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 SWIA2024111200831Beam · gougedAFT BAGGAGE BAY STRUCTURE UPPER/OUTBOARD BEAM HAS GOUGES AT FS 1000.00 AND FS 1047.00. (C-CHECK RO 11/11/2024) REMOVED BAD AND INSTALLED REPLACEMENT OUTBOARD BEAM FOR AFT BAGGAGE BAY STRUCTURE AT FS 1000.00 TO FS 1047.00 REF CRJ900 SRM 51-42-21-001-001-Aug 31, 2024 · N161PQ · Cndair CL6002D24SDR CALA2024090302361Nut Plate · corrodedGEN ITEM 19-5310-1-2576 APU DOOR EXTERNAL SURROUND STRUCTURE LIF TED FWD LWR REF NR 172653-300-0008 FOUND STRAP NUTPLATE SURFACE 100% CORRODED INTERGRANULAR CORROSI VE THROUGHOUT FOUND TO BE OUT OF LIMITS, REPLACED STRP PN 148N31 38-20 IAW B757 SRM 51-40-02 PAAug 31, 2024 · N14121 · Boeing 757224SDR SWIA20240830Splice · corrodedUNION SPLICE AT FS 559.00-RBL9 IS CORRODED. REMOVED CORROSION AT UNION SPLICE AT FS 559.00-RBL9 REF SRM 51-21-06EVALUATED. ORIGINAL THICKNESS UPPER SIDE 0.150" REF STANDAR CMS6798 REV--, MINIMUM THICKNESS MEASURED 0.030", MATERIAL LOSS 0.120" WAS FOUND OUT OAug 30, 2024 · N906EV · Cndair CL6002B19SDR CALA2024090502389Spar · crackedEA5310-07557 REV A OP002 - 1EA HOLE FOUND CRACK AT LH BS1035 CENTER TANK FRONT SPAR WEB TRANSFER REF. NON-ROUTINE HX NRC WO.3636415 AND ORIGINATED BY EMP NO. V897470 LH BS1035 CENTER TANK FRONT SPAR WEB REPAIRED AND LOWER CHORD REPAIRED AS PER ECRA 5710-02889 Aug 30, 2024 · N778UA · Boeing 777222SDR CALA2024090502388Spar · crackedRH BS1035 CENTER TANK FRONT SPAR 1EA HOLE CRACK WAS FOUND ON THE WEB LAYER APPROX 0.040" AT 6 O`CLOCK POSITION. RH BS1035 CENTER TANK FRONT SPAR WEB REPAIRED AS PER ECRA 5710-02890 REV- PART 1 ITEM 1 INTERIM REPAIR, AND SPAR LOWER CHORD REPAIRED REFER HX NRCAug 30, 2024 · N778UA · Boeing 777222SDR CALA2024090402384Spar · crackedTWO HOLES FOUND CRACKED AT RT BS1035 CENTER TANK FRONT SPAR LOWER CHORD. CENTER TANK FRONT SPAR LOWER CHORD REPAIRED AS PER SRM 57-10-10-2R-1 REPAIR 1.Aug 30, 2024 · N778UA · Boeing 777222SDR CALA2024090402383Spar · crackedTHREE HOLES FOUND CRACKED AT RH BS1035 CENTER TANK FRONT SPAR LOWER CHORD. LH BS1035 CENTER TANK FRONT SPAR LOWER CHORD REPAIRED AS PER SRM 57-10-10-2R-1 REPAIR 1.Aug 30, 2024 · N778UA · Boeing 777222SDR UIEA2024083000881Fuel Cell · leakingRH AND LH WING DRY BAY, FUEL LEAK BETWEEN BAY BARRIER AND RIB 8 W.STA 375.8.(<P>FUEL LEAK WAS REPAIRED & THE SEALANT WAS APPLIED CORRECTLY IAW AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED</P>)Aug 30, 2024 · N1709A · Boeing 767375SDR DALA2024090208609Fitting · corrodedSHIP 3148 CORROSION CENTER FITTING FROM FRAME 16 TO FRAME 20 AT LEVEL STRINGER 23 RIGHT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING LOC. FRAME 16 TO FRAME 20 AT LEVEL STRINGER 23 RIGHT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72Aug 30, 2024 · N348NB · Airbus A319114SDR