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 IPXA2022072784614Panel · crackedINSPECTION TYPE:SEGPRECOOLER PANEL 423BL HAS 2EA CRACKS ON VENT GRILLS.ACCOMPLISHED WELD REPAIR PER SRM 54-52-51SDR SWAA2022081735071Web · crackedCRACK WEB - INTERCOSTAL LOCATED BTW BS 500 TO BS 500A STR 26L FWD CARGO COMPARTMENT 2022-365945 / [01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 500 TO BS 500A STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG # 143A7505 REV. -. SEESDR IPXA2022081285169Tie Clip · corrodedINSPECTION TYPE:CK17FWD CARGO DOOR AT APPROX FS 580 LOWER INNER T CHORD IS CORRODEDREMOVED AND REPLACED T CHORD USING AN 10136-1503 PER SRM 51-40-02 PAR 9SDR R61A2022081200509Panel · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FWD FUSELAGE FLOOR STRUCTURE R/H SILL CORRODED AT FR 12 TO FR 15, RBL 39. FWD FUSELAGE FLLOR STRUCTURE R/H SILL AT FR 12 TO FR15 RBL 39 REMOVED AND REPLACED IAW ERJ 170 SRM 53-10-11. FASTENERS INSTALLED IAW ERJ 170 SRM 51SDR NACA2022072600001Skin Panel · dentedDURING WALKAROUND FOUND DENT ON RH SIDE OF FUS BETWEEN STA 1439-1461, STRINGERS BETWEEN S-24 AND S-25, LENGTH 22.750" WIDTH 2.250 AND DEPTH 0.234. REPAIR ACCOMPLISHED PER NAC EO 767-53-0026SDR IPXA2022072684579Stringer · corrodedINSPECTION TYPE:SEG1AGING AIRCRAFT INSPECTION AT STA 1625 L, S 26L, SEVERAL RIVETS WITH CORROSIONWORKED PER UPS RCD 256496, REPAIRED IAW B757-SRM 53-00-03-2R-1SDR UIEA2022072600784Structure · crackedFOUND DOOR CUTOUT STRUCTURE CRACK AT L5 DOOR STA 2230(<P>1) REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 95. 2) REPAIR DAMAGE AREA IAW SRM 53-60-15-2R-3 REV 95. 3) INSTALL FASTENERS IAW SRM 53-60-15-2R-3 REV 95. 4) JOB COMPLETED AND CONDITION SDR R61A2022081200506Shear Panel · corrodedL/H SHEAR PLATE AT FR 87 TO 88 CORRODED. R&R IAW SRM 51-42-01.SDR R61A2022081200508Shear Panel · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CTR FUSE III, R/H SHEAR PANEL AT FR 87 TO FR 88 CORRODED. REPLACED R/H SHEAR PANEL AT FR87 TO FR88 CTR FUS III IAW ERJ-170 SRM 51-42-01, SRM 51-42-02 AND SRM 51-43-01.SDR R61A2022081200505Gusset · corrodedFLOOR STRUCTURE R/H GUSSET PLATE AT FR 90. RBL 29 CORRODED. R7R IAW SRM 51-40-02.SDR QXEA2022072800260Panel · looseDURING OPERATIONAL CHECK FLIGHT FELT A VIBRATION AT 20,000 FT ASL, AIRSPEED 230 KIAS CONDITION LEVERS 900. VIBRATION ENDED AT AIRSPEED 246 KIAS CONDITION LEVERS 850. EVENT MARKER PUSHED. ALL ENGINE SYSTEMS WERE DISPLAYING NORMAL INDICATIONS. FELT LIKE AIRFRAMSDR FDEA202207251795None · unknownEXISTING MAJOR REPAIR FOUND ON FLOOR BEAM, UPPER CHORD AT STA 345, 40 RBL TO 52 LBL. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. EVALUATED EXISTING REPAIR LOCATED ON FLOOR BEAM UPPER CHORD AT STA 345, 40 RBL TO 52 LSDR SWAA2022080232793Doubler · deterioratedEXTERNAL GROUND POWER DOOR CUTOUT; PREVIOUS REPAIR IS DETERIORATED AND PULLING AWAY FROM STRUCTURE / [01] REMOVED DAMAGE PART IAW SRM 53-10-15-2R-4;[02] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[03] VERIFIED MATERIASDR EVCA072622Panel · corrodedINNER DOUBLER CORROSION DAMAGE ON THE LEFT-HAND SIDE AFT LOWER SHELL: FWD EDGE. THE DAMAGE IS AT LBL:19.75 TO LBL:22.75, STA:121.44 THRU STA:122.94, WL:SDR IPXA2022072384465Frame · corrodedINSPECTION TYPE:SEG1DURING ACCOMPLISHMENT OF E.O. B757-5310-73926-A, FOUND EXISTING REPAIR AT STA 1560 BETWEEN S-24L AND S-27LWORKED PER UPS EO B757-5310-83788-A, UPS RCD 256301, AND VT MAE