# Service difficulty reports: N402FE, cancelled Jan 25, 2016

A list on [N402FE, cancelled Jan 25, 2016](https://openairdocs.org/deregistered/N402FE-2016-01-25.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 181 reports

- [SDR FDEA201007162570](https://openairdocs.org/sdr/FDEA201007162570.md): Skin · corroded · Jul 16, 2010 · N402FE · Airbus A310203 · Wing, Plate/Skin
  > RT WING UPPER SKIN SURFACE 8 INCH AFT OF REAR SPAR AND RIB 4 HAS 4 SQ INCH OF CORROSION COMMON TO FASTNER HEAD. REPAIR ACCOMPLISHED IAW EA 6-5730-135225 IAW APPROVED DATA REF 6, RAS/BAE/1013408/2010, ISSUE A. THE REPAIR IS IAW THE A/B REPAIR RECOMMENDATIO
- [SDR FDEA201007132499](https://openairdocs.org/sdr/FDEA201007132499.md): Frame · dented · Jul 13, 2010 · N402FE · Airbus A310203 · Fuselage Main, Frame
  > FUSELAGE INTERNAL STRUCTURE AT FR 54.2 HAS (2 EA) AREAS DENTED. AREA NR1=.0781 IN.D X.7500 IN W. AREA NR2 =.0469 IN D X.5 IN W BETWEEN STRINGER 12-15 LT SIDE. REPAIRED FRAME IAW SRM 53-10-12, PARA 5, REPAIR 202, AND EA 6-5310-135243.
- [SDR FDEA201007122480](https://openairdocs.org/sdr/FDEA201007122480.md): Fitting · corroded · Jul 12, 2010 · N402FE · Airbus A310203 · Nacelle/Pylon, Attach Fittings
  > NR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE HAS CORROSION AROUND 4 EA MOUNT HOLES (APPROX 6 SQ IN TOTAL) REMOVED CORROSION FROM NR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE. AROUND 4 EA HOLES IAW SRM 54-51-81 PAGE 101-102 FIG 104 NDT CHECK C/W
- [SDR FDEA201007112475](https://openairdocs.org/sdr/FDEA201007112475.md): Frame · dented · Jul 11, 2010 · N402FE · Airbus A310203 · Fuselage Main, Frame
  > FUSELAGE INTERNAL STRUCTURE FR 54.3 L HAS A DENT APPROX 3/32 INCH DEEP AND 1.5 IN DIAM. BETWEEN STR 14-13 LT MEASURED DENT ON FR 54.3 AT STR. 13L-14L FOUND TO BE OUT OF LIMIT IAW SRM 53-16-13. REPAIRED FR 54.3L IAW EA 6-5310-135243 INSTRUCTIONS AND SRM 53-10-
- [SDR FDEA201007082425](https://openairdocs.org/sdr/FDEA201007082425.md): Rib · gouged · Jul 8, 2010 · N402FE · Airbus A310203 · Leading Edge Devices
  > LT WING L/E KRUEGER FLAP LOWER LIP OTBD L/E GOUGED, 2 SQ INCHES FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, IAW DWG A57843755 AND INSTALLED ON LT WING KRUEGER FLAP OTBD L/E IAW
- [SDR FDEA201007082424](https://openairdocs.org/sdr/FDEA201007082424.md): Shear Tie · cracked · Jul 8, 2010 · N402FE · Airbus A310324 · Cargo/Baggage Doors
  > FWD CARGO DOOR STRUCTURE SKIN SUPPORT ANGLE AFT OF ACTUATOR HINGE FITTING LOWER END HAS 1 IN CRACK REMOVED DAMAGED ANGLE AND STRINGER CLIPS, FABRICATED REPLACEMENT ANGLE AND 2 EA STRINGER CLIPS IAW MFG DWG A52370111 AND DWG A52370142 AND INSTALLED REPLACEMENT
- [SDR FDEA201007082422](https://openairdocs.org/sdr/FDEA201007082422.md): Skin · damaged · Jul 8, 2010 · N402FE · Airbus A310203 · Cargo/Baggage Doors
  > FWD CARGO DOOR HAS DAMAGE STRUCTURE WEB AND HOLE BETWEEN FR 22A AND FR 23 AT BEAM 2. REMOVED DAMAGED AREA OF DOOR SKIN BY CUT OUT OF APPROX 2 IN X 3 IN AND INSTALLED FRAME, STRINGER AND SKIN REPAIR FILLERS AND DOUBLER BETWEEN FR 22 AND FR 23 AT BEAM NR 2 IAW
