JASC 5312

Service difficulty reports · 20,045

Reports filed under 5312 · Fuselage Main, Bulkhead, 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 jasc_code = '5312'
  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 SWAA2020120730692Bulkhead Web · crackedLT STA 663 VAPOR BARRIER CRACKED 2 PLS AT LBL 45. REPAIRED DAMAGED AREA AT LT VAPOR BARRIER, PER B737-700 SRM 51-70-04-2R-0. MATERIAL USED RESIN EY3804 P/N 1691080 FIBERGLASS P/N 1694548. TOUCHED UP AS REQUIRED, REF B737-700 AMM 51-21-73-370-803.Nov 16, 2020 · N7741C · Boeing 7377BDSDR REXA2020111800780Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS 3 CHAFED AREAS AT WL 103 RBL 36.20, RBL 27.50, AND RBL 18.00 .200 LONG BY .200 WIDE .003 DEEP. REPAIRED 3 CHAFED AREAS OF REAR PRESSURE BULKHEAD WEB AT WL 103 RBL 36.20, RBL 27.50 AND RBL 18.00, IAW REO 601R-53-61-21-55 RENov 16, 2020 · N8839E · Cndair CL6002B19SDR SWIA202054505Isolator · gougedFS 621 PRESSURE BULKHEAD FORWARD SIDE HAS THE TOP ISOLATOR BRACKET AT RBL 18 WITH 2 GOUGES IN RADIUS. C-CHECK RO 12/04/2020. REMOVED DAMAGED ISOLATOR BRACKET, FABRICATED A NEW BRACKET AND INSTALLED, IAW BOMBARDIER REO.Nov 15, 2020 · N951SW · Cndair CL6002B19SDR SWIA202054504Isolator · brokenFORWARD SIDE OF FS 621 PRESSURE BULKHEAD HAS TWO BROKEN ISOLATORS. 1 RBL 27 BOTTOM, 1 RBL 45 BOTTOM. C-CHECK RO 12/04/2020. REMOVED TWO EACH DAMAGED ISOLATOR MOUNTS INSTALL NEW, IAW CRJ200 SRM.Nov 15, 2020 · N951SW · Cndair CL6002B19SDR SWIA202054503Pressure Blkhd · chafedFORWARD SIDE OF FS 621 PRESSURE BULKHEAD HAS A CHAFED RIVET AT WL 86.5, RBL 18. C-CHECK RO 12/04/2020. REPLACED CHAFE RIVETS AT FS 621 BULKHEAD AT WL 86.5 RBL 18 UPON FURTHER INVESTIGATION FOUND AND REPLACED 5 EA CHAFE RIVETS ON 621 BULKHEAD, IAW CRJ200 SRM.Nov 15, 2020 · N951SW · Cndair CL6002B19SDR A6WA202102147630Pressure Blkhd · crackedCRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT RBL 18.00 36 INCHES ABOVE FLOOR AND ON LBL 36.20 6 INCHES ABOVE FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DAMAGE AREAS ON AFT PRESSURE BULKHEAD AT RBL 18.00, 36 INCHES ABOVE FLOOR LEVEL ANov 13, 2020 · N454AW · Cndair CL6002B19SDR SWIA202054983Bulkhead · corroded67.5% REAR SPAR BULKHEAD AND SUPPORT ANGLE CORRODED AT BL 0 LOWER POSITION. C-CHECK RO 12/30/2020. REPAIRED IAW REO. MAJOR REPAIR TASK CARD & FORM M337 COMLETED AND ATTACHED. WEIGHT CHANGE AS NOTED ON CONTINUE CARD.Nov 13, 2020 · N924SW · Cndair CL6002B19SDR A6WA202011167420Bulkhead Web · crackedCRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT FS 621 LBL 36.2, 6" ABOVE THE FLOOR LINE. AIRCRAFT REMOVED FROM SERVICE. CRACK REPAIRED AT FS 621 LBL 36.2, 6" ABOVE THE FLOOR LINE, IAW REO 601R-53-61-1285.Nov 13, 2020 · N454AW · Cndair CL6002B19SDR SWIA202055041Bulkhead Web · corrodedAT 280 BULKHEAD ON LEFT HAND SIDE OF ENTRANCE TO FLIGHT DECK AT STR 2L (TOP), FOUND BRACKET TO BE HEAVILY CORRODED, MARKED WITH ORANGE TAPE. C-CHECK RO 12/30/2020. REMOVED AND REPLACED NEW ANGLE PN NR 600-34017-569 & ANLGE DOUBLER PLATE 600-34017-567, IAW CRNov 12, 2020 · N924SW · Cndair CL6002B19SDR SWIA202054828Bulkhead Web · crackedLT FS 280 BULKHEAD LOWER WEB STRUCTURE HAS A CRACKED ANGLE STIFFENER AT LBL 26. C-CHECK RO 12/26/2020. REMOVED AND REPLACED LT FS 280 BULKHEAD LOWER WEB STIFFENER AT LBL 26 WITH NEW, LOCATED AND DRILLED NEW STIFFENER, REF CRJ 900 SRM.Nov 12, 2020 · N802SK · Cndair CL6002D24SDR A6WA202011137417Bulkhead Web · crackedCRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT RBL 18 36" ABOVE FLOOR LEVEL FS 621. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DAMAGE ON AFT PRESSURE BULKHEAD AT RBL 18 FS 621 36" ABOVE FLOOR LEVEL, IAW BOMBARDIER REO 601R-53-61-1285 REV D.Nov 12, 2020 · N454AW · Cndair CL6002B19SDR SWIA202054812Bulkhead Web · corrodedRT FS 280 LOWER BULKHEAD WEB HAS CORROSION. C-CHECK RO 12/26/2020. REMOVED CORRODED RT FS 280 LOWER BULKHEAD WEB AND REPLACED WITH NEW, REFERENCING CRJ 900 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.Nov 11, 2020 · N802SK · Cndair CL6002D24SDR SWIA202054811Bulkhead Web · corrodedLT FS 280 LOWER BULKHEAD WEB HAS CORROSION. C-CHECK RO 12/26/2020. REMOVED CORRODED LT FS 280 LOWER BULKHEAD WEB AND REPLACED WITH NEW, REFERENCING CRJ 900 SRM. COMPLIED WITH SKYWEST TASK CARD. COMPLETED SKYWEST FORM M-337.Nov 11, 2020 · N802SK · Cndair CL6002D24SDR SWIA202054342Rivet · gougedFS 621 BULKHEAD FWD SIDE HAS 4 GOUGES RIVET HEADS AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW FASTENERS ON FWD SIDE OF FS 621 BULKHEAD AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36Nov 9, 2020 · N907SW · Cndair CL6002B19SDR SWIA202054341Isolator · looseFS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS LOOSE, MARKED. C-CHECK RO 11/23/2020. REPLACED 6 EA SOLID RIVETS ON FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS, REF CRJ200 SRM.Nov 9, 2020 · N907SW · Cndair CL6002B19SDR SWIA202054340Isolator · bentFS 621 BULKHEAD FWD SIDE HAS 14 ISOLATOR BRACKETS BENT/DEFORMED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND REPLACED 14 EA ISOLATOR BRACKET ASSEMBLY FROM FWD SIDE OF FS 621 BULKHEAD, REF CRJ200 SRM, NO LEAKS NOTED.Nov 9, 2020 · N907SW · Cndair CL6002B19SDR SWIA202054314Bulkhead · gougedFS 621 BULKHEAD FWD SIDE HAS 3 GOUGES AT APPROXIMATELY WL 103 & RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. BLENDED OUT DAMAGE TO A SMOOTH SURFACE AT FS 621 WL 103 & RBL 18, RBL 27, RBL 36, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED ANDNov 9, 2020 · N907SW · Cndair CL6002B19SDR SWAA2020111128946Vapor Barrier · crackedRIGHT WHEEL WELL VAPOR BARRIER CRACKED AT BS 663.75 BETWEEN RBL 31.83 AND RBL 45.64 8 INCHES ABOVE LOWER PANEL. CRACK MEASURES 14 INCHES, PERFORMED INTERIM REPAIR BY APPLYING BMS SEALANT AND ONE PLY OF BMS 9-3 FIGERGLASS CLOTH TO DAMAGED AREA, PER SRM 57-10-1Nov 7, 2020 · N8311Q · Boeing 7378H4SDR SWAA2020121028801Angle · crackedLT LOWER FUSELAGE AT STA 663.75 LBL 44 