EA 757-5360-27-A2978 REV-SDR IPXA2022080284840Floor Panel · corrodedINSPECTION TYPE:SEG2FLOOR BEAM AT STA 1100 LBL4 HAS CORROSION OUT OF LIMITS. ORIGINAL THICKNESS .200" MATERIAL REMAINING .140" MATERIAL LOSS .060"REPLACED SECTION OF UPPER FLANGE FROM RBL 13.0 TO LBL 12.0 PER EO B757-5310-27-A2990SDR IPXA2022072284451Bracket · crackedINSPECTION TYPE:SEGAFT CARGO COMPT. AT FR 54 FWD BULKHEAD LH O/B UPPER PANEL SUPPORT BRACKET IS CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21SDR IPXA2022072284450Bracket · crackedINSPECTION TYPE:SEGAFT CARGO COMPT. AT FR54 FWD BULKHEAD RH O/B UPPER PANEL SUPPORT BRACKET IS CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21SDR IPXA2022072284449Support Plate · crackedINSPECTION TYPE:SEGRH MAIN CABIN BETWEEN FRAME 38.1 AND FRAME 38.2 AT FLOOR LEVEL STR 26 SUPPORT WEB IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21SDR IPXA2022072284448Support Plate · crackedINSPECTION TYPE:SEGLH MAIN CABIN BETWEEN FRAM 38.1 AND FRAME 38.2 AT FLOOR LEVEL STR 26 SUPPORT WEB IS CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21SDR KCSA202207221093Web · corrodedTORQUE BOX WEB AT STA 610 RBL 44 SHOWS EVIDENCE OF CORROSIONSDR ASAA2022072139339Transition Panel · corrodedAFT CARGO R/H AFT TRANSITION PANEL CORRODED. GROUNDED - YES. BLENDED CORRODED AREAS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REPAIRED IAW B737-900ER SRM 53-00-53-2R-5 W=.5 O=.040 R=.031 L=1.1 D=.009SDR ASAA2022072139263Transition Panel · corrodedAFT CARGO L/H AFT TRANSITION PANEL CORRODED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TRANSITION PANEL TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 REPAIRED TRANSITION PANEL IAW B737-900ER SRM 53-00-53-2R-5W=.5 O=.040 R=.034 L=1.2 D=.SDR ASAA2022072139262Web · corrodedFORWARD CARGO COMPARTMENT THRESHOLD WEB HAS CORROSION. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-30-15-1A-1 REMOVED AND REPLACED WEB IAW B737-900ER SRM 51-40-02-0G-0W- 1.0 O- .056 R- .041 L- 6.0 D- .01SDR IPXA2022072884666Intercostal · crackedINSPECTION TYPE:CRT WING BELOW #3 SPOILER I/B HINGE ARM END RIB INTER-COSTAL WEB CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21SDR IPXA2022072184408Frame · dentedINSPECTION TYPE:SEG1AFT CARGO COMPARTMENT, LOWER FRAME STA 1300 L/H BETWEEN STR 25L TO STR 26L HAS A DENTWORK PER RCD 256338, REPAIRED PER 757-200PF SRM REV 114.00 53-00-07-2R-6 DETAIL III PER SRM 53-60-07-2RSDR IXXA2022072104Skin · corrodedLEFT WING LOWER SKIN PANEL CORRODED.SDR IXXA2022072103Stiffener · corrodedRWW UPPER PRESSURE DECK STIFFENER CORRODEDSDR IXXA2022072102Skin · corrodedCORROSION UPPER SURFACE LWSDR IXXA2022072101Stiffener · corrodedRWW STIFFENER CORRODEDSDR JJBA20220721021Bulkhead · crackedAT LH MLG WHEEL WELL, AFT BULKHEAD CRACKED AT 2 PLACES. INNER REINFORCEMENT ANGLE ON LH WING STUB SPAR 3 (WHEEL WELL AFT BULKHEAD) FAIRING ATTACHMENT ANGLE.SDR DALA2022120807901Crossbeam · crackedSHIP 3229 DURING H2 AND WHILE INSPECTING PER ER/A 540618-14, REV A, SECTION II, A CRACK WAS FOUND IN HOLE #3 OF FR 16 CROSSBEAM SPLICE LHS. CORRECTIVE ACTION: COMPLIED WITH ERA. (2328386)SDR ASAA2022072039428Trans Panel · corrodedAFT PIT R/H FWD TRANSITION HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. BLENDED CORRODED AREAS FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2, REPAIRED IAW B737-900ER SRM 53-00-53-2R-5W 5 O .040 R .030 L 1.2 D .010.SDR SWAA2022080931234Angle · corrodedG4B