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.
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
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 DHL2002803537Skin · dentedITEM REF. N/R: 0179: FUS. EXT. EXTERNAL SKIN DENTED 30.0000 " LONG NEAR L14R STA. 35.000 - STA. -12.000 ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW FAX BOEING DHL-CVG-02-00057H; ED-3135 & ED-3142. REMOVED FASTNERSIAW SRM 51-1-21 PG. 1 , CLEANED , TREATED SDR ABXA020296Cap · corrodedFORWARD CARGO LOWER LOBE, STATION 676, DEEP CORROSION ON UPPER CAP AT LEFT BUTT LINE 20. REPLACED CAP IAW SRM 51-40-02.SDR ABXA020260Fitting · crackedANGLE CRACKED AT LONGEON 30 JUST AFT OF FORWARD 'P' DOME, KEEL AREA. REPLACED ANGLE IAW DC-9 SRM 51-30-5.SDR ABXA020250Splice · crackedINBOARD AFT FITTING, FLOOR BEAM STA. 965 LEFT, WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA020295Cap · corrodedFORWARD CARGO LOWER LOBE, STATION 522, RIGHT BUTT LINE 25, DEEP CORROSION ON UPPER CAP. REPLACED CAP IAW SRM 51-40-02.SDR ABXA020248Fitting · crackedFITTING CRACKED, FORWARD OF INBOARD GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR DL76L021154Structure · vibrationFLIGHT ATTENDANTS NOTICED VIBRATIONS IN THE AREA OF THE MID GALLEY WITH MORE NOTICED ON THE RIGHT SIDE. CONFIRMED BY THE RELIEF PILOT AND NOTICED THAT VIBS DECREASED WITH ACFT SLOWING DOWN BELOW 300 KTS. ON APPROACH THE VIBRATIONS INCREASED AND THEN WENT AWASDR ABXA020298Floor Panel · corrodedFORWARD CARGO LOWER LOBE, STATIONS BETWEEN 544 - 610, FROM RIGHT BUTT LINE 10, LEFT BUTT LINE 10, CORRODED SHEAR FLOOR PANEL. REPLACED PANEL IAW N.R.C. LT 135 AND SRM.SDR C2XA02TY147Sill · corrodedTYS, During a scheduled inspection the service door seal was found corroded. Maintenence repaired the damage by cleaning the corrosion and installing a lateral doubler. I/A/W-EMB-135/145-SRM-53-21-02, 51-40-02, CPM-51-21-04,05 & 06 and GST-2807/02. The repair SDR ABXA020223Longeron · crackedLONGERON 4 LEFT, CRACKED AT F.S. 200. REPLACED LONGERON IAW DC-9 SRM.SDR COMA0260527Angle · crackedRH OBLIQUE ANGLE IS CRACKED AT FS 625.0 P/N 601R35012-52.REPAIRED RH OBLIQUE ANGLE AT F.S. 625.0 P/N 601R35012-52 I/A/W CANADAIR REO 601R-53-61-100.SDR ABXA020217Angle · crackedSHEARTIE AT F.S. 1059, LONGERON 15 RIGHT WAS CRACKED. REPAIRED SHEARTIE IAW DC-9 SRM 51-30-5 AND ABX DRAWING #K05159.SDR COMA0260521Angle · crackedRIGHT SIDE F.S. 484 ANGLE CRACKED ON OUTBOARD SIDE AT RBL 36.FABED AND INSTALLED NEW ANGLE ON F.S. 484 OUTBOARD SIDE AT RBL 36 IAW WVAC EO 601R-53-3438A.SDR COMA0260511Intercostal · crackedINTERCOSTAL CRACKED AT F.S. 460 OUTBOARD OF LBL9.REPAIRED F.S. 460 INTERCOSTAL I/A/W WVAC EO 601R-53-3440B.SDR ABXA020169Skin · corrodedDURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN, LOCATED AT THE LOWER CARGO DOOR JAMB, FORWARD LOWER CORNER. THE DAMAGE TO THE SKIN WAS TRIMMED OUT AND A NEW SECTION OF SKIN WAS SPLICED IN, IAW DC-9 SRM 53-04, FIG. SDR ABXA020168Doubler · corrodedDURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN RESULTING IN THE DISCOVERY OF CORROSION ON THE INTERNAL DOUBLER P/N 5910158-24. THE DAMAGE TO THE INTERNAL DOUBLER WAS TRIMMED OUT AND A NEW SECTION SPLICED IN IAW DC-SDR CX2A02SH60Butt StrapSHV DURING C CHECK LEFT HAND LATERAL FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074.THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH045Butt Strap · corrodedSHV-DURING C-CHECK INSPECTION, THE RIGHT HAND LATERAL FLOOR BEAM WAS FOUND TO HAVE CORROSION AROUND THE NUTPLATE HOLES BETWEEN FRAMES 59 AND 61.MIANTENANCE REMOVED AND REPLACED THE RIGHT HAND BUTT STRAP BETWEEN FRAMES 59 AND 61 IN ACCORDANCE WITH EMB 