Airbus A310-203

Service difficulty reports · 2,392

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 aircraft_model_key = 'A310203'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201107222904Floor Panel · contaminatedFLOOR PANEL 147BF IS OIL SOAKED. FABRICATED REPLACEMENT PANEL 147BF IAW DWG SRZ-25-005, REV J.Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107222902Floor Panel · damagedAVIONICS COMPT FLOOR PANEL 121JF HAS 1 EA CORNER BROKEN AND 1 EA CORNER PLIES WORN THRU. FABRICATED REPLACEMENT FLOOR PANEL 121JF IAW DWG SRZ-25-005, REV J.Jul 22, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107212888Spar · corrodedLEFT HORIZONTAL STAB UPPER REAR SPAR TOP FLANGE BOTTOM SIDE CORRODED AT 4EA NUTPLATE HOLES LOCATED 6 TO 18 INCHES OTBD OF FUSELAGE BETWEEN RIBS 3 AND 5 MEASURED 8 SQ INCHES. REMOVED CORROSION IAW A SRM 51-74-10, FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 COJul 21, 2011 · N435FE · Airbus A310203 · Horizontal Stabilizer, Spar/RibSDR FDEA201107202831Skin · corrodedLT WING OUTER OVERWING REFUEL ADAPTOR REMOVED, FOUND CORROSION AT TOP SKIN SHROUND (FROM 5 TO 11 O'CLOCK POSITION ). ACCOMPLISHED EA 6-5720-149013. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. CLEANED UP IAW AMM 28-11-00.Jul 20, 2011 · N428FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201107202832Skin · chafedLT WING OUTER OVERWING REFUEL ADAPTOR REMOVED. FOUND CORROSION AT TOP SKIN SHROUND (FROM 5 TO 11 O'CLOCK POSITION ). ACCOMPLISHED EA 6-5730-149017. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 20, 2011 · N428FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201107192817Floorbeam · crackedFWD CARGO MAIN DECK FLOORBEAM AT FRAME 34 CRACKED AT STIFFENER, BETWEEN SEAT TRACKS 2 & 3 RT SIDE. CUTOUT DAMAGE AT FLOORBEAM IN FWD CARGO COMPARTMENT SUPPORT FR 34 RT SIDE IAW SRM 53-10-15. NDT IAW NTM 51-10-08 SHOW NO CRACK INDICATION AFTER CUTOUT OF DAMAGJul 19, 2011 · N435FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192816Skin · crackedAPU EXHAUST DOOR 317AL RT LOWER LATCH CUTOUT SKIN HAS A .10 INCH CRACK. ROUTED OUT CRACK, NDT FOUND NO CRACKS, REPROTECTED AREA IAW SRM 52-41-18, PAGE 203 AND SRM 51-75-10. FABRICATED DOUBLER, DRILLED AND INSTALLED IAW SRM 52-41-18, FIG 201, PAGES 207-208.Jul 19, 2011 · N435FE · Airbus A310203 · Auxiliary Power Unit (APU) DoorsSDR FDEA201107192798Clevis · bentMDCC AT FS 54.1 BETWEEN SEAT TRACKS 2 & 3 RT CLEVIS ADAPTER FWD FLANGE IS BENT IN 2 EA PLACES. R & R ADAPTER AT FR 54.1 MDCC BETWEEN TRACKS 2 & 3 ON RT SIDE IAW SRM 51-72-10 PARA 5A & 6A . LOCATED, DRILLED & DEBURRED NEW ADAPTER IAW SRM 51-40-44, PG 1-16.Jul 19, 2011 · N435FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107192797Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 58, RBL 67 FOUND WITH A 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203 SHT 1 & 2. REPAIR PROFILE FABRICATED AND INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1 & 2. ACCOMPLISHED EA 6-5310-143632. Jul 19, 2011 · N436FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192796Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 34, RBL 27 FOUND WITH A 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203, SHT 1. REPAIR PROFILE FABRICATED AND INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1.Jul 19, 2011 · N436FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192795Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 37, RBL 27 FOUND WITH 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR CLASSIFIED ASJul 19, 2011 · N436FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192794Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 37, RBL 67 FOUND WITH 0.28 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15 REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SRM 53-10-15, REV 18, FIG 203 SHEET 1. REPAIR CLASSIFIED AS MJul 19, 2011 · N436FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192793Clevis · crackedMDCC AT FS 54.1 AT SEAT TRACK 3RT CLEVIS ADAPTER MOUNT FITTING CRACK APPROX 2" LONG. R & R CLEVIS IN MDCC AT FR 54.1 ON RT NR 3 TRACK IAW SRM 51-72-10 PARA 5A & 6A. LOCATED, DRILLED & DEBURRED NEW CLEVIS IAW SRM 51-40-44, PG 16.Jul 19, 2011 · N435FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192792Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 37, RBL 27 FOUND WITH 0.25 INCH CRACK. TRIMMED OUT IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR Jul 19, 2011 · N436FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107192791Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 36, RBL 27 FOUND WITH 0.25 INCH CRACK. TRIMMED OUT IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR Jul 19, 2011 · N436FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201107182783Floor Panel · crackedFLOOR PANEL 147 AF HAS A 1" INCH CRACK AND IS OIL SOAKED. FABRICATED REPLACEMENT FLOOR PANEL 147 AF USING DWG SRZ 25-005, REV J.Jul 18, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107182782Floor Panel · damagedFLOOR PANEL 241 MK HAS 2EA AREAS CRUSHED TOTAL 32 SQ" INCHES, IN ZONE 240. FABBED REPLACEMENT FLOOR PANEL 241 MK USING DWG SRZ 25-005, REV J.Jul 18, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107182778Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 60 - 62, X= -55 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 18, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162734Skin · misrepairedREPAIR FOUND AT LT WING T/E FLAP LOWER SURFACE OTBD AREA RIB 9 & RIB 10. FOUND PREVIOUSLY NOT REPAIRED IAW ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED IAW SRM 57-52-12 REV 79, FIGURE 205. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201107162763Support · crackedFWD CARGO COMPARTMENT CENTER CARGO CONTAINER GUIDE AT FR36 BETWEEN 1L AND 1R LOADING TRACK SUPPORT STRUCTURE HAS CRACK THAT MEASURE .5"(L) .03"(W) . R & R CRACKED LOADING SUPPORT TRACK PLATE IAW SRM 51-40-21, PARAGRAPH 5, PG 7. R & R YZ LATCHES IAW CMM 2Jul 16, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107162760Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 35 - 36, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162759Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT AT FRAME 62 - 65, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162757Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT AT FRAME 60 - 62, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162756Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT FRAME 55/58 - 60, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162754Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT AT FRAME 54.2 - 55/58, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162753Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT AT FRAME 54 - 54.2, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162750Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT AT FRAME 46 - 51, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162749Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL LT AT FRAME 43 - 46, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162747Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL AT LT FRAME 40/41-43, X= 67 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162745Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 37 - 38.2, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162744Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 38.2 - 40/41, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162743Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 40/41 - 43, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162742Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 43 - 46, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162741Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 46 - 51, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162740Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 51 - 54, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162739Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 54 - 55, X= -35, FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162738Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 54 -55, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162737Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL RT AT FRAME 58 - 60, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. AND INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162736Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL AT FRAME 61, X= -35 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 30.0. FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED IAW AMM 53-10-25, REV 30.0. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 16, 2011 · N436FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107162735Skin · dentedRT AFT PAX DOOR EXTERIOR SURFACE AFT LOWER EDGE FOUND WITH DENT. REPAIR CARRIED OUT IAW EA 6-5210-14361.Jul 16, 2011 · N436FE · Airbus A310203 · Passenger/Crew DoorsSDR FDEA201107152715Support · damagedFORWARD CARGO COMPARTMENT RT SIDE AT FR 21 & FR 22 CARGO DOOR INTERNAL STRUCTURE PANEL SUPPORT HAS 2EA DAMAGE NUTPLATE HOLES. REMOVED AND REPLACED INTERNAL STRUCTURAL PANEL ON UPPER FORWARD CARGO DOOR FRAME CUTOUT AREA BETWEEN FR 21 AND FR 22 IAW SRM 51-72-1Jul 15, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107152721Support Angle · chafedFORWARD CARGO COMPARTMENT LT SIDE BETWEEN NR2 AND NR3 LOADING TRACKS AT FR 25 HAS A SUPPORT ANGLE WITH CHATTER MARKS DAMAGE. R & R FILLER IN FWD CARGO PIT ON LT SIDE, BETWEEN TRACKS 2 & 3 AT FR 25 IAW SRM 51-40-21, PARA 6 & 51-72-10 PARA 5A & 6A. FABRICATED Jul 15, 2011 · N435FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201107142690Fitting · cracked1EA CRACK (.2500", .1250") WAS FOUND AT NLG DOOR ACTUATOR UPPER ATTACHMENT RT FITTING. REMOVED NLG DOOR ACTUATOR R/H UPPER FITTING. MATCHED DRILL HOLES FROM OLD FITTING TO NEW FITTING IAW EO 6-5340-7-5001 A5. IAW EO 6-5340-7-5001 A5 PT2, REPLACEMENT OF NLG Jul 14, 2011 · N428FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201107142696Floor Panel · crackedFLOOR PANEL 252UH HAS 1 EA, 14 IN. CRACK. FABRICATED NEW PANEL 252UH IAW DWG SRZ 25-5-005, REV J.Jul 14, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107142695Floor Panel · crackedFLOOR PANEL 242LK IS CRACKED IN HALF. FABRICATED NEW PANEL 242LK IAW DWG SRZ 25-5-005, REV J.Jul 14, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107142713Floor Panel · damagedFLOOR PANEL 242ZJ HAS 7 EA CRUSHED AREAS. FABRICATED REPLACEMENT PANEL 242ZJ IAW DWG SR2 25-005 REV J.Jul 14, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107142701Floor Panel · crackedFLOOR PANEL 242AJ HAS A CRACK ACROSS PANEL. FABRICATED REPLACEMENT PANEL 242AJ IAW DWG SR2 25-005 REV J.Jul 14, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107142689Rib · crackedLT WING NR 6 SPOILER INBD HINGE SUPPORT RIB GOT CRACKED AT LWR CORNER . REPAIRED IAW SRM 57-51-11 FIT.203. CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 14, 2011 · N428FE · Airbus A310203 · Wing, Rib/BulkheadSDR FDEA201107142711Floor Panel · damagedFLOOR PANEL 242UJ HAS 3 EA AREAS CRUSHED, 42 SQ INCHES TOTAL. FABRICATED REPLACEMENT PANEL 242 UJ, REFERENCE DWG SRZ 25-005 REV J.Jul 14, 2011 · N435FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201107142712Floor Panel · crackedFLOOR PANEL 241WH HAS 1 EA, 10 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL 241WH, IAW DWG SRZ 25-005, REV J.Jul 14, 2011 · N435FE · Airbus A310203 · Fuselage Floor Panel
Back to Airbus A310-203