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 IPXA2016072106135Door Frame · dentedINSPECTION TYPE: C-17, LWR AFT CARGO DOOR LOWER AFT FRAME IS GOUGEDREMOVED AND REPLACED AFT CARGO DOOR LWR AFT CORNER PER UPS B757-200PF SRM 51-40-02SDR AALA201607229008Beam · corrodedHEAVY CORROSION ON NUT PLATE FOR BULK CARGO DOOR THRESHOLD SILL BEAM AT FRAME 62 -1" AND STRINGER 37R. REPAIRED SILL BEAM IAW EA 261799 AND SRM 53-41-49-201-FIGURE 203.SDR IPXA2016071906057Door Frame · crackedINSPECTION TYPE: 2C, L3 DOOR FWD FRAME INTERIOR TORQUE BOX DOUBLER CRACKED BS 1256. REPAIRED THE DOOR JAMB FWD DOUBLER IAW SRM 53-40-15 REPAIR 3 FIG. 201. MAJOR REPAIR.SDR IPXA2016071505883Web · crackedINSPECTION TYPE: 2C, R3 DOOR AFT FRAME INTERNAL TORQUE BOX WEB CRACKED BS 1305 X -19. REPAIRED THE WEB IAW SRM 53-40-15 REPAIR 3 FIG. 201. MAJOR REPAIR.SDR SWAA2016071453813Crease Beam · corrodedR2 DOOR AREA CREASE BEAM CORRODED FROM FORWARD DOOR CORNER TO AFT DOOR CORNER BELOW CENTER THRESHOLD. R & R THE CREASE BEAM IAW SRM AND DWG.SDR AALA201607129004Box Beam · crackedRIGHT SIDE BOX BEAM UPPER FLANGE AFT 2 FASTENER HOLES HAVE CRACKS AT FRAME 43 AND -Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.SDR AALA201607129003Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE CRACKED AT FR 43, +Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.SDR AALA201607189034Beam · corrodedCORROSION ON L1 DOOR CUT OUT LOWER BEAM BETWEEN FRAMES 16 AND 19 AT STRINGER 17 LEFT. REPLACED THE BEAM IAW DRAWING 170-01330-507, SRM 51-43-02,51-43-01,51-41-01 & 51-23-04.SDR WVER070620160003Seal Rest · chafedPERFORMED REPAIR OF DAMAGED PASSENGER DOOR SEAL-STRIKER IAW REO 670-53-22-001-TYPE 1 REV H.SDR AALA201607189026Beam · corrodedCORROSION ON R1 DOOR CUT OUT LOWER BEAM BETWEEN FRAMES 16 AND 19, +Y1250. REPLACED THE BEAM IAW SRM 51-40-02, 51-43-03/-04, & DRAWING 170-65480-445.SDR IPXA2016070705516Angle · crackedINSPECTION TYPE: 3C, RIGHT SIDE AVIONICS COMPARTMENT FRAME 10 CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21.SDR DALA2016070605108Beam · crackedCRACKS ON BEAM 1 FWD AND AFT EDGE AT FWD ENTRY DOOR. BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND FIG 202 TYPE A. CRACKS OF .650" AND .850".SDR REXA2016070401298Beam · corrodedRIGHT BEAM AT FS 280 HAS POSSIBLE CORROSION DAMAGE BENEATH CORROSION CAP AT RBL 9-12. REMOVED CORRODED RT BEAMS. RECEIVED NEW BEAM. LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-SDR FOTR20160704002Door Frame · corrodedCARGO DOOR JAMB CUT OUT HAS CORROISION AT STA. 1400-1440 STRINGER 27RSDR DALA2016070405076Pan · crackedCRACK ON UPPER FWD RING PAN STA Y=756, RT AT PAX CABIN, CARD 29, ZONE 201. UPPER FWD RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L=0.523" HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS FOUND AT TIME OF INSPECTION.SDR DALA2016070405075Pan · crackedCRACK ON UPPER AFT RING PAN STA Y=832 LH AT PAX, CABIN. UPPER AFT RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L =0.510". HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION.SDR DALA2016070405074Pan · crackedCRACK ON LOWER FWD RING PAN STA Y=636 LT AT PAX CABIN, CARD 28, ZONE 201. LOWER RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L=0.480", HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION.SDR DALA2016070405073Pan · crackedCRACK ON UPPER AFT RING PAN STA Y=851 RT AT