JASC 5300

Service difficulty reports · 8,206

Reports filed under 5300 · Fuselage Structure (General), 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 = '5300'
  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 TSAA20211117035Stringer Clip · crackedREPLACED STRINGER CLIP @ STA. 727D STR. 5R IAW ECO NO.3759R2 DATED 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 REV.125.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117036Stringer Clip · crackedREPLACED CRACKED STRINGER CLIP @ STA 727E, STR 1 IAW ALOHA AIR CARGO ECO 3759 REV 2, DATE 3/20/17, PARA 8.0, PART III, FIG 16. FASTENERS INSTALLED IAW 8737-300 SRM CH 51-40-02, REV 125.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117037Stringer Clip · crackedREPLACED CRACKED STRINGER CLIP STA 727E STR 5L IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17, IAW 8737-300 SRM REV 125 51-40-02.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117038Stringer Clip · crackedREPLACED STRINGER CLIP STA 887 STR 4R IAW ALOHA AIR CARGO ECO 3759 REV 2 DATE 3/20/17. FASTENERS INSTALLED IAW 8737-300 SRM 51-40-02 PG 2 REV 125.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117039Stringer Clip · crackedREPLACED STRINGER CLIP STA 685 STR10L IAW ALOHA AIR CARGO ECO 3759 REV 2 3/20/17 PARA 8.0 PART III FIGURE 16.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117041None · noneREPLACED AUXILIARY CHORD AT STA 727 LH BETWEEN STR 17L & STR 22L. I.A.W. B737-300 SRM REV 126 CH 51-40-02 REF BOEING DOC #65-46547 REV:DK.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117029Stringer Clip · cracked1000605593 - REPLACED STRINGER CLIP@ STA 685, STR 7L IAW ALOHA AIR CARGO ECO 3759 REV 2, DATE 3/20/17, PARA 8.0 PART ILL FIG16. + IAW B737-300 SRM CH 51-40-02 REV 125.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117028Stringer · cracked1000605592 - REPLACED STRINGER CLIP@ STA639 STR. 2R IAW ECO NO.3759R2 DATED 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 REV. 125.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117027Stringer Clip · cracked1000605591 - REPLACED STRINGER CLIP@ STA 597 STR 7L IAW ECO. NO. 3759R2 DATED 3/20/17. FASTENERS INSTALLED IAW B737-300 SRM 51-40-02 REV.125Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117047Intercostal · corrodedCORROSION ON INTERCOSTAL UNDER ANCHOR NUT @ STA 500A+18" BETWEEN STR 25L-26L REMOVED I.A.W. SRM REV 125 CH 51-10-02. NOMINAL THICKNESS: 0.020", REMAINING THICKNESS: 0.011". MATERIAL REMOVAL OF 0.009" IS NOT WITHIN ALLOWABLE LIMITS OF 0.002" I.A.W. B.737-300 SRNov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117026Flange · corroded1000582166 - REPAIRED FWD FLANGE ON O/B CHORD@ B.S 727 R/H STR 18R I.AW KF