# Service difficulty reports: N405FE, cancelled Jan 25, 2016

A list on [N405FE, cancelled Jan 25, 2016](https://openairdocs.org/deregistered/N405FE-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 3 · 117 reports

- [SDR FDEA201104051323](https://openairdocs.org/sdr/FDEA201104051323.md): Fuel Filter · contaminated · Apr 5, 2011 · N405FE · Airbus A310203 · Engine Fuel Distribution
  > DURING GO-AROUND WITH APPROX 4.5 THOUSAND POUNDS OF FUEL IN EACH OUTER TANK, NR 1 ENG FUEL CLOG LIGHT ILLUMINATED. IT EXTINGUISHED, THEN RE-ILLUMINATED IN LEVEL FLIGHT, THEN EXTINGUISHED. NO ENGINE SECONDARIES. CREW REPORTED NO NOTICED FLUCTUATION OF NR 1
- [SDR FDEA201008253130](https://openairdocs.org/sdr/FDEA201008253130.md): Relay · malfunctioned · Aug 25, 2010 · N405FE · Airbus A310203 · Landing Gear Position and Warning
  > AT APPROX 400' AGL WHILE FLYING RNAV/GPS APP RWY 29. RECEIVED "TO LOW GEAR" CALL OUT. EXECUTED GO AROUND. SELECTED SYS NR 2 ON GEAR AND LANDED WITHOUT OTHER WARNINGS. PER TSM INSPECTED NLG MSW 79GB, NO DEFECTS NOTED. CLEANED AND RESEATED C/P ON
- [SDR FDEA201004301403](https://openairdocs.org/sdr/FDEA201004301403.md): Angle · corroded · Apr 30, 2010 · N405FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT BETWEEN FR 38.2 AND FR 39 AND BETWEEN STRINGER 46L AND STRINGER 45L HAS A 2 SQ INCH OF CORROSION. REMOVED ALL EVIDENCE OF CORROSION IN FWD CARGO COMPT BETWEEN FR 38.2 AND FR 39 AND BETWEEN STR 45L AND STR 46L IAW SRM 51-74-10. REPAIRED
- [SDR FDEA201004261364](https://openairdocs.org/sdr/FDEA201004261364.md): Fitting · corroded · Apr 26, 2010 · N405FE · Airbus A310203 · Passenger/Crew Doors
  > R 1 DOOR EXTERIOR SIDE HAS CORROSION ON INSIDE HANDLE AREA BOX, 3 IN X 3 IN REMOVED LEVEL 1 CORROSION. REMOVED CORRODED FITTING ON R 1 DOOR HANDLE EXTERIOR BOX, FABRICATED REPLACEMENT PART IAW DRW A52111407201 AND INSTALLED PART IAW SRM 51-72-10.
- [SDR FDEA201004261363](https://openairdocs.org/sdr/FDEA201004261363.md): Frame · chafed · Apr 26, 2010 · N405FE · Airbus A310203 · Fuselage Main, Frame
  > MAIN CARGO COMPT FRAME 36 AT LT LONGERON NR 10 HAS CHAFED AREA.015 IN DEP CUT OUT DAMAGE SECTION AT FRAME 36, LONGERON 10 LT IN MAIN UPPER DECK COMPT, FABRICATED REPAIR PARTS AND INSTALLED FRAME REPAIR-INNER FLANGE IAW SRM 53-10-13, FIG 202, PAGE 209.
- [SDR FDEA201004241350](https://openairdocs.org/sdr/FDEA201004241350.md): Seat Track · corroded · Apr 24, 2010 · N405FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPT SEAT TRACK NR 5 RT BETWEEN FR 15 AND FR 19 HAS CORROSION, APPROX 56 SQ IN, REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK AND REPLACED WITH NEW TRACK AT TRACK NR5 RT BETWEEN FR 15 AND FR 19 IAW SRM 51-72-10, PAGE 2.