- [SDR FDEA201007082421](https://openairdocs.org/sdr/FDEA201007082421.md): Rib · damaged · Jul 8, 2010 · N402FE · Airbus A310203 · Leading Edge Devices
  > RT WING KRUEGER FLAP FWD OTBD CORNER HAS IMPACT DAMAGE TO THE EXTERIOR SKIN & CLOSE OUT RIB. FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, AND INSTALLED ON RT WING KRUEGER FLAP IAW SR
- [SDR FDEA201007082406](https://openairdocs.org/sdr/FDEA201007082406.md): Spar · corroded · Jul 8, 2010 · N402FE · Airbus A310203 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB T/E PANEL ATTACH ANGLEAT RT SIDE HAS APPROX 2 SQ INCH OF VISIBLE CORROSION BETWEEN RIB 9 AND AT RIB 10 AT STA 286 AND 309 (2 EA LOCATIONS) BETWEEN RIB. REMOVED CORROSION FROM VERTICAL STAB T/E PANEL ATTACH ANGLE RT SIDE BETWEEN RIB 9 AND R
- [SDR FDEA201007072398](https://openairdocs.org/sdr/FDEA201007072398.md): Crossbeam · cracked · Jul 7, 2010 · N402FE · Airbus A310203 · Fuselage Main, Structure
  > CLS AT FR 36 BETWEEN SEAT TRACKS 3 RT AND 2 RT FWD SIDE LWR SURFACE REPAIR ANGLE CRACKED ON RADIUS, APPROX 1.5 IN LONG REMOVED EXISTING REPAIR ANGLE AT FRAME 36 BETWEEN SEAT TRACKS NR 2 RT AND NR 3 RT FWD SIDE FLOORBEAM, FABRICATED NEW REPAIR ANGLE AND INSTAL
- [SDR FDEA201007072396](https://openairdocs.org/sdr/FDEA201007072396.md): Seat Track · corroded · Jul 7, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 5 RT AT FR 34 TO FR 36 HAS CORROSION AT 3 EA LOCATIONS UPPER SURFACE, APPROX 3 SQ IN REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK, FABRICATED REPLACEMENT SECTION OF TRACK IAW DWG 537B1054 AND INSTALLED REPLACEMENT TRACK AT TRACK 5 R
- [SDR FDEA201007072395](https://openairdocs.org/sdr/FDEA201007072395.md): Floorbeam · corroded · Jul 7, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPT FLOORBEAM CORRODED ON UPPER SURFACE,FR 14 AT SEAT TRACK 3 LT REMOVED LEVEL 1CORROSION. REMOVED, FABRICATED REPLACEMENT TRACK SECTION AND REPLACED DAMAGED SECTION OF TRACK NR3 LT BETWEEN FR 10 AND FR 15A IAW SRM 51-72-10 AND SRM 53-12-15.
- [SDR FDEA201007072394](https://openairdocs.org/sdr/FDEA201007072394.md): Floor Panel · corroded · Jul 7, 2010 · N402FE · Airbus A310203 · Fuselage Floor Panel
  > FRAME 26 SEAT TRACK 4 LT OTBD JUST AFT OF CLS, FOUND CORROSION IN FLOOR PANEL, APPROX 1 SQ INCH REMOVED LEVEL 1 CORROSION. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-10-00, FIG 102. R & R SHEAR PLATE BETWEEN FR 26/32 AND FR 36 AND SEAT TRACK 4LT AND SEAT TRACK 5
- [SDR FDEA201007072393](https://openairdocs.org/sdr/FDEA201007072393.md): Seat Track · corroded · Jul 7, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 6LT INBD SIDE UPPER SURFACE IS CORRODED JUST FWD OF FR 33, APPROX 1 SQ IN REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF SEAT TRACK 6 LT BETWEEN FR 33 AND FR 36 AND INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 53-10-16, FIG 208A, PG 250C/250
- [SDR FDEA201007022330](https://openairdocs.org/sdr/FDEA201007022330.md): Web · damaged · Jul 2, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > WEB BETWEEN FR 14 AND FR 15 BENEATH TRACK 3 LT IS DAMAGED REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 14 AND FR 15 AT SEAT TRACK 3 LT IAW SRM 51-75-10.
