N411FE, cancelled Apr 23, 2020

Service difficulty reports · 62

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

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 n_number = 'N411FE' AND deregistration_id = 'N411FE-2020-04-23'
  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 FDEA201111225002Duct · leakingDURING CLIMB ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. REMOVED AND REPLACED NR 1 SYS ANTI-ICE DUCT IN PYLON PER AMM 20-26-00-000. PERFORMED LEAK CHECK WITH APU AIR, FOUND NO LEAKS AT DUCT. ACFT OK FOR SERVICENov 22, 2011 · N411FE · Airbus A310203 · Air Intake Anti/De-Ice SystemSDR FDEA201111225003Warning Light · illuminatedDURING CLIMB, ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK, COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. OPENNov 22, 2011 · N411FE · Airbus A310203 · Pneumatic Distribution SystemSDR FDEA201108243464Bellcrank · failedDURING LANDING GEAR FREE FALL EXTENTION TEST PROCEDURES, THE LT AND RT MLG FAILED TO EXTEND AFTER HANDLE REACHED MAXIMUM ALLOWABLE TURNS OF 20.5. REMOVED AND REINSTALLED FLOOR PANELS FOR ACCESS IAW AMM 53-23-04. R & R FREE FALL CONTROL BELL CRANK IAW SRM 51-Aug 24, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR FDEA201108243463Skin · corrodedCENTER WING BOX LT FR 49 HAS OXIDATION AT UPPER SURFACE BETWEEN STR 27-28. BELOW SEAT TRACK 6L DEFECT MEASURES 8 SQ INCHED IN THE CORNER. CLEANED UPPER SURFACE OF CWT BOX FR 49 STR 27-28 AT ST 6L IAW SRM 51-74-10. R & R FASTENER IAW SRM 51-40-21. REMOVED AAug 24, 2011 · N411FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108243458Attach Fitting · corrodedCTR WING BOX BETWEEN SEAT TRACK L5-L6 HYD LINES ATTACHMENT FITTING CORRODED FR 49-50. CLEANED 6 EA LINES AND FITTING FOUND TO BE OUT OF LIMIT IAW AMM 12-21-12-02 R & R 6EA FITTING IAW 51-40-10 PRESSURE AND LEAK CK SATISFACTORY IAW AMM29 10-00-04.Aug 24, 2011 · N411FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201108153281Fitting · failedNLG LEG DOOR LOWER RT ATTACHMENT FORK BROKEN. R & R NLG LEG DOOR RT FITTING AND ATTACHMENT FORK ,OPS CHECKED GOOD ALL IAW 32-22-15-04.Aug 15, 2011 · N411FE · Airbus A310203 · Landing Gear Door Retract SectionSDR FDEA201108133264Floor Panel · delaminatedFLOOR PANEL 242UJ HAS IMPACT DAMAGE. CUTOUT DAMAGE, & FABRICATED REPLACEMENT FLOOR PANEL 242UJ IAW DWG SRZ 25-005, REV J.Aug 13, 2011 · N411FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201108123247Adapter · failedCLEVIS ADAPTOR AT FRAME 43 BETWEEN SEAT TRACKS 2R AND 3R BROKEN. REMOVED AND REPLACED CLEVIS ADAPTOR AT FRAME 43 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 51-40-21 & 51-72-10.Aug 12, 2011 · N411FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201107273001Spring · bentLT MLG 2 DOWNLOCK SPRINGS BENT. REPLACED BENT SPRINGS LT MAIN GEAR LOCK LINK IAW AMM 32-11-19-04.Jul 27, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR FDEA201107273000Spring · bentRT MLG DOWNLOCK SPRINGS (2 EA) BENT. REPLACED BENT SPRINGS FOR RT MLG LOCK LINK IAW AMM 32-11-19-04.Jul 27, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR