N808FD, cancelled Mar 2, 2024

Service difficulty reports · 104

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 = 'N808FD' AND deregistration_id = 'N808FD-2024-03-02'
  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 FDEA201902120385Strut · inoperativeON APPROACH INITIAL GEAR EXTENSION DID NOT SHOW NOSE GEAR GREEN LOCKED INDICATION BUT RED UNLOCKED. RAN QRH AND ATTEMPTED MANUAL GEAR EXTENSION. ON FIRST ATTEMPT MANUAL DID NOT WORK. WENT INTO E&E COMPT. GREEN INDICATION NOT VISIBLE. SECOND ATTEMPT TO INSURE MFeb 12, 2019 · N808FD · Airbus A310324 · Nose/Tail Landing Gear Strut/AxleSDR FDEA2019020870269Sequence Valve · malfunctionedON APPR FOR 20 YEG, GEAR DOWN SELECTED, GOT AN UNSAFE GEAR INDICATION ON NOSE GEAR. FOLLOWED ECAM & QRH. EXTENDED GEAR W/GRAVITY PROCEDURE. TUG TO GATE. CARRIED OUT LUBE SERVICING INSTRUCTIONS ON NOSE GEAR ASSEMBLE AS PER AIRBUS AMM 12-22-32-00. NOSE GEARFeb 7, 2019 · N808FD · Airbus A310324 · Landing Gear Door Retract SectionSDR FDEA2018040853507Arm · failedAFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES,, SHOWED LOCKED ON SYSTEM 1 AND 2. REMOVED AND REPLACED NOSE GEAR TELESCOPIC DRAG STRUT ROCKER ARM ASSY. (40GB) ADJUSTED (49GB) IAW AMM 32-31-24-04Dec 15, 2018 · N808FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201812153507Warning System · malfunctionedAFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES, SHOWED LOCKED ON SYSTEM 1 AND 2.Dec 15, 2018 · N808FD · Airbus A310324 · Landing Gear Position and WarningSDR FDEA201710193010Slide · inoperativeL1 DOOR SLIDE IS INOPERATIVE.Oct 19, 2017 · N808FD · Airbus A310324 · Escape SlideSDR FDEA201707151956Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 60 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151951Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 16 HOLE, NDT INSPECTION FOUND CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151950Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 12 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151949Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 7 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151948Angle · crackedLEFT REAR SPAR INTERNAL ANGLE NR 61 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151947Spar · crackedLEFT WING REAR SPAR INTERNAL ANGLE NR 13 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151959Skin · crackedRIGHT WING RIB 11, CRACKED ON LOWER SKIN ACROSS A FASTENER HOLE APPROX 1.0 INCH IN LENGTH NEAR ACCESS PANEL 681AB. COMPLIED WITH EA 6-5730-T0334254 P1. MAJOR REPAIR IAW IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201707151958Skin · crackedLEFT WING RIB 11, CRACKED ON THE LOWER SKIN ACCROSS A FASTENER HOLE APPROX 1.5 INCH IN LENGTH, NEAR ACCESS PANEL 581AB. COMPLIED WITH EA 6-5730-T0334254, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201707151946Angle · crackedLEFT REAR SPAR INTERNAL ANGLE NR 53 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-5710-7Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151957Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. RIGHT REAR SPAR INTERNAL ANGLE 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. REAM THE AFFECTED HOLE THROUGH ALL LAYERS STEP BY STEP WITH INCREASING DIA OF 0.4 MM IAW SRM 51-40-44, PERJul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151955Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 38 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10-01, & NTM 