- [SDR FDEA201007022329](https://openairdocs.org/sdr/FDEA201007022329.md): Web · damaged · Jul 2, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > WEB HAS DAMAGED HOLES AT FR 10 AND FR 12A SEAT TRACK 3 LT REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 10 AND FR 112A AT SEAT TRACK 3 LT IAW SRM 51-75-10.
- [SDR FDEA201007022328](https://openairdocs.org/sdr/FDEA201007022328.md): Web · damaged · Jul 2, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > WEB BETWEEN FRAME 12A AND 14, BENEATH TRACK 3 LT, IS DAMAGED. REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 12A AND FR 14 AT SEAT TRACK 3 LT IAW SRM 51-75-10.
- [SDR FDEA201007022327](https://openairdocs.org/sdr/FDEA201007022327.md): Floorbeam · corroded · Jul 2, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPT CROSSOVER BEAM HAS CORROSION ON UPPER SURFACE FR 14, BETWEEN SEAT TRACKS 3 LT AND 4 LT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED BEAM, FABRICATED REPLACEMENT BEAM IAW DWG A53611789 AND INSTALLED REPLACEMENT BEAM IAW SRM 51-75-10.
- [SDR FDEA201007022324](https://openairdocs.org/sdr/FDEA201007022324.md): Plate · corroded · Jul 2, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > SUB FLOOR CORRODED APPROX 1 SQ IN AFT OF FR 25 BETWEEN SEAT TRACKS 4 LT AND TRACK 3 LT REMOVED LEVEL 1 CORROSION. R & R SUB FLOOR THRUST PLATE BETWEEN FR 25 AND FR 26/32 AND BETWEEN SEAT TRACKS 3 LT AND 4 LT IAW SRM 51-72-10.
- [SDR FDEA201007022323](https://openairdocs.org/sdr/FDEA201007022323.md): Stringer · corroded · Jul 2, 2010 · N402FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT BILGE AREA, STR 44 LT HAS CORROSION ON VERTCAL LEG FROM FR 62 TO FR 63,APPROX 10 SQ IN. REMOVED LEVEL 1 CORROSION. CUT OUT DAMAGED SECTION OF STR 44 LT AND INSTALLED STRINGER REPAIR AT STR 44 LT BETWEEN FR 62 AND FR 63 IAW SRM 53-10-14, FIG 2
- [SDR FDEA201007012313](https://openairdocs.org/sdr/FDEA201007012313.md): Skin · corroded · Jul 1, 2010 · N402FE · Airbus A310203 · Elevator, Plate/Skin
  > RT ELEVATOR LWR SURFACE SKIN HAS CORROSION 56 INCHES FROM OTBD END, 6 INCHES FWD OF AFT EDGE APPROX 5 SQ IN TOTAL, APPROX ER 34 REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, FOUND LOWER SURFACE OUT OF LIMITS IAW SRM 55-10-00. FABRICATED REPAIR PARTS AND INSTA
- [SDR FDEA201007012312](https://openairdocs.org/sdr/FDEA201007012312.md): Floor Support · corroded · Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > MDCC SEAT TRACK 5L HAS A 4 SQ INCH AREA OF CORROSION BENEATH FLOOR PANEL FR 16A. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-15 FIG 101 FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK 5L, AT FR 16A. IAW SRM 51-40- 21 AND 51-72-10.
