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.
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 COEA2022020104819Angle · crackedWO 232464 NR 200017 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE FRAME 14 STRINGER 6L UPPER CORNER STRUCTURE FOR CARGO DOOR CUTOUT HAS A CRACK. CORRECTIVE ACTION: REPLACED FWD CARGO DOOR FWD ANGLE PER ATR72 SRM 533780-14-A01.SDR COEA2022012503819Stringer · gougedWO 232464 NR 200007 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE FWD OF FR23A STRINGER 6L STRINGER HAS GOUGE. CORRECTIVE ACTION: REPAIRED PER ATR72 SRM 530000-300-824-A01.SDR COEA2022012502819Floorbeam · crackedWO 232464 NR 100013 HEAVY CHECK COE/MAJOR REPAIR: MAIN CABIN L/H LONGITUDINAL FLOORBEAM BETWEEN FRAMES 23C-23D IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-02.SDR COEA2022012501819Floorbeam · crackedWO 232464 NR 100014 HEAVY CHECK COE/MAJOR REPAIR: MAIN CABIN L/H LONGITUDINAL FLOORBEAM BETWEEN FRAMES 23A-23B IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-02.SDR QXEA2022011100022Splice · corrodedCORROSION FOUND ON LONGITUDINAL SPLICE LOCATED IN THE AFT WET AREA FR89-90 STG 17 Y-00+10. BLENDED OUT DAMAGE ON LONGITUDINAL SPLICE LOCATED IN THE AFT WET AREA FR89-90 STG 17 Y-00+10 PER SRM 51-10-03 PART HAS 100% MATERIAL LOSS AND PART REQURIES REPLACEMENT. SDR QXEA2022011100021Crossbeam · corrodedCORROSION FOUND ON CROSSBEAM LOCATED IN THE AFT WET AREA FR87-88 STG 17. BLENDED OUT DAMAGE ON LONGITUDINAL SPLICE LOCATED IN THE AFT WET AREA FR87-88 STG 17 PER SRM 51-10-03 PART HAS 100% MATERIAL LOSS AND PART REQURIES REPLACEMENT. LOCATED, DRILED, AND ALODISDR JJBA20220104003Not Reported · not reportedUNDER BAGGAGE COMP UNDER RADIO ALT 2 CORROSION. REMOVED AND REPLACED UNDER BAGGAGE COMP RADIO ALT #2 ANTENNA SUPPORT.SDR HNAA2022010400039None · noneE893519 - CORROSION ON LH OTBD #1 SEAT TRACK - RAR LH OUTBD#1 SEAT TRACK IAW EMB 145 AMM 53-01-06SDR HNAA2022010400038None · noneE893451 - FUSELAGE SKIN IS CRACKED BETWEEN FR 80-81 NEAR STR 13R ... COMPLETED REPAIR OF FUSELAGE SKIN BTW FR 80-81 STGR 13R-15R IAW ETD# ETD2021-145-041044 AND PIEDMONT EO1-53-21-0356.SDR HNAA2022010400037None · noneE893326 - RH FUSELAGE DRAG ANGLE FWD SECTION AFT AREA HAS POSSIBLE CRACKS AT FASTENER HOLE AREAS MARKED ... COMPLETED INSTALLATION OF SERVICEABLE FