N216WR

Service difficulty reports · 301

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 = 'N216WR' 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 SWAA2022032168784Support · corrodedACB RH FLOOR TO SIDEWALL SUPPORT CORRODED. RBL21; BS727D+8'; BS727D+10.5'; BS727D+15'; BS727D+18.5'; BS727D+19'; BS727E+2.5' BS727E+6.5'; BS727E+10.75'; BS727E+14'; BS727E+17.5' / [01] REMOVED CORROSION ON ABC RH FLOOR TO SIDEWALL SUPPORT ; RBL 21; WORK AREAS Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168783Support · corrodedACB RH FLOOR TO SIDEWALL SUPPORT CORRODED. RBL21; BS727+8'; BS727+11.5'; BS727A+2'; BS727A+10.75'; BS727B+6.5'; BS727B+10.5'; BS727C; BS727C+2.5'; BS727C+6.5'; BS727D+6.25' / [01] REMOVED CORROSION ON ACB RH FLOOR TO SIDEWALL SUPPORT ; WORK AREAS BS 727+8; L 1Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168792Intercostal · corrodedACB INTERCOSTAL BETWEEN BS747 & BS767 CORRODED. RBL21.5; BS747+6.5'; BS747+10.5'; BS747+14'; BS747+18'; BS747+19' / [01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM FOR BS747 - 767 RBL 21.5; PART TO BE REPAIRED BY REPLACMENT PER SRM 51-10-02-0G-0;[02] NO ALLOWABLEFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168787Support · corrodedACB LH FLOOR TO SIDEWALL SUPPORT CORRODED. LBL 21; BS727+11.5'; BS727A+2.5'; BS727B+2.5'; BS727B+18.5'; BS727C+2.5'; BS727C+14'; BS727D+3'; BS727D+8'; BS727D+15.5'; BS727D+18.5'; / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;09] FABRICATED ACB L/H NEW FLOFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168788Support · corrodedACB LH FLOOR TO SIDEWALL SUPPORT CORRODED. LBL 21; BS727E+2.5'; BS727E+10.5'; BS727E+14.5; BS727E+18'; BS747+2.5'; BS747+6'; BS747+10' TO BS747+17'; BS747+18.5'; BS747+18.75'; BS767 / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] EVALUATED CORROSION ONFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168789Support · corrodedACB LH FLOOR TO SIDEWALL SUPPORT CORRODED. LBL 21; BS767+3.5'; BS767+4'; BS767+4.75'; BS767+14.5'; BS767+18.'; BS787+3.5'; BS787+6.5'; BS787+10.5'; BS787+18.5' / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] EVALUATED CORROSION ON ACB LH FLOOR TO SIDEWFeb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168790Support · corrodedACB LH FLOOR TO SIDEWALL SUPPORT CORRODED. LBL 21; BS827+2.5'; BS827+3.5'; BS827+17' TO BS827+19' / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] EVALUATED CORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT LBL 21 AT ; BS 827+2.5 L=1'XW=.2'XD=.002'; BS 827+Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168806Rail · corrodedACB FLOOR RAIL CORRODED AT BS767+5' LBL3. / [01] REMOVED CORROSION ON ACB FLOOR RAIL AT BS 767+5 LBL3 IN AREA OF L=1' X W=3' D=.007' REMAINING THICKNESS =.056' FROM ORIGINAL THICKNESS .063' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-01-2; SRM 53-00-53-1A-2 B (Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032168807Rail · corrodedACB FLOOR RAIL CORRODED AT BS767+5' LBL12.50 / [01] REMOVED CORROSION ON ACB FLOOR RAIL AT BS 767+5 LBL 12.50 IN AREA OF L=1' X W=3' D=.008' REMAINING THICKNESS =.055' FROM