- [SDR FDEA201004241349](https://openairdocs.org/sdr/FDEA201004241349.md): Skin · dented · Apr 24, 2010 · N405FE · Airbus A310203 · Cargo/Baggage Doors
  > BULK CARGO DOOR EXT SKIN AT LOWER FWD END HAS DENT 2.5 IN LONG X.20 IN WIDE X.004 IN DEEP CUT OUT DAMAGED SECTION OF EXT SKIN, FABRICATED REPAIR PARTS AND INSTALLED CORNER MEMBER TO SKIN REPAIR ON BULK CARGO DOOR FWD LOWER CORNER IAW SRM 52-30-00, FIG 207,
- [SDR FDEA201004241348](https://openairdocs.org/sdr/FDEA201004241348.md): Seat Track · cracked · Apr 24, 2010 · N405FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT SEAT TRACK NR3 RT BETWEEN FRAMES 45 AND 54 HAS 4 EA CRACKS ON UPPER SURFACE AREA, MAX LENGTH.50 IN. REMOVED DAMAGED TRACK AND REPLACED WITH NEW SEAT TRACK NR3 RT IN MAIN DECK BETWEEN FR 45 AND FR 54 IAW A310 SRM 51-72-10 PG 2.
- [SDR FDEA201004231346](https://openairdocs.org/sdr/FDEA201004231346.md): Floorbeam · cracked · Apr 23, 2010 · N405FE · Airbus A310203 · Fuselage Main, Floor Beam
  > AFT CARGO PIT MDC FLOORBEAM FR 54.3 BETWEEN SEAT TRACK 2R-3R, CRACK LENGTH IS 0.125 IN ROUTED OUT CRACK FABRICATED, TREATED AND PRIMED AND INSTALLED REPAIR CHANNEL AT AFT CARGO PIT MDC FLOORBEAM FR 54.3 BETWEEN SEAT TRACK 2R-3R IAW SRM 53-10-15, PG 257-258, F
- [SDR FDEA201004201255](https://openairdocs.org/sdr/FDEA201004201255.md): Plate · corroded · Apr 20, 2010 · N405FE · Airbus A310203 · Emergency Exits
  > LT OVERWING EMERGENCY EXIT DOOR, EXTERIOR HANDLE BOX AREA, ON AFT SIDE HAS 2 SQUARE INCHES OF CORROSION. REMOVED CORROSION FROM SEAL PLATE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 52-20-00 FIG.101 (100 PERCENT MATERIAL LOSS). REMOVED INNER SKIN SE
- [SDR FDEA201004191254](https://openairdocs.org/sdr/FDEA201004191254.md): Seat Track · corroded · Apr 19, 2010 · N405FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR NR 1 SEAT TRACK HAS 12 " LONG HEAVY CORROSION BETWEEN FR15A AND 16A. REMOVED CORROSION IAW SRM 51-74-10, TRACKS FOUND OUT OF LIMITS IAW SRM 53-10-10, FIG. 101. REPLACED TRACKS IAW SRM 51-72-10, SRM 51-40-44 PARA. 3A & SRM 53-12-16, FIG 1.
