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 SWIA202265121None · corrodedAFT WET AREA SHEAR CLIP CORRODED AT FR 85 AND 28R (C-CHECK RO 03-19-2022) REMOVED AND REPLACED SHEAR CLIP AT FRAME 85, BETWEEN STRINGER 27R - 28R, REF EMB175 SRM 51-40-08, SEE CONTINUATION CARD FOR WORK PERFORMED. PART REPLACED WITH OEM PART NO CHANGE TO WMar 1, 2022 · N244SY · Emb ERJ170200LRSDR SWIA202265120None · corrodedCORROSION ON SHEAR CLIP AT FR88 BETWEEN STGR 27R-28R. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED SHEAR CLIP AT FRAME 88 BETWEEN STRINGERS 27R AND 28R REF EMB175 SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.PART CHANGE WITH OEM PART NO CHANGE TOMar 1, 2022 · N244SY · Emb ERJ170200LRSDR SWIA202265119None · corrodedCORROSION ON SHEAR CLIP AT FR87 BETWEEN STGR 27R-28R. (C-CHECK RO 03-19-2022) REMOVED AND REPLACED SHEAR CLIP AT FRAME 87 BETWEEN STRINGERS 27R AND 28R REF EMB175 SRM 51-40-08. SEE CONTIUATION CARD FOR WORK PERFORMED. PART REPLACED WITH OEM PART NO CHANGE Mar 1, 2022 · N244SY · Emb ERJ170200LRSDR DALA2022030101285None · none(LOG 6822842) DURING INSPECTION FOUND CRACK LOCATED LBL 45 LBS 663.75 WING /CENTER SECTION REAR SPAR PRESSURE WEB. COMPLETED REPAIR INSTRUCTIONS PER B737-800 SRM 57-10-10-2R-4.Feb 25, 2022 · N3766 · Boeing 737832SDR CALA2022022100468Pressure Blkhd · damagedRII INSPECTION REQUIRED PRESSURE BULKHEAD AND J & Y CHORDS AT STA. 100 ARE BEING REPLACED DUE LIGHTNING STRIKE DAMAGE. REF LP 7695225. REQUIRED AS MAJOR REPAIR. AN ESFR MUST BE ACCOMPLISHED AND RECORDED. COMPLETED/FILED ESFR FORM. SFR 1027782. COMPLETED/FILED Feb 21, 2022 · N29981 · Boeing 7879SDR SWAA2022040476103Bulkhead · crackedAFT CARGO COMPT. FWD BULKHEAD PANEL 141LW CRACKED / [01] RECIVED NEW PANEL 141LW AND REPLACED AS PER B737-700 AMM 25-52-01-201-801-NG PANEL WILL BE INSTALL ON CLOSING CARD TTG8Q00AME14;[02] VERIFIED 1Feb 20, 2022 · N425LV · Boeing 7377H4SDR SWAA2022040476101Bulkhead · crackedAFT CARGO COMPT. FWD BULKHEAD PANEL 142NWB CRACKED/DAMAGED / [01] RECIVED NEW LINING PANEL 142NWB AND REPLACED AS PER B737-700 AMM 25-52-01-201-801-NG. PANEL WILL BE INSTALL ON CLOSING CARD TTG8Q00AYAJG;[02] RECIVED NEW LINING PANEL 142NWBAND REPLACED AS PER BFeb 20, 2022 · N425LV · Boeing 7377H4SDR SWAA2022032076094Panel · crackedCRACK BULKHEAD PANEL 142NWA AFT CARGO COMPARTMENT 2022-85145 / [01] TOOL USED: CALIPER P/N: 700-113-10; S/N: 0033158; DUE DATE: 01-OCT-22;[02] REPAIRED BULKHEAD PANEL 142NWA AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805. PARA. 4.F. SEE INDIVIDUAL Feb 20, 2022 · N7727A · Boeing 737*SDR SWAA2022032076093Panel · crackedCRACK BULKHEAD PANEL 142NWB AFT CARGO COMPARTMENT 2022-85147 / [01] TOOL USED: CALIPER P/N: 700-113-10; S/N:0033158; DUE DATE: 01-OCT-22;[02] REPAIRED BULKHEAD PANEL 142NWB AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805 PARA. 4.F. SEE INDIVIDUAL SIFeb 20, 2022 · N7727A · Boeing 737*SDR SWAA2022030373418Stringer · crackedSTR 15L IS