JASC 5340
Service difficulty reports · 22,405
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 SWAA2024081309164Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 9; WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 9 WL 208 PER SRM 51-10-02-0G-0 PAR 9 AND BOEING DWG 143A5400;[02] REMOVED AND REPLACED INTERCOSTAL UPPER ATTACH ANGLE SSDR VNAA202408090010Attach Angle · corrodedCORROSION ON ANGLE ATTACHED TO STRINGER 26LH (2EA) IN STA. FS= 349 TO FS= 364 AT MAIN AVIONICS COMPARTMENT.(E/E) WA REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND ANGLE ATTACHED TO STRINGER 2SDR YENA2024071100954Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON FITTING BTW FR13- FR14 INTERNAL STRUCTURE LOWER AREA ON LH AVIONICS COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00051) REF AEROMAN NR 2024-298984 WO# 2024-177/1 REMOVED AND REPLACED FITTING AND FASTSDR SWAA2024072308440Bracket · crackedL/H A/C BAY FWD DUCT BRACKET JUST OBD OF KEEL BEAM BOX CRACKED (MARKED)<[01] REMOVED; AND REPLACED BRACKET IAW. SOPM. 20-50-01.;[02] VERIFIED WORK PERFORMED.SDR DALA2024070806838Attach Fitting · wornWHILE PREFORMING AMDS WORK CARD 2515-01014-02A NOTED LT LOWER ATTACHMENT FITTING SHOWING SIGNS OF WEAR. REPAIRED PER ERA 619027-14AD REV. ORIG. SEC I RII COMPLETE.SDR DALA2024070806837Attach Fitting · damagedWHILE PREFORMING AMDS WORK CARD 2515-01014-02B FOUND RH LOWER ATTACHMENT FITTING HOLE ELONGATED. REPAIRED PER ERA 619027-14AD REV ORIG. SEC I. RII COMPLETE.SDR SWAA2024072907628Attach Angle · corrodedUPPER WEB ATTACH ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 HAS CORROSION AT STA 946.<[01] REMOVED CORROSION UPPER WEB ATTACH ANGLE LOCATED BETWEEN STA?S 927-947; RBL 25 . ORIGINAL THICKNESS OF 0.070; MATERIAL REMOVED .019; REMAINING THICKNESS IS 0.051. ANGLE SDR DALA2024070506773Attach Angle · cracked(LOG 0423436) CRACK IN VAPOR BARRIER ATTACH ANGLE THRU FUEL TANK AT STA 663 WL 176 RBL 11. REPAIRED VAPOR BARRIER ATTACH ANGLE THRU FUEL TANK AT STA 663 WL 176 RBL 11 IAW ERA/619038-14 REV ORIGINAL.SDR SWAA2024081211973Bracket · crackedCRACK ON LT FORWARD BRACKET AT P5 OVERHEAD COCKPIT PANEL 2024-414779<[01] REPLACE LT FORWARD BRACKET AT P5 OVERHEAD COCKPIT PANEL IAW B737-800 SRM 51-40-02;[02] REPLACE LT FORWARD BRACKET AT P5 OVERHEAD COCKPIT PANEL IAW B737-800 SRM 51-40-02SDR HNAA2024090400220Bracket · crackedLH SIDE AT FRAME 46 CLOSING ANGLE BRACKET FOUND CRACKED JUST UNDER FLOOR LEVEL.SDR AALA202407084490Attach Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD ATTACH RAIL ASSEMBLY AT STA 500I FROM LBL 25 TO RBL 25. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.SDR DALA2024062706573Fitting · corrodedAIRCRAFT 9524, CORROSION ON MAIN FRAME FITTING STAY=560 L18L AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2. MAIN FRAME FITTING STAY= 560 L18L AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-01-0G AND SRM 51-41-05-0G. (LP 0414381)SDR VNAA202406230013Stringer Clip · corrodedFOUND CORROSION ON STRINGER CLIP AT STR 18R AT FS 1000SDR VNAA202406230007Stringer Clip · corrodedSTGR 19R CLIP IS CORRODED AT FS 1000.00SDR IPXA2024070258045Fitting · crackedR/H FRONT SPAR THE INERCOSTAL LUG FITTING AT RBL 11.33 STA 1000 REMOVED BOTS AT STA 1000. CKD NORMAL. REMOVED TUBE. CKD NORMAL IAW IPC 57-14-01-01A.SDR IPXA2024070257995Fitting · crackedL/H FRONT SPAR THE INTERCOSTAL LUG FITTING AT LBL 11.30, STA 1000.REMOVED AND REINSTALLED THE BOLTS AND TUBE AT STA 1000. CONDITIONS WERE NORMAL IAW AMM 20-11-28-964-010SDR R61A2024062100282Nut Plate · corrodedCORROSION FOUND ON CF111 AFT CARGO BILGE NUT HOLDER BTWN FR 76-77 STR 