R/H STRAP BACKSIDE BOTTOM HAS CORROSION / [01] G4B R/H STRAP CONNECTOR ANGLE HAS NO LIMITS ON CORROSION; OUT OF LIMITS AND SRM 51-10-02-0G-0 IS APPLICABLE REPLACEMENT OF PART.;[02] REMOVED AND REPLACED G4B R/H STRAP CONNECTOR ANGLE PER SOPM 20-50-01.;[03] SDR R61A2022080900500Floor Support · corrodedR/H PNL SUPPORT AT FR 84 RBL 48 FOUND CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.SDR R61A2022080900499Floor Support · corrodedL/H PNL SUPPORT AT FR 84 TO LBL 48 FOUND CORRODED. R&R IAW SRM 51-41-01 AND 51-41-03.SDR R61A2022080900498Seat Track · corrodedR/H I/B SEAT TRACK BTWN FR 25 TO 27, FR 31 TO 32 AND FR 34 TO 35. R&R IAW SRM 51-43-03 AND 51-43-02.SDR R61A2022080900497Shear Web · corrodedR/H SHEAR WEB BTWN FR17 TO 20 FOUND CORRODED. R&R IAW SRM 51-41-02,51-42-02 AND 51-43-04.SDR R61A2022080900496Shear Web · corrodedR/H SHEAR WEB BTWN FR 12 TO 14 FOUND CORRODED. R&R IAW SRM 51-41-02 AND 51-43-04.SDR R61A2022080900495Shear Web · corrodedL/H SHEAR WEB BTWN FR 13 TO 16 FOUND CORRODED. R&R IAW SRM 51-41-02.SDR R61A2022080900494Seat Track · corrodedSEAT TRACK BTWN FR 12 TO 20 LBL 18 FOUND CORRODED OUT OF LIMITS . R&R IAW SRM 51-41-02, 51-43-03 AND 51-43-04.SDR R61A2022080900493Seat Track · corrodedSEAT TRACK BTWN FR 12 TO 20 RBL 18 FOUND CORRODED OUT OF LIMITS. R&R IAW SRM 51-41-02, 51-43-03 AND 51-43-04.SDR JR2R8543665Web · crackedLH WHEEL WELL WEB CRACKEDSDR ASAA2022072039287Transition Panel · corrodedAFT PTI L/H FWD TRANSITION HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TRANSITION PANEL TO BE OUT OF LIMITS AIW B737-900ER SRM 53-00-53-1A-2. REPAIRED TRANSITION PANEL IAW B737-900ER SRM 53-00-53-2R-5W .5 O .040 SDR ASAA2022072039286Transition Panel · corrodedFWD PIT L/H TRANSITION IS CORRODED FROM STA 500H TO 500I. GROUNDED - YES. REMOVED CORRODED SECTION OF LH TRANSITION PANEL (SIDEPLATE) STA 500F+10 TO STA 500L IAW B737-9000ER SRM 53-00-53-2R-5 (AREA OF 100% MATERIAL LOSS). INSTALLED NEW LH TRANSITION PANEL (SIDSDR IPXA2022072984678Frame · damagedINSPECTION TYPE:SEG2DURING ACCOMPLISHMENT OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT STA 1560 BETWEEN S-24R AND S-27R. ALTERNATE INSPECTION REQUIREDACCOMPLISHED REPAIR PER EO B757-5310-83923-A, UPS RCD 277195 AND VT MAE 757-5360-27-A2984SDR SWAA2022072530973Structure · missingGROUND POWER ACCESS DOOR CUTOUT HAS MISSING STRUCTURE AT LOWER REPAIR DOUBLER / [01] PERFORMED HFEC PART 6 PROCEDURE 23 AS REQUIRED BY SRM 53-10-15-2R-4 REPAIR 4;[02] REPAIRED GROUND POWER D0OR ACCESS CUTOUT AT LOWER DOUBLER PER SRM 53-10-15-2R-4 REPAIR 4SDR FDEA202207201784Beam · crackedFUSELAGE- R/H SIDE OF LH GANTRY 5 AT FR50B CRACK WAS FOUND (LENGTH:14MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 LWR FLANGE AT FR50B PER EO: 6-5310-7-5021 F PT8 & AIRBUS DWG: R53810583 ISSUE: D. THIS IS CATEGORY A REPAIR. MAJOR REPAISDR FDEA202207201783Beam · crackedFUSELAGE- L/H SIDE OF LH GANTRY 4 AT FR50.1 CRACK WAS FOUND (LENGTH:15MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 4 LWR FLANGE AT FR50.1 PER EO: 6-5310-7-5021 F PT6 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REPSDR FDEA202207201782Beam · crackedFUSELAGE- L/H SIDE OF LH GANTRY 4 AT FR49.1 CRACK WAS FOUND (LENGTH:56MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 4 LWR FLANGE AT FR49.1 PER EO: 6-5310-7-5021 F PT6 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REP
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