N575UP

Service difficulty reports · 253

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 = 'N575UP' AND registry_match = 'registration'
  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 IPXA2024051423435Floor Panel · brokenFAULT - BROKEN - FOUND MAIN DECK FLOOR PANEL BROKEN, PNL NO. 211DF. ( P/N : 141U5876-55 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42Apr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423470Floor Panel · crackedFAULT - CRACK - FOUND MAIN DECK FLOOR PANEL CRACK, PNL NO. 231EF. ( P/N : 141U5877-134 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL.JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-RApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423429Floor Panel · crackedFAULT - CRACK - FOUND MAIN DECK FLOOR PANEL CRACK, PNL NO. 272NF. ( P/N : 146U5884-11 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-4264Apr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024051423426Floor Panel · crackedFAULT - CRACK - FOUND MAIN DECK FLOOR PANEL, PNL NO. 212JG. ( P/N : 141U5876-104 ) (REPAIR) I.A.W AMM 53-21-02-404-006 REV.110 INSTALL MAIN DECK FLOOR PANEL. 6. JOB COMPLETED AND CONDITION CHECK SATISFACTORY. 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-REQApr 29, 2024 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2024052345715Hinge Fitting · damagedFOUND R/H WING NO.10 SPOILER INBD NO.1 HINGE BOLT HOLE ENLARGE.COMPLETED MACHINING THE HINGE FITTING I.A.W. EI NO.F2024A57M-1178 REV.0 SEQUENCE:AApr 24, 2024 · N575UP · Boeing 74744AF · SpoilersSDR IPXA2024052590591Shear Tie · crackedFAULT - CRACK, DURING PERFORM EO-80332-JIC001 FOUND SHEAR TIE CRACK AT STA 1000, LBL 33.99. (REPLACE). ACCOMPLISH REPAIR PER EO-90397-REQ1 . ACCOMPLISHED EO-80332-JIC006 REV2. REVIEW COMPLETEDApr 20, 2024 · N575UP · Boeing 74744AF · Fuselage Internal Mounting StructureSDR IPXA2024051780188Roller · damagedFOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT FWD - UPPER SIDE. (REPLACE). I.A.W AMM 52-11-01-735-080 REV 110 REPLACED L1 ENTRY DOOR LATCH ROLLER.Apr 19, 2024 · N575UP · Boeing 74744AF · Passenger/Crew DoorsSDR IPXA2024041980188Roller · damagedFOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT FWD - UPPER SIDE. (REPLACE). OPENApr 19, 2024 · N575UP · Boeing 74744AF · Passenger/Crew DoorsSDR IPXA2025022634582Skin · damagedWHILE REMOVING LH I/B FOREFLAP, THE LEADING EDGE WAS DAMAGED NEAR O/B HINGE FITTING. 1.INSTALLED L/H WING INBD FORE FLAP TOP PANELS I.A.W SRM 51-40-02-0G REV 100 AND AMM 20-51-01-912-008 REV 110 . 2. JOB COMPLETED. REVIEW COMPELTEDFeb 17, 2024 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2023092821122Unknown · damagedDAMAGE/GOUGE ON THE OUTBOARD EDGE OF THE L/H AFT FLAP MEASURING .0205 DEEP (LINKED TO T3F18E002BVB2) ***LMX EVAL *** REMOVED AND REPLACED THE LH OUTBD AFT FLAP PER AMM 27-51-06. OPS CHECK GOOD. R R FLAP PER AMM SEE CORRECTION ON LINE ITEM 5Sep 2, 2023 · N575UP · Boeing 74744AF · Wing StructureSDR IPXA2023092821106Unknown · unknownL/H OUTBOARD AFT FLAP GOUGED/DAMAGED .0575 DEEP (LINKED TO T3F18E002BVB9) ***LMX EVAL REQ*** WITNESSED INSTALLATION AND TORQUE OF LH WING OUTBOARD AFT FLAP IAW AMM 27-51-06. OPS CHECKS GOOD R R FLAP PER AMM OPS CHECK GOODSep 2, 2023 · N575UP · Boeing 74744AF · Wing StructureSDR IPXA2023090321122Unknown · unknown*** SDR FILED OPEN *** DAMAGE/GOUGE ON THE OUTBOARD EDGE OF THE L/H AFT FLAP MEASURING .0205 DEEP (LINKED TO T3F18E002BVB2) ***LMX EVAL *** R R FLAP PER AMM SEE CORRECTION ON LINE ITEM 5Sep 2, 2023 · N575UP · Boeing 74744AF · Wing StructureSDR