JASC 5340
Service difficulty reports · 22,406
Reports filed under 5340 · Fuselage Main, Attach Fittings, 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 = '5340' 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.
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 = '5340' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HNAA2023051900167Unknown · unknownE970489 SSI 53-20-11 LAVATORY RH BEAM GUSSET HAS NUMEROUS SPOTS OF CORROSION. R&R'D GUSSET IAW EMB145 SRM 51-40-02SDR SWAA2023051528467Attach Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION1.;[03] REMOVED DAMAGEDSDR AALA202307122517Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING CENTER POST LOWER RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 344136.SDR AALA202307123820Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING CENTER POST LOWER LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 344136.SDR SWAA2023050927757Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT ACB BS827 LBL6 WL157.<[01] FOUND TO BE WITH NO LIMITS PER SRM 53-00-53-1A2;[02] REMOVED STRINGER CLIP IAW SRM 51-40-02;[03] RECEIVED NEW STRINGER CLIP LOCATED AND DRILLED<BR>AT ACB BS827 LBL6 WL 157<BR>P/N 146A1010-10 LOT# 1478113SDR SWAA2023050927751Attach Angle · corrodedCORROSION ON INTERCOSTAL TO WEB ATTACH ANGLE BS767+2; 767+5; 767+9; 767+16; 767+19 RBL21 WL156.<[01] FOUND TO BE OUT OF LIMITS EXFOLIATED CORRODED WITH MORE THE 50 % OF MATERIAL LOST IWA B 737-700 SRM 53-60-15 REMOVED DAMAGE PART PER SRM 51-40-02;[02] SRM 53-6SDR SWAA2023050927758Attach Angle · corrodedCORROSION ON ATTACH ANGLE AT ACB BS727E LBL7 WL152.<[01] FOUND TO BE WITH NO LIMITS IAW SRM 53-00-53-1A-2;[02] PART TO BE REPAIR BY REPLACEMENT PEER SRM 51-10-02 PARAGRAPH 9.C;[03] REMOVED ATTACH ANGLE AT ACB BS 727E LBL7 WL 152 IAW SRM 51-40-02;[04] RECEIVED SDR SWAA2023050827765Attach Angle · crackedFWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500A FWD SIDE LBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER SSDR SWAA2023050827766Attach Angle · crackedFWD CARGO BAY BAFFLE ATTACH ANGLE CRACKED BS500B FWD SIDE RBL25 WL155.<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL;FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEMENT;PER SSDR SWAA2023053127371Angle · crackedCRACK INTERNAL AREA RT SIDE BODY STA 663.75 SUPPORT ANGLE AT AIR CONDITIONING BAY 2023-257905<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 14SDR SWAA2023050926302Web · crackedINTERNAL - HORIZONTAL PRESSURE DECK WEB STA 663 TO STA 675 - LBL 30 TO LBL 45. MULTIPLE CRACKS NOTED. MARKED AREAS.<[01] SRM 53-40-51-2R-2 REPAIR 2 IS APPLICABLE TO THIS A/C;[02] CUT AND REMOVED THE DAMAGED PART OF WEB IAW SRM 53-40-51-2R-2 REPAIR 2 STEP 4C(3)SDR SWAA2023051724711Floor Support · crackedCRACK ON PASSENGER CABIN FLOOR SUPPORT AT BS 540 LBL 2 WL 208.<[01] REMOVED PANEL BREAK ASSY LOCATED AT B.S. 540; LBL 2; WL 208 PER SRM 51-10-02-0G-0 PARA: 4.C.