ORIGINAL THICKNESS .063' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-01-2; SRM 53-00-53-Feb 4, 2022 · N216WR · Boeing 737* · Fuselage Main, Floor BeamSDR SWAA2022032167039Angle · cracked(LEFT WING) T/E COVE SEAL SUPPORT ANGLE CRACKED AT LOWER ATTACH POINT ON TRANSVERSE WEB RSS273 / [01] REMOVED AND REPLACED L/W T/E COVE SEAL SUPPORT ANGLE COMMON TO TRANSVERSE WEB IAW SRM 51-40-02-0G-0 STEP 4;[02] INSPECTION COMPLETEFeb 3, 2022 · N216WR · Boeing 737* · Wing Main, Frame StructureSDR SWAA2022032167659Bracket · crackedPNEUMATIC DUCT CLAMP SUPPORT BRACKET IS CRACKED AT B.S. 540+6; R.B.L. 6; W.L. 160. / [01] REMOVED DAMAGED PNEUMATIC DUCT CLAMP SUPPORT BRACKET AT B.S. 540+6; R.B.L. 6; W.L. 160. AND REPAIRED BY REPLACEMENT IAW SRM 51-40-02-0G-0;[02] REJECTION OF ACTION 1. FWD Feb 3, 2022 · N216WR · Boeing 737* · Fuselage Main, Attach FittingsSDR SWAA2022032167661Panel · chafedWING TO BODY FAIRING PANEL 192F HAS CHAFE DAMAGE ALONG AFT EDGE. / [01] IDENTIFIED PANEL 192F IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 15. UPON INSPECTION OF PANEL FOUND CHAFING DAMAGE TO FWD EDGE; AND 1EA MOUNTING CUT OUT 15' FROM FWD EDGE ON L/Feb 3, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032167645Angle · crackedCRACKED ATTACH ANGLE AT MID PASSENGER CABIN ABOVE PRESSURE DECK BS691 RBL1 WL206. / [01] RECEIVED HEAT TREATED BACKET FROM OSS JOB # 541207 LOCATED AND DRILLED ; TRIMMED TO SIZE AND DEBURRED PER SRM 51-40-05 AND DWWG # 273A9112 REV-;[02] PRIOR TO STEP 1. REMOVFeb 2, 2022 · N216WR · Boeing 737* · Wing Miscellaneous StructureSDR SWAA2022032167650Support · crackedCRACKED FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 RBL1 WL208. / [01] REMOVED AND REPLACED FLOOR SUPPORT ON STA 540 RBL 1 WL 208 IAW DWG 143A0060 AND SRM 51-40-02-0G-0.;[02] EDITED TO REQUIRE PROPER CO SIGN.;[03] VERIFIED;[04] VERIFIED CORRECTIVE ACTION ENTIFeb 2, 2022 · N216WR · Boeing 737* · Wing Main, Frame StructureSDR SWAA2022032167651Support · crackedCRACKED FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 LBL1 WL208. / [01] REMOVED AND REPLACED FLOOR SUPPORT ON STA 540 LBL 1 WL 208 IAW DWG 143A0060 AND SRM 51-40-02-0G-0.;[02] CORRECTED SPELLING ERROR IN MEASUREMENT CHART;[03] VERIFIED;[04] VERIFIED CORRECTIVEFeb 2, 2022 · N216WR · Boeing 737* · Wing, Center BoxSDR SWAA2022032167643Strap · corrodedCORROSION ON STRAP AT MID PASSENGER CABIN BS720 RBL66. MARKED. / [01] REMOVED CORROSION ON PRESSURE DECK SUPPORT ANGLE AT BS 720 RBL66 WL202 IN A 1/2'X1.'X.004' AREA IAW SRM 51-10-02-0G-0. SRM DOES NOT HAVE PRESSURE DECK ALLOWABLE DAMAGE LIMITS FOR SUPPORT ANGFeb 2, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032167640Scuff Plate · crackedFWD CARGO DOOR; FWD SCUFF PLATE IS CRACKED / [01] WELDED CRACK ON FCD; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID: E10583 S/N; KJ256554;[02] VERIFIED CORRECTIVE ACTION 1;[03]Feb 1, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032167641Scuff Plate · crackedFWD CARGO DOOR; AFT SCUFF PLATE IS CRACKED / [01] WELDED CRACK ON FCD; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID: E10583 S/N; KJ256554;[02] VERIFIED