# Service difficulty reports: N156FE, cancelled Oct 15, 2002 A list on [N156FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N156FE-2002-10-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 98FDEA00545](https://openairdocs.org/sdr/98FDEA00545.md): Annunciator Pnl · failed · Sep 3, 1998 · N156FE · Boeing 72725 · Landing Gear Position and Warning > LT MLG GREEN LIGHT DID NOT COME ON AFTER GEAR EXTENSION. RAISED GEAR AND REPLACED LEFT GEAR BULBS AND TESTED LIGHTS. THE LT GEAR GREEN LIGHTS TESTED GOOD BUT NOSE GEAR DID NOT TEST. REPLACED NOSE GEAR BULBS STILL DID NOT TEST BUT LOWERED GEAR AND GOT ALL GR - [SDR 98FDEA00138](https://openairdocs.org/sdr/98FDEA00138.md): Skin · damaged · Feb 24, 1998 · N156FE · Boeing 72725 · Fuselage Structure (General) > WORKING FASTENERS IN RT SIDE OF FUSELAGE OF NR 2 ENGINE AT BS 1342 BETWEEN RAIN GUTTER AND ACCESS PANEL. *S/D* REMOVED DAMAGED SECTION OF SKIN BS 1328 TO 1342, STR 20 RT TO STR 27 RT PER FED-EX SRM 53-30-3 FIG 15A. FABRICATED REPAIR PARTS AND INSTALLED REPA - [SDR 98FDEA00094](https://openairdocs.org/sdr/98FDEA00094.md): Web · corroded · Feb 10, 1998 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > NR 0400 006 WHILE WORKING NR0259, FOUND CORROSION ON FLOOR WEB BS 294-328, RBL 15-30, WL 168. FOUND CORROSION ON FLOOR WEB BS 294-328, RBL 15-30, WL 168 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. FABRICATED NEW WEB BS 294 TO 350, RBL 15-30, WL 168 IAW FED-E - [SDR 98FDEA00093](https://openairdocs.org/sdr/98FDEA00093.md): Web · corroded · Feb 10, 1998 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > WHILE WORKING NR0159 FOUND CORROSION BETWEEN THE NOSE WHEEL WELL HORIZONTAL WEB AND BONDED DOUBLER AT BS 306, WL 182, LBL 14 TO RBL 14. *S/D* FOUND CORROSION ON WEB BS 306, WL 182, LBL 14 TO RBL 14 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REPAIRED WEB BY - [SDR 98FDEA00088](https://openairdocs.org/sdr/98FDEA00088.md): Chord · corroded · Feb 5, 1998 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > NR 0401 004 WHILE WORKING NR 0259 FOUND CORROSION BS 300, WL 168, RBL 16 ON NOSE WHEEL WELL CHORD. REMOVED AND REPLACED NOSE WHEEL WELL CHORD BS 300, WL 168, RBL 16 IAW FED-EX DRAWING 65-18415 AND FED-EX SRM 51-30-2. - [SDR 98FDEA00087](https://openairdocs.org/sdr/98FDEA00087.md): Chord · corroded · Feb 5, 1998 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > CORROSION (C53- 224-03) BS 351.2, WL 168, LBL 16 ON NOSE WHEEL WELL CHORD. *S/D* CORROSION BS 351.2, WL 168, LBL 16 ON NOSE WHEEL WELL CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED LT MED CHORD BS 294.5 -0 350 AND REPLACED WITH NEW (P/N 65 - [SDR 98FDEA00084](https://openairdocs.org/sdr/98FDEA00084.md): Fitting · corroded · Feb 3, 1998 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > NR 0145 001, CORROSION (C53-224-04) ON BRACKET AT BS 1180, RBL 66, WL 208. CORROSION ON BRACKET AT BS 1180, RBL 66, WL 208 FOUND TO BE OUT OF LIMITS. REMOVED.060 FROM.080 ORIGINAL THICKNESS MATERIAL AS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED BRACKET - [SDR 98FDEA00082](https://openairdocs.org/sdr/98FDEA00082.md): Frame · corroded · Feb 3, 1998 · N156FE · Boeing 72725 · Fuselage Main, Frame > NR 0265 002, CORROSION (C53-224-03(1 AND 2) ON FRAME AT BS 425, LBL 11 - RBL 11, WL 150 (FWD OF E-BAY DOOR). FOUND FRAME TO BE CORRODED BEYOND LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED BS 425 FRAME LBL 11 - RBL 13, WL 150 PER BOEING DRAWING 65-1635 - [SDR 96FDEA00349](https://openairdocs.org/sdr/96FDEA00349.md): Position Switch · malfunctioned · Feb 28, 1996 · N156FE · Boeing 72725 · Leading Edge Slat Control System > LEFT I/B LEADING EDGE DEVICE NR 3 WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES WITH NO RETRACTION. REPLACED NR 3 KREUGER FLAP POSITION SWITCH PER MM 27-82-1, OPS CHECK GOOD. - [SDR 95FDEA01201](https://openairdocs.org/sdr/95FDEA01201.md): Floorbeam · corroded · Aug 25, 1995 · N156FE · Boeing 72725 · Fuselage Main, Floor Beam > CORROSION (72C235-02), ON FLOORBEAM UPPER FLANGE BS 620 RBL 8 TO 17 WL 208. REMOVED AND REPLACED UPPER FLOORBEAM T-CHORD BS 620 LBL 15 RBL 34 PER FEDEX SRM 53-10-8. - [SDR 95FDEA01177](https://openairdocs.org/sdr/95FDEA01177.md): Rib · cracked · Aug 23, 1995 · N156FE · Boeing 72725 · Elevator, Spar/Rib > POSSIBLE CRACK ON THE NR 6 ELEVATOR HINGE RIB UPPER SURFACE BETWEEN THE 2ND AND 3RD RIVET FORWARD FROM THE T/E BEAM. NDI VERIFIED CRACK, REMOVED AND REPLACED NR 6 ELEVATOR HINGE RIB PER FEDEX MM 27-30-21, SRM 51-30-02, EA 7-5510-25592A. - [SDR 95FDEA01176](https://openairdocs.org/sdr/95FDEA01176.md): Spar · corroded · Aug 23, 1995 · N156FE · Boeing 72725 · Wing Spar > CORROSION ON LOWER WING SPAR CHORD AT STA 740, LBL 16, WL 168. ACCOMPLISHED REPAIR OF LOWER 740 CHORD AND SKIN IAW FEDEX EA 7-5710-25579. - [SDR 95FDEA01175](https://openairdocs.org/sdr/95FDEA01175.md): Skin · dented · Aug 22, 1995 · N156FE · Boeing 72725 · Fuselage Main, Plate/Skin > DENT IN FUSELAGE SKIN BS 1135 BETWEEN 2R - 3R. REMOVED DAMAGED SKIN AND REPAIRED PER FEDEX SRM 53-30-3. - [SDR 95FDEA01174](https://openairdocs.org/sdr/95FDEA01174.md): Shear Tie · cracked · Aug 22, 1995 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > SHEAR TIE CRACKED AT BS 1203, WL 249, RBL 66. REPAIRED SHEAR TIE PER EWO 95-2953, BS 1203, RBL 66, WL 249. - [SDR 95FDEA01173](https://openairdocs.org/sdr/95FDEA01173.md): Keel Beam · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Fuselage Main, Keel > CORROSION AROUND FASTENER ON KEEL BEAM AT BS 990-1010 AND BS 1030-1050, S29R. CORROSION REMOVAL WAS OUT OF LIMITS, OVERSIZED FASTENER HOLES TO REMOVE CORROSION, FABRICATED FREEZE PLUGS AND REPAIR ANGLES, INSTALLED ALL WORK DONE PER TRAMCO EWO NR 95-2968, EA 7 - [SDR 95FDEA01172](https://openairdocs.org/sdr/95FDEA01172.md): Bullnose · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Leading Edge Devices > CORROSION ON NR 6 K-FLAP O/B BULLNOSE ACTUATING ROD LOWER ATTACH POINT AT BULLNOSE. REMOVED AND REPLACED NR 6 K-FLAP PER FEDEX MM 27-81-01. - [SDR 95FDEA01171](https://openairdocs.org/sdr/95FDEA01171.md): Skin · cracked · Aug 22, 1995 · N156FE · Boeing 72725 · Fuselage Main, Plate/Skin > LIGHTNING STRIKE BS 444 BETWEEN FASTENER ON STR 4L. FOUND LIGHTNING STRIKE DAMAGE TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. - [SDR 95FDEA01170](https://openairdocs.org/sdr/95FDEA01170.md): Skin · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Leading Edge Devices > CORROSION ON NR 4 K-FLAP O/B UPPER GROUND WIRE ATTACH POINT. REMOVED AND REPLACED NR 4 K-FLAP PER FEDEX MM 27-81-1. - [SDR 95FDEA01169](https://openairdocs.org/sdr/95FDEA01169.md): Bonding Jumper · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Leading Edge Devices > CORROSION ON NR 5 K-FLAP I/B UPPER BONDING JUMPER ATTACH POINT. REMOVED AND REPLACED NR 5 K-FLAP PER FEDEX MM 27-01-01. - [SDR 95FDEA01168](https://openairdocs.org/sdr/95FDEA01168.md): Skin · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Leading Edge Devices > CORROSION UNDER DATA PLATE NR 2 K-FLAP. REMOVED AND REPLACED NR 2 K-FLAP PER FEDEX MM 57-53-0. - [SDR 