(3) AND SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED PANEL BREAK ASSY PER SRM 51-40-05-0G-0; SRM 51-40SDR IPXA2023050193052Stringer Clip · brokenINSPECTION TYPE:DI*SUPPLEMENTAL SDR* *FILED AGAINST INCORRECT TAIL # PLEASE DISREGARD* STRINGER CLIP AT 18L STA 418 LOWER LEG BROKEN.REMOVED, FABRICATED, AND INSTALLED CLIP IAW SRM 51-40-02.SDR ASAA2023040542813Door Sill · corrodedSHAPE SILL CORRODED BEYOND LIMITS AT R2 DOOR. (REF G1724557 HAECO CARD 28057) GROUNDED - YES. NEW SHAPE SILL RECEIVED IAW A320 IPC 53-41-69-02-A, EA A320-53EA-01730. REPLACEMENT ACCOMPLISHED ON CUSTOMER CARD G1724552 (HAECO OPS 28052).SDR WX0A1900010031752Unknown · unknownNRC 1000-0128: S/M (338-29) DURING REMOVAL OF LOWER SILL BEAM (FOR REPLACEMENT) AT BULK CARGO DOOR, CORROSION FOUND AT UPPER FLANGE ON FRAME 62 AND STR 38R/AR BULK CARGO DOOR SURROUND AREA, CORROSION ON FR62,STR38R, REPAIRED AS PER AIRBUS DOSSIER 81200977, REPSDR GTIA2023040637100Web · cracked"CRACKED WEB FAIRING SUPPORT AT FUSELAGE STATION FR.. 49 AND STR. 27R
RAF-01 3069143-02 GENERATED-PERFORMED PERMANENT REPAIR ON SUPPORT WEB BELLY FAIRING AT LEVEL FR 49 RH SIDE LOWER FUSELAGE IAW A320 SRM 53-45-12-300-010 THIS REPAIR IS CATEGORY A"SDR 8G9R20230406001Stop · missingCO-PILOT FWD SEAT STOP ON OUTBOARD SEAT TRACK NOT INSTALLED.SDR SWAA2023042823696Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS663+28 LBL1 WL206.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT BS 663+28 LBL 1 WL 206 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIMITS GIVEN PART REPARABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC 9.;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2023042823697Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS663+28 RBL1 WL206.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT BS 663+28 RBL 1 WL 206 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIMITS GIVEN PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC .9 REMOVED ATTACH ANGLE AT BS 663SDR SWAA2023042823699Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS663+29 LBL23 WL203.<[01] REMOVED CRACK DAMAGED ATTACH ANGEL AT MID CABIN BS 663+29 LBL 23 WL 203 IAW SRM 51-40-02-0G-0 NO DAMAGE LIMITS GIVEN IN SRM PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC 9.;[02] VERIFIED CSDR SWAA2023042823698Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS663+29 RBL23 WL203.<[01] REMOVED CRACK DAMAGED ATTACH ANGLE AT MID CABIN BS 663+29 RBL 23 WL 203 IAW SRM 51-40-02-0G-0 NO SRM DAMAGE LIMITS GIVEN PART REPARABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 SEC 9.;[02] VERIFIED CORRESDR CALA2023040401037Flange · crackedWHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 O REACHES 49,948 TOTAL FLIGSDR AALA202306223482Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU RIGHT HAND LOWER LATERAL FORK END FITTING WORN AND BUSHING HAS MIGRATED AT FR 24 AT S32R. REPLACED FORK END FITTING PER EA 343789.SDR AALA202306228316Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU LEFT HAND LOWER LATERAL FORK END FITTING WORN AND BUSHING HAS MIGRATED AT FR 24 AT S32L. REPLACED FORK END FITTING PER EA 343789.SDR YENA2023033000292Unknown · unknownDURING HEAVY MAINTENANCE: CRACK ON STRG 10R AT FR 73 AT CENTER FUS INTERNAL STRUCTURE; STRG 10R AT FR 73 AT CENTER FUS II INTERNAL STRUCTURE WAS REPLACED PER EMB-190 SRM 51-43-02 AND SRM 