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.

SDR DALA2016022701498Pan · crackedCRACK ON LT WINDOW WING PAN UPPER FWD CORNER BS 788 AT PAX CABIN INNER STRUCTURE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/AS 493648-14MA, REV A AND 487747-14MA REV ORIGINAL.Feb 26, 2016 · N904DE · Doug MD88SDR DALA2016022701496Pan · crackedCRACK ON RT FWD LOWER CORNER RING PAN, BS 1098-1117. RING PAN RT FWD LOWER CORNER AT BS 1098-1117 WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 AND 53-05 FIG 122 AND ER/AS 497747-14MA REV ORIGINAL AND 493648-14MA, REV A.Feb 26, 2016 · N904DE · Doug MD88SDR DALA2016022701495Pan · crackedCRACK ON RT LOWER AFT CORNER OF RING PAN BETWEEN BS 886-905. FASTENERS AND DAMAGE AREA WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE TREATED/PAINTED IAW SRM 51-10-3, PAR 14 ANFeb 26, 2016 · N904DE · Doug MD88SDR DALA2016022701494Pan · crackedCRACK ON RT AFT UPPER CORNER RING PAN BS 1041-1060. RING PAN RT AFT UPPER CORNOR AT STA 1041-1060 WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 AND 53-05, FIG 122 AND ER/A'S 497747-14. REV ORIGINAL AND 493648-14MA, REV A.Feb 26, 2016 · N904DE · Doug MD88SDR DALA2016022701493Angle · crackedCRACK ON ANGLE FITTING AT RT AFT UPPER CORNER RING PAN BS 984-1003. DAMAGE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122 AND REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 14 AND 21 AND ER/AS 497747-14MA, REV. ORIGINAL AND 493648-14MA, REV A.Feb 26, 2016 · N904DE · Doug MD88SDR DALA2016022701492Pan · wornWEAR ON RT LOWER AFT CORNER RING PAN, BS 1060-1079. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 AND 53-05, FIG 122 AND ER/A 497747-14MA, REV ORIGINAL AND 493648-14MA, REV A.Feb 26, 2016 · N904DE · Doug MD88SDR YENA20160226138Beam · corrodedAFT PASSENGER DOOR LOWER BEAM 2" AFT OF FRAME 85, LBL47, CORRODED ETD 2016-190-010746 ATTACHED. REPAIRED IAW EC E16-094-01, REF EAMS NR H4859-00093.Feb 26, 2016 · N236JB · Emb ERJ190100IGWSDR YENA20160226137Beam · corrodedAFT PASS DOOR LOWER BEAM 6" AFT OF FRAME 85, LBL47" CORRODED. REPAIRED IAW EC E16-094-01.Feb 26, 2016 · N236JB · Emb ERJ190100IGWSDR QXEA2016031400186Beam · corrodedOUTER EDGE BEAM HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-07, SRM 51-40-07, 51-42-05, AND DWG:85339541, REV B.Feb 25, 2016 · N422QX · Bombdr DHC8402SDR IPXA2016030300288Crossbeam · deformedINSPECTION TYPE:10YR, CABIN OVERWING AREA FR 49 CROSSBEAM AT -Y450 TO -Y953 IS BOWED REPLACED CROSSBEAM SRM 51-40-21.Feb 25, 2016 · N173UP · Airbus A300F4622RSDR IPXA2016030300287Crossbeam · deformedINSPECTION TYPE:10YR, CABIN OVERWING AREA FR 48 CROSSBEAM AT -Y450 TO -Y953 IS BOWED REPLACED CROSSBEAM IAW SRM 51-40-21.Feb 25, 2016 · N173UP · Airbus A300F4622RSDR IPXA2016030300286Crossbeam · deformedINSPECTION TYPE:10YR, CABIN OVERWING AREA FR 