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 SWIA2021072259710Bulkhead Web · corrodedF.S.280 R/H LOWER WEB CORRODED AT APPROX RBL 11. (C-CHECK RO 7/20/2021) REPLACED FS.280 RH LOWER WEB. WITH NEW REF. CRJ 700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND SKYWEST M-337 FORM.May 3, 2021 · N790SK · Cndair CL6002C10SDR SWAA2021062368917Bulkhead · crackedREPAIR CRACK ON B.S. 663 LOWER COMPOSITE BULKHEAD AT R.B.L. 50; W.L. 158. / REPAIRED CRACK ON B.S. 663 LOWER COMPOSITE BULKHEAD AT R.B.L. 50; W.L. 158 PER SRM 51-70-04-2R-10.May 3, 2021 · N938WN · Boeing 7377H4SDR SWIA202158683Bulkhead Web · crackedR/H SIDE FS280 BULKHEAD LOWER WEB HAS CRACKED ATTACH ANGLE (C-CHECK RO 6/04/2021) REMOVED AND INSTALLED NEW SERVICEABLE BULKHEAD LOWER WEB ATTACH ANGLE AT RH SIDE FS280 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01 AND BOMBARDIERMay 3, 2021 · N702SK · Cndair CL6002C10SDR SWIA202158124Nut Plate · damagedFWD CARGO FWD LH BULKHEAD LOWER CENTER NUTPLATE DAMAGED (C-CHECK RO 5/5/2021) REMOVED AND REPLACED THE LOWER CENTER NUTPLATE FOR THE LH FWD BULKHEAD IN THE FWD CARGO. REF E-175 SRM 51-45-00.May 3, 2021 · N404SY · Emb ERJ170200LRSDR SWIA2021072259706Bulkhead Web · corrodedF.S.280 L/H LOWER WEB CORRODED AT APPROX LBL 11. (C-CHECK RO 7/20/2021) EXFOLIATION CORROSION FOUND AND 100% MATERIAL LOSS. REMOVED EXISTING SPLICE PLATE AND PERFORMED REPAIR ON FS280.00 L/H LOWER WEB AND BUTTSTRAP. REF: CRJ700 SRM 51-42-06-001-001-A01,May 2, 2021 · N790SK · Cndair CL6002C10SDR AALA202105029011Bulkhead Web · crackedAIRCRAFT IN BASE MAINTENANCE: 1.25 INCH LONG CRACK FOUND ON WEB BETWEEN LBL 31.83 AND LBL 40 ON LEFT SIDE OF WING CENTER SECTION KEEL BEAM. INSTALLED DOUBLER REPAIR PER B737NG SRM 57-10-10-2R REPAIR 4.May 1, 2021 · N839NN · Boeing 737823SDR IPXA2021042968782Pressure Blkhd · chafedINSPECTION TYPE:SEGNWW PRESSURE PAN GOUGED OUT OF LIMITS.REMOVED AND REPLACED PAN ASSY BOEING DRAWING 141N2938.Apr 29, 2021 · N462UP · Boeing 75724APFSDR SWAA2021062368400Bulkhead · crackedB.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT R.B.L. 50; W.L. 158. / REMOVED R/H VAPOR BARRIER BS 663 IAW SRM 51-40-02; REPAIRED R/H VAPOR BARRIER ON W/C U 314243; RE-INSTALLED R/H VAPOR BARRIER IAW SRM 51-40-02; DWG 111A1000 REV.A; DWG 111A1001 REV. A. APPLApr 28, 2021 · N938WN · Boeing 7377H4SDR REXA2021050300286Pressure Blkhd · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS 9 AREAS WITH MULTIPLE INDICATIONS NOTED. LBL 36.20 WL 77 1" 90% FSH, LBL 27.50 WL 101 5" 90% FSH, LBL 9.5 WL 110 2" 5% FSH, BL0.0 