51-43-01.'SDR SWAA2023042521496Panel · crackedCRACKED BREAK PANEL STA 540; LBL 1; WL 208<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART;[02] REMOVED DAMAGED BREAK PANEL AT STA 540 LBL 1; WL 207 IAW SRM 51-40-02-0G-0.;[03] LOCATSDR AALA202304035199Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX SHEAR FITTING ABOVE FORWARD UPPER SPAR LOCATED AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER SRM 51-40-02-0G AND EA 343131A.SDR AALA202304035138Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX SHEAR FITTING ABOVE FORWARD UPPER SPAR LOCATED AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER SRM 51-40-02-0G AND EA 343131A.SDR P5CA2023032600006Unknown · unknownLOGPAGE 1669079 ITEM 6, AIRCRAFT WAS STRUCK BY A CARGO CONTAINER @ APPROX STATION STRINGER 44 AFT OF CARGO DOOR(<P>LOGPAGE 1669079 M6: EVALUATING DAMAGE AT STA 2100 TO STA 2120 STR 44 AFT OF BULKHEAD CARGO DOOR; REMOVED "BKND-OUT" GOUGE AT FUSELAGE AND ELEVATESDR SWAA2023041924744Panel · crackedLOWER FUSELAGE CENTER AFT ACCESS PANEL # 194E HAS SEVERAL FASTENER HOLES BULGING/CRACKED<[01] ACCOMPLISHED REPAIR OF PANEL 194E; REF: B737 SRM 51-70-06-2R-9;[02] VERIFIED REPAIRSDR DALA2023032702329Unknown · unknown(LOG 2685512) DURING INSPECTION FOUND BUSHING CORRODED, FWD TRUNNION IB FITTING, IB AND OB SIDE. REPAIRED PER B737-900 SRM 57-20-90.SDR CALA2023032700872Frame · cracked(AD 2022-15-05) DURING HFEC INSP OF THE RH FR68. CRACK INDICATION WAS NOTED ON UPPER AND LOWER STGR22 WEB, HORIZONTAL FLANGE RADII. CRACK LENGTH APPROX. OF .852" ON UPPER SIDE AND .959" ON LWR SIDE. CRACK ENDS MARKED IN RED. CONTACT ENGINEERING FOR REPAIR INSDR FDEA202303240499Longeron · crackedAFT FUSELAGE - WHILE CARRYING OUT AGING REPAIR AT STATION 2140 (REFERENCE SNRM N01163) FOUND LONGERON 33 RIGHT FASTENER HOLE CRACKED. CRACKED LONGERON 33 RIGHT FASTENER HOLE AT AFT FUSELAGE STATION 2140 (REFERENCE SNRM N01163) REPAIRED AS PER EA # 1-5330-TSDR SWAA2023041317946Panel · crackedCRACKED BREAK PANEL STA 540; BL 0- LBL 25; WL 208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART;[02] REMOVED DAMAGED BREAK PANEL AT STA 540 BL0- LBL25; WL 207 IAW SRM 51-40-02-0G-SDR SWAA2023041917580Bracket · crackedAFT CARGO WATER TANK SUPPORT BRACKET CRACKED STA 947 LBL 10. (MARKED)<[01] REMOVED AFT CARGO WATER TANK SUPPORT BRACKET PER SRM 51-40-02.;[02] INSTALLED NEW AFT CARGO FITTING PART #149A8113U6 IAW SRM 51-40-02;[03] VERIFIED C/A #2.SDR AALA202305123431Attach Fitting · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD ATTACH FITTING HAS MIGRATED BUSHING ON THE FORWARD LUG AT FR 43 AND Y254. REPLACED LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FORWARD FITTING PER EA 344171SDR SWAA2023042826086Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE RBL42 HAS CRACK<[01] REMOVED AND INSTALLED NEW FABRICATED ATTACH ANGLE AT VAPOR BARRIER ON RBL 42 AT STA 663 AS PER REPAIR REFERENCE SRM 51-10-10-2R-5 AND DW 111A1000.;[02] VERIFIED REPAIRSDR SWAA2023042826087Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE LBL42 CRACK<[01] REMOVED; FABRICATED AND INSTALLED NEW REPAIR AT VAPOR BARRIER ATTACH ANGLE ON STA 663 