50 AT -Y450 TO -Y953 IS BOWED. REPLACED CROSSBEAM IAW SRM 51-40-21.Feb 25, 2016 · N173UP · Airbus A300F4622RSDR IPXA2016030300285Crossbeam · crackedINSPECTION TYPE:10YR, CABIN OVERWING AREA FRAME 51 AT -Y450 TO -Y953 IS CRACKED. REPLACED CROSSBEAM IAW A300, SRM 51-40-21.Feb 25, 2016 · N173UP · Airbus A300F4622RSDR DALA2016022601453Door Frame · corrodedCORROSION ON MID CARGO COMPARTMENT LOWER FWD DOOR JAMB BEAM BETWEEN BS 665-690. JAMB BEAM WAS REPAIR IAW ERA 543157-14.Feb 25, 2016 · N991DL · Doug MD88SDR SWAA2016031449851Crease Beam · damagedRIGHT CREASE BEAM WEB DAMAGED, BETWEEN BS 927 - 947. R & R WEB IAW DWG & SRM.Feb 24, 2016 · N391SW · Boeing 7373H4SDR IPXA2016030300314Door Frame · dentedINSPECTION TYPE:SVC, LOWER AFT CARGO DOOR BOTTOM DOOR FRAME IS GOUGED AND DENTED AT CORNER. R & R AFT CARGO DOOR LOWER AFT FRAME CORNER IAW SRM 51-40-02.Feb 24, 2016 · N408UP · Boeing 75724APFSDR ASAA2016022315705Door Frame · corrodedAFT CARGO COMPARTMENT CARGO DOOR SURROUND LOWER SILL WEB IS CORRODED. ACFT GROUNDED. ACCOMPLISHED BLENDOUT OF CORRODED AREA AT AFT CARGO COMPARTMENT CARGO DOOR SURROUND LOWER SILL WEB IAW SRM 51-10-02. ORIGINAL MATERIAL: .056", REMAINING MATERIAL: .035", MAFeb 23, 2016 · N557AS · Boeing 737890SDR SWAA2016030249578Crease Beam · corrodedLEFT CREASE BEAM WEB CORRODED, BETWEEN BS 460 - 480, WL 208. R & R WEB IAW SRM & DWG.Feb 23, 2016 · N384SW · Boeing 7373H4SDR SWAA2016030249577Crease Beam · corrodedRIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 400 - 420, WL 208. R & R WEB IAW SRM & DWG.Feb 23, 2016 · N384SW · Boeing 7373H4SDR DALA2016022501401Pan · crackedCRACKS ON AFT/LOWER CORNER OF LT WINDOW RING PAN AT BS 275-598 PASSENGER CABIN, SM REASON FOR RE-WRITE INADECUATE WASHERS ON REPAIR RE-WRITE FROM CARD 86, ZONE 201. NEW HARDWARE WERE INSTALLED IAW SRM 51-30-5, PAR 7 AND SRM 53-05, FIG 122.Feb 23, 2016 · N993DL · Doug MD88SDR SWAA2016031849996Crease Beam · corrodedRIGHT CREASE BEAM CORRODED AT STATION 970. REPAIRED BEAM IAW SRM.Feb 22, 2016 · N391SW · Boeing 7373H4SDR SWAA2016031449850Crease Beam · corrodedLEFT CREASE BEAM CORRODED, BETWEEN BS 986 - 992, STRINGER 17L. R & R CREASE BEAM IAW SRM & DWG.Feb 22, 2016 · N391SW · Boeing 7373H4SDR SWAA2016031449849Crease Beam · corrodedRIGHT CREASE BEAM CORRODED AT BS 1002, STRINGER 17R. R & R CREASE BEAM IAW SRM & DWG.Feb 22, 2016 · N391SW · Boeing 7373H4SDR DALA2016022301339Door Frame · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR JAMB UPPER BEAM FROM BS 1155 TO 1190. BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.Feb 22, 2016 · N926DL · Doug MD88SDR ASOA20160222009VBeam · corrodedDURING C-CHECK, BOLT HOLES FOR CTR 3 PIECE TRIM ON PLANE AREA CORRODED INTERNALLY. R & R CARGO DOOR CUTOUT LOWER BEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.Feb 22, 2016 · N18557 · Emb EMB145LRSDR C77A20160222018Beam · corrodedDURING BASIC CHECK IN SAT, INSPECTION DISCOVERED CORROSION ON THE AFT CABIN RT AFT BEAM, PN 170-65669-004, UPPER SURFACE ON THE SUBJECT FLOORBEAM. THE DAMAGE DIMENSIONS ARE REPORTED AS FOLLOWS, 1.40 INCHES X 1.40 INCHES TO A MAX DEPTH OF .025 INCH DEEP. REQUFeb 22, 2016 · N623CZ · Emb ERJ170200LRSDR SWIA201641950Door Frame · damagedPAX DOOR FWD FORMER OUT OF LIMITS. REPLACED THE PAX DOOR FWD FORMER IAW AMM. PRESSURE AND OPS CHECKED GOOD.Feb 21, 2016 · N813SK · Cndair CL6002D24SDR ASAA2016022115692Web · gougedLOWER FUSELAGE ELECTRONIC EQUIPMENT COMPARTMENT DOOR CUTOUT, RT INTERCOSTAL WEB UPPER EDGE IS GOUGED. ACFT GROUNDED. R & R WEB, PN 141A8512-28, REF SRM 51-40-02, BAC DWG 141A8511. OPS CHECK GOOD. REMOVED DOT.Feb 21, 2016 · N557AS · Boeing 737890SDR SWAA2016030149562Crease Beam · crackedL1 DOOR CREASE BEAM CRACKED AT BS 302.5 AT FWD FASTENER LOCATION. R & R BEAM IAW SRM & DWG.Feb 21, 2016 · N918WN · Boeing 7377H4SDR DALA2016022201296Door Frame · corrodedCORROSION ON LT LOWER SECTION OF VENTRAL STAIRWAY DOOR JAMB FRAME BS 1338 AT PASSENGER CABIN INTERNAL STRUCTURE. LOWER SECTION OF VENTRAL STAIRWAY DOOR JAMB FRAME WAS REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED INSTALLED IAW SRM 51-70-4, FIG 1, 51Feb 21, 2016 · N993DL · Doug MD88SDR DALA2016022201292Door Frame · crackedCRACKED PREVIOUS REPAIR ON NLG DOOR JAMB BS Y=46, X=+18LHZ=-29 AT NLG WHEEL WELL. DOUBLER PREVIOUS REPAIR WAS REPLACED IAW 53-05, FIG 110, 51-10-2, 51-10-4, 51-10-3 AND 51-30-2.Feb 21, 2016 · N926DL · Doug MD88SDR DALA2016022201271Door Frame · corrodedFORWARD CARGO COMPARTMENT DOOR JAMP LOWER SILL 4.5" SPLICE STRAP CORRODED 5" AFT STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCEPTABLE LIMITS, ORGINAL MATERIAL .080, REF SRM 53-20-15, FIG 1. MATERIAL LOSS OF .040 USFeb 21, 2016 · N893AT · Boeing 717200SDR SWIA201641972Door Frame · corrodedPAX DOOR FRAME AT FS 313.56L HAS A CLIP THAT IS CORRODED. REPLACED IAW SRM.Feb 20, 2016 · N441SW · Cndair CL6002B19SDR ASOA2016022014541Crossbeam · corrodedCORROSION ON CROSSBEAM 559 + 80 AND RBL 9. REMOVED CORROSION IAW SRM 51-21-06. REWORKED WITH THE ALLOWABLE DAMAGE LIMITS OF SRM 53-51-15-01 AND SRM 53-00-00-01, FIG 102.Feb 20, 2016 · N902EV · Cndair CL6002B19SDR DALA2016022001353Profile · crackedCRACK ON FWD LOAD TRANSMITTING PROFILE AFT EMERGENCY DOOR RT IN PASSENGER CABIN, REPLACED FWD LOAD TRANSMITTING PROFILE AFT EMERGENCY DOOR RT IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279020.Feb 20, 2016 · N365NW · Airbus A320212SDR SWAA2016032450184Crease Beam · crackedRIGHT CREASE BEAM CRACKED AT STATION 616. REPAIRED CREASE BEAM IAW EA.Feb 19, 2016 · N358SW · Boeing 7373H4SDR SWAA2016032250110Crease Beam · corrodedCREASE BEAM CORRODED AT BS 320, RBL 58. R & R