FDEA201011034246Switch · failedON DEPARTURE RECEIVED LANDING GEAR RETRACTION FAULT. DOWN AND LOCKED "GREEN" LIGHTS NEVER WENT OUT. FOUND ACFT IN SYS 2 ON ARRIVAL. TALKED TO CAPTAIN OF INBD FLIGHT. TRIED SYS NR1 AS WELL AS SYS NR 2. NO RETRACTION OF LANDING GEAR. ACFT IAW MM 07-11-00-00Nov 3, 2010 · N411FE · Airbus A310203 · Landing Gear Position and WarningSDR FDEA201009303801Fitting · corroded134AR ACCESS DOOR SURROUNDING INTEGRAL FITTING FOUND CORROSION (FR23- 24, STGR49R-STGR54L) REMOVE CORROSION IAW SRM 51-74-10. MEASURE THE REMAINING THICKNESS IAW NTM51-10-04 AND NTM51-10-08 CHECK FOR CRACK. MAKE THE REPAIR PARTS IAW SRM53-13-12-201 REPAIRSep 30, 2010 · N411FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201009293798Fitting · corroded136 AR ACCESS DOOR SURROUNDING INTEGRAL FITTING FOUND CORROSION (FR38.1- FR38.2, STGR49R-STGR54L) REMOVE CORROSION IAW SRM51-74-10. MEASURE THE REMAINING THICKNESS IAW NTM51-10-04 AND NTM51-10-08 CHECK FOR CRACK. MAKE THE REPAIR PARTS IAW SRM53-14-12-201 RESep 29, 2010 · N411FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201009273730Beam · crackedLT AFT CREW DOOR FRAME FR73A TO FR75A, STRINGER 11 LONGITUDINAL BEAM NDT FOUND CRACK INDICATION FROM 5 FASTENER HOLES. REMOVE THE COVER PLATE AND DOOR FRAME BEAM IAW SRM51-40-21. DRILL FASTENER HOLES ON THE NEW PART IAW SRM51-40-40. INSTALL THE NEW PART ANDSep 27, 2010 · N411FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201009273729Frame · damaged2 DISTORTIONS FOUND ON FR54.2 FRAME BETWEEN STGR13L-15L 1.CUT OUT THE DAMAGED SECTION OF FRAME 54.1 BETWEEN STGR13L-15L AND MAKE THE REPAIR PART IAW SRM53-10-13-201, PARA6 AND EA6-5310-141632. INSTALL THE REPAIR PART IAW SRM 53-10-13-201, PARA6 AND EA 6-5310-Sep 27, 2010 · N411FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201009273728Frame · gougedGOUGE FOUND ON FR54.1 FRAME BETWEEN STGR13L-14L 1.CUT OUT THE DAMAGED SECTION OF FRAME 54.1 BETWEEN STGR13L-15L AND MAKE THE REPAIR PART IAW SRM53-10-13-201, PARA6 AND EA6-5310-141632. INSTALL THE REPAIR PART IAW SRM53-10-13-201 PARA6 AND EA6-5310-141632.Sep 27, 2010 · N411FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA200811144882Housing · brokenON ARRIVAL INTO MEM, THE NOSE GEAR INDICATED UNSAFE ON BOTH SYSTEM 1 AND 2. COMPLIED WITH QRH AND USED THE MLG GRAVITY EXTEND CHECKLIST. WHEN THAT WAS COMPLETED THE UNSAFE WARNING REMAINED. THEN WENT DOWNSTAIRS TO VISUALLY CHECK. IT INDICATED DOWN AND LOCKNov 14, 2008 · N411FE · Airbus A310203 · Landing Gear Position and WarningSDR 08FDEA04882Housing · crackedON ARRIVAL, NOSE GEAR INDICATED UNSAFE ON BOTH SYSTEM 1 AND 2. COMPLIED WITH QRH AND USED MLG GRAVITY EXTEND CHECKLIST. WHEN COMPLETED UNSAFE WARNING REMAINED, VISUALLY CHECKED. INDICATED DOWN AND LOCKED. LANDED WITH INDICATION. FOUND SWITCH 40 GB HOUSING BNov 14, 2008 · N411FE · Airbus A310203 · Landing Gear Position and WarningSDR 07FDEA03423Transmitter · malfunctionedDURING CRUISE, GREEN HYDRAULICS SHOWED "0" PRESSURE AND "LO RSVR QUANTITY" ON ECAM. QUANTITY CONFIRMED ON OVERHEAD PANEL. DIVERTED TO ATL. DURING MANUAL GEAR EXTENSION, QUANTITY