DALA2024083008600Cap · crackedCRACK ON CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN. SUMMARY OF NRC 00554: CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN WAS REPAIRED PER ERA 620017-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620017-14 REV 1. ASSOCIATED ER/A 14-620017 ADDED FOR AC 9527Aug 30, 2024 · N989AT · Boeing 717200SDR 2024FA0000676Panel · gougedNOSE WHEEL WELL RH SIDE GOUGE (REF NJA RFTS-111517 REV - DATED 08/15/2024).Aug 30, 2024 · N388QS · Cessna 680SOVSDR SWIA20240829Pressure Deck · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55667-601R-53-41-2669-N487CA MXCODEID50804-PR - THE PRESS FLOOR SKIN HAS 2-OFF CRACKS AT FS461 BTWN LBL9-RBL9. REMOVED DAMAGE AND APPLIED TEMP DBLR REPAIRS IN REF TO REO 601R-53-41-2669 REV--, DTD 01/14/2020. PERFORAug 29, 2024 · N487CA · Cndair CL6002B19SDR SWI2024F01172Window Post · crackedCRACKED UPPER OTBD BOLTHOLE ON PILOT WINDSHIELD SIDE POST (C-CHECK RO 11/7/2024) REMOVED AND INSTALLED PILOT COCKPIT SIDE WINDOW POST REF CRJ-200 SRM 51-42-21 AND DWG#601R33223 REV J DATED 03/30/1992,COMPLIED WITH TASK CARD 51-900-1003-SKY AND 56-220-10Aug 29, 2024 · N932SW · Cndair CL6002B19SDR SWI2024F01171Window Post · crackedCRACKED UPPER OTBD BOLTHOLE ON CO-PILOT WINDSHIELD SIDE POST (C-CHECK RO 11/7/2024) REMOVED CRACKED CO-PILOT SIDE WINDSHIELD POST REF CRJ200 SRM 51-42-21 AND INSTALLED NEW CO-PILOT SIDE WINDSHIELD POST REF DWG NO. 601R33007 REV U, COMPLIED WITH 51-900-1Aug 29, 2024 · N932SW · Cndair CL6002B19SDR SWAA2024092331974Stub Frame · crackedTYPICAL CRACK FOUND AT R1 DOOR STUB FRAME JUST ABOVE SEAL DEPRESSOR. CRACK LENGTH : 0.781'.<[01] REMOVED AND REPLACED STUB FRAME AT R1 DOOR SURROUND STRUCTURE SRM 51-40-02-0G-0 AND DWG:141A8370;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.Aug 29, 2024 · N555LV · Boeing 7377BDSDR 2A6R2024082971108Deck Plate · corrodedFASTENER HOLE DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK PANEL (PN: L533M1017293) UNDER THE AFT OUTBOARD SECTION OF THE RH XY FITTING. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEETAug 29, 2024 · N534LN · Urocop EC135P2SDR DALA2024082908542Window Frame · cracked(LOG 0527929) CRACK EVIDENCE ON CUTOUT UPPER OUTBD SIDE OF WINDOW #1 RH AT EXTERNAL FUSELAGE. CUTOUT UPPER OUTBD SIDE OF WINDOW #1 RH AT EXTERNAL FUSELAGE WAS REPAIRED PER ER/A 619752-14AD.Aug 29, 2024 · N3732J · Boeing 737832SDR DALA2024082908541Window Frame · cracked(LOG 0527923) CRACK EVIDENCE ON CUTOUT UPPER OUTBD SIDE OF WINDOW #1 LH AT EXTERNAL FUSELAGE. CRACK ON CUTOUT UPPER OUTBD SIDE OF WINDOW #1 LH AT EXTERNAL FUSELAGE WAS REPAIRED PER ER/A 619735-14AD.Aug 29, 2024 · N3732J · Boeing 737832SDR WRXR20240829001Door Frame · scratchedLIGHT SCRATCHES FOUND IN MULTIPLE AREAS ON THE UPPER AND LOWER EDGE FRAME OF THE AFT CARGO