CORRECTIVE ACTION 1.;[03Feb 1, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032166500Scuff Plate · crackedFWD CARGO DOOR; AFT SCUFF PLATE IS CRACKED ; / WELDED CRACK ON FCD, AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4) WELDING MACHINE CAL ID: E10583 S/N; KJ256554Feb 1, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032166499Scuff Plate · crackedFWD CARGO DOOR; FWD SCUFF PLATE IS CRACKED ; / WELDED CRACK ON FCD, FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT# 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4) WELDING MACHINE CAL ID: E10583 S/N; KJ256554Feb 1, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032167606Rib · crackedRT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) HAS CRACK AT STIFFENER #2 LOWER RADIUS. / REMOVED DAMAGED AT RT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) STIFFENER #2 LOWER RADIUS. IAW B737 SRM 55-10-09-2R-5.;[02] VERIFIED CORRECTIVE ACTION 1CUT AND REMOVEDJan 31, 2022 · N216WR · Boeing 737* · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2022032167607Stiffener · crackedRT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) HAS CRACK AT STIFFENER #3 LOWER RADIUS. / [01] VERIFIED APPLICABILITY OF REPAIR MANUAL SRM 55-10-09-2R-5. <BR>REMOVED DAMAGED AT RT HORIZONTAL STABILIZER RIB 4 (STAB STA120.30) STIFFENER #3 LOWER RADIUS. IAW B737Jan 31, 2022 · N216WR · Boeing 737* · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2022032065932Seat Track · corrodedSEAT TRACK HAS CORROSION AND MECHANICAL DAMAGE IN WELL AND CROWN; RBL25; BS518-520; BS500C+7 TO 500D; BS500B-1 TO 500B+10; BS500+6 TO +18; BS476-485 / [01] REMOVED CORROSION AND MECHANICAL DAMAGE FROM WELL AND CROWN OF SEAT TRACK; RBL25; BS476 - BS520 IAW SRM Jan 31, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032065933Seat Track · corrodedSEAT TRACK HAS CORROSION AND MECHANICAL DAMAGE IN WELL AND CROWN; RBL45; BS518-520; BS500C+7 TO 500D; BS500B-1 TO 500B+10; BS500+6 TO 500+18; BS483-485 / [01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1<BR>REMOVED CORROSION AND MECHANICAL DAMAGE FROM SEAT TRAJan 31, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032066075Seat Track · corrodedSEAT TRACK CORROSION AND MECHANICAL DAMAGE IN WELL AND CROWN; LBL25; BS540-552; BS569-582; BS590-614; BS634-646; BS663-675; BS690-709; BS727-727+11; / [01] VERIFY APPLICABILITY FOR SRM 53-00-52-1A-1.<BR>REMOVED MECHANICAL DAMAGE AND CORROSION FROM SEAT TRACK WJan 31, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032165929Seat Track · corrodedSEAT TRACK HAS CORROSION AND MECHANICAL DAMAGE IN WELL AND CROWN; RBL25; BS860-870; BS827-842; BS800-807; BS867-877; BS737-748; BS727D-2 TO 727D+8; BS727B+6 TO 727C; / [01] VERIFY APPLICABILITY FOR SRM 53-00-52-1A-1.[11] INSTALLED NEW PASSENGER CABIN SEAT TRACJan 31, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032071830Panel · crackedPANEL 211A FWD UPPER CORNER CRACKED / [01] APPLIED FIBERGLASS REPAIR TO THE INNER SURFACE OF THE CRACKED CORNER IAW CMM 25-00-66 REPAIR 3-1 PAGES 603-604 STEP 4.C.