PAX CABIN, SM, CARD 25, ZONE 201. UPPER AFT RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. L= 0.420", HFEC WAS PERFORMED ON TRIMMED OUT AREA AND NO CRACKS FOUND AT TIME OF INSPECTION.SDR DALA2016070405072Pan · crackedCRACK ON LOWER FWD T-RING PAN STA Y=655 LT AT PAX CABIN, CARD 27, ZONE 201. LOWER FWD RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION, CRACK L=0.450".SDR DALA2016070405071Pan · crackedCRACK ON LOWER FWD RING PAN, STA Y=636 RT AT PASSENGER CABIN. SM, CARD 30, ZONE 201. LOWER FWD RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. LONG CRACK L= 0.510" HFEC PERFORMED TRIMMED AREA AND NO CRACKS FOUND AT TIME OF INSPECTION.SDR REXA2016070101347Window Frame · crackedWEB BELOW LEFT WINDSHIELD SIDE POST SUPPORT IS CRACKED. REMOVED AND REPLACED WEB BELOW LEFT WINDSHIELD SIDE POST IAW SRM 51-42-06.SDR IPXA2016071205744Door Frame · corrodedINSPECTION TYPE: 3C, AFT CARGO DOOR FRAME HAS CORROSION AT BS 1959 BETWEEN X 30 TO 40 AND Z 80. REPAIRED THE DOOR FRAME IAW EA 011-5310-A6351 REV. I/R AND EO MD11-5310-61221-A. (MINOR)SDR CALA2016070500404Crease Beam · corrodedLBL 70, CREASEBEAM, BS 760 CORRODED, REMOVED DAMAGE SECTION OF CREASEBEAM STA 735-STA 765. INSTALLED REPAIR REF SRM 53-00-13, FIG 201, REPAIR 1.SDR IXXA20160817044Failsafe · crackedLEFT FAILSAFE STRAP HAS CRACK INDICATION IN LOWER BOLT HOLE OF TRIM OUT AREA. FAILSAFE STRAP TRIM OUT AND REPAIRED IAW ENGINEERING DOCUMENT 47008ORD03.SDR AALA201607069005Box Beam · crackedRIGHT SIDE BOX BEAM UPPER FLANGECRACKED AT FRAME 43 AND -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.SDR AALA201607069004Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE CRACKED AT FRAME 43 AND +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.SDR ASOA20160630042VBeam · corrodedDURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CALA2016070195493Door Frame · crackedR4 ENTRY DOOR FRAME CRACKED AT AFT UPPER CORNER. STOP DRILLED. HFEC. MFG & INSTALL REPAIR IAW SRM 52-10-02.SDR DALA2016062905018Pan · crackedCRACK ON LT UPPER FWD WINDOW RING PAN AT STA Y=769 AND STA Y=886, AT FUSELAGE CABIN STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3 PAR 21,14, 51-30-2, 51-30-5, 51-30-03, ER/A 493648-14 MA, REV A AND ER/A 487747-14 MA, REV A.SDR DALA2016062905016Pan · crackedCRACK ON RT UPPER FWD WINDOW RING PAN AT STA Y=886, AND Y=946 AT CABIN FUSELAGE STRUCTURE. RING PAN WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA 487747-14MA, REV A AND 493648-14MA, REV A.SDR DALA2016062905015Pan · crackedCRACK ON RT LOWER FWD WINDOW RING PAN AT STA Y=1136, Y=1155, Y=1193 AND Y=1231 AT CABIN FUSELAGE STRUCTURE. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, PAR 139, FIG 122, 51-30-2, 51-30-05, ERA 487747-14MA, REV A, 493648-14 MA, REV A.SDR DALA2016062905014Pan · crackedCRACK ON LT LOWER FWD WINDOW RING PAN AT STA Y=984, Y=1022, Y=1041, Y=1079 AND Y=1098, AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14, 51-30-2, 51-30-5, 51-30-03, ER/A 493648-14MA REV A AND ER/A 487747-14MA, RSDR DALA2016062905013Pan · crackedCRACK ON RT UPPER AFT WINDOW RING PAN AT STA Y=1041, Y= 1098, Y=1117, Y=1193 AND 1212 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, PAR 139, FIG 122, 51-30-02, 51-30-05, ERA487747-14MA, REV A, 493648-14 MA, REV A.SDR AALA201607299027Structure · corrodedLOWER SILL BETWEEN FRAMES 66 TO 68, STRINGER 