JASC 5300

Service difficulty reports · 8,206

Reports filed under 5300 · Fuselage Structure (General), 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 = '5300'
  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.

SDR CALA2022021800409Joint · dentedLH FUSELAGE SKIN HAS DENT/GOUGE DAMAGE AT THE 360 BUTT SPLICE AREA (STA 251- STA 360) BETWEEN STRINGERS S-21L AND S-22L. DAMAGE APROX 6" LONG X 5.60 WIDE X.230 DEEP. PREPERATION FOR FERRY FLIGHT ECRA ISSUED 5310-07797 HFEC AND DVI INSPECTIONS WERE PERFORMED BYFeb 16, 2022 · N31412 · Boeing 737900SDR QXEA2022021600080None · corrodedSEAT RAIL 9 IS CORRODED ON THE SIDE FLANGE BY AFT SCREW HOLE. SEAT RAIL 9 REPAIRED IAW REPAIR DRAWING 84-53-10542.Feb 16, 2022 · N446QX · Bombdr DHC8402SDR SWIA202265373None · damagedPASSENGER DOOR PIANO HINGE HALF REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED AND REPLACED PASSENGER DOOR PIANO HINGE HALF WITH REFERENCE TO SRM 52-11-01. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337.Feb 15, 2022 · N708EV · Cndair CL6002C10SDR R61A2022030800180Doubler · corroded"CORROSION ON WASTE BOX DOUBLER ON THE I/B FWD SIDE. REMOVED AND REPLACED DAMAGED WASTE BOX DOUBLER BETWEEN FR88-FR89 AND STRINGER 28R-26R. REF SRM 51-40-08.Feb 15, 2022 · Emb ERJ170200LRSDR EE4Y2022022815211Web · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK RELATED TO MPD TASK ZL-500-03, IT WAS FOUND ON AFT FUSELAGE AFT RH DOOR ENTRANCE AREA BETWEEN FR67/68 SILL WEB WITH CORROSION AND THERE IS A SKIN WITH 2EA ELONGATED HOLES. ACTION: DUE TO THIS FACT, DETAILS WEREFeb 15, 2022 · N233NV · Airbus A320214SDR 2022F00100None · noneCRACKING ON FUSELAGE SKIN LAP JOINT. ROGHT SIDE STR 10R BETWEEN BS727C AND BS727D. FOUND DURING ACCOMPLISHMENT OF AD 2012-26-02Feb 15, 2022 · Boeing 73733RSDR 2022F00099None · noneCRACKING ON FUSELAGE SKIN LAP JOINT. ROGHT SIDE STR 10R BETWEEN BS727C AND BS727D. FOUND DURING ACCOMPLISHMENT OF AD 2012-26-02Feb 15, 2022 · Boeing 73733RSDR 2022F00102None · noneCRACKING ON FUSELAGE SKIN LAP JOINT. ROGHT SIDE STR 10R BETWEEN BS727C AND BS727D. FOUND DURING ACCOMPLISHMENT OF AD 2012-26-02Feb 15, 2022 · Boeing 73733RSDR R61A2022022200160Shear Web · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII, FLOOR STRUCTURE, CENTER SHEAR WEB AT FR87 TO FR88 CORRODED. CENTER SHEAR WEB FLOOR STRUCTURE LOCATED BETWEEN FR87 AND FR88 IN CENTER FUSELAGE III WAS REMOVED AND REPLACED IAW SRM 51-42-01.Feb 15, 2022 · N743YX · Emb ERJ170200LRSDR R61A2022022200159Gusset · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII FLOOR STRUCTURE, FLOOR GUSSET CORRODED AT FR89, RBL 12. STRUCTURAL FLOOR SPLICE LOCATED AT FR89, RBL 12 IN CENTER FUSELAGE III WAS REMOVED AND REPLACED IAW SRM 51-43-01.Feb 15, 2022 · N743YX · Emb ERJ170200LRSDR R61A2022022200158Shear Web · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII FLOOR SUPPORT RH SHEAR WEB AT FR87 TO FR88 RBL 23 CORRODED. FLOOR SUPPORT RH SHEAR WEB AT FR87 TO FR88 RBL 23 WAS REMOVED AND REPLACED IAW SRM 51-42-01 AND SRM 51-42-02.Feb 15, 2022 · N743YX · Emb ERJ170200LRSDR R61A2022022200157Floor Support · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII, FLOOR STRUCTURE FLOOR SUPPORT CORRODED AT FR 88 TO FR90, RBL 