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 JR2R20221011921Beam · corrodedFLOOR BEAM CORRODED BETWEEN FR90 AND FR90A AT RBL9SDR JR2R20221011920Gusset · corrodedFLOOR GUSSET CORRODED AT FR90A AND RBL9SDR JR2R20221011928Beam · corrodedFLOOR BEAM CORRODED BETWEEN FR89 AND FR90 AT RBL 9SDR JR2R20221011922Gusset · corrodedFLOOR GUSSETT CORRODED AT FR90 AND RBL9SDR JR2R20221011927Gusset · corrodedFLOOR GUSSET CORRODED AT FR89 AND RBL9SDR JR2R20221011924Gusset · corrodedFLOOR GUSSET CORRODED AT FR90 AND RBL24SDR JR2R20221011930Shear Panel · corrodedRH SHEAR PANEL CORRODED BETWEEN FR87 AND FR88SDR 2A6R2022101103Deck Plate · delaminatedDURING 1000 HOUR INSPECTION, DELAMINATION DAMAGE WAS DISCOVERED ON THE AFT CABIN FLOOR (PN: L533M1015104) ON THE LOWER SKIN PANEL (PN: L533M1416234) MEASURING APPROXIMATELY 8.5” X 7.75” AT THE FORWARD SIDE OF THE FLOOR. A DETAILED DESCRIPTION OF THE DAMAGE ANSDR JR2R20221011005Strap · corrodedFLOOR BEAM STRAP BETWEEN FR85 AND FR86 CORRODEDSDR JR2R20221011006Strap · corrodedFLOOR BEAM STRAP BETWEEN FR85 AND FR86 CORRODEDSDR JR2R20221011959Doubler · corrodedCORROSION FOUND AT FR14 IN THE FWD DRY AREA ON THE RH SIDE JUST BEFORE GALLEYSDR 2A6R2022101165201Deck Plate · corrodedDURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE COCKPIT FLOOR (PN: L533M1013108) AT THE RH FORWARD GROUNDING POINT. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDASDR SWAA2022111058364Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BTW BS 492.4 TO BS 500A AT LEVEL STR 26R WL 156.5 FWD CARGO COMPARTMENT 2022-562058 / [01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 492.4 TO BS 500A AT LEVEL STR 26R WL 156.5 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 SDR SWAA2022111058356Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022- 562039 / [01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02; SRM-51-40-02 AND DWG 143SDR SWIA202266715Rod · gougedPILOT DV WINDOW LOWER ROD IS GOUGED. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED PIOT DV WINDOW LOWER ROD. ADJUSTMENT CHECK GOOD. REF EMB 175 AMM 56-12-00.SDR SIMA20221009004Seat Track · corrodedSSI 53-21-005 RH FLOOR SEAT TRACK IS CORRODED BTW FRAMES 24-25. (LEVEL 2 CORROSION)-C/A-REMOVED CORROSION AND INSTALLED SPLICE DEVICE FITTINGS ONTO RH LOWER SEAT TRACK AT FR 24-25 IAW EMB 175 AMM 25-21-11SDR SIMA20221009003Seat Track · corrodedSSI 53-21-005 RH FLOOR SEAT TRACK IS CORRODED AT FRAME 32 (LEVEL 2 CORROSION)-C/A-REMOVED CORROSION AND INSTALLED SPLICE DEVICE REPAIR FITTINGS ON RH FLOOR SEAT TRACK AT FR 32 IAW EMB 175 AMM 25-21-11SDR FDEA202210092521None · noneMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSS BEAM CRACKED AT FR27, BETWEEN Y-450 AND Y-953.SDR 2022FA0000587Angle · corrodedCORROSION ON R1 DOOR ANGLE LOWER MAIN SILL AT BS 312SDR 2022F00389None · crackedCRACKED STRINGER CLIP BS 847 AT STRINGER 25L IN AFT CARGO PIT.SDR SWAA2022111057794Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 STR10R WL252.6 AT FWD GALLEY AREA 2022-561898 / [01] REPLACED TIE CLIP LOCATED BS277 STR10R WL252.6 AT FWD GALLEY AREA<BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 141A1110 REV -;[02] CORRECTED STEP 1 <BR>REPLACED TSDR HNAA2022102500290Beam · corrodedE938516 - CORROSION IN GALLEY AREA ON CENTER BEAM GUSSET .... REMOVED CORRODED GALLEY AREA CENTER BEAM GUSSET AND INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02, EMB 145 CPM 51-21-06, PIEDMONT BULLETIN 51-02.SDR