23R IS CORRODED. REMOVED AND REPLACED SILL IAW SRM A319 51-72-11, DWG D53474250, D534800009 AND EA 261873.SDR AALA201607299026Structure · corrodedLOWER SILL BETWEEN FRAMES 66 AND 68 LEFT SIDE AT AFT GALLEY IS CORRODED. REMOVED AND REPLACED LOWER SILL IAW SRM A319 51-72-11, DRAWING D53480009. AND EA # 261664..SDR DALA2016062804974Door Frame · corrodedCORROSION ON DOOR JAMB WEB BETWEEN STA Y=1155 TO Y=1164 AT C3. WEB WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 DWG 5936442, REV A.SDR DALA2016062804973Pan · crackedCRACK ON LT LOWER AFT WINDOW RING PAN AT STA Y=598 AND Y=826 AT CABIN FUSELAGE STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.SDR DALA2016062804969Pan · crackedCRACK ON LT UPPER FWD WINDOW RING PAN AT STA Y=275, Y=522, Y=560, Y=693 AND Y=712 AT FUSELAGE CABIN STRUCTURE. RING PANS WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.SDR DALA2016062804966Pan · crackedCRACK ON LT UPPER AFT WINDOW RING PAN AT STA Y=1041, Y=1079, Y=1193, Y=1212, Y=1231, AND Y=1250 AT CABIN FUSELAGE STRUCTURE. RING PAN WERE REPAIRED IAW SRM 53-05, FIG 122, 51-10-3 PAR 21, 14 AND 51-30-2, 51-30-5, 51-30-03 AND ER/A 487747-14MA, REV A.SDR DALA2021012800524Attach Fitting · crackedDURING INSPECTION A CRACK WAS FOUND ON THE UPPER ATTACHMENT OF THE LT SLIDING WINDOW FRAME IN HOLE NR 3. CORRECTIVE ACTION: PERFORMED REPAIR ON LATERAL POST WINDSHIELD ATTACHMENT IN COCKPIT ON FRAME 4 LT, AS PER ER/A NR 536222-14AD. CONT ON INSP MON.SDR SWIA201642381Angle · corrodedBS 1098.20 LOWER CAP ANGLE BETWEEN STRINGER 23 - 24L HAS CORROSION. REPAIRED IAW EA.SDR WVER2016062650513Door Frame · crackedCREW ESCAPE HATCH AFT SURROUND STRUCTURE IS CRACKED IN THE RADIUS APPROXIMATELY .250" LONG NEXT TO THE RT HINGE FITTING.SDR AALA201608019005Pressure Deck · crackedPRESSURE DECK MEMBRANE HAS 9 FASTERNER HOLES WITH CRACK INDICATIONS BETWEEN FRAMES 36 + 2.5" AND 36 + 21", +Y1523. REPAIRED THE PRESSURE DECK MEMBRANE IAW EA 261648.SDR UIEA2016062800534Door Frame · corrodedMAIN DECK OVERWING EXIT AFT FRAME OF CUTOUT DOOR, STA 885.5 JUST ABOVE LOWER DOORSILL FRAME FAILSAFE CHORD IS CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-00-15. FABRICATED REPAIR STRAP OUT OF 7075-TG .063 AND INSTASDR IPXA2016070705510Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 7 HAS CORROSION. REPAIRED THE FLOOR FITTING IAW EA 011-5340-01-A6346 REV. I/R AND EO MD11-5340-61193-A. (MINOR)SDR AALA201607069002Gusset · elongatedELONGATED FASTENER HOLES ON RIGHT HAND INBOARD GUSSET AT FRAME 90 AND Y=-273. REPLACED GUSSET IAW SRM 51-41-02.SDR 29GA2016062400001Seal Rest · damagedFLIGHT 72 , CABIN DOOR DIFFICULT TO CLOSE FROM OUTSIDE & INSIDE THE AIRCRAFT. COMPLIED WITH 340B-5370-2016-001, REPAIR TO LOWER RT MAIN DOOR SEAL SEAT HOLE. R&R RT LOWER SEAT SEAL IAW SRM 53-70-30-208. FIT CHECK GOOD PRESSURE CHECK GOOD.SDR SWAA2016062453210Crease Beam · corrodedRT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 830. REPAIRED WEB IAW SRM.SDR DALA2016062404899Door Frame · crackedCRACKED MLG DOOR JAMB FRAME, STA Y=937 RT WHEEL WELL. JAMB WAS REPLACED IAW SRM 51-30-2 AND 51-30-5, DWG 5930584, REV.SDR DALA2016062404897Strap · crackedCRACKED STRAP REPAIR ON LOWER DOOR JAMB BETWEEN STA Y=1193 TO Y=1212 AT AFT CARGO DOOR JAMB C3. STRAP WAS REPLACED IAW SRM 53-05, FIG 123, SHEET 3, -9.
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