36. CENTER FUSELAGE III CORRODED FLOOR BOARD AT FR88 TO FR90 AT RBL36 WAS REMOVED AND REPLACED IAW SRM 51-43-03.Feb 15, 2022 · N743YX · Emb ERJ170200LRSDR R61A2022022200156Gusset · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CFIII, FLOOR STRUCTURE, GUSSET PLATE AT FR90, RBL 26 CORRODED. GUSSET PLATE AT FR90, RBL26, LOCATED ON FLOOR STRUCTURE IN CENTER FUSELAGE III WAS REMOVED AND REPLACED IAW SRM 51-41-02.Feb 15, 2022 · N743YX · Emb ERJ170200LRSDR CALA2022021600401Intercostal · damaged(A3NB-53-4-0033) DURING ROTO INSPECTION OF RH FR66 STGR12 GUSSET PLATE. REJECTABLE DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHAN ICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN RED.() DURING ROTO INSPECTION OF RH FR66 STGR 12 GUSET PLATE REJECTABLE MOBIFeb 15, 2022 · N475UA · Airbus A320232SDR ANCF20220216009Nose Cowl · not reportedPILOT REPORT: 14.FEB.2022 WO 54'346'752=> BIRD IMPACT DURING TAKE OFF ROLL LANDING WAS MADE WITH 62.6 TONS AND NO VARIATIONS OF PARAMETERS OCURRED CORRECTIVE ACTION 14. FEB.2022 =>THE RADOME WAS REMOVED AND REPLACED IN ACCORDANCE WITH AMM TASK 53-15-11-00Feb 14, 2022 · N743AV · Airbus A320214SDR CALA2022021600398Fitting · cracked(AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 LH SIDE CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR BEFO RE NEXT FLIGHT.Feb 14, 2022 · N475UA · Airbus A320232SDR CALA2022021600397Crossbeam · cracked(AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IAFeb 14, 2022 · N475UA · Airbus A320232SDR CALA2022021600392Fitting · corrodedSHEAR TIE CORRODED AT STA 28L FWD OF STA 1560. REMOVED AND REPLACED SHEAR TIE AT STA 1560 S-28L IAW B757 SRM 51 -40-02 PARA 4. WORK PERFORMED BY V936267, V933877 SEE REF AMES NR142726-0100-0082 FOR INSPECTION RII SIGN OFF BY INSPECTOR V933877Feb 14, 2022 · N14107 · Boeing 757224SDR QXEA2022021500063None · corrodedSEAT RAIL 19 CORRODED AT FSX 435.000 RBL Y 40. SEAT RAIL 19 AT FSX 435.000 RBL Y40 BLENDED WITHIN LIMITS IAW SRM 53-30-49-02-02 REV 21.Feb 14, 2022 · Bombdr DHC8402SDR UIEA2022021400108None · noneCRACK ON SIDE ANGLES OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300 AND STA 320, RBL 30, WL 190.(<P>ACCOMPLISHED EI NO T2022A53M-088, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021400109None · noneCRACK ON SIDE ANGLES OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300, LBL 30, WL 190.(<P>ACCOMPLISHED EI NO T2022A53M-087 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021400110None · noneFOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STA 500 - STA 520, S-26L - S-28L.(<P>EXISTING REPAIR DOUBLER WAS COVERED BY EO NO 4453B133 REV 1 AND EI NO T2022A53M-351 REV 1. REFER RAM FORM N408MC-22-22. JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500118None · noneDEVIATION WAS FOUND DURING PERFORMING SB 747-53A2450.(<P>ACCOMPLISHED IAW EI NO T2022A53M-355 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500119None · noneREPAIR - CRACK DAMAGE ON A FASTENER HOLE OF RH AFT INNER CHORD OF STA 2598 BULKHEAD AT RBL 37, WL 267(<P>REMOVED AFFECTED FASTENERS IAW SRM 51-40-02 REV 93. REPAIRED DAMGED AREA IAW EI NO T2022A53M-139 REV 2. INSTALL FASTENER IAW SRM 51-40-02 REV 93 AND DWG NOFeb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500121None · noneBROKEN - DAMAGE ON THE CRGO TRACK BETWEEN STA 1840 AND STA 1860, RBL 24.75(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV 93. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-10 REPAIR 10 REV 93 AND EI NO T2022A53M-302 REV 1. INSTALLED FASTENER IAW SRM 51-40-02 REV 93Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500122None · noneCORROSION DAMAGES ON MAIN - DECK OUTBD FLOOR PANEL SUPPORT BETWEEN STA 1900 AND STA 1920, RBL 117.(<P>ACCOMPLISHED THE REPAIR IAW EI NO T2022A53M-083 REV 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500123None · noneFOUND CORROSION DAMAGE ON MAIN DECK FLOOR BEAM UPPER CAP AT STA 2040 LBL 65.(<P>REMOVED DAMAGED PART IAW SRM 51-40-02 REV 93. REPAIRED DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 93 AND EI NO T2022A53M-220 REV 1. INSTALL FASTENERS IAW SRM 51-40-00-02 REV 93Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500125None · noneCORROSION WAS FOUND ON THE UPPER CAP (P/N 65B04352-167) OF MAIN DECK FLOOR STRUCTURE AT STA 2300 LBL 56(<P>ACCOMPLISHED EI NO T2022A53M-203 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500126None · noneCORROSION DAMAGE ON THE SEAT TRACK (P/N 65B38961-4) OF MAIN DECK BETWEEN STA 2100 AND STA 2110.45, RBL 98.58.(<P>REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 93. REPAIRED CORROSION AREA IAW SRM 53-00-52 REPAIR 6 REV 93 AND EI NO T2022A53M-354 Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500127None · noneFOUND CORROSION DAMAGE ON MAIN DECK FLOOR BEAM UPPER CAP AT STA 2040 BETWEEN RBL 75.92 AND RBL 98.58(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV 93. REPAIRED THE DAMAGED AREA IAW SRM 53-00-551-2R-3 REPAIR 3 REV 93 AND EI NO T2022A53M-224 REV 1. INSTALL FASTEFeb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500129Angle · noneCORROSION - BRACKET, FWD WING TO BODY FAIRING INTERNAL BRACKET STA 977 TO STA 982 LBL 3.(<P>REMOVED DAMAGE PART IAW SRM 51-40-02 REV 93. INSTALL NEW PART IAW SRM 51-40-02 REV 93 AND BOEING DWG NO 65B06976 SH 2 REV G. JOB COMPLETED AND CONDITION CHECK NORMAL.</Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500130Splice · noneCORROSION - M/D STIFFENER SPLICE AT STA 1947 LBL 75.92(<P>REMOVED DAMAGED PARTS IAW SRM 51-40-02-0G-0 , REV 93. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0, REV 93 AND DWG NO 65B38251 SHEET 32 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500131Angle · noneCORROSION DAMAGE WAS FOUND ON ANGLE (P/N 65B04351-334) OF M/D CGO FLOOR STRUCTURE AT STA 2280, RBL 49(<P>REMOVED DAMAGED ANGLE IAW SRM 51-40-02 REV 93. FABRICATE NEW ANGLE IAW EI NO T2022P53M-188 REV 0. INSTALL NEW ANGLE IAW SRM 51-40-02 REV 93 AND DWG 65B0435Feb 14, 2022 · N408MC · Boeing 74747UFSDR UIEA2022021500132Intercostal · noneCORROSION DAMAGE WAS FOUND ON INTERCOSTAL (P/N 146U3014-3) OF AFT CGO COMPARTMENT NEAR S-38R AND STA 1975(<P>REMOVE THE DAMAGED PARTS IAW SRM 51-40-02 REV 93. FABRICATION NEW PART IAW EI NO T2022P53M-357 REV 0. INSTALL NEW PART IAW DWG NO 65B04652 SH1 REV J, SFeb 14, 2022 · N408MC · Boeing 74747UFSDR CALA2022021400383Crossbeam · cracked(AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IAFeb 14, 2022 · N475UA · Airbus A320232SDR CALA2022021400382Skin · damagedAIRCRAFR DAMAGE,LEFT SIDE, BELOW THE 14TH WINDOW, 7:00 POSITION, DAMAGE OUTER SKIN 10 INCH BY 4 INCH VERIFIED PER AVO 5900 PART A. STEPS 1 THRU 6. OK TO CONTINUE. PER AVO 5900 COMPLIED WITH PART A. STEPS 1 THRU 6. PER AVO9500 PART A STEP 7 HFEC CW ON CUTOUT RFeb 14, 2022 · N76062 · Boeing 767424ERSDR JR2R20220213453Beam · corrodedLH FLOOR BEAM IS CORRODED AT FR87 AND LBL9Feb 13, 2022 · N88341 · Emb ERJ170200LRSDR JR2R20220213450Beam · corrodedFLOOR BEAM CORRODED AT FR87 AND RBL9Feb 13, 2022 · N88341 · Emb ERJ170200LRSDR JR2R20220213446Intercostal · corrodedFLOOR BEAM CORRODED BETWEEN FR89 AND FR90 AT RBL9Feb 13, 2022 · N88341 · Emb ERJ170200LRSDR JJBA20220212020Not Reported · not reported1 EA DOUBLE DRILLED HOLE AT FRAME 21 STR 15L COMMON TO FLOOR SILL. REPAIRED HOLES AT FRAME 21 STR 15L COMMON TO FLOOR SILL.Feb 12, 2022 · N11199 · Emb EMB145XRSDR FDEA202202120281Stiffener · crackedEMPENNAGE - AFT FUSELAGE BULKHEAD STATION 2163.685 LEFT HAND SIDE LOWEST STIFFENER GUIDE PIN RECEPTACLE AREA FOUND CRACK 0.8 INCHES. EMPENNAGE - AFT FUSELAGE BULKHEAD STATION 2163.685 LEFT HAND SIDE LOWEST CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM Feb 12, 2022 · N576FE · Doug MD11FSDR JJBA20220212010Not Reported · not reportedPOSSIBLE CORROSION LAV FLOOR (LATERAL) SUPPORT FR 59-60+8 STR 15L. REMOVED DAMAGE FLOOR SILL, LOCATED AND DRILLED NEW FLOOR SILL AND INSTALLED NEW FLOOR SILL.Feb 12, 2022 · N13202 · Emb EMB145XRSDR SCNA202217003None · noneDEFECT SECTION 43 FUSELAGE SKIN GOUGED FROM BS414 TO BS438 AT S-20R. RESOLUTION: DAMAGE WAS TRIMMED OUT FROM BS414 TO BS438 AT STRINGER 20R. STRINGER 20R WAS FOUND CRAKCED ATHE THE AFT THREE FASTENER HOLES WHICH WAS TRIMMED AND REPAIRED. A REPLACEMENT STRINGFeb 12, 2022 · N816SY · Boeing 7378Q8SDR SCNA20220217002None · noneWO 67327: REPAIR OF GROUND DAMAGE TO THE FUSELAGE AT BS 410-440 AND STRINGER 19R-21R. BOEING WAS CONTACTED FOR REPAIR OF THE DAMAGE. RESOLUTION: COMPLIED WITH ACCOMPLISHMENT OF REPAIR PER ATS ER 22-01166 REV IR.Feb 12, 2022 · Boeing 7378Q8SDR CALA2022021400369Frame · gougedUPON REMOVAL OF EXTERNAL POWER RECEPTACLE FOUND GOUGES ON FRAME AT STA 235.8 WL181.1 BL55.5. (DOT AP56-065).(REF AAR RFD NR 99927570).Feb 12, 2022 · N38403 · Boeing 737924SDR IXXA2022021203Stand Off · bentFLOORBOARD STANDOFF BENTFeb 12, 2022 · N762CX · Boeing 767232SDR IXXA2022021201Access Door · bentACCESS PANEL BENTFeb 12, 2022 · N762CX · Boeing 767232SDR SCNA20220325019None · noneDEFECT: ROW 14 ABC EMERGENCY LIGHT ON DOOR KEEPS FLICKERING ON AND OFF. RESOLUTION: R&R ROW 14ABC SIDEWALL LIGHT REF AMM 33-21-00 OPS CHECK GOOD.Feb 11, 2022 · N832SY · Boeing 7378SDR SCNA20220322007None · noneDEFECT: DURING INSPECTION OF THE BS 967 FLOOR BEAM (PN 147A5505-6), CORROSION WAS FOUND ON THE UPPER FLANGE BETWEEN LBL4 AND LBL20,WL208. RESOLUTION: ACCOMPLISHED REPAIR OF BS967 FLOOR BEEAM UPPER "T" CHORD FROM RBL2 TO LBL32 IN ACCORDANCE WITH ATS ER 22-0113Feb 11, 2022 · N823SY · Boeing 73785PSDR IXXA2022030305Web · corrodedFLC BILGE PANEL @STA 610-632 LBL 12-36 FOUND TO BE CORRODEDFeb 11, 2022 · N449AZ · Boeing 7673P6
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