AEROSPACE DWG #R27904.1-053-017-001 REV NC AND BOEING PREVENTATIVE MOD SB 737-53A1166 REV 2 DATED JUNE 30, 1994Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117048Intercostal · corrodedCORROSION ON INTERCOSTAL UNDER ANCHOR NUT @ STA 5008+2" BETWEEN STR 25L-26L REMOVED I.A.W. B.737-300 SRM REV 125 CH 51-10-02. NOMINAL THICKNESS:0.020", REMAINING THICKNESS:0.008". MATERIAL REMOVAL OF 0.012" IS NOT WITHIN ALLOWABLE LIMIT OF 0.002" I.A.W. B.737-Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117049Beltframe · gougedPERFORMED HFEC SURFACE INSPECTION ON BLENDED AREAS ON BELTFRAME STA 727B STR 20R-23R. NO CRACKS FOUND. SEE EXECAIRE WO #498478. REMOVED GOUGES ON I/B FLANGE OF BELTFRAME, STA 727B STR 20R-23R IAW B737-300 SRM REV 125 51-10-02 PARA 5. NOM THICK .063", REMOVED .Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117051Stringer Clip · crackedREPLACED STRINGER CLIP STA 685 STR 10L IAW ALOHA AIR CARGO ECO 3759 REV 2 3/20/17 PARA 8.0 PART III FIGURE 16.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117052None · noneREPLACED AUXILIARY CHORD AT STA 727 LH BETWEEN STR 17L & STR 22L. I.A.W. B737-300 SRM REV 126 CH 51-40-02 REF BOEING DOC #65-46547 REV:DK.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117053Beltframe · crackedREPLACED BELTFRAME @ FS 440 R/H SIDE BETWEEN ST 17R-16R WITH MADE REPAIR PART IAW B737-300 SRM REV 125 51-10-02 PARA 8. INSTALLED BELTFRAME IAW BOEING DWG 65-20722 REV: AH AND B737-300 SRM REV 125 51-40-02.Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117056Stringer Splice · crackedCOMPLIED WITH AD 2014-01-05, PERFORMED INSPECTION OF STRINGER SPLICES AND BUTT STRAPS AND REPLACEMENT IAW ALOHA AIR CARGO ECO 3866, PT. II, REVISION 1, DATE: 8/17/17, CRACKS FOUND. SEE NDT REPORT NDT21-1540 ON STRINGER SPLICE AT STA 908 AT STR 4R & 4L CRACKS Nov 15, 2021 · N301KH · Boeing 737330SDR TSAA20211117001Structure · corrodedCORROSION ON FUSELAGE BELLY SKIN AT STA 727B, STR 26R FOUND TO BE BEYOND LIMITS IAW B737-300 REV 125 SMR 53-00-01, NOM THICKNESS OF 0.063", ALOWABLE REMOVEL 0.0063", REAMING THICKNESS 0.053", REPAIRED FUSELAGE BELLY SKIN AT STA 727B STR 26R IAW B737-300 REV 12Nov 15, 2021 · N301KH · Boeing 737330SDR CALA2021111702115Stringer · crackedAFT CARGO COMPT STA 1205 S-36L AREA FOUND CORROSION CRACK. TRANSFER REF NR LP 9131558 AND ORIGINATED BY V897013. AFT CARGO COMPT STRINGER 36L BETWEEN STA 1197+120VAND STA 1219 REPAIRED AS PER SRM 53-00-03 REPAIR 2 FIG 201. WORK ACCOMPLISHED BY MECHANIC V897532Nov 15, 2021 · N662UA · Boeing 767322SDR GTIA2021111536124None · noneR1 R2 & L2 DOOR ASSIST BOTTLES REQUIRE SERVICE -SERVICED R1 R2 & L2 DOOR ASSIST BOTTLES IAW AMM 52-10-00Nov 15, 2021 · N685NK · Airbus