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 LR7A2021011402660Bulkhead · chafedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 417 UNDERFLOOR BULKHEAD UPPER CAP CHAFED AT LBL 15-16, WL 146. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70. NR 1000302561.Jan 14, 2021 · Lkheed 382GSDR LR7A2021011402658Bulkhead · corrodedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 257 UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT LBL 17-57, WL 146. REPAIRED IAW LAC MEA 382-53-20-084 NR 1000302542.Jan 14, 2021 · Lkheed 382GSDR LR7A2021011402657Bulkhead · corrodedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 337.0E UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT LBL 40-RBL 40 WL 146. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70 NR 1000302533.Jan 14, 2021 · Lkheed 382GSDR LR7A2021011402653Bulkhead Web · corrodedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC 5314, FOUND THE FS 277.0E UNDERFLOOR BULKHEAD UPPER WEB CORRODED AT LBL 44, WL 146. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70 NR 1000302515.Jan 14, 2021 · Lkheed 382GSDR LR7A2021011402652Bulkhead · corrodedDURING P4-LAS SCHEDULED C-3 CHECK UNDER JOB CARD HC5314, FOUND THE FS 277.0E UNDERFLOOR BULKHEAD CORRODED BEYOND LIMITS UNDER RBL 40 ANCHOR NUT AT WL146. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70 NR 1000302514.Jan 14, 2021 · Lkheed 382GSDR SWIA202156275Bulkhead · corroded* FS 280 RBL 9.0 AT BOTTOM OF BULKHEAD THERE IS CORROSION AND SHEARED RIVET. (C-CHECK) RO 2/13/2021 COMPLIED WITH REO 670-53-11-745 REV.-A DATED 2016-10-28. INSTALLED €“ 4 POST LOWER END AND -6 ANGLE ON R/H FS 280.00 DOOR POST REPAIR COMPLIED WITH SKYWESTJan 9, 2021 · N760SK · Cndair CL6002C10SDR SWIA202156274Bulkhead · corrodedFS 280 LBL 9.0 AT FLOOR LEVEL CORROSION AND SHEARED FASTENER.AT BASE OF BULKHEAD. (C-CHECK) RO 2/13/2021 COMPLIED WITH REO 670-53-11-745 REV.-A DATED 2016-10-28. INSTALLED €“ 3 POST LOWER END AND -5 ANGLE ON L/H FS 280.00 DOOR POST REPAIR COMPLIED WITH SKJan 9, 2021 · N760SK · Cndair CL6002C10SDR AALA202101119018Pressure Blkhd · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED VERTICAL PRESSURE DECK WEB AT BS 663 BETWEEN RBL 40 AND RBL 45.64. REPAIRED VERTICAL PRESSURE DECK WEB, PER SRM 57-10-10-2R-4.Jan 9, 2021 · N822NN · Boeing 737823SDR A6WA202101087520Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 103.43 TO WL 114.93 LENGTH 11.5'' BL 0.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM. L=12.0'' W=1.8'', REF BOMBARDIER REO 601R-53-61-1285 REV E DATED 2016-10-31. PERFORMED HFEC INSPECTIJan 8, 2021 · N437AW · Cndair CL6002B19SDR A6WA202101087516Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 126.88 TO WL 136.18 LENGTH 9.5'' BL 0.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM L=10.0'' W=1.85''. CUT OUT ON STRAP FOR REPAIR DIM L=7.0'' W=2.50'', REF BOMBARDIER REO 601R-53-61-128Jan 8, 2021 · N437AW · Cndair CL6002B19SDR A6WA202101087519Bulkhead Web · crackedAFT PRESSURE BULKHEAD FWD SURFACE CRACKED AT FS 621.00 WL 131.98 TO WL 135.93 LENGTH 5.0'' RBL 18.0. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA DIM L=4.9'' W=1.7''. CUT OUT ON STRAP FOR REPAIR DIM L=8.2'' W=2.5'', REF BOMBARDIER REO 601R-53-61-1285Jan 8, 2021 · N437AW · Cndair CL6002B19SDR SWAA2021020843695Vapor Barrier · crackedCRACK VAPOR BARRIER LH SIDE AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER LH SIDE AT MAIN WHEEL WELL COMPARTMENT ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10 TOOL USED CALIPER PN 500-197-30 SN 15120589 DUE DATE 14SEP-21 HOT BONDER PN HCS9000B SN 1509209Jan 7, 2021 · N7724A · Boeing 7377BDSDR SWAA2021020843696Vapor Barrier · crackedCRACK VAPOR BARRIER RT SIDE AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER RT SIDE AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700SRM 51-70-04-2R REPAIR 10 TOOL USED CALIPER PN 500-197-30SN 15120589 DUE DATE 14-SEP-21 HOT BONDER PN HCS9000B SN 18175469 DJan 7, 2021 · N7724A · Boeing 7377BDSDR SWAA2021041939950Post · damagedELONGATED HOLE BULKHEAD PANEL 141QW VERTIVAL POST ON BST 907 AT AFT CARGO COMPARTMENT / REPLACED BULKHEAD VERTICAL POST ON BST 907 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 PN 149A8113Y26 BATCH 202019608900101 (ON ACCESS PANEL 141QW)Jan 6, 2021 · N406WN · Boeing 7377H4SDR K11A2021011800037Angle · corrodedBULK PIT, AFT BULKHEAD LOWER ANGLE HAS EVIDENCE OF CORROSION AFT SURFACE STA 907 LBL 16.Jan 5, 2021 · N730CK · Boeing 7374C9SDR SWAA2021020239525Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULK HEAD RIGHT HAND UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 7; W.L. 164. / ACCOMPLISHED PERMANENT REPAIR AT BS 663 LOWER COMPOSITE BULK HEAD RIGHT HAND UPPER ATTACH ANGLE AT RBL 7; WL.164 I.A.W SRM. 57-20-20-2R-5. FIG. 202 SHEET #4. DJan 4, 2021 · N565WN · Boeing 73776QSDR SWIA202155760Angle · crackedANGLE CRACKED AT STR 16L BETWEEN FS 621 AND FS 625 (C-CHECK) RO 2/1/2021 REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW CRJ200 SRM 51-42-21, 51-40-11Jan 3, 2021 · N498CA · Cndair CL6002B19SDR DALA2021010200005Pressure Blkhd · puncturedWORKING PRI 589215-14 TO REPAIR WHERE THE PRESSURE BULKHEAD, AT STA 110, HAD BEEN PUNCTURED BY CONTACT WITH LANDING GEAR STRUCTURE. COMPLETED PRI 589215-14 REV 0 1 2 3 4. COMPLETING ER/A 589215-14 REV A.Jan 1, 2021 · N993AT · Boeing 717200SDR FDEA202012273223Web · crackedRT MLG WHEEL WELL FWD PRESSURE BULKHEAD HAS SUSPECT CRACK AT STIFFENER OUTER END JUST BELOW ACCESS PANEL. MWT REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER, PER EA 1-5310-T0358831 P1.Dec 27, 2020 · N586FE · Doug MD11FSDR SWIA202056379Bulkhead Web · failedFOUND REAR PRESSURE BULKHEAD WEB AT RBL 27.50 WL112 HAS MULTIPLE INDICATIONS NOTED 7 INCHES LONG 90%FSH FAILED NDT INSPECTION. (C-CHECK) RO 2/21/2021. PERFORMED REPAIR OF FS 621 PRESSURE BULKHEAD IAW REO 601R-53-61-1240 REV D DATED 2016-10-31. REFERENCE CONDec 24, 2020 · N246PS · Cndair CL6002B19SDR SWIA202056030Firewall · chafed* TAILCONE FORWARD FIREWALL, CHAFED ON AFT UPPER RH SIDE (MARKED) (C-CHECK) RO 2/6/2021 REPAIRED THE TAILCONE FORWARD FIREWALL ON AFT UPPER SIDE AS PER CRJ 700 SRM 53-84-10-201-001-A01. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.Dec 23, 2020 · N708SK · Cndair CL6002C10SDR REXA2020122600858Bulkhead Web · chafedFS 621 BULKHEAD WEB CHAFED 2 LOCATIONS: FWD FACE WL 137.00, RBL 8.0 AND LBL 8.0. PERFORMED LPI OF FS 621 RPB FWD FACE WL 137 RBL 8 & LBL 8. REWORKED AREAS, IAW MHIRJ REO 601R-53-61-7500 REV- DATED 2020-12-04 STEP 3 NR 3. NO INDICATIONS NOTED AT THIS TIME.Dec 21, 2020 · N833AY · Cndair CL6002B19SDR DALA2020122104176Bulkhead Web · crackedDURING INSPECTION FOUND CRACKS (2 EA) ON VAPOR BARRIER STA 663.75 LBL 15.54 AND LBL 45.64, 8" UP FROM LOWER SKIN AT LT WHEEL WELL. VAPOR BARRIER STA 663.75 LBL 15.54 AND LBL 45.64, 8" UP FROM LOWER SKIN AT LT WHEEL WELL WAS REPAIRED, PER 737-800 SRM 57-10-10-Dec 20, 2020 · N379DA · Boeing 737832SDR SWIA202055653Bulkhead · misinstalledLT INLET PANDOWN IS INSTALLED INCORRECTLY. WHILE C/W NDT TASK 54-430-602, NOTED A REPAIR DOUBLER IN THE INSPECTION AREA PREVENTING THE INSPECTION FROM BEING ABLE TO BE DONE AS WRITTEN. AFTER INVESTIGATION, FOUND THAT PANDOWN IS INSTALLED WITH THE MOUNTING FLDec 17, 2020 · N957SW · Cndair CL6002B19SDR FDEA202012173175Doubler · crackedFUSELAGE: CENTER LANDING GEAR WHEEL WELL, RIGHT HAND BULKHEAD FORWARD DOUBLER APPROXIMATELY AT STATION 1381, X= -31.50, FLIGHT CONTROL ROD FEED THROUGH POSITION FOUND CRACKED. FUSELAGE CENTER LANDING GEAR WHEEL WELL RIGHT HAND BULKHEAD FORWARD CRACKED DOUBLDec 17, 2020 · N599FE · Doug MD11FSDR FDEA202012173174Doubler · crackedFUSELAGE: CENTER LANDING GEAR WHEEL WELL, LEFT HAND BULKHEAD FORWARD DOUBLER APPROXIMATELY AT STATION 1381, X=31.50, FLIGHT CONTROL ROD FEED THROUGH POSITION FOUND CRACKED. FUSELAGE CENTER LANDING GEAR WHEEL WELL LEFT HAND BULKHEAD FORWARD CRACKED DOUBLER APPDec 17, 2020 · N599FE · Doug MD11FSDR SWIA202055507Stiffener · crackedWHILE WORKING F.S.621 BULKHEAD REPAIR FOUND STIFFENER OUTBOARD OF LBL 36 JUST ABOVE FLOOR LEVEL IN AFT SIDE OF BULKHEAD CRACKED. C-CHECK RO 1/16/2021. INSTALLED STIFFNER P/N 601R36008-51 COMMON TO AFT BULKHEAD AT FS 621 LBL 36, IAW CRJ-200 SRM 51-42-06 REV 3Dec 16, 2020 · N701BR · Cndair CL6002B19SDR SWAA2021011537104Vapor Barrier · crackedLT WHEEL WELL STA 663 VAPOR BARRIER CRACKED. CLEANED AND REPAIRED DAMAGED A CRACK ON LT WHEEL WELL VAPOR BARRIER STA 663 RBL 34, AS PER B737 SRM 51-70-04-2R-10. PERFORMED TAP TEST AFTER REPAIR FOUND NO DELAMINATION, AS PER B737 NDTM 51-05-01 (SEC 5) MATERIALDec 16, 2020 · N7715E · Boeing 7377BDSDR SWAA2021011836962Attach Angle · crackedVERTICAL BULKHEAD FWD OF LEFT WHEEL WELL FWD FACE UPPER CHORD ATTACHED ANGLE CRACKED AT STA 663.75 LBL 12, MARKED DOT 60-012. REMOVED