JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 SWAA2022041982724Structure · crackedCRACK FLOOR STRUCTURE INNER CHORD LOCATED BS303.9 AT LEVEL STR17L AT FWD GALLEY AREA 2022-122214 / [01] REPLACED INNER CHORD LOCATED BS267 TO BS360 TO AT LEVEL STR17L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8110 REV A <BR>SDR SWAA2022041982727Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND RBL31 FWD GALLEY AND LAV 2022-122220 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND RBL31 FWD GALLEY AND LAV IAW SRM B737-700 51-40-02 AND DWG 141ASDR VNAA202203151111Skin · gougedDURING ROUTINE MAINTENANCE AT DAYTON OH (DAY). THE MAINTENANCE TEAM REPORTS A FUSELAGE SKIN GOUGE AT FS661.00+16 BELOW STGR19R. THE GOUGE IS 0.004Ï¿½ DEEP AND 0.25Ï¿½ WIDE AND .5Ï¿½ LONG. THE SKIN PANEL, P/N SH690-33124-15, IS MADE FROM 0.118Ï¿½ THICK 2024-T3 SDR IXXA2022061306Floor Support · corrodedALC BALLMAT SUPPORT STRUCTURE CORRODEDSDR IXXA2022051805Shear Tie · corrodedSHEAR TIE AT STA 1395 BETWEEN STRINGERS 3R-38R CORRODEDSDR SWAA2022041882333Retainer · brokenFOUND 1 EACH REAINER ASSY-SLIDE BROKEN AT STOWAGE INST-BOOK / [01] REMOVED AND REPLACED 1 EACH RETAINER ASSY-SLIDE AT STOWAGE INST-BOOK; AS PER REF: SRM 51-40-02-0G-0;[02] VERIFIED STEP1.SDR AALA202203104777Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CAPTAIN'S #2 WINDOW FRAME LOCATED AT STA 196.5 AND WL 246.1. REPAIRED PER SERVICE BULLETIN 737-53-1336SDR AALA202203106711Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FIRST OFFICER'S #3 WINDOW POST LOCATED AT STA 220 AND STR 11R. REPAIRED POST PER EO 5319J023-008.SDR IPXA2022031079952Frame · noneINSPECTION TYPE:SEG1PREVIOUS REPAIR FOUND DURING FRAME INSPECTION AT STA 1480, S26R.WORKED PER VT MAE EA 757-5360-27-A2845 REV -SDR IPXA2022031079946Frame · noneINSPECTION TYPE:SEG1LOWER FRAME GOUGED AT STA 1380 R/H BY STR 26RREPAIRED PER VT MAE EA 757-5360-27-A2850 REV-SDR IXXA2022061313Frame Angle · corrodedCORROSION ON THE UPPER CHORD OF FRAME 1562SDR IXXA2022051803Ceiling Panel · corrodedCORROSION ON 2 ALC CEILING SUPPORTS, FROM STA 1285 TO STA 1307 AT RBL80 LOCATED ABOVE ALC DOORWAYSDR IXXA2022051801Stiffener · corrodedCORROSION ON THE WASTE VALVE BOX, FROM STA 1567 TO STA 1575SDR SWAA2022040782013Channel · crackedFWD ENTRY DOOR MOP SILL CRACKED AT BS 309 LBL 56 WL 208. / [01] REMOVED FWD ENTRY DOOR MOP SILL AT BS 270 - BS 360 LBL 56 WL 208 IAW SRM 51-40-02-0G-0;[02] PRIOR TO REMOVING FWD ENTRY DOOR MOP SILL; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1 PARG 4;[03] VSDR IPXA2022031480092None · damagedINSPECTION TYPE:A300DAMAGED CORNERSREPAIR IAW SREO A300-5320-42722-F.SDR FDEA202203090452Angle · crackedMAIN CABIN FLOOR SUPPORT SPLICE ANGLE IS CRACKED AT APPROX. STA 1575, LBL 85 REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT SPLICE ANGLE AT APPROX. STA 1575 AND LBL 85 IAW BAC SWG 146T5650, REV. C.SDR FDEA202203090451Angle · crackedMAIN CABIN FLOOR SUPPORT SPLICE ANGLE IS CRACKED AT APPROX. SAT 1575, RBL 85 REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT SPLICE ANGLE AT APPROX. STA 1575 AND RBL 85 IAW BAC DWG 146T5650, REV. C.SDR CALA2022031000627None · noneAFT CARGO PIT STRINGER 42 LEFT BETWEEN FRAME 63-64 HAS CORROSION