N894AT

Service difficulty reports · 119

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 = 'N894AT' 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 DALA2024071807236Coax · looseSHIP 9554 -ATO- THE FLIGHT CREW ABORTED THE TAKEOFF AT 130 KTS DUE TO THE #1 PRIMARY FLIGHT DISPLAY AND MULTI-FUNCTIONAL DISPLAY BLANKING OUT. CORRECTIVE ACTION: MAINTENANCE FOUND 2 EACH COAX CABLES LOOSE ON VIA #1 SPLITTERS AND REPLACED BOTH DISPLAY UNITS. (LJul 13, 2024 · N894AT · Boeing 717200 · Instrument System WiringSDR DALA2023092207784Unknown · unknownDOOR R1 EXIT SIGN IS MISSING. MAINTENANCE REPLACED AND INSTALLED THE MISSING LENS COVER IAW B717 AMM 33-51. LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4579222)Sep 21, 2023 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2023071805821Unknown · unknownCRACKS ON LH CUSP WEB AROUND RING BTW STA 652 AND 655. SUMMARY OF NRC 00668: LH CUSP WEB AROUND RING BTW STA 652 AND 655 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 PAR 5. B. FIGURE 211. (LP #2863892 )Jul 18, 2023 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025013000727Skin · corroded-AD- CENTER WING BOX LOWER SKIN XCW=20 TO XCW=42 REAR SPAR TO STRINGER #12 HAS CORROSION AND ELONGATED HOLES. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 14MAR23. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS RMar 15, 2023 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023031401845Unknown · unknownCORROSION WAS FOUND ON FWD PASSENGER DOOR STAIRWELL INTERNAL STRUCTURE IN REF NRC 2060-1001. SUMMARY OF NRC 00572: CORROSION LEVEL 2. FWD PASSENGER DOOR STAIRWELL WAS REPLACED WITH SERVICEABLE STAIRWELL PER B717-200 AMM 52-63-01. TOOL USED CALIBRATED STD DUE DMar 9, 2023 · N894AT · Boeing 717200 · Entrance StairsSDR DALA2023030201555None · noneSKIN PANELS BTW STA 954 TO STA 974 LONG 30 TO R29 ARE CORRODED OUT OF LIMITS. WITH ORIGINAL THICKNESS OF 0.071 IN. AND THE MAXIMUM REMOVED MATERIAL FOUND IS 0.033 IN. THEREFOR AREA IS OUT OF LIMITS IN REF NRC 00192 AT AFT CARGO (C2). SUMMARY OF NRC 00512: CORRMar 1, 2023 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023030101525None · noneSEVERAL DENTS ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING (AI). SUMMARY OF NRC 00160: DENTS (26 EAS) ON AFT MOVABLE FLAP VANE (LOWER SURFACE) AT LH WING WERE FOUND AND EVALUATED AS FOLLOWS, WHERE, L=LENGTH, W=WIDTH, Y=DEPTH, AND W/Y MUST BE 10 OR MORE,Feb 27, 2023 · N894AT · Boeing 717200 · Aileron TabsSDR DALA2023022401415None · noneCORROSION ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 (CPAX)( W1). SUMMARY OF NRC 00425: CORROSION LEVEL 2. CORROSION WAS REMOVED ON SEAT TRACKS STA Y=200-237 X=-22, STA Y=200-218 X=-44.5 AND STA Y=200 X=22 PER B717-200 SRM 51-Feb 22, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023022401414None · noneCRACK ON PAN, FWD/UPPER INNER SIDE NEAR TO BEAM 5 OF FWD CARGO COMPARTMENT DOOR. (C1) SUMMARY OF NRC 00541: PAN FWD/UPPER OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201. (LP #2640421)Feb 22, 2023 · N894AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2023022201326None · noneCORROSION ON FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 (CPAX)(W1). SUMMARY OF NRC 00433: CORROSION LEVEL 2. FLOOR SUPPORT 4 (EA) STA Y=218 AND X=0 TO X=13.5, STA Y=200 X=16 TO X=-6, STA Y=200-210 X=-10.5 WEFeb 22, 2023 · N894AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023022001254None · noneCRACK ON LONGERON 2RH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00414- LONGERON 2RH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05- 2R REPAIR 2. (LP #2633164)Feb 17, 2023 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023021701231None · noneA.A. A.D. CRACK WAS FOUND