JASC 5310
Service difficulty reports · 38,548
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 DALA2017100307221Beam · crackedCRACKED NR 4 BEAM ON FWD RIGHT GALLEY DOOR. THE BEAM WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-41-05.SDR FDEA201710012850Crease Beam · corrodedBS 370 - 377, RBL 64, LOWER SURFACE OF CREASE BEAM INBD ANGLE HAS SIGNS OF CORROSION. REMOVED THE CREASE BEAM IAW SRM 51-10-02. OUTT OF LIMITS IAW SRM 53-30-13-1A. REMOVED THE WEB IAW SRM 51-40-02. FABRICATED A NEW WEB IAW DWG 141N8322, REV K. INSTALLED TSDR SWAA2022020258028Intercostal · crackedINTERCOSTAL AT S-23L STA 294-320 FOUND CRACKED PRIOR TO INSTALLATION / FABRICATED NEW INTERCOSTAL P/N: 141A8131-45 LOCATED AT S-23L; STA 294 - 320 IAW BOEING DWG 141A8131 REV - AND SMAL CONTROL # PO263117.SDR SIMA20170930004Beam · corrodedLEFT LAVATORY BEAM, UNDER THE LT BEAM GUSSET FOUND CORRODED AROUND FORWARD NUTPLATE HOLE. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-2953.SDR ASOA201709305115Web · damagedWHILE PERFORMING SB 670SH-53-042 ONE HOLE WAS ELONGATED AT BS 741, LBL 36, THRU DIAPHAM AND PRESSURE FLOOR. REPAIRED IAW REO 670-53-41-337. ACFT RETURNED TO SERVICE.SDR ASOA201709305114Structure · damagedDURING C CHECK , ON REMOVAL OF AT NLG FLOOR SPLICE ANGLE FOUND OVERSIZED HOLE AT LBL 7.5 OUTBOARD MEASURING .225. REPAIRED IAW REO 670-53-11-1328.SDR DALA2017100107181Fitting · crackedCRACK IN UPPER PAN FITTING NEAR BS 974 AT THE AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-04, AND 51-41-05, PARAGRAPH 10.SDR SWAA2022020210671Intercostal · crackedPASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 LBL 47 INTERCOASTAL IS CRACKED AS MARKED / AT PASSENGER CABIN; FWD WET AREA; BETWEEN STA 312 TO 328 LBL 47REMOVED + REPLACED INTERCOSTAL IAW- BOEING DWG 141A5400 REV:- AND B737-700 SRM 51-40-02-0G-0 PAR 7.D.SDR SWAA2022020210672Intercostal · crackedPASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 RBL 31 INTERCOASTAL IS CRACKED AS MARKED / AT PASSENGER CABIN FWD WETAREA BETWEEN B.S.312 TO 328 RBL31 REMOVED AND REPLACED INTERCOSTAL I.A.W. BOEING DWG 141A541OU12;AND B737-700 S.R.M 51-40-02 PAR 7.FIG12; SDR SWAA2022020220680Bracket · corroded*** CORROSION *** ACB L/H FLOOR TO SIDEWALL SUPPORT MOUNTING BRACKET AT STA 727; LBL 22 HAS CORRODED NUTPLATE ON LOWER SURFACE / REMOVED AND REPLACED ACB L/H FLOOR TO SIDEWALL SUPPORT MOUNTING BRACKET AT STA 727; LBL 22. NUTPLATE ON LOWER SURFACE IAW. SRM 51-4SDR SWAA2022020220685Support · corroded*** CORROSION *** ACB R/H FLOOR TO SIDEWALL SUPPORT 3RD SECTION (ACB DOOR LWR MAIN SILL; FWD SHIELD) HAS MULTIPLE AREAS OF CORROSION (UPR & LWR SURFACES); SCREW-START DAMAGE; AND DRILLED OUT FASTENERS; STA 