- [SDR FDEA201004161209](https://openairdocs.org/sdr/FDEA201004161209.md): Floor Support · corroded · Apr 16, 2010 · N405FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO COMPT FLOOR SUPPORT BEAM HAS CORROSION APPROX 1.5 X 1.0 INCH BETWEEN FLOORBEAM 17L & 16L NEAR L1 DOOR. R & R FLOOR SUPPORT FRAME IAW SRM 51-72-10, AND FABBED NEW T-CAP FROM 7075T6511-NSA348070 IAW DWG 12-A53611789. INSTALLED NEW TRACK IAW SRM
- [SDR FDEA201004161203](https://openairdocs.org/sdr/FDEA201004161203.md): Seat Track · corroded · Apr 16, 2010 · N405FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO SEAT TRACK CORROSION ON Y1959 BETWEEN FR 15B AND FR 15, REFER TO NON- ROUTINE N01238 DATED 03/28/10. AFTER CORROSION REMOVAL, THE SEAT TRACK PN Y1959 BETWEEN FR 15 AND FR 15B WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-16-10. REMOVED SEAT TRACK
- [SDR FDEA201004141179](https://openairdocs.org/sdr/FDEA201004141179.md): Seat Track · corroded · Apr 14, 2010 · N405FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT, SEAT TRACK 5L BETWEEN FR 78 AND FR 79 HAS A 1 SQ INCH AREA OF CORROSION. REMOVED CORROSION FROM SEAT TRACK 5L BETWEEN FR 78 & FR 79, CHECKED FOUND OUT OF LIMIT. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 207.
- [SDR FDEA200908072945](https://openairdocs.org/sdr/FDEA200908072945.md): Gearbox · leaking · Aug 7, 2009 · N405FE · Airbus A310 · Leading Edge Slat Control System
  > SLAT SYS 1 & 2 FAULT DURING ACFT CONFIGURATION REMOVED AND REPLACED LEFT WING SLAT NR 2 LINE GEARBOX PER AMM 27-84-16. REMOVED AND REPLACED RT WING SLAT IN LINE GEARBOX PER AMM 27-84-16. REMOVED AND REPLA CED RIGHT WING PPU PER AMM 27-81-14. OPEN
- [SDR FDEA200907252758](https://openairdocs.org/sdr/FDEA200907252758.md): Computer · failed · Jul 25, 2009 · N405FE · Airbus A310203 · Trailing Edge Flap Control System
  > FLAPS SYS 1 AND SYS 2 LIGHT CAME ON WHEN SELECTING FLAPS 20 ON APPROACH. FLAPS STUCK HALFWAY BETWEEN 15 AND 20. EXECUTED MISSED APPROACH, CYCLED FLAPS SUCCESSFULLY AND EXECUTED NORMAL SLAT/FLAPS 30/40 APPROACH. REMOVED AND REPLACED NR1 AND NR2 SFCC IN REF TO
- [SDR 07FDEA03393](https://openairdocs.org/sdr/07FDEA03393.md): Support · corroded · Sep 6, 2007 · N405FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FWD PIT LT SIDE PANEL SUPPORT HAS CORROSION ON LOWER SURFACE AT FR 36 LBL 50 REMOVED NUTPLATES AND CORROSION IAW FEDEX A310 SRM 51-40-21 AND 51-74-10. FOUND TO BE OUT OF LIMITS IAW FEDEX A310 SRM 53-10-00. REMOVED AND REINSTALLED LT SLANT PANELS CARGO GUIDE
- [SDR 07FDEA03302](https://openairdocs.org/sdr/07FDEA03302.md): Sill · failed · Sep 2, 2007 · N405FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FWD LOWER CARGO PIT ANGLE REPAIR AT FR 24 STRINGER 43R AT DOOR SILL JAMB. EVALUATED AND FOUND TO NOT MEET APPROVED FAA REQUIREMENTS. REMOVED AND REPLACED REPAIR ANGLE AT FR 24 STRINGER 43R IAW FEDEX EA NR 6-5310-112957 FUSELAGE FWD CARGO DOOR LOWER SILL INCOM
- [SDR 07FDEA03301](https://openairdocs.org/sdr/07FDEA03301.md): Stringer · corroded · Sep 2, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER 55L REQUIRES REPLACEMENT FROM FR 58 TO 63. STRINGER HAS HEAVY CORROSION REMOVED SHEAR TIES AT STATION 59, 60, 61. CUT OUT STRINGER 55L FROM FRAME 58 TO 63 IAW A310 SRM FIG 20. FABBED STRINGER AND COUPLINGS IAW A310 SRM 53-10-14 FIG 201. AL
- [SDR 07FDEA03291](https://openairdocs.org/sdr/07FDEA03291.md): Frame · cracked · Aug 31, 2007 · N405FE · Airbus A310203 · Fuselage Main, Frame
  > FRAME 38 CRACKED WHERE FRAME LEG ATTACHES TO FUSELAGE SKIN, BETWEEN STR 41L AND STR 42L. TRIMMED CRACKED FLANGE, FABRICATED AND INSTALLED REPAIR FALSE FLANGE IAW EA 6-5310-109195, FUSELAGE FRAME, FRAME 38 BETWEEN STRINGER 41 AND 42 CRACKED FLANGE, REPAIR.