AALA202211012639None · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO RIGHT TRANSITION PANEL BETWEEN 500D AND 500I HAS CORROSION LOCATED AT STR 25R AND RIGHT BUTT LINE 26. REMOVED AND REPLACED RIGHT TRANSITION PANEL PER SRM 51-40-02.SDR AALA202211018185None · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO RIGHT TRANSITION PANEL BETWEEN STATION 500B AND 500C HAS CORROSION AT STR 25 AND RIGHT BUTT LINE 26. REMOVED AND REPLACED TRANSITION PANEL. PER SRM 51-40-02.SDR AALA202210135705None · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT PASSENGER / CREW DOOR CUT OUT LOWER DOOR SILL PLATE AT FR 68 AND -Y1292. REPAIRED SILL PLATE PER SRM 53-41-14-300-001 PRINCIPLE 7.SDR SWAA2022111056933Angle · crackedCRACK ANGLE LOCATED BS 727B CEILING AREA LH SIDE AFT CARGO COMPARTMENT 2022-561842 / [01] REPLACED ANGLE LOCATED BS 727B CEILING AREA LH SIDE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A9490 REV- SHEET 21 SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRSDR AALA202210242486None · damagedAIRCRAFT IN BASE MAINTENANCE: STRINGER CLIP FOUND DAMAGED AT STA 947.5 AND STRINGER 18L. REMOVED AND REPLACED OLD STRINGER CLIP PER AARD 51-00-05-1.SDR SIMA20221006003None · corrodedAFT GALLEY R/H AFT SLICE PLATE FLOOR STRUCTURE AT FR90 IS CORRODED.(MARKED)(LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY R/H AFT SLICE PLATE FLOOR STRUCTURE AT FR90 IAW EMB-175 SRM 51-40-08, 51-21-01.SDR SIMA20221006002Panel Support · corrodedAFT GALLEY R/H PANEL SUPPORT AT FR 89 IS CORRODED.MARKED)(LEVEL 2 CORROSION)-C/A-RAR AFT GALLEY R/H PANEL SUPPORT AT FR 89 IAW EMB-175 SRM 51-40-08SDR SIMA20221006001None · corrodedAFT GALLEY CENTER SHEAR PANEL FLOOR STRUCTURE AT FR87-88 IS CORRODED ON TOP SIDE. (MARKED)(LEVEL 2 CORROSION) -C/A-REMOVED AND REPLACED AFT GALLEY CENTER SHEAR PANEL FLOOR STRUCTURE AT FR87-88 IAW EMB-175 SRM 51-40-08, 51-21-01, AND 51-40-02SDR AALA202210100316Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR INTERCOSTAL CORRODED LOCATED AT STA 960 AND RIGHT BUTT LINE 47. REMOVED AND REPLACED MAINT CABIN FLOOR INTERCOSTAL STA 960 AND RIGHT BUTT LINE 47 PER SRM 51-40-02-0G.SDR ABXA2023050985Failsafe · corrodedDURING AIRCRAFT C-CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED AN AREAS OF CORROSION ON THE UPPER SURFACE OF THE FAIL-SAFE STRAP (P/N 143T15910-2) INSTALLED ON THE FORWARD FRAME OF THE FORWARD LOWER CARGO DOOR JAMB. THE CORROSION WAS LOCATED AT STATION 53SDR R61A2022102100654Crossbeam · corrodedFWD FUSELAGE RH CROSS BEAM AT FR 14 CORRODED. R&R IAW SRM 53-00-10 REPAIR 03.SDR SIMA20221005001None · corrodedSSI# 53-10-027 FWD GALLEY R/H FWD SILL BETWEEN FRAMES 12 AND 14 HAS CORROSION (LEVEL 2 CORROSION)-C/A-RAR FWD GALLEY RH FWD SILL BETWEEN FRAMES 12 AND 14 IAW EMB-175 SRM 51-40-08SDR CALA2022100602707Floor Support · corroded(B757-53-3-0480) MAIN CABIN FLOOR STRUCTURE STA 720 RBL 20 TO RB L 50 UPPER STRAP CORRODED ON UPPER SURFACE. TRANSCRIBED FROM HA ECO GSO NRC# 9282322SDR SWAA2022111055637Scuff Plate · crackedCRACK CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-561756 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20289362;DUE DATE:03-DEC-22.;[02] REPAIRED CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975SDR IPXA2022101287082Spar · crackedINSPECTION TYPE:3CCENTER UPPER AUXILIARY TANK FRONT SPAR CLIP BETWEEN STA X17 AND X46 IS CRACKED.REPLACED CRACKED CLIP IN CTR UPPER AUXILIARY TANK IAW SRM 51-33-01 (MINOR)SDR CALA2022100602697Stop Fitting · crackedWHILE WORKING EA 5340-01724 REV C OP002, STEP 3.1 NDT NOTED A CRACK INDICATION IN DOOR STOP FITTING 1 BOTTOM IB HOLE AT 4:00 POS ITION FACING AFT. FRAME 68 LH REPAIRED LWR I/B HOLE AT L/H FR68 DOOR STOP FITTING #1 IAW SRM 5 3-41-12-300-010. AND INSTALLED DOOR SDR CALA2022100602696Fitting · crackedLH FRAME FOOT AT FR43 CRACKED IN OUTBOARD POSITION 3:00 FACING A FT. REPAIR BEFORE NEXT FLIGHT.SDR FDEA202210042461Fitting · noneACCOMPLISH FEDEX E.A. F-5310-T0357573-P2 REQUIRED, REPLACEMENT OF THE L4 DOOR LOWER HINGE SUPPORT FITTING P/N 146N8762-13. REMOVED AND REPLACED THE L-4 DOOR LOWER HINGE SUPPORT FITTING IAW BAC DWG 146N8739, REV. K AND FEDEX E.A. F-5310-T0357573-P2, TITLE: SDR SWAA2022110252307Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 344 AND 360 LBL 11 WL 208.1 IS CRACKED. 124-012 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK. CRACK LENGTH 0.750'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE 03/23.;[02]SDR SWAA2022110152296Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 277 AND 294.5 BL-0 WL 208.1 IS CRACKED. 124-001 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK. CRACK LENGTH 1.250'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE 03/23.;[02]SDR SWAA2022110152306Intercostal · crackedFWD CABIN INTERCOSTAL BETWEEN STA 344 AND 360 BL-0 WL 208.1 IS CRACKED. 124-011 / [01] PERFORMED HFEC INSPECTION PER B737 NDT PART 6 51-00-00 PROCEDURE 23; VERIFIED 2 CRACKS. CRACK LENGTHS ARE BOTH 0.750'. TOOL USED OLYMPUS NORTEC 600 B/C 172389; CAL DUE DATE SDR HNAA2022102500276Door Frame · corrodedE937764 - SSI 52-21-06 CORROSION ON LOWER FRAME AROUND RUBBER STOP ON RH EMERGENCY ESCAPE HATCH ... 4 REMOVED AND REPLACE LOWER FRAME AROUND RUBBER STOP ON RH EMERGENCY ESCAPE HATCH IAW EMB145 SRM 51-40-02 AND AMM 52-21-00.SDR R61A2022102400669Crossbeam · corroded"R/H PASSENGER FLOOR CROSS BEAM HAS CORROSION AROUND FASTENERS AT FRAME 17.REMOVED CORROSION FROM CROSSBEAM AT FR 17 BY CUTTING OUT DAMAGE , FABRICATING AND INSTALLING FILLERS AND L ANGLE DOUBLER REF EMB SRM 53--
00-10/REPAIR03"SDR R61A2022100700622Structure · crackedLH NLG SPIN BRAKE WEBBING FOUND CRACKED AND PREVIOUSLY STOP DRILLED. CRACK PROGRESSED BEYOND PREVIOUS STOP DRILL. REPAIRED DAMAGE IAW ETD2022-170-030541 REV. B.SDR FDEA202210022443Door Frame · crackedRH FWD CREW DOOR - FRAME SEGMENT CRACKED AT FR14C ITEM 40 REPLACED RH FWD CREW DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299 (ISSUE.G). TRACKING EA 6-5210-T0370794 P1 RAISED ANDSDR ASAA2022100140401Door Sill · corrodedFWD MAIN CABIN FLOOR SUPPORT, FWD ENTRY DOOR CUTOUT LOWER SILL, Z-CHANNEL UPPER SKIN HAS CORROSION, LBL-60, BS326. GROUNDED - YES. REMOVED CORROSION FROM THE FORWARD MAIN CABIN, FORWARD ENTRY DOOR LOWER MAIN SILL, INNER CHORD:ORIGINAL THICKNESS 0.090",REMOVED SDR ASAA2022100140400Intercostal · corrodedFWD MAIN CABIN FLOOR SUPPORT, U-CHANNEL UPPER SKIN HAS CORROSION , LBL 11.16, BS 270- BS277. GROUNDED - YES. REMOVED CORROSION FROM THE UPPER SURFACE OF THE INTERCOSTAL LOCATED IN THE FORWARD WET AREA AT STA 270- STA 277, LBL 11.16, WL 208.10, ORIGINAL THICKNESDR ASAA2022100140225Intercostal · corrodedFWD MAIN CABIN FLOOR SUPPORT, STRAP UPPER SKIN HAS CORROSION AROUND FSTNR HOLE, LBL-13, BS326. GROUNDED - YES. REMOVED CORROSION ON FLOOR SUPPORT AT STA. LBL-13 BS326,ORIGINAL THICKNESS .080 REMAINING THICKNESS .054 REMOVED .026 FOUND TO BE OUT OF LIMITS PER B
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