JASC 5311

Service difficulty reports · 61,537

Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311'
  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 JJBA20250513052Frame · crackedEXTERNAL RF II CRACK FOUND FRAME 79 BTW STR 4R-3R AND BTW STR 4R-5R. REPAIR DOUBLER ON RH REAR FUSE II SKIN, AT FR79 BTW STR 3R-5R.May 1, 2025 · N21144 · Emb EMB145XRSDR REXA2025050200547Frame · corrodedF.S. 349 STR 26L-25R CORRODED IN MULTIPLE PLACES REMOVED AND REPLACED FRAME PN SH670-31357-5 AT F.S.349May 1, 2025 · N690CA · Cndair CL6002C10SDR CALA2025050204412Frame · crackedFRAME 68 RH AT STR 8 HAS CRACK INDICATION ON AFT FACE AT RADIUS OF FLANGE JUST ABOVE UPPERMOST FASTENER IN WEB, APPROX .50 INCH LONG. PREFORMED FRAME FITTING REPAIR AT FR68 RH STR8R IAW A320SRN53-41-12. W/P/B PERFORMED FRAME FITTING REPAIR AT FR68 RH STR8R May 1, 2025 · N460UA · Airbus A320232SDR CALA2025050204411Frame · dented(19-5310-1-2500) STR-AFT CARGO COMPT. L/SIDE FR1260 BTWN STRG 25 /26 HAS A DENT ON FEE FLANGE AREA DOT 34-005 SDR/SFR REPORTING ONLY REPAIR ON AFT CARGO COMPARTMENT STA 1260 STR 25LH WAS PERFORMED IAW WORK PER UAL EC/RA #5360-01947 AND VT MAE EA 757-5360-13-A3May 1, 2025 · N17126 · Boeing 757224SDR SWAA2025060366068Frame · crackedCRACK ON BS 312 FRAME COMMON TO STR 5L ABOVE FWD ENTRY DOOR UPPER SILL WEB.<[01] REPAIRED BS 312 FRAME COMMON TO STR 5L ABOVE FWD ENTRY DOOR UPPER SILL WEB IAW EA 22-153-01244.;[02] VERIFIED ACTION 1Apr 30, 2025 · N288WN · Boeing 7377H4SDR SWAA2025060266041Stub Frame · crackedCRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR; BETWEEN S-8R AND S-9R; LENGTH 1.6' (MARKED)<[01] REMOVED AND REPLACED STUB FRAME AT FWD SERVICE DOOR UPPER FWD AREA PER SRM 51-40-02; SRM 53-10-01-2R-6 REP 6 AND DWG 141A8370 REV D;[02] CORRECTIVEApr 30, 2025 · N285WN · Boeing 7377H4SDR SWAA2025060266067Frame · crackedCRACKED FRAME BS 259.5 AT CUTOUT RBL 40 WL 260.<[01] THE DAMAGE WAS REPAIRED WITH A WEB SEGMENT SPLICE PER EA 25-153-01133. AN INSPECTION THRESHOLD IS DEFINED IN EA 25-153-01133-DTI.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Apr 30, 2025 · N288WN · Boeing 7377H4SDR DALA2025050503444Frame · damaged(LOG 0941672) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE LEFT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGERS S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING, AND PEApr 30, 2025 · N374DA · Boeing 737832SDR DALA2025050103381Frame · damagedSHIP 3407 FR62 AFT SIDE BETWEEN STR 1L AND 1R HAS 2 OPEN HOLES AND TOOLING DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 625466-14 REV C. (0942161)Apr 30, 2025 · N407DX · Airbus A330941SDR AALA202507169685Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 BETWEEN S8R AND S9R. REPAIRED FRAME PER EA 364839.Apr 29, 2025 · N182UW · Airbus A321211SDR SWAA2025060665675Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 1.250 INCH AT PASSENGER CABIN 2025-291010<[01] REPLACED STUB FRAME LOCATED ON BTW BS 294.5 TO BS 296 AND BETWEEN STR-7R TO STR-10R Apr 29, 2025 · N222WN · Boeing 7377H4SDR DALA2025043003325Frame · damagedSHIP 3407 AFT SIDE OF FRAME 63 BETWEEN STRINGER R1 AND L1 TOOLING DAMAGE ON FACE OF BRACKET. REPAIRED PER SECTION II OF ERA 625466-14 REV. A AND REV B AND REV. C.Apr 29, 2025 · N407DX · Airbus A330941SDR AALA202507064513Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE AT OPEN FASTENER HOLE 2 INCH OB FROM -Y1292. CRACK DIRECTION ARE 6 AND 12 OCLOCK, CRACK DEPTH IS 0.090 INCH, IN FWD CARGO COMPARTMENT. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIApr 28, 2025 · N760US · Airbus A319112SDR SWIA20250612428Frame · crackedFRAME SECTOR FS605.00 CRACKED BETWEEN STR18L - STR19L. (FILED CLOSED)REF CP 30108469 FOR FRAME SECTOR FS 605 REPLACEMENT FROM STR17L - STR21L AND ALTERNATE FASTENER REO.Apr 28, 2025 · N954SW · Cndair CL6002B19SDR SWAA2025060565031Frame · crackedCRACK ON FRAME WEB LOCATED BS 259.5 BTW STR 8R TO STR 9R AT FWD GALLEY AREA 2025-290962<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 220272712; DUE DATE: 28-JAN-26.;[02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBApr 28, 2025 · N222WN · Boeing 7377H4SDR SWI2025F00596Frame · crackedFRAME SECTOR FS605.00 CRACKED BETWEEN STR18L - STR19L. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSApr 28, 2025 · N954SW · Cndair CL6002B19SDR SCN2025F00001Frame · crackedINITIAL INSPECTION: CRACK ON FRAME STA 500H APPROX LBL 17.5 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE - RESOLUTON:FRAME STA 500H APPROX LBL 17.5 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIR PER ETI-737-25-061 REV. 2 AND SCX MDDR 131702 LOG 812909 AND EA Apr 27, 2025 · N804SY · Boeing 7378SDR 2025FA0000322Frame · crackedFOUND 12MM CRACK ON THE INNER CHORD TRANSITION RADIUS LOWER EDGE, STA 903 L/H.Apr 27, 2025 · N29383 · Boeing 7673Q8SDR YENA2025042900446Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND OPEN HOLE B FR16LH LOC DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOK (VIEW OUTSIDE SKIN) CRACK DEPTH 0.100 INCH; (RESOLVED ON W/O: 1356112 TASKCARD: NR-00040) PERFORMED PERMANENT REPAIR ON HOLE B LOC FR16LH LOC DOApr 26, 2025 · N526JL · Airbus A320232SDR YENA2025042900445Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND OPEN HOLE B FR16LH LOC DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK (VIEW OUTSIDE SKIN) CRACK DEPTH 0.100 INCH; PERFORMED PERMANENT REPAIR ON HOLE B LOC FR16LH LOC DOUBLE JOGGLE AREA DIRECTION 9 OCLOCK IAW A320 Apr 26, 2025 · N526JL · Airbus A320232SDR DALA2025042803285Bracket · mislocatedSHIP 3407 WIRE BUNDLE BRACKET'S (2) ON FR 64 BETWEEN STGR 1L/1R IS NOT LOCATED IN THE CORRECT POSITION PER DRAWING. CORRECTIVE ACTION: CORRECTED PER NON-ROUTINE 86 IN THE WORK PACKAGE. (0933271)Apr 25, 2025 · N407DX · Airbus A330941SDR SWAA2025052928123Frame · crackedCRACK FRAME ON BS 947.5 AND RBL 8.1 AT AFT CARGO COMPARTMENT 2025-274492 <[01]. REPLACED FRAME LOCATED ON BS 947.5 BETWEEN STR 23 RH TO STR 23 LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWApr 24, 2025 · N291WN · Boeing 7377H4SDR CALA2025042804277Frame · crackedRH FR 16 DOUBLE JOGGLE HOLE 7 HAS 2EA CRACK INDICATIONS IN FRAME LAYER ONLY 80% S.H.Apr 24, 2025 · N496UA · Airbus A320232SDR CALA2025042804276Frame · corrodedFUSELAGE UNDERFLOOR AFT FACE OF FR 67 HAS CORROSION B/W LSTR42 A ND RSTR42.Apr 24, 2025 · N496UA · Airbus A320232SDR DALA2025042503253Frame · dentedSHIP 6710 DTA MONITOR INSPECTION LOG REF ERA 625729-14, FUSELAGE / AFT CARGO COMPARTMENT / FRAME BOTTOM / BSTA 1520 / BTW S-25L & S-27L / DENT. (0930830)Apr 24, 2025 · N6710E · Boeing 757232SDR DALA2025042503250Frame · dentedSHIP 6710 DENT ON FRAME AT STA 1520 AND S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00380. FRAME AT STA 1520 AND S-26L AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 625729-14AD REV ORIGINAL SECTION I: REPAIR INSTRUCTIONS AND PRI 625729-1Apr 24, 2025 · N6710E · Boeing 757232SDR AALA202507123917Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT DOUBLE JOGGLE AREA, FR 16 RIGHT AND DOOR STOP #7. REPAIRED FRAME PER EA 364655.Apr 23, 2025 · N180US · Airbus A321211SDR VNAA20250529023Frame · corrodedCORROSION ON FRAME AND ATTACH FLANGE FS1047.00 BTW STGR 24L-26L AT AFT CARGO COMPARTMENT . EVALUATED DAMAGE ON FRAME AND ATTACH FLANGE FS1047.00 BTW STGR 24L-26L AT AFT CARGO COMPARTMENT ITS NOT ALLOWED PER CRJ900 SRM 53-61-06-101-003-A02 AND REPAIRED PER REApr 23, 2025 · N553NN · Bombdr CL6002D15SDR SWAA2025051957594Frame · crackedCRACKED FRAME AT AFT CABIN BS727D S-8L.<[01] FRAME REPAIRED AND FASTENERS INSTALLATION ACCOMPLISHED (REF: SUBTASK TTG8Q010729D; EA# 25-153-01123 REV: A);[02] VERIFIED CORRECTIVE ACTION ENTRY 1.Apr 23, 2025 · N437WN · Boeing 7377H4SDR YENA2025042400425Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE HORIZONTAL FLANGE RADIUS AT STGR 8, WEB AFT FACE. CRACK LENGTH IS 0.210 INCH APPROX AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389929 TASKCARD: NR-00028) REF AE WO 2025-134/1. N/R# 2025 - 237225Apr 23, 2025 · N531JL · Airbus A320232SDR YENA2025042400424Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 STGR 8RH / HORIZONTAL FLANGE / HOLE 1 AND 7 / CRACKS – PERMANENT REPAIR; /1/ EA 53-0020-25 REV 0 (COVER AND PART (1-3)) /2/ RDAF 81571877/003/2025 ISSUE A /3/ DOSSIER 81571877 /4/ SRM 53-41-12-300-012.Apr 23, 2025 · N531JL · Airbus A320232SDR DALA2025042403194Floor Support · corrodedCORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY A REA (SSI 534147). REPLACED FLOOR SUPPORT -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53472780, DWG D53472816 ISSUE F AND DApr 23, 2025 · N342NB · Airbus A319114SDR DALA2025042403193Frame · crackedCRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE 4 AT DOOR S TOP FITTING 1 POSITION, CRACK DIRECTION ARE 6 AND 12 OCLOCK, CRACK DEP TH IS 0.120 INCH APPROX, HOLE DIAMETER IS 0.250 INCH APPROX, AA 5311-0 1216, AD RELATED, ACTIONS REQUIRED PRIOR TO FURApr 23, 2025 · N321NB · Airbus A319114SDR DALA2025042303173Frame · damagedSHIP 3356 WHILE ACCOMPLISHING W/C:5230-01164-10 TO REPLACE FORK FRAME FR61, FR61A, FR64, FOUND HOLES H-5 AND H-6 WILL SHORT EDGE MARGIN AT BEAM4. CORRECTIVE ACTION: COMPLIED WITH ERA 625519-14AD SECTION II REV ORIGINAL. (0928076)Apr 23, 2025 · N856NW · Airbus A330223SDR VNAA20250602006Frame · corrodedCORROSION ON FRAME 847.00 + 32.00 BTW STGR 26L TO STGR 26R AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON FRAME 847.00 + 32.00 BTW STGR 26L TO STGR 26R AT FUSELAGE INTERNAL STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PApr 22, 2025 · N598NN · Cndair CL6002D24SDR VNAA20250601010Frame · corrodedCORROSION ON FRAME 645.00 BTW STGR 18L AND STGR 19L AT AT CABIN FLOOR STRUCTURE. ON FRAME 645.00 BTW STGR 18L AND STGR 19L AT AT CABIN FLOOR STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-0Apr 22, 2025 · N598NN · Cndair CL6002D24SDR SWAA2025052956934Stub Frame · crackedCRACK INDICATION (2 E/A) ON STUB FRAME LOCATED AT BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH: 0.875 INCHES AND 0.680 INCHES APPROX. 