CRACKED AT BS 295.5 / REMOVED FASTENER ON STRINGER 15 L BTW B/S 277 TO B/S 303.9 IAW SRM 51-40-02;[04] UPDATE STEP #1 PARTIAL;[05] UPDATE STEP #2 PARTIAL;[06] UPDATE STEP #3 PARTIAL;[07] VERIFIED WORK;[08] VERIFIED CORRECTIVE ACTIONS 1-3;[09] REQUESFeb 16, 2022 · N469WN · Boeing 737*SDR DALA2022021701062None · noneSHIP 175 FOUND A CRACK AT THE 3RD FASTENER FROM THE TOP OF THE INSPECTION AREA ON THE BS1725 BULKHEAD OUTER CHORD STRAP AT STR-7R, CORRECTIVE ACTION: DAMAGE AREA REPAIRED AS PER B767-300 SRM53-80-01 -2R REPAIR 5 (2117874)Feb 11, 2022 · N175DN · Boeing 767332SDR SWIA202265461None · corrodedFS693 BULKHEAD LOWER CAP ANGLE HAS CORROSION AT APPROX. STGR 26R-26L. (C-CHECK RO 4/25/2022) : REMOVED DAMAGED FS693 BULKHEAD LOWER CAP ANGLE BETWEEN STGR 21L AND 21R. REF. CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 AND INSTALLED NEW FFeb 10, 2022 · N549CA · Cndair CL6002D24SDR SWAA2022032070229Bulkhead · distortedAFT CARGO COMPARTMENT FWD BULKHEAD UPPER LH #141LW SURFACE WAVY/DISTORTED. / [01] FABRICATED AFT CARGO COMPARTMENT FWD BULKHEAD UPPER LH#141JW IAW B737-700 AMM 25-52-01-201-801-NG MATERIALS USED A60SG4W;[02] (CORRECTING STEP 1) FABRICATED AFT CARGO COMPARTMENTFeb 8, 2022 · N946WN · Boeing 737*SDR AALA202202283956Support · corrodedAIRCRAFT IN BASE MAINTENANCE: LOWER CHANNEL OF REMOVABLE BULKHEAD CORRODED AT STA 500I AND LEFT BUTT LINE 24 TO RIGHT BUTT LINE 24. REMOVED AND REPLACED LOWER CHANNEL OF REMOVABLE BULKHEAD PER SRM 51-40-02.Feb 8, 2022 · N827NN · Boeing 737*SDR 2A6D20220208002Skin Panel · dentedDENT DAMAGE TO ENGINE DECK. THE DAMAGE IS LOCATED AT STA 4387 WL 1780 RBL 254. AND MEASURES APPROXIMATELY 0.048” IN DEPTH AND 1.4” IN DIAMETER.Feb 8, 2022 · N491LG · Snias AS350B3SDR 2A6D20220208001Skin Panel · chafedCHAFING WAS DISCOVERED ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR LH PASS THROUGH. THERE ARE SEVERAL CHAFE DAMAGES AT THE PASS-THROUGH, WITH THE LARGEST CHAFE MEASURED TO BE APPROXIMATELY 0.229” AND 0.007” DEEP. THERE IS ALSO AN ENLARGED ANCHOR NFeb 8, 2022 · N491LG · Snias AS350B3SDR SWAA2022032169957Bracket · crackedL/H STA 540 UNDER ACCESS DOOR 192CL ANTIC ICE DUCT SUPPORT BRACKET CRACKED / [01] REMOVED AND REPLACED ANTIC ICE SUPPORT BRACKET AT L/H STA 540; INSIDE ABOVE ACCESS DOOR 192CL AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED 1.Feb 7, 2022 · N946WN · Boeing 737*SDR JJBA20210207018Not Reported · not reportedCNTR OMEGA BEAM - FR 46 THRU FR 53 BL "0" I/B LWR FLANGE - HAS CORROSION MULTIPLE LOCATIONS. REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAME 46 THRU FR 53Feb 7, 2022 · N12145 · Emb EMB145XRSDR JJBA20220207017Not Reported · not reportedLH OMEGA BEAM FR 38 + 5 THRU FR 46 I/B LWR FLANGE HAS CORROSION MULTIPLE LOCATIONS. REMOVED AND REPLACED LH OMEGA BEAM AT FRAME 38 + 5 TO FRAME 46Feb 7, 2022 · N12145 · Emb EMB145XRSDR SWAA2022032169858Stiffener · crackedFWD OF L/H MAIN WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST HAS STEFFINER CRACKED @ LOWER END MKD DOT / [01] REMOVED DAMAGE STEFFINER AT FWD OF L/H MAIN WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST AS PER B737-700Feb 6, 2022 · N946WN · Boeing 737*SDR SWAA2022032176955Vapor Barrier · debondedLOWER FUSELAGE L/H WHEEL WELL VAPOR BARRIER LBL 35' AND 9' FROM BOTTOM PREVIOUS REPAIR SEALANT DISBONDING / [01] PREPARED DAMAGEAREA FOR DRY-OUT AT VAPOR BARRIER B737-700 51-70-2R-0;[02] VERIFIED STEP #1.;[03] PERFORMED DRY OUT ON L/H VAPOR BARRIER AS PER B737Feb 4, 2022 · N946WN · Boeing 737*SDR SWAA2022022366939Bulkhead · crackedBS 663 LOWER BULKHEAD IS CRACKED AT R.B.L. 50 W.L. 158. DAMAGE OUT OF LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D. REMOVED AN APPROXIMATE 13'X.01' LENGTH OF CRACK DAMAGE FROM AN AREA LOCATED 46.5' FROM THE IN BOARD EDGE AND 5.5' FROM UPPER EDGE IAW SRM 51-70-04-2Feb 2, 2022 · N7725A · Boeing 73776NSDR DALA2022020100659None · none(LOG 8479733) DURING SERVICE CHECK FOUND 2(EA) CRACKS ON FWD MWW VERTICAL PRESSURE WEB BS663, LBL34, AND LBL44. INSTALLED REPAIR PER B737-800 SRM 57-10-10 REPAIR #4.Jan 28, 2022 · N378DA · Boeing 737832SDR SWAA2022013163934Intercostal · crackedFWD CARGO RH INTERCOSTAL ABOVE AC MIX MANIFOLD IS CRACKED . ; / [01] REMOVED AND REPLACED FWD CARGO RH INTERCOSTAL ABOVE AC MIX MANIFOLD PER SRM 51-40-02 AND AMM 20-50-11.Jan 25, 2022 · N8648A · Boeing 7378H4SDR SWAA2022021063838Bracket · crackedAFT CARGO FWD BULKHEAD BRACKET SUPPORT CRACK; STA 727 RBL 5 ; / [01] REMOVED SUPPORT BRACKET ON AFT CARGO FWD BULKHEAD STA 727 PER REF 737 SRM 51-4-02-0G-0; [02] CORRECTION REMOVED AFT CARGO SUPPORT BRACKET; FWD BULKHEAD STA 727 PER REF. 737 SRM 51-40-02-0G-0;Jan 24, 2022 · N791SW · Boeing 7377H4SDR R61A2022020300088Stringer · corrodedSTRINGER 22L CORRODED BETWEEN FRAMES 80 - 81 IN AFT CARGO. PERFORMED A STRINGER SPLICE REPAIR ON STRINGER 22L FROM FRAME 78/79 TO FRAME 84 REF ETD2022-170-001953Jan 21, 2022 · N227JQ · Emb ERJ170200LRSDR SWIA202265399None · crackedFS 280 BULKHEAD AFT SIDE, UPPER WEB AND INBD CHANNEL BENT WITH POSSIBLE CRACK NEAR CEILING. (C-CHECK RO 4/20/2022) REPAIRED FS 280 BULKHEAD AFT SIDE UPPER WEB AND INBD CHANNEL IAW MHIRJ REO 601R-53-11-3755 REV -- DATED 2022-03-16. COMPLIED WITH SKY CAJan 19, 2022 · N479CA · Cndair CL6002B19SDR R61A2022020300087Crossbeam · corrodedAFT WET AREA HAS CORROSION AT FRAME 84 ON THE CROSS BEAM ON THE LH SIDE AS MARKED. FABRICATED AND INSTALLED DOUBLER PER SRM 53-00-10/REPAIR 03.Jan 19, 2022 · N227JQ · Emb ERJ170200LRSDR CALA2022011700156Stringer · damagedSTRINGER S-21L IS BROKEN BETWEEN STA.400 AND STA.420 DUE TO GROUND DAMAGE. VISUALLY INSPECTED AREA OF REMOVED DAMAGED STRINGER 21L BETWEEN STA 380-440 LH. NO FURTHER DAMAGE NOTED. OK TO CONTINUE CUT AND REMOVED DAMAGED STRINGER SECTION BETWEEN STA.380 AND STAJan 14, 2022 · N16713 · Boeing 737724SDR JJBA20220110011Not Reported · not reportedCORROSION - "Y" - 18 AT FR 23 THRU FR 29 +5 OMEGA BEAM I/B LWR