RETURNED TO GREEN BAND (BELOW TOP HAT). INSTALLED ALL THREE GEAR PINS IN AIRCRSep 5, 2007 · N411FE · Airbus A310203 · Hydraulic Quantity SensorSDR 07FDEA03392Transmitter · leakingDURING CRUISE, GREEN HYDRAULICS SHOWED "0" PRESSURE AND "LO RSVR QUANTITY" ON ECAM. QUANTITY CONFIRMED ON OVERHEAD PANEL. DURING MANUAL GEAR EXTENSION, QUANTITY RETURNED TO GREEN BAND (BELOW TOP HAT). FOUND HYD PRESSURE TRANSMITTER IN LT WHEEL WELL LEAKING.Sep 5, 2007 · N411FE · Airbus A310203 · Hydraulic Quantity SensorSDR 07FDEA01653Skin · misrepairedPREVIOUS REPAIR LOCATED ON R/SIDE FUSELAGE SKIN BETWEEN FR 66 TO 67 BETWEEN STR 35TO 38 RT HAS AN EXTERNAL REPAIR DOUBLER MEASURING 8.8 BY 11.9. REPAIR REVIEWED AND FOUND NOT TO BE IAW A310-200 SRM 53-10-12 FIG 226 SHEET 2. REWORKED REPAIR IAW A310-200 SRM 5Apr 27, 2007 · N411FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA01655Skin · misrepairedPREVIOUS REPAIR LOCATED ON L-SIDE FUSELAGE SKIN BETWEEN FR 21-22 BETWEEN STR 34-36 LT AT LAP SEAM HAS AN EXTERNAL DOUBLER MEASURING 6.25 BY 9 IN REPAIR DETERMINED NOT TO BE IAW A310-200 SRM 53-10-12 FIG 205, REPAIR REWORKED IAW A310-200 SRM EA 6-5330-110187.Apr 27, 2007 · N411FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA01241Floorbeam · cracked1 CRACK EXIST IN FLOORBEAM VERTICAL STIFFENER AT FR 36 BETWEEN SEAT TRACK L4 AND L5, MEASURING 0.450" P/N 537B1041000 A310-200 AMM 53-10-15-6. REMOVED 1 CRACK IN FLOORBEAM VERTICAL STIFFENER AT FRAME 36 BETWEEN SEAT TRACK L4 AND L5 IAW A310-200 SRM 53-10-15 FApr 2, 2007 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA01185Floorbeam · cracked1 CRACK EXIST IN FLOORBEAM VERTICAL STIFFENER AT FRAME 36 BETWEEN SEAT TRACK L2 AND L3 MEASURING .5" REF R537B1041000 A310-200 AMM 53-10-15-6. REMOVED CRACK PER A310 SRM SUPP 53-10-15 FIG 201. NDT C/W PER NTM 51-10-08, NO CRACK INDICATIONS NOTED. FABBED REMar 29, 2007 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA01184Floorbeam · cracked1 CRACK FOUND .75" IN UPPER SUPPORT LEG ON AFT SIDE OF FLOORBEAM FR 58 BETWEEN SEAT TRACK 4L AND 5L EXTENDING INTO FLOORBEAM WEBBING UNDER CLS ADAPTER IAW A310-200 AMM 53-16-11-6. REMOVED DAMAGED AREA AND REPAIRED IAW AB DWG R53270150 AND EA 6-5310-107708.Mar 29, 2007 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA01080Floorbeam · crackedFORWARD CARGO COMPARTMENT, FLOORBEAM (C25) FORWARD FACE OF BEAM LOCATED BETWEEN R2 AND R3 SEAT TRACK HAS A .400 INCH CRACK IN VERTICAL STIFFENER. REPAIRED FLOORBEAM IAW A310/200 SRM SUPPLEMENT 53-10-15. REMOVED AND REINSTALLED FLOORBOARD IAW A310/200 AMM SUPMar 22, 2007 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA01078Floorbeam · crackedFWD CARGO COMPARTMENT, OVER HEAD FLOORBEAM [ C34 ] FWD FACE OF BEAM , LOCATED BETWEEN L4 AND L5 SEAT TRACK HAS A 0.425 INCH CRACK IN VERTICAL STIFFENER. REMOVED AND REINSTALLED FLOOR BOARD 231KF AND 231QF TO FOM REPAIR IAW A310-200 AMM 53-10-25-4. REPAIRED FMar 22, 2007 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA01076Track · misrepairedPREVIOUS REPAIR LOCATED ON AFT CARGO ROLLER TRACK LEFT NR 2 HAS A 9 INCH LONG REPAIR SECTION