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 DALA2019062003666Reinforcement · crackedCRACK ON LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER AT FLIGHT COMPARTMENT (CPIL). NRC 00475: BRACKET LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #1130511)SDR AALA201906199018Structure · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CHORD BETWEEN BS 294.5 AND BS 360 AT S23L. REPLACED CHORD PER EA 294928 AND AARD 51-00-05-1.SDR DALA2019061903652Beam · crackedCRACK ON BEAM STA Y=737, X= 54 AND Z=-2 LH SIDE AT WING BOX. NRC 00467: FLOOR BEAM WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G .SDR SWAA2022031047573Support · corroded***CORROSION*** FCB; AFT LOWER BULKHEAD SUPPORT; BS 500D; LBL 24-RBL 24; WL 156 / NO ALLOWABLE DAMAGE LIMITS ARE GIVEN IN THE SRM FOR THIS PART; AND IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-0G-0 STEP 9. REMOVED AND REPLACED AFT LOWER BLKHD. SUPPORT (RAILASDR 4S42020F00002Doubler · crackedTHE FOLLOWING IS THE INFORMATION FOR THE FAA FORM 8010-4 MALFUNCTION OR DEFECT REPORT REFERENCE CRACKS IN THE MLG ACTUATOR BULKHEAD DOUBLERS ON CESSNA 210E SN 21058705 N404BN TOTAL TIME AIRFRAME IS 5455.8 HOURS. AFTER RESEARCH OF THE ACFT LOG BOOKS IT WAS DETSDR CALA2019062211004Floorbeam · corrodedB757-53-3-0480 CORROSION ON MAIN CABIN FLOOR BEAM UPPER SURFACE AT STA 680 RBL-53 REF. ST. ENGINEERING N/R 0065606 FOUND CORROSION OUT OF LIMIT IAW B757-300 SRM 53-30-51 L=1.3,W=. 8,D=.037 ON CABIN FLOOR BEAM AT STA 680 RBL 53 AND ACCOMPLISHED PERMANENT REPAIRSDR DALA2019062093693Strap · corrodedCORROSION LOWER CUTOUT ON STRAP IN FWD CARGO COMPARTMENT, REPLACED STRAP ON LOWER FUSELAGE CUT OUT IN FWD CARGO COMPARMENT (1 E/A) AS PER SRM A320 51-72-11 AND DRAWING D53231563SDR DALA2019061903649Pressure Panel · crackedHOLE 7 SHOWS CRACK INDICATION THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. HOLE 7 WAS REPAIRED ON WORK CARD 5311-01171-04A.SDR DALA2019061903648Pressure Panel · crackedHOLE A SHOWS CRACK INDICATION THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. HOLE A WAS REPAIRED ON WORK CARD 5311-01171-04A.SDR DALA2019061903647Pressure Panel · crackedLH FR35-36 PRESSURE FLOOR PANEL "CRACK FOUND AT HOLE A. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT." AA 5311-01171, SB A320-53-1264 AND AD-2018-06-04.SDR DALA2019061903646Pressure Panel · crackedHOLE 21 SHOWS CRACK INDICATION THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH. HOLE 21 WAS REPAIRED PER PRI 578745-14AD, ER/A 578745-14AD, AND AA5311-01171 -04.SDR SWAA2022031047566Support · crackedFLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; L.B.L. 0 - 24.5; W.L. 208.1. / REMOVED AND INSTALLED A NEW FLOOR PANEL SUPPORT AT B.S 540 BL0-LBL 24.5; WL 208.1 IAW SRM 51-40-05; SRM 51-40-02; DWG 143A0060 SHT 