OF 0.250" LENGTH ON FRAME STA Y=737 RH SIDE IN REF CARD 5310-01439-01D JOB# 094-0004 STEP: 4. SUMMARY NRC 00154: OVER WING FRAME STA Y=737 BTW LONG 8 TO 18 RH WAS REPLACED PER WORK CARD 5310-01439-02B. ASSOCIATED AA 5310-01439 ADDED FFeb 16, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021701229None · noneCRACK ON INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22, PASSENGER CABIN. SUMMARY OF NRC 00442: INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1. (LP #2631096)Feb 16, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021701228None · noneSEVERAL HIDDEN CRACKS ON RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 IN REF NRC 00154. SUMMARY OF NRC 00514: RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2 R REP 4 PAR 5 FIFeb 15, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021501180None · noneCORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=200 X=-9 TO X=-44. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.045 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00431 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00484: CORROSION LEVEFeb 13, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023021501179None · noneIN REFERENCE TO NRC 00066, AFTER REMOTION OF RETAINER SEALS, CRACK WAS FOUND ON PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2. SUMMARY OF NRC 00511: PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2 WAS REPAIRED PER B7Feb 13, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023021401136Unknown · unknownCORRODED DIAPHRAGM ON STA Y=200 X=-22. ORIGINAL THICKNESS WAS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.012 IN, THEREFORE IT IS OUT LIMITS IN REF NRC 00424 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00510: CORROSION LEVEL 2. DIAPHRAGM (WEB) ON STA Y=200 X=-22Feb 11, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021401134Unknown · unknownCORRODED FLOOR SUPPORT STA Y=157-200 AND X=44.5, STA Y=180 AND X=12 TO X=38. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.035 IN, THEREFORE THE AREA IS OUT LIMITS IN REF NRC 00434 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00485: CORROSIONFeb 11, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023021401129Unknown · unknownCRACK ON WEB OF FUSELAGE DOOR FRAME, STA. 208, OVER LONGERON 11 LH AND LONGERON 15 LH. (CPAX). SUMMARY OF NRC 00394: WEB OF FUSELAGE DOOR FRAME, STA. 208, OVER LONGERON 11 LH AND LONGERON 15 LH WAS REPAIRED PER B717-200 SRM 53-10-15-2R PROCEDURE 1 REPAIR 1. (LFeb 10, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021401127Unknown · unknownCRACKS (2EAS, FWD AND AFT SIDES) WERE FOUND ON BEAM 1 DURING THE WORK PROCESS ON NRC 00081 AT L1 PASSENGER DOOR. (PTAS). SUMMARY OF NRC 00487: FWD AND AFT SIDES OF BEAM 1 AT L1 PASSENGER DOOR WERE REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LPFeb 10, 2023 · N894AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023021401126Unknown · unknownCORROSION IS OUT OF LIMITS AT THE LH CUSP WEB MEMBRANE AT STA 395 X=54 TO X=59. ORIGINAL THICKNESS WAS 0.020 INCHES AND REMAINING THICKNESS AT STA 395 IS 0.008 INCHES. THEREFOR AREA IS OUT LIMITS. REF NRC 00293 AT PAX CABIN (CPAX). SUMMARY OF NRC 00509: CORROSFeb 10, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021401125Unknown · unknownPUNCTURES (2EA) WERE FOUND ON FLOOR WEB STA Y=128 AND X=17 AT FLIGHT DECK IN REF CARD 2060-1007. SUMMARY OF NRC 00503: WEB STA Y=128 AND X=17 AT FLIGHT DECK WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #2622123)Feb 9, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021401121Unknown · unknownSCRATCH (2 EA) ON DIAPHRAGM STA Y=189 AND X=45 (CPAX) (W1). SUMMARY OF NRC 00423: DIAPHRAGM STA Y=189 AND X=45 WAS PERMANENTLY REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 PAR. 4 FIG. 201 (SHEET 2). (LP #2621668)Feb 9, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021401119Unknown · unknownELONGATED AND BENT HOLE ON RH CUSP WEB STA Y=715 TO 756 X-44 TO X-60 IN REF NRC 00154. SUMMARY OF NRC 00446: RH CUSP WEB STA Y=715 TO 756 X-44 TO X-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REP. 4 FIGURE 221. (LP #2620447)Feb 8, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023021401118Unknown · unknownCORROSION ON FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE (PAX CAB) (W2). SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 53-20-51-0I,Feb 8, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023020800983Not Reported · not reportedSECONDARY NRC 00428: FLOOR SUPPORT STA Y=180 AND X=-9 TO X=-43 HAS CORROSION. ORIGINAL THICKNESS IS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.020 IN, THEREFORE THE AREA CORROSION IS OUT LIMITS AT PAX CABIN. (CPAX)(W1). SUMMARY OF NRC 00489: CORROSION LEVELFeb 7, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023020800982Not Reported · not reportedCORROSION ON FLOOR SUPPORTS (3 EA) STA Y=196 TO 200 FROM X=16 TO X=55.5 AT PAX CABIN FLOOR STRUCTURE. CPAX. SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) AT STA Y=196 TO 200 FROM X=16 TO X=55.5 WERE REPLACED PER B717-200 SRM 51-41-05 PAR 8, 51Feb 7, 2023 · N894AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023020700925Not Reported · not reportedCRACK ON RH CUSP WEB MEMBRANE AT STA 655 TO 674 & X=-54 TO X=-59 PASSENGER CABIN FLOOR (CPAX). SUMMARY OF NRC 00292: RH CUSP WEB MEMBRANE AT STA 655 TO 674 & X=-54 TO X=-59 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIG 216. (LP #2618034Feb 7, 2023 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2020112303837Battery Pack · inoperativeBOTH THE L1 AND R1 LOWER EXIT SIGNS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK ABOVE SEAT 2CD, IAW B717 AMM 33 -51. OPERATIONAL CHECK WAS GOOD.Nov 23, 2020 · N894AT · Boeing 717200 · Emergency LightingSDR 2020F00248Spoiler · delaminatedDISBONDEDFeb 26, 2020 · N894AT · Boeing 717200 · SpoilersSDR DALA2020011600323Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 30, BETWEEN STA 948- 954 IS CORRODED. NRC 040-0008:5331-2001/004 00196: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM STA 937-965 REF SRM 53-20-05-2R PROC 1.Jan 15, 2020 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020011600322Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 30, STA 986 IS CORRODED. NRC 040-0008:5331-2001/001 00193: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM STA 965-1012 REF SRM 53-20-05-2R PROC 1.Jan 15, 2020 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2020010700089Doubler · damagedRAMP REPORTS DAMAGE AT AFT LOWER EDGE OF C1 CARGO DOOR. DAMAGE IS TO EXISTING DOUBLER EDGE. REMOVED, FABRICATED, AND DRILLED UP NEW DOUBLER AND TRIMED DAMAGE IAW B717 SRM 53-20-15-2R-5 OPTION 2. INSTALLED REPAIR DOUBLER PER B717 SRM 53-20-15 FIG 202 OPT. 2. ALJan 6, 2020 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 2019F00174Skin · delaminatedINB SPOILER HAS DELAMINATION BOTTON SURFACE. LARGE DELMINATION AREA.Mar 29, 2019 · N894AT · Boeing 717200 · SpoilersSDR DALA2018120306972Cover · missingHORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS - MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. ON WALK AROUND FOUND HORIZONTAL STAB BEARING COVER MISSING. DEFERRED ITEM. WILL NEED A SUPPLEMETAL SDR ONCE REAPIR IS COMPLETE. REPODec 2, 2018 · N894AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2018070404359Light · brokenFOUND EMERGENCY LIGHT L2-938 BROKEN AFT COMPARTMENT. REPLACED TERMINALS NEEDS LIGHT ASSY