- [SDR FDEA201007012311](https://openairdocs.org/sdr/FDEA201007012311.md): Floorbeam · cracked · Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM FWD FACE HAS 0.188 INCH CRACK, ON FR 38, 67 INCHES FROM CTR LINE, LT SIDE. TRIMMED OUT DAMAGE AREA IAW SRM 53-10-15, FIG 201, NDT CHECK IAW NTM 51-10-08. FOUND CRACK EXTENDS TO 1.0 INCH. CUT OUT CRACK DAMAGE AREA IAW SRM 53-10-15, FIG
- [SDR FDEA201007012305](https://openairdocs.org/sdr/FDEA201007012305.md): Floorbeam · corroded · Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MDCC FLOORBEAM HAS CORROSION ON UPPER SURFACE AT FR 14 6IN. BETWEEN SEAT TRACK 3L AND 4L. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND CROSSBEAM SECTION OUT OF LIMITS IAW SRM 51-74-10 AND SRM 53-10-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51
- [SDR FDEA201007012304](https://openairdocs.org/sdr/FDEA201007012304.md): Floorbeam · damaged · Jul 1, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > BULK CARGO COMPT FLOOR STRUCTURE FRAME 69 RBL 20 FLOORBEAM SUPPORT HAS MISDRILLED HOLE THRU UPPER CHORD FWD SIDE. REMOVED DAMAGE AND FABRICATED SPLICE IAW SRM 53-10-15 PG 241/242 FIG 207. INSTALLED REPAIR IAW SRM 53-10-15 AND SRM 51-40-21
- [SDR FDEA201007012303](https://openairdocs.org/sdr/FDEA201007012303.md): Skin · corroded · Jul 1, 2010 · N402FE · Airbus A310203 · Elevator, Plate/Skin
  > RT ELEVATOR UPPER SURFACE HAS APPROX 1.5 SQ IN OF CORROSION AT APPROX. ER36 1 IN. FWD OF AFT EDGE REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND UPPER SURFACE 1 IN FWD OF AFT EDGE, OUT OF LIMITS IAW SRM 55-10-00 FABRICATED REPAIR PARTS AND INSTALL
- [SDR FDEA201007012302](https://openairdocs.org/sdr/FDEA201007012302.md): Skin · corroded · Jul 1, 2010 · N402FE · Airbus A310203 · Elevator, Plate/Skin
  > RT ELEVATOR LWR SURFACE CTR SPLICE HAS CORROSION 8 IN FWD FROM AFT EDGE APPROX 1.5 SQ IN APPROX STA ER21. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND LWR SURFACE CTR SPLICE OUT OF LIMITS IAW SRM 55-10-00. REMOVED DAMAGE, FABRICATED REPAIR PARTS
- [SDR FDEA201006302296](https://openairdocs.org/sdr/FDEA201006302296.md): Support Fitting · cracked · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > AFT CARGO BILGE AREA- FR 54 BULKHEAD SUPPORT FITTING AT STR 53R HAS A 1 IN. CRACK ON OTBD. SIDE ABOUT 3 IN AFT OF BULKHEAD. REMOVED SPLICE AND 2 EA ATTACH FITTINGS IAW SRM 51-72-10, VERIFIED MATERIAL 7175-T7351 08-101155 IAW SRM 53-15-14, FABBED SPLICE FITTING
- [SDR FDEA201006302295](https://openairdocs.org/sdr/FDEA201006302295.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 6R HAS 5EA AREAS CORRODED APPROX 6 SQ IN FROM FR 34 TO FR 39 REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REPAIRED SEAT TRACK 6R BETWEEN FR 34 AND FR 39 IAW DWG R537 B1054 REV B AND SR
- [SDR FDEA201006302294](https://openairdocs.org/sdr/FDEA201006302294.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > 5L SEAT TRACK HAS CORROSION AT 7 EA. LOCATIONS BETWEEN FR 33 AND FR38.1 APPROX 15 SQ INCH REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REPAIRED SEAT TRACK IAW DWG R537, B1054, REV B.
