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 A6WA202021247169Bulkhead Web · crackedAFT PRESSURE BULKHEAD IS CRACKED AT CARGO DOOR AFT TRACK, APPROX. LBL27.5 AND WL 130. AIRCRAFT REMOVED FROM SERVICE REPAIR TRANSFERRED TO AAR W.O. 1018176/2000/0019 C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS6Feb 12, 2020 · N410AW · Cndair CL6002B19SDR A6WA2020021347170Bulkhead Web · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0, WL 111.00. AIRCRAFT REMOVED FROM SERVICE WORK TRANSFERRED TO AAR W.O. 1018176/2000/0019, S/N 7601432, C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING BOMBARFeb 12, 2020 · N434AW · Cndair CL6002B19SDR SWAA2021082318534Doubler · crackedDOUBLER ON FWD SIDE OF BS663 COMMON TO VAPOR BARRIER AT RBL70 WL166 IS CRACKED / REMOVED AND REPLACED DOUBLER ON FWD SIDE OF BS.663 COMMON TO VAPOR BARRIER AT RBL70 WL166. IAW SRM 51-40-02; 51-40-02 AND DWG 111A1001Feb 11, 2020 · N235WN · Boeing 7377H4SDR AALA202002129020Bulkhead Web · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT BS 663 AND LBL 28. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R REPAIR 2 AND AARD 57-10-10-9 REPAIR 9.Feb 11, 2020 · N923AN · Boeing 737823SDR DALA2020021101065Gasket · damagedRIGHT WHEELWELL SLANT PANEL LEAKING. GASKET IS DAMAGED. MAINTENANCE REPLACED THE SLANT PANEL GASKET REF B717 AMM 53-32-02. LEAK CHECK IS GOOD. (LP #1484805)Feb 11, 2020 · N893AT · Boeing 717200SDR SWAA2020022874904Bulkhead Web · crackedR/H VAPOR BARRIER WAS CRACKED AT BS. 663. / R&R VAPOR BARRIER IAW SRM & DWG.Feb 10, 2020 · N453WN · Boeing 7377H4SDR SWAA2020022641710Attach Angle · crackedLOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE WAS CRACKED AT BS. 663, RBL 8. / REPAIRED ANGLE IAW SRM.Feb 10, 2020 · N453WN · Boeing 7377H4SDR SWAA2020022641709Attach Angle · crackedLOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS. 663, LBL 8. / REPAIRED ANGLE IAW SRM.Feb 10, 2020 · N453WN · Boeing 7377H4SDR SWAA2020021941465Bulkhead Web · crackedEXISTING REPAIR ON VAPOR BARRIER WEB CRACKED AND DISBONDED AT BS. 663, RBL 11. / REPAIRED WEB IAW SRM.Feb 10, 2020 · N799SW · Boeing 7377Q8SDR CALA2020021200404Bulkhead Web · crackedCENTER WING REAR SPAR VAPOR WEB SHOWS CRACK AT LOWER R/H SIDE @ RBL30.(MARKED) INSTALLED INTERIM REPAIR PER SRM 57-10-10,REPAIR 2. INITIATED DI P TO PERFORM DETAIL VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. LENGTH OF CRACK MEASURES 8.5" LONG. SEE FLEET CYCLEFeb 10, 2020 · N36444 · Boeing 737924ERSDR 2A6D2020021003Bulkhead · chafedDURING INSPECTION FOUND A CHAFE IN THE RIGHT HAND LATERAL BULKHEAD (X-FRAME) ON THE EXTERIOR SIDE AND IS .022" DEEPFeb 10, 2020 · N354CF · Snias AS350B3SDR 2A6D2020021001Bulkhead · chafedFOUND CHAFE DAMAGE AT THE BACK BAGGAGE COMPARTMENT ON THE FORWARD WALL IN THE TAILBOOM. STA.4174, BL. R355, WL. 2672.2. ATTACHED ARE THE PICTURES OF THE DAMAGE. THERE ARE 3 SEPARATE AREAS THAT MEASURE 10 IN. IN TOTAL LENGTH. THE DEEPEST GOUGE RUNS .028 IN.Feb 10, 2020 · N354CF · Snias AS350B3SDR SWAA2021082318414Bulkhead Web · crackedREMOVE AND REPLACE R/H BS663 VAPOR BARRIER WEB DUE TO CRACK BETWEEN RBL45 AND RBL55 WL160 / REMOVED AND REPLACED CRACKED R/H VAPOR BARRIER; BS 663 RBL 5-RBL 72 WL 160 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 111A1000; DWG 111A1001Feb 8, 2020 · N235WN · Boeing 7377H4SDR SWIA2020030549051Bulkhead · crackedREAT PRESSURE BULKHEAD U/T CRACK INDICATION RBL 36.20 49"-55" ABOVE FLOOR (6EA FASTNERS) (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO .215 ON REAR PRESSURE BULKHEAD 49"-54" ABOVE FLOOR AND INSTALLED FASTENERS PER CRJ200 SFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549049Bulkhead · crackedULTRA SOUND REAR PRESSURE BULKHEAD CRACK INDICATION AT FASTNER RBL 27.50 31" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENER AND REAMED FASTENER HOLE FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 50" AND 52" ABOVE FLOOR INSTALLED FASTENER PER Feb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549047Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION. FASTNER HOLE RBL 27.50 41" AND 44" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 41" AND 44" ABOVE FLOOR INSTALLED Feb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549046Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION RBL 18.00 32" AND 33" ABOVE FLOOR EMITTING FROM FASTNER HOLES (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 32" AND 33" ABOVE FFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549045Bulkhead · crackedREAR PRESUURE BULKHEAD ULTRA SOUND CRACK INDICATION EMITTING FROM FASTNER HOLES RBL 18.00 50 AND 52" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 50" AND 52" ABOVE FLOFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549044Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION EMITTING FROM FASTNER HOLES LBL 9.5 13" AND 35" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD LBL 9.50 13" AND 35" ABOVE FLOORFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549043Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION EMITTING FROM FASTNER HOLES AT LBL 18.00 26" AND 27" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD LBL 18.00 26" AND 27" ABOVEFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549042Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION LBL 36.20 13" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENER AND REAMED FASTENER HOLE FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD LBL 36.20 13" ABOVE FLOOR INSTALLED FASTENER PER CRJ200 SRM. ACCOMPLFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549041Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK INDICATIONS (2 EA) FASTNERS IN UPPER CHORD. LBL 5.00 (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO #5 ON REAR PRESSURE BULKHEAD UPPER CHORD (2EA) HOLES AT LBL 5.00 INSTALLED FASTENERS PER CRJ20Feb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549040Bulkhead · crackedREAR PRESSURE BULKHEAD UPPER CHORD CRACK INDICATIONS EMITTING FROM FASTER (2EA) HOLES AT LBL 11.0 (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO #5 ON REAR PRESSURE BULKHEAD UPPER CHORD (2EA) HOLES AT LBL 11.0 INSTALLED FASFeb 8, 2020 · N945SW · Cndair CL6002B19SDR SWIA2020030549039Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK INDICATION EMITTING FROM FASTNER HOLE IN UPPER CHORD LBL 19.00 (C CHECK) RO 3/2/2020 REMOVED FASTENER AND REAMED FASTER HOLE FROM 5/32" TO #5 ON REAR PRESSURE BULKHEAD UPPER CHORD LBL 19.00 INSTALLED FASTENER PER CRJ200 SRM. ACFeb 8, 2020 · N945SW · Cndair CL6002B19SDR LR7A2020021082243Bulkhead Web · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS935 LH SIDE BULKHEAD J-SECTION (WEB) CRACKED AT WL256, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000151720.Feb 8, 2020 · N409LC · Lkheed 382GSDR LR7A2020021082242Bulkhead Web · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS902 RH SIDE BULKHEAD WEB CRACKED AT WL230, RBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000151719.Feb 8, 2020 · N409LC · Lkheed 382GSDR LR7A2020021080241Tee Fitting · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS792 RH BULKHEAD INBOARD CAP (TEE) CRACKED AT WL166, RBL65. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-14. NR# 1000151183. / AD 2012-06-09, PSE# 53-50-07.Feb 8, 2020 · N409LC · Lkheed 382GSDR LR7A2020021080240Tee Fitting · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS814 RH BULKHEAD INBOARD CAP (TEE) CRACKED AT WL170, RBL65. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-14. NR# 1000151182. / AD 2012-06-09, PSE# 53-50-07.Feb 8, 2020 · N409LC · Lkheed 382GSDR LR7A2020021080239Tee Fitting · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS858 LH SIDE BULKHEAD TEE (INBOARD CAP) CRACKED AT WL198, LBL69. / REPAIRED IAW LAC MEA 382-53-20-018. NR# 1000151181. / AD 2012-06-09, PSE# 53-50-07.Feb 8, 2020 · N409LC · Lkheed 382GSDR CALA2020020800353Bulkhead Web · crackedCENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB IS CRACKED AT THE TOP OF STA 663.75 LBL 43. REF FLEET CYCLE LOG PAGE 9721878. A/C REQUIRES DIP TO REINSPECT REPAIR AT 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION AND 36000 FLIGHT CYCLES THERE AFTER. CENTER WINGFeb 6, 2020 · N76254 · Boeing 737824SDR FDEA202002060276Stiffener · crackedRH WW AFT BULKHEAD IB SIDE LWR STIFFENER CRACKED REMOVED RH WW AFT BULKHEAD IB SIDE LWR STIFFNER IAW B757 SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW STIFFNER IAW B757 SRM 51-40-05 AND 51-40-02Feb 6, 2020 · N976FD · Boeing 7572B7SDR SWAA2020022091550Bulkhead Web · crackedMAIN WHEEL WELL COMPARTMENT VAPOR BARRIER CRACKED AT BS. 663, LBL 30. / REPAIRED VAPOR BARRIER PER SRM.Feb 5, 2020 · N921WN · Boeing 7377H4SDR SWAA2020021241338Floor Panel · crackedAFT CARGO COMPARTMENT FLOOR PANEL 140AF CRACKED. / FABRICATED FLOOR PANEL 140AF IAW DWG.Feb 5, 2020 · N921WN · Boeing 7377H4SDR IPXA2020020551852Frame · bentINSPECTION TYPE:SPVCHORD ON RIGHT SIDE PRESSURE BULKHEAD HAS SLIGHT BENT AT STA200 RBL37 WL200REMOVED DAMAGED AREA AND INSTALLED NEW SECTION AND REPAIRED SPLICEFeb 5, 2020 · N406UP · Boeing 75724APFSDR IPXA2020020551851Bulkhead Web · dentedINSPECTION TYPE:SPVFWD PRESSURE BULKHEAD WEB PART #141N2800-164 DENTED BLKHD STA199 RBL30 WL200REMOVED DAMAGE, INSTALLED FILLER AND REPAIR DOUBLERFeb 5, 2020 · N406UP · Boeing 75724APFSDR V0XD20200502001Bulkhead Web · corrodedR/H BULKHEAD WEB AT F.S. 280.00 CORRODED. CORRECTIVE ACTION: REPAIRED R/H BULKHEAD WEB AT F.S. 280.00 BY REMOVING CORREDED BULKHEAD WEB, FABRICATING AND INSTALLING NEW BULKHEAD WEB IAW BOMBARDIER REO# 670-53-11-594 REV A DATED: 2015/06/26Feb 5, 2020 · N340CA · Cndair CL6002C10SDR SWIA2020040749990Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWLOF BOMBARDIER. (J)(2) MODIFYIFeb 4, 2020 · N903EV · Cndair CL6002B19SDR SWIA2020031649297Beam · crackedFS 409.00+128 BULKHEAD BEAM BL 27L/H LOWER INBOARD SIDE HAS A POSSIBLE CRACK GOING UP FROM BOTTOM AS MARKED. (C-CHECK) RO 3/13/2020 REMOVED AND INSTALLED NEW F.S 409+128 BULKHEAD BEAM/POST AT LBL 27 REF. BOMBARDIER REO. COMPLIED