LBL42 AS PER REPAIR REFERENCE (SRM 57-10-10-2R-5) AND DW 111A1000.;[02] VERIFIED REPAIRSDR WX0A1900010031742Unknown · unknownNRC 1000-0005: (S/M 141-2) AFT CARGO COMPARTMENT, CORROSION FOUND ON STRINGER 44 BTW FR 64-65./AFT CARGO COMPARTMENT, STRINGER 44 BTWN FR 64-65 REPAIRED AS PER SRM 53-41-13-300-004 REV144. PERMANENT REPAIR CATEGORY ""A"". NO FURTHER ACTION REQUIRED. SEE NDT RESDR SWAA2023041915035Shear Tie · crackedSHEAR TIE (P/N 144A7716-8) FOR RIGHT HAND PRESSURE DECK ASSY IS CRACKED<[01] VERIFIED PART USING PART NUMBER 144A7716-8 AND ATAG A171211;[02] AND USING DWG -4 144A7730 REV C<BR> (EDIT FROM ABOVE);[03] VERIFIED STEPS 1 & 2;[04] LOCATED AND DRILLED SEAR TIE IWA SDR ASAA2023030942525Track · corrodedAFT PIT RH CARGO TRACK IS CORRODED BETWEEN STA 787-807. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED CARGO TRACK FROM STA 887 TO STA 767 IAW B737-800 SRM 53-00-53-2R-3W=1 O=.072 R=.059 L=2 D=.033.SDR ASAA2023030942523Cargo Track · corrodedAFT PIT RH CARGO TRACK IS CORRODED BETWEEN STA 787-807. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED CARGO TRACK FROM STA 887 TO STA 767 IAW B737-800 SRM 53-00-53-2R-3W=1 O=.072 R=.059 L=2 D=.033.SDR SWAA2023033013013Web · crackedSTA 867 FRAME WEB IS CRACKED 3' BELOW STRINGER S-8R; AT BIN RAIL FITTING.<[01] WILL BE ACCOMPLISHED ON CUSTOMER FAULT TTG8Q00JBFXZ.;[02] VERIFIED CORRECTIVE ACTION 1;[03] ALL STEPS COMPLETESDR CALA2023030600631Flange · crackedDURING HMV4 VISIT AT BFM ACCOMPL''G EA5341-01231 (B) CRACKS WERE FOUND AT FR68 LH STGR 22 WEB HORIZ FLANGE UPPER & LWR BOTTOM RADIUS. ADDITIONALLY, WHILE ACCOMPL''G EA5340-01724(C) OP2 A CRACK WAS NOTED AT FR68 LH DOOR STOP FITTING #1 WORK ACCOMPLISHED ON VTAESDR WX0A2023032031738Unknown · unknownNRC 2000-0070: CRACK FOUND ON FRAME 68 LH SIDE AT DOOR STOP FITTING #6, LOWER INBOARD HOLE. / ON FRAME 68 LH SIDE AT DOOR STOP FITTING #6, LOWER INBOARD HOLE PERMANENTLY REPAIRED AS PER SRM 53-41-12-300-010 REV. 144. REPAIR MAJOR CATEGORY B. FUTURE AIRCRAFT INSDR IPXA2023032392177Fitting · gougedINSPECTION TYPE:C3RCB WALL FITTING #12 IS GOUGED AT STATIC STRAP ATTACHMENTREPAIRED #12 RCB WALL FITTING IAW VTSAA EA 011-5340-01-A9876 I/R DATED 03/20/2023 (MINOR)SDR IPXA2023032392169Fitting · gougedINSPECTION TYPE:C3RCB WALL FITTING # 6 IS GOUGEDREPAIRED # 6 FITTING IAW VTSAA EA011-5340-01 A9872 REV I/R AND UPS EOMD11-5340-862276-A.(MINOR)SDR IPXA2023032392168Fitting · gougedINSPECTION TYPE:C3RCB WALL FITTING # 13 IS GOUGED AT STATIC STRAP ATTACHMENT.REPAIRED # 13 RCB FITIING IAW VTSAA EA 011-5340-01-A9875 I/R DATED 03/20/2023. (MINOR)SDR IPXA2023032392167Fitting · gougedINSPECTION TYPE:C3RCB WALL FITTING #11 IS GOUGED AT STATIC STRAP ATTACHMENT .REPAIRED #11 POSITION RCB WALL FITTING IAW VTSAA EA 011-5340-01-A9877 IR DATED 03/22/2023 AND UPS EO MD11-5340-86275-A (MINOR)SDR IXXA2023040102Bulkhead · cracked2E CRACKS WERE DETECTED ON THE R/H FORWARD OUTER CHORD I/B FLANGE AT BS 1809.5 BULKHEAD WHILE ACCOMPLISHING INSPECTION PER T/C ATI-53-767-05111. PERMANENT REINFORCING REPAIR WAS INSTALLED PER EO NO. 53-767-5111 REV 05.
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