A3NB-53-4-6179 PER HAECO LCQ NON ROUTINE 9298197/30197 GENERATED BY V052030 REMOVED & INSTALLED STRINGER @ FRAMES 60-64, 42L STR. IAW A320 T ASK 51-72-11-11-001, TASK 53-41-13-283-002 & TASK 51-7SDR 2A6D620220309001Bulkhead · usedDAMAGE TO THE 15° BULKHEAD LH POST (PN: 350A21-1031.33) WAS NOTED IN THE FORM OF CHAFING. THE CHAFING DAMAGE IS APPROXIMATELY 0.40” IN LENGTH, 0.07” IN WIDTH AND 0.017” IN DEPTH.SDR FDEA202203090443None · noneMAIN DECK FR63 -Y2462 SEAT TRACK BROKEN. EAT TRACK PER A300-600F SRM53-10-16-201 PARA.4. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100SDR FDEA202203081165Seat Track · corrodedREPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 745 - 785 LBL 8.5 HAS EXISTING SEAT TRACK REPAIR DOT 35. REPAIRED PER SRM 53-00-52 FIG.201, REPAIR 1.SDR FDEA202203081164Seat Track · corrodedREPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 745 - 8055 LBL 27.5 HAS EXISTING SEAT TRACK REPAIR DOT 34. REPAIRED PER SRM 53-00-52 FIG. 201, REP. 1.SDR FDEA202203081163Seat Track · corrodedREPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 745 - 765 LBL 75.5 HAS EXISTING SEAT TRACK REPAIR DOT 33. REPAIRED PER SRM 53-00-52 FIG. 201. REP. 1SDR FDEA202203081162Seat Track · unknownREPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX. 625 - 645 LBL 8.5 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOSULY INSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.SDR FDEA202203081161Seat Track · corrodedREPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX 585 - 645, RBL 27.5 HAS EXISTING SEAT TRACK REPAIR DOT 31. REPAIRED PER SRM 53-00-52 FIG. 201 REP. 1SDR FDEA202203081160Seat Track · unknownREPAIR ASSESSMENT: MAIN DECK L/H SIDE STA APROX 625 - 645, LBL 48 HAS EXISTING SEAT TRACK REPAIR. EXISTING MAJOR REPAIR PREVIOUSLY INSSTALLED PER SRM 53-00-52-2R REPAIR 1, FIG. 201, SHT. 1 - 3.SDR FDEA202203081159Seat Track · corrodedREPAIR ASSESSMENT: MAIN DECK R/H SIDE STA APROX 615 - 655, RBL 48 HAS EXISTING SEAT TRACK REPAIR DOT 29. SEATTRACK SPLICE REPAIR PER SRM 53-00-52 FIG. 201, REP. 1.SDR FDEA202203081152Stiffener · unknownREPAIR ASSESSMENT: CENTER W/W, R/H SIDE STA APROX 1451 HAS EXISTING STIFFENER / DOUBLER REPAIR DOT 28. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED BY PREVIOUS OPERATOR LUFTHANSA EI: L2009A53B-002.SDR FDEA202203081150Membrane · unknownREPAIR ASSESSMENT: FWD AVIONICS COMP. FLITH DECK FLOOR LEVEL STA APROX. 366, X= 0, Z= -27 HAS EXISTING WEB REPAIR DOUBLER. EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 53-10-51-2R REPAIR 1, FIG. 202, SHT. 1 - 4.SDR FDEA202203081064Fitting · unknownREPAIR ASSESSMENT: L/H SIDE NOSE LANDING GEAR TRUNING STA APROX 595 HAS EXISTING STRAP REPAIR DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-10-14-2R REPAIR 2, FIG. 201, SHT. 1 -4. REPAIR REQUIRES REPETITIVE INSPECTION OF HFEC EVERY 250 CSDR FDEA202203081062Fitting · noneREPAIR ASSESSMENT: R/H SIDE NOSE LANDING GEAR TRUNING STA APROX 595 HAS EXISTING STRAP REPAIR DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 53-10-14-2R REPAIR 2, FIG. 201, SHT 1 - 4. REPAIR REQUIERES REPETITIVE INSPECTION OF HFEC EVERY 250 CSDR AALA202203223049Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT HAND