JASC 5300
Service difficulty reports · 8,205
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 YENA2023061600636Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE BTW STRINGER 41R AND STRINGER 42R AT LEVEL OF FRAM E 32 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REF TO AEROMAN W/O 2023 200/1 NR2023-25254 REMOVED AND REPLACED SHEAR TIE BTW STRINGER 41R AND STSDR YENA2023061600635Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FRONT WINDSHIELDS / CENTER POST / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023061600634Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 BULKHEAD WEB AT STR 30LH / CRACKED HOLE - TIME-LIMITED REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR CALA2023061401858Unknown · corroded(SUPPORT TASK) PASSENGER CABIN FLOOR STRUCTURE AT STR 20 RH JUST FWD OF STA 967 RH HAS CORROSION ON THE UPPER HAT FLANGE ON STR 20 RHSDR CALA2023061401856Unknown · crackedFRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). FRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). ADD EMP:V921218SDR CALA2023061401855Frame · crackedCRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). CRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). ADD EMP:V931845SDR CALA2023061401850Frame · crackedFRAME CRACKED AT STA 760 BELOW STR 8-R UPPER CABIN AT ATTACH BRACKET RIVET HOLE FOR OVER HEAD STOWAGE BINS. V931857SDR FDEA202306141033Panel · damagedMAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL24 TO LBL45. REMOVED AND REPLACED FLOOR PANEL AT STA 560 - 680 LBL 24 - LBL45 IAW B757 AMM 53-01-01-4 AND FEDEX DWG SRZ-25-005 REV RSDR FDEA202306141032Panel · damagedMAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL 0 TO LBL 24. REMOVED AND REPLACED FLOOR PANEL AT STA 560-680 LBL 0 - LBL 24 IAW B757 AMM 53-01-01-4 AND FEDEX DWG SRZ-25-005 REV R.SDR JJBA20230705004Unknown · unknownCF1, CRACK FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-24. BEAM REPAIRED WITH A DOUBLER.SDR JJBA20230705003Unknown · unknownCRACKS FOUND ON TOP OVERHEAD MIDDLE FRAME LH + RH SIDE AROUND NUT PLATE ON WINDSHIELD SURROUND STRUCTURE COCKPIT AREA.TOP OVERHEAD MIDDLE FRAME LH + RH SIDE INSTALLED REPAIR DOUBLERS.SDR IXXA2023070303Frame · corrodedAFT CARGO FLOORBOARD ATTACH ANGLE AT 153EF STA 1197 RBL18 CORRODEDSDR IXXA2023070302Frame · corrodedAFT CARGO ATTACH ANGLE LOWER SURFACE HAS CORROSION AT STA 1197 RBL 12SDR IXXA2023070301Unknown · corrodedAFT CARGO FLOOR BOARD ATTACH ANGLE HAD A BAD NUTPLATE AND CORROSION ON THE LOWER SURFACE AT STA 1197+132 RBL6SDR IPXA2023062693516Splice · unknownINSPECTION TYPE:3C*MAJOR REPAIR* FOUND EXISTING REPAIR SPLICE FITTING AT STA Y=6-80 LONGERON 46L WITH NO HISTORY.REPLACED EXISTING REPAIR SPLICE FITTING AT STA Y= 6-80 LONGERON 46L IAW SRM 53-00-05 FIG 201 REPAIR 1. (MAJOR)SDR AALA202306149995Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PRESSURE BULKHEAD LOWER WEB LOCATED AT BS 1016 FROM RBL 56.98 TO RBL 16.73. REMOVED, FABRICATED, AND INSTALLED LOWER WEB PER SRM 51-40-02-0G.SDR CALA2023061401839Bolt · missingPDA 3 REFERENCE LOG ENTRY 4860584: MISSING FASTENER ON THE 192AR PANEL. FASTENER IS LOCATED AT STATION 800, APPROX STRINGER 23, 21ST FASTENER UP FROM THE BOTTOM OF THE FAIRING, ON FRAME 149N7122, ITEM 16 (REF SRM 53-30-71-0L-1. THIS IS A CATEGORY 3 PDA. INSSDR DALA2023061404850Unknown · unknownCORROSION ON FLOOR SUPPORT BTW STA Y=120 AND Y=148 X=-50 AT COCKPIT. SUMMARY OF NRC 00440: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=120 TO Y=148 X=-50 AT COCKPIT WAS REPLACED PER B717-200 SRM 51-41-08-0G. (LP #2814601)SDR CALA2023061601888Frame · crackedCRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). CRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). ADD EMP:V931845SDR CALA2023061401842Unknown · unknownAIRCRAFT RELEASED FROM REPAIR STATION WAS MAINTAINED IAW FAA REG S. AND UNITED SPECIFICATIONS AND PROCEDURES AND IS AIRWORTHY WITH RESPECT TO WORK PERFORMED. PERTINENT DETAILS ARE ON FILE AT THE REPAIR STA. IN THE SIGNOFF, LIST THE VISIT TYPE,CERTIFICATE #, ANSDR UIEA2023052600524Unknown · unknownCOCKPIT - RH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(<P>COCKPIT - RH RUDDER PEDAL CAVITIES, RH PILOT FWD PANEL SUPPORT WEB P/N: 233U2320-212 CRACK AREA REPAIRED IAW RI-53-16279 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023052600525Unknown · unknownCOCKPIT - LH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(<P>COCKPIT - LH RUDDER PEDAL CAVITIES, LH PILOT FWD PANEL SUPPORT WEB P/N: 233U2320-210 CRACK AREA REPAIRED IAW RI-53-16-16279 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023052600527Unknown · unknown1EA SURFACE CRACK FOUND ON LH STA 2231 STR 21L TO STR 22L REVEAL CRACK APPROX 2.375" IN LENGTH.(<P>STA 2231 STR 21L TO 22L, #5 DOOR REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3 FIG 203. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023053000528Unknown · unknownAFT CARGO STA 1700 FLOOR BEAM MIDDLE AREA FOUND CHAFING.(<P>AFT CARGO STA 1700 FLOOR BEAM UPPER CHORD P/N: 65B07373-3 CHAFING AREA REPAIRED IAW RI-53-60-16278 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060100552Unknown · unknownLH STA 720 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 720 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060100553Unknown · unknownRH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 760 RH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060100554Unknown · unknownLH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 760 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500565Shear Tie · unknownSTA 1000 FRONT SPAR SHEAR TIE CRACK FOUND RBL 33.99(<P>STA 1000 RBL 33.99 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 APRT 8 AND RI-53-43-16281 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500566Shear Tie · unknownSTA 1000 FRONT SPAR SHEAR TIE CRACK FOUND LBL 75.92(<P>STA 1000 LBL 75.92 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 6 AND RI-53-43-16285 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500567Unknown · unknownBODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE FOUND CRACK(<P>BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE CRACK AREAS REPAIRED IAW RI-53-40-16280 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500568Unknown · unknown1EA THOUGHT THICKNESS CRACK FOUND ON LH BS2231 S16 STRAP (COUNT FROM O/B SECOND LAYER) RUNNING FWD AT 4 O/C POSITION (VIEW LOOKING O/B).(<P>M/D - STA 2231 STR 16L FRAME STRAP P/N: 65B01849-25 CRACK AREA REPAIRED IAW RI-53-60-16284 REV.A. NO FURTHER DEFECTS NOTSDR UIEA2023060500569Longeron · unknownSTA 1480 RH LONGERON EXTENSION FTG FOUND CRACKED(<P>STA 1480 RH LONGERON EXTENSION FTG P/N: 65B15034U24 REPLACED AND INSTALLED IAW EO 4453A818 PART 4. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500570Longeron · unknownSTA 1480 LH LONGERON EXTENSION FTG FOUND CRACKED(<P>STA 1480 LH LONGERON EXTENSION FTG P/N: 65B15034U23 REPLACED AND INSTALLED IAW EO 4453A818 PART 3. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060600581Unknown · unknownDAMAGE LOG D-4-15 - DENT BOTTOM OF BULK CARGO FRAME, STA 1992 WL175, L=3/4" X W=3/4" X D=1/32", PER SRM 53-00-01-1A-1 TABLE 1 DETAIL 3 ADL LIMIT.