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 SWAA2023081459510Vapor Barrier · crackedLOWER FUSELAGE CENTER WING BULKHEAD L/H VAPOR BARRIER UPPER CHORD ATTACHED ANGLE CRACKED @ LBL 5 STA 663.75 MKD DOT<[01] ACCOMPLISHED CAP SEAL AND FILLET SEAL ARROUND REPAIR EDGES AS PER B737-700 SRM 57-10-10-2R-5.;[02] REPAIRED L/H VAPOR BARRIER UPPER ATTACH Jun 15, 2023 · N444WN · Boeing 7377H4SDR SWAA2023072559811Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023 394560<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189515;DUE DATE:19-DEC-23.;[02] TOOL USED RADIOMETER PHOTOMETER P/N XRP-3000 S/N 1753759 DUE DATE 14-OCT-23.;[03] REPAIRED FWD CORNER SCUFF PJun 15, 2023 · N561WN · Boeing 73773VSDR SWAA2023071159786Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED BETWEEN STA 277-294.5 BL0<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 277-294.5 PER REF SRM 51-40-02-0G-0 AND DWG 141A5410.;[02] VERIFIED STEP # 1Jun 15, 2023 · N291WN · Boeing 7377H4SDR SWAA2023071059475Scuff Plate · crackedCRACK SCUFF PLATE OF FWD SERVICE DOOR AT FWD GALLEY AREA 2023-378942<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30; S/N:A21042057; DUE DATE: 04/APR/24;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N:1753759; CAL DUE DATE: 14-OCT-23;[03] REPAIRED THE SJun 15, 2023 · N298WN · Boeing 7377H4SDR SWAA2023071059476Bracket · brokenBROKEN BRACKET LOCATED ON VAPOR BARRIER BS 663 LH SIDE AT LOWER FUSELAGE 2023-378938<[01] REPLACED BRACKET LOCATED ON VAPOR BARRIER BS 663 LH SIDE AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #111A1000; SHEET 259 REV A.;[02] REPLACED BRACKET LOCAJun 15, 2023 · N298WN · Boeing 7377H4SDR CALA2023061601878Panel · dentedDENT ON LEFT SIDE FUSELAGE 29 INCH AFT OF FWD BULK HEAD 8 INCH BELOW STATIC AREA .047. MOVING TO DIAGRAM FOR DENT TYPE 1, BACK INTO AIRBUS SRM REQUIREMENTS CAPITAL D IS .100 AND LITTLE D IS 19 INCHES.MOVING WITHIN R4 OR R5 AS THAT SHOWS A 45 DEGREE ANGLE FROMJun 15, 2023 · N808UA · Airbus A319131SDR AALA202306209352Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST LOWER ATTACHMENT AT FR 2. REPAIRED WINDSHIELD FRAME PER EA 343625.Jun 15, 2023 · N656AW · Airbus A320232SDR AALA202306201120Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD LEFT HAND FRAME CENTER POST LOWER ATTACHMENT AT FR 2. REPAIRED WINDSHIELD FRAME PER EA 343625.Jun 15, 2023 · N656AW · Airbus A320232SDR SWI2023F00174Unknown · corrodedPAX DOOR DD8 CLIP ON THE AFT SIDE ON FRAME 320.163 IS CORRODED (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DD8 CLIP ON THE AFT SIDE ON FRAME 320.163 IAW CRJ200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR DD8 CLIP ON THE AFT SIDE ON FRAME 320.163 IAW CRJ200 SJun 14, 2023 · N965SW · Cndair CL6002B19SDR SWIA2023008020614Unknown · corrodedPAX DOOR DD8 CLIP ON THE FWD SIDE ON FRAME 320.163 IS CORRODED (C-CHECK RO 7/30/2023) REMOVED PAX DOOR DD8 CLIP ON THE FWD SIDE ON FRAME 320.163 IAW CRJ200 SRM 51-42-06 AND INSTALLED NEW PAX DOOR DD8 CLIP ON THE FWD SIDE ON FRAME 320.163 IAW CRJ200 SRJun 14, 2023 · N965SW · Cndair CL6002B19SDR SWAA2023072559097Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW RBL 40 TO RBL 50 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROXIMATELY: 0.375 INCH. 