WITH 2 REPAIR ANGLES ON THE OUTBD SIDE MEASURING 7 INCH LONG EACH BETWEEN FRAMES 54.3 TO55/58 PREVIOUSLY INSTALLED REPAIR WAS DETERMINED NOT TO BE IAW A310 SRM 53-1Mar 22, 2007 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 06FDEA04243Control Unit · malfunctionedON CLIMB-OUT, AUTO BRAKE FAIL LIGHT CAME ON, LIGHT STAYED ON UNTIL LEVEL OFF AND THEN AFTER A PERIOD OF TIME THE LIGHT WENT OUT. LIGHT THEN CAME ON AFTER A PERIOD OF TIME. CYCLE REPEATED ITSELF OFF AND ON SEVERAL TIMES. PERFORMED BITE TEST ON BSCU FAULT CODDec 14, 2006 · N411FE · Airbus A310203 · Landing Gear Brake SystemSDR 06FDEA2663Pitot Tube · dirtyRIGHT AFTER ROTATION BOTH ATS LEVERS DROPPED OFF. ADC FAILED ON CAPT SIDE SWITCHED OVER TO OTHER SYSTEM REENGAGED ATS LEVERS AS PER ECAM THROTTLE RETARDED TO IDLE AS SOON AS ATHR BUTTON PUSHED. NO ECAM FOR ADC. ALSO NR 1 FLT DIRECTOR FAILED. CAPTS ALTIMETEJul 23, 2006 · N411FE · Airbus A310 · Pitot/Static SystemSDR 06FDEA2659Adc · failedJUST AFTER ROTATION BOTH ATS LEVERS DROPPED OFFLINE AND WOULD NOT RESET. YAW DAMP DROPPED OFF, WOULD NOT RESET. CAPTS PFD, ADC FAILED. SWITCHED OVER TO F/O SYSTEM. HAD NUMEROUS AIRSPEED WINDSHEAR VMO MMO WARNINGS EVEN THOUGH USING STBY SYSTEMS. AT THAT POJul 22, 2006 · N411FE · Airbus A310 · Air Data ComputerSDR 06FDEA1782Computer · faultedON T/O AT LAX, DID A RTO AT 90 KTS THE ECAM ALERT WAS BOTH PITCH 1/2 AND BOTH RUDDERS 1/2 FAULTED. REMOVED AND REPLACED NR 1 AND NR 2 FEEL LIMITATION COMPUTERS PER M/M 27-23-26-4. OPS CK'S NORMAL. PERFORMED AFTER BRAKE OVERHEAT INSP REF MM 05-51-16-0-01. May 11, 2006 · N411FE · Airbus A310203 · Rudder Control SystemSDR 05FDEA04399Indicator · smokeN CRUISE BURNING SMELL IN COCKPIT, DIVERTED AND LANDED. STRONGEST SMELL FROM THROTTLE QUADRANT AREA, FIRE CREW TEMP DETECTOR SHOWED HIGHEST HEAT IN THAT LOCATION. NEVER ANY VISIBLE SPARKS OR FLAMES, SOME SMOKE. INSPECTED THROTTLE QUADRANT AREA AND FOUND THE Dec 22, 2005 · N411FE · Airbus A310203 · Rudder Tab Control SystemSDR 05FDEA01899Access Panel · damagedACCESS PANEL 650GB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.Jul 12, 2005 · N411FE · Airbus A310 · Wing, Plate/SkinSDR 05FDEA01898Access Panel · damagedACCESS PANEL 650 FB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.Jul 12, 2005 · N411FE · Airbus A310 · Wing, Plate/SkinSDR 04FDEA02798Angle · corrodedBULK CARGO COMPT FLOOR STRUCTURE FS 67 2EA AREAS OF CORROSION NOTED ON TOP AND BOTTOM SURFACES. REMOVED AND REPLACED PROFILE ANGLE IAW A310 SRM 51-40-21.Sep 21, 2004 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02797Floorbeam · corrodedBULK CARGO COMPT FLOOR STRUCTURE FS 65 ON LT SIDE, MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACES. REMOVED AND REPLACED BEAM IAW A310 SRM 53-10-15.Sep 21, 2004 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 04FDEA02796Seat Track · corrodedMDCC SEAT TRACK L4 FRAME 74-80 HAS 5EA CORRODED AREAS. REPAIRED SEAT TRACK BY SPLICING IAW A310 SRM 51-22-00, 51-40-21 AND 53-10-16.Sep 21, 2004 · N411FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02795Floorbeam · corrodedAFT CARGO