- [SDR 07FDEA03220](https://openairdocs.org/sdr/07FDEA03220.md): Structure · corroded · Aug 29, 2007 · N405FE · Airbus A310203 · Fuselage Main, Structure
  > AFT PIT BETWEEN FRAMES 66 AND 65 T CAP NUT PLATE JUST FWD OF FRAME 66 ABOVE STRINGER 45R CORRODED UNDERNEATH. REMOVED T-CAP IAW A310 SRM 51-40-21, RECEIVED NEW PROFILE P/N A5397426020451 PO J80248.1. INSTALLED NEW PROFILE IAW A310 SRM 51-40-21 PARA 7 AND PAR
- [SDR 07FDEA03219](https://openairdocs.org/sdr/07FDEA03219.md): Stringer · corroded · Aug 29, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER 55L BETWEEN FRAMES 54.2 AND 54.3 CORRODED LEFT SIDE COMPLIED WITH EA 6-5310-112955 FUSELAGE AFT PIT STRINGERS P52L, P54L, P55L REPAIR.
- [SDR 07FDEA03192](https://openairdocs.org/sdr/07FDEA03192.md): Skin · dented · Aug 28, 2007 · N405FE · Airbus A310324 · Fuselage Main, Plate/Skin
  > SKIN DIMPLED FRAME 38, LT SIDE STR 35L AROUND 3 FASTENERS. ACCOMPLISHED HFEC INSPECTION ON 3 EACH DENTS IAW A310 NTM 51-10-03 WITH NO DEFECTS NOTED. DRESSED OUT TWO DENTS AT STR 39 AND STR 40 IAW A310 SRM 51-73-10. BOTH DENTS FOUND TO BE WITHIN LIMITS IAW
- [SDR 07FDEA03132](https://openairdocs.org/sdr/07FDEA03132.md): Floorbeam · corroded · Aug 26, 2007 · N405FE · Airbus A310203 · Fuselage Main, Floor Beam
  > AFT PIT FRAME 58 T CAP LEFT SIDE ABOVE STRINGER 50L NUT PLATE CORRODED REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED CROSS BEAM AND SPLICE, FABBED CROSSBEAM T-CAP AND SPLICE ANGLES. TREATED REPAIR PARTS AND INSTALLED, IAW A31-200 SRM 51-74-10, 53-10-
- [SDR 07FDEA03105](https://openairdocs.org/sdr/07FDEA03105.md): Fitting · cracked · Aug 24, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FWD PIT, FRAME FITTING CRACKED, FR38 (X2082), BL 60L (Y1520), AT PIT FLOOR LEVEL.. REMOVED CRACKED FITTING IAW FEDEX A31 SRM 51-40-21 LOCATED DRILLED NEW FITTING PO 583026.6 IAW FEDEX SRM 51-40-44 PARA2. INSTALLED NEW FRAME FITTING IAW FEDEX SRM 51- 40-27
- [SDR 07FDEA03109](https://openairdocs.org/sdr/07FDEA03109.md): Stringer · corroded · Aug 24, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT, STR 54L CORRODED BETWEEN FR 58 AND FR61 (STA X3143 AND STA X3302) CUT OUT CORRODED SECTION OF STR 54L FROM STA X3143 TO STA X3302. FABRICATED AND SPLICED IN REPAIR SECTION IAW A310-200 SRM 53-10-14 FIG 201, 51-21-10 AND 51-23-10.