2023-394451<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 31-JAN-24;[02] TOOLJun 14, 2023 · N561WN · Boeing 73773VSDR SIMA20230614004Seat Track · corrodedSSI 53-21-005 LH UPPER SEAT TRACK CORRODED BTW FR 20-23. (LEVEL 2 CORROSION) -C/A-DETERMINED LEVEL OF CORROSION TO BE LEVEL 2 PER ENVOY GPM 11-04. PERFORMED CUTOUT AS REQUIRED TO REMOVE DAMAGED TEETH FROM LH UPPER SEAT TRACK BETWEEN FR 20-23 IAW EMB 170 SRM 53Jun 14, 2023 · N809MD · Emb ERJ170100SUSDR SWAA2023071159070Support Bracket · crackedAFT OF AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED @ S-27L STA 867 BELOW WASTE CENTER ENCLOSURE POST<[01] REMOVED AND REPLACED AFT OF AFT CARGO COMPARTMENT NEW FLOOR SUPPORT BRACKET S-27L STA 867 BELOW WASTE CENTER ENCLOSURE PER REF SRM 51-40-02-0G-0;[Jun 14, 2023 · N8542Z · Boeing 7378H4SDR SIMA20230614002Skin Panel · corrodedSSI 53-23-003 FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 87-88 AND STGR 28R-27R (LEVEL 2 CORROSION)-C/A-BLENDED OUT CORROSION ON FUSELAGE INTERNAL SKIN BTW FR 87-88 AND STGR 28R-27R IAW EMB 170 SRM 51-10-03. BLENDED AREA ON FUSELAGE INTERNAL SKIN BTW FR 87-Jun 14, 2023 · N809MD · Emb ERJ170100SUSDR SIMA20230614001Stringer · corroded53-23-003 STR 27R CORRODED BETWEEN FR 87-88 (LEVEL 2 CORROSION)-C/A-BLENDED OUT CORROSION ON STGR 27R BTW FR87-88 IAW EMB 170 SRM 51-10-03. BLENDED AREA ON STGR 27R BTW FR87-8 FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 170 SRM 51-75-16Jun 14, 2023 · N809MD · Emb ERJ170100SUSDR JR2R20230614615Gusset · corrodedGUSSET ON TOP OF FR90 AND RBL11 CORRODEDJun 14, 2023 · N86350 · Emb ERJ170200LRSDR JR2R20230614616Unknown · corrodedRH FLOOR SILL BETWEEN FR88 THRU FR90 CORRODEDJun 14, 2023 · N86350 · Emb ERJ170200LRSDR JR2R20230614614Gusset · corrodedGUSSET ON TOP OF FR89 AND RBL11 CORRODEDJun 14, 2023 · N86350 · Emb ERJ170200LRSDR JR2R20230614611Support · corrodedFLOOR PANEL MOUNT FITTING ON THE FWD SIDE OF FR87 AT ABOUT RBL28 CORRODEDJun 14, 2023 · N86350 · Emb ERJ170200LRSDR JR2R20230614628Doubler · corrodedFLOOR WEB BETWEEN FR12 THRU FR14 AND RBL36 THRU RBL48 CORRODEDJun 14, 2023 · N86350 · Emb ERJ170200LRSDR JR2R20230614610Support · brokenFLOOR PANEL MOUNTING ANGLE ON THE BACK SIDE OF FR86 AT ABOUT RBL28 BROKEN OFFJun 14, 2023 · N86350 · Emb ERJ170200LRSDR SWAA2023071158769Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED RADIUS OF FWD CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; CALIBRATION DUE DAJun 13, 2023 · N963WN · Boeing 7377H4SDR SWAA2023062957860Stiffener · crackedLOWER FUSELAGE CENTER WING STIFFENER CRACKED AT R/H VAPOR BARRIER O/B A/C AIR EXIT EXHAUST DUCT RBL 25 STA 663.75<[01] REMOVED DAMAGE STIFFENER AND INSTALLED NEW STIFFENER ON R/H VAPOR BARRIER STA. 663.75 RBL 25; PER REF. SRM 51-40-02-0G-0 AND DRAWING # 111A10Jun 11, 2023 · N942WN · Boeing 7377H4SDR FDEA202306111108Stringer · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR 36~37, STGR 33L COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, Jun 11, 2023 · N728FD · Airbus A300*SDR CALA2023061201825Door Frame · crackedB767-06-3-7011 FWD CARGO : FWD CARGO DOOR AT STA 542 FRAME LOWER PORTION FOUND CRACKED TRANSFER REF HXWO 1851416 AND ORIGINATED BY EMP V898555 FWD CARGO DOOR STA542.4 FRAME INNER CHORD REPAIRED AS PER ECRA5234-01095 REV - ATTACH FORM 44.0008 ITEM 1 TO ITEM 19 Jun 11, 2023 · N649UA · Boeing 767322SDR SWAA2023070757935Stringer · crackedCRACK ON STR28R LOCATED BTW BS312 TO BS328 AT EQUIPMENT ELECTRONIC COMP 2023-365685<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221860711; DUE DATE: 07 NOV 23.