N799SW

Service difficulty reports · 334

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 = 'N799SW' 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 SWAA2020040126856Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241 FF L/H/S BOTTOM EDGE AREA OF BOARD HAS 2EA AREAS OF FOD INPREGINATION IN BOARD / PASSENGER CABIN FLOOR BARD #241 FF WAS REPLACED BY FABRICATING NEW FLOOR PANEL BOARD #241 FF REFERENCE NON ROUTINE CARD: Y174719Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126855Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241 FF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR BOARD #241FF I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0013 REV:- AND BAC 5085 REFeb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126854Floorboard · puncturedPASSENGER CABIN FLOOR BOARD # 242CF L/H/S EDGE BOTTOM SKIN PLIES FWD OF #1 INSERT IS PUNTURED AS MARKED / PASSENGER CABIN FLOOR BARD #242 CF WAS REPLACED BY FABRICATING NEW FLOOR PANEL BOARD #242 CF REFERENCE NON ROUTINE CARD: Y174716Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126853Floorboard · puncturedPASSENGER CABIN FLOOR BOARD # 242CF R/H/S EDGE BETWEEN INSERT #2 AND #3 TOP SKIN IS PUNTURED AS MARKED / PASSENGER CABIN FLOOR BARD #242 CF WAS REPLACED BY FABRICATING NEW FLOOR PANEL BOARD #242 CF REFERENCE NON ROUTINE CARD: Y174716Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126852Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 242CF TOP SKIN SURFACE THE LENGTH AND WIDTH OF BOARD SEVERAL AREAS SKIN FIBER DAMAGED / FABRICATED NEW FLOOR PANEL #241 DF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0009 REV:- AND BAC 5085 REVFeb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126850Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241DF TOP SKIN SURFACE R/H EDGE THE LENGTH OF BOARD SKIN FIBER DAMAGED / PASSENGER CABIN FLOOR BOARD #241 DF WAS REPLACED BY FABRICATING NEW FLOOR PANEL FEFERENCE NON ROUTINE CARD: Y174722Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126849Floor Panel · damagedPASSENGER CABIN FLOOR BOARD # 241CF TOP SKIN PLIES HAVE FIBER DAMAGE IN SEVERAL AREAS AS MARKED / REPAIRED PASSENGER CABIN FLOOR PANEL 241 CF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-20-2R-1 REPAIR 1 REV 69 A72547; A79470Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126848Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 231FF BOTTOM SKIN OF BOARD DAMAGED ON R/H EDGE 4 EA AREAS AS MARKED HAS SKIN PLIES WITH CORE BROKEN / REPAIRED PASSENGER CABIN FLOOR BOARD 231FF I/A/W SRM 53-00-50-2R-0 REV 69 AND 53-00-50-2R-1Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126847Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 231FF L/H EDGE OF BOARD AROUND #5 INSERT TOP SKIN OF BOARD SKIN PLIES ARE DAMAGED / REPAIRED DAMAGE TO PASSENGER CABIN FLOORBOARD 231FF I/A/W SRM 53-00-50-2R-1 REV 69 AND I/A/W SRM 53-00-50-2R-0 REV 69 A79470; A55972; A72547Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126846Floorboard · puncturedPASSENGER CABIN FLOOR BOARD # 231FF R/H EDGE OF BOARD AREA AROUND 9TH INSERT TOP SKIN PLIES ARE PUNTURED AND DAMAGED / REPAIRED DAMAGE TO PASSENGER CABIN FLOOR BOARD 231FF I/A/W SRM 53-00-50-2R-0 REV 69 AND I/A/W SRM 53-00-50-2R-1 REV 69Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020040126844Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 231FF AFT TOP SKIN AREA OF FLOOR BOARD WIDTH OF BOARD AS MARKED UPPER SKIN FIBERS ARE DAMAGED / REPAIRED DAMAGE ON PASSENGER CABIN FLOORBOARD 231FF IAW SRM 53-00-50-2R-0 REV 69 AND SRM 