- [SDR 07FDEA03108](https://openairdocs.org/sdr/07FDEA03108.md): Stringer · corroded · Aug 24, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT, STR 45R CORRODED, FR 54.2 TO FR 54.3 (X3037 TO X3090) CUT OUT CORRODED SECTION OF STRINGER 45R, FROM STA X2984 TO X 3090, FABRICATED AND SPLICED IN REPAIR SECTION, IAW A310-200 SRM 53-10-14 FIG 201, 51-71-30 FIG 202, 51-40-21 PAR 6, 51-21-10 AN
- [SDR 07FDEA03103](https://openairdocs.org/sdr/07FDEA03103.md): Fitting · cracked · Aug 24, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FWD PIT, FRAME FITTING CRACKED, FR 36, (STA. X1976) BL 60L (Y1520). 09-04-07 REMOVED AND REPLACED FRAME FITTING IAW A310-200 SRM51-40-21, PART 6 & 7.
- [SDR 07FDEA03009](https://openairdocs.org/sdr/07FDEA03009.md): Skin · misrepaired · Aug 21, 2007 · N405FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > EXTERNAL REPAIR DOUBLER LT FUSELAGE FR26/32 STR39L-40L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA VISUALLY INSPECTED REPAIR DOUBLER LT FUSELAGE FR26/32 STR39L-40L. FOUND NOT TO BE WITHIN ANY FAA AP
- [SDR 07FDEA02996](https://openairdocs.org/sdr/07FDEA02996.md): Stringer · corroded · Aug 20, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT LOWER CARGO PIT STRINGER 52R HAS CORRODED ANGLE WITH MISSING FASTENERS BETWEEN FR 58 AND 59. [08-29-07] REMOVED STRINGER SECTION AND ANGLE IAW A310-200 51-40-21 PARA 6. FABRICATED NEW STRINGER 52R SECTION AND COUPLING IAW SRM 51-10-14 FIG 201. ALODIN
- [SDR 07FDEA02995](https://openairdocs.org/sdr/07FDEA02995.md): Stringer · corroded · Aug 20, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT LOWER CARGO PIT, CORROSION ON STRINGER 53L BETWEEN FR 64 AND 65. REMOVED, FABRICATED REPAIR SECTION OF STRINGER AND COUPLING AND INSTALLED PER A310-200 SRM 51-40-11, 53-17-14, 51-40-44, 51-40-21DAN 50-04, DAN320B14.
- [SDR 07FDEA02994](https://openairdocs.org/sdr/07FDEA02994.md): Skin · cracked · Aug 20, 2007 · N405FE · Airbus A310203 · Wing, Plate/Skin
  > LEFT WING BOTTOM SKIN PANEL NR 2, SKIN CRACKED I/B OF RIB 11, AFT OF REAR SPAR, WRI 57-10 9572, W/C T 6-5710-91017. STOP DRILLED CRACK, AND PERFORMED HFEC INSPECTION IAW A310 NTM 51-10-08 PT6, TO CONFIRM NO CRACK PAST STOP DRILLED AREA. INSTALLED SKIN DOUBLE
- [SDR 07FDEA02965](https://openairdocs.org/sdr/07FDEA02965.md): Stringer · corroded · Aug 17, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > ALC STR 52L CORRODED BETWEEN FR 64 AND 65. REMOVED CORROSION IAW A310 SRM 51-40-11. FOUNDED OUT OF LIMITS IAW A310 SRM 53-17-14. NEW MATERIAL ID FOR STRINGER IS DANS 0B09P0081641.218 COUPLING THAT IS DAN 200IT 79511 MAT EXTRUSION PO NR 580294.2. FABRICATED
- [SDR 07FDEA02964](https://openairdocs.org/sdr/07FDEA02964.md): Frame · corroded · Aug 17, 2007 · N405FE · Airbus A310203 · Fuselage Main, Frame
  > AFT PIT T CAP FRAME 60, CENTER, ABOVE S57 CORRODED. REMOVED CORROSION PER A310-200 SRM 51-74-10. FOUND TO BE OUT OF LIMITS PER A310-200 SRM 53-10-00 PG 123. REMOVED DAMAGED CROSSBEAM, FABBED NEW CROSSBEAM SECTION. INSTALLED NEW CROSSBEAM SECTION PER A310-2
- [SDR 07FDEA02953](https://openairdocs.org/sdr/07FDEA02953.md): Floorbeam · corroded · Aug 16, 2007 · N405FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD PIT CORRODED ON FLOORBEAM LATERAL ANGLE AT FR 38 UNDER ROLLER TRAY, RBL 28R TO 34R REMOVED CORRODED PART, FABBED REPAIR PARTS AND INSTALLED REPAIR ANGLE PER A310-200 SRM 51-74-10 PARA 6B, 53-14-15 FIG 41, 51-31-20 FIG 17, 53-10-15.