BAY DOOR. @ STRINGER 11-STRINGER 20 FS977-FS1051. LH SIDE SKIN PN: MM670-35116-007. SMOOTHED AND BLENDED LIGHT SCRATCHES FOUND IN MULTIPLE AREAS ON THE UPPER AND LOWER Aug 29, 2024 · N532EA · Cndair CL6002C10SDR DALA2024083008595Window Frame · crackedCRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW. SUMMARY OF NRC 00693: FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0526479)Aug 28, 2024 · N951AT · Boeing 717200SDR DALA2024083008593Beam · crackedCRACK BEAM #1 AFT EDGE AT L1 DOOR PTAS. SUMMARY OF NRC 00320: BEAM #1 AFT EDGE AT L1 DOOR PTAS WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0526246)Aug 28, 2024 · N989AT · Boeing 717200SDR CALA2024083002335Angle · crackedB757-06-3-0237 - LH WHEEL WELL AREA PANEL 197BL INTERNAL AFT FRAME INB BRACKET AND OUTB BRACKET (2EA) WITH CRACK.Aug 28, 2024 · N57869 · Boeing 75733NSDR CALA2024083002328Deck Plate · dentedB757-06-3-0254 - FLT COMPT FLOOR HAS LARGE DENT AFT CENTER AREA.Aug 28, 2024 · N57869 · Boeing 75733NSDR DALA2024082908557Door Frame · out of toleranceSHIP 3164 FRAME 66 R/H DOOR STOP FITTING #4 ALL FOUR HOLES OUT OF TOLERANCE. CORRECTIVE ACTION: REPAIRED PER ER/A 619947-14AD. (0526395)Aug 28, 2024 · N364NB · Airbus A319114SDR YENA2024082901186Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR ( AFT RH EEH DOOR 844 ) CRACK L=0.135 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404155 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460556 AND EC#Aug 28, 2024 · N706JB · Airbus A320232SDR YENA2024082901185Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833 ) CRACK L=0.130 INCH APRPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460553 AND EC#Aug 28, 2024 · N706JB · Airbus A320232SDR YENA2024082901184Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WAS FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR ( FWD RH EEH DOOR 843 ) CRACK L=0.200 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460554 AND EC# Aug 28, 2024 · N706JB · Airbus A320232SDR YENA2024082901183Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WASA FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834 ) CRACK L=0.220 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460555 AND EC# Aug 28, 2024 · N706JB · Airbus A320232SDR YENA2024082901182Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL FITTING I/B LOWER HOLE COMMON TO DOOR STOP FITTING Ñ7 AT FR16 RH. CRACK DIRECTION AT 9 O CLOCK VIEW LO OKING FORWARD; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00050) REMOVED AND REPLACED INTERCOSTALAug 28, 2024 · N706JB · Airbus A320232SDR SWI2024F01185Door Frame · corrodedFORWARD BAGGAGE BAY SURROUND STRUCTURE - FORWARD INNER UPPER JOINT PLATE HAS MULTIPLE AREAS OF CORROSION. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED AND REPLACED WITH NEW FWD BAGGAGE BAY SURROUND FWD INNER JOINT PLATE REF CRJ700 SRM 51-42-21-001-001Aug 27, 2024 · N755EV · Cndair CL6002C10SDR SWI2024F01181Door Frame · damagedFORWARD CARGO DOOR SURROUND STRUCTURE - INNER SKIN BETWEEN THE FORWARD AND AFT JOINT PLATES HAS DAMAGE ON THE EDGE BEHIND THE FORWARD AND AFT DOOR HINGES. (MARKED IN RED) (C-CHECK RO 11-6/2024) REPAIRED FORWARD CARGO DOOR SURROUND STRUCTURE - INNER SKINAug 27, 2024 · N755EV · Cndair CL6002C10SDR SWI2024F01180Door Frame · corrodedFORWARD BAGGAGE BAY SURROUND STRUCTURE - AFT INNER JOINT PLATE HAS MULTIPLE AREAS OF CORROSION FS578.00 STGR25L. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED AFT INNER JOINT PLATE (LOWER EXTERNAL), FROM FORWARD BAGGAGE BAY SURROUND STRUCTURE, FS578.0Aug 27, 2024 · N755EV · Cndair CL6002C10SDR SWIA2024092300827Beam · corrodedL/H BEAM @ FR 90 HAS CORROSION. (C-CHECK RO 9/20/2024) REMOVED AND REPLACED L/H BEAM AT FR 86/90 IAW REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED. OEM PARTS CHANGE - DOES NOT AFFECT WEIGHT AND BALANCE OF AIRCRAFT.Aug 27, 2024 · N110SY · Emb ERJ170200LRSDR SWAA2024083030851Post · corrodedPASSENGER CABIN FORWARD LAVATORY AFT DOOR POST IS CORRODED FROM THE FLOOR UP APPROX 2.5 INCHES.<[01] REPAIRED FWD LAV AFT DOOR POST PER YOKOHAMA CMM 25-42-44 FIG 605.;[02] VERIFIED REPAIR OF FWD LAV AFT DOOR POST PER YOKOHAMA CMM 25-42-44 FIG 605.Aug 27, 2024 · N7740A · Boeing 7377BDSDR DALA2024082808515Door Frame · crackedSHIP 3164 FRAME/FORMERS FRAME 16 RH AT DOOR STOPS NUMBER 7 DOUBLE JOGGLE HOLES 6 & 7 CRACKS. CORRECTIVE ACTION: REPAIRED PER ERA 593392-14AD. (0524996)Aug 27, 2024 · N364NB · Airbus A319114SDR DALA2024082808514Door Frame · crackedSHIP 3164 FRAME/FORMERS FRAME 16 RH AT DOOR STOPS NUMBER 7 DOUBLE JOGGLE HOLES 6 & 7 CRACKS. CORRECTIVE ACTION: REPAIRED PER ERA 593392-14AD. (0524992)Aug 27, 2024 · N364NB · Airbus A319114SDR DALA2024082708491Door Frame · corrodedAIRCRAFT 9550, CORROSION ON DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160 FOUND PREVIUOS HOLE PLUGGED LIKE REPAIR AND NO DECAL FOUND. CORRECTIVE ACTION: CORROSION LEVEL 2 // DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160 Aug 27, 2024 · N717JL · Boeing 717200SDR DALA2024082708479Window Frame · cracked(LOG 0524113) LHS NO. 3 FLIGHT COMPARTMENT WINDOW FRAME LOWER FWD CORNER CRACK. COMPLIED WITH E/RA 620400-14AD REV. ORIG.Aug 27, 2024 · N3769L · Boeing 737832SDR IPXA2024092464213Support · looseLOWER FWD WING TO BODY SUPPORT IN FRONT OF LEFT ECS BAY DOOR STA 900 HAS EXFOLIATING CORROSION DOT 47-10. INSTALLED NEW T-CHORD IN STRUCTURES ZONE 100 LOWER FWD WING TO BODY FRONT OF LEFT ECS BAY DOOR STA 900 IAW SRM 51-4O-02.Aug 26, 2024 · N402UP · Boeing 75724APFSDR SWAA2024092030428Beam · crackedCRACK FOUND AT I/B FASTENER HOLE ON #4 BEAM (141A6536-14) OF FORWARD SERVICE DOOR.