WL 125 8" 90% FSH, BL 0.0 WL 110 16" 60% FSH, RBL 27.50 WL 112 5" 50% FSH, RBL 27.50 WL 103 3Apr 28, 2021 · N924EV · Cndair CL6002B19SDR REXA2021050300285Bulkhead · damagedR/H 9G BULKHEAD HAS 20EA AREAS OF DAMAGE AROUND POTTED INSERTS. "REPAIRED R/H 9G BULKHEAD IAW EO CL600-2B19-53-L06717, REV.IR DATED 4/15/21 "Apr 28, 2021 · N924EV · Cndair CL6002B19SDR REXA2021050300284Bulkhead · damagedCENTER 9G BULKHEAD HAS 6EA AREAS OF DAMAGE AROUND PUTTED INSERTS. REPAIRED CENTER 9G BULKHEAD AND REPLACED 3EA INSERTS IAW CRJ200 EO CL600-2B19-53-L06716, REV.IR DATED 4/15/21 AND C&D ZODIAC SB B01002-25-01, REV.0 4/19/11.Apr 28, 2021 · N924EV · Cndair CL6002B19SDR SWAA2021062368388Stiffener · crackedB.S. 663 LOWER COMPOSITE BULKHEAD VERTICAL 'L' ANGLE STIFFENER IS CRACKED AT L.B.L. 26; W.L. 150; ON AFT SIDE OF B.S. 663 BULKHEAD. / REMOVED AND REPLACED B.S. 663 LOWER COMPOSITE BULKHEAD VERTICAL 'L' ANGLE STIFFINER AT L.B.L 26; W.L. 150; ON AFT SIDE OF B.S.Apr 27, 2021 · N938WN · Boeing 7377H4SDR SWIA202158671Bulkhead Web · corrodedCORROSION FOUND ON R/H FS280 BULKHEAD LOWER WEB (C-CHECK RO 6/04/2021) INSTALLED NEW SERVICEABLE L/H FS280 BULKHEAD LOWER WEB REF CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 53-11-10-Apr 27, 2021 · N702SK · Cndair CL6002C10SDR REXA2021050300287Stiffener · chafedCHAFE DAMAGE TO FS 621 BULKHEAD AFT VERTICAL STIFFENER @ BL O, APPROX 13' FROM TOP OF STIFFENER. REPAIRED FS 621 BULKHEAD AFT VERTICAL STIFFENER IAW ENDEAVOR EA CRJ253-11480 REV A, DATED 4/25/2021.Apr 27, 2021 · N924EV · Cndair CL6002B19SDR SWIA2021080960131Bulkhead Web · damagedFOUND REAR PRESSURE BULKHEAD WEB HAS 2 INDICATIONS NOTED 1) LBL9.5 WL76 1.5 INCHES LONG 100 FSH AND 2) LBL18 WL76 1 INCH LONG 90%FSH BOTH FAILED NDT INSPECTION (C-CHECK RO 8/5/2021) REPAIRED DAMAGE IAW MHIRJ REO 601R-53-61-7644 REV -- DATED 2021-06-14.Apr 26, 2021 · N693BR · Cndair CL6002B19SDR SWIA2021080960130Bulkhead · damagedFS 621 REAR PRESSURE BULKHEAD FWD FACE FOUND 6 INDICATIONS 1 BL 0 WL 134-128 50% FSH, 2 RBL 27 WL 107-111 40% FSH, 3RBL 18 WL 108-111 50% FSH, 4 RBL 18 WL 98-100 55% FSH, 5 BL 0 WL 97-116 100% FSH, 6 BL 0 WL 93-95 100% FSH FAILED NDT MARKED ON SKIN (C-CHECApr 25, 2021 · N693BR · Cndair CL6002B19SDR SWIA2021062358915Bulkhead Web · corroded*FS 280 WEB HAS CORROSION AT APPROX RBL 42 / FLOOR LEVEL. (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED THE FS280 R/H LOWER WEB REF CRJ700 SRM 51-42-06-001-001-A01, / SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, DWG: CC670-34Apr 24, 2021 · N603SK · Cndair