(1).;[02] REPAIRED OUTER OF PANEL AT THE REPAIRED CORNER IAW CMM 25-00-66 REPAIR 3-1 PAGE 604 STEJan 29, 2022 · N216WR · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022032164845Skin · crackedCRACK ON R/H WING L/E SLAT NOSE SKIN LOWER SURFACE AT #5 SLAT STATION 85.19.(MARKED) / [01] REQUEST NDT VERIFICATION CRACK CONDITION EXIST;[11] INSTALLED REPAIR PARTS IAW SRM 57-42-01-2R-8; PARA. 4. AND FIG.202.;[12] INSPECTED ACTION 11;[13] OK YO REINSTALL SLJan 27, 2022 · N216WR · Boeing 737* · Leading Edge DevicesSDR SWAA2022032164846Skin · crackedCRACK ON R/H WING L/E SLAT NOSE SKIN LOWER SURFACE AT #8 SLAT STATION 451.97.(MARKED) / [01] REQUEST NDT VERIFICATION CRACK CONDITION EXIST[14] INSTALLED COUNTERSINK FILLERS IN SLAT NOSE SKIN IAW SRM 57-42-01-2R-8 PARA. 4. OK TO INSTALL REPAIR PARTS.;[15] INSPJan 27, 2022 · N216WR · Boeing 737* · Leading Edge DevicesSDR SWAA2022032164847Skin · crackedCRACK ON L/H WING L/E SLAT NOSE SKIN LOWER SURFACE AT #2 SLAT STATION 202.45.(MARKED) / [01] REQUEST NDT VERIFICATION CRACK CONDITION EXIST[11] COMPLETED REPAIR PARTS FABRICATION. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND BARE AREAS OFJan 27, 2022 · N216WR · Boeing 737* · Leading Edge DevicesSDR SWAA2020071398786Lens · missingFWD SERVICE & ENTRY DOOR LOWER EMER EXIT LENS MISSING DIRECTIONAL ARROW. REMOVED AND REPLACED BOTH FWD SERVICE & ENTRY DOOR LOWER EMER EXIT LENS IAW 33-51-01.Jul 9, 2020 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2020063095648Flap · delaminatedRIGHT WING O/B AFT FLAP - I/B UPPER AFT CORNER DELAMINATED. MOD / INSPECTED R/W O/B AFT FLAP ON THE I/B UPPER AFT CORNER AND FOUND .5 INCH X .5 INCH DELAM IN ZONE 1. APPLIED ALUMINUM FOIL TAPE TO DELAM AREA PER SRM 57-53-01-1A-4. INSPECT DELAMINATED AREA ANJun 26, 2020 · N216WR · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2020061091054Light · inoperativeEMERGENCY LIGHT AFT OF LEFT WING INOP. RELAMPED EMERGENCY LIGHT AFT OF LEFT WING IAW MM 33-51-04. OPS CHECK GOOD.Jun 10, 2020 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2020033034449Charger · inoperativeAFT EMER LIGHT INOP / REPLACED CHARGER AND BATTERY PACK PER 33-51-06 OF THE AMMMar 26, 2020 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2020032442641Cover · damagedAFT FLIGHT ATTENDANT EMERGENCY LIGHT BUTTON COVER DAMAGED. REMOVED AND REPLACED PER SIPMar 18, 2020 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2020020441062Battery Pack · inoperativeFORWARD RH EMERGENCY LIGHT BATTERY PACK INOPERATIVE. / R&R BATTERY PACK PER AMM.Feb 3, 2020 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2019110438483Lens · looseAFT GALLEY EMERGENCY EXIT LENS LOOSE. / SECURED LIGHT ASSEMBLY PER MM.Nov 3, 2019 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2022030705301Panel · elongated193B PANEL HOLES ARE ELONGATED AT THIS LOCATIONS 3 ;4; 5; 6; & 33 THUR 38 AND 14 THRU 22 MOD / R/R PNL 193B PER AMM 53-51-21. DRILLED; COUNTER SINK AND TRIMED TO FIT PNL 193B PR SRM 51-20-07-06-0; 51-040-08 86275Apr 21, 2019 · N216WR · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2019041231625Power Supply · inoperativeL/H OVERWING EMERGENCY LIGHT BATTERY PACK INOP AT M1668. / R&R POWER