WITH TASK CARD. PRESSURE Feb 4, 2020 · N461SW · Cndair CL6002B19SDR DALA2020020650938Pressure Panel · crackedCRACK INDICATION FOUND IN OPEN HOLES (2 E/A) LOCATED ON PRESSURE PANEL AT FRAME 36 RH SIDE AND -Y1292+2", AND OTHER -Y1292+3". REPAIRED ON OPEN HOLES LOCATED PRESSURE PANEL AT FRAME 36 R/H SIDE AND -Y1292+5", AND OTHER -Y1292+3" (2 E/A) BETWEEN FR35 AND FR36 WFeb 4, 2020 · N330NB · Airbus A319114SDR DALA2020020650937Pressure Panel · crackedCRACK FOUND AT HOLE A REPAIR IN ACORDANCE WORD CARD 531 1-01171-04B PRIOR TO FURTHER FLIGHT AA 5311-01171 ,SB A320- 531264, AD- 2018-06-04. REPAIRED ON OPEN HOLE "A" LOCATED PRESSURE PANEL AT FRAME 36 R/H SIDE WAS ACCOMPLISHED WITH WORK CARD 5311-01171-04B RIIFeb 4, 2020 · N330NB · Airbus A319114SDR IPXA2020021435103Bulkhead · corrodedINSPECTION TYPE:S/VRIGID CARGO BARRIER WALL HAS HEAVY CORROSION IN MANY PLACES.REMOVED AND REPLACED RIGID CARGO BARRIER ASSY., S/N UP69216 IAW AMM 25-59-13-400-801. (MINOR)Feb 3, 2020 · N291UP · Doug MD11FSDR CALA2020020870336Bulkhead Web · cracked(DIP)LOG PAGE NO. 8619163 R/H UPPER VAPOR BARRIER CRACKED O/B OF RATIO CHANGER REQUIRES PERMANENT REPAIR. REF TO PEMCO NR 2675N1382. REPAIRED REAR SPAR VERTICAL PRESSURE DECK WEB RBL25-50 PER BOEING 737-800 SRM 57-10-10 REPAIR NUMBER 3 ALTERNATIVE 2 FIG 204. IFeb 3, 2020 · N27246 · Boeing 737824SDR AALA2020030369008Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LOWER BULKHEAD ANGLE AT BS 500I BETWEEN LBL 24 AND RBL 24. REPLACED ANGLE PER SRM 51-40-02.Feb 2, 2020 · N982AN · Boeing 737823SDR SWAA2020022871772Bulkhead Web · damagedVAPOR BARRIER HAD TEMPORARY REPAIR THAT WAS PEELING AT APPROXIMATELY BS. 663, RBL 30. / REPAIRED VAPOR BARRIER PER SRM.Feb 1, 2020 · N8601C · Boeing 7378H4SDR SWAA2020021941474Stanchion · crackedAFT CARGO BAY BULKHEAD STANCHION ASSEMBLY 149A8118-3 CRACKED AT BS. 947. / R&R STANCHION IAW SRM.Feb 1, 2020 · N7824A · Boeing 7377BKSDR SWAA2020020541032Bulkhead · crackedR/H MAIN LANDING GEAR FORWARD BULKHEAD AT B.S. 540 VAPOR BARRIER CRACKED IN TWO (2) LOCATIONS. / REPAIRED BARRIER PER REPAIR 57 EA-07683 FOR FURTHER CORRECTIVE ACTION REF 943 & #V005123 / REPETITIVE ACTION REQUIRED: / REMOVE ALUM FOIL TAPE AND PERFORM DETAILEDFeb 1, 2020 · N8600F · Boeing 7378H4SDR AALA2020020549062Bulkhead Web · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER BETWEEN RBL 34 AND RBL 36 AT THE 4TH BAY OUTBOARD OF THE KEEL BEAM. REPAIRED VAPOR BARRIER PER AARD 57-10-40-9 AND SRM 57-10-10-2R2.Jan 31, 2020 · N981AN · Boeing 737823SDR SWAA2020022094560Bulkhead Web · crackedLOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 56. / R&R VAPOR BARRIER PER SRM & DWG.Jan 30, 2020 · N425LV · Boeing 7377H4SDR REXA2020021230202Bulkhead · damagedAFT FUSE FS 621 BULKHEAD DAMAGED FROM SCREW SHANKS @ RBL 9, 18, 27, 36 AND LBL 18, 27 APPRX 28" ABOVE FLOOR REPAIRED FS 621 BULKHEAD AT RBL 9,18,27 AND LBL 18 AND 27 IAW REO 601R-53-61-2155 REV A. REPAIRED FS 621 BULKHEAD AT RBL 36 IAW REO 601R-53-61-1285 REVJan 30, 2020 · N8943A · Cndair CL6002B19SDR DALA2020013000695Doubler · corrodedREMOVED DOUBLER ON LOWER INBD OF PRESSURE BULK HEAD DUE TO CORROSION. REQUIRES OPEN HOLE INSP BHEC. NO CRACKS NOTED QC1988. REPLACED WITH NEW DOUBLER TO AFT PRESSURE BULKHEAD PER SRM 51-40.Jan 30, 2020 · N964AT · Boeing 717200
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