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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2022052603098Tie Clip · crackedCRACK TIE CLIP LOCATED BS 277 S-10R AT PASSENGER CABIN 2022-230947 / [01] REPLACED TIE CLIP LOCATED BS 277 S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 141A1110; SHEET 18; REV._;[02] CORRECTED STEP 1. REPLACED TIE CSDR JJBA20220503006None · noneCORROSION ON FLOOR GUSSET FR20 BL0 - RBL 17, REMOVED AND REPLACED BEAMSDR SWAA2022052601813Angle · crackedCRACK ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN 2022-257561 / [01] REPLACED ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #141A8310SDR SWAA2022051000882Angle · crackedLH STA 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT LBL 9 / [01] REMOVED ALL FASTENERS AND TRIMMED OUT DAMAGED SECTION OF VAPOR BARRIER ANGLE IAW SRM 57-10-10-2R-5;[02] PERFORMED DETAILED VISUAL INSPECTION OF REPAIR AREA AND UNDERLYING STRUCTURE; NO DEFECTS NOTESSDR SWAA2022051200352Bulkhead · crackedAFT CARGO FORWARD BULKHEAD 142 NWB CRACKED A225-006 / [01] VERIFIED AND REPLACED AFT CARGO FWD BULKHEAD PANEL # 142NWB ON PARTS RACK IAW IPC 25-52-19-01B AND BOEING DWG# 453A25110 ID:0001 REV:C;[02] VERIFIED STEP 1 COMPLETE<BR>AUDIT C/WSDR SWAA2022052697417Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-207141 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. ;[02] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGESDR SWAA2022052697415Web · crackedCRACK WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA 2022-207128 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE 01-JUN-22;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 1SDR SWAA2022052597414Stringer · crackedCRACK STRINGER 16L BETWEEN BS294.5 TO BS303.9 AT PASSENGER CABIN 2022-207127 / REPAIRED STRINGER 16L BETWEEN BS294.5 TO BS303.9 AT PASSENGER CABIN B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. REPAIRSDR SWAA2022052597413Stringer · crackedCRACK STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN 2022-207139 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:210136503; DUE DATE: 11-APR-23;[02] TOOL MEASUREMENT ULTRASONIC THICKNESS USED P/N: 45MG S/N: 130060401 DUE DATE: 26-JSDR DALA2022042602923Tee Fitting · corrodedSHIP 1818 RH STA 955 FAIL-SAFE STRAP REMOVED "T" FITTING FOUND CORROSION. CORRECTIVE ACTION: RH STA 955 "T" FITTING REPLACED AS PER B767-400 SRM 51-40-02 RELEASE:65.00-03/16/22. REF TO W/C:5312-01170-10B-02. (2209027)SDR DALA2022042202845Tee Fitting · corrodedSHIP 1818 LH STA 955 FAIL-SAFE STRAP REMOVED "T" FITTING FOUND CORROSION. CORRECTIVE ACTION: LH STA 955 CORROSION "T" FITTING REPLACED AS PER B767-400 SRM 51 -40-02 RELEASE 65.00-03/16/22. REF TO W/C:5312-01170-10A-02. "T" (2206470)SDR SWAA2022051196165Web · corrodedCORROSION ON AFT CARGO BAY AT BS 1016+1 RBL 1. CORROSION FOUND ON ACB BS 1016+1 RBL 1 BULKHEAD WEB FRONT LOWER SIDE / [01] REMOVED CORROSION ON ACB BULKHEAD WEB BS 1016+1'' RBL1-6 IAW SRM 51-10-02-0G-0; MEASURES L=6.2'' X W=2'' TOOL USED CALIPER ID:ATS2381 S/NSDR LR7A2022041603098Cap · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS814 BULKHEAD INBOARD CAP CRACKED THOUGH FASTENER HOLE AT RBL61, WL179. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR# 1000726675. / PSE# 53-50-07, AD 2012-06-09SDR LR7A2022041603097Cap · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS814 BULKHEAD INBOARD CAP CRACKED THOUGH FASTENER HOLE AT LBL61, WL179. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-22. NR# 1000726672. / PSE# 53-50-07, AD 2012-06-09SDR DALA2022041902666None · noneA CRACKED AFT BULKHEAD IN THE NOSE LANDING GEAR WHEEL WELL STA 110 WAS FOUND (IN REF NRC 00167). SUMMARY OF NRC 00169: BULKHEAD WAS REPAIRED PER ERA 598690-14 REV. ORIGINAL SECTION I: TEMPORARY REPAIR. ACCOMPLISH THE SECTION II: REPETITIVE INSPECTIONS EVERY 24SDR SWAA2022051194219Pressure Web · crackedCRACK FOUND AT MAIN WHEEL WELL VERTICAL PRESSURE WEB BETWEEN RBL40.00 AND RBL 45.64 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH :0.843'. CRACK FOUND AT MAIN WHEEL WELL VERTICAL PRESSURE WEB BETWEEN RBL40.00 AND RBL 45.64 IAW NDTM PART 651-00-00 PROCEDUSDR SWAA2022051094381Vapor Barrier · crackedB.S. 663 VAPOR BARRIER IS CRACKED AT R.B.L. 42; W.L. 155 / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-10-10-0I-2; FIGURES 1-2; TABLE 2; ITEM [4].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4.D (1) (A) 1).<BR>DAMAGE WILL BESDR DALA2022041902730None · noneSHIP 3265 NEED TO COMPLY WITH AFT PRESSURE BULKHEAD INSP. CORRECTIVE ACTION: COMPLIED WITH ERA 543323-14AD REV C. INSPECT FOR CRACKS. OK FOR SERVICE. (2196390)SDR DALA2022041902726None · noneSHIP 3265 NEED TO INSPECT AFT PRESSURE BULKHEAD. CORRECTIVE ACTION: INSPECTED PER ERA 543323-14AD REV C. OK FOR SERVICE. (2196386)SDR DALA2022041902725None · noneSHIP 3265 NEED TO COMPLY WITH AFT PRESSURE BULKHEAD INSP. CORRECTIVE ACTION: COMPLIED WITH ERA 543323-14AD REV C. INSPECT FOR CRACKS. OK FOR SERVICE. (2196384)SDR DALA2022041902724None · noneSHIP 3265 NEED TO INSPECT AFT PRESSURE BULKHEAD. CORRECTIVE ACTION: INSPECTED PER ERA 543323-14AD REV C. OK FOR SERVICE. (2196377)SDR DALA2022041902723None · noneSHIP 3265 NEED TO COMPLY WITH AFT PRESSURE BULKHEAD INSP. CORRECTIVE ACTION: COMPLIED WITH ERA 543323-14AD REV C. INSPECT FOR CRACKS. OK FOR SERVICE. (2196376)SDR JJBA20220412008None · noneLH OMEGA BEAM AT FR 38 - FR 44 HAS CORROSION AROUND SURFACE OF FASTENER HOLES. REMOVED AND REPLACED LH OMEGA BEAM.SDR 2022F00184None · noneWHILE PERFORMING BOMBARDIER SB 670BA-53-044 REV F, FOUND LEFT FS 202.75 BULKHEAD TO HAVE BEEN PREVIOUSLY REPAIRED BY BOMBARDIER REO 690-53-11-703 AND REO 690-53-11-704. C/A: REPAIRED IAW MHIRJ REO 690-53-11-1411 REV -- DATED 2022-04-03 AND MESA AIRLINES RO CRJSDR 2022F00183None · noneWHILE PERFORMING BOMBARDIER SB 670BA-53-044 REV F, FOUND FASTENER HOLES AT LH STRINGER 13ATO HAVE BEEN PREVIOUSLY UP SIZED. REPAIRED IAW MHIRJ REO 690-53-11-1415 REV -- DATED 2022-03-25.SDR DALA2022092706306None · noneSHIP 3270 NEED TO COMPLY WITH ER/A 597588-14 SECTION II. CORRECTIVE ACTION: COMPLIED WITH ER/A 597588-14 SECTION II. (2188111)SDR A6WA202204068166Bulkhead · gougedBULKHEAD Z-MEMBER AT FS 621.00, CENTER, SHOWS DEEP GAUGE LOCATED AT THE TOP END. ****AIRCRAFT REMOVED FROM SERVICE**** REPAIRED BULKHEAD AFT VERTICAL STIFFENER AT FS 621.00 IAW EA# AWAC-CRJ253-01806SDR SWAA2022042791441Panel · crackedCRACK BULKHEAD PANEL 141SW AT AFT CARGO COMPARTMENT 2022-194770 / [01] EVALUATED CRACK BULKHEAD PANEL 141 SW AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 AMM 25-52-00-200-806 PARAGRAPH 6.D. (3) (4). DAMAGE SIZE: L=1IN; AND REPAIRED ASDR JJBA20220325011None · noneCORROSION FOUND ON THE OMEGA BEAM LOCATED BETWEEN FR59 TO FR 61, Y.00-19. REPAIRED OMEGA BEAM AT FR 59 - FR61 AND Y.00-16SDR JJBA20220325010None · noneCORROSION FOUND ON THE OMEGA BEAM LOCATED BETWEEN FR59 TO FR 61. REPAIRED OMEGA BEAM AT FR 59 - FR61 AND Y.00+16SDR DALA2022040402245None · none(LOG 2180906) DURING INSPECTION FOUND LH MAIN WHEEL WELL, FWD BULKHEAD, LOWER CENTER WEB IS CRACKED. LH MAIN WHEEL WELL, FWD BULKHEAD LOWER CENTER WEB WAS REPAIRED IAW SRM 57-10-10-2R-2 PAGE 1,16 FIG 202 AND 41-70-04-2R-10.SDR UIEA2022031900203Pressure Blkhd · corrodedBULK CARGO COMPARTMENT LOWER STRUCTURE STA 1582, THE PRESSURE BULHEAD SKIN CORROSION BETWEEN S-38L AND S-38R AFT FACE OF RIB(<P>CORROSION DAMAGE WAS REPAIRED AS PER MEXICANA MRO REF. TRE6753473, REVISION 01</P>)SDR SWAA2022042787611Vapor Barrier · crackedLOWER FUSELAGE CENTER WING VERTICAL BULKHEAD VAPOR BARRIER HAS SMALL CRACK @ RBL-15 ;I/B OF R/H A/C AIR EXIT EXHAUST CUTOUT MKD DOT / [01] MEASUREMENTS;[02] CLEANED DAMAGE AREA OF VAPOR BARRIER FOR REPAIR; STOP DRILL CRACK; AND PERFORMED DRY OUT ;FOUND NO WATESDR SWAA2022041986133Angle · crackedCRACK ANGLE LOCATED BS294.5 AND RBL53 AT LEVEL FLOOR STRUCTURE AT PASSENGER CABIN 2022-148046 / [01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A20231804 DUE DATE: 26-AUG-22;[02] REPLACED ANGLE LOCATED BS294.5 AND RBL53 AT LEVEL FLOOR STRUCTURE AT PASSENGESDR SWAA2022042085910Panel · deterioratedAFT CARGO ;FWD BULKHEAD PNL 142MW DETERIORATED. / [01] FABRICATED NEW AFT CARGO BULKHEAD PANEL 142MW IAW B737 AMM 25-52-01-201-801. USED REMOVE LINER AS A TEMPLATE.;[02] VERIFIEED STEP 1.SDR SWAA2022042085911Panel · deterioratedAFT CARGO ;FWD BULKHEAD PNL 141KW DETERIORATED. / [01] FABRICATED NEW AFT CARGO FWD BULKHEAD PANEL 141KW; USED OLD PANEL AS A TEMPLATED I.A.W B737 AMM 25-52-01-201-801.;[02] VERIFIED STEP 1.SDR SWAA2022041985223Bear Strap · crackedCRACK IN BEAR STRAP AT B.S. 294.5 BETWEEN STRINGERS 8 RIGHT AND 9 RIGHT JUST FORWARD OF FORWARD SERVICE DOOR. / [01] TRIMED DAMAGED AREA AT BEARSTRAP BS 294.5 BETWEEN STR 8 - STR 9 RIGHT JUST FWD OF FWD SERVICE DOOR L=1.2 W= 1.0 PER SRM 53-10-01-2R-6 REP. 6 STSDR SWAA2022041984731Bulkhead · crackedAFT CARGO BAY FWD