JASC 5300
Service difficulty reports · 8,204
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.
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
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 IXXA2023070202Seal Depressor · damagedMCD CUTOUT FORWARD LOWER CORNER DAMAGEDSDR IXXA2023070201Seal Depressor · damagedMCD CUTOUT AFT LOWER CORNER DAMAGEDSDR HNAA2023080700300Unknown · unknownE983801 SSI 53-30-03 CORROSION ON SHEAR CLIP AT BAGGAGE DOOR CUT-OUT AT FRAME 65 PREVIOUS REPAIR. REMOVED AND INSTALLED SERVICEABLE SHEAR CLIP AT BAGGAGE DOOR CUTOUT AT FRAME 65 IAW EMB 145 SRM 53-31-04 AND PIEDMONT EO1-53-23-0194.SDR HNAA2023080700299Unknown · unknownE983799 SSI 53-30-03 CORROSION ON SHEAR CLIP AT BAGGAGE DOOR CUT-OUT AT FRAME 68 PREVIOUS REPAIR. REMOVED AND INSTALLED SERVICEABLE FRAME 68 SHEAR CLIP LOWER SECTION IAW EMB 145 SRM 53-31-04 AND PIEDMONT EO1-53-23-0193.SDR NACA202307070027Unknown · unknownHFEC INSPECTION FOUND 01 EA CRACK OF LEFT BS883.5 FRAME INNER CHORD TRANSITION RADIUS AT LBL 89 BELOW WL200,IT IS ABOUT 0.2 INCH LONG. CARRIED OUT THE REPAIR AT LH FRAME INNER CHORD OF BS 883.5 LBL89 BELOW WL200 AS PER SB 767-53A0209 REV. 2 JUNE 07, 203.SDR NACA202307070018Unknown · unknown- CORROSION FOUND ON THE KEEL BEAM T CHORD AROUND STA1003 BETWEEN LBL9 AND RBL 9. REPLACED THE DAMAGED T CHORD ON THE KEEL BEAM STA 1003 BETWEEN LBL9 AND RBL9 AS PER B767-300 SRM 51-40-05 REVISION NO.122 - APR 15/2023SDR NACA20230707012Unknown · unknownFOUND THE FWD CARGO LOWER DOOR CUTOUT A SUPPORT CORROSION AT STA487.67,RBL38 TO RBL 41. REMOVED AND REPLACED THE DAMAGED SUPPORT AT FWD CARGO LOWER DOOR CUTOUT STA 487.67 RBL38 TO RBL41 AS PER B767-300 SRM 51-40-02 REVISION NO. 122 APR 15/2023.SDR NACA202307070012Unknown · unknown- PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN ABOUT 1.5" AFT OF STA132 AND LOOKING AFT AT 1 O'CLOCK. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.080", THE
DEPTH OF CLEANUP X=0.004" <15%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 5SDR NACA202307070011Unknown · unknownPITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN BETWEEN STR26R AND STR36R ,BETWEEN STA1832 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.071", THE DEPTH OF CLEANUP X=0.003" < 15% T. FOUND WITHING LIMITS AS PER B767-300 SRMSDR NACA202307070010Unknown · unknownHFEC INSPECTION FOUND 01 EA CRACK ABOUT 0.3 INCH LONG OF THE RIGHT VERTICAL CHORD ON THE AFT BULKHEAD OF THE NOSE WHELL WELL AS MARKED .IT DOES NOT EXTENED BELOW WL159 AND REPAIR IAW BOEING 767-300 SRM 51-70-12. REPAIRED THE CRACKED RIGHT VERTICAL CHORD ON THESDR NACA202307070007Unknown · unknownSX NR 6500161718 - PITTING CORROSION FOUND ON THE UPPER SURFACE EXTERNAL SURFACE BETWEEN STR2L AND STR3L,FROM STA368 AND STA 390. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X=0.003" <10%T. FOUND WITHIN LIMIT AS SDR NACA2023070100004Unknown · unknownPITTING CORROSION FOUND ON THE UPPER SURFACE EXTERNAL SURFACE AROUND STR 2R, BETWEEN STA 368 AND STA 390 THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.071", THE
DEPTH OF CLEANUP X=0.005" <10%T. FOUND WITHIN LIMIT AS PER B767-300 SRM 53-00-0SDR NACA2023070100002Unknown · unknownSX NR 6500161617 - PITTING CORROSION FOUND ON THE FUSELAGE EXTERNAL SKIN AROUND STR26L ,BETWEEN STA1788 AND STA1809. THE CORROSION REMOVED AND MEASURED: THE ORIGINAL THICKNESS T = 0.056", THE DEPTH OF CLEANUP X = 0.002" < 15%, FOUND WITHIN LIMITS AS PER B767-3SDR NACA2023070100001Unknown · unknown- CORROSION FOUND ON THE KEEL BEAM T CHORD AROUND STA960 BETWEEN LBL9 AND RBL 9. REPLACED THE DAMAGED T CHORD ON THE KEEL BEAM STA 960 BETWEEN LBL9 AND RBL9 AS PER B767-300 SRM 51-40-05 REVISION NO.122SDR CALA2023070302141Lock Fastener · unknownPERFORM INSPECTION PER ECRA5310-08171 TO VERIFY REPAIR FASTENERS ARE INSTALLED AT STA727 & S-18A LHS & RHS. INSPECTION IS TO BE ACCOMPLISHED AT RFD DURING D1 CHECK. CARRIED BY ELB PERFORMED INSPECTION OF LH & RH LOWER FRAME PREVENTATIVE MOD IAW EC/RA 5310-081SDR HNAA2023080700298Unknown · unknownE983490 FRAME 22 CORRODED AT SERVICE DOOR CUT-OUT LOWER AFT CORNER. CUT, FABRICATED, DRILLED AND INSTALLED FR 22 REPLACEMENT SECTION BTW STGR 11R-18R AND L-ANGLE SPLICES IAW EMB 145 SRM 53-00-04 ITEM 17 FIGURE 209, ETD# ETD2023-145-017207, EO1-53-23-0196, ANDSDR HNAA202308040275Unknown · unknownE983559 CORROSION ON RH OTBD CROSS FLOORBOARD SUPPORT AT FRAME 53. REMOVED AND REPLACED R/H OTBD CROSS FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02SDR HNAA2023080400274Unknown · unknownE983530 CORROSION IN LAV AREA ON LH FLOOR SILL. : REMOVED AND REPLACED LH FLOOR SILL IN LAV AREA IAW EMB 145 SRM 51-40-02SDR HNAA2023080400273Unknown · unknownE983523 L/H #1 OUTBOARD FLOOR SUPPORT CORRODED MARKED. REMOVED AND REPLACED LH #1 OUTBD FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.SDR HNAA2023080400272Unknown · unknownE983504 CORROSION ON LH OTBD # 6 FLOOR SILL. RAR L/H OUTBD #6 FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR HNAA2023080400271Unknown · unknownE983502 CORROSION ON RH OTBD # 4 FLOOR SILL. RAR R/H OTBD # 4 FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR HNAA2023080400270Unknown · unknownE983499 CORROSION ON LH OTBD # 2 FLOOR SILL. RAR LH OTBD # 2 FLOOR SILL IAW EMB-145 SRM 51-40-02.
