JASC 5310

Service difficulty reports · 38,528

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 FDEA202207201781Beam · crackedFUSELAGE- R/H SIDE OF LH GANTRY 5 AT FR51A CRACK WAS FOUND (LENGTH:25MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 LWR FLANGE AT FR51A PER EO: 6-5310-7-5021 F PT8 & AIRBUS DWG: R53810583 ISSUE: D. THIS IS CATEGORY A REPAIR. MAJOR REPAIJul 20, 2022 · N741FD · Airbus A300*SDR FDEA202207201780Beam · crackedFUSELAGE- R/H SIDE OF LH GANTRY 5 AT FR52A CRACK WAS FOUND (LENGTH:35MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 5 LWR FLANGE AT FR52A PER EO: 6-5310-7-5021 F PT8 & AIRBUS DWG: R53810583 ISSUE: D. THIS IS CATEGORY A REPAIR. MAJOR REPAIJul 20, 2022 · N741FD · Airbus A300*SDR FDEA202207201777Beam · crackedFUSELAGE - L/H SIDE OF LH GANTRY 2 AT FR49.1 CRACK WAS FOUND (LENGTH:30MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 2 LWR FLANGE AT FR49.1 PER EO: 6-5310-7-5021 F PT2 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REJul 20, 2022 · N741FD · Airbus A300*SDR FDEA202207201776Beam · crackedFUSELAGE - L/H SIDE OF LH GANTRY 4 AT FR51A, FR52 & FR52A FOUND 3EA CRACKS. (LENGTH: 30MM, 11MM, 32MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME LH SIDE OF LH GANTRY 4 LWR FLANGE AT FR51A, FR52 & FR52A PER EO: 6-5310-7-5021 F PT6 & AIRBUS DWG: R53810581 ISSUJul 20, 2022 · N741FD · Airbus A300*SDR IPXA2022072084384Frame · dentedINSPECTION TYPE:SEG1AFT CARGO COMPARTMENT, LOWER FRAME UPPER FLANGE AT STA 1500 R/H HAS A DENT BETWEEN STR 25R TO STR 26RWORKED PER RCD 256340. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 114.00 CHAPTER 53-00-07-2R-5 DETAIL III PER SRM 53-60-07-2RJul 20, 2022 · N424UP · Boeing 75724APFSDR IXXA2022072006Angle · corrodedLMLG DOOR FORWARD LOWER ANGLE CORRODEDJul 20, 2022 · N752CX · Boeing 757200SDR IXXA2022072005Panel · corrodedPANEL 117BL CORRODEDJul 20, 2022 · N752CX · Boeing 757200SDR FDEA202207201779Beam · crackedFUSELAGE - R/H SIDE OF RH GANTRY 4 AT FR52A CRACK WAS FOUND (LENGTH:18MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF RH GANTRY 4 LWR FLANGE AT FR52A PER EO: 6-5310-7-5021 F PT7 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REPAJul 20, 2022 · N741FD · Airbus A300*SDR FDEA202207201778Beam · crackedFUSELAGE- R/H SIDE OF LH GANTRY 3 AT FR50.1 CRACK WAS FOUND (LENGTH:96MM) REPAIRED THE CRACKED FUSELAGE MAINFRAME RH SIDE OF LH GANTRY 3 LWR FLANGE AT FR50.1 PER EO: 6-5310-7-5021 F PT4 & AIRBUS DWG: R53810581 ISSUE: C. THIS IS CATEGORY A REPAIR. MAJOR REPJul 20, 2022 · N741FD · Airbus A300*SDR IXXA2022072003Skin Splice · corrodedLWW ANGLE CORRODEDJul 20, 2022 · N752CX · Boeing 757200SDR CALA2022072001841None · corrodedAFT CARGO COMPT: AFT CARGO DOORSILL CUTOUT SURFACE FR55A TO FR59 HAS SEVERAL POINT POINT WITH CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00 IS FOUND OUT LIMIT IAW S NSTALLED NEW SHEET THRESHOLD IAW SRM 51-42-11 AND DRAWING PART L RM 53-41-49-283-003, REMOJul 20, 2022 · N855UA · Airbus A300*SDR IXXA2022072002Skin Splice · corrodedANGLE CORRODED LWWJul 20, 2022 · N752CX · Boeing 757200SDR IXXA2022072010001Pressure Deck · corrodedRIGHT WHEEL WELL PRESSURE DECK CORRODEDJul 20, 2022 · N752CX · Boeing 757200SDR DALA2022120807902Window Frame · crackedSHIP 3229 A CRACK WAS FOUND IN THE UPPER SECTION OF THE RHS FWD FRONT WINDSHIELD FRAME AT THE ATTACHMENT AREA FR4 RHS. CORRECTIVE ACTION: COMPLIED WITH ERA 600111-32. (2327601)Jul 19, 2022 · N329NW · Airbus A320211SDR R61A2022080900492Shear Plate · corrodedR/H SHEAR SPLICE BTWN FR 87 TO 88 FOUND CORRODED. R&R IAW SRM 51-42-02.Jul 19, 2022 · N856RW · Emb ERJ170100SESDR R61A2022080900491Upper Sheet · corrodedL/H (UPPER SHEET) T PNL BTWN FR 85 TO 86 FOUND CORRODED. R&R IAW SRM 51-41-01 AND 51-43-01.Jul 19, 2022 · N856RW · Emb ERJ170100SESDR R61A2022080900490Upper Sheet · corrodedR/H (UPPER SHEET) T PNL BTWN FR 85 TO 86 FOUND CORRODED. R&R IAW SRM 51-41-01 AND 51-43-01.Jul 19, 2022 · N856RW · Emb ERJ170100SESDR R61A2022080900489Floorbeam · corrodedFLOOR BEAM AT LBL 18 BTWN FR 86 TO 89 FOUND CORRODED. R&R IAW SRM 51-41-01, 51-42-01 AND 51-43-01.Jul 19, 2022 · N856RW · Emb ERJ170100SESDR R61A2022080900488Floorbeam · corrodedFLOOR BEAM AT RBL 18 BTWN FR 86 TO 89 FOUND CORRODED. R&R IAW SRM 51-41-01, 51-42-01 AND 51-43-01.Jul 19, 2022 · N857RW · Emb ERJ170100SESDR SWAA2022080830997Web · corrodedAFT CARGO BAY SUBTHRESHOLD WEB HAS CORROSION AT BS807 RBL26 WL156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 807 RBL 26 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATSJul 19, 2022 · N8642E · Boeing 7378H4SDR SWAA2022080830999Web · corrodedFWD CARGO BAY CENTER THRESHOLD WEB HAS CORROSION BS462 RBL28 WL156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 462 RBL 28 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ATJul 19, 2022 · N8642E · Boeing 7378H4SDR IPXA2022080584952Skin Panel · dentedINSPECTION TYPE:CK14DEFERRAL ITEM# 762227. FUSELAGE SKIN DOUBLER HAS DENT AT STA 400-405 BETWEEN S3L AND S4LREPLACED EXISTING DOUBLER IAW UPS EO B757-5330-45385-C AND VT MAE EA 757-5310-27-A2993Jul 19, 2022 · N453UP · Boeing 75724APFSDR R61A2022080400478Beam · corrodedDURING HEAVY CHECK INSPECTION, FOUND FORWARD PASSENGER DOOR CUTOUT BEAM HAS CORROSION ON AND AROUND FASTENERS LOCATED BELOW BOTH EVAC SLIDE FITTINGS. REMOVED AND REPLACED FWD PAX DOOR CUTOUT BEAM PER SRM 51-40-08.Jul 19, 2022 · N237JQ · Emb ERJ170200LRSDR IPXA2022080384867Floor Panel · damagedINSPECTION TYPE:SEGPNL 242EF DAMAGEDFABBED IAW SREO A300-5320-40552-BJul 19, 2022 · N150UP · Airbus A300F4622RSDR SWAA2022082430611Threshold Web · corroded*CORROSION* AFT CARGO DOOR CUTOUT THRESHOLD WEB STA 794.3 TO STA 847 WL 156.4 HAS CORROSION AS MARKED. 