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE:Jun 10, 2023 · N7827A · Boeing 73779PSDR SIMA20230610002Bearing · corrodedSSI 53-23-014 AFT PASSENGER DOOR CUT-OUT AFT EVACUATION SLIDE FITTING HOUSING CORRODED AREA (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-RAR AFT PAX DOOR CUTOUT LOWER SILL IAW EMB-170 SRM 51-40-08Jun 10, 2023 · N809MD · Emb ERJ170100SUSDR UIEA2023060700604Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)Jun 10, 2023 · N1181A · Boeing 7673Y0SDR UIEA2023060600593Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 174.5 AND 5 INCH ABOVE OF STRINGER S-27LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED.</P>)Jun 10, 2023 · N1181A · Boeing 7673Y0SDR UIEA2023060600589Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 325 AND STRINGERS S-28LH / S-29LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)Jun 10, 2023 · N1181A · Boeing 7673Y0SDR UIEA2023060600588Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 412 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)Jun 10, 2023 · N1181A · Boeing 7673Y0SDR UIEA2023060600587Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 390 AND STRINGERS S-27LH / S-28LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)Jun 10, 2023 · N1181A · Boeing 7673Y0SDR UIEA2023060600586Unknown · unknownLIGHTNING STRIKE DAMAGE ON EXTERNAL FUSELAGE SKIN BETWEEN STA 196.5 AND 8.5 INCH LOWER OF STRINGER S-21LH(<P>AFFECTED AREA WAS OVERSIZED AND REPAIRED PER SRM 53-00-01-2R-8. NO FURTHER DEFECTS NOTED</P>)Jun 10, 2023 · N1181A · Boeing 7673Y0SDR FDEA202306091179Splice · corrodedAVIONICS COMP'T BILGE STRUCTURE OF SPLICE GOT CORRODED AT FR19,STGR-52L POSITION REPLACED THE CORRODED SPLICE WITH NEW PART I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~23Jun 9, 2023 · N728FD · Airbus A300*SDR ASAA2023060943753Web · corrodedBS 987 L/H PRESSURE WEB CORRODED. GROUNDED - YES. REMOVED CORROSION.ORIGINAL WEB THICKNESS AT CORROSION AREA 0.020 IAW BAC DWG 147A5712 REV B REMAINING THICKNESS 0.004,REMOVED 0.016.OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1REMOVED WEB IAW B737-800 SRM 51-40Jun 9, 2023 · N585AS · Boeing 737890SDR CALA2023061201815Unknown · gougedABOVE R4 DOOR, ON FRAME 1640, THERE IS A GOUGE IN THE FRAME. (SEE IMAGES) INTERIM REPAIR ACCOMPLISHED AT FUSELAGE STA 1640 FRAME AND S5R-S6R - ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF EC/RA 5360-01713 ON OR BEFORE 22-NOV-Jun 9, 2023 · N14115 · Boeing 757224SDR IPXA2023062393501Adapter · brokenINSPECTION TYPE:1CMAIN DECK CARGO FLOOR SEAT ADAPTER AT FR 34 L/H BETWEEN Y1959 AND Y2462 BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.Jun 8, 2023 · N126UP · Airbus A300F4622RSDR KCSA202306081067Skin · damagedR/H UPPER FUSELAGE BETWEEN STR 11R AND 13R B.S. 2638.0 - 2658.0 SKIN DAMAGEJun 8, 2023 · N716CK · Boeing 7474B5FSDR SCNA20230613184Angle · corrodedDEFECT NR00188: CORROSION FORWARD CARGO BAY , RH