29R-STR29L. MADE REPAIR PART TECH DRAWING PN 170-85396-401 IAW SRM 51-41-02.SDR AALA202406217310Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406210018Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406212984Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406213499Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406213808Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406218771Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202406215853Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR SWAA2024080703635Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] REMOVED AND REPLACED B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE L.B.L. 6-70; W.L. 165. IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV.-;111A7000 REV.A AND 111A10SDR SWAA2024071803194Fitting · crackedCRACK FOUND AT RH BS 727 STRINGER 18A AFT UPPER FITTING LOWER FASTENER HOLE; CRACK DIRECTION 3 O'CLOCK; CRACK DEPTH 0.030 CRACK FOUND AT RH BS 727 STRINGER 18A AFT UPPER FITTING LOWER FASTENER HOLE CRACK DIRECTION 3 O'CLOCK CRACK DEPTH 0.030'.<[01] ***SUMMARY*SDR IPXA2024062705848Tee Angle · corrodedL/H LOWER FUSELAGE BETWEEN STA. 1200-1260 T-CORD HAS CORROSION INSTALLED T-CHORD L/H FUSELAGE BETEWEEN STA 1200- 1260 IAW SRM 51-40-02.SDR SWAA2024071802382Fitting · crackedCRACK FOUND AT LOWER FASTENER OPEN HOLE OF BS 727 INNER CHORD AT STRIMGER 18A R/S.<[01] FAULT TO BE RESOLVED ON ITEM # TTG8Q00U011U.;[02] CORRECTION TO READ FAULT TO BE RESOLVED ON ITEM # TTG8Q00U1GHG.;[03] VERIFIED STEP 2 FAULT WILL BE RESOLVED ON TTG8Q00U1GHSDR SWAA2024071802524Fitting · crackedCRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT 2024-393287<[01] REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT IAW B737-700 SRM51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 TOOK MEASURE OF CRACK IS : SDR SWI2024F01107Fitting · corrodedFORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED FITTING (LBL24) (SH670-33390-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED CLOSED)FORWARD BAGGAGE BAY, INTERNAL STRUCTURE, MACHINED FITTING AT LBL24 (SH670-33390-1) REPLACED IAW CRJ 700 SRM 51-42-SDR SWI202408260788Fitting · gougedTHE RH MLG SIDE STAY FITTING IS GOUGED ON THE INBD SIDE. (MARKED) (C-CHECK RO 8/24/2024) REPAIRED THE RH MLG SIDE STAY FITTING ON THE INBD SIDE BY COMPLYING WITH REO 690-57-11-128 REV -- DATED 2024-07-14, COMPLIED WITH 51-900-1002-SKYSDR SWAA2024070201770Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 160.<[01] STEPS 6 AND 8 COMPLETE;[02] REPAIRED UPPER ATTACH ANGLE BS663 RH PER SRM 57-10-10-2R-5- REPAIR 5 AND EA 24-157-01651 REV A;[03] VERIFIED.;[04] THE DAMAGE WAS REPAIRED PER 737-700 SSDR 2A6D20240614001Attach Angle · crackedDAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DAMAGE MEASURED TO BE APPROXIMATELY 0.13” IN DIAMETER.SDR AALA202407117001Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING LOWER INBOARD HOLE AT FR 16 LEFT AND DOOR STOP FITTING #1. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.SDR SWAA2024070101542Attach Angle · crackedCRACKED ATTACH ANGLE AT MID CABIN BS690 RBL1 WL206. MARKED<[01] REMOVED ATTACH ANGLE AT MID CABIN BS 690 RBL1 WL206 P/N 273A9112-48 IAW SRM 51-40-02.;[02] COMPLETED STEP 2;[03] COMPLETED STEP 3; STEP 1 IS COMPLETE; VERIFIED ALL STEPS COMPLETESDR SWAA2024071800913Attach Bracket · crackedRIGHT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM CRACKED B.S. 540+5' RBL' 6'. (DOT 51-002)<[01] REMOVED AND REPLACED RIGHT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM REF B-737 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEDSDR SWAA2024071800912Attach Bracket · crackedLEFT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM CRACKED B.S.540+5' LBL. 6'. (DOT 51-001)<[01] REMOVED LEFT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM REF B-737 SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED LEFT A/C BAY PNEUMATSDR SWAA2024070201106Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 160.