124-003 / [01] FOUND EXFOLIATE CORROSION ON AFT CARGO LOWER THRESHOLD WEB BETWEEN STA. 794.3 AND STA 847; OUT OF LIMTS PER REF SRM 53-60-15-1A-1;[02] VERIFIEJul 18, 2022 · N950WN · Boeing 7377H4SDR SWAA2022082230554Fitting · crackedFSD CUTOUT; FWD FRAME; UPPER HINGE BOX FTG CRACKED (MARKED) / [01] CUTOUT CRACK FROM UPPER HINGE BOX FITTING IN THE FWD FRAME OF THE FSD CUTOUT. DAMAGE REMOVAL AREA MEASURES .1' X .4'. DAMAGE REMOVED PER SRM 51-10-02-0G-0.;[02] AFTER DVI; CRACK NOTED ON INBOARJul 18, 2022 · N490WN · Boeing 7377H4SDR SWAA2022081130645Tie Clip · crackedCRACK ANGLE -CLIP LOCATED ON BS 294.5 STR 13L AT FWD GALLEY AREA 2022-381663 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15259471; DUE DATE: 10-DEC-22;[02] REPLACED ANGLE -CLIP LOCATED ON BS 294.5 STR 13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPHJul 18, 2022 · N484WN · Boeing 7377H4SDR IPXA2022080284841Floor Panel · damagedINSPECTION TYPE:SEGPNL 252QQ IS BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884660Floor Panel · damagedINSPECTION TYPE:SEGPNL 252ZWJ BROKENFABBED IAW SREO A300-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884659Floor Panel · damagedINSPECTION TYPE:SEGPN 242YH IS BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884658Floor Panel · damagedINSPECTION TYPE:SEGPN 2526J IS BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884657Floor Panel · damagedINSPECTION TYPE:SEGPN 262BM IS BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884656Floor Panel · damagedINSPECTION TYPE:SEGPNL 262DM BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884655Floor Panel · damagedINSPECTION TYPE:SEGPNL 261GH BROKENFABBED IAW SREO A300-5320-40552-B.Jul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884654Floor Panel · damagedINSPECTION TYPE:SEGPN 251FM IS BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884644Floor Panel · damagedINSPECTION TYPE:SEGPNL 251YM IS BROKENFABBED IAW SREO A300-5320-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR IPXA2022072884643Floor Panel · damagedINSPECTION TYPE:SEGPNL 261GB IS BROKENFABBED IAW SREO A300-40552-BJul 18, 2022 · N150UP · Airbus A300F4622RSDR CALA2022072001815Seat Track · corrodedCORROSION FLOOR STRUCTURE LOCATED FR16 AND Y 1292 IN PASSENGER CABIN REMOVED AND REPLACED SEAT TRACK Y 1292 LOCATED BTW FR 12 TO FR USED: ELECTRONIC CALIPER P/N: 500-196-30 ,S/N:A21033544 ,DUE 24 IN PASSENGER CABIN IAW A320 SRM 51-72-11-911-001, DATE: OCT 09 Jul 18, 2022 · N439UA · Airbus A320232SDR ASAA2022071739247Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL FROM STA. 722J - STA 767 CORRODED OUT OF LIMITS. GROUNDED - YES. REPAIRED AFT PIT L/H TRANSITION PANEL FROM STA 727H+12 TO 794 IAW B737-800 SRM 53-00-53-2R-5.Jul 17, 2022 · N562AS · Boeing 737890SDR IPXA2022072584557Beam · crackedINSPECTION TYPE:SEGMAIN DECK CARGO FLOOR CROSS BEAM AT FR51 BETWEEN -Y450 AND -Y953 IS CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21Jul 