- [SDR 07FDEA02952](https://openairdocs.org/sdr/07FDEA02952.md): Stringer · corroded · Aug 16, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT PIT BETWEEN FRAME 66 AND 65 STRINGER 46L CORRODED REMOVED CORRRODED STRINGER. FABBED REPAIR PARTS. INSTALLED REPAIR PARTS PER A310-200 51-40-21, 53-10-14 PG 203, 51-21-10, 51-23-10.
- [SDR 07FDEA02887](https://openairdocs.org/sdr/07FDEA02887.md): Stringer · corroded · Aug 14, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > ALC STR 48R CORRODED BETWEEN FR 58 AND FR 60 REMOVED CORRODED AREA PER A310-200 SRM 51-40-21. FABBED REPAIR (STRINGER AND COUPLING) PER A310-200 SRM 53-10-14 PG 203, 51-21-10,51-23-10. INSTALLED REPAIR PARTS PER A310-200 SRM 53-10-14.
- [SDR 07FDEA02886](https://openairdocs.org/sdr/07FDEA02886.md): Stringer · corroded · Aug 14, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT PIT FRAME 63 STRINGER 48R CORRODED REMOVED CORRODED AREA FABBED REPAIR PARTS (STRINGER AND COUPLING) INSTALLED REPAIR PER A310-200 SRM 53-10-14, 51-21-10, 51-23-10, AND DRAWING A53974202.
- [SDR 07FDEA02861](https://openairdocs.org/sdr/07FDEA02861.md): Fitting · cracked · Aug 13, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME FITTING C38.2 CRACKED AND CORRODED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-40-21 PARA 6 PO NR 583026.5.
- [SDR 07FDEA02860](https://openairdocs.org/sdr/07FDEA02860.md): Stringer · corroded · Aug 13, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > ALC STR 49L CORRODED BETWEEN FR 58 AND FR 60 REPLACED STRINGER 49L BETWEEN FRAME 58 AND 60 IN AFT PIT IAW A310-200 SRM 53-10-14, FIG 201 PG 203/204.
- [SDR 07FDEA02859](https://openairdocs.org/sdr/07FDEA02859.md): Fitting · cracked · Aug 13, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME FITTING C38.1 IS CRACKED AND CORRODED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-40-21 PARA 5-7 PO NR 583026.8.
- [SDR 07FDEA02828](https://openairdocs.org/sdr/07FDEA02828.md): Floorbeam · corroded · Aug 11, 2007 · N405FE · Airbus A310203 · Fuselage Main, Floor Beam
  > ALC, FR 64, T-CAP CORRODED, BL 36R. (-Y910) REMOVED AND REPLACED T-CAP SECTION IAW A310-200 SRM 51-21-10 AND 53-10-15.
- [SDR 07FDEA02830](https://openairdocs.org/sdr/07FDEA02830.md): Frame · dented · Aug 11, 2007 · N405FE · Airbus A310203 · Fuselage Main, Frame
  > AFT PIT FRAME 67 BETWEEN STRINGER 49R AND 50R DENTED FORMED FRAME TO ORIGINAL CONTOUR REF: A310-200 SRM 51-73-10. PERFORMED HFEC, INSPECTION OF AREA IAW A310-200 NTM 51-10-08, NO CRACKS NOTED.
- [SDR 07FDEA02829](https://openairdocs.org/sdr/07FDEA02829.md): Stringer · corroded · Aug 11, 2007 · N405FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT PIT, STR 55R CORRODED FROM FR 61 TO FR 63 (STA X 3302 - X 3408). THIS SDR ALSO INCORPORATES DISCREPANCY AND REPAIR DONE ON NON ROUTINE NR N000443, W/O 00037436, (STR 55R CORRODED FROM FR61 - 62). REMOVED AND REPLACED CORRODED SECTION OF STR 55R FROM FR 6
- [SDR 07FDEA02791](https://openairdocs.org/sdr/07FDEA02791.md): Frame · cracked · Aug 7, 2007 · N405FE · Airbus A310203 · Fuselage Main, Frame
  > FRAME FITTING C35 IS CRACKED AT LBL 60 IN FWD PIT UNDER T-CAP REMOVED FITTING, FWD LOWER LT AT FR 35 REF A310 SRM 51-40-21 PARA 6. LOCATED AND DRILLED NEW FITTING REF A310 SRM 51-40-44 PARA 2. INSTALLED NEW FITTING REF A310 SRM 51-40-21 PARA 7.
- [SDR 07FDEA02702](https://openairdocs.org/sdr/07FDEA02702.md): Fitting · cracked · Aug 1, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME FITTING C38.1 CRACKED AT RBL 60, FWD PIT FLOOR. REMOVED AND REPLACED FRAME FITTING IAW A310-200 SRM 51-40-24 PAR 7.
- [SDR 07FDEA02689](https://openairdocs.org/sdr/07FDEA02689.md): Fitting · cracked · Jul 31, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME FITTING C35 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL. REMOVED AND REPLACED FRAME FITTING PER A310-200 SRM 51-40-21 PARAGRAPH 6.
- [SDR 07FDEA02688](https://openairdocs.org/sdr/07FDEA02688.md): Floorbeam · corroded · Jul 31, 2007 · N405FE · Airbus A310203 · Fuselage Main, Floor Beam
  > T-CAP CORRODED FR35 AT RBL 56 TO 62 FWD PIT REMOVED AND REPLACED T-CAP PER A310-200 SRM 51-40-21 PARAGRAGH 7 AND 53-10-15, PAGE 241 AND 242.
- [SDR 07FDEA02687](https://openairdocs.org/sdr/07FDEA02687.md): Floorbeam · corroded · Jul 31, 2007 · N405FE · Airbus A310203 · Fuselage Main, Floor Beam
  > T-CAP CORRODED FR35 AT RBL 56 TO 62 FWD PIT REMOVED AND REPLACED T-CAP PER A310-200 SRM 51-40-21 PARAGRAGH 7 AND 53-10-15, PAGE 241 AND 242.
- [SDR 07FDEA02686](https://openairdocs.org/sdr/07FDEA02686.md): Fitting · cracked · Jul 31, 2007 · N405FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME FITTING C37 IS CRACKED AT RBL 60 FWD PIT FLOOR LEVEL REMOVED AND REPLACED FITTING PER A310-200 SRM 51-40-21 PARAGRAGH 5 AND 6.

Next page: https://openairdocs.org/deregistered/N405FE-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 = 'N405FE' AND deregistration_id = 'N405FE-2016-01-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N405FE-2016-01-25/reports

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