CL6002C10SDR SWIA202158658Bulkhead Web · corrodedCORROSION FOUND ON L/H FS 280 BULKHEAD LOWER WEB (C-CHECK RO 6/04/2021) INSTALLED NEW LH FS280.00 LOWER WEB REF BOMBARDIER DWG.NO. CC670-34010 REV -B, CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRM 53-11-10-201-004-A01Apr 24, 2021 · N702SK · Cndair CL6002C10SDR REXA2021050300288Pressure Blkhd · crackedCRACK @ LBL36.0 ON 621 RPB OUT OF LIMITS PER MHIRJ REO 601R-53-61-1240. REPAIRED CRACK @ LBL 36.0 ON 621 BULKHEAD IAW BOMBARDIER REO 601R-53-61-7632.Apr 24, 2021 · N924EV · Cndair CL6002B19SDR IPXA2021060370125Beam · crackedINSPECTION TYPE:3CFWD CARGO AFT PRESSURE BULKHEAD AT STA 595 RBL 42 VERTICAL BEAM IS CRACKED.REPAIRED CRACKED FWD CARGO AFT PRESSURE BULKHEAD AT STA 595 RBL 42 VERTICAL BEAM IAW EA 011-5311-01-A9054 REV. IR AND UPS EO MD11-5310-80436-A. MAJORApr 23, 2021 · N265UP · Doug MD11FSDR A6WA202106117801Bulkhead · crackedCRACK INDICATIONS (7 TOTAL) AT FS621.00 AFT PRESSURE WEB. CRACKS AT THE FOLLOWING LOCATIONS, WL 128.5 - 131.2, LBL 18.0, CRACK LENGTH 2.7"L, WL 113.5 - 114.2, LBL 9.50, CRACK LENGTH 0.7"L, 109.5 - 112.0, BL 0.0, CRACK LENGTH 2.5"L, WL 110.5 - 111.2, RBL 9.50, Apr 21, 2021 · N465AW · Cndair CL6002B19SDR SWIA202158138Bulkhead Web · crackedFR 52 LH WEB FWD OF THE LH MLG WHEEL WELL AREA HAS DAMAGE/ CRACKED IN 2 AREAS. (C-CHECK) REMOVED AND REPLACED L/H FR 52 WEB FWD OF MLG WHEEL WELL REF SRM 51-40-08. TOPCOATED FASTENERS REF SRM 51-23.-06.Apr 21, 2021 · N156SY · Emb ERJ170200LRSDR SWAA2021042665419Bulkhead · crackedCENTER CARGO BULKHEAD PANEL AT STA 731 HAS LARGE CRACK. RR CENTER CARGO BULKHEAD AT STA 731 IAW AMM 255218.Apr 21, 2021 · N914WN · Boeing 7377H4SDR HNAA2021051900214Bulkhead · damagedPILOTS BULK HEAD LOWER GUIDE PIN HOLE IS ELONGATED AT FR15. REPAIRED PILOTS BULK HEAD LOW-ER GUIDE PIN ELONGATED HOLE AT FR 15 IAW PIEDMONT EO1-53-21-0108.Apr 18, 2021 · N644AE · Emb EMB145LRSDR SWIA202158189Bulkhead Web · crackedFS.621 PRESS BULKHEAD LWR WEB AFT STIFFENER LOCATED OUTBD OF LBL36 ABOVE FLOOR AT WL80 FOUND CRACKED . (C-CHECK RO 5/16/2021) REMOVED AND INSTALLED REPLACEMENT FS.621 PRESS. BULKHEAD WEB AFT SIDE STIFFENER P/N 601R36008-51 AT WL.79 OUTBD OF LBL36 PER Apr 16, 2021 · N925EV · Cndair CL6002B19SDR SIMA20210416009Firewall · crackedAPU FIREWALL HAS A CRACK PROTRUDING FROM THE UPPER R/H MOUNT-C/A-REPAIRED APU FIREWALL ON RH UPPER MOUNT IAW ETN-EM-53-244 R3.Apr 16, 2021 · N668HH · Emb EMB145LRSDR SWAA2021042065017Bulkhead Web · crackedLH MLG WHEEL WELL VAPOR BARRIER HAS A CRACK MEASURING 15.5' AT LBL 