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 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 51-40-02Jul 8, 2016 · N413UP · Boeing 75724APFSDR 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.Jul 7, 2016 · N539UW · Airbus A321231SDR 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.Jul 7, 2016 · N292UP · Doug MD11FSDR 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.Jul 7, 2016 · N292UP · Doug MD11FSDR 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.Jul 7, 2016 · N487WN · Boeing 7377H4SDR 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.Jul 7, 2016 · N184US · Airbus A321211SDR AALA201607129003Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE CRACKED AT FR 43, +Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.Jul 7, 2016 · N184US · Airbus A321211SDR 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.Jul 6, 2016 · N959UW · Emb ERJ190100IGWSDR WVER070620160003Seal Rest · chafedPERFORMED REPAIR OF DAMAGED PASSENGER DOOR SEAL-STRIKER IAW REO 670-53-22-001-TYPE 1 REV H.Jul 6, 2016 · N927LR · Cndair CL6002D24SDR 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.Jul 5, 2016 · N959UW · Emb ERJ190100IGWSDR IPXA2016070705516Angle · crackedINSPECTION TYPE: 3C, RIGHT SIDE AVIONICS COMPARTMENT FRAME 10 CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21.Jul 5, 2016 · N144UP · Airbus A300F4622RSDR 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".Jul 5, 2016 · N958AT · Boeing 717200SDR 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-Jul 4, 2016 · N907XJ · Cndair CL6002D24SDR FOTR20160704002Door Frame · corrodedCARGO DOOR JAMB CUT OUT HAS CORROISION AT STA. 1400-1440 STRINGER 27RJul 4, 2016 · N273DH · Boeing 7572Q8SDR 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.Jul 3, 2016 · N958AT · Boeing 717200SDR 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.Jul 3, 2016 · N958AT · Boeing 717200SDR 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.Jul 3, 2016 · N958AT · Boeing 717200SDR 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.Jul 3, 2016 · N958AT · Boeing 717200SDR 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".Jul 3, 2016 · N958AT · Boeing 717200SDR 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.Jul 3, 2016 · N958AT · Boeing 717200SDR 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.Jul 1, 2016 · N8694A · Cndair CL6002B19SDR 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)Jul 1, 2016 · N285UP · Doug MD11FSDR 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.Jul 1, 2016 · N14106 · Boeing 757224SDR 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.Jun 30, 2016 · N255CM · Boeing 767223SDR AALA201607069005Box Beam · crackedRIGHT SIDE BOX BEAM UPPER FLANGECRACKED AT FRAME 43 AND -Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.Jun 30, 2016 · N185UW · Airbus A321211SDR AALA201607069004Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE CRACKED AT FRAME 43 AND +Y1622. REPAIRED BOX BEAM IAW EO 5315Y066.Jun 30, 2016 · N185UW · Airbus A321211SDR 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.Jun 30, 2016 · N11526 · Emb EMB135LRSDR CALA2016070195493Door Frame · crackedR4 ENTRY DOOR FRAME CRACKED AT AFT UPPER CORNER. STOP DRILLED. HFEC. MFG & INSTALL REPAIR IAW SRM 52-10-02.Jun 29, 2016 · N174UA · Boeing 747422SDR 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.Jun 28, 2016 · N995DL · Doug MD88SDR 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.Jun 28, 2016 · N995DL · Doug MD88SDR 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.Jun 28, 2016 · N995DL · Doug MD88SDR 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, RJun 28, 2016 · N995DL · Doug MD88SDR 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.Jun 28, 2016 · N995DL · Doug MD88SDR 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.Jun 27, 2016 · N710UW · Airbus A319112SDR 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..Jun 27, 2016 · N710UW · Airbus A319112SDR 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.Jun 27, 2016 · N900DE · Doug MD88SDR 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.Jun 27, 2016 · N995DL · Doug MD88SDR 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.Jun 27, 2016 · N995DL · Doug MD88SDR 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.Jun 27, 2016 · N995DL · Doug MD88SDR 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.Jun 26, 2016 · N344NW · Airbus A320212SDR SWIA201642381Angle · corrodedBS 1098.20 LOWER CAP ANGLE BETWEEN STRINGER 23 - 24L HAS CORROSION. REPAIRED IAW EA.Jun 26, 2016 · N609SK · Cndair CL6002C10SDR WVER2016062650513Door Frame · crackedCREW ESCAPE HATCH AFT SURROUND STRUCTURE IS CRACKED IN THE RADIUS APPROXIMATELY .250" LONG NEXT TO THE RT HINGE FITTING.Jun 26, 2016 · N505MJ · Cndair CL6002C10SDR 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.Jun 25, 2016 · N710UW · Airbus A319112SDR 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 INSTAJun 25, 2016 · N658GT · Boeing 767281SDR 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)Jun 24, 2016 · N285UP · Doug MD11FSDR AALA201607069002Gusset · elongatedELONGATED FASTENER HOLES ON RIGHT HAND INBOARD GUSSET AT FRAME 90 AND Y=-273. REPLACED GUSSET IAW SRM 51-41-02.Jun 24, 2016 · N959UW · Emb ERJ190100IGWSDR 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.Jun 23, 2016 · N348AG · Saab 340BSDR SWAA2016062453210Crease Beam · corrodedRT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 830. REPAIRED WEB IAW SRM.Jun 23, 2016 · N253WN · Boeing 7377H4SDR 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.Jun 23, 2016 · N900DE · Doug MD88SDR 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.Jun 22, 2016 · N998DL · Doug MD88
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