FLANGE - MULTIPLE LOCATIONS. REMOVED AND REPLACED OMEGA BEAM AT FR 23 - FR 29 +5"Jan 10, 2022 · N16147 · Emb EMB145XRSDR SWAA2022021159626Panel · elongatedELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT ; 2022-11300 / [01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A2510 ; SHEET : 4 REV : FROM MATERIAL: CONOLITE P/N: A60SG4W THK 0.060? P.O: 2021Jan 9, 2022 · N453WN · Boeing 737*SDR CALA2022011000089Stringer · damagedSTRINGER S-21L IS BROKEN BETWEEN STA.400 AND STA.420 DUE TO GROUND DAMAGE. VISUALLY INSPECTED AREA OF REMOVED DAMAGED STRINGER 21L BETWEEN STA 380-440 LH. NO FURTHER DAMAGE NOTED. OK TO CONTINUE CUT AND REMOVED DAMAGED STRINGER SECTION BETWEEN STA.380 AND STAJan 9, 2022 · N16713 · Boeing 737*SDR SWAA2022013159334Bulkhead · corrodedCORROSION FWD CARGO COMPARTMENT AFT BULKHEAD SIDEWALL SUPPORT ANGLE BS 500D RBL 25 ; / [01] UPDATED MEASUREMENT TABLE; [02] EVALUATED CORROSION; FOUND 0.045 MATERIAL REMAINING FROM BS 500D RBL 26 WL156 MAX ALLOWABLE OF NO LESS THAN 0.056 REQUIRED IN A 1'X1' ARJan 7, 2022 · N233LV · Boeing 7377H4SDR DALA2022011000161None · none(LOG 2078682) DURING INSPECTION FOUND "OIL CAN" CONDITION ON AFT PRESSURE BULKHEAD WEB STA 1016, BETWEEN BL-0 AND S-5L , UPPER SIDE. "OIL CAN" CONDITION ON AFT PRESSURE BULKHEAD WEB STA 1016, BETWEEN BL-0 AND S-5L , UPPER SIDE WAS REPAIRED PER ETI-37-21-542 REJan 7, 2022 · N397DA · Boeing 737832SDR V0XD20220206003Bracket · corrodedCORRODED AT BRACKET. LOCATION: FRAME STATION: 285.00, RIGHT BUTT LINE: 9. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET FITTING (P/N: SH670-32149-3) AT FRAME STATION 285.00, RIGHT BUTT LINE 09 IN ACCORDANCE WITH CRJ STRUCTURAL REPAIR MANUAL 51-40-21-001-001-Jan 6, 2022 · N525AE · Cndair CL6002C10SDR YENA2022031400191Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 TO PRESSURE BULKHEAD ATTACHMENT AREA FWD FACE AT FASTENER HOLE LOCATED 1 INCH BELOW ST30LH LEVEL, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, CRACK LENGTH ARE L1=0.375 INCH APPROX, L2=0.28 0 INCH APPROX IN FWD CAJan 5, 2022 · N506JB · Airbus A320232SDR YENA2022031400188Bulkhead · crackedDURING HEAVY MAINTENANCE, (E/C A21-1362-01) FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / BULKHEAD / CRACKS AT FASTENER HOLES – PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)Jan 5, 2022 · N506JB · Airbus A320232SDR CALA2022010700039Pressure Blkhd · crackedLEFT WW VERTICAL PRESSURE DECK WEB CRACKED APPROX 2" BETWEEN LBL 40.00 AND LBL 45.64 --- SEE PHOTO,S COMPLIED WITH HFEC REF NDT PART 6 51-00-00 23. CRACK VERIFIED. REF SRM 57-10-10-2R4 STEP 4B. PERFORMED HFEC PER STEP 4C NO C/W SRM 57-10-10 2R4 STEP 4E HFEC ONJan 5, 2022 · N16701 · Boeing 737724SDR CALA2022010700038Pressure Blkhd · crackedLEFT WW VERTICAL PRESSURE DECK WEB CRACKED APPROX 1" BETWEEN LBL 31.83 AND LBL 40.00 --- SEE PHOTO,S COMPLIED WITH HFEC REF NDT PART 6 51-00-00 23. CRACK VERIFIED. REF SRM 57-10-10-2R4 STEP 4B. PERFORMED HFEC PER STEP 4C