.SDR HNAA2023080400269Unknown · unknownE983494 CORROSION ON LH BEAM GUSSET # 5. : REMOVED AND INSTALLED NEW & SERVICEABLE L/H BEAM GUSSET #5 IAW EMB-145 SRM 51-40-02.SDR HNAA2023080400268Unknown · unknownE983491 CORROSION ON CENTER BEAM GUSSET # 4. REMOVED AND REPLACED CENTER BEAM GUSSET # 4 IAW EMB-145 SRM 51-40-02SDR HNAA223080400267Unknown · unknownE983486 CORROSION ON RH OTBD # 3 FLOOR SILL. : RAR R/H OTBD # 3 FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2023080400266Unknown · unknownE983484 CORROSION ON RH OTBD # 2 FLOOR SILL. RAR R/H #2 OUTB FLOOR SILL IAW EMB 145 SRM 51-40-02.SDR HNAA2023080400265Unknown · unknownE983483 CORROSION ON RH OTBD # 1 FLOOR SILL. RAR R/H OTBD # 1 FLOOR SILL IAW EMB 145 SRM 51-40-02SDR CALA2023063002106Coupling · corrodedAFT CARGO BILGE STR 43L ANGLE HAS CORROSION FR47/51. REMOVED AND REPLACED COUPLING P/N D5347100720490 BATCH# 00041310 38 RECEIVED. IAW. SRM 51-42-11/001, SRM 51-72-11-911-001, SRM 51 -49-00. EMP: V940362 WC: 58608 STA: ST ENG BFM.SDR HNAA2023080400276Unknown · unknownE983561 CORROSION ON RH OTBD # 6 FLOOR SILL. REMOVED AND REPLACED R/H OTBD #6 FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2023080400264Unknown · unknownE983413 LH #3 OUTBD FLOOR SILL IN CARGO IS CORRODED. REMOVED AND REPLACED LH #3 OUTBD FLOOR SILL IN CARGO IAW EMB-145 SRM 51-40-02SDR HNAA2023080400263Unknown · unknownE983412 LH #2 OUTBD FLOOR SILL IN CARGO IS CORRODED. RAR L/H #2 OUTBD CARGO FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2023080400262Unknown · unknownE983407 RH #2 OUTBD FLOOR SILL IN CARGO IS CORRODED. BLENDED CORROSION ON RH #2 OUTBD FLOOR SILL IN CARGO AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW EMB-145 SRM 51-10-03, & SRM 53-31-10 AD. RAR RH #2 OUTBD FLOOR SILL IN CARGO IAW EMB-145 SRM 51-40-02.SDR HNAA2023080400261Unknown · unknownE983403 LH #1 OUTBD FLOOR SILL IN CARGO IS CORRODED AT FWD END. REMOVED & REPLACED LH #1 OUTBD FLOOR SILL IN CARGO IAW EMB-145 SRM 51-40-02SDR HNAA2023080400260Unknown · unknownE983372 FUSELAGE INTERNAL RH#3 UPPER SEAT TRACK CORRODED IN NUMEROUS AREAS. : BLENDED OUT CORRSION ON R/H UPPER SEAT TRACK #3 IAW EMB 145 SRM 51--10-03. PART MECHANICALLY MEASURED .32" AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW EMB 145 SRM 53-00-11 AD. USEDSDR CALA2023063002081Intercostal · corroded(B737-06-3-0049) CORROSION ON MAIN DECK FLOOR STRUCTURE TOP SURF ACE RBL 48, BS 958 REMOVED AND INSTALLED NEW INTERCOSTAL FLOOR STRUCTURE RBL48 BS 9 58 IAW B737-700ER SRM 51-40-02-0G-0 7.A. DATA WAS TRANSCRIBED FR OM PAPER DOC AERSALE WO 3953 NR 33007 WORK ACPSDR CALA2023063002079Flange · corrodedFLANGE CORRODED ON THE APU RAM AIR INLET DOOR BOX REMOVED AND REPLACED FWD STRAP AT THE APU RAM AIR INLET DOOR BOX AT STA 1785. THE SSFR WAS COMPLETED AND UP DATED.SDR SWIA20230627Unknown · corrodedMAIN AVIONICS BAY STR 22L SPLICE AT FS333.00 CORRODED (C-CHECK RO 8/31/2023) REMOVED AND INSTALLED NEW MAIN AVIONICS BAY STR 22L SPLICE AT FS333.00 REF. DWG SH670-32420 REV E, CRJ 700 SRM 51-42-06-001-001-A01.PERFORMED PRESSURE CHECK THROUGH REPAIR ARSDR SWAA2023072872060Cover · crackedCRACK COVER TOP LOCATED BS332.1 AT LEVEL STR9R AT PASSENGER CABIN 2023-405075<[01] REPLACED