2025-274283 <[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BTW STR 7R TO STR 10R IAW B737-700 SApr 22, 2025 · N291WN · Boeing 7377H4SDR NI6R202505260062Frame · crackedWHILE PERFORMING ZONE 4 INSPECTION OF SB 244, FOUND CRACKS IN UPPER FRAME AT FS 386 IN BOTH PASS THROUGH HOLES.Apr 22, 2025 · N690TG · Gulstm 690ASDR NI6R202505260061Frame · crackedWHILE PERFORMING ZONE 4 INSPECTION OF SB 244, FOUND CRACKS IN UPPER FRAME AT FS 386 IN BOTH PASS THROUGH HOLES.Apr 22, 2025 · N690SG · Gulstm 690ASDR SWAA2025052058363Door Frame · crackedPASSENGER CABIN FED UPPER FRAME BS 312 STR 5L CRACKED<[01] REPAIR ACCOMPLISHED AT M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L)<BR>'EA-GENERAL' REPAIR REFERENCE IS SELECTED.Apr 22, 2025 · N226WN · Boeing 7377H4SDR UIEA2025041200454Frame · mechanic errorFWD CARGO COMPARTMENT STA 500B LBL 21.5" FRAME I/B FLANGE WITH MIS DRILLED HOLE.(<P>REPAIRED FUSELAGE FRAME I/B FLANGE SECTION AT STA 500B BTWN STR 25LH I/A/W COOPESA COO-EO-2025-21962-R00 DATED MAR/25/2025 CATEGORY B REPAIR. DOCUMENTED ON FAA FORM 8110-3. NO Apr 22, 2025 · N5113A · Boeing 73783NSDR UIEA2025041400457Frame · mechanic errorFWD CARGO COMPARTMENT STA 500G LBL 21.5" FRAME I/B FLANGE WITH MIS DRILLED HOLE.(<P>REPAIRED FUSELAGE FRAME I/B FLANGE SECTION AT STA 500G BETWEEN STR 25L AND STR 27L I/A/W COOPESA COO-EO-20-25-21968- R00 REV00, DATED MAR 15-25, CATEGORY B REPAIR. DOCUMENTED Apr 22, 2025 · N5113A · Boeing 73783NSDR IPXA2025050234228Frame · dented*** MAJOR REPAIR *** DENT ON FRAME STA 760 S23L AT FWD CARGO COMPARTMENT. DOT 21-03. PERFORMED TRIM OUT TO REMOVED DAMAGED IAW B757-200-SRM-51-10-02 AND SRM 53-00-07-2R-5 DETAIL I. LOCATED AND DRILLE NEW FRAME IN STA 760 S23L AT GWD CARGO IAW B757-200PF SRM Apr 18, 2025 · N447UP · Boeing 75724APFSDR IPXA2025050534270Frame · dentedDENT ON FRAME STA 840 S24R AT FWD CARGO COMPARTMENT. DOT 21-02.PERFORMED TRIM OUT AT DAMAGE AREA IAW SRM-51-10-02 AND B757-200 SRM 53-00-07-2R-5.REMOVED FASTENERS COMMON WITH THE REPAIR IAW SRM-51-40-02 AND B757-200 SRM 53-00-07-2R-5.PERFORMED HFEC ON TRIM OUTApr 18, 2025 · N447UP · Boeing 75724APFSDR CALA2025042304163Frame · deformedFRAME STA 1440 BTW STR 26LH-27LH HAS A DENT ESFR ENTRY DENT OF FRAMESTA 1440 DIMENSIONS; L=1.5, W=.900 D=.070. PERFORME D REPAIR AS PER SRM 53-00-07-2R-5. REQUIRES REPEAT INSPECTIONS ADD EMP:V940985 PER SRM 53-00-07-2R-5 TABLE 2 ZONE 1 37,500 FLIGHT CYCLES AFTApr 18, 2025 · N57111 · Boeing 757224SDR DALA2025042203153Frame · dentedSHIP 6712 STA 540 BTW S26L-S25L FRAME DENTED. CORRECTIVE ACTION: FRAME FOUND TO BE OUT OF LIMITS IAW 53-00-07-1A-1 FIGURE 101 FRAME REPAIRED IAW PRI REV 1. WORK COMPLETE. (0920331)Apr 18, 2025 · N6712B · Boeing 757232SDR DALA2025042203151Frame · dentedSHIP 6710 DENT ON FRAME AT STA 1400 S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00381 PERMANENT REPAIR CATEGORY "B" ON FRAME AT STA 1400 S-26L AT AFT CARGO COMPARTMENT WAS PERFORMED PER B757- 200 SRM 53-00-07-02R REPAIR 5. (0919734)Apr 18, 2025 · N6710E · Boeing 757232SDR DALA2025042203150Frame · dentedSHIP 6710 DENT ON FRAME AT STA 1400 S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00381 PERMANENT REPAIR CATEGORY "B" ON FRAME AT STA 1400 S-26L AT AFT CARGO COMPARTMENT WAS PERFORMED PER B757- 200 SRM 53-00-07-02R REPAIR 5. (0919685)Apr 18, 2025 · N6710E · Boeing 757232SDR N6WA2025041903Frame · corrodedCORROSION ON ATTACHED FLANGE AND WEB AT FS295 BETWEEN STGR26L AND STGR25R. REMOVED AND REPLACED FRAME AND ATTACHED FLANGE IAW AWATS EO-25-CRJ5-53-066 AND GOJET EO-C550-53MR-065-O.Apr 18, 2025 · N540GJ · Cndair CL6002C11SDR N6WA2025041902Frame · corrodedCORROSION ON ATTACHED FLANGE AND WEB AT FS310.00 BETWEEN STGR26L AND STGR25R. REMOVED AND REPLACED FRAME AND ATTACHED FLANGE IAW AWATS EO-25-CRJ5-53-065 AND GOJET EO-C550-53MR-066-OApr 18, 2025 · N540GJ · Cndair CL6002C11
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