NO C/W SRM 57-10-10 2R4 STEP 4E HFEC ONJan 5, 2022 · N16701 · Boeing 737724SDR DALA2022010400064None · noneSHIP 3248 CRACK INDICATION ON FRAME 35 BULKHEAD TO SKIN ATTACHMENT AREA LH SIDE AT OPEN FASTENER HOLE H16. CORRECTIVE ACTION: REPAIRED PER ER/A 595693-14AD REV ORIGINAL. (2074203)Jan 3, 2022 · N348NW · Airbus A320212SDR DALA2022010400063None · noneSHIP 3248 CRACK INDICATION ON FRAME 35 LH SIDE AT OPEN FASTENER HOLE COMMON TO BULKHEAD AND MILLED COUPLING H6. CORRECTIVE ACTION: REPAIRED PER ER/A 595693-14AD REV ORIGINAL. (2074200)Jan 3, 2022 · N348NW · Airbus A320212SDR DALA2022010300029None · noneSHIP 3248 NEED TO PERFORM DTA MONITOR CRACK INSPECTION ER/A 596106-14. CORRECTIVE ACTION: COMPLIED WITH ERA. OK TO CONTINUE ON MON. (2072344)Jan 1, 2022 · N348NW · Airbus A320212SDR DALA2022010300033None · none(LOG 2070376) DURING INSPECTION FOUND CRACK ON STA 663, VAPOR BARRIER LEFT LOWER BEAM BTW LBL 6.15 TO LBL 10.54. AT MLG W/W. CRACK ON STA 663, VAPOR BARRIER LEFT LOWER BEAM BTW LBL 6.15 TO LBL 10.54. AT MLG W/W. WAS REPAIRED PER B737-800 SRM 57-10-10-2R-2.Dec 31, 2021 · N397DA · Boeing 737832SDR DALA2022010300009None · noneREF NRC 276 "WEAR MARKS ON OUTSIDE OF MATING SURFACE TO SLANT PANEL". SMOOTHED 3EA AREAS AND LOWEST READING WAS .092. ORIG MATL THICKNESS IS .125. REMOVED INBOARD SLANT PANEL BRACKET FOR FOM. ROUTED TO SHOP. COMPLIED WITH PRI 596194 -14 REV 0, REV,1, REV 2, REDec 31, 2021 · N998AT · Boeing 717200SDR SWAA2022013157203Angle · corrodedFWD CARGO AFT R/H BULKHEAD LOWER CURVED 'L' ANGLE AT STA 500D HAS CORROSION LOWER END. (MARKED) ; / [01] FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1.; [02] 1. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 05:56 UTC<BR>FOUND TO BE OUT OF LIMITS PER SRM 53-30-08Dec 30, 2021 · N917WN · Boeing 7377H4SDR DALA2022010300030None · noneSHIP 3248 NEED TO COMPLY WITH ERA INSPECTION ER/A 595693-14. CORRECTIVE ACTION: COMPLIED WITH ERA (CRACK INSPECTION) OK TO CONTINUE. (2072092)Dec 29, 2021 · N348NW · Airbus A320212SDR MK1Y20211226004None · noneDURING MAINTENENCE INSPECTION FOUND GOUGE ON AFT PRESSURE BULKHEAD, STA 1582, BETWEEN WL 190 AND WL 200.Dec 26, 2021 · N641AZ · Boeing 767332SDR SWIA202165838None · 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 23, 2021 · N933EV · Cndair CL6002B19SDR SWIA202164602None · corrodedLH FS.280 LOWER BULKHEAD WEB HAS CORROSION AT FLOOR LEVEL LBL12. (C-CHECK RO 2/22/2022) REMOVED AND REPLACED L/H FS280.00 LOWER BULKHEAD WEB. REF. CRJ700 SRM 53-11-10-201-004-A01.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Dec 17, 2021 · N713SK · Cndair CL6002C10SDR LR7A2021121303062Cap · corrodedDURING SCHEDULED C-9 CHECK UNDER JOB CARD HCHC5314, FOUND FS277.0E UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT LBL60 TO RBL60, WL143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0828. / PSE# 53-40-11, AD 2012-06-09Dec 13, 2021 · Lkheed 382G
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