# Service difficulty reports: N430FE A list on [N430FE](https://openairdocs.org/aircraft/N430FE.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 · 110 reports - [SDR FDEA201502240588](https://openairdocs.org/sdr/FDEA201502240588.md): Valve · unknown · Feb 24, 2015 · N430FE · Airbus A310203 · Standard Practices/Structures > IAW MOCC REQUEST NEED TO R & R DEPRESSURIZATION VLV 93 HM. PART ON ORDER. R & R DEPRESSURIZATION VLV 93 HM IAW 21-31-15-04-01. - [SDR FDEA201304150784](https://openairdocs.org/sdr/FDEA201304150784.md): Skin · cracked · Apr 15, 2013 · N430FE · Airbus A310203 · Fuselage Main, Plate/Skin > NDT INSPECTION OF LT FRAME 54, SKIN JOINT BETWEEN S36 AND 37L, SHOWS SIX HOLES WITH POSITIVE CRACK INDICATIONS. INDICATIONS ARE AT MULTIPLE CLOCK POSITIONS. POSITIVE HOLES ARE 1, 5, 6, 8, 11 AND 13. REF ALI 53-15-90. COMPLIED WITH EA 6-5315-T0300240, REV. - [SDR FDEA201304020712](https://openairdocs.org/sdr/FDEA201304020712.md): Shear Tie · damaged · Apr 2, 2013 · N430FE · Airbus A310203 · Fuselage Internal Mounting Structure > WHILE ACCOMPLISHING WC E6-5310-7-5020 A PT2, FOUND FR 43 SHEAR TIE HAS SHORT E.D. REMOVED AND REPLACED IAW SRM 51-72-10 AND DWG 57112116 - [SDR FDEA201303170590](https://openairdocs.org/sdr/FDEA201303170590.md): Seat Track · damaged · Mar 17, 2013 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > DUMMY TRACK 4L FR 54 / 54.2 FAILED GAP CHECK. REMOVED, REPAIRED AND INSTALLED DUMMY TRACK IAW SRM 53-15-16, FIG 203. - [SDR FDEA201303150574](https://openairdocs.org/sdr/FDEA201303150574.md): Seat Track · loose · Mar 15, 2013 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > DUMMMY TRACK 3R FR 38.2 /40 FAILS GAP CHECK. REMOVED DUMMY TRACK AT FR 38.2 /40 IAW SRM 51-40-21, PAR 5 & PAR 7. REPAIRED DUMMY TRACK IAW SRM 53-15-16 PG 209 -216, REINSTALLED TRACK AT FR 38.2 /40 IAW SRM 51-40-21, PAR 5-7. REPROTECTED AREA IAW SRM 51-75-10 - [SDR FDEA201303140568](https://openairdocs.org/sdr/FDEA201303140568.md): Seat Track · worn · Mar 14, 2013 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > DUMMY TRACK 2R FR 54 TO 54.2 FAILS GAP CHECK. REMOVED DUMMY TRACK 2R FR 54/54.2 IAW SRM 53-15-16. REPAIRED DUMMY TRACK 2R FR 54/54.2 IAW SRM 53-15-16. INSTALLED REPAIRED DUMMY TRACK 2R FR 54/54.2 IAW SRM 51-40-21 AND SRM 53-15-16. - [SDR FDEA201303130567](https://openairdocs.org/sdr/FDEA201303130567.md): Floorbeam · corroded · Mar 13, 2013 · N430FE · Airbus A310203 · Fuselage Main, Floor Beam > UPON REMOVAL OF SEAT TRACK SECTION, FOUND CORROSION ON FLOORBEAM UPPER TEE TOP SURFACE AT FR 16A, Y1959 (5L)(APPROX 1 SQ IN TOTAL) - [SDR FDEA201303120556](https://openairdocs.org/sdr/FDEA201303120556.md): Seat Track · corroded · Mar 12, 2013 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK 5L AT FR 18 HAS CORROSION ON TOP SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED IAW DWG. A53610798, AND REPLACED SEAT TRACK IAW SRM 51-40-21 PARA. 6 AND 13. - [SDR FDEA201303110547](https://openairdocs.org/sdr/FDEA201303110547.md): Floor Panel · damaged · Mar 11, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 252GF CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J. - [SDR FDEA201303110548](https://openairdocs.org/sdr/FDEA201303110548.md): Floor Panel · damaged · Mar 11, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 252MF CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J. REMOVED AND INSTALLED FLOOR PANEL IAW AMM 53-10-25-04 - [SDR FDEA201303090534](https://openairdocs.org/sdr/FDEA201303090534.md): Angle · cracked · Mar 9, 2013 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > UPON INSP/NDT OF HOLES H1 AND H2 AT ARCH FITTING AT FR43 LT SHOWS INDICATION OF CRACK ON BRACKET SIDE. REMOVED AND REPLACED ANGLE IAW SRM 51-72-10. - [SDR FDEA201303090533](https://openairdocs.org/sdr/FDEA201303090533.md): Attach Angle · cracked · Mar 9, 2013 · N430FE · Airbus A310203 · Fuselage Main, Attach Fittings > FOUND UPPER ATTACH ANGLE TO BE VISIBLY CRACKED. R & R FR 43 UPPER FWD ATTACH ANGLE AT ARCH FITTING IAW SRM 51-72-10. - [SDR FDEA201303090530](https://openairdocs.org/sdr/FDEA201303090530.md): Floor Panel · damaged · Mar 9, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > PANEL 232XH CRUSHED AT CLS. FABRICATED REPLACEMENT PANEL232XH IAW DWG SRZ-25-005, REV Z. - [SDR FDEA201303080526](https://openairdocs.org/sdr/FDEA201303080526.md): Floor Panel · cracked · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 252 UF HAS 10 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J. - [SDR FDEA201303080522](https://openairdocs.org/sdr/FDEA201303080522.md): Floor Panel · cracked · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 251GF HAS 12 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-10-25-04. - [SDR FDEA201303080518](https://openairdocs.org/sdr/FDEA201303080518.md): Floor Panel · damaged · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 252SF CRUSHED AT CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J. - [SDR FDEA201303080517](https://openairdocs.org/sdr/FDEA201303080517.md): Floor Panel · damaged · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 252BF CRUSHED AT CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J. - [SDR FDEA201303080527](https://openairdocs.org/sdr/FDEA201303080527.md): Floorboard · damaged · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOORBOARD 242UJ CRUSHED AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J. - [SDR FDEA201303080525](https://openairdocs.org/sdr/FDEA201303080525.md): Floorboard · delaminated · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOORBOARD 232LT IS CRUSHED AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J. - [SDR FDEA201303080524](https://openairdocs.org/sdr/FDEA201303080524.md): Floorboard · damaged · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOORBOARD 232SF IS CRUSHED AT CLS CUTOUT. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J. - [SDR FDEA201303080523](https://openairdocs.org/sdr/FDEA201303080523.md): Floor Panel · damaged · Mar 8, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 242QJ CRUSHED AT CLS CUTOUT. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J. - [SDR FDEA201303070506](https://openairdocs.org/sdr/FDEA201303070506.md): Floor Panel · crushed · Mar 7, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 242ZJ CRUSHED AT CUTOUT. FABRICATED REPLACEMENT PANEL IAW DWG SRZ-25-005, REV J. - [SDR FDEA201303070505](https://openairdocs.org/sdr/FDEA201303070505.md): Floor Panel · crushed · Mar 7, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 242EK CRUSHED AT CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J. - [SDR FDEA201303070507](https://openairdocs.org/sdr/FDEA201303070507.md): Floor Panel · damaged · Mar 7, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 241NK IS BROKEN IN HALF AT CLS CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005 REV. J. - [SDR FDEA201303060500](https://openairdocs.org/sdr/FDEA201303060500.md): Floor Panel · damaged · Mar 6, 2013 · N430FE · Airbus A310203 · Fuselage Floor Panel > FLOOR PANEL 147AF EDGE SEALANT SOFTENED & MISSING BY A PERIMETER LENGTH OF 50". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J. - [SDR FDEA201203311201](https://openairdocs.org/sdr/FDEA201203311201.md): Pressure Switch · failed · Mar 31, 2012 · N430FE · Airbus A310203 · Engine Fuel Indicating System > NR 2 ENGINE FUEL FILTER CLOG ECAM/ MASTER CAUTION IMMEDIATELY AFTER TAKE OFF. ECAM CAUTION EXTINGUISHED AROUND 80 PERCENT N1 WHEN THROTTLES RETARDED. REMOVED AND INSPECTED NR 2 ENGINE FUEL FILTER. NO DEBRIS FOUND. INSTALLED NEW FILTER IAW MM 73-12-03-02. - [SDR FDEA201103010805](https://openairdocs.org/sdr/FDEA201103010805.md): Frame · cracked · Mar 1, 2011 · N430FE · Airbus A310203 · Fuselage Main, Structure > AVIONICS COMPARTMENT FORWARD DOOR INT SIDE, AFT FRAME IS CRACKED IN 2 PLACES AT LIGHTENING HOLES. CRACKED DOOR FRAME WAS REMOVED PER SRM 51-40-21, PARA 6. NEW FRAME WAS FABRICATED PER DWG A52110744, ISSUE "F". FRAME WAS ALODINED PER SRM 51-21-10, PAGE 2. P - [SDR FDEA201102240727](https://openairdocs.org/sdr/FDEA201102240727.md): Transition Panel · corroded · Feb 24, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT TRANSITION PANEL 131 WF HAS MULTIPLE AREAS OF CORROSION ON THE FRONT. TRANSITION PANEL WAS CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10. PANEL WAS REMOVED AND FABRICATED IAW DWG A53272783 AND SRM 51-71-40. PARTS WERE ALODINED - [SDR FDEA201102240726](https://openairdocs.org/sdr/FDEA201102240726.md): Transition Panel · corroded · Feb 24, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT TRANSITION PANEL 132 WF HAS MULTIPLE AREAS OF CORROSION, FRONT AND BACK. TRANSITION PANEL WAS CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10. PANEL WAS REMOVED AND FABRICATED IAW DWG A53272783 AND SRM 51-71-40. PARTS WERE ALODI - [SDR FDEA201102230701](https://openairdocs.org/sdr/FDEA201102230701.md): Skin · dented · Feb 23, 2011 · N430FE · Airbus A310203 · Trailing Edge Flaps > LT WING INBD FLAP SKIN IS DENTED. BLENDED AREA NOTED; FOUND 100 PERCENT MATERIAL THICKNESS GONE IAW SRM 57-52-12, FIG 107. REMOVED DAMAGED SKIN AND REPAIRED IAW SRM 57-52-10, FIG 204 & PARA 4-D. ALODINED BARE SURFACES, SEALED DOUBLER & PRIMED IAW SRM 57-5 - [SDR FDEA201102230697](https://openairdocs.org/sdr/FDEA201102230697.md): Arm · worn · Feb 23, 2011 · N430FE · Airbus A310203 · Elevator Structure > RT ELEVATOR AT 2 HINGE ARM LOWER FWD BEARING SWAGE LOOSE IN ARM - INBD TO OTBD MOVEMENT AS SEEN FROM THE TOP OF STAB. REMOVED RT ELEVATOR NR 2 HINGE ARM; R & R 2 EA FWD BEARINGS AND REINSTALLED RT NR 2 ELEVATOR HINGE ARM; FUNCTIONAL CHECK GOOD OF NR 2 ELEVA - [SDR FDEA201102230696](https://openairdocs.org/sdr/FDEA201102230696.md): Structure · damaged · Feb 23, 2011 · N430FE · Airbus A310203 · Wing Main, Frame Structure > LT WING T/E THROUGH HOLES FOR HYD LINES ARE ELONGATED AT WS OWS 1083. - [SDR FDEA201102210646](https://openairdocs.org/sdr/FDEA201102210646.md): Web · cracked · Feb 21, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS CRACKED BETWEEN FRAME 37 & FRAME 38; LBL 56. REMOVED AND REINSTALLED PALLET LATCH AT FRAME 37, RBL 33 IAW AMM 25-52-34- 04, PARA 2B1 & 2E2. REMOVED AND REINSTALLED PDU TRAY AT FRAME 37 TO 38 RT IAW SRM 51-4 - [SDR FDEA201102210645](https://openairdocs.org/sdr/FDEA201102210645.md): Web · cracked · Feb 21, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT UNDER FLOOR VERTIVAL WEB IS CRACKED BETWEEN FRAME 36 & FRAME 37; LBL 56. UPPER AND LOWER WEBS WERE REMOVED IAW SRM 51-40-21, PARA 6. NEW WEBS LOCATED AND DRILLED IAW SRM 51-40-44, PAGE 1. BOTH WEBS INSTALLED IAW SRM 51-40-21, PARA 7. - [SDR FDEA201102180603](https://openairdocs.org/sdr/FDEA201102180603.md): Floor Panel · delaminated · Feb 18, 2011 · N430FE · Airbus A310203 · Fuselage Floor Panel > TAIL COMPARTMENT WORK PLATFORM IS SPONGY AND HAS EXPOSED CORE - DIRECTLY INBD OF ACCESS DOOR 312 AR CUTOUT. REPAIRED TAIL COMPARTMENT WORK PLATFORM WITH THE FABRICATION OF A NEW FLOOR PANEL USING THE OLD FLOOR PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "H - [SDR FDEA201102180606](https://openairdocs.org/sdr/FDEA201102180606.md): Angle · damaged · Feb 18, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > AFT PIT SHEAR PLATE TOP "L" ANGLE HAS PREVIOUSLY DOUBLE DRILLED HOLES BETWEEN FRAME 64 AND FRAME 65; STRINGER 44L. REMOVED ANGLE IAW SRM 51-40-21, PARA 6. FABBED NEW ANGLE IAW DWG A53974252, ISSUE "G". ALODINED IAW SRM 51-21-10, PG 1. PRIMED IAW SRM 51- - [SDR FDEA201102180605](https://openairdocs.org/sdr/FDEA201102180605.md): Angle · damaged · Feb 18, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > AFT PIT SHEAR PLATE TOP "L" ANGLE HAS PREVIOUS DOUBLE DRILLED HOLES BETWEEN FRAME 65 AND FRAME 66; STRINGER 44LT. REMOVED ANGLE IAW SRM 51-40-21, PARA 6. FABRICATED NEW ANGLE IAW DWG A53974254, ISSUE "D". ALODINED IAW SRM 51-21-10, PG 1. PRIMED IAW SRM 5 - [SDR FDEA201102180604](https://openairdocs.org/sdr/FDEA201102180604.md): Web · dented · Feb 18, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS DENTED BETWEEN FRAME 34 - FRAME 35; LBL 56. REMOVED WEB IAW SRM 51-40-21, PARA 6. DISPLACED, CAPPED AND STOWED WIRING THROUGH WEB IAW AMM 20-33-22. LOCATED & DRILLED NEW WEB IAW SRM 51-40-44, PG 1. INSTAL - [SDR FDEA201102170592](https://openairdocs.org/sdr/FDEA201102170592.md): Seat Track · corroded · Feb 17, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN SEAT TRACK BETWEEN FRAME 72 AND 73 LBL 34 IS CORRODED. REMOVED CORROSION IAW SRM 53-10-16. CHECKED LIMITS, ORIGINAL THICKNESS 0.140. MATERIAL LOSS 0.041. MATERIAL REMAINING 0.099. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION, MATERIAL - [SDR FDEA201102160571](https://openairdocs.org/sdr/FDEA201102160571.md): Spar · cracked · Feb 16, 2011 · N430FE · Airbus A310203 · Nacelle/Pylon, Frame/Spar/Rib > NR 2 PYLON HORIZ HEAT SHIELD BELOW THE LOWER SPAR IS CRACKED AND MISSING PIECES. WELD REPAIRED IAW EA 6-5750-136739. - [SDR FDEA201102160570](https://openairdocs.org/sdr/FDEA201102160570.md): Spar · cracked · Feb 16, 2011 · N430FE · Airbus A310203 · Nacelle/Pylon, Frame/Spar/Rib > LT PYLON HORIZ HEAT SHIELD BELOW THE LOWER SPAR IS CRACKED AND MISSING PIECES. WELD REPAIRED IAW EA 6-5750-136739. - [SDR FDEA201102160572](https://openairdocs.org/sdr/FDEA201102160572.md): Seat Track · corroded · Feb 16, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 AND FRAME 76; LBL 30. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS, ORIGINAL THICKNESS 0.0140. MATERIAL REMOVED 0.058. MATERIAL REMAINING 0.082. FOUND TO BE OUT OF LIMITS IAW SRM 51-31-20 & SRM 53-10 - [SDR FDEA201102140565](https://openairdocs.org/sdr/FDEA201102140565.md): Floorboard · corroded · Feb 14, 2011 · N430FE · Airbus A310203 · Fuselage Floor Panel > BULK CARGO COMPARTMENT FLOORBOARD 162 HF METAL TOP IS CORRODED. REMOVED TOP SHEET IAW DWG SRZ 25-011, REV "C". TOP SHEET MATERIAL ID 2024-T3 IAW DWG SRZ 25-011, REV "C". FABRICATED TOP SHEET IAW DWG SRZ 25-011, REV "C". BONDED TOP SHEET TO FLOORBOARD IAW - [SDR FDEA201102140556](https://openairdocs.org/sdr/FDEA201102140556.md): Seat Track · corroded · Feb 14, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 & FRAME 76; LBL 43. REPAIRED MAIN DECK SEAT TRACK BETWEEN FRAME 74 TO FRAME 76 WITH 35 INCHES OF SEAT TRACK SECTION AND SPLICE IAW SRM 53-10-16, FIG 208, SHEET 1, LBL 43. - [SDR FDEA201102090511](https://openairdocs.org/sdr/FDEA201102090511.md): Skin · corroded · Feb 9, 2011 · N430FE · Airbus A310203 · Cargo/Baggage Doors > FWD CARGO DOOR INNER SKIN IS CORRODED UNDER THE LOWER SEAL RETAINER. REMOVED AND REPLACED SECTION OF SKIN IAW A310-200 SRM 51-40-21, PARA 6, 7 & 13. - [SDR FDEA201102090512](https://openairdocs.org/sdr/FDEA201102090512.md): Skin · corroded · Feb 9, 2011 · N430FE · Airbus A310203 · Fuselage Main, Plate/Skin > FUSELAGE INTERGAL PLATE HAS CORROSION AT FRAME 38.2; STRINGER 52R. REMOVED CORROSION PER SRM 51-74-10. FOUND TO BE OUT OF LIMITS PER SRM 53-14-12, FIG 101. FABRICATED REPAIR PARTS PER SRM 53-14-12, REPAIRS 4 & 5. ALODINED PER SRM 51-21-10. PRIMED PER SRM - [SDR FDEA201102080499](https://openairdocs.org/sdr/FDEA201102080499.md): Floor Panel · cracked · Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 241 YN IN ZONE 240 IS CRACKED. FABRICATED NEW FLOOR PANEL 241 YN IAW DWG SRZ 25-005, REV "H". - [SDR FDEA201102080498](https://openairdocs.org/sdr/FDEA201102080498.md): Floor Panel · cracked · Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 231 R IN ZONE 230 IS CRACKED. FABRICATED NEW FLOOR PANEL 231 RG IAW DWG SRZ 25-005, REV "H". - [SDR FDEA201102080497](https://openairdocs.org/sdr/FDEA201102080497.md): Floor Panel · cracked · Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 241 NK IS CRACKED; ZONE 240. FABRICATED NEW FLOOR PANEL 241 NK IAW DWG SRZ 25-005, REV "H". - [SDR FDEA201102080496](https://openairdocs.org/sdr/FDEA201102080496.md): Floorboard · damaged · Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor Panel > MAIN CABIN FLOORBOARD HAS A BROKEN OFF OTBD FWD CORNER FROM FRAME 25-FRAME 27; RBL 78 TO RBL 100. FABRICATED NEW FLOORBOARD 231 VG IAW DWG SRZ 25-005, REV "H". Next page: https://openairdocs.org/aircraft/N430FE/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 = 'N430FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N430FE/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.