30. ACCOMPLISHED INTERIM REPAIR IAW SRM 5710101A2.Apr 16, 2021 · N940WN · Boeing 7377H4SDR SWAA2021042064847Bulkhead Web · crackedLH WHEEL WELL VAPOR BARRIER HAS 6' CRACK AT LBL 45.64 REMAINING AFTER PERMANENT REPAIR.ACCOMPLISHED INTERIM REPAIR IAW SRM 5710102R2.REPETITIVE ACTION REQUIRED:DO A DETAILED VISUAL INSPECTION EVERY 3000 FLIGHT CYCLES IAW SRM 5710102R2 PAR.2.C. IF ADDITIONAL DAApr 16, 2021 · N8303R · Boeing 7378H4SDR SWAA2021042064848Bulkhead Web · crackedMAIN WHEEL WELL LEFT HAND SIDE VAPER BARRIER OUTSIDE OF RIB 383 BEHIND B SYS. MAIN HYDRAULIC FITTER HAS 6INCH CRACK REPETITIVE ACTION REQUIRED PERFORMED INTERIM REPAIR IAW SRM 5710101A2. REQUIRES VISUAL INSPECTION OF AREA AT 1200 FLIGHT CYCLES INTERVAL OR MOREApr 16, 2021 · N8305E · Boeing 7378H4SDR SWAA2021042064441Bulkhead Web · crackedFOUND CRACK ON VAPOR BARRIER AT R/H WHEEL WELL FORWARD TO HYD RETURN FILTER BETWEEN RBL 31 AND RBL 45 SIX INCHES IN LENGTH.DAMAGE IS ALLOWABLE PER SRM 5710101A2. APPLIED ALUMINUM FOIL TAPE TO AREA OF CRACK. DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIApr 16, 2021 · N8329B · Boeing 7378H4SDR SWAA2021042064858Bulkhead Web · crackedFOUND CRACK ON VAPOR BARRIER AT RH WHEEL WELL FORWARD TO HYD RETURN FILTER BETWEEN RBL 31 AND RBL 45 SIX INCHES IN LENGTH.DAMAGE IS ALLOWABLE PER SRM 5710101A2. APPLIED ALUMINUM FOIL TAPE TO AREA OF CRACK. DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGApr 16, 2021 · N8329B · Boeing 7378H4SDR QMLA2021041520029Bulkhead · corrodedBK117-C2 S/N 9080 WAS FOUND TO HAVE CHAFE DAMAGE TO THE UPPER BULKHEAD ANGLE P/N L533K3138-201 AT STA 4963, RBL 40, WL 2625. THE DAMAGE MEASURES 0.01” DEEP, AND 0.25” X 0.25” IN AREA.Apr 15, 2021 · N984ME · Bolkms BK117C2SDR FDEA202104151057Support · corrodedSTRUCTURES - FUSELAGE SEALS AND DRAINS: DURING FUSELAGE PRESSURIZATION, AT R/H MAIN LANDING GEAR WHEEL WELL R/H UPPER T-CORD FWRD BULKKHEAD LEAKING, SHOWING SHOWING WHITE POWDERY SUBSTANCE UNDER 4 EACH CLAMPS/CLIPS & RUB STRIP MIGRATED MIGRATED BETWEEN CLApr 15, 2021 · N316FE · Doug MD1030FSDR FDEA202104151136Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL, L/H FWD VERTICAL BULKHEAD, AT TRANSITION HOLE FOR SPOILER/AILERON CONTROL RODS, STA 1381 Z=-76 TO -87. DOUBLER FITTING AEA0486 HAS A FOUR INCH CRACK ALONG THE VERTICAL FASTENER ROW, TOP AREA. (MKD) REMOVE AND REPLACE LONGERApr 15, 2021 · N316FE · Doug MD1030FSDR SWIA202157922Bulkhead · crackedLH SIDE FWD OF MLG BULKHEAD AT FR52 L-ANGLE IS CRACKED AT OUTBD FASTENER HOLE AS MARKED (C-CHECK RO 4/27/2021) INSTALLED