53-00-50-2R-1Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020030542158Floorboard · damagedAFT GALLEY/LAV WET AREA, FLOORBOARD 241ADF, HAS 3 AREAS MISSING INSERTS/PLUGS (EMPTY HOLES) . REPAIRED FLOOR PANEL 241 ADF AFT GALLEY / LAV WET AREA WITH PUNCTURES TOP/IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REP, REV 69 A7947Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2020030442127Floorboard · damagedAFT GALLEY/LAV WET AREA, FLOORBOARD 242UF, INSERT HAS PULLED THROUGH THE EDGE OF THE PANEL. REPAIRED EDGE AT PULLED THROUGH INSERT SURFACE WITH WET-LAY-UP REPAIR ON FLOORBOARD PANEL (242-UF) I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-N (REV 69).Feb 7, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2021081626808Shield · corrodedAFT CARGO COMPARTMENT R/H FWD SHIELD STR 25R STA 767 + 2' UPPER SURFACE CORRODED. / REMOVED CORROSION ON R/H FWD SHIELD; AFT CARGO COMP. STA 767+2' STR 25R. EVALUATED AT LOSS & FOUND ORIG 'T' .050' REMAINING .044' LOSS OF .006' FOUND TO BE OUT OF LIMITS REMOVEFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2021080526814Strip · corrodedAFT CARGO COMPARTMENT STA 887 FLOOR PANEL TRANSITION STRIP UPPER SURFACE CORRODED. / REMOVED AND REPLACED AFT CARGO COMPARTMENT STA 287 FLOOR PANEL TRANSITION STRIP. IAW B737-700 SRM 51-40-02-0G-0. AIPC 53-42-11-30 CORROSION OUT LIMITS DUE TO NO PUBLISHED LIMIFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020040126779Fitting · corrodedAFT CARGO COMPT. STA 727D+6; S-27R; WL150 THREE EACH CLIPS HAVE CORROSION / REMOVED AND REPLACED AFT CARGO COMPT. STA 727 D+6 S-27 R WL 150 3 EACH CLIPS WITH P/N 146A7734-1 AND 146A7734-2 IAW BOEING DWG 146A7730 REV B. DWG 146A7734 REV - AND SRM 51-40-02.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020040126780Fitting · corrodedAFT CARGO COMPT. STA 727D+6; S-27L; WL150 TWO EACH CLIPS HAVE CORROSION / REMOVED AND REPLACED AFT CARGO COMPT STA 727 D+6 S-27 L WL 150 2 EACH CLIPS WITH P/N 146A7734-1 AND 146A7734-2 IAW BOEING DWG 146A7734 REV A. DWG 146A7734 REV - AND SRM 51-40-02Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020040126802Skate Angle · wornVERTICAL STAB.RH FWD SKATE ANGLE AFT OF DORSAL FIN AREA WORN / REMOVED AND REPLACED FWD SKATE ANGLE RH SIDE PER SRM 51-40-02-0G-0 AND DWG 147A0030 REV BFeb 6, 2020 · N799SW · Boeing 7377Q8 · Vertical Stabilizer Miscellaneous StructureSDR SWAA2020040126803Skate Angle · wornVERTICAL STAB.RH AFT SKATE ANGLE WORN FWD AND AFT OF VERTICAL STAB; ATTACH POINTS / REMOVED AND REPLACED RH AFT SKATE ANGLE PART # 148A8310-4 PER SRM 51-40-02-0G-0 AND DWG 148A8300 REV CFeb 6, 2020 · N799SW · Boeing 7377Q8 · Vertical Stabilizer Miscellaneous StructureSDR SWAA2020040126804Skate Angle · wornVERTICAL STAB.LH AFT SKATE ANGLE WORN AFT OF VERTICAL STAB; ATTACH POINTS / REMOVED AND REPLACED RH AFT SKATE ANGLE PART # 148A8310-3 PER SRM 51-40-02-0G-0 AND DWG 148A8300 REV CFeb 6, 2020 · N799SW · Boeing 7377Q8 · Vertical Stabilizer Miscellaneous StructureSDR SWAA2020040126817Stiffener · crackedBS 663; VAPOR BARRIER WEB; HORIZONTAL STIFFENER; LBL 6 TO LBL 30; P/N 111A1301-5; CRACKED. / LOCATED AND DRILLED NEW STIFFNER PART # 111A1301-5 PER DWG 111A1001 REV - AND SRM 51-40-05-0G-0. -5 STIFFNER REMOVED AND REPLACED ON CARD NO. Y174343Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020040126832Seat Track · corrodedSTA.706 + 10' TO STA. 727 + 10' LBL45 SEAT TRACK CORROSION UPPER CROWN AND LOWER CHANNEL. / REMOVED CORROSION FROM SEAT TRACK UPPER AND LOWER SURFACES IAW B737-700 SRM 51-10-02-0G-0 PARA 6 A EVALUATED MATERIAL LOSS OF .044' ALLOWED .040' FOUND