36SDR SIMA2019062417009Door Frame · corrodedCARGO DOOR SILL IS CORRODED NEAR FRAME 67. DRILLED, COUNTERSUNK AND INSTALLED A NEW CARGO SILL IAW SRM 51-40-02.SDR CALA2019062210987Pressure Panel · crackedLH AND RH SIDE PRESSURE PANELS BETWEEN FR 35 AND 36 HAVE MULTIPL E CRACKS IN FASTENER HOLES. INTERIM REPAIR ACCOMPLISHED TO LH AND RH FR 35-36 PRESSURE PANEL S PER ECRA 5331-02397 PART 1.SDR SWAA2019062134000Crease Beam · corrodedCREASE BEAM AT AFT WET AREA ENTRANCE DOOR CORRODED BETWEEN BS. 986.5 TO BS. 967, RBL 54. / REPAIRED CREASE BEAM PER SRM.SDR A6WA2019061846666Beam · gougedCARGO DOOR BEAM GROOVED AT AFT END OF BEAM DUE TO CARGO DOOR SPRING CABLE. REPLACED CARGO DOOR BEAM MEMBER IAW CRJ200 SRM 51-42-06, 51-42-21.SDR R61A201906160629Crossbeam · corrodedWHILE IN HEAVY CHECK - MAJOR REPAIR - CORROSION AS MARKED AT FRM 14 CROSS BEAM RH SIDE. REPAIRED CROSSBEAM FR14 RH SIDE AS
MARKED BY TRIMMING OUT DAMAGE, FABRICATING, AND
INSTALLING REPAIR DOUBLER AND FILLER REF. EMB SRM
53-00-10/REPAIR03P.SDR CALA2019061700966Beam · crackedSPEC A3NB-05-3-6171 DOT A-24-001 RH O/WING HATCH RIB CRACKED AT RIVET HOLE. NONROUTINE 9025688 REMOVED AND REPLACED FWD SIDE BEAM AND SEGMENT FOR R/H OVER WING EMERGENCY EXIT DOOR IAW A319 SRM 51-72-11-911-001. ADD EMP:V918825SDR SWAA2019070834659Crease Beam · corrodedCREASE BEAM CORRODED AT BS. 747, LBL 70. REPAIRED CREASE BEAM PER SRM & DWG.SDR SWAA2019070834628Crease Beam · corrodedCREASE BEAM CORRODED AT BS. 727 LBL 70. R&R CREASE BEAM PER SRM & DWG.SDR SWAA2019062133951Crease Beam · corrodedPASSENGER CABIN FORWARD WET AREA LOCATED AT CREASE BEAM CORRODED BETWEEN BS. 312 TO BS. 294.5, LBL 55. REPAIRED CREASE BEAM IAW SRM.SDR A6WA2019061746663Fitting · crackedCENTER WINDSHIELD POST LOWER FITTING CRACKED LH SIDE IN RADIUS. REPLACED.SDR WVER201906140014Frame · corrodedPERFORMED A MAJOR REPAIR TO PASSENGER DOOR FRAME DD4 AND DD5 AT FS 313.56, P/N: 601R318086-1. FRAME WAS CORRODED OUT OF LIMITS AND WAS REPLACED IN ACCORDANCE WITH BOMBARDIER CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. REF WVAC JOB# 41500981, OP#SDR SWAA2022031005227Web · corroded***CORROSION***ON AFT CARGO BAY VERTICAL WEB BS945; LBL3; WL170. / REMOVED AND REPLACED WEB ASSY B.S. 927-947 LBL 3 HFAB 53-WB-011/NEW RO#750203-SWA PER SRM 51-40-02-0G-0 AMM 51-21-41-370-802 SRM 51-40-05 SRM 53-00-53-1A-2 AND DWG 147A7500SDR SWAA2022031032897Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 277-294.5; B.L. 0; W.L. 208.1. / REMOVED AND REPLACED INTERCOSTAL AT BS 277 - 294.5 BL 0 WL 208.1 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 83802U 25JUN19SDR SWAA2022031032898Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 328-344; L.B.L. 47; W.L. 208.1. / REMOVED AND INSTALLED NEW INTERCOSTAL AT B.S 328 344; LBL 47 WL 208.1 