ZEE AT STA 500A TO 500I AROUND MULTIPLE NUTPLATES. - - - RESOLUTION: REMOVED FABRICATED AND INSTALLED NEW ZEE CHANNEL REPLACEMENT AT RH STA 500-500I, IAW B737-SRM-51--40-02, DWG 143A7501 DWG 143A7500.Jun 7, 2023 · N7901A · Boeing 7378SDR SCNA202306132183Channel · corrodedSUPPLEMENTAL: DEFECT NR00191: CORROSION AFT CARGO BAY LH ZEE UPPER SURFACE, VARIOUS AREAS AT STA 727 TO 727G+10. - - - RESOLUTION: REMOVED AND REPLACED AFT CARGO ZEE CHANNEL STA 727 TO 727G WITH NEW ITEM #BAC1496-337 #7075T62 LOT#5130352-1 IAW B737 SRM 53-00-5Jun 7, 2023 · N7901A · Boeing 7378SDR AALA202309192617Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK FRONT WINDSHIELD RIGHT HAND FRAME LOWER RADIUS AT FR 3 AND Y0 RIGHT. REPAIRED FRAME PER EA 345858.Jun 6, 2023 · N712US · Airbus A319112SDR REXA2022072000516Door Frame · corrodedPAX DOOR FRAME AT FS 327.763 BETWEEN DD6 AND HINGE FOUND TO BE CORRODED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FRAME AT FA327.763 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01 PN: 601R318062-3Jun 6, 2023 · N181PQ · Cndair CL6002D24SDR SWAA2023071056769Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS727A TO BS727D LBL 21 WL 155.5 AT AFT CARGO COMPARTMENT 2023-365567<[01] ULTRASONIC EQUIPMENT USED: P/N:45MG; S/N:130064101; DUE DATE: 12-OCT-23;[02] REPLACED SUPPORT ZEE AND FASTENERS LOC.BS 727 TO BS 847 AND FASTENERS LBL Jun 6, 2023 · N7827A · Boeing 73779PSDR SWAA2023071056768Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS727D TO BS727E RBL 23 WL 155.5 AT AFT CARGO COMPARTMENT 2023-365566<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 221859911 DUE DATE: 07-NOV-23;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL 23 WL 155.5 Jun 6, 2023 · N7827A · Boeing 73779PSDR VNAA202306230009Crossbeam · corrodedCORROSION ON CROSSBEAM AT FS 280.00 BTW RBL 9.00 AND LBL 9.00. CROSSBEAM AT FS 280.00 BTW RBL 9.00 AND LBL 9.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01Jun 6, 2023 · N551NN · Cndair CL6002D24SDR JR2R20230606413Beam · corrodedRH AFT LONG BEAM CORRODEDJun 6, 2023 · N88327 · Emb ERJ170200LRSDR JR2R20230606407Crossbeam · corrodedCROSSBEM 17 CORRODED OUT OF LIMITS AT APPROX. LBL7Jun 6, 2023 · N88327 · Emb ERJ170200LRSDR SWI2023F00169Unknown · corrodedDURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON FORMER @ FS 329.76 BETWEEN DD5 AND DD6. (C-CHECK RO 7/30/2023) REMOVED DAMAGE FORMER ON PAX DOOR AT FS 329.76 BETWEEN DD5 AND DD6 REF CRJ 200 SRM 51-42-06 AND INSTALLED NEW FORMER ON PAX DJun 5, 2023 · N965SW · Cndair CL6002B19SDR SWI2023F00164Unknown · corrodedDURING REMOVAL OF THE PAX DOOR INNER SKIN CORROSION WAS FOUND ON FWD FORMER @ FS320.163. (C-CHECK RO 7/30/2023) REMOVED FWD FORMER AT FS 320.163 REF CRJ 200 SRM 51-42-06,51-42-21 AND 51-42-13 AND INSTALLED FWD FORMER AT FS 320.163 REF CRJ 200 SRM 51-Jun 5, 2023 · N965SW · Cndair CL6002B19SDR SWAA2023071056369Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS727D AFT CARGO COMPARTMENT 2023-365524<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; CAL DUE DATE: 30/AUG/23;[02] REPAIRED CARGO TRACK SECTION LOCATED FROM BS727B TO BS767 RBL 13.84 AT AFT CARGO COMPARTJun 5, 2023 · N7827A · Boeing 73779P
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