VAPOR BARRIER ANGLE HAS SUSPECT CRACK. ACCOMPLISHED REPLACEMENT ANGLE AT LT LOWER FUSELAGE STA 663 BETWEEN LBL 20' TO LBL 60' VAPOR BARRIER ANGLE, REF B737-7 SRM 57-10-10-2R-5 FIG 202 AND DWG 111A1000. LEAK CHECK BEING Nov 6, 2020 · N432WN · Boeing 7377H4SDR REXA2020111800757Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 WL 112 1.0" LONG. 100% FSH FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD, IAW CRJ 200 REO 601R-53-1285 REV E, 2016-10-31.Nov 6, 2020 · N8839E · Cndair CL6002B19SDR SWIA202056163Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHNov 5, 2020 · N876AS · Cndair CL6002B19SDR A6WA202011067399Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 LBL 27.5 AND WL 130.0 0.85'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 LBL 27.5 AND WL 130.0 CUTOUT MEASURES L=2.100'' W=1.00", REF REONov 5, 2020 · N450AW · Cndair CL6002B19SDR SWAA2020112328770Bulkhead Web · crackedCUSTOMER REQUEST RIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT APPROXIMATELY RBL40. CLEANED DAMAGE RT VAPPOR BARRIER FOR REPAIR, AS MARKED. PERFORMED DRY-OUT NO WATER FOUND, STOP DRILL CRACK. INSTALLED REPAIR ON RT VAPOR BARRIER, AS PER B737 SRM 51-70-Nov 4, 2020 · N265WN · Boeing 7377H4SDR 2A6D2020110403702Bulkhead · chafedCHAFING DAMAGE WAS DISCOVERED ON THE LT LATERAL BULKHEAD (X FRAME) P/N: 350A21-1051 ON THE INBOARD FACE. THE DAMAGE IS LOCATED ON THE INTERIOR (INBOARD) SIDE OF THE X FRAME LT AFT LOWER LEG STA 3650, BL 430L AND WL 2305.Nov 4, 2020 · N807LF · Snias AS350B3SDR CALA2020110401241Pressure Blkhd · crackedCRACK FOUND AT RT SIDE FASTENER HOLE ''B'' ON THE PRESSURE PANEL BETWEEN FR 35 & FR 36, REF EA 5330-05216 REV. "B". CRACK LOCATION 6 O'CLOCK, REF AAR N/R: 9469143 GENERATED BY: V909151. INSTALLED REPAIR AT RT SIDE PRESSURE PANEL BETWEEN FR 35-FR 36, AS PER UNov 3, 2020 · N457UA · Airbus A320232SDR KCSA202011021163Bulkhead Web · crackedWEB CRACKED AT STA 1480 BULKHEAD LBL 110 WL 150.Nov 2, 2020 · N716CK · Boeing 7474B5FSDR A6WA202102127628Bulkhead Web · cracked1" CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT LBL 27.50. 36" ABOVE FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED CRACK OF FWD FACE OF AFT PRESSURE BULKHEAD AT LBL 27.50 36 INCHES ABOVE FLOOR LEVEL IAW BOMBARDIER REO 601R-53-61-1285Oct 31, 2020 · N449AW · Cndair CL6002B19SDR FDEA202010312730Bulkhead · corrodedFWD CARGO FR 39, Y-450 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y-450 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROSION ON PRESSUREOct 31, 2020 · N654FE · Airbus A300F4605RSDR FDEA202010312729Bulkhead · corrodedFWD CARGO FR 39, Y450 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y450 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROSION ON PRESSURE FOct 31, 2020 · N654FE · Airbus A300F4605RSDR FDEA202010312728Bulkhead · corrodedFWD CARGO FR 39, Y-1959-Y-2164 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y-1959-Y-2164 