ATTACHED ANGLE CRACKED FROM VERTICAL BULKHEAD FWD OF LEFT WHEEL WELL FWD FACE UPPER CHORD STA 663 BETWEEN LBL 6 AND LBL 64, PDec 15, 2020 · N7715E · Boeing 7377BDSDR SWIA202058749Bulkhead Web · 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 WITHDec 13, 2020 · N904EV · Cndair CL6002B19SDR SWIA202057875Bulkhead · 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 WITHDec 13, 2020 · N873AS · Cndair CL6002B19SDR SWIA202056191Bulkhead Web · crackedAFT PRESSURE BULKHEAD F/S 621.0 STIFFENER IS CRACK (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED NEW BULKHEAD STIFFENER REF: CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-40-11, CRJ 200 SRM 51-25-16, SRM 51-21-11 AND BOMBARDIER DWG 601R36008 REV. BC. COMPLIED WITH TADec 13, 2020 · N876AS · Cndair CL6002B19SDR REXA2020122600857Bulkhead Web · chafed(2) CHAFES ON FS 621 BULKHEAD FWD FACE WL 87.5, RBL 18.0 AND 27.0. COMPLIED WITH STEP 4 OF MHIRJ REO 601R-53-61-7500 REV- DATED 2020-12-04. RESTORED FINISH OF REWORKED AREAS A010, PER SRM 51-21-16.Dec 12, 2020 · N833AY · Cndair CL6002B19SDR SWIA202055758Bracket · crackedAFT SIDE OF AFT BULKHEAD, LH SIDE @ FS625.30 STR 14, @ THREE INCHES FROM OUTBOARD SKIN, CRACKED BRACKET (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED BRACKET AFT SIDE AFT PRESSURE BULKHEAD LH SIDE @FS625.30 STR14 IAW CRJ200 SRM 51-42-21 AND 51-40-11Dec 10, 2020 · N498CA · Cndair CL6002B19SDR SWIA202055757Angle · crackedAFT BULKHEAD, AFT SIDE, RH CLIP CRACKED @ FS 621 STR 14 (C-CHECK) RO 2/1/2021 REMOVED AND LOCATED AND DRILLED, INSTALLED AND PAINTED NEW CLIP IAW CRJ 200 SRM 51-40-11,51-42-21, AND 51-25-21.Dec 10, 2020 · N498CA · Cndair CL6002B19SDR SWIA2021080960126Bulkhead · 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 WITHDec 8, 2020 · N693BR · Cndair CL6002B19SDR SWIA202057494Bulkhead · 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 WITHDec 8, 2020 · N908EV · Cndair CL6002B19SDR SWIA202057259Bulkhead · 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 WITHDec 8, 2020 · N943SW · Cndair CL6002B19SDR SWAA2020120934320Vapor Barrier · crackedFOUND CRACK ON VAPOR BARRIER LOWER LEFT WEB STA 663.75 LBL 48 LENGTH: 2'. CRACK IS WITHIN ALLOWABLE DAMAGE LIMITS, PER SRM 57-10-10-1A-2(4) NOT MORE THAN 16 INCH ZONE 1. PERFORMED INTERMIN REPAIR, PER SRM57-10-10-1A-2(4)(A). VISUAL INSPECTION OF REPAIR AREADec 6, 2020 · N254WN · Boeing 7377H4SDR A6WA202012087452Angle · corrodedT CAP CORRODED BEYOND LIMITS AT FS 621 TO FS 559+112 LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TCAP AT FS 559+112 TO FS 621, IAW CRJ SRM 51-42-21 AND BOMBARDIER DWG 601R35031.Dec 2, 2020 · N432AW · Cndair CL6002B19SDR A6WA202101257563Pressure Blkhd · crackedAFT PRESSURE BULKHEAD FWD SURFACE FS 621.00, WL 130.93 TO WL 133.93 CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED SPRING BRACKET AND CARGO DOOR TRACK AT REPAIR AREA, REF CRJ200 SRM 51-40-11, (REV 38) AND BOMBARDIER REO 601R-53-61-1541 DATED: 2020-12-06, (RDec 1, 2020 · N437AW · Cndair CL6002B19SDR SWAA2020122133646Bulkhead · crackedVAPOR BARRIER AT BS 663 RIGHT HAND SIDE IS CRACKED AT RBL 50. REMOVED AND REPLACED VAPOR BARRIER AT BS 663 RIGHT HAND SIDE, PER SRM 51-40-02 DWG 111A1000; DWG 111A1001; SRM 51-40-05-0G-0, ATSHFAB-101-203; PO 752673-ATS.Nov 30, 2020 · N563WN · Boeing 737752SDR SWAA2020120433315Bulkhead · crackedRT 663 VAPOR BARRIER HAS A CRACK AT APPROXIMATELY RBL 49 AND 9 IN FROM STRINGER. COMPLETED TIME LIMITED REPAIR EA 1-A57-13410 REV 01 REPETITIVE INSPECTION ACTION: REMOVE ALUMINUM FOIL SPEED TAPE AND INSPECT CRACKS FOR ADDITIONAL GROWTH. IF NO ADDITIONAL GROWNov 30, 2020 · N8319F · Boeing 7378H4SDR SWAA2020121632276Bulkhead Web · crackedLEFT MAIN WHEEL WELL STA 663 LOWER BULKHEAD VAPOR BARRIER CRACKED LBL 33 AND 7' UP FROM LOWER WHEEL WELL FAIRING. EVALUATED LT STA 663 VAPOR BARRIER AND FOUND CRACK OF 15' AT LBL 33 FOUND TO BE REPAIRABLE, IAW SRM 57-10-10-2R-2. REPAIRED LT VAPOR BARRIER, IANov 24, 2020 · N8607M · Boeing 7378H4SDR SWIA202055413Bulkhead Web · chafedTHE FS 621 PRESSURE BULKHEADS FWD FACE "PICKET FENCE" STRAPS HAVE 22 LOCATIONS OF CHAFES: LBL 36.20 HAS 2 AREAS, LBL 27.50 HAS 2 AREAS, LBL 18.00 HAS 2 AREAS, LBL 9.50 HAS 4 AREAS, RBL 9.50 HAS 4 AREAS, RBL 18.00 HAS 2 AREAS, RBL 27.50 HAS 3 AREAS, RBL 36.20 HNov 23, 2020 · N868AS · Cndair CL6002B19SDR AALA202011239017Bulkhead · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK IN LT FWD BULKHEAD AT LBL 35, MEASURING L=9.0 IN. ACCOMPLISHED PERMANENT REPAIR, IAW AARD 57-10-10-9 3B 2A AND SRM 57-10-10-1A-2 WITH REINSPECT EVERY 3000 CYCLES.Nov 22, 2020 · N880NN · Boeing 737823SDR BLUA20210825001Bulkhead · damagedDURING COMPLIANCE WITH DOCUMENT 4 REV 44, DAMAGE WAS FOUND ON AFT SIDE OF AFT TAILCONE BULKHEAD AT 5:30 CLOCK POSITION. DAMAGE APPEARS TO BE CONSISTENT WITH THE TAIL OF A LONG SCREW CONTACTING THE BULKHEAD. A TOO-LONG SCREW WAS NOT REMOVED FROM THAT LOCATIONNov 20, 2020 · N560ML · Cessna 560XLSDR AALA202011209027Bulkhead · deterioratedAIRCRAFT IN BASE MAINTENANCE. DETERIORATED EXISTING REPAIR SEALANT OF FWD BULKHEAD IN RT WHEEL WELL AT STA 540 AND LBL 35, MEASURING L=9.0 IN, W=0.025 IN, D=0.01 IN. ACCOMPLISHED PERMANENT REINFORCING BONDED REPAIR OF BULKHEAD, IAW AARD 57-10-10-9.Nov 19, 2020 · N880NN · Boeing 737823SDR AALA202011209026Bulkhead · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK IN LT FWD LOWER BULKHEAD AT STA 540 AND LBL 35, MEASURING L=9.0 IN, W=0.025 IN, D=0.01 IN. ACCOMPLISHED PERMANENT REINFORCING BONDED REPAIR, IAW AARD 57-10-10-9.Nov 19, 2020 · N880NN · Boeing 737823SDR IPXA2020111762495Bulkhead · corrodedINSPECTION TYPE: SEG 4 RT MLG WHEEL WELL BULKHEAD AREA JUST FWD OF THE RAT PANEL HAS CORROSION. REMOVED, FABRICATED, INSTALLED NEW CHORD IN REFERENCE TO DWG 149N7528 & SRM 51-40-02-OG.Nov 17, 2020 · N462UP · Boeing 75724APF
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