NEW LH SIDE FWD OF MLG BULKHEAD AT FR52 L-ANGLE AND CAP SEALED INNER FUEL TANK FASTENERS PER REF SRM 51-40-08, 51-21-05Apr 15, 2021 · N182SY · Emb ERJ170200LRSDR DALA2021041902262Bulkhead Web · corrodedCORROSION AT AFT PRESSURE BULKHEAD FS1053 BETWEEN LONGERONS 28L AND 29L. NRC 031-0022:5310-2014/003 00411: REPAIRED PER PRI 590913- 14 REV ORIG AND ER/A 590913-14 REV ORIG. ALL STEPS MATCH. ASSOCIATED ER/A 00-590913 ADDED FOR AC 9502. (LP #1782629)Apr 15, 2021 · N942AT · Boeing 717200SDR SWAA2021052764278Bulkhead Web · crackedCRACK VAPOR VARRIER LH SIDE AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER LH SIDE AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10Apr 14, 2021 · N939WN · Boeing 7377H4SDR SWIA2021062859038Bulkhead · corroded* CORROSION FOUND ON BOTTOM OF FWD PRESSURE B/H F/S 693 BTWN STRS 26L AND 26R (C-CHECK RO 6/22/2021) REMOVED CORROSION ON OUTBOARD FLANGE OF FORWARD PRESSURE BULKHEAD AT FS693 BETWEEN STGRS 26L & 26R PER REF CRJ900 SRM 51-21-06-001-001-A01. ORIGINAL THApr 9, 2021 · N800SK · Cndair CL6002D24SDR SWIA2021062859032Bulkhead · dented*FS 847 LH WHEEL WELL THERE IS A DENT WITH CREASE ( MARKED ) (C-CHECK RO 6/22/2021) REPAIRED DENT ON FS 847 LH WHEEL WELL BULKHEAD REF REO 690-53-41-265 REV -- DATED 2021-05-11, COMPLIED WITH SKYCARD 51-900-1002 SKY CL600-2D24 STRUCTURAL MAJOR REPAIR.Apr 9, 2021 · N800SK · Cndair CL6002D24SDR A6WA202104147742Bulkhead Web · cracked6 CRACKS WERE FOUND ON FS621.00 BULKHEAD WEB AT FS621.00 AS FOLLOWS: 1. FS 621 WL 91.0 - 91.50, RBL 27.50 CRACK LENGTH .50" 2. FS 621 WL 92.25 - 92.75, RBL 18.00 CRACK LENGTH .50" 3. FS 621 WL 101.50 - 102.00, RBL 27.50 CRACK LENGTH .50" 4. FS 621 WL 109.50 -Apr 7, 2021 · N461AW · Cndair CL6002B19SDR SWIA202158367Bracket · brokenFS.621 BULKHEAD HAS 3EA BROKEN BRACKETS @ APPROX. STRG.13-15 (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED 3 NEW BRACKETS (PN:601R45156-75) ON THE FS.621 BULKHEAD AT APPROX STRG 13R-15R REF CRJ 200 SRM 51-42-06. LEAK CHECK GOOD.Apr 6, 2021 · N956SW · Cndair CL6002B19SDR SWIA202158319Stiffener · crackedFS409.00+128 PRESSURE BULKHEAD LBL 27 SUPPORT POST CRACKED AT BOTTOM INNER (MARKED - OUT OF SCOPE) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED A NEW FS.409+128 LBL 27 SUPPORT POST REF REO 601R-53-41-2909 REV -- DATED 2021-05-05 AND DWG #601R32208 REV Apr 6, 2021 · N956SW · Cndair CL6002B19SDR SWAA2021042362297Bulkhead Web · crackedR/H BS 663 GFRP VAPOR BARRIER CRACKED JUST ABOVE HYDRAULIC SERVICE HANDLE / REPAIRED CRACK DAMAGE JUST ABOVE HYDRAULIC SERVICE