95FDEA01166](https://openairdocs.org/sdr/95FDEA01166.md): Spar · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Wing Spar > WHILE WORKING CUST ID NR0579, FOUND CORROSION ON REAR SPAR LOWER CHORD L/W STA 250. REPAIRED LOWER REAR SPAR CHORD IAW FEDEX EA 7-5710-25573 AT WS 224.5. - [SDR 95FDEA01165](https://openairdocs.org/sdr/95FDEA01165.md): Floorbeam · corroded · Aug 22, 1995 · N156FE · Boeing 72725 · Fuselage Main, Floor Beam > CORROSION (72C235-02), ON FLOORBEAM BOTTOM SIDE OF UPPER FLANGE BS 660 RBL 50 WL 208. - [SDR 95FDEA01136](https://openairdocs.org/sdr/95FDEA01136.md): Bonding Jumper · corroded · Aug 18, 1995 · N156FE · Boeing 72725 · Leading Edge Devices > CORROSION ON BULLNOSE BONDING JUMPER ON K-FLAP I/B UPPER ATTACH POINT. REMOVED CORROSION AND RELOCATED BONDING JUMPER ON K-FLAP PER FEDEX DRAWING SR37-57-010 RMB. - [SDR 95FDEA01119](https://openairdocs.org/sdr/95FDEA01119.md): Shear Tie · cracked · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > CRACKED SHEAR TIE BS 1148 WL 151 LBL 9.5. REMOVED AND REPLACED SHEAR TIE BS 1148 WL 151 LBL 9.5 PER SRM 51-30-2. - [SDR 95FDEA01118](https://openairdocs.org/sdr/95FDEA01118.md): Frame · cracked · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Main, Frame > CRACK IN FRAME STA 1070 STR 27L. REMOVED DAMAGED AREA OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-4. - [SDR 95FDEA01117](https://openairdocs.org/sdr/95FDEA01117.md): Floor Beam · corroded · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Main, Floor Beam > CORROSION 72C285-02 ON FLOOR BEAM BS 480 RBL 34 - LBL 22 WL208. REMOVED AND REPLACED FLOOR BEAM UPPER T-CHORD FROM BS480 RBL 35 - LBL 35 WL 208 PER SRM 53-10-8. - [SDR 95FDEA01116](https://openairdocs.org/sdr/95FDEA01116.md): Spar · corroded · Aug 15, 1995 · N156FE · Boeing 72725 · Trailing Edge Flaps > R/W I/B FOREFLAP I/B END POTTING COMPOUND MISSING. REMOVEDUPPER SKIN SURFACE OF FLAP, FOUND L/E SPAR CORRODED. REMOVED CORRODED SPAR AND REPLACED WITH NEW SPAR. LAYED UP SKIN REPAIRS. ALL WORK DONE IAW FEDEX SRM 51-40-6, 51-30-2 AND FEDEX MM 51-20-151, 51- - [SDR 95FDEA01115](https://openairdocs.org/sdr/95FDEA01115.md): Stringer · damaged · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Main, Longeron/Stringer > WHILE REMOVING STR CLIP 2R, DAMAGED STR BS 660. REMOVED AND REPLACED DAMAGED STR 2R FROM BS 670-690 PER SRM 53-10-3. - [SDR 95FDEA01114](https://openairdocs.org/sdr/95FDEA01114.md): Floor Beam · corroded · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Main, Floor Beam > CORROSION 72C235-02 ON FLOOR BEAM BS 560 RBL 4-23 WL 208. REMOVED AND REPLACED UPPER T-CHORD PER FEDEX SRM 51-30-08. - [SDR 95FDEA01113](https://openairdocs.org/sdr/95FDEA01113.md): Str Clip · damaged · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > DAMAGED STR CLIP BS 660 STR 2R. REMOVED AND REPLACED STR CLIP 2R PER FEDEX SRM 51-30-2. - [SDR 95FDEA01107](https://openairdocs.org/sdr/95FDEA01107.md): Spar · corroded · Aug 15, 1995 · N156FE · Boeing 72725 · Trailing Edge Flaps > R/W I/B FOREFLAP I/B END POTTING COMPOUND MISSING. REMOVED UPPER SKIN SURFACE OF FLAP, FOUND L/E SPAR CORRODED. REMOVED CORRODED SPAR AND REPLACED WITH NEW SPAR LAID UP SKIN REPAIRS, ALL WORK DONE IAW FEDEX SRM 51-40-6, 51-30-2 AND FEDEX MM 51-20-151 AND 51- - [SDR 95FDEA01106](https://openairdocs.org/sdr/95FDEA01106.md): Stringer · damaged · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Main, Longeron/Stringer > WHILE REMOVING STR CLIP 2R DAMAGED STR BS 660. REMOVED ANDREPLACED DAMAGED STR NR 2R FROM BS 670 TO 690 PER SRM 53-10-3. - [SDR 