51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, & 6-5710-7-3Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151954Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 35 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10-01, & NTM 51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, & EO 6-5710Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151953Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 33 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01, & NTM51-10-18 AND NO CRACK WAS FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151952Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 30 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-571Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151945Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 35 HOLE NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE AFFECTED HOLE THROUGH ALL LAYERS IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AFTER EACH STEP AND NO CRACK FOUND. WET INSTAJul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707111907Angle · crackedLEFT WING REAR SPAR INERNAL ANGLE 16 HOLE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 11, 2017 · N808FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201707051852Skin · corrodedFWD TOILET SERVICE PANEL LOWER CUTOUT SKIN DELAMINATED. INSPECTED FOUND SKIN INNER STIFFENER CORRODED AND OUT OF LIMITS IAW SRM 51-40-21, & SRM 53-12-18, FIG 2, SHEET 3, ITEM 205, REPLACEED THE STIFFENER. . MAJOR REPAIR IAW GMM 6-2-100.Jul 5, 2017 · N808FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201705011301Pump · inoperativeIN CRUISE FL360 GOT GREEN HYD SYSTEM OVERHEAT. ECAM ADVISED TO TURN OFF GREEN ENGINE PUMPS 1 AND 2. ENG HYD 1 PUMP SHUT OFF NORMALLY. ENG HYD 2 GREEN PUMP TURNED OFF MOMENTARILY. ITS CB POPPED AND THE PUMP STARTED OPERATING AGAIN. CORDINATED WITH MOCC TO RESETMay 1, 2017 · N808FD · Airbus A310 · Hydraulic Pump (Electric/Engine), MainSDR FDEA201602150560Skin Panel · corrodedCORROSION ON UPPER RT WING SKIN, APPROX 83.5" FROM WTB. CORROSION FORMED AROUND FASTENER HEAD & EXTENDS AFT, APPROX 2"X4". REMOVED VISIBLE CORROSION ON RT WING UPPER SKIN IAW SRM 51-74-10. CHECKED LIMITS BLEND AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 57-2Feb 15, 2016 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201512284090Engine · power lossDURING DESCENT BELOW PROFILE THRUST WAS APPROX 75 - 77% N1. AT PROFILE THROTTLES REDUCED TO IDLE & APPROX 60% N1, A THUMPING SOUND WAS HEARD & FELT. SUSPECT COMPRESSOR STALL. ALTITUDE 30000 FT SPEED 0.8. NO ABNORMAL ENG INDICATIONS. SUSPECT ENG NR 2. Dec 28, 2015 · N808FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR FDEA201506171831Windshield · crackedAT FL 370 CAPTAIN`S OUTER WINDSCREEN SHATTERED. PRESSURIZATION HELD OK, DIVERTED. R & R CAPTAIN`S WINDSHIELD PANEL IAW AMM 56-11-11-04. WINDSHIELD PANEL ANTI-ICING & DE- FOGGING OPERATIONAL TESTED SATISFACTORY.Jun 17, 2015 · N808FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201504301331Window · failedAFTER TAKEOFF GOT RT WINDOW HEAT FAULT. FOLLOWED QRH & RESET RT WINDOW HEAT. LATER CLIMBING THROUGH FL 280, THE LT WINDSHIELD COMPLETELY SHATTERED ON THE OUTSIDE PANE WITH NO WARNING. THERE WAS SOME ELEC ARCING AFTERWARD. LATER ON DESCENT GOT RT WINDOW HEAApr 30, 2015 · N808FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201502220573Skin · damagedFOUND ONE LIGHTNING STRIKE AT THE TRAILING EDGE OF THE LT WING TIP UPPER INBD SURFACE. REPLACED THE SKIN