BULKHEAD SUPPORT BRACKET IS CRACKED AT STA 727+2; WL 163; RBL 5. / [01] THIS PART DOES NOT HAVE ENTRY ON THE LOWER ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[02] VERIFIED CORRECTIVE ACTION SDR SWAA2022040784591Doubler · crackedRIGHT WHEEL WELL FWD BULKHEAD WEB BY EXHAUST BETWEEN RBL 15' AND RBL 25' I/B HOLE CRACKED / [01] FABRICATED NEW RIGHT WHEEL WELL FWD BULKHEAD DOUBLER BY EXHAUST BETWEEN RBL 15 - RBL 25. IRW B737-700 SRM 51-30-01-0G-0 AND DWG # 111A1511;[02] LOCATED AND DRILLEDSDR LR7A2022031603088Bulkhead Web · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS880 SIDE BULKHEAD WEB CRACKED THOUGH FASTENER HOLE AT LBL68, WL212. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR# 0075. / PSE# 53-50-07, AD 2012-06-09SDR LR7A2022031603087Bulkhead Web · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB3200, FOUND RH MLG WHEEL WELL FS477 SIDE BULKHEAD WEB CRACKED THROUGH THE NUTPLATE HOLE AT RBL80, WL207. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0074. / PSE# 53-40-17, SDR LR7A2022031603085Fitting · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB3200, FOUND RH MLG WHEEL WELL BOW BEAM LOWER FITTING CRACKED THROUGH FASTENER HOLE AT FS557, RBL61, WL143.5. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0061.SDR 2A6D20220315001None · usedCUSTOMER HAS REPORTED DAMAGE TO THE AFT BULKHEAD WEB (PN: 350A21-1036.60) IN THE FORM OF NUMEROUS
CHAFES. THE CHAFES WERE MEASURED TO BE ON AVERAGE 0.50” IN LENGTH WITH THE DEEPEST CHAFE
BEING 0.008” DEEP.SDR AALA202203151635Bulkhead · canningAIRCRAFT IN BASE MAINTENANCE: AFT PRESSURE BULKHEAD UPPER AFT SIDE HAS OIL CANNING BETWEEN BL-0 AND S-1R AT BS 1016. REPAIRED AFT PRESSURE BULKHEAD PER EA 334576.SDR SWAA2022040784589Vapor Barrier · crackedRT SIDE VAPOR BARRIER AT STA 663 FOUND CRACKED / [01] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT VAPOR BARRIER AT STA 663 FOUND CRACK 19'' OF LENGTH. REF B737-700 NDT PART 1 51-05-01PARAGRAPH 5.;[02] DRILLED STOP DRILL ON THE CRACK END. REF 57-10-1SDR DALA2022031001587None · noneSHIP 3259 PASSENGER CREW DOOR 832 DOES NOT PASS FUNCTIONAL TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER. OPS TEST GOOD. (2149137)SDR JR2R20220306909Bulkhead · dentedFWD BULKHEAD AT FS 169 DENTED AND CRACKED IN MULTIPLE LOCATIONSSDR UIEA2022022600170Failsafe · crackedFUSELAGE SECTION 45 STA 955 REAR SPAR BULKHEAD SIDE FITTINGS FAIL SAFE STRAP RH SIDE WITH CRACK INDICATION.(<P>FAIL SAFE STRAP WAS REPAIRED</P>)SDR KCSA202203031015Bulkhead · corrodedCORROSION - NOSE GEAR WELL - STA 340, 33" FROM L/H & R/H SIDES & 14 " FROM TOP OF WELLSDR SWAA2022033179332Bulkhead · corrodedCORROSION ON AFT CARGO BAY LOWER BULKHEAD AT BS 947 RBL 21-LBL 10. / [01] LOCATED AND DRILLED NEW TRACK P/N149A8118 IAW SRM 51-40-02 OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1.;[03] INSTALLED 10 HI-LOCK IAW SRM 51-40-02 AND DWG 149A8110 ID:0013 REV:B;[04]
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