ITEM # 141A5410-16 IAW SRM 51-40-02-0G-0; DWG # 141A5400 57319U 06-17-19SDR R61A2019062930666Frame Splice · crackedMAINTENANCE REPORTED A CRACK ON THE SPLICE AT FRAME 59 AND STRINGER 9R. MAINTENANCE REMOVED AND REPLACED THE SPLICE AT FRAME 59 AND STRINGER 9R IAW EMB SRM 51-43-03 AND 51-43-04.SDR IPXA201906143238Structure · damagedINSPECTION TYPE:SEG3DURING REMOVAL OF DENT ON NR 115828 FOUND DAMAGE TO CHORD UNDERNEATH.REPAIRED PER RCD# 116143 UPS EO # B757-5310-72739-A AND VTMAE EA #757-5310-27-A2349-REV.SDR CALA2019061400947Stop Fitting · crackedR/H FR68 DOOR STOP FITTING #1 BOTTOM FITTING I/B LOWER FASTENER HOLE HAS CRACK INDICATION. REPAIR BEFORE NEXT FLIGHT REPAIRED R/H FR68 DOOR STOP FITTING #1 I/B LOWER FASTENER HOLE WITH FREEZE PLUG DIA 0.415 FOR HOLE 0.435 IAW SRM 53-41-12-300-0 10. DOOR STOP SDR SWAA2022031028480Intercostal · crackedFWD CABIN FLOOR INTERCOSTAL IS CRACKED AT SCREW HOLE STA 312 TO 328 LBL45 / REMOVED CRACKED FWD CABIN FLOOR INTERCOSTAL FROM STA 312 TP 328 LBL 45 IAW SRM 51-40-02-0G-0. LOCATED NEW INTERCOSTAL PART NO 141A5410-12 AND DRILLED TO SIZE IAW SRM 51-40-05-0G-0 AND SDR SWAA2022031078762Stop · corroded***CORROSION*** ON RH OVERWING EXIT LOWER SILL LINING STOP ASSY BS 627; WL 221. / REMOVED AND REPLACED R/H OVERWING EXIT LOWER SILL LINING STOP ASSY AT B.S627; WL221 IAW SRM 51-40-02-0G-0 AND DWG 411A2800.SDR SWIA2019080546127Door Frame · crackedPASSENGER DOOR UPPER SILL STGR3 L/H AT FS379.0 CLIP HAS CRACKED. REMOVED AND REPLACED THE PASSENGER DOOR UPPER SILL STGR3 L/H IAW REO AND SRM. LEAK CHECKS GOOD.SDR SWAA2019071134747Crease Beam · crackedL1 DOOR CREASE BEAM INNER CHORD CRACKED AT BS. 301, LBL 54. REPAIRED CREASE BEAM CHORD PER SRM & EA.SDR SWAA2019062534076Crease Beam · corrodedPASSENGER CABIN FLOOR STRUCTURE R2 CREASE BEAM CORRODED AT DOOR WAY. R & R CREASE BEAM IAW SRM AND DWG.SDR C77A2019061200001Fitting · corrodedCORROSION HAS BEEN FOUND ON THE FWD CARGO DOORWAY – FWD FITTING P/N 170-66803-401, CENTER FITTING P/N 170-66804-401, AND/OR AFT FITTING P/N 170-66803-402 ON SEVERAL COMPASS AIRCRAFT DURING BASIC CHECK. SINCE EMBRAER CLASSIFIES THESE FITTINGS AS PSES, COMPASS HSDR R61A2019062910667Angle · crackedFORWARD FUSELAGE E-BAY ACCESS HATCH SURROUNDING STRUCTURE FOUND 1 ANGLE CRACKED AT FR 05 STR 26R. REPLACED ANGLE IAW SRM 51-41-02 AND 51-43-0.SDR CALA2019062401048Crease Beam · corrodedCORROSION ON MAIN CABIN LH CREASE BEAM INNER CHOR D UPPER SURFACE FROM STA 730-755 LBL-64 RG30 REF. ST. ENGINEERIN G N/R 0065600 REMOVED & REPLACED L/H CREASE BEAM INNER CHORD AT L2 DOOR SURROU ND IN MAIN CABIN AT STA. 663 TO 757,LBL 65 IAW BOEING DWG NO 143 NSDR SWAA2019062133962Web · crackedFORWARD CARGO DOOR SURROUND STRUCTURE INTERCOSTAL CRACKED BETWEEN BS. 492 TO BS. 500, STR. 22R, AFT LOWER CORNER RADIUS. / R&R