- [SDR FDEA201006302293](https://openairdocs.org/sdr/FDEA201006302293.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 6L HAS 7 AREAS OF CORROSION BETWEEN FR 35 TO FR38 APPROX 10 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REPAIRED SEAT TRACK 6L BETWEEN FR35 AND FR38 IAW SRM 53-10-16, FIG 208A PAGE 250A/
- [SDR FDEA201006302292](https://openairdocs.org/sdr/FDEA201006302292.md): Stringer · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BILGE AREA STR. 45L HAS CORROSION AT FR60 TO FR60 2 INCHES APPROX TOTAL 2 SQ INCHES. REMOVED CORROSION IAW SRM 51-74-10, CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-00 PAGE 106. REPAIRED STR 45LT BETWEEN FR 60 AND FR 61 IAW A310 SRM 53-1
- [SDR FDEA201006302290](https://openairdocs.org/sdr/FDEA201006302290.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK HAS CORROSION 4 EA AREAS ON UPPER SURFACE BETWEEN FR 15 AND FR 16A AT 4L. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REPLACED SEAT TRACK 4L, BETWEEN FR 15 AND FR 16A IAW SRM 51-
- [SDR FDEA201006302285](https://openairdocs.org/sdr/FDEA201006302285.md): Floorbeam · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > AFT CARGO COMPT FLOORBEAM FR63, RBL 45, PRODUCTION SPLICE HAS CORROSION BETWEEN IT AND T-CHORD APPROX. 5" LONG (EXFOLIATION) REMOVED CORROSION ON AFT CARGO COMPT FLOORBEAM FR 63, RBL 45, IAW A310 SRM 51-74-10 PG 205. CHECKED LIMITS AND FOUND TO BE OUT OF LIM
- [SDR FDEA201006302283](https://openairdocs.org/sdr/FDEA201006302283.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 4L IS CORRODED AT 4 EA LOCATIONS FROM FR 33 TO FR 38.1 APPROX 6 SQ IN. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK 4L IAW SRM 53-10-16, FIG 208, PG 247/248.
- [SDR FDEA201006302280](https://openairdocs.org/sdr/FDEA201006302280.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 2R INBD SIDE CORRODED AT 4 EA LOCATIONS FROM APPROX 16 IN FWD OF FR33 TO 10 INCHES AFT OF FR 33 APPROX 5 SQ INCH TOTAL. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16 PAGE 103, FIG 101 FOUND TO BE OUT OF LIMITS. REPAIRED SEAT
- [SDR FDEA201006302279](https://openairdocs.org/sdr/FDEA201006302279.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 2L APPROX 18 IN FWD OF FR33 IS CORRODED APPROX 1 SQ IN REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16, FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK 2L BETWEEN FR 32 AND FR 33 IAW SRM 53-10-16 FIG 208.
- [SDR FDEA201006302278](https://openairdocs.org/sdr/FDEA201006302278.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 2R HAS 2EA. LOCATIONS CORRODED BETWEEN FR49 TO FR46. CORROSION IS ON THE OTBD UPPER AND LOWER SURFACE APPROX. 4SQ IN. REMOVED CORROSION IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16 FIG 101, FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM
- [SDR FDEA201006302268](https://openairdocs.org/sdr/FDEA201006302268.md): Skin · damaged · Jun 30, 2010 · N402FE · Airbus A310203 · Trailing Edge Flaps
  > LT WING INBD FLAP LWR T/E SURFACE HAS IMPACT DAMAGE MEASURING 6 IN. X 6 IN. X.32 IN. D REPAIRED IMPACT DAMAGE ON LT WING INBD FLAP LWR T/E SURFACE USING COR REPLACMENT WITH EXTERNAL BONDED METAL DOUBLER IAW SRM 57-53-12, PARA 12, A,B,C FIG 208.
- [SDR FDEA201006302267](https://openairdocs.org/sdr/FDEA201006302267.md): Seat Track · corroded · Jun 30, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR1 HAS 2EA LOCATIONS THAT ARE CORRODED FR 33 TO APPROX 18 IN FWD OF FR 33 REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND TRACK SECTION OUT OF LIMITS IAW SRM 53-10-16. FABRICATED AND INSTALLED SEAT TRACK REPAIR IAW SRM 53-10-16, FIG 205
- [SDR FDEA201006292225](https://openairdocs.org/sdr/FDEA201006292225.md): Floor Support · corroded · Jun 29, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FLOORBOARD SUPPORT STRUCTURE THAT TURNS INTO THE 5L SEAT TRACK IS CORRODED, FR 14 TO FR 15 APPROX 72 IN LONG. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL, FOUND FLOOR SUPPORT AND SUPPORT FITTING OUT OF LIMITS IAW SRM 53-10-16. R & R FLOOR SUPPORT AND
- [SDR FDEA201006242141](https://openairdocs.org/sdr/FDEA201006242141.md): Seat Track · corroded · Jun 24, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK 3R, AT FR 54.2 HAS 1 SQ INCH OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10, CHECKED SEAT TRACK 3R AT FR 54.2 FOUND OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R AT FR 54.2 IAW SRM 51-72-00.