767 TO STA787+6' / DETERMIND NO ALLOWABLE DAMAGE LIMITSDR SWAA2022020220698Web · corroded*** CORROSION *** ACB DOOR LWR MAIN SILL WEB UPR SURFACE HAS MULTIPLE AREAS SHOWING EVIDENCE OF FILLAGREE CORROSION / REMOVED CORROSION 38' X 2.5' X .025' FROM .050' ORIGINAL MATERIAL THICKNESS AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED AND RSDR IXXA20170929320Window Frame · corrodedUPPER CARGO WINDOW FRAME L21 HAD CORROSION ON THE LOWER TURFACE AREA. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02, PARAGRAPH 7, AND DRAWING 144N3200.SDR DALA2017100207216Door Frame · dirtyR4 DOOR SLIDE INDICATIOR INOPERATIVE. CLEANED DEBRI FROM DOOR FRAME SURROUNDING AND OPERATED DOOR, LIGHT WORKS OK, INDICATIONS ARE OK. ARMED AND DISARMED OK.SDR UIEA2017100101911Vent · crackedDURING POST FLIGHT INSPECTION , FOUND A .750 INCH CRACK AT THE RT BS 2090 WASTE SYSTEM OVERBOARD VENT. REPAIRED IAW EO 4453B398.SDR DALA2017093007180Pan · crackedCRACK ON THE LT UPPER, AFT CORNER OF WINDOW RING PAN BS 832 AND 870. REPAIRED IAW 56-20-02-2R.SDR SWAA2022020210662Angle · corrodedFORWARD CARGO PIT STA 500D BULKHEAD LOWER ANGLE LBL 24 - RBL 24 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION AT STA 500D LBL 24 - RBL 24 ON ANGLE ASSY FOUND TO BE 100% OUT OF LIMITS IAW SRM 51-10-02-0G-0 & SRM 53-00-53-1A-2 VERIFIED P/N FOR NEW RAIL ASSYSDR SWAA2022020210647Angle · corrodedAFT CARGO COMPARTMENT; STA 947.5; AFT BULKHEAD LOWER ATTACH ANGLE RBL 9-14 HAS CORROSION. / REMOVED AND REPLACED AFT BULKHEAD LOWER ATTACH ANGLE AT RBL 9 - 14 DUE TO CORROSION ORIGINAL THICNKESS .090' MATERIAL REMAINING .060' MATERIAL IS OUT OF LIMITS IAW SRM SDR SWAA2022020210657Web · corrodedFORWARD CARGO PIT LOWER SILL WEB STA 440 - 492 RBL 24 - RBL 29 HAS CORROSION ON UPPER AND LOWER SURFACES / BLEND CORROSION ON FWD PIT SILL WEB IAW SRM 53-30-15-1A-1; ORIGINAL THICKNESS .045; .007 MAT'L LOSS WITH .038 REMAINING OUT OF LIMITS VERIFIED NEW SILL WSDR SWAA2017101717144Crease Beam · corrodedAFT GALLEY R2 CUTOUT CREASE BEAM INBOARD CORRODED BETWEEN BS 956 TO 992. R & R THE CREASE BEAM IAW SRM AND DWG.SDR SWAA2017101617067Crease Beam · crackedL1 DOOR CUTOUT LT CREASE BEAM VERTICAL FLANGE WAS CRACKED AT BS 302. R & R THE CREASE BEAM IAW DWG AND SRM.SDR DALA2017100207219Door Frame · crackedL1 DOOR FRAME CRACKED. THE DOOR FRAME WAS REPAIRED AND REFURBISHED IAW ER/A 534742-14 REV. ORIGINAL.SDR DALA2017092907177Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER ON THE AFT CARGO DOOR FRAME BS 954. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-7, FIG 201.SDR SWAA2022020241973Splice · corrodedUPON REMOVAL OF FLOORBAORD 140AF FOUND PANEL SPLICE CORRODED / REMOVED AND REPLACED FLOOR PANEL SPLICE TEE ASSEMBLY P/N 146A9401-8 SI #3530741 'A'TAG # ES1089 IAW B737 DRAWING # 146A7500 ID0025 REV A AND B737 SRM 51-40-02-0G-0 TOOL #AAR 2246 AND B737 AMM 24-52SDR SWAA2022020207790Angle · corrodedAFT CARGO LEFT HAND TRANSITION ANGLE HAS CORROSION AT STA 727D. / REMOVED DAMAGED L/H TRANSITION ANGLE AND INSTALLED NEW L/H TRANSITION ANGLE STA 727-847 PER SRM 53-00-53-2R-5; SRM 51-40-02; AND SRM 53-60-53-01-2. SEE INDIVIDUAL SIGNOFFS FOR WORK ACCOMPLISHED.SDR SWAA2022020207791Angle · corrodedAFT CARGO LEFT HAND TRANSITION ANGLE HAS CORROSION AT STA 767 + 6. / REMOVED DAMAGED L/H TRANSITION ANGLE AND INSTALLED NEW L/H TRANSITION ANGLE STA 727-847 PER SRM 53-00-53-2R-5; SRM 51-40-02; AND SRM 53-60-53-01-2. SEE INDIVIDUAL SIGNOFFS FOR WORK ACCOMPLISHSDR FDEA201709272925Web · crackedNOSE WHEEL WELL LEFT VERTICAL WEB PANEL BS 315, HAS A CRACK BEHIND THE HYDRAULIC LINES. REMOVED AND REPLACED DAMAGED SECTION OF THE WEB IAW SRM 53-00-01, FIG 10, SHT 4, 5, 7, PGS 50, 51, 53, AND DWG NCA6046, AND ACA3837.SDR IXXA20170927297Window Frame · corrodedUPPER CARGO R8 WINDOW FRAME CORRODED. THE WINDOW FRAME WAS REPAIRED IAW ENGINEERING AUTHORIZATION 47285REA04.SDR IXXA20170927296Window Frame · corrodedUPPER CARGO R5 WINDOW FRAME HAS CORROSION. THE WINDOW FRAME WAS REPAIRED IAW ENGINEERING AUTHORIZATION 47285REA04.SDR IXXA20170927312Window Frame · corrodedUPPER CARGO WINDOW FRAME L7 HAS CORROSION ON THE LOWER SURFACE AREA. THE WINDOW FRAME WAS REPAIRED IAW REA 47285REA04.SDR DALA2017092807137Beam · crackedCRACKED RT NOSE LANDING GEAR BEAM. REPAIRED IAW SRM 53-10-14-2R-2.SDR DALA2017092807136Beam · crackedCRACKED LEFT NOSE LANDING GEAR BEAM. REPAIRED IAW SRM 53-10-14-2R-2.SDR SWAA2022020360267Pressure Web · crackedCABIN STA 663 VERTICAL PRESSURE WEB CRACKED AT RBL 35 AT WL 194 APPROX. 1 INCH LONG VERIFIED WITH HFEC / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2022020220582Support · corroded***CORROSION*** FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION BETWEEN BS 400 AND BS 500B LBL 22. / REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT BS 400-500D LBL-22 IN AREAS OF 1' X 1' X 0.007' FOUND TO BE OUT OF LIMIT ORIGINAL MATERSDR YADA20170926002Door Frame · crackedWHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND CRACK ON CARGO DOOR FRAME P/N:114-430125-5 AT F.S.: 509.50 . CRACK IS 1.6 INCHES LONG AND BEYOND LIMITS. FRAME SECTION WILL BE REPLACED AND DOUBLER INSTALLED.SDR YADA20170926001Door Frame · crackedWHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND MULTIPLE CRACKS AT AIRSTAIR DOOR FRAME. ONE LOCATED ON FRAME P/N:114-420041-37 AND ONE LOCATED ON AIRSTAIR DOOR CHANNEL P/N:114-420041-41. BOTH