95FDEA01105](https://openairdocs.org/sdr/95FDEA01105.md): Floorbeam · corroded · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Main, Floor Beam > CORROSION 72C235-02, ON FLOORBEAM BS 560 RBL 4 TO 23 WL 208. REMOVED AND REPLACED UPPER T-CHORD PER FEDEX SRM 51-30-08. - [SDR 95FDEA01104](https://openairdocs.org/sdr/95FDEA01104.md): Clip · damaged · Aug 15, 1995 · N156FE · Boeing 72725 · Fuselage Miscellaneous Structure > DAMAGED STR CLIP BS 660 STR 2R. REMOVED AND REPLACED STR CLIP 2R PER FEDEX SRM 51-30-2. - [SDR 95FDEA01093](https://openairdocs.org/sdr/95FDEA01093.md): Seat Track · corroded · Aug 11, 1995 · N156FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings > CORROSION (72C236-02), AROUND SEAT TRACK BS 774 TO 788 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK BS 774 TO 788 LBL 25 WL 208 PER FEDEX SRM 51-30-2. - [SDR 95FDEA01092](https://openairdocs.org/sdr/95FDEA01092.md): Seat Track · corroded · Aug 11, 1995 · N156FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings > CORROSION (72C236-02) FOUND ON SEAT TRACK BS 950 TO 848 RBL25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 950 TO 848 RBL 25 WL 208 PER FEDEX SRM 51-30-2. - [SDR 95FDEA01091](https://openairdocs.org/sdr/95FDEA01091.md): Skin · cracked · Aug 11, 1995 · N156FE · Boeing 72725 · Fuselage Main, Plate/Skin > CRACK IN SKIN AT PREVIOUS REPAIR, BS 1330 LBL 35 WL 163 ON LT SIDE OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR PERFEDEX SRM 53-30-3. - [SDR 95FDEA01080](https://openairdocs.org/sdr/95FDEA01080.md): Bracket · cracked · Aug 9, 1995 · N156FE · Boeing 72725 · Leading Edge Devices > RIGHT WING NR 6 SLAT O/B TRACK TO T/E SKIN MOUNTING BRACKETCRACKED. FABRICATED REPLACEMENT BRACKET IAW FEDEX DWG 69-17497-1, FEDEX SRM 51-20-1. REPLACED CRACKED BRACKET WITH FABRICATED BRACKET IAW FEDEX SRM 51-30-2. - [SDR 95FDEA01079](https://openairdocs.org/sdr/95FDEA01079.md): Seat Track · corroded · Aug 9, 1995 · N156FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings > CORROSION (72C235-02) ON SEAT TRACK BS 693-704 RBL 46 WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM STA 690-740 IAW SRM 51-10-1, 51-30-2, ANDFEDEX MM 51-20-2, 57-20-01. - [SDR 95FDEA01078](https://openairdocs.org/sdr/95FDEA01078.md): Floor Beam · corroded · Aug 9, 1995 · N156FE · Boeing 72725 · Fuselage Main, Floor Beam > CORROSION (72C235-02) ON FASTENER HOLES AT BS 344 LBL 33-57WL 208 DOUBLE DRILLED HOLE AT BS 344 LBL 51 WL 208. REPAIRED FLOOR BEAM IAW FEDEX SRM 53-10-1 AND FEDEX DWG NR SR 27-53-007. - [SDR 95FDEA01077](https://openairdocs.org/sdr/95FDEA01077.md): Escape Slide · torn girt · Aug 9, 1995 · N156FE · Boeing 72725 · Escape Slide > FORWARD ENTRY DOOR ESCAPE SLIDE GIRT IS TORN 1.5 PER TC 72C247-00 THIS REQUIRES REPLACEMENT. REPLACED FORWARD ENTRY DOOR ESCAPE SLIDE ASSY IAW FEDEX MM 25-60-13. - [SDR 95FDEA01075](https://openairdocs.org/sdr/95FDEA01075.md): Skin · puncture · Aug 4, 1995 · N156FE · Boeing 72725 · Trailing Edge Flaps > L/W I/B FOREFLAP HAS A PUNCTURE ON UPPER SURFACE 64 FROM I/B END. L/W I/B FOREFLAP WAS REPAIRED I/W FEDEX SRM 51-40-6. - [SDR 95FDEA01074](https://openairdocs.org/sdr/95FDEA01074.md): Skin · dented · Aug 4, 1995 · N156FE · Boeing 72725 · Trailing Edge Flaps > L/W I/B AT FLAP DENTED LWR SURFACE 56 FROM I/B END. L/W I/B AFT FLAP REPAIRED IAW FEDEX SRM 51-40-6. ## 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 = 'N156FE' AND deregistration_id = 'N156FE-2002-10-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N156FE-2002-10-15/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.