MOUNTED. MOUNTED LIGHT ASSY CKS GOOD.Jul 3, 2018 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2018030901588Latch · damagedTAIL CONE SLIDE COVER WAS FOUND NOT SECURE. REPLACED A DAMAGED LATCH ON THE SLIDE COVER IAW AMM 25-61-02 AND RIG SLIDE IAW TASK CARD 2561-9006.Mar 9, 2018 · N894AT · Boeing 717200 · Escape SlideSDR DALA2018030601404Frame · gougedGOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 RT SIDE APPROX RBL 4-6. NRC 001-0253:5300-2004/005 00214: 566363-14 REV 1 AND ER/A 566363-14 REV O MATCH WORK COMPLIED WITH PER ER/A 566363-14 REV O.Mar 6, 2018 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018030601403Frame · gougedGOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 LT SIDE APPROX LBL 4-7. NRC 001-0253:5300-2004/004 00213: PRI 566363-14 REV 1 AND ER/A 566363-14 REV O MATCH. WORK WAS PERFORMED PER ER/A 566363-14 REV O.Mar 6, 2018 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018030401383Bearing · looseRIGHT INBD SPOILER PANEL CENTER HINGE BEARING LOOSE IN BORE. THE SPOILER PANEL WAS REPLACED.Mar 3, 2018 · N894AT · Boeing 717200 · SpoilersSDR DALA2018021901529Lens · damagedEMERGENCY LIGHT LENS DAMAGED. REPLACED THE DAMAGED LENS.Feb 18, 2018 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2018030801530Bracket · damagedFOUND EMERGENCY LIGHT AT ESCAPE RAMP PANEL IN POOR CONDITION. REPLACED THE BRACKETS IAW SRM 51-40-02.Jul 28, 2017 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2017032802517Charger · inoperativeON SVC FOUND EMERG BATT PACK INOPERATIVE. R&R BATT CHARGER / BATT B5-235 REF AMM 33-51, WDM 33-51. CHECKS GOOD. OK FOR SVC.Mar 28, 2017 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2016040502626Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY SIDEWALL WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Apr 5, 2016 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2016040502568Cusp Web · corrodedRIGHT CUSP WEB BS 389-503 UPPER AND LOWER SURFACES, HAS SEVERAL AREAS OF CORROSION. INSTALLED NEW CUSP WEB IAW SRM 51-41-02, SRM 51-41-01 AND SRM 51-41-05.Apr 4, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016040502567Cusp Web · corrodedLEFT OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED THE CUSP WEB IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, REPAIR 4.Apr 4, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016032902390Spar · corrodedLEFT CENTER TANK UPPER REAR SPAR CORRODED AT XCW 13, 18, 52, & 59L. CORROSION ON UPPER CENTER TANK WAS REPAIRED IAW ER/A 543586-14, FASTENER HOLES DAMAGED COMMON TO CORROSION BLENDOUT AREA. WERE REPAIRED IAW PRI, REV 3, 543589-14 AND ER/A 543589-14, REV ORIGMar 28, 2016 · N894AT · Boeing 717200 · Wing SparSDR DALA2016032702329Skin · crackedBS 1087 ABOVE STRINGER 14R, SKIN HAS A 2 DIRECTIONAL CRACK, VERTICAL LEG .5" & HORIZONAL LEG .1250". HFEC VERIFIED IAW NDT SPM 06-10-01.001 REQUEST ENGINEERING DISPOSITION. REPAIRED CRACK AT BS 1087, 514R IAW ER/A 543584-14 ASSOCIATED ER/A 00-543584 ADDED Mar 26, 2016 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016032202228Skin · crackedBS 1022, STRINGER 14R, SKIN HAS A TWO INCH HORIZONTAL CRACK HFEC VERIFIED IAW NDT SPM 06-10-01.001 PROCEDURE 1. INSTALLED REPAIR IAW PRI 543585-14, REVISION 2, AND ER/A 543585-14 REV.Mar 21, 2016 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016030901764Skin · crackedBS 1133, 1.5" OTBD OF STR 2L HAS .1250 INCH SKIN CRACK AT SHEAR TIE FASTENER LOCATION. HFEC VERIFIED IAW NDTSPM 06-10-01, 001 PROCEDURE, 1 REF ORNRC 0300-0005. REMOVED CRACK FROM FUSELAGE SKIN AT BS 1133, OTBD OF STR 2L AND REPAIRED IAW EA 543582-14AD.Mar 7, 2016 · N894AT · Boeing 717200 · Fuselage Main, Plate/Skin
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