<[01] REPAIRED UPPER ATTACH ANGLE BS663 LH PER SRM 57-10-10-2R-5- REPAIR 5 AND EA 24-157-01650 REV A;[02] VERIFIED.;[03] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 57-10-10-2R-5 (REPAIR 5)SDR UIEA2024050600337Fitting · chafedM/D STA 1000 RBL 11" INTERCOSTAL LUG FITTING FASTENER HOLE CHAFING(<P>CHAFING INTERCOSTAL LUG FITTING REPLACEMENT AS PER IAI DWG: 366-53-15-A2614 SHT.1 ISSUE J. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024050600338Fitting · chafedM/D STA 1000 LBL 11" INTERCOSTAL LUG FITTING BOLT HOLE CHAFING(<P>CHAFING INTERCOSTAL LUG FITTING REPLACEMENT AS PER IAI DWG: 366-53-15-A2614 SHT.1 ISSUE J. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024061000512Fitting · damagedFITTING FOUND 2EA FASTENER HOLES S.E.M.(<P>S.E.M. CONDITION ACCEPTED AS PER RI-53-00-16880 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR SWI202408260753Fitting · corrodedCORROSION ON FLOORBEAM FITTING AT STGR 18L, FS 349.00 (C-CHECK RO 8/24/2024) REPLACED FLOOR BEAM FITTING AT FS 349.00 STR 18L REF DWG # SH670-32120 REV AL AND DWG #SH670-31810 REV AE CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-06-001-001-A01, CRJ9SDR SWI202408260759Nut Plate · corrodedCABIN INTERIOR CORROSION FS565.00 STGR22L MOUNT PLATE AT NUT PLATES AS MARKED (C-CHECK RO 8/24/2024) REPLACED FWD CARGO DAMAGED BRACKET SH670-33390-2 LOCATED AT FS565.00 ON STGR22L. INSTALLED NEW BRACKET P/N: SH670-33390-2 REF CRJ-900 SRM 51-42-22-001-SDR IPXA2024062245622Adapter · brokenMAIN DECK CLS ADAPTER AT FR 33 BETWEEN SEAT TRACK Y2462 AND Y1959 IS BROKEN DOT 06999-08. INSTALLED ADAPTER IAW A300 SRM 51-40-21 PARAGRAPH 7.SDR IPXA2024062245618Adapter · brokenMAIN DECK CLS ADAPTER AT FR 34 BETWEEN SEAT TRACK Y2462 AND Y1959 IS BROKEN DOT 06999-09. INSTALLED ADAPTER IAW SRM 51-40-21 PARAGRAPH 7.SDR SWAA2024071698887Bracket · crackedCRACK ON BRACKET LOCATED BS 867 BTW STR 2R TO SR 3R AT PASSENGER CABIN 2024-357506<[01] REPLACED BRACKET LOCATED BS 867 BTW STR 2R TO SR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 146A7901 REV -: AND MEASURE OF CRACK IS: L: 0.500 INCHSDR SWAA2024062597988Attach Bracket · cracked(A204 DOT 19) AFT CARGO. STA 867; LBL 12; LAV BULKHEAD SUPPORT ATTACH BRACKET IS CRACKED AT CARGO FLOOR; FLOOR LINE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-D00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>TAG: A2425SDR SWIA202408130673Tie Down · corrodedFORWARD BAGGAGE BAY CARGO TIEDOWN PAD AT FS581.00 BETWEEN STGR23L AND STGR22L CORRODED AS MARKE (C-CHECK RO 8/11/2024) REMOVED FROM FORWARD BAGGAGE BAY CARGO TIEDOWN PAD ( BRACKET ) AT FS581.00 BETWEEN STGR23L AND STGR22L REF. CRJ-700 SRM 51-42-21-001-0SDR SWAA2024062797233Stringer Clip · crackedFWD CARGO COMPARTMENT FLOOR STRUCTURE AT STA 500I AND RBL 21; HAS STRINGER CLIP UNDER SIDEPLATE CHANNEL WITH CRACKS ORIGINATING FROM FASTENER. (MARKED)<[01] REMOVED FASTENERS; REMOVED RH TRANSITION ANGLE FROM STA 500D+10 TO STA 500I TO FOM PER SRM 51-40-02.<BRSDR SWAA2024062796967Stringer Clip · crackedFWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT BOTH FRAME RIVETS; STA 500I STR 25R. HFEC VERIFIED.<[01] REMOVED AND REPLACED IAW SRM 51-40-02 AND SRM 51-40-05.;[02] C/W INSPECTION
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