-1, 51-30-2. - [SDR 00FDEA00637](https://openairdocs.org/sdr/00FDEA00637.md): Wire · broken · Sep 6, 2000 · N147FE · Boeing 72722 · Light System Wiring > DURING ROUTINE INSP, THE EMERGENCY ESCAPE SLIDE LIGHT WIRE WAS FOUND BROKEN BETWEEN THE BATTERY AND LIGHT. REPAIRED BROKEN WIRE PER IAW WDM 33-51-02. - [SDR 97FDEA00829](https://openairdocs.org/sdr/97FDEA00829.md): Switch · inoperative · Nov 13, 1997 · N147FE · Boeing 72722 · Door Warning System > EQUIPMENT ACCESS DOOR LIGHT INOPERATIVE. AIRCRAFT TOOK OFF WITH ELECTRICAL EQUIPMENT COMPARTMENT OPEN. RAMP ACCOMPLISHED PUSH BACK, INSPECTED ELECTRICAL EQUIPMENT BAY. NO DAMAGE NOTED. CLOSED ELECTRICAL EQUIPMENT DOOR. DEFERRED ELECTRICAL EQUIPMENT DOOR W - [SDR 96FDEA00331](https://openairdocs.org/sdr/96FDEA00331.md): Trim Motor · failed · Feb 28, 1996 · N147FE · Boeing 72722 · Stabilizer Control System > AFTER TAKEOFF, MAIN STABILIZER TRIM FAILED. RESET CIRCUIT BREAKER TO NO AVAIL, CRUISE TRIM WORKED NORMALLY. REPLACED MAIN ELECTRIC STABILIZER TRIM MOTOR PER MM 27-40-31 PAGE 201, OPS CHECK GOOD. - [SDR 95FDEA01315](https://openairdocs.org/sdr/95FDEA01315.md): Skin · corroded · Sep 12, 1995 · N147FE · Boeing 72722 · Fuselage Main, Plate/Skin > STR 9R STA 1352 TO 1420 PILLOWING SKIN. REMOVED AND REPLACED 30 INCHES OF SKIN AND REPAIRED SKINS BOTH FWD AND AFT OF STA 1365.5 STR 9R, PER FEDEX SRM 53-30-3, 51-30-2. - [SDR 95FDEA01313](https://openairdocs.org/sdr/95FDEA01313.md): Chord · corroded · Sep 12, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous Structure > CORROSION ON REINFORCEMENT CHORD STA 1176.9 RBL 55 WL 208. REMOVED PARTS, SECONDARY STRUCTURE AND REMOVED CORRODED REINFORCEMENT CHORD. INSTALLED NEW CHORD AND SECONDARY STRUCTURE. ALL WORK DONE IAW FEDEX SRM 53-10-1, 51-30-2. REPLACED CHORD BS 1176.9 LBL - [SDR 95FDEA01312](https://openairdocs.org/sdr/95FDEA01312.md): Chord · corroded · Sep 12, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous Structure > CORROSION FOUND ON HORIZONTAL CHORD AT RBL 16.5 TO 20 WL 191.5. REPAIRED CORRODED AREA PER EA 7-5310-25687. - [SDR 95FDEA01316](https://openairdocs.org/sdr/95FDEA01316.md): Floor Support · corroded · Sep 8, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous Structure > FLOOR SUPPORT FLANGE AT STA 840 LBL 24 WL 208 HAS INTERGRANULAR CORROSION THAT IS OUT OF LIMITS. FABRICATED REINFORCEMENT STRAP PER EWO NO 95-3069. - [SDR 95FDEA01314](https://openairdocs.org/sdr/95FDEA01314.md): Skin · corroded · Sep 8, 1995 · N147FE · Boeing 72722 · Fuselage Main, Plate/Skin > STRINGER 9L STA 1372 TO 1389 PILLOWING SKIN. REMOVED DAMAGE SECTION OF SKIN AND REPAIRED IAW FEDEX SRM 53-30-3, 51-30-2. - [SDR 95FDEA01272](https://openairdocs.org/sdr/95FDEA01272.md): Stiffener · gouged · Sep 7, 1995 · N147FE · Boeing 72722 · Fuselage Miscellaneous Structure > GOUGE IN FLOORBEAM VERTICAL STIFFENER STA 312 RBL 52 WL 207. REMOVED AND FABRICATED FLOORBEAM VERTICAL STIFFENER. ALL WORK DONE IAW FEDEX SRM 53-20-1. - [SDR 95FDEA01271](https://openairdocs.org/sdr/95FDEA01271.md): Seat Track · corroded · Sep 7, 1995 · N147FE · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK AND FASTENERS AT STA 760 TO 850 LBL 25. REMOVED AND REPLACED SEAT TRACK. ALL WORK DONE IAW FEDEX SRM 53-10-1 AND FEDEX MM 53-20-12. ## 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 = 'N147FE' AND deregistration_id = 'N147FE-2003-03-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N147FE-2003-03-06/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.