HANDLE ON R/H BS 663 GFRP VAPOR BARRIER IAW SRM 51-70-04-2R-10 7062U 4-10-21Apr 6, 2021 · N958WN · Boeing 7377H4SDR CALA2021040600432Pressure Web · cracked2EA CRACKS FOUND AT EXTERNAL CENTER WING REAR SPAR VERTICAL PRESSURE WEB CRACK NO.1 LOCATED BETWEEN LBL 45.64 TO LBL 40.00 LENGTH OF CRACK APPROX 1IN. CRACK NO.2 LOCATED BETWEEN LBL 31.83 TO LBL 24.92 LENGTH OF CRACK APPROX .400IN REF AAR N/R 9614270 REAPAIREDApr 6, 2021 · N33294 · Boeing 737824SDR SWIA202158315Attach Angle · cracked* FS 621 BULKHEAD AFT RIGHT SIDE ATTACHING CLIP AT APROX. STGR 15R IS CRACKED. (C-CHECK RO 5/20/2021) INSTALLED NEW BULKHEAD RH SIDE ATTACHING CLIP AT APPROX 15R, RESTORED FINISH TO ATTAHING CLIP. REF: CRJ200 SRM 51-42-06 AND DRAWING #601-35012 REV, -D.Apr 4, 2021 · N956SW · Cndair CL6002B19SDR SWAA2021051262463Bulkhead Web · crackedCRACK BODY STATION 663.75 VAPOR BARRIER LBL 35 APROX. AT MAIN WHEEL WELL COMPARTME. REPAIRED BODY STATION 663.75 VAPER BARRIER LBL 35 APPROX AT MAIN WHEEL WELL ASPER B737700 SRM 5170042R10 REP 10 TOOL USED CALIPER PN 50019730 SN 15120589 DUE DATE 14SEP21 HOT BApr 4, 2021 · N7856A · Boeing 7377Q8SDR SWAA2021042865751Angle · crackedCRACK VAPOR VARRIER UPPER ANGLE LOC ON BS663 BETWEEN BL0 AT RBL 64 AT MAIN WHEEL WELL COMPARTME (1 EA) / REPLACED VAPOR VARRIER UPPER ANGLE LOC ON BS663 BETWEEN BL0 AT RBL64 AT MAIN WHEEL WELL COMPARTMENT (1E/A) IAW B737-700 SRM 51-40-02 AND DWG #111A1000 REV.Apr 3, 2021 · N443WN · Boeing 7377H4SDR SWIA2021070159257Angle · crackedFS. 280 BULKHEAD ANGLE AT LBL 26 IS CRACKED THROUGH BOTTOM FASTENER HOLE. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED ANGLE AT LBL 26 AT F.S 280 BULKHEAD WITH NEW PART PN:CC670-34117-5 IAW CRJ 700 SRM 51-42-06-001-001 AND REF: SRM 53-11-10-201-004-A01 LApr 1, 2021 · N656CA · Cndair CL6002C10SDR SWIA2021070159252Angle · crackedFS. 280 BULKHEAD ANGLE AT RBL 26 IS CRACKED THROUGH BOTTOM TWO FASTENER HOLE. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED ANGLE AT RBL 26 AT F.S 280 BULKHEAD WITH NEW PART PN:CC670-34117-6 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND REF: SRM 53-11-10-201-0Apr 1, 2021 · N656CA · Cndair CL6002C10SDR SWIA202157568Support Angle · crackedCARGO DOOR OPENING UPPER BEAM AFT SUPPORT ANGLE IS CRACKED. FS621.00 AT WL 115.08. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR OPENING UPPER BEAM AFT SUPPORT ANGLE IN REF TO SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY. COMPLETED M-337.Apr 1, 2021 · N448SW · Cndair CL6002B19
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