(<P>FX - STA 1992 STR 42R TO STR 43R SKIN DAMAGED AREA REPAIRED IAW RI-53-61-16293 REV.A. NO FURTHER DEFECTS NOTED<SDR UIEA2023060700597Unknown · unknownLH BS 740 TENSION TIE FWD CHANNEL 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT 12 O'CLOCK AND 6 O'CLOCK POSITION.(<P>STA 740 LH TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060800609Unknown · unknownEO 4453A516 PART 4, STA 400 RH WAS A REPAIR PREVIOUSLY INSTALLED IN THE MODIFICATION AREA.(<P>FX STA 400 RH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 4 AND RI-53-18-16306 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060800610Unknown · unknownFX STA 400 LH NOSE WW AFT CORNER SKIN CRACK(<P>FX STA 400 LH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND RI-53-18-16306 REV.A. NO FURTHER DEFECTS NOTED</P>)SDR EVCA202306130001Intercostal · unknownCRACK FOUND ON TAILBOOM UPPER LEFT-HAND INTERCOSTALSDR AALA202306125009Structure · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FAILSAFE CHORD LOCATED AT BS 767 ABOVE S27R. REPAIRED FAILSAFE CHORD PER EA 345277.SDR R61A2023070800385Skin · dentedR791276/1 TRANSFER FROM VP- 014782-2021 C1 & C2. DENT ON LH FWD FUSELAGE BETWEEN FRAME 6-7 STR 17L & 18L. DENT IS W=1.4", H=0.015", W/H= 93.- 333".GOUGE A DEPT. PERFORMED PERMANENT REPAIR BY CUTOUT AND DOUBLER REPAIR AT LH FWD FUSELAGE BETWEEN FRAME 6-7 STR 17SDR AALA202306122838Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING CENTER POST AREA RIGHT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 3436250.SDR AALA202306120627Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK WINDSHIELD FRAMING CENTER POST AREA LEFT HAND CONTINUITY FITTING AT FR 2 AND Y0. REPLACED CONTINUITY FITTING PER EA 3436250.SDR VNAA202306110001Fitting · unknownNEW HSTA FITTING AV670-23105-006S MISDRILLED AND REQUIRES NEW FITTING. PERFORMED A MAJOR REPAIR TO R/H HSTA UPPER FITTING ASSY.SDR IPXA2023070506430Unknown · corroded*MAJOR REPAIR* FAULT-MAIN CARGO COMPARTMENT AT FR 1360 THE FLOOR BEAM HAS SPOTS WITH CORROSION.NO DOT ACCOMPLISH REPAIR PER EO-87430-REQ1 AND EA 757-5360-27-A3261. WORK ACCOMPLISHED PER EO-87430-REQ1. REVIEWEDSDR UIEA2023060600583Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1562 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753595 REV 1 ISSUED ON MAY 15, 2023 (FVCI PROJECT NO. 23088-6). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500580Unknown · unknownCORROSION ON INTERNAL FUSELAGE BEARSTRAP BETWEEN STA 1540 AND STRINGER S-10RH / S-11RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753594 ISSUED ON MAY 09, 2023 (FVCI PROJECT NO. 23088-5). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500578Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-14RH / S-15RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753590 ISSUED ON MAY 04, 2023 (FVCI PROJECT NO. 23088-1). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500577Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-12RH(<P>THE SURFACE PROTECTION WAS RESTORED ON THE REWORKED AREA PER MXA EO TRE6753591 (FVCI PROJECT NO. 23088-2). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500576Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1461 AND STRINGER S-8RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753592 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-3). NO FURTHER DEFECTS NOTED</P>)SDR UIEA2023060500575Unknown · unknownCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN STA 1480 / DSTA 876.3 AND STRINGER S-9RH / S-10RH(<P>DOUBLER REPAIR WAS INSTALLED PER MXA EO TRE6753593 ISSUED ON MAY 05, 2023 (FVCI PROJECT NO. 23088-4). NO FURTHER DEFECTS NOTED</P>)
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