IAW SRM 57-30-11.Feb 22, 2015 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201502160536Fitting · crackedAFT CARGO COMPARTMENT DOOR ACTUATOR FITTING CRACKED. REMOVED THE AFT CARGO DOOR ASSEMBLY IAW AMM 52-32-11-04. REPLACED THE FRAME HEAD IAW SRM 51-40-21. INSTALLED THE AFT CARGO DOOR ASSEMBLY IAW AMM 52-32-11-04. TESTED OK.Feb 16, 2015 · N808FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201502130527Crossbeam · corrodedAFT CARGO FLOOR FRAME 63 CROSSBEAM CORRODED BETWEEN Y140 & Y805. REPAIRED THE CROSSBEAM PER SRM 53-10-15 FIG.209.SHT.1Feb 13, 2015 · N808FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201502130526Crossbeam · corrodedAFT CARGO FLOOR FRAME 61 CROSSBEAM CORRODED BETWEEN -Y805 & Y805. REPAIR THE CROSSBEAM PER SRM 53-10-15 FIG.209 SHT.1Feb 13, 2015 · N808FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201501070049Bleed Valve · malfunctionedFLIGHT DEPARTED WITH MEL 36-11-06-1A, NR 1 BLEED AIR VLV INOPERATIVE. DURING CLIMB OUT, WE DEVELOPED A NR 2 HP BLEED FAULT. FOLLOWED ECAM & QRH PROCEDURES. PROCEDURES LED US TO DUAL BLEED FAILURE CHECKLIST & WE COMPLIED. R & R NR 2 ENG HP BLEED VLV IAW MM Jan 7, 2015 · N808FD · Airbus A310324 · Compressor Bleed ValveSDR FDEA201303120549Rib · crackedLT WING T/E AT 284.85, SUPPORT RIB CRACKED, JUST BETWEEN SPOILER NR 5 AND SPOILER NR 6.Mar 12, 2013 · N808FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201205011689Angle · crackedLEFT FRAME40 PICK UP ANGLE FOUND CRACK EXTENDED FURTHER THAN STOP HOLE (EXTENDED CRACK LENGTH:0.2INCHES) COMPLY WITH EA 6-5310-161218, PART 1.May 1, 2012 · N808FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201112295456Oil System · overtempNR 2 ENG, HIGH OIL TEMP - ABOVE 180 DEG - SHUT ENG DOWN. ALL OTHER ENG PARAMETERS OK. INSPECTED NR2 ENG INLET & EXHAUST AREA; NIL ABNORMALTIES NOTED. VISUAL CK OIL QTY; NORMAL. R & R NR 2 ENGINE IAW WC 44T0105-2 AND 44T0708-2. RUN ENG IAW JRH LEAK CHECKEDDec 29, 2011 · N808FD · Airbus A310324 · Turbine Engine Oil SystemSDR FDEA201109203976Cabin Pressure · malfunctionedRED CABIN ALTITUDE WARNING, PERFORMED DESCENT TO 10,000 FT ON CABIN PRESSURE SYS PAGE, BOTH OUTFLOW VALVES SHOW AMBER & FULL OPEN - NO ECAM MESSAGE, CABIN ALTITUDE 10,000 FT. UNABLE TO CONTROL CABIN ALTITUDE . PACK VALVES SHOW AMBER AND CLOSED INTERMITTENTSep 20, 2011 · N808FD · Airbus A310324 · Cabin Pressure Control SystemSDR FDEA200912084382Computer · malfunctionedON CLIMB OUT, FLAPS AND SLATS UP, CAPT MAX SPEED INDICATOR (ZIPPER) REMAINED AT 245 KTS. F/O SPD LIMIT REMAINED "ON". R & R NR 2 SFCC DUE TO FAULT AND R & R NR 1 SFCC AS A PRECAUTION IAW AMM 27-51-18-4 AND TESTED IAW AMM 27-51-00-0, BITE TESTS PASS NO FAULTDec 8, 2009 · N808FD · Airbus A310324 · Speed-Attitude Correction SystemSDR FDEA200904011132Wire · faultedAFTER T/O FLAPS STUCK AT ABOUT 5 DEGREES, COMPLIED WITH QRH. NO LUCK, RETURNED TO IND FLAPS CAME DOWN OK FOUND SAME FAULT CODES AS BEFORE SFCC 1 AND 2 LT VANE OUT. INSPECTED JAM DETECTOR UNITS NO INDICATION OF CRUSHED HONEYCOMB, BROKEN SHEAR PIN, OR OTHER DAApr 1, 2009 · N808FD · Airbus A310324 · Flight Control System WiringSDR FDEA200812315323Damper · malfunctionedLANDING GEAR WOULD NOT RETRACT ON TAKEOFF ALTHOUGH AUTO THROTTLES WAS ENGAGED IT WAS INOP IN THE INITIAL CLIMB AUTO THROTTLE WORKED AGAIN ONCE SLATS WERE EXTENDED. PERFORMED BITE CHECK ON PROX BOX AT HGR RAMP AND CAME UP WITH (LB) FAULT AT THIS TIME. NO OTHDec 31, 2008 · N808FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR 08FDEA04005Seat Track · damagedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE HAS SCRATCH AT FR 40 LT, BELOW FLOOR PANEL 231QH, AFT SIDE REMOVED DAMAGED SEAT TRACK AND FABRICATED AND INSTALLED REPLACEMENT TRACK AT TRACK NR 4LT BETWEEN FR 40 AND FR 45 IAW AIRBUS DRAWING A53811923 AND A310-300 SSep 23, 2008 · N808FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03938Seat Track · corrodedMDCC SEAT TRACK 4R CORRODED 2 AREAS FRAME 42 AND 44 4 SQ INCH. REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FR 40 TO 44.5 RT AT Y-1456 IAW SRM 53-10-16 FIGURE 203 SHEET 5.Sep 18, 2008 · N808FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03937Floorbeam · crackedMDCC FLOOR FRAME 30 HAS 1 INCH CRACK BETWEEN SEAT TRACK 2L AND 3L REMOVED CRACK AND INSTALLED FLOORBEAM REPAIR BETWEEN SEAT TRACK 2L AND 3L AT FR 30 IAW SRM 53-10-15 FIGURE 211 SHEET 1 AND 2.Sep 18, 2008 · N808FD · Airbus A310324 · Fuselage Main, Floor BeamSDR 08FDEA03936Seat Track · corrodedMDCC SEAT TRACK NR 1 CORRODED AT FRAME 71 2 SQ IN REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION AT FR71 TO 74 AND INSTALLED NEW SECTION IAW SRM 53-10-16 FIG 208 SHEET 1, PG 247/248.Sep 18, 2008 · N808FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03935Skin · damagedRIGHT SIDE FUSELAGE FR 37 STRINGER 30 1 LIGHTNING STRIKE REMOVED DAMAGED AREA AT FR37 RT SIDE STR 30 AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-12 FIG 224 SHEET 3.Sep 18, 2008 · N808FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 08FDEA03934Seat Track · corrodedMDCC SEAT TRACK 3R CORRODED 2 AREAS AT FRAME 46 4 INCH SQ IN REMOVED LEVEL 1 CORROSION ON SEAT TRACK SECTION AND INSTALLED NEW SEAT TRACK 3R FROM FRAME 44 TO 49 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 102 PG 105 AND SRM 51-40- 21.Sep 18, 2008 · N808FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03910Seat Track · damagedMAIN DECK CARGO SEAT TRACK NR 4LT BETWEEN FR 59.2 AND FR 59.3 HAS 2 AREAS OF DAMAGED SCALLOPS REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED REPLACEMENT TRACK AT NR 4 LT BETWEEN FR 58 AND FR 60.5 IAW A310-300 SRM 51-40-210AND 53-17-16Sep 17, 2008 · N808FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00544Wire · damagedAFTER START GOT OVERBOARD VALVE FAULT COMPLIED WITH ECAM QRH AND CHECKED MEL. DURING CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AVIONICS EXTRACT VALVE TO FOM AV LINE C/B'S 60HR, 61HR PULLED AND COLLARED. FOUND WIRE BUNDLE CUT, FOR AV EXTRACT VALVE. Feb 21, 2008 · N808FD · Airbus A310324 · Air Conditioning System WiringSDR 07FDEA03455Stringer · corrodedFOUND CORROSION ON STRINGER 50, BETWEEN FRAME 55/58-59 LHS, OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Sep 7, 2007 · N808FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR 07FDEA03463Skin Panel · corrodedHEAVY CORROSION FOUND ON CENTER WING BOX TOP SKIN AT TR5 AND TR6 RT/LT, FRAME 43-46.2. REPAIR PERFORMED IAW SRM 57-10-12/FIG 201 AND RAS/042817/015/2006 ISSUE A, EXCEPT FOR DAMAGES AT FRAME 44, BEAM 5 AND 6 LT AND RT, WHICH WAS REPAIRED BY DOUBLER IAW RAS/042Sep 7, 2007 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR 07FDEA03462Stringer · corrodedFOUND CORROSION ON STRINGER 43 RT BETWEEN FRAME 47-48, OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE CORRODED AREAS IAW EA 6-5315-99192 AND RAS/043644/008/2006 ISSUE A.Sep 7, 2007 · N808FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
Back to N808FD, cancelled Mar 2, 2024