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 FDEA202503090345Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR55 AND FR57.2 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR55 AND FR57.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 Mar 9, 2025 · N673FE · Airbus A300F4605RSDR CALA2025031002667Web · crackedFLIGHT DECK FLOOR WEB HAS CRACK FR 11 RBL 30. REMOVED & REPLACED CRACKED WEB AT FLIGHT DECK FR11 RBL 30 IAW A3 20 SRM 51-72-11-911-001.Mar 9, 2025 · N459UA · Airbus A320232SDR QXEA2025031900064Frame · damagedMISDRILLED HOLE THROUGH CROSS FRAME 19 ON LH SIDE AFT OF FWD PAX DOOR AT LH WINDSCREEN SUPPORT. PLUGGED HOLE WITH FASTENER AT CROSS FRAME 19 ON LH SIDE OF FWD PAX DOOR AT LH WINDSCREEN SUPPORT. REF EDT2025-170-903388.Mar 8, 2025 · N627QX · Emb ERJ170200LRSDR R61A2025030800131Beam · crackedDURING HEAVY CHECK FOUND NLG WHEEL WELL UPPER BULKHEAD I BEAM HAS CRACK. REPLACED BEAM IAW ETD2025-170-902367Mar 8, 2025 · N752 · Emb ERJ170100LRSDR NACA2025030700002Retainer · corrodedRH OVERWING EMER EXIT HATCH GOT CORROSION AROUND SEAL RETAINER AREA. 1.REMOVE THE DOOR SEAL RETAINER TO GET ACCESS FORM CORROSION DAMAGED AREA 2.CORROSION REMOVE & CONDITION CHECK NORMAL 3. THE BLEND-OUT DEEP IS 0.002" INCH WITHIN ALLOWABLE LIMIT 4.DOOE SEAL RMar 7, 2025 · N304KH · Boeing 7373Q8SDR DALA2025031101871Window Frame · cracked(LOG 0845967) DURING INSPECTION, DAMAGE WAS FOUND TO THE LOWER FWD CORNER OF THE LH NO. 3 FLIGHT COMPARTMENT WINDOW. THE DAMAGE CONSISTS OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (E-F POST) THROUGH A FASTENER LOCATION AND CONTINUES THROUGH Mar 7, 2025 · N3750D · Boeing 737832SDR DALA2025031101867Window Frame · cracked(LOG 0846017) FOUND L/H #3 WINDOW FRAME CRACKED THROUGH FASTENER HOLE 2ND FROM BOTTOM. ACCOMPLISHED PER ER/A 624108-14AD REV 0 ON L/H #3 WINDOW FRAME.Mar 7, 2025 · N3750D · Boeing 737832SDR SWIA202503100007Structure · damagedGEAR DISAGREE WARNING MESSAGE ON THE GO AROUND AFTER WE SELECTED FLAPS 8 AND POSITIVE RATE. AIRSPEED WAS LESS THAN 200 KNOTS. RAN THE QRH AND HAD TO PULL THE LANDING GEAR MANUAL HANDLE AND THE MESSAGE WENT AWAY AND THE GEAR WAS LOCKED AND GREEN. (FLIGHT 53Mar 7, 2025 · N969SW · Cndair CL6002B19SDR SWAA2025031003169Panel · crackedR1 DOOR FWD SURROUND PANEL IS CRACKED AT OUTLET CUTOUT<[01] REPAIRED CRACK AT OUTLET CUTOUT ON R1 DOOR FWD SURROUND PANEL IAW CMM 25-00-66 PAGES 602-603 REPAIR 1-1 SECTION 3 AND PAGE 603 REPAIR 2-1 SECTION 4.;[02] VERIFIED CORRECTIVE ACTION STEP 1.Mar 7, 2025 · N8901Q · Boeing 7378SDR CALA2025031002661Crossbeam · crackedFRAME 16 RH CROSSBEAM HOLE #H6 HAS CRACK INDICATION IN BOTH LAYE RS AT 12 OCLOCK 100% S.H. AD 2024-04-04. REAMED HOLE #6 AT FRAME 16 RH AT .2500 (6.35MM) NO DEFECTS NOTED . COLDWORKED AS REQ'D FINAL REAMED AT .2780(7.061MM) INSTALLED N EW FASTENER. ALL WORKMar 7, 2025 · N434UA · Airbus A320232SDR VNAA202503070012Joint · corrodedCORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 25LH TO STGR 25 RH. CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 25LH TO STGR 25 RH WAS REPAIRED PER REO 690-53-21-1885 REV.