A321231SDR GTIA2021111536122None · noneL1 AND L2 DOOR ASSIST REQUIRE SERVICE-SERVICE L1 AND L2 DOOR ASSIST WITH NITROGEN PER AMM 52-10-00 LEAK CHECK GOODNov 15, 2021 · N630NK · Airbus A320232SDR JJBA20211115023None · noneSIGNS OF CORROSION ON RH UPPER FLOOR BEAM TRACK SUPPORTS AFT OF FRM 52. REMOVED AND REPLACED BEAM, HAT ASSY FROM FR 49 - FR 55 RHNov 15, 2021 · N11193 · Emb EMB145XRSDR 2021FA0000320Skin · chafedTWO AREAS OF DAMAGE FROM WIRES CHAFING, TOP OF STINGER SKIN. TEXTRON AVIATION ENGINEERING MEMO DQ32377M1 DATED 11NOV2021.Nov 15, 2021 · N508QS · Cessna 680ASDR SWIA202163841None · damagedEXTRA HOLE ON AIRCRAFT STRUCTURE UNDER RAM AIR PANEL 323AT (MARKED) (C CHECK RO 1/16/2022) REPAIRED EXTRA HOLE ON AIRCRAFT STRUCTURE UNDER RAM AIR PANEL 323AT. REF: MHIRJ REO 670-55-31-153 REV -- DATED 2021-11-19. COMPILED WITH SKYWEST TASK CARD 51-900-100Nov 14, 2021 · N770SK · Cndair CL600*SDR SWIA202163435None · corrodedFWD WATER-WASTE SURROUND STRUCTURE IMPACT ANGLE CORRODED (C CHECK RO 12-31-21) REPLACED FWD WATER WASTE SURROUND STRUCTURE IMPACT ANGLE REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-32280 REV. H. COMPIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.Nov 14, 2021 · N824SK · Cndair CL6002D24SDR SWIA202163434None · corrodedFWD WATER-WASTE SURROUND STRUCTURE LWR DIAPHRAGM CORRODED (C CHECK RO 12-31-21) REPLACED FWD WATER WASTE SURROUND STRUCTURE LWR DIAPHRAGM REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-32280 REV. H. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GONov 14, 2021 · N824SK · Cndair CL6002D24SDR CALA2021111502105None · corrodedAFT CGO COMPT STA 1285 LBL 24" FLOOR BEAM UPPER CHORD FOUND CORROSION CRACK. TRANSFER REF. HX NON-ROUTINE LP 9131773 AND ORIGINATED BY EMP NO. V896921 AFT CARGO COMPT STA 1285 LBL 20.5 - LBL 25.5 WL 123 FRAME INNER CHORD J SECTION REPAIRED AS PER EC/RA 5360-01Nov 14, 2021 · N662UA · Boeing 767322SDR 2022F00108None · noneUPPER AFT FUSELAGE SKIN GOUGE UNDER DORSAL STRAKE. CORRECTIVE ACTION: REMOVED DAMAGE BY BLENDED AND PERFORMED NDT UT, HFEC IN AREA FROM F.S. 879 TO FS 1126 ON FUSELAGE SKIN AT STR 0 IAW WITH EA 21-C7-53-1222 REV A DATE 11/26/2021.Nov 13, 2021 · N527EA · Bombdr CL6002D15SDR SWIA202162607None · damagedTRANSFER FROM EAML 778862 : TRANSFERRED FROM CAMP 23817432. DAMAGE FOUND TO BE ON RIGHT SIDE OF AIRCRAFT BETWEEN FS 379.00 AND FS 394.00 TO BE AS FOLLOWS: / (1-OFF) DENT DAMAGE MEASUREING 1.25" LENGTH X .075" WIDTH X 0.060" MAX DEPTH & (1-OFF) GOUGE DAMAGE MENov 13, 2021 · N917EV · Cndair CL6002B19SDR JJBA20211113024None · noneLH AFT FUSELAGE, INTERIOR AT FR59-FR61 @ Y=479.0 HAS SIGNS OF CORROSION UNDER FLOOR BY LAV. REMOVED AND REPLACED LH FR 59 - FR 61 @ Y=479 