<[01] ACCOMPLISHED REMOVAL OF #4 BEAM (141A6536-14) AND INSTALLATION OF NEW #4 BEAM (141A6536-20) OF FORWARD SERVICE DOOR<BR>IN ADDITION; ASSEMBLED R-1 DOOR PARTS THAT WERE REMOVAug 26, 2024 · N555LV · Boeing 7377BDSDR IPXA2024091164453Door Frame · damagedCREW ENTRY DOOR STOP FITTING HAS MATERIAL LOSE. DOT 28-02. (RO-28). APPLIED TREATMENT, PRIMER AND TOP COAT AT CREW ENTRY DOOR STOP FITTING IAW B757 SRM 51-20-01 AND AMM 51-21-15; REVIEWEDAug 26, 2024 · N402UP · Boeing 75724APFSDR CALA2024082802301Window Frame · crackedREF.EA5310-04554 OP002-TYPICAL CRACK FOUND ON RT #1 WINDOW FRAME UPPER AFT CORNER. ACCOMPLISHED RH #1 WINDOW FRAME PERMANENT REPAIR / PREVENTIVE / TRIPLER AS A PERMANENT REPAIR . MODIFICATION IAW EA#5310-04554 REV."C"OP-004,WHICH REQUIRES TO REF. AAR N/R:9Aug 26, 2024 · N24202 · Boeing 737824SDR DALA2024082708486Window Frame · crackedAIRCRAFT 9510, HIDDEN DISCPRECANCY; AFTER BRACKET WAS REMOVED, CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW. CORRECTIVE ACTION: FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCAug 26, 2024 · N951AT · Boeing 717200SDR IPXA2024082764453Stop Fitting · damagedCREW ENTRY DOOR STOP FITTING HAS MATERIAL LOSE. DOT 28-02. (RO-28)Aug 26, 2024 · N402UP · Boeing 75724APFSDR HYIA20240827003Spar · crackedDURING MAINTENANCE A .187 INCH CRACK WAS VISUALLY IDENTIFIED ON THE LEFT HAND SIDE OF THE FORWARD CARRY THROUGH SPAR, ON THE FORWARD WEB, IN THE AREA OF THE SPAR WEB CUT OUT LOCATED AT LBL 32.55. THIS CRACK IS CONSISTENT WITH OTHER CRACKS VISUALLY IDENTIFIED IAug 26, 2024 · N890CA · Cessna 402CSDR AALA202411201683Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLE AT FR 36 AND -Y1516. REPAIRED PRESSURE DECK MEMBRANE PER EA 357693.Aug 25, 2024 · N162UW · Airbus A321211SDR AALA202411204384Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLE AT FR 36 AND +Y1516. REPAIRED PRESSURE DECK MEMBRANE PER EA 357693.Aug 25, 2024 · N162UW · Airbus A321211SDR IXXA20241002012Access Panel · gougedP32 PANEL LH DOOR GOUGEDAug 25, 2024 · N491AZ · Boeing 767323SDR SWAA2024091930026Window Frame · crackedCRACK WINDOW 3 FRAME LT SIDE AT COCKPIT 2024-489385<[01] PERFORMED A PERMANET REPAIR ON WINDOW 3 FRAME LT SIDE AT COCKPIT IAW EA- 24-153-02350-WIP1 [TTG8Q00VGP0W]; EA-24-153-02350-WIP2 [TTG8Q00VPE70]; 24-153-02350-WIP3 [TTG8Q00VT5E5]; 24-153-02350-WIP4 [TTG8Q0Aug 25, 2024 · N495WN · Boeing 7377H4SDR U2RA2024090800051Door Frame · out of limits"REF HAECO XMN (TX9Y778Y) NRC#:KUL9555 - AN EXISTING OVERSIZED HOLE WAS FOUND ON FRAME STRUCTURE AT STA 2231, STR-25L DURING SB 747-53A2450 REV. 08 INSPECTION. THE DIAMETER (0.309"") IS GREATER THAN SB 747-53A2450 REV. 08 ALLOWED (MAX 0.2817"")."Aug 25, 2024 · N756CA · Boeing 747412
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