17, 2022 · N150UP · Airbus A300F4622RSDR SIMA20220717003Floor Splice · corrodedAFT GALLEY OUTBD RH FLOOR SPLICE AT FR 90 IS CORRODED (MARKED) (LEVEL 2 CORROSION)-C/A-REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE AFT GALLEY OUTBD RH FLOOR SPLICE AT FR 90 IAW ERJ 175 SRM 51-40-08, 51-40-02 AND 51-40-04Jul 17, 2022 · N240NN · Emb ERJ170200LRSDR QXEA2022071800250Floor Panel · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN UNDER SCUFF PLATE FOOTPRINT OF THE AFT SERVICE DOOR. CORROSION UNDER SCUFF PLATE OF THE AFT SERVICE DOOR BLENDED IAW SRM TASK 53-40-31-02-05. NDT CARRIED OUT AT BLENDED AREAS, NO CRACKS FOUND, REFERENCE: SKYSERVICE WO#TWO365Jul 17, 2022 · N432QX · Bombdr BD1001A10SDR QXEA2022071800249Floor Panel · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN UNDER SCUFF PLATE FOOTPRINT OF THE AFT ENTRY DOOR. CORROSION UNDER SCUFF PLATE FOOTPRINT OF THE AFT ENTRY DOOR BLENDED IAW SRM TASK 53-40-31-02-05. NDT CARRIED OUT AT BLENDED AREAS, NO CRACKS FOUND, REFERENCE: SKYSERVICE WO#Jul 17, 2022 · Bombdr BD1001A10SDR CALA2022071801801Door Sill · corrodedAFT WET AREA FR66 DOOR SILL -Y1732 CORRODED. GENERATED AT HAECO LCQ PER NR 9294473 (40473) BY V061629 {A3NB-53-3-686} REMOVED AND REPLACED R-2 DOOR SILL AFT WET AREA PER A320 51-42-1 1/001. PERFORMED BY V061737 INSP BY V919150.Jul 17, 2022 · N496UA · Airbus A320232SDR SWAA2022081029999Web · corrodedFWD CARGO COMPARTMENT THRESHOLD WEB HAS LIGHT SURFACE CORROSION. (MARKED) / [01] WEB WAS FOUND TO BE OUT OF LIMITS AS NOTED IN STEP 1. OBTAINED REPLACEMENT PART. DRILLED AND COUNTERSUNK FASTENER HOLES; AND ATTACHED NUTPLATES PER SRM 51-40-02; TREATED AND PRIMEJul 16, 2022 · N8639B · Boeing 7378H4SDR YENA2022071900676Skin · damagedDURING HEAVY MAINTENANCE AT MCN-EAMS: FUSELAGE/ FWD FUSELAGE/ UPPER SKIN/ RH DONE/ BIRD STRIKE- PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Jul 16, 2022 · N354JB · Emb ERJ190100IGWSDR CALA2022071801785Stringer · corrodedMAIN CABIN R2 DOOR CUTOUT FR 68 FORWARD FACE AND FASTENER HOLE A T STRG 23R HAS CORROSION. GENERATED BY V917055 ON HAECO LCQ NR 9 294582/40582 .098" MAXIMUM ALLOWED = .02". REMOVED = .035" W= .700" L=.500". 50% OF NOMINAL. INSTALLED REPAIR PART IAW SRM 53-41-1Jul 16, 2022 · N496UA · Airbus A320232SDR CALA2022071801791Stringer · crackedFR 35 STR30 RH HOLE #2 HAS OUT OF ROUND CONDITION UNABLE TO INSP FOR CRACKS REQUIRES ROTO SCAN AFTER HOLE BECOMING ROUND AND TRUE A3NB-53-3-6315 PER HAECO LCQ N/R 9294111/40111 GEN BY V892444 ER. STEP REAMED HOLE TO 0.3710IN AND VERIFIED THE HOLE IS ROUND. 15IJul 16, 2022 · N496UA · Airbus A320232SDR IXXA202271610Tie Clip · crackedFS 1678 FRAME TO STRINGER 3R CLIP CRACKED.Jul 16, 2022 · N311AZ · Boeing 767300SDR IXXA202271609Tie Clip · crackedFS 1702 FRAME TO STRINGER 3R CLIP CRACKED.Jul 16, 2022 · N311AZ · Boeing 767300
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