CRACKS ARE BEYOND LIMITS AND PARTS WILL BE REPLACEDSDR C77A20170925003Beam · corrodedDURING A BASIC CHECK, INSPECTION DISCOVERED THE L1 DOOR LOWER BEAM TO HAVE CORROSION DAMAGE THAT IS BEYOND THE ALLOWABLE SRM LIMITS. BLENDED THE AREA TO REMOVE THE CORROSION. THE BLENDED AREA MEASURES THE FOLLOWING APPROXIMATE DIMENSIONS OF 1.765 INCHES X 1.SDR SWAA2022020258022Angle · crackedINTERCOSTAL UPPER ATTACH ANGLE CRACKED AT STA 500D TO 520 BL 0 / REMOVED AND REPLACE UPPER ATTACH ANGLE AT STA 500D TO 520 BL 0 IAW B737 SRM 51-40-02-0G-0 AND BOEING DRW 143A5400SDR SWAA2022020258019Panel · crackedCABIN FLOOR STRUCTURE; STA. 540 ; BL 0 TO LBL 24.75; PANEL BREAK IS CRACKED. / REMOVED AND REPLACED PANEL BREAK ON STA 540 BL 0 TO LBL 24.75 IAW B737 SRM 51-40-02-0G-0 AND BOEING DRW 143A0060 REV B.SDR SWAA2022020258020Panel · crackedCABIN FLOOR STRUCTURE; STA. 540; BL 0 TO RBL 24.75; PANEL BREAK IS CRACKED. / REMOVED AND REPLACED PANEL BREAK ON STA 540 BL 0 TO RBL 24.75 IAW B737 SRM 51-40-02-0G-0 AND BOEING DRW 143A0060 REV BSDR IXXA20171109336Window Frame · corrodedUPPER CARGO WINDOW FRAME CORRODED ON LOWER SURFACE AREA. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02, PARA 7, AND DWG 144N3200.SDR DALA2017092407057Door Frame · damagedAWR HIDDEN DAMAGE: ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT. ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT WERE REPAIRED PER ETI-88-17-235 REV 3 AND ER/A 560942-14 REV ORG.SDR SWAA2017101917225Door Frame · crackedR1 DOOR UPPER STUB FRAME CRACKED AT BS 295.5, STR 9R. REPAIRED STUB FRAME IAW SRM AND DWG.SDR SWIA2017110643954Beam · corrodedRIGHT TRANSVERSE BEAM AT BS 349 IS CORRODED. REPAIRED THE TRANSVERSE BEAM IAW REO.SDR SWIA2017100643834Fitting · crackedLEFT LOWER OUTBD WINDSHIELD ANGLE IS CRACKED. REMOVED AND REPLACED THE LT WINDSHIELD POST FITTING IAW SRM.SDR SIMA20170921005Profile · gougedCARGO DOOR UPPER OTBD EDGE OF FRAME IS GOUGED. R & R THE PROFILE IAW SRM 51-40-02.SDR DALA2017092207091Door Frame · bentAPU DOOR AFT LT FRAME BENT JUST ABOVE BS 1963. REMOVED AND REPLACED THE DOOR FRAME IAW DWG 148N1605-7, SRM 51-40-05, & 51-40-02.SDR UIEA2017092501849Failsafe · crackedFOUND A CRACK INDICATION IN THE FAILSAFE STRAP. REPAIRED IAW EO 6753A070, REV 10, AND SB 767-53A0100, REV 3.SDR UIEA2017092501850Failsafe · crackedFOUND CRACK INDICATION IN THE FAILSAFE STRAP AT LOWER FASTENER HOLE IAW EO 6753A070 REV.10 PART 2, STEP 8, AND SB 767-53A0100 REV 3 AD 2012-09-04. REPAIRED IAW EO 6753A070, REV 10 AND SB 767-53A0100 REV 3.SDR A6WA2017092245297Plate · corrodedLIPPED PLATE COMMON TO THE RT FLOOR SUPPORT AT BS 559+86 IS CORRODED.
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