145 SRM 5SDR C2XA02SH044Butt Strap · corrodedSHV-DURING C-CHECK INSPECTION, THE LEFT LATERAL BEAM AND CENTER FLOOR BEAM NUTPLATE HOLES WERE FOUND TO BE CORRODED AT BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT HAND AND CENTER BUTT STRAP'S BETWEEN FRAMES 59 AND 61 IN ACCORDANCE WSDR ABXA020205Angle · damagedRIGHT DORSAL FIN ATTACH ANGLE HAD TOOLING DAMAGE IN THE RADIUS. REPLACED DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5, AND REA D953-44887.SDR VNAA0208023Structure · vibrationDURING CLIMBOUT, THE CREW REPORTED A VIBRATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND PERFORMED A FUNCTIONAL CHECK FLIGHT WITH THE CREW AND COULD NOT DUPLICATE THE VIBRATION. AFTER THE SATISFACTORY FUNCTIONAL CHECK FLIGHT, THE AIRCRAFT WAS RELEASED FSDR ABXA020200Former · crackedFORWARD LOWER CARGO DOOR, LOWER FORWARD STOP INTERCOSTAL FORMER WAS CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR DHL2002363522Cover · corrodedC-check/web between fr. 25 an fr. 26 above str. 45R has 10 sq. in. of corrosion.Corrective action/ Removed corroded web IAW A300 SRM 51-30-30. Went for engineering support.Fabricated new cover plate from 0.025" 2024-T3 clad. Cutout cover plate per Fig. 1. TreaSDR DHL2002363511Skin · corrodedC-check/Sta.1380 STR. 48L interior of skin has 3 SQ" of moderate corrosion.Corrective action/ Smoothed an blended area of corrosion IAW A300 SRM 51-40-11. Material removed is .022" max allowable material loss is .047" area within limits IAW A300 SRM 53-12-00 FSDR COMA0260476Intercostal · crackedWHILE ACCOMPLISHING THE REPLACEMENT OF FRAME 574 THE INTERCOSTAL FOR THE CARGO DOOR SUPPORT STRUCTURE WAS DAMAGED. THE INBOARD FLANGE WAS BENT AND TWO CRACKS DEVELOPED.THE DAMAGED FLANGE WAS CUT OFF AND A REPAIR ANGLE WAS FABRICATED AND INSTALLED I/A/W WVAC EOSDR COMA0260470Flange · crackedTHE INTERCOSTAL FLANGE AT BL36 (L/H & R/H)AND ANGLES AT BL27(L/H&R/H) ARE CRACKED AT F.S. 484.REPAIRED INTERCOSTAL FLANGE AND ANGLES AT (L/H&R/H) AT BL36 AND BL27 I/A/W WVAC E.O. 601R-53-3409 AT F.S. 484.SDR DHL2002363521DoublerC-check/R/H aft. fuselage external doubler is bulging @ Fr. 72,str. 46R to 44R.Corrective action/ Removed 5 ea. hilocks from fr. 72 IAW A300 SRM 51-30-30.Inspected holes for corr. or seperation of doubler found no defect.Installed 5 ea. hilocks in fr. 72 IAW ASDR DHL2002363510Skin · corrodedC-check/R/H aft upper fuselage ext. skin has areas of corr. @ fr80 between STR. 12R to 17R.Corrective action/removed corrosion IAW A300 SRM 51-40-11. UT thickness checked per NTM 51-20-00 before 2.04 mm minimum after 1.97 mm. Treated an protected area IAW A300SDR DHL2002363509Skin · corrodedC-check/R/H aft upper fuselage ext. skin has areas of corr. @ FR. 80 between STR. 4R to 11RCorrective action/Removed corr. IAW A300 SRM 51-40-11. UT thickness checked per NTM 51-20-00, minimum remaining1.75 mm before 1.85 mm within limits per SRM A300 53-10-00SDR COMA0260454Angle · crackedTHERE WAS A CRACKED INTERCOSTAL ANGLE AT STR 12L BETWEEN FS621 AND FS625.3.REMOVED THE CRACKED ANGLE. FABRICATED PER SAMPLE (FROM S6144-4 PERFORMED ANGLE) A REPAIR ANGLE AND INSTALLED THE REPAIR ANGLE I/A/W WVAC EO 601R-53-3390.SDR ABXA020172Angle · crackedLOWER RIGHT PYLON ATTACH ANGLE WAS CRACKED AT STATION 1072. INSTALLED SECTION OF ATTACH ANGLE IAW DC-9 SRM 54-04.SDR SIMA200220502Fastener · elongatedFOUND RIGHT HORIZONTAL STABILIZER UPPER FORWARD SPAR CAP FASTENERS HOLE AT THE INBOARD END WAS FOUND TO BE ELONGATED. REMOVED HORIZONTAL STAB. LEADING EDGE RIB AND MOUNTING ANGLE ON THE SPAR WEB. FABRICATED A REPLACEMENT SECTION SPAR WEB, TWO DOUBLER, ANGLE SDR C2XA02SH029Sill · corrodedSHV - DURING C-CHECK INSPECTION THE LEFT HAND SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 60 AND 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IN ACCORDANCE WITH EMB-145 SRM51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ABXA020140Shear TieSHEAR TIE INSTALLED AT STATION 1417, BETWEEN STRINGER 20 LEFT TO STRINGER 21 LEFT, HAD SHORT EDGE MARGIN TO FASTENER. REPAIRED AREA IAW REA B653-43456-DE.SDR SIMA200220503Windshield · corrodedFOUND PILOT WINDSHIELD CUTOUT LOWER STRIP HAS 6 CORRODED HOLES. REMOVED CORROSION BY REAMING HOLES 2 AND 4 TO ALLOWABLE LIMITS. REAMED HOLES 1 AND 4 TO .313 TO REMOVE CORROSION. FABRICATED TO FREEZE PLUGS. REPAIR DONE IAW SRM. (B8349)SDR C2XA02SH030Butt Strap · corrodedSHV-DURING C-CHECK INSPECTION,THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 22.MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTIONS OF BUTT STRAP IN ACCORDANCE WITH EMB-145 SRM 51-40-02,AND THE AIRCRAFT WAS WAS APPROVED FOR RETURN TO SESDR C2XA02SH028Crease Beam · corrodedSHV-DURING C-CHECK INSPECTION.THE RIGHT HAND O/B CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22.MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IN ACCORDANCE WITH EMB-145 SRM 51-40-02,AND THE AIRCRAFT WAS APPROVED FOR RETURNSDR C2XA02SH027Crease Beam · corrodedSHV - DURING C-CHECK INSPECTION, THE RIGHT HAND O/B CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RSDR C2XA02SH026Butt Strap · corrodedSHV - DURING C-CHECK INSPECTION, THE LEFT, CENTER, AND RIGHT HAND BUTT STRAPS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTIONS OF BUTT STRAPS IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SDR C2XA02SH025Butt Strap · corrodedSHV - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 18. MAINTENANCE REMOVED THA DAMAGED SECTIONS OF BUTTSTRAP, AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND THE AIRCRAFT WAS APPROVSDR ABXA020155Doubler · crackedCRACK IN FUSELAGE SKIN AT STATION 994, LONGERON 12 RIGHT, BETWEEN 2 RIVETS AND EXTENDING 1/4" PAST BOTH RIVETS. REPAIRED CRACK IAW DC-9 DWG SR09530151 AND E.A. 5311005-034.SDR ABXA020100Beam · corrodedMAIN CABIN STATION 940, RIGHT BUTT LINE 68, CORROSION UNDER BEAM AND SHEAR WEB PANEL, LOWER SIDE CORNER. REPAIRED AREA IAW REA D853-43931-MR.SDR ABXA020097Web · corrodedMAIN CABIN STATION 960, CORROSION UNDER BEAM AND SHEAR WEB BY LEFT BUTT LINE 68. REPAIRED AREA IAW ABX REA D853-43930-MR.SDR 02FDEA00499Stringer · corrodedN 108 STRINGER 56R AT CONNECTOR AFT OF FRAME 72. R&R STRINGER PER SRM 53-10-14.SDR COMA0260415Angle · crackedFS 621 FLOOR SUPPORT ANGLE CRACKED WL 73.50 RBL 41.COMPLIED WITH REO 601R-53-61-117 REV A AND WVAC EO 601R-53-3339. LOCATED AND INSTALLED ANGLES 601R53-61-004-2, 601R53-61-004-6 AND 601R53-61-004-4. INSTALLED FABRICATED RADIUS BLOCK IAW REO 601R-53-3339.SDR ABXA020105Fitting · crackedCABIN UNDER FLOOR FRAME STIFFENER WAS CRACKED AT FS 780, LEFT BUTT LINE 47.0. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D, 51-3-2 AND 51-3-0.SDR ABXA020094Longeron · corrodedAIR COND/PRESS COMPARTMENT AT FS 36, LONGERON 31 RIGHT, AT OUTBOARD SIDE WAS CORRODED AROUND FASTENERS. FABRICATED REPAIR STRAP AND REPAIRED AREA IAW REA D853-43733-MR, SRM 53-2-0, 51-1-8, 51-1-20D.SDR ABXA020156Doubler · cracked5" CRACK TOP OF FUSELAGE AT #1 LONGERON IN AFT PRESSURE BULKHEAD AREA. REPAIRED CRACK IAW DC-9 DWG SR0953151 AND E.A. 5311005-034.SDR 377PA0005Skin · damagedFuselage skin damaged by belt loader at sta 789 to sta 799 between str26Rt. and str27Rt.SDR 377PA0004Skin · damagedFuselage skin damaged by belt loader sta 797 to sta 818 at str27Lt.
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