--. THE AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROMar 7, 2025 · N594NN · Cndair CL6002D24SDR VNAA202503070007Beam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR LONGITUDINAL BEAM ON COCKPIT (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1935 REV.--Mar 7, 2025 · N594NN · Cndair CL6002D24SDR EE4Y2025030721914Crossbeam · corrodedDURING THE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE CROSS BEAM FR84 WITH CORROSION (4 LOCATIONS) BETWEEN Y-330/-Y860, THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900179-A AND THE COOPESA ENGINEERING ORDMar 7, 2025 · N228JB · Emb ERJ190100IGWSDR NACA2025071700001Longeron Splice · damagedLH FUSELAGE, LONGERON SPLICE PLATE, REMOVED FROM STA 933 TO 977 AND BELOW STR 22L HAS SEVERAL NICKS AND GOUGES IDENTIFIED WITH ORANGE STICKER 118-001. 1)ACCOMPLISHED EA 767-5700-73-B0451, IR (REV) AT L/H FUSELAGE LONGERON SPLICE PLATE BTWN. STA 916 TO STA 977 Mar 6, 2025 · N379CX · Boeing 767323SDR SWI2025F00763Fitting · crackedCO-PILOT SIDE WINDOW POST LOWER FITTING P/N: 601R33235-2 CRACKED. #29747104 (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED 1EA NEW R/H LWR SIDE POST FITTING (P/N 601R33235-2) PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARD 51-90Mar 6, 2025 · N919EV · Cndair CL6002B19SDR SWIA2025062400306Window Frame · crackedCO-PILOT SIDE WINDOW POST LOWER FITTING P/N: 601R33235-4 CRACKED. #29747105 (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED 1EA NEW R/H COCKPIT SIDE POST LWR FITTING (P/N 601R33235-4) PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CAMar 6, 2025 · N919EV · Cndair CL6002B19SDR AALA202506137275Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 3 FR16RH DOOR STOP 7 . CRACK DIRECTION 9 OCLOCK. CRACK DEPTH 0.100 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING #7 LOC BTW FR15 TO FR16 RH SIDE AND FASTENER I.A.W EA#362898, REPAIR DRAWING R53Mar 6, 2025 · N775XF · Airbus A319112SDR SWI2025F00492Cleat · crackedCENTER POST RH LOWER CLEAT CRACKED AS MARKED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED CENTER POST RH LOWER CLEAT WITH A NEW SERVICEABLE UNIT REF CRJ 200 SRM 51-42-21 AND DWG 601R33007 REV U. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.Mar 6, 2025 · N693BR · Cndair CL6002B19SDR SWIA20250418306Window Frame · crackedPILOT WINDSHIELD SIDE POST LOWER AFT ATTACH FITTING IS CRACKED (MARKED) (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED 1EA NEW L/H WINDSHIELD SIDE POST SUPPORT ANGLE P/N 601R33235-3 PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARMar 6, 2025 · N693BR · Cndair CL6002B19SDR AALA202504072739Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 1 FR16 LH DOOR STOP 7 CRACK DIRECTION 5 O' CLOCK. CRACK DEPTH 0.100 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING AT FR16 L/H DOOR STOP 7 I.A.W A319 SRM 51-42-11-801 AND A319 SRM 51-72-11-911Mar 6, 2025 · N775XF · Airbus A319112SDR AALA202504010553Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 1 FR16 LH DOOR STOP 7 CRACK DIRECTION 5 O CLOCK. CRACK DEPTH 0.100 INCH. MAINTENANCEREPLACED INTERCOSTAL FITTING LOC.ON FR16 L/H DOOR STOP 7 I.A.W A319 SRM 51-42-11-801 AND A319 SRM 51-72-11-91Mar 6, 2025 · N775XF · Airbus A319112SDR SWI2025F00414Stop Fitting · gougedCARGO DOOR SURROUND LOWER AFT STOP FITTING IS GOUGED (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW AFT LOWER STOP FITTING P/N:601R35203-5 & SHIM LAMINATED P/N: 601R35207-9. REF DWG 601R35207 REV -W AND REF CRJ 200 SRM 51-41-02. COMPLIED WITH SKYWEST TASK CAMar 6, 2025 · N962SW · Cndair CL6002B19SDR SWIA2025033106Stop Fitting · gougedCARGO DOOR SURROUND LOWER FWD STOP FITTING IS GOUGED (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW CARGO DOOR SURROUND FWD LOWER STOP FITTING P/N:601R35203-5 & SHIM LAMINATED P/N: 601R35207-9 IAW CRJ 200 SRM 51-41-02 AND DWG 601R35203 REV -A. TORQUE WRENCH Mar 6, 2025 · N962SW · Cndair CL6002B19SDR CALA2025031002654Door Frame · crackedCRACK ON DOOR FRAME FWD SIDE OF DOOR 119BL-DOT 46-04 ESFR ENTRY REPAIRED ACCESS DOOR 119BL IAW UAL EC/RA#:5330-07477 AND VT MAE EA 757-5330-13-A3801 REV-MAJOR REPAIR ALL INSPECTIONS ACCOMPLISHED AT STENGINEERING IN PNS AS PER UAL EC/RA#:5330-07477 AND VT MAE EMar 6, 2025 · N21108 · Boeing 757224SDR CALA2025030702612Door Frame · crackedRH AFT EMERGENCY DOOR AFT CENTER FRAME HAS CRACK. REMOVED AND REPLACED FRAME AT AFT CENTER OF RH AFT EMERGENCY EXI T DOOR IAW A320 SRM 51-42-11, SRM 51-72-11.Mar 6, 2025 · N459UA · Airbus A320232SDR CALA2025030702611Door Frame · crackedRH FWD EMERGENCY EXIT AFT FRAME CRACKED. REMOVED AND REPLACED FRAME AT RH FWD EMERGENCY EXIT DOOR AFT SEC TION IAW A320 SRM 51-42-11, SRM 51-72-11.Mar 6, 2025 · N459UA · Airbus A320232SDR CALA2025030702610Door Frame · crackedRH AFT EMERGENCY DOOR FWD CENTER FRAME HAS CRACK. REMOVED AND REPLACED FRAME AT FWD CENTER OFRH AFT EMERGENCY ENT DOOR IAW A320 SRM 51-42-11, SRM 51-72-11.Mar 6, 2025 · N459UA · Airbus A320232SDR NACA20250717011Pressure Deck · corrodedAFTER REMO VAL OF GUSSET FROM L/H WW PRESS.DECK AREA STA 955 LBL 85 (APPROX) FOUND CORROSION ON MATING SURFACE OF GUSSET. REMOVED CORROSION ON GUSSET FROM L/H WW PRESS. DECK AREA STA 955 LBL 85, DIMENSIONS L=3.050" W=2.500 IAW SRM 51-10-02 STEP 15A3. EVALUATMar 5, 2025 · N379CX · Boeing 767323SDR IXXA20250423002Retainer · gougedFLIGHT DECK L2 SLIDING WINDOW CUTOUT FWD LOWER SEAL RETAINER DAMAGEMar 5, 2025 · N229AZ · Boeing 767323SDR VNAA202504130009Plate · corrodedCORROSION WAS FOUND ON KICKPLATE OF SURROUND STRUCTURE AT PASSENGER DOOR (L1). CORROSION ON KICKPLATE OF SURROUND STRUCTURE AT PASSENGER DOOR (L1) WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-001-Mar 5, 2025 · N597NN · Cndair CL6002D24SDR IPXA2025040777848Crossbeam · crackedMCD FLOOR STRUCTURE CROSSBEAM C74 -Y2127 SUPPORT ANGLE HAS A CRACK. DOT 68-05. INSTALL PANELS: 262PF, 262VF, 262JM, 252TU,262DX, 262GX. VERIFIED ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-93165-REQ1 AND VT-MAE EA 300-5318-27-A3864, REV. -.Mar 5, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025040484412Adapter · corrodedMDC FR57 UNDER FLOOR PANEL 251LG ADAPTER CLS HAS CORROSION.