COMPT FS 63 FLOOR STRUCTURE, ON LEFT SIDE 3EA AREAS OF CORROSION ON TOP SURFACE AND UNDERNEATH FLOOR STRUCTURE. REMOVED AND REPLACED FLOOR STRUCTURE BEAM IAW A310 SRM 51-40-21.Sep 21, 2004 · N411FE · Airbus A310 · Fuselage Main, Floor BeamSDR 04FDEA02794Structure · corrodedAFT CARGO COMPT FWD OF FS 54.2 BILGE AREA NOTED SPOT OF CORROSION AROUND THE HOLE PLUG. REPAIRED BILGE AREA IAW EA 6-5330-55370.Sep 21, 2004 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02793Seat Track · corrodedMDCC SEAT TRACK R1 BETWEEN FRAME 73-80 HAS 7EA DISCREPANT AREAS 5EA AREAS THAT ARE CORRODED AND GOUGED AND 2EA AREAS THAT ARE GOUGED. REMOVED AND REPLACED R1 SEAT TRACK FRAME 73-80 IAW A310 SRM 51-40-21 AND SRM 53-10-16.Sep 21, 2004 · N411FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02724Seat Track · crackedMDCC SEAT TRACK SECTION AT R2, BETWEEN FR54 TO 8 INCHES AFT OF FR54.1 HAS DAMAGE TO THE SCALLOP LUGS. (ON EDGES AND BENEATH LUGS) REMOVED DAMAGE AND FOUND TO BE CRACKED IAW SRM 51-73-10. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21.Sep 17, 2004 · N411FE · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02698Floorbeam · crackedFWD CARGO FLOORBEAM STRUCTURE FR33 NOTED INDICATION OF CRACK. REMOVED DAMAGED AREA IAW A310 SRM 53-10-15, AND REPAIRED BY INSTALLING A DOUBLER IAW A310 SRM 53-10-15.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 04FDEA02697Adapter · crackedTRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02696Adapter · crackedTRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA02695Seat Track · gougedSEAT TRACK AT FR 36 AFT APPROX 8 INCHES IS GOUGED. BLENDED AREA PER A310 SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS PER A310 SRM 53-10-16. REPAIRED BY REMOVING DAMAGED SECTION OF TRACK AND SPLICING IN A REPAIR SECTION PER A310 SRM 51-40-21 AND 53-10-16.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02694Seat Track · corrodedSEAT TRACK 0, SECTION BETWEEN FR73 TO FR80 HAS TWO DISCREPANT AREAS. TRACK 0 AT APPROX 12 INCHES AFT FROM FR 77 HAS 2 GOUGES INSIDE OF SCALLOPED AREA. TRACK 0 APPROX 10 INCHES AFT OF FR78 HAS CORROSION ON TOP OF TRACK AND IN SCALLOPED AREA. REMOVED CORROSIOSep 16, 2004 · N411FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02693Floorbeam · crackedBULK CARGO COMPT FLOOR STRUCTURE ON FR67 AT RT SIDE CORNER UNDERNEATH NOTED CRACK. REMOVED AND REPLACED BEAM IAW A310 SRM 51-40-21.Sep 16, 2004 · N411FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 04FDEA02692Floor Support · corrodedBULK CARGO COMPT. FLOOR STRUCTURE FR66 LT SIDE , MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW SRM 51-74-10, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D CSep 16, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous StructureSDR 04FDEA02691Floor Support · corrodedBULK CARGO COMPT. FLOOR STRUCTURE, ON RT SIDE FR 66 TO FR 63 CORROSION ON TOP AND BENEATH SURFACE. REMOVED CORROSION IAW SRM 51-70-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING ****Sep 16, 2004 · N411FE · Airbus A310 · Fuselage Miscellaneous Structure
Back to N411FE, cancelled Apr 23, 2020