GUSSETNov 13, 2021 · N11193 · Emb EMB145XRSDR JJBA20211113022None · noneSIGNS OF CORROSION UNDER GUSSET LH AT HAT BEAM FR59-61 BL-479. ACCOMPLISHED CENTER FUSELAGE IV-CF IV FLOOR STRUCTURE OMEGA BEAM, CORROSION PERMANENT REPAIR AT FR 59 AT FR61 BL479 LNov 13, 2021 · N11193 · Emb EMB145XRSDR JJBA20211113021None · noneSIGNS OF CORROSION UNDER GUSSET CENTER AT HAT BEAM FR59-61, BLO. ACCOMPLISHED CENTER FUSELAGE IV-CF IV FLOOR STRUCTURE-OMEGA BEAM CORROSION PERMANENT REPAIR. HAT BEAM, CENTER FR59-FR61, BLONov 13, 2021 · N11193 · Emb EMB145XRSDR JJBA20211113020None · noneAFT FUSELAGE INTERIOR, FR 59-61 C Y=0.0 HAS SIGNS OF CORROSION UNDER FLOOR BY LAV. REMOVED AND REPLACED GUSSET AT FR 59 - 61 CY=0.0Nov 13, 2021 · N11193 · Emb EMB145XRSDR 2021FA0000349Intercostal · crackedMAIN CABIN FWD. FLOOR AREA R/H SIDE HAS A CRACKED INTERCOSTAL AT STA. 270.000, REF NRC B000331.Nov 12, 2021 · N782SP · Doug 600NSDR CALA2021111502097Beam · corroded(A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR24 AT Y-1292, SEAT TRACK WITH CORROSION. DOT 88-001.() DAMAGE FOUND WITHOUT OF LIMITS IAW A319 SRM 53-00-15-283-001, RE PLACED PER NEW FLOOR BEAM P/N: D5311278220201 BATCH 0003778671, INSTNov 12, 2021 · N838UA · Airbus A319131SDR FDEA202111112917None · gougedMDCC SEAT TRACK CROSS BEAM ADAPTER FND GOUGE AT FR54 BTN Y-1959 AND Y-2452 REMOVED THE DAMAGED CROSS BEAM AND INSTALLED THE NEW CROSS BEAM I.A.W A300-600F SRM 51-72-10-001 PAGE2 AND 51-40-21-001 PARA7 PAGE24-PAGE50.Nov 11, 2021 · N685FE · Airbus A300*SDR 2022F00118Skin · chafedCHAFE ON THE FUSELAGE SKIN FROM THE CROSS-OVER VALVE.Nov 11, 2021 · N639QS · Cessna 680ASDR 2A6R2021111162101Frame · chafedDURING INSPECTION, CHAFE DAMAGE WAS NOTED TO THE AFT BOX BEAM UPPER FRAME INSIDE SKIN (PN: B533K3606-205) IN THE FORM OF CHAFING MEASURING TO BE APPROXIMATELY 0.70” LONG AND 0.020” DEEP FOR BOTH LOCATIONS. THE DAMAGE WAS REPAIRED VIA REPAIR DOUBLERS TO REINFONov 11, 2021 · N146HC · Bolkms BK117C2SDR JR2R2021111112110Floorbeam · corrodedMAIN CABIN FLOOR BEAM IS CORRODED OUT OF LIMITS AT FR85 AND RBL9 AREA. REPAIRED BEAM BY REPLACING DAMAGED SECTION IAW EMBRAER ETD2021-170-037328Nov 11, 2021 · N82338 · Emb ERJ170200LRSDR SWIA202163862None · corroded* LH EMER. DOOR LOWER SILL STEP PLATE CORRODED IN MULTIPLE SPOTS (MARKED). (C CHECK RO 1/16/2022) REMOVED AND REPLACED CORRODED LH EMER. DOOR LOWER SILL STEP PLATE WITH NEW ONE REF. CRJ-700 SRM 51-41-02-001-001-A01. SEE CONTINUE CARD FOR DETAILSNov 10, 2021 · N770SK · Cndair CL600*SDR SWIA202163837None · corroded* AFT CARGO DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C CHECK RO 1/16/2022) REPLACED AFT CARGO DOOR LOWER SILL REF CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01, AND