SUPPLY PER AMM.Apr 12, 2019 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2022030705492Splice Strap · corrodedFLOOR BOARD SPLICE STRAP AT STA 767 +5 HAS CORROSION IN AND AROUND FASTENER HOLES / WP:E51496-NGUYEN; THANH C - 04/11/2019 09:26 COMPLETE: REMOVED AND REPLACED FLOOR BOARD SPLICE STRAP ( P/N # 146A9401-4 ) AT STA 767 +5 PER SRM 51-40-02 .Apr 11, 2019 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022030705493Splice Strap · corrodedFLOOR BOARD SPLICE STRAP AT STA 727 D+5 HAS CORROSION IN AND AROUND FASTENER HOLES / REMOVED AND REPLACED FLOOR BOARD SPLICE STRAP ( P/N # 146A9401-8 ) AT STA 727 +5 PER SRM 51-40-02 .Apr 11, 2019 · N216WR · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2019041231626Housing · damagedL/H EXTERNAL EMERGENCY LIGHT HOUSING JUST AFT OF OVERWING EXIT DAMAGED. / R&R LIGHT ASSEMBLY PER AMM.Apr 11, 2019 · N216WR · Boeing 7377H4 · Emergency LightingSDR SWAA2022030705480Angle · corrodedAFT CARGO COMPARTMENT STA 787 RIGHT TRANSITION ANGLE HAS CORROSION MARKED FWD OF CARGO DOOR / E72995-OTTO; PERRY - 04/07/2019 21:42 COMPLETE: REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE STA 787 IAW SRM 51-10-02; INSTALLED FASTENERS IAW SRM 51-40-02.Apr 7, 2019 · N216WR · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2019040831421Rib · crackedL/H HORIZONTAL STABILIZER CRACKED ON RIB AT 2ND VERTICAL STIFFENER FROM FRONT EDGE AT STAB. STA. 120.3. / REPAIRED RIB IAW SRM.Apr 4, 2019 · N216WR · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2019040831420Rib · crackedL/H HORIZONTAL STABILIZER CRACKED ON RIB AT 3RD VERTICAL STIFFENER FROM FRONT EDGE AT STAB. STA. 120.3. / REPAIRED RIB IAW SRM.Apr 4, 2019 · N216WR · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022030705462Skin · crackedRH WING FIXED L/E SKIN JUST INBD OF ENGINE PYLON #2 FASTENER HOLE IN ZONE 1 HAS A CRACK INDICATION IN COUNTERSINK PER NDT PART 6 53-30-05 / REPAIRED CRACK PER EA 1-757-16135 AND SRM 57-41-01-2R-7 REPAIR 7.Apr 3, 2019 · N216WR · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2022030705458Bracket · crackedR/H WING I/BD T/E SHELF PANEL FWD SIDE BRACKET CRACKED (MARKED) / REMOVED AND REPLACED BRACKET PER SRM 51-40-02Apr 2, 2019 · N216WR · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022030405442Skin · bentAFT CARGO DOOR FUSELAGE CUT OUT; FWD EDGE; FUSELAGE SKIN BENT AND DEFORMED IN TWO PLACES APPROXIMATELY 19' FROM LOWER EDGE OF CUT OUT JUST ABOVE LAP SEAM / REPAIRED IAW EA 1-753-34531.Mar 28, 2019 · N216WR · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022030405443Skin · gougedAFT CARGO DOOR FUSELAGE CUT OUT; FWD EDGE; FUSELAGE SKIN BENT AND GOUGED WITH MATERIAL MISSING IN TWO PLACES ON INNER SURFACE APPROXIMATELY 19' FROM LOWER EDGE OF CUT OUT JUST ABOVE LAP SEAM / REPAIRED IAW EA 1-753-34531.Mar 28, 2019 · N216WR · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA1939030131166Skin · damagedFUSELAGE SKIN CREASED BETWEEN BS 325 TO BS 340, BETWEEN STR 20R TO STR 21R. REPAIRED SKIN PER SRM.Mar 26, 2019 · N216WR · Boeing 7377H4 · Fuselage Main, Plate/Skin
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