INTERCOSTAL WEB PER SRM AND DWG.SDR CHIA2019061413966Door Frame · crackedDURING REMOVAL OF THE AFT EMERGENCY EXIT HATCH, FOUND CRACK AT STA 482, BL 50L, WL +50. REMOVED DAMAGED WEB, LOCATED AND INSTALLED NEW WEB P/N 145S3106-5 (PO# A043423) IAW 234-3 SRM REV. 2, SECTIONS 53-13-03 AND 51-50-00.SDR FXGA201906111946Door Frame · corrodedMAIN CARGO DOOR JAMB INNER SKIN REPLACEMENT. TO REPLACE THE MAIN CARGO DOOR JAMB INNER SKIN (FORWARD LOWER SECTION AT F/STA 520) FOR CORROSION DAMAGE. REMOVE AND REPLACE CORRODED SECTIO OF DOOR JAMB PER B727 SRM 51-30-2.SDR SWAA2019062634169Crease Beam · corrodedL1 DOOR CREASE BEAM CORRODED. R&R CHORD IAW SRM AND DWG.SDR IPXA2019061443256Structure · gougedINSPECTION TYPE:12YRLOWER CARGO DOOR SURROUND AFT LOWER SEALING SECTION IS GOUGED AT MULTIPLE AREAS.REMOVED AND REPLACED IAW A300-600 SRM 51-40-21.SDR IPXA2019061443255Structure · gougedINSPECTION TYPE:12YRLOWER CARGO DOOR SURROUND AFT MIDDLE SEALING SECTION IS GOUGED AT MULTIPLE AREAS.REMOVED AND REPLACED IAW A300-600 SRM 51-40-21.SDR FDEA2019062801421Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR60, BTW Y-1456 AND Y-1959 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR60, BTW Y-1456 AND Y-1959) PER A300-600F SRM53-10-15-201 FIGURE SDR REXA2019062780970Vertical Beam · crackedFS409.00 + 128 VERTICAL BEAM AT LBL27 SHOWS VISUAL SIGNS OF A CRACK OF A CRACK ON INBD BOTTOM SIDE. THIS ENTRY ICLUDES WORK CONTINUATION CARD JOB 87768111 OP312
REPAIRED LBL27 POST AT FS409+128 IAW BOMBARDIER GREO 601R53-41-056. WVAC EMP STAMP 769SDR SWAA2019062634161Beam · corrodedR2 DOOR CREASE BEAM WEB CORRODED. R&R BEAM WEB IAW SRM, EA, AND DWG.SDR AALA2019061209016Box Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CABIN FLOOR BOX AT FR 43 LEFT AT THE AFT HOLE. REPAIRED BOX BEAM PER EO5315Y066-001.SDR DALA2019061293522Door Frame · crackedR/H FWD MAIN LANDING GEAR WHEEL FRAME IS CRACKED. ACCOMPLISHED SEC I TIME LIMITED REPAIR PER ER/A 578803-14 REV ORIGINAL. ASSOCIATED ER/A 14-578803. REPLACED R/H MLG FWD DOOR JAMB PER RI SEC II REF BOEING DWG #5930584. LANDING GEAR DOOR OPS CHECK GOOD REF MD88SDR ASOA201906087055Window Post · crackedL/H WINDSHIELD LATERAL POST CRACKED AT UPPER O/B CORNER AROUND RIVET. REMOVED RIVETS, BOLTS AND SUPPORTS TO FACILITATE INSTALLATION OF REINFORCEMENT FOR L/H WINDSHIELD PILLAR. DRILLED REINFORCEMENT, CUT OUT PILLAR SKIN CRACKED SECTION, COLD WORKED 14 HOLES ON SDR SWAA2022031076888Doubler · corrodedPASSENGE CABIN; STA 663+3; LBL 65; HORIZONTAL PRESURE DECK DOUBLER ANGLE HAS CORROSION AROUND FASTNERS / REMOVED CORROSION IAW B737-700 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS = .063' AFTER BLENDING .060' REMAINS = .003' MATERIAL LOSS. REPAIRED IAW EA 190566
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