- [SDR FDEA201006242140](https://openairdocs.org/sdr/FDEA201006242140.md): Seat Track · corroded · Jun 24, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK 4R BETWEEN FRAMES 18 & 19 HAS 5 SQ. INCH OF CORROSION. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, CHECKED FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 53-12-16, PB 201.
- [SDR FDEA201006192080](https://openairdocs.org/sdr/FDEA201006192080.md): Skin · dented · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > RAMP REPORTED 3 SMALL DENTS 10 IN AFT OF AFT LOWER CARGO COMPT DOOR. REF WRITE UP WRI 53-30 1790. CUT OUT DAMAGE AREA IAW SRM 53-17-12, FIG 205, NDT VERIFIED NO CRACKS IAW NTM 51-10-08. REPAIRED SKIN IAW SRM 53-17-12, FIG 205.
- [SDR FDEA201006192079](https://openairdocs.org/sdr/FDEA201006192079.md): Stringer · corroded · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT HAS CORROSION AT STRINGER 31 RT FROM FRAME 54.1 TO FRAME 54.1, 12 IN TOTAL AREA APPROX 13 SQ IN. REMOVE CORROSION IAW SRM 51-74-10, CHECK FOUND OUT OF LIMIT IAW WITH SRM 53-10-00, PG 106. REPAIRED STRINGER 31RT IAW SRM 53-10-14.
- [SDR FDEA201006192078](https://openairdocs.org/sdr/FDEA201006192078.md): Seat Track · corroded · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FR 54 SEAT TRACK 3R CORROSION ON A FLANGE UPPER SURFACE. REMOVED CORROSION IAW SRM 51-74-10 CHECK LIMIT FOUND OUT OF LIMIT IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 51-40-21.
- [SDR FDEA201006192077](https://openairdocs.org/sdr/FDEA201006192077.md): Floorbeam · corroded · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage Main, Floor Beam
  > AFT CARGO COMPT FRAME 58 LT SIDE FLOOR SUPPORT BEAM, LBL 44 UNDER SIDE HAD EXFOLIATION CORROSION APROX 4SQ IN IN TOTAL. REMOVED CORROSION IAW SRM 51-74-10 CHECK AREA FOUND TO BE OUT OF LIMIT IAW SRM 53-10-15. REPAIRED FLOOR SUPPORT BEAM IAW SRM 53-10-15.
- [SDR FDEA201006192076](https://openairdocs.org/sdr/FDEA201006192076.md): Floor Support · corroded · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPT FLOOR STRUCTURE LONGITUDINAL SUPPORT BETWEEN FRAME 65-66, LBL 5. UPPER AND LOWER SURFACES HAVE CORROSION IN AND AROUND FASTENER HOLES, APPROX 10 SQ IN IN TOTAL. REMOVED CORROSION FROM PROFILE IAW SRM 51-74-10 CHECK LIMIT IAW SRM 53-10-00, P
- [SDR FDEA201006192072](https://openairdocs.org/sdr/FDEA201006192072.md): Stringer · corroded · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FUSELAGE SKIN STRINGER HAS 1" X 1" CORROSION FWD OF AFT PRESSURE BULK HEAD 10" FWD OF FR 80/82 STR 56R REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, FIG 201. CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-14 PAGE 203/204, FIG 201. REPAIRED STR 56R IAW SRM 53-10-14
- [SDR FDEA201006192071](https://openairdocs.org/sdr/FDEA201006192071.md): Stringer · corroded · Jun 19, 2010 · N402FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > FUSELAGE SKIN STRINGER HAS 1" X 1" CORROSION FWD OF AFT PRESSURE BULKHEAD 10" FWD OF FR 80/82 STR 56L. REMOVED CORROSION IAW SRM 51-74-10, PAGE 205, FIG 201, CHECKED FOUND OUT OF LIMITS IAW SRM 53-10-14 PAGE 203/204, FIG 201. REPAIRED STRINGER 56L IAW SRM 53-

Next page: https://openairdocs.org/deregistered/N402FE-2016-01-25/reports.md?page=2

## 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 = 'N402FE' AND deregistration_id = 'N402FE-2016-01-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N402FE-2016-01-25/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.