CREASE BEAM IAW SRM.Feb 19, 2016 · N391SW · Boeing 7373H4SDR SWAA2016031649950Crease Beam · crackedRIGHT CREASE BEAM CORRODED AT STATION 294 - 328. REPAIRED CREASE BEAM IAW SRM.Feb 19, 2016 · N391SW · Boeing 7373H4SDR SWAA2016031449847Door Frame · crackedR1 DOOR CUT OUT AFT FRAME STRUCTURE, T CHORD CRACKED AT BS 332, AT DOOR STOP NR 1. R & R T CHORD IAW SRM & DWG.Feb 19, 2016 · N391SW · Boeing 7373H4SDR DALA2016021901427Not Reported · corrodedRT CABIN TRUSS SUPPORT AT BS 1166 AND S20R FOUND CORROSION AND REPAIRED.Feb 19, 2016 · N186DN · Boeing 767332SDR REXA2016021800326Beam · crackedBEAM 280 IS CRACKED JUST OTBD OF LBL 9, LOWER SIDE, BELOW FLOOR. PERFORMED REPAIR TO THE CRACK IN FS 280 BEAM AT LBL 9 IAW REO 601R-53-11-171.Feb 18, 2016 · N8970D · Cndair CL6002B19SDR DALA2016021901252Pan · crackedCRACKED AFT/LWR CORNER ON RT RING PAN BS 731, 905, 1136, AND 1231. DAMAGES WERE REMOVED, INSPECTION WAS PERFORMED ON TRIMMED AREA, NO CRACKS WERE FOUND. REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, INSTALLED IAW SRM 53-05, FIG 122, 51-10-3 PAGE 14 AND 21,Feb 18, 2016 · N993DL · Doug MD88SDR DALA2016021901250Pan · crackedCRACKS ON RING PAN AFT LOWER CORNER IN BS 712 AND 731 LT SIDE AT CABIN PASSENGER RING PANS WERE REPAIRED IAW ER/A 543142-14, REV ORIGINAL.Feb 18, 2016 · N991DL · Doug MD88SDR AC2R201602180001Plate · corrodedLEFT SPONSON AFT PLATE CORRODED. WHEN THE CORROSION WAS REMOVED, THE DEPTH EXCEEDED THE ALLOWABLE LIMIT. THE CORROSION APPEARS TO HAVE STARTED FROM PREVIOUSLY DRILLED HOLES WHICH WERE UNTREATED WITH A CORROSION PREVENTATIVE COMPOUND. THIS SHOULD HAVE BEEN AFeb 18, 2016 · N639NA · Agusta AW139SDR SWAA2016031749971Crease Beam · corrodedRIGHT CREASE BEAM CORRODED AT STATION 970. REPAIRED BEAM IAW SRM.Feb 17, 2016 · N391SW · Boeing 7373H4SDR DALA2016030101560Door Frame · crackedLEFT WHEEL WELL FWD DOOR JAM CRACKED. STOP DRILLED CRACK ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR IAW ERA 544047-14. PERMANENT REPAIR TO BE ACCOMPLISHED IAW ERA 544047-14 WITHIN 10 DAYS FWD TO MON.Feb 17, 2016 · N912DE · Doug MD88SDR DALA2016021701418Not Reported · corrodedBULK CARGO COMPARTMENT AT BS 1540, STR 39L FOUND CORROSION AND REPLACED.Feb 17, 2016 · N186DN · Boeing 767332SDR DALA2016021701416Not Reported · corrodedBULK CARGO COMPARTMENT AT BS 1540 STR 36R, FOUND CORRODED AND REPAIRED.Feb 17, 2016 · N186DN · Boeing 767332SDR DALA2016021701415Not Reported · corrodedBULK CARGO COMPARTMENT AT BS 1540, STR 39R CORRODED AND REPAIRED.Feb 17, 2016 · N186DN · Boeing 767332SDR DALA2016021901255Fitting · crackedCRACKED FITTING ON BS 927 X=44 Z=-15 AT WING BOX AREA. CRACKED FITTING ON BS 927, X= 44Z=-15 AT WING BOX WAS R & R IAW 51-30-5 AND DWG 9923417 ID:1, REV:B.Feb 17, 2016 · N993DL · Doug MD88
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