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROct 31, 2020 · N654FE · Airbus A300F4605RSDR N6WA2020103002Bulkhead Web · corrodedRT LOWER WEB BEHIND 280.00 BEAM IS CORRODED. REMOVED AND REPLACED RT LOWER WEB BEHIND FS 280.00 BEAM, IAW CRJ 700 SRM 51-42-06 AND REO 670-53-11-544.Oct 30, 2020 · N501GJ · Cndair CL600*SDR DALA2020110203547Bulkhead Web · damagedDURING INSPECTION FOUND DAMAGED LAYERS ON PREVIOUS REPAIR ON RT FWD PRESSURE BULKHEAD VAPOR BARRIER WEB STA 663 BETWEEN RBL 45.64 AND RBL 31.83. RT FWD PRESSURE BULKHEAD VAPOR BARRIER WEB STA 663 BETWEEN RBL 45.64 AND RBL 31.83 WAS REPARED, PER B737-800 S.R.MOct 29, 2020 · N3764D · Boeing 737832SDR DALA2020110203546Bulkhead Web · crackedDURING INSPECTION FOUND CRACKED ON LT FWD PRESSURE VAPOR BARRIER BULKHEAD WEB STATION 663 LBL 15 (SM) LT MLG WHEEL WELL. VAPOR BARRIER BULKHEAD WEB STA 663 LBL 15 WAS REPARED, PER B737-800 SRM 57-10-10-2R REPAIR INSTRUCTIONS 5.Oct 29, 2020 · N3764D · Boeing 737832SDR SWIA202054577Isolator · brokenREAR PRESSURE BULKHEAD FS 621 HAS THREE BROKEN ISOLATORS AT APPROXIMATELY BL 46.5 RT BETWEEN WL 87.5 AND WL 99.5. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW QTY 3 ISOLATOR AT PRESSURE BULKHEAD, IAW CRJ 200 SRM.Oct 28, 2020 · N939SW · Cndair CL6002B19SDR R61A2020112500813Skin · damagedLEFT HORIZONTAL STABILIZER LOWER SKIN DAMAGE BETWEEN RIBS 11 AND 12 AND FROM FRONT SPAR TO STGR 02L. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN BETWEEN RIBS 11 AND 12 AND FROM FRONT SPAR TO STGR 02L AND 11L TO RIB 12L, IAW ETD 2020-170-030610.Oct 28, 2020 · N732YX · Emb ERJ170200LRSDR A6WA202010297373Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 BL 0.0 AND WL 130.0 0.75'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 BL 0.0 AND WL 130.0 CUTOUT MEASURES L=1.992'' W=1.262, REF REO 601Oct 28, 2020 · N450AW · Cndair CL6002B19SDR A6WA202010297371Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 LBL 36 AND WL 79.25 1.00'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 LBL 36 AND WL 79.25 CUTOUT MEASURES L=1.190'' W=1.130, REF REO 601Oct 28, 2020 · N450AW · Cndair CL6002B19SDR A6WA202010297372Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 LBL 18 AND WL 104.5 1.25'' IN LENGTH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CUTOUT OF AFT PRESSURE BULKHEAD CRACKED AREA AT FS 621.00 LBL 18 AND WL 104.5 CUTOUT MEASURES L=2.925'' W=1.242, REF REO 601Oct 28, 2020 · N450AW · Cndair CL6002B19SDR SWIA202054444Pressure Blkhd · damagedFS 621 BULKHEAD HAS CHAFED RIVET HEAD AT RBL 18 AT APPROXIMATELY WL 82. C-CHECK RO 11/24/2020. REMOVED AND REPLACED FS 621 BULKHEAD RIVET AT RBL 18 AT APPROXIMATELY WL 82, IAW CRJ 200 SRM. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Oct 26, 2020 · N928EV · Cndair CL6002B19SDR SWIA202054108Bulkhead Web · corrodedCORROSION FOUND ON RT FS 280 BULKHEAD WEB. C-CHECK RO 11/16/2020. REMOVED CORROSION FROM RT FS 280 LOWER BULKHEAD WEB AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPAIRED RT FS 280 LOWER BULKHEAD WEB, REF REO. COMPLIED WITH TASK CARD.Oct 26, 2020 · N786SK · Cndair CL6002C10SDR SWIA202054189Bulkhead Web · crackedFS 621 PRESSURE BULKHEAD WEB AFT STIFFENER P/N 601R36008-51 LOCATED AT LBL 36 & WL 80 FOUND CRACKED. C-CHECK RO 11/21/2020. REPLACED FS 621 PRESSURE BULKHEAD WEB AFT STIFFENER P/N:601R36008-51 LOCATED AT LBL 36 AND WL 80 AND REPLACED WITH NEW, REF CRJ-200 SOct 24, 2020 · N223JS · Cndair CL6002B19SDR REXA2020102200716Bulkhead Web · chafedFOUND REAR PRESSURE BULKHEAD WEB HAS 5 CHAFED AREA WL 103, LBL 27.50, LBL 18.00, RBL 18.00, RBL 27.50 AND RBL 36.20 .200" LONG BY .200" WIDE .003 DEEP. REPAIRED CHAFED AREAS OF REAR PRESSURE BULKHEAD WEB, IAW BOMBARDIER REO 601R-53-61-2155, REV A.Oct 20, 2020 · N686BR · Cndair CL6002B19SDR SWIA202054173Pressure Blkhd · gougedAFT PRESSURE BULKHEAD VERTICAL STIFFENER AT BL 0.00 IS GOUGED, MARKED. C-CHECK RO 11/21/2020. BLENDED OUT DAMAGED TO A SMOOTH CONTOUR ON AFT FS 621 PRESSURE BULKHEAD VERTICAL STIFFENER AT FS BL0.00, NDT INSPECTED NO DEFECTS NOTED. INSTALLED REPAIR PART P/N Oct 19, 2020 · N223JS · Cndair CL6002B19SDR N6WA2020101903Bulkhead Web · corrodedRT FS 280 BULKHEAD WEB CORRODED ABOVE FLOORBEAM. R & R RT FS 280 BULKHEAD LOWER WEB, IAW CRJ SRM 51-42-06.Oct 19, 2020 · N540GJ · Cndair CL600*SDR N6WA2020101902Bulkhead Web · corrodedLT FS 280 BULKHEAD WEB CORRODED ABOVE FLOORBEAM. R & R LT FS 280 BULKHEAD LOWER WEB, IAW CRJ SRM 51-42-06.Oct 19, 2020 · N540GJ · Cndair CL6002C10SDR SCNA20201116291Bulkhead Web · corrodedEVIDENCE OF CORROSION ON STATION 1016 BULKHEAD LOWER CLOSEOUT WEB LBL 24 WL 208. REMOVED AND REPLACED LOWER CLOSEOUT WEB STA 1016 BULKHEAD LBL 24 WL 208, IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 148A0922.Oct 18, 2020 · N813SY · Boeing 7378Q8SDR SCNA20201116256Bulkhead Web · crackedCRACK IN RIGHT HAND CENTER SECTION 663 BULKHEAD FORWARD SIDE RBL 12. ACCESSED & RESTORED RIGHT HAND CENTER SECTION 663 BULKHEAD FORWARD SIDE RBL 12, IAW SRM 51-40-02, DWGS 149A7216, DWG 111A1000. REPAIR ACCOMPLISHED ON CUSTOMER CARD 00444.Oct 18, 2020 · N813SY · Boeing 7378Q8SDR TIPR2020121544264Pressure Blkhd · corrodedAFT PRESSURE BULKHEAD AT STA 1016, AFT SIDE OF BULKHEAD, S12R STRINGER END FITTING AT BULKHEAD CORRODED, REPLACED.Oct 17, 2020 · N303KH · Boeing 737319SDR SWIA202054302Pressure Blkhd · crackedPRESSURE BULKHEAD AFT OF FS 621.0 STIFFENER IS CRACK. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW STIFFENER, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD.Oct 17, 2020 · N441SW · Cndair CL6002B19SDR SWAA2020102024116Bulkhead Web · crackedCENTER WING REAR SPAR VAPOR BARRIER WEB HAS AN 11.5' CRACK JUST INBOARD AND BELOW THE HYDRAULIC MODULAR PACKAGE ASSEMBLY AT LBL 39. ACCOMPLISHED INTERIM REPAIR, IAW SRM 57-10-10-1A-2 AND AFB SRM SUPPLMENT DOCUMENT NR AP 37.7-0602; 57-10-10 ALLOWABLE DAMAGE 2 Oct 17, 2020 · N275WN · Boeing 7377H4
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