OUT OF LIMITS IAFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020040126837Seat Track · wornLH. INBD SEAT TRACK STA. 638 - 639 UPPER LOCK LUG WORN / REMOVED DAMAGE FROM L/H INB SEAT TRACK STA 638-639 UPPER LUG IAW SRM 53-00-52-1A-1; EVALUATED MATERIAL LOSS OF .025' ALLOWED .020' FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1 USING TOOL # 21461 DUE 08/01/2Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020040126836Seat Track · wornLH. OTBD. SEAT TRACK STA. 638 - 639 UPPER LOCK LUG WORN / REMOVED WORN SEAT TRACK LBL 45 STA 727 B-630 IAW SRM 737-700 51-40-02-0G-0 VERIFIED NEW SEAT TRACK IAW DWG 25220030 REV A PART# BAC 1520-2779 AND SRM 53-00-52-2R-3 ATAG# A29391; LOCATED AND DRILLED HOLEFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020040126769Cargo Track · gougedAFT CARGO COMPT. STA 727+9; LBL 3 RAIL IS GOUGED / AFT CARGO COMPARTMENT RAIL LBL 3 WL 155 BS 727-727B & 4'. REMOVED DAMAGE RAIL; ORIGINAL .071' LOSS .015'; REMAINING MATERIAL .056' OUT OF LIMITS IAW 53-00-53-1A-2. FABRICATED NEW RAIL; AND INSTALLED NEW RAIL IFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020032442802Attach Angle · crackedLT MAIN WHEEL WELL, BS 663, UPPER VAPOR BARRIER ATTACHMENT CHORD CRACKED AT LBL 7. REPAIRED LT MAIN WHEEL WELL, BS 663, UPPER VAPOR BARRIER ATTAH ANGLE AT LBL 7 IAW EA# 200122 REV. IR AND SWA EA# 1-757-16837 REV. IR.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020031142355Stringer Clip · corrodedAFT CARGO COMPT. STA 767, S-26R, WL150 STRINGER CLIP HAS CORROSION REMOVED CORROSION FROM AFT CARGO COMPT STRINGER CLIP AT STA 767 S-26R WL 150 AND VERIFIED WITH 10X MAGNIFYING GLASS - NO DEFECTS NOTED IAW SRM 51-10-02-0G-0 NO PUBLISHED LIMITS FOR STRIFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020030942290Crease Beam · corrodedAFT PASSENGER CABIN STA 967 + 17" RBL 56 R/H CREASE BEAM HAS SURFACE CORROSION. REMOVED & REPLACED CREASE BEAM IAW DWG 147A8501 & B737-700 SRM 51-40-02-0G-0. (P/N 147A854048 ATAG WN7140) DWG 147A8501-REV- DWG 147A8540-REV- DWG 147A0000 REV AFeb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, StructureSDR SWAA2020022841979Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 767, STR. 26L. / R&R STRINGER CLIP IAW DWG AND SRM.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020022841768Cargo Track · corrodedAFT CARGO COMPARTMENT RAIL SPLICE CHANNEL HAD CORROSION AT BS. 727+10, LBL 3. / R&R SPLICE IAW SRM.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020022874834Angle · corrodedAFT CARGO COMPARTMENT R/H "Z" ANGLE CORRODED BETWEEN BS. 887 TO BS. 927, STR. 25R UPPER SURFACE. / R&R "Z" ANGLE IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020021941535Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 827, STR. 27L. / R&R STRINGER CLIP IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020021941532Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 787, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020021941531Angle · corrodedAFT CARGO COMPARTMENT Z-ANGLE HAD CORROSION UPPER SURFACE BETWEEN BS. 727 TO BS. 767, RBL 21. / R&R Z-ANGLE PER SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020021941530Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 747, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020021941464Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 807, STR. 26L. / R&R STRINGER CLIP IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020021941463Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 747, STR. 26L. / R&R STRINGER CLIP IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020021941462Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 727E, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2020021941461Stringer Clip · corrodedAFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 727D, STR. 26R. / R&R STRINGER CLIP IAW SRM AND DWG.Feb 6, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Attach FittingsSDR SWAA2021082726755Balance Weight · corrodedLEFT WING AILERON NOSE FITTING BAY #5; 5EA. BALANCE WEIGHTS SHOW SIGNS OF CORROSION. / REMOVED AND REPLACED (4EA) #2 AILERON #5 BAY WEIGHTS I/A/W B737 AMM 27-11-31-400-801 WN8522Feb 5, 2020 · N799SW · Boeing 7377Q8 · AileronsSDR SWAA2021081626739Isolator · brokenAFT GALLEY DOOR PANEL 844DZ BOTTOM AFT ISOLATOR BROKEN / REMOVED BROKEN ISOLATER AFT GALLEY DOOR PANEL 844DZ BOTTOM AFT. REPLACED ISOLATOR IAW AIPC 52-41-00-07 AND SRM 51-40-02-0G-0 ATAG-A74860Feb 5, 2020 · N799SW · Boeing 7377Q8 · Galley DoorsSDR SWAA2021080526733Cargo Track · corrodedAFT CARGO COMPARTMENT AT DOOR AFT FLOOR PANEL SPLICE/TIE DOWN CORRODED. / ON AFT CARGO COMPARTMENT AT DOOR AFT FLOOR PANEL SLICE / TIE DOWN REPLACED FOR NEW PART P/N 453A2611-2 A TAG # A55090 IAW B 737-700 AIPC 25-52-10-02 ITEM 75Feb 5, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2021072926727Panel · corrodedVERTICAL STABILIZER PANEL 324ML HAS CORROSION ON BOTH SIDES OF PANEL / REMOVED CORROSION FROM VERTICAL STABILIZER PNL #324 ORIG 'T' 0.050'; LOSS 0.004'; REMAIN 0.046' FOUND OUT OF LIMITS DUE NO ALLOWABLE DAMAGE FOUND. VERIFIED MATERIAL (20-24-73 0.050'); LOCATFeb 5, 2020 · N799SW · Boeing 7377Q8 · Vertical Stabilizer, Plate/SkinSDR SWAA2020040126750Web · puncturedAFT WET AREA FLOOR STRUCTURE STA 1016 + 12' RBL 4 WL 208 WEB PUNCTURED. / REMOVED & REPLACED PUNCTURED WEB 147A5744-7 IN AFT WET AREA STA 1016+12 RBL4 WL 208 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; B-DWG 147A5744 REV B; 147A5730 REV AFeb 5, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020031742537Floorbeam · corrodedTOP OF FLOOR BEAM STA 987 RBL 37 WL 208 CORROSION FOUND ON EXISITING T CAP REPAIR. REMOVED EXISTING T-CAP REPAIR FROM TOP OF FLOOR BEAM STA 987 RBL 37 WL 208. VERIFIED REPAIR PARTS IAW BAC1490-2811, ATAG A06033 & BAC1490-2887, ATAG A47859, ATAG 09055 &Feb 5, 2020 · N799SW · Boeing 7377Q8 · Fuselage Main, Floor BeamSDR SWAA2020021241355Rib · crackedVERTICAL STABILIZER LEADING EDGE STA. 278.8 RIB CRACKED. / R&R RIB IAW SRM AND DWG.Feb 5, 2020 · N799SW · Boeing 7377Q8 · Vertical Stabilizer, Spar/RibSDR SWAA2020021241354Rib · crackedVERTICAL STABILIZER LEADING EDGE STA. 288.2 RIB CRACKED. / R&R RIB IAW SRM AND DWG.Feb 5, 2020 · N799SW · Boeing 7377Q8 · Vertical Stabilizer, Spar/RibSDR SWAA2021080526717Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL # 140CF EDGES CORRODED. / ON AFT CARGO COMPARTMENT FLOOR PANEL # 140 CF IS REPLACEDFOR NEW PANEL P/N 4532610-18 TAG # WN5166 IAW B 737 AIPC 25-52-10-02 ITEM 160 (PART ON RACK)Feb 4, 2020 · N799SW · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2021071585017Support Angle · bentBS695 RBL 15.0 ANGLE SUPPORT HAS ONE CORNER BENT. ABOVE WHEEL WELL. / ANGLE SUPPORT COLD STRAIGHTENED IAW 8.6.3.BAC5300-2 PG. 33. SUPPORT ANGLE REMOVED AND REINSTALLED IAW B-737 SRM 51-40-02-0G-0. AT BS 695' RBL 15' ABOVE WHEEL WELL. RESTORED FINISHES IAW B-73Feb 4, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2020022841757Gusset · crackedFORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM & DWG.Feb 4, 2020 · N799SW · Boeing 7377Q8 · Fuselage Miscellaneous Structure
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