DWG MM670-35085 REV J. COMPLIED WITH TASK CARD Nov 10, 2021 · N770SK · Cndair CL600*SDR V6NA2021111001Web · crackedDURING SCHEDULED INSPECTION, DISCOVERED 1.5 INCH CRACK RUNNING LONGITUDINALLY ON RIGHT SIDE OF NOSE LANDING GEAR WHEEL WELL THROUGH EXISTING FASTENER HOLES, START AND STOP. CRACK LOCATION WAS OUTSIDE THE PRESSURE VESSEL. DAMAGE AREA WAS REMOVED AND ALUMINUM FLNov 10, 2021 · N367LJ · Lear 60LEARSDR R61A2021120400981Intercostal · corrodedCORROSION ON INTERCOSTAL AFT OF HOT DRAIN MAST INTERNAL SIDE OF FUSELAGE FROM FR 86-87 STGR 26R - 25R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAME 86-87 BETWEEN STRINGER 26R - 25R REF SRM 51-40-08.Nov 10, 2021 · N121HQ · Emb ERJ170200LRSDR R61A2021120400980Intercostal · corrodedCORROSION ON INTERCOSTAL FWD OF HOT DRAIN MAST INTERNAL SIDE OF FUSELAGE FROM FR 86 - 87 STGR 26R - 25R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAME 86-87 BETWEEN STRINGER 26R-25R REF SRM 51-40-08. SEE WIPS AND TASKS FOR WORK PERFORMEDNov 10, 2021 · N121HQ · Emb ERJ170200LRSDR R61A2021120400972Shear Tie · corrodedCORRODED SHEAR CLIP AND HARDWARE AT FR 87 , STGR 27R - 28R AS MARKED. CORRODED SHEAR CLIP AND HARDWARE AT FR 87 , STGR 27R - 28R AS MARKED. EVALUATED SHEAR CLIP AND HARDWARE AT FR 87, STGR 27R -28R REF SRM 51-40-03AND FOUND SHEAR CLIP TO HAVE 100% MATERIAL LNov 10, 2021 · N121HQ · Emb ERJ170200LRSDR R61A2021120400971Shear Tie · corrodedCORRODED SHEAR CLIP AT FRAME 90, STGR 29R - 28R. REMOVED SHEAR CLIP AT FRAME 90, STGR 29R - 28R REF SRM 51-40-08 CORRECTIVE ACTION INSTALLED NEW SHEAR CLIP AT FRAME 90, STGR 29R - 28R REF SRM 51-40-08 APPLIED PRIMER, TOP COAT AND CIC REF EMB SRTM 51-23-05, 5Nov 10, 2021 · N121HQ · Emb ERJ170200LRSDR R61A2021120400970Shear Tie · corrodedCORRODED SHEAR CLIP AT FR 76, STGR 29R -29L AS MARKED. REMOVED AND REPLACED SHEAR CLIP AT FR 76, STGBR 29R - 29L REF : EMB 175 SRM 51-40-08Nov 10, 2021 · N121HQ · Emb ERJ170200LRSDR R61A2021120400969Shear Tie · corrodedCORRODED SHEAR CLIP AND HARDWARE AT FR 88, STGR 27R - 28R AS MARKED. REMOVED AND REPLACED SHEAR CLIP AT FR - 88 OTBD OF STGR 28 REF SRM 51-40-08. INSTALL WAS COMPLIED WITH ON WO H8297 SN 688.Nov 10, 2021 · N121HQ · Emb ERJ170200LRSDR JJBA20211110019None · noneRH FLOOR SILL FROM FR 65-68 HAS SIGNS OF CORROSION. REMOVED AND REPLACED DAMAGE SILL AT FR 65-68 RH SIDE,Nov 10, 2021 · N11193 · Emb EMB145XRSDR JJBA20211110018None · noneFLOOR BEAM DOUBLERS LOCATED AT STGR 15R BETWEEN FRM 20 & 22 SHOW SIGNS OF CORROSION ON HARDWARE HOLES. BLEND OUT CORROSION DOUBLER AT FR 22 FOUND TO BE IN LIMITS AND RESTORED FINISH. REMOVED AND REPLACED DOUBLER AT FR 20 RH.Nov 10, 2021 · N11193 · Emb EMB145XR
Back to JASC 5300