PASSENGER / CREW DOOR CUT OUT LOWER SILL PLATE AT FR 68 AND -Y1450. REPAIRED SILL PLATE PER SRM 53-41-14-300-001.SDR QXEA2022031400113Support · corrodedCORROSION ON FWD RH SILL BETWEEN FR 12-FR14 AND Y= +47". REMOVED AND REPLACED FWD RH SILL BETWEEN FR 12-14 AND Y= +47 IAW SRM 51-40-08.SDR R61A2022031400206Skin · dentedDENT FROM BIRD STRIKE ON FWD FUSELAGE NEAR F/O WINDSHIELD FROM FRA 2 TO FRA 4 AND STR 2R TO 4R. REPAIRES DENT IAW EMB ETD2022-170-008549. REF VP-010016-2022 N/R #1 AND LP R958122.SDR FDEA202203080439None · noneMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR58, BETWEEN Y1456 AND Y1959. REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR58, BETWEEN Y1456 AND Y1959. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMSDR VNAA202203089991Seat Track · corrodedLBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 693 TO 863.SDR REXA2022040600564Threshold · corrodedSERVICE DOOR THRESHOLD IS CORRODED AROUND SCREW HOLES & HAS 1 BROKEN NUTPLATE - REPLACED SERVICE DOOR THRESHOLD I/A/W CRJ-900 SRM 51-40-11-001-001-A01.SDR FDEA202203070425None · noneCOCKPIT FLOOR FWD OF STEP DOWN IS PUNCTURED ACCOMPLISHED FEDEX EA # F-5310-T0367130 : FUSELAGE - MAINFRAME - CABIN FLOOR STA 300- 312 BL 0 - LBL 20, PUNSDR IXXA2022061311Web · corrodedFLOOR WEB CORRODEDSDR IXXA2022061309Stringer · corrodedSTRINGER FLANGE CORRODED STA 434SDR SIMA20220306001None · noneSSI: 53-32-005 AFT GALLEY FLOOR RH SHEAR PANEL CORRODED BETWEEN FR 87-88 (MARKED) (LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY RH SHEAR PANEL BETWEEN FR 87-88 IAW EMB 175 SRM 51-40-02, EMB 175 SRM 51-40-08 AND EMB 175 SRM 51-21-02.SDR JR2R20220306910Skin · dentedUPPER LH FUSELAGE SKIN DENTED AT FWD BULKHEADSDR IXXA2022061310Support Bracket · corrodedCORROSION ON THE BULK CARGO CEILING SUPPORTSDR SWAA2022041880329Barrier · crackedRIGHT MLG WHEEL WELL VAPOR WEB FIBERGLASS PANEL CRACKED WITH TEMPORARY REPAIR AT B.S. 663.75 R.BL. 35'. / [01] MESUREMENT;[02] CLEANED AREA AND STOP DRILL CRACK AT R/H MLG WHEEL WELL VAPOR BARRIER AS PER BOEING 737 SRM 51-70-04-2R-10 REPAIR 10.;[03] PERFORMED SDR SWAA2022041880330Angle · crackedLEFT MLG WHEEL WELL VAPOR WEB LOWER VERTICAL ATTACH ANGLE CRACKED AT B.S. 663.75 L.BL. 26'. / [01] REMOVED VERTICAL ANGLE CRACKED AS PER B-737-700 SRM 51-40-02-OG-0;[02] LOCATED AND DRILLED NEW STIFFENER [ANGLE] AS PER B-737-700 SRM 51-40-02-OG-0;[03] VERIFIEDSDR AALA202203315231None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5. **SUPPLEMENTAL REPORT FOR AALA202203285231TO CHANGE SECTION 7 CORROSION LEVEL TO RESDR AALA202203301669None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5. **SUPPLEMENTAL REPORT FOR AALA202203301669 TO CHANGE SECTION 7 CORROSION LEVEL TO SDR AALA202203281669Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5.SDR AALA202203285231Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5.SDR SWAA2022032880294Stiffener · crackedCRACK VAPOR VARRIER STIFFENER LOC APROX RBL 25 OF BST 663.75 AT MAIN WHEEL WELL COMPARTME 2022-98618 / [01] REPLACED STIFFENER LOC. ON VAPOR VARRIER APROX RBL 25 OF BST 663.75 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DRAWINGS 111A1000
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