COVER TOP LOCATED BS332.1 AT LEVEL STR9R AT PASSENGER CABIN IAE SOPM 20-50-01 REV 38;[02] REPLACED COVER TOP LOCATED BS332.1 AT LEVEL STR9R AT PASSENGER CABIN IAE SOPM SDR CALA2023062802070Fitting · unknownREMOVE AND REPLACED FLOOR SUPPORT FITTING AT STA 395-418 I/A/W 5 1-40-05 REMOVED AND REPLACED FLOOR SUPPORT FITTING AT 395-415 I/A/W SRM 51-40-02 AND ECRA 5316-01014.SDR CALA2023062802069Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1280 BETWEEN S8 R AND S9R REF SRM 53-00-07 REPAIR 8 THE INSPECTION GIVEN IN TABLE 203/REPAIR 8. THRESHOLD ZONE 3 12, FLIGHT CYCLES WHICHEVER COMES FIRST. METHOD OF INSPECTION DETAIL 000 FLIGHT CYCLES FROM REPAIRSDR CALA2023062802067Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1580 BETWEEN S8 L AND S9L REF SRM 53-00-07 REPAIR 8 IS GIVEN IN TABLE 203/REPAIR 8.DO THE INSPECTION THRESHOLD 12,00 FLIGHT CYCLES WHICHEVER COMES FIRST.METHOD OF INSPECTION DETAILE 0 FLIGHT CYCLES FROM REPAIR ISDR CALA2023062802066Frame · damagedCUTOUT DAMAGE AND REPAIR FUSELAGE FRAME AT STA 1580 BETWEEN S8R A ND S9R REF SRM 53-00-07 REPAIR 8 5 TABLE 203/REPAIR 8. DO THE INSPECTION REQUIREMENTS AS GIVEN IN TABLE 203/ CUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1580 BETWEEN S8 R AND S9R REF SRM 53SDR CALA2023062802065Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 760 BETWEEN S8R AND S9R REF SRM 53-00-07 REPAIR 8 STEP 5 TABLE 203/REPAIR 8.DO THE INSPECTION AS GIVEN IN TABLE 20 OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST. METHOD O INSPECTION INTERVAL 3/REPAIR 8 SDR CALA2023062802064Forging · crackedAFTER HFEC INSPECTION ON R/H # 1 WINDOW FRAME FOUND TO BE CRACKED, COMPLY WITH ESFR FROM AND CREATE LOG PAGE. (REF: AAR NR 99973293) PERFORMED ALL WORK IAW B737 EA 5310-04554 REV B ROUTINE CARD 350 1849/2000/0239 SN 775 WORK PEFORMED 737NG RH #1 WINDOW FRAME ISDR AALA202306277960Fork · wornAIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER LEFT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32L. REPLACED FORK END (AALA202306277960) AND FITING (AALA202306274651) PER EA 343852.SDR AALA202306272377Fork · wornAIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER RIGHT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32R. REPLACED FORK END (AALA202306272377) AND FITING (AALA202306275345) PER EA 343852.SDR AALA202306275345Fitting · wornAIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER RIGHT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32R. REPLACED FORK END (AALA202306272377) AND FITING (AALA202306275345) PER EA 343852.SDR EE4Y2023062717942Frame · unknownDURING THE STRUCTURAL INSPECTION AS PER ALLEGIANT TASK: 534124-01-2-001 AN EXISTNG REPAIR WHICH INTERFERES WITH THE INSPECTION AND WITH A DEVIATION WAS FOUND. ALL DETAILS ABOUT EXISTING REPAIR WERE SENT TO AIRBUS ASKING ABOUT FORM APPROVAL TO COVER THE DEVIATISDR IXXA2023062703Skin · abnormalHOLE IN SKIN FOUND @ STA 344, S21RSDR R61A2023071400103Seal Rest · gougedFWD PAX DOOR CUTOUT AFT SEAL REST GOUGED. REMOVED AND REPLACED FWD PAX DOOR AFT SEAL REST. RESTORED ORIGINAL FINISH / SURFACE PROTECTION. REF EMB SRM 51-40-08, 51-23-04, 51-23-- 06, 51-23-05. CPM 51-25-00
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