IPXA2023090321106Unknown · unknown*** SDR FILED OPEN *** L/H OUTBOARD AFT FLAP GOUGED/DAMAGED .0575 DEEP (LINKED TO T3F18E002BVB9) ***LMX EVAL REQ*** R R FLAP PER AMM OPS CHECK GOODSep 2, 2023 · N575UP · Boeing 74744AF · Wing StructureSDR IPXA2025022659129Structure · damagedLH INBRD MID FLAP BIRD STRIKE **FLAP R&R** INSTALLED REMOVED CARRIAGE ONTO NEW MID FLAP, TORQUED AND SAFETY APPLIED IAW AMM 27-51-23. INSTALLED RIGHT INBOARD FLAP ASSAY PER MM 27-51-01-404-030 UP TO STEP H(10). VERIFIED OPERATION CHECK OF FLIGHT CONTROLS (FLAPAug 20, 2023 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2023043029468Battery · inoperativeFAULT - FOUND THE UPPER DECK EMERGENCY LIGHT INOP AT CEILING PANEL STA 550 AND STA 587. (REPLACE) 1.I.A.W AMM 33-51-04-902-001-001 REV.107.00 REPLACED EMERGENCY LIGHT BATTERY (M5169) AT UPPER DECK STA 590 RBL 83 WL 323 AND PERFORMED EMERGENCY LIGHT OPERATIONApr 29, 2023 · N575UP · Boeing 74744AF · Emergency LightingSDR IPXA2023042819659Light · inoperative*SDR FILED OPEN* FAULT - FOUND L1 DOOR DOORWAY EMERGENCY LIGHT INOP. I.A.W AMM 33-51-05-962-031 REV.107.00 REPLACED THE L1 DOOR DOORWAY EMERGENCY LIGHT LAMPS AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST, RESULT WAS SATISFACTORYApr 28, 2023 · N575UP · Boeing 74744AF · Emergency LightingSDR IPXA2023070582421Unknown · unknown*MAJOR REPAIR* MAIN CARGO AREA, POSITION 7 RIGHT,INBOARD AFT FLOOR HAS A HOLE . [MARKED]***SM26/LM8*** INSTALLED IN REF TO AMM 25-52-05Jan 4, 2023 · N575UP · Boeing 74744AF · Cargo CompartmentsSDR IPXA2022020841715Skin · damaged*SDR FILED OPEN* *MAJOR REPAIR* VERTICAL STABILIZER LEFT SKIN PANEL DAMAGE REPAIR***SM120/LMX0***CONTACT AMC FOR FOLLOW ON ACTIONS TO BE ACCOMPLISHED*** WILL REQUIRE S/M 120 HRS TO R&R SKIN PANEL. HANGAR IS NEEDED, PARTS ON ORDER.May 1, 2022 · N575UP · Boeing 74744AF · Vertical Stabilizer, Plate/SkinSDR IPXA2022071356953Skin Panel · damagedVERTICAL STABILIZER LEFT SKIN PANEL DAMAGE REPAIR DEFER PER EO 83598-REQ1Feb 9, 2022 · N575UP · Boeing 74744AF · Crew Oxygen SystemSDR IPXA2022020978814None · noneINSPECTION TYPE:CKLT VERT STAB SKIN PANEL DELAMINTEDINSTALLED TEMPORARY PANEL IAW EO B747-5530-82778-AFeb 9, 2022 · N575UP · Boeing 74744AF · Vertical StabilizerSDR IPXA2021052669862Circuit Card · no testINSPECTION TYPE:N/AFINDING OF DOC FIRE SYSTEM TEST FAIL.PERFORMED FIM 26-16-00-812-902, REPLACED AFOLTS A6 CARD IAW AMM 26-10-01-401. PERFORMED OPS TEST IAW AMM 26-10-01-754-013. TEST PASSED. P/N ON-OFF: 285N0028-136, S/N ON: D18599, S/N OFF: D17244. EFF REF IMay 26, 2021 · N575UP · Boeing 74744AF · Fire DetectionSDR IPXA2020120663107Warning Message · illuminatedINSPECTION TYPE: NA DIV EMERGENCY DECLARED, NO EQUIP USED. A/C OUT OF SERVICE. EICAS MESSAGES PACK 2 & 3, HYD PRESS DEM 2, AIL LOCKOUT, RUD RAT SNGL, AIR/GROUND SYS YAW DAMP LOWER 1ST MESSAGES TO SHOW. STATUS MESSAGES RES 3B XFR VALVE RES 2B XFR VALVE GR MODec 6, 2020 · N575UP · Boeing 74744AF · DC Generating SystemSDR IPXA2020070657352Battery · dischargedINSPECTION TYPE:C2 FOUND L1 DOOR EMERGENCY LIGHT INOP. IAW AMM 33-51-04-902-001-001 REV 98.01 REPLACED THE EMERGENCY LIGHT BATTERY M5170 AT U/D STA 550 WL323 LBL83. IAW AMM 33-51-04-902-001 REV 98.01 PERFORMED EMERGENCY LIGHT BATTERY OPERATION TEST, RESULT WJul 5, 2020 · N575UP · Boeing 74744AF · Emergency LightingSDR IPXA2020070357243Floor Panel · damagedINSPECTION TYPE:C2 DAMAGE ON M/D CARGO FLOOR PANEL FROM STA 2140 TO STA 2220 NEAR LBL 98.58, PANEL NR 271MF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B747-5320-42648-A.Jun 22, 2020 · N575UP · Boeing 74744AF · Fuselage Floor PanelSDR IPXA2020070657320Skin · delaminatedINSPECTION TYPE:C2 DENT DAMAGE WITH DELAMINATION FOUND ON UPPER SURFACE OF BOND ASSY ( P/N:65B05751-25) ON LT OUTBD ELEVATOR. REPAIR IAW SRM 55-20-01-2R-1 REV 89.00 AND SRM 51-70-07-0G REV 89.00.Jun 19, 2020 · N575UP · Boeing 74744AF · Elevator, Plate/SkinSDR IPXA2020070657319Skin Panel · dentedINSPECTION TYPE:C2 MULTIPLE DENT DAMAGES FOUND ON UPPER SURFACE OF PANEL ASSY (P/N:65B05762-56) ON RT OUTBD ELEVATOR. REPAIR IAW SRM 55-20-01-2R-1 REV 89.00 AND SRM 51-70-07-0G REV 89.00.Jun 19, 2020 · N575UP · Boeing 74744AF · Elevator, Plate/SkinSDR IPXA2020070657318Skin Panel · dentedINSPECTION TYPE:C2 MULTIPLE DENT DAMAGED FOUND ON UPPER SURFACE OF TRAILING EDGE UPPER PANEL ASSY OF RT INBD AILERON. REPAIR IAW SRM 57-60-01-2R-1 REV 89.00 AND SRM 51-70-06-0G REV 89.00.Jun 19, 2020 · N575UP · Boeing 74744AF · AileronsSDR IPXA2020070657317Panel · dentedINSPECTION TYPE:C2 MULTIPLE DENTS ON LT WING INBD MID FLAP UPPER INBD PANEL ASSY BETWEEN SPAR NR 2 TO SPAR NR 3. REPAIR THE DAMAGED PANEL IAW SRM 57-53-01-2R-1, REV 89.00, SRM 51-70-10-2R-2 REV 89.00, SRM 51-70-10-2R.Jun 19, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020070657316Skin Panel · dentedINSPECTION TYPE:C2 MULTIPLE DENT DAMAGES FOUND ON UPPER SURFACE OF UPPER PANEL ASSY OF RT INBD AILERON. REPAIR IAW SRM 57-60-01-2R-1 REV 89.00 AND SRM 51-70-06-0G REV 89.00.Jun 19, 2020 · N575UP · Boeing 74744AF · AileronsSDR IPXA2020070667315Panel · dentedINSPECTION TYPE:C2 MULTIPLE DENTS ON LT WING INBD TE MID FLAP UPPER OUTBD PANEL ASSY BETWEEN SPAR NR 2 TO SPAR NR 3. REPAIR THE DAMAGED PANEL IAW SRM 57-53-01-2R-1 REV 89.00, SRM 51-70-10-2R-2 REV 89.00 SRM 51-70-10-2R.Jun 19, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020070657323Skin Panel · dentedINSPECTION TYPE:C2 MULTIPLE DENT DAMAGES FOUND ON UPPER SURFACE OF TRAILING EDGE UPPER PANEL ASSY (P/N:65B02224-36) OF LT INBD AILERON. REPAIR IAW SRM 57-60-01-2R-1 REV 89.00 AND SRM 51-70-07-0G REV 89.00.Jun 18, 2020 · N575UP · Boeing 74744AF · AileronsSDR IPXA2020060856266Aileron · dentedINSPECTION TYPE:N/A REMOVE DAMAGED AREA WITHIN DENTS AND REPAIR PER EO 747-5750-76757-A. REMOVED DAMAGE, 4EA DENTS AND REPAIRED PER EO B747-5750-76757.Jun 8, 2020 · N575UP · Boeing 74744AF · AileronsSDR IPXA2020060856249Skin · dentedINSPECTION TYPE:N/A LT INBD MID FLAP IS DENTED UPPER SKIN REF EO B747-5750-74270-B. REPAIRED PER EO B747-5750-74270-B.Jun 7, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020050655017Stringer · damagedINSPECTION TYPE:N/ADAMAGE AT STRINGER 38L AT STA 550REPAIRED DAMAGED STRINGER PER 30L AT STA 550 IAW EO B747-5310-76293-AMay 6, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Longeron/StringerSDR IPXA2020050655016Skin · damagedINSPECTION TYPE:N/ADAMAGE AT FUSELAGE SKIN AT STA 500 TO STA 520 AND STRINGER 36L TO 38LREPAIRED DAMAGED SKIN AT STA 500, S36L TO 38L IAW EO B747-5330-76297-AMay 6, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2020050655015Skin · damagedINSPECTION TYPE:N/ADAMAGE AT FUSELAGE SKIN STA 480 TO STA 500 AND STRINGER 35L TO 37LREPAIRED DAMAGED SKIN AT STA 480 TO 500 $35 L TO 37 L IAW EO B747-5330-76296-AMay 6, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2020050655018Skin · damagedINSPECTION TYPE:N/ADAMAGE AT FUSELAGE SKIN AT STA 520 TO 580 AND STRINGER 37L TO 41LREPAIRED DAMAGED FUSELAGE SKIN AT STA 520 TO 580 AND STRINGER 37 L TO 41 L IAW EO B747-5330-76292-AMay 4, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2020050154815Skin · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE LEFT SIDE OF FUSELAGE SKINS AT STA 520 TO STA 580 STRINGER 37L TO 41L P/N: 142U3260-12 AND P/N: 142U3262-11 (REF SRM 53-20-01-0I-1 FIG 1 ITEM 5 AND 21)ACCOMPLISHED EO# B747-5330-76292-A REV 04/XX/2020Apr 30, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2020050154814Stringer · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE FUSELAGE STRINGER 38L AT STA 550 P/N: 142U7724-21 (REF SRM 53-20-03-0I FIG 1 DETAIL 1 ITEM 17).ACCOMPLISHED EO# B747-5310-76293-A REV 04/23/2020.Apr 30, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Longeron/StringerSDR IPXA2020050154813Skin · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE LEFT SIDE FUSELAGE SKIN AT STA 500 TO STA 520 AND S36L TO 38L, P/N: 65B07659-305 (REF SRM 53-10-01-OI-1 FIG 1 DETAIL III ITEM 1).ACCOMPLISHED EO# B747-5330-76297-A REV 04/29/2020.Apr 30, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2020050154812Skin · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE LEFT SIDE FUSELAGE SKIN AT STA 480 TO STA 500 AND S35L TO 37L, P/N: 65B07659-305 ( REF SRM 53-10-01-0I-1 FIG 1 DETAIL III ITEM 1)ACCOMPLISHED EO# B747-5330-76296-A REV 04/XX/2020.Apr 30, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Plate/SkinSDR IPXA2020050154811Stringer · damagedINSPECTION TYPE:N/AAC MX REPORTED DAMAGE TO THE FUSELAGE STRINGER 38L AT STA 490 P/N: 65B07659-578 (SRM 53-10-03-01 FIG 1 DETAIL III ITEM 1) AT APPROX STA490.ACCOMPLISHED EO# B747-5310-76291-A REV 04/23/20.Apr 30, 2020 · N575UP · Boeing 74744AF · Fuselage Main, Longeron/StringerSDR IPXA2020041054041Skin · dentedINSPECTION TYPE:N/ARH INBD TE AFT FLAP UPPER SURFACE DENT 19" FROM TE AND 9.5" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTALL. 4Apr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020041054040Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 19.5" FROM TE AND 8.5" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTApr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020041054039Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 19.2" FROM TE AND 57" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTAApr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020041054038Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 19.5" FROM TE AND 93" FROM IB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTAApr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020041054037Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 20.5" FROM TE AND 97" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTAApr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020041054036Skin · dentedINSPECTION TYPE:N/ARH INBD TE AFT FLAP HAS UPPER SURFACE DENT 21" FROM TE AND 157.5" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTApr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020041054035Skin · dentedINSPECTION TYPE:N/ARH INBD AFT FLAP HAS UPPER SURFACE DENT 20.5" TROM TE AND 89" FROM IB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI 51-05-01. GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTALL 45011Apr 8, 2020 · N575UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA2020032553431Floor Panel · puncturedINSPECTION TYPE:N/AMAIN DECK FLOOR BOARD PUNCTURE IN UPPER SURFACE STA 1730 CENTERLINE.REMOVED UPPER SKIN PLIES - NO CORE DAMAGE. DAMAGE REMOVAL OK PER QC, OK TO INSTALL REPAIR PER QC. POTTED HOLE AND FABRICATED PRE CURED DOUBLER PER SRM 53-00-50-2R-1 FIG 201 Mar 22, 2020 · N575UP · Boeing 74744AF · Fuselage Floor Panel
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