- DOT 11-008. INSTALLED ADAPTER IAW A300-600 SRM 51-40-21 WITH FASTENERS P/N: DAN8-6-14 BATCH:0004085613 AND COLLAR P/N: BACC30U4 BATCH:0001224358. REVIEWEDMar 5, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025040484376Adapter · corrodedMDC FR57.1 UNDER FLOOR PANEL 251LG ADAPTER CLS HAS CORROSION.- DOT 11-007. OK TO INSTALL CLS ADAPTER GIVEN. COMPLIED WITH STEP 10 OF PELIMINARY 2 E.A.# 300-5316-27-A3846. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93187-REQ1 AND VT-MAE EA 300-5316-27-AMar 5, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025040478227Adapter · corrodedMCD FLOOR STRUCTURE CROSSBEAM C60 AT Y0 CLS ADAPTER HAS EXFOLIATION. DOT 68-07. OK TO INSTALL CLS ADAPTER GIVEN. COMPLIED WITH STEP 10 OF PELIMINARY 2 E.A.# 300-5317-27-A3844. REVIEWEDMar 5, 2025 · N121UP · Airbus A300F4622RSDR IPXA2025040178227Adapter · corroded**SDR FILED OPEN** MCD FLOOR STRUCTURE CROSSBEAM C60 AT Y0 CLS ADAPTER HAS EXFOLIATION. DOT 68-07 ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93185-REQ1 AND VT-MAE EA 300-5317-27-A3844, REV. -.CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED Mar 5, 2025 · N121UP · Airbus A300F4622RSDR NACA2025030500004Door Frame · damagedA BROKEN HOLE (1"X0.75" IN AREA) FOUND ON FWD CARGO DOOR SURROUND STRUCTURE PLATE AT BS439 BETWEEN S-24R AND S-25R AS MARKED. 1. REMOVED FASTENER COMMON TO REPAIR AREA 2. TRIM OUT DAMAGED AREA 3. MORE REPAIR PARTS TO INSTALL WITH SEALANT PER B737-300 SRM 51-70Mar 5, 2025 · N304KH · Boeing 7373Q8SDR NACA2025030500003Plate · damagedA BROKEN HOLE (1"X0.75" IN AREA) FOUND ON FWD CARGO DOOR SURROUND STRUCTURE PLATE AT BS439 BETWEEN S-24R AND S-25R AS MARKED. 1. REMOVED FASTENER COMMON TO REPAIR AREA 2. TRIM OUT DAMAGED AREA 3. MORE REPAIR PARTS TO INSTALL WITH SEALANT PER B737-300 SRM 51-7Mar 5, 2025 · N304KH · Boeing 7373Q8SDR IPXA2025032683675Adapter · brokenMCD FLOOR STRUCTURE AT FR32/Y1952 HAS ADAPTER CLS BROKEN (REF. PNL 241EF). DOT 34-010. INSTALLED NEW ADAPTOR CLS IAW SRM A300/600 TASK: 51-40-21.Mar 5, 2025 · N121UP · Airbus A300F4622RSDR DALA2025031001839Window Frame · cracked(LOG 0842152) DURING INSPECTION DAMAGE WAS FOUND TO THE UPPER RIGHT CORNER OF THE RH NO. 1 FLIGHT DECK WINDOW. THE DAMAGE CONSISTS OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-6) OF THE RH NO. 1 Mar 5, 2025 · N3750D · Boeing 737832SDR DALA2025031001838Window Frame · cracked(LOG 0842124) DURING INSPECTIONS, DAMAGE WAS FOUND TO THE UPPER RIGHT CORNER OF THE LH NO. 1 FLIGHT DECK WINDOW. THE DAMAGE CONSISTS OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-5) OF THE LH NO. Mar 5, 2025 · N3750D · Boeing 737832SDR DALA2025031001836Doubler · corroded(LOG 0843102) CORROSION ON DOUBLER AT FCB, BS500C+12 BL0 WL149. REMOVED, FABRICATED A NEW DOUBLER (NUTPLATE RETAINER ASSY) OUT OF 2024-T3 CLAD 0.050" LOT #1320308-1 PER GO GO DWG: NO: P20196 REV.C. INSTALLED NEW DOUBLER (NUTPLATE RETAINER ASSY) PER GOGO DWG. NMar 5, 2025 · N859DN · Boeing 737932ERSDR DALA2025031001831Window Frame · cracked(LOG 0842341) WHILE ACCOMPLISHING STEP 2 OF CUSTOMER CARD 5311-2003 A CRACK WAS NOTED ON THE INTERNAL SURFACE OF THE #1 L/H WINDOW FRAME INNER CORNER RADIUS. C/W ER/A 624122-14AD.Mar 5, 2025 · N3750D · Boeing 737832SDR DALA2025031001830Window Frame · cracked(LOG 0842328) FOUND CRACK IN R/H C-D POST, #1 WINDOW FRAME IN UPPER CORNER. C/W ER/A 624033-14AD.Mar 5, 2025 · N3750D · Boeing 737832SDR AALA202503063653Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED AR FR 1 AND Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.Mar 5, 2025 · N173US · Airbus A321211SDR IPXA2025031846582Door Frame · corrodedFWR CARGO DOOR INTERNAL LWR FWD FRAME HAS CORROSION NOTED. DOT 06677-01. VERIFIED INSTALLATION OF ANGLE AT FWR CARGO DOOR INTERNAL LWR FWD FRAME IAW B757-200 SRM 51-40-02-0G MATERIAL USED: P/N BACR15GF6D BTCH: 0004023215 P/N04-001-0109 BTCH:0004355128. REVMar 4, 2025 · N442UP · Boeing 75724APFSDR SIMA20250304001Door Frame · corrodedSSI 53-23-018 AFT GALLEY DRAIN MAST CUTOUT INTERIOR SUPPORT FWD FRAME IS CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT GALLEY DRAIN MAST CUTOUT INTERIOR SUPPORT FWD FRAME IAW EMB 170 SRM 51-40-08.Mar 4, 2025 · N742GR · Emb ERJ170100SUSDR CALA2025031002649Crossbeam · damagedWHILE SURVEYING THE UPPER TWO ROWS AT L/H FR20 CROSSBEAM FRAME S PLICING IT WAS FOUND THAT THERE WERE NON-ORIGINAL TYPE FASTENERS INSTALLED. REPAIRED LH FR20 CROSSBEAM FRAME SPLICING UPPER TWO ROWS FASTENE RS IAW UAL EA 5310-06784-001.Mar 4, 2025 · N434UA · Airbus A320232SDR FDEA202503040322Crossbeam · misrepairedEXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FRAME 20A BETWEEN STGR33RH AND STGR45RH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FRAME 20A BETWEEN STGR33RH AND STGR45RH WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6Mar 4, 2025 · N673FE · Airbus A300F4605RSDR FDEA202503040314Panel · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "F" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA 6-5710-T0382800 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE F AT FR47 RHS DURING SB57-6068 EMBMar 4, 2025 · N673FE · Airbus A300F4605RSDR DALA2025030401661Beam · damagedSHIP 3354 AD/EM-EO TASK - QTY: 2EA FASTENER HOLES E/M LESS THAN 2D (D= DIAMETER) AT HOLE MARKING H-5 & H-6 OF AFT CARGO DOOR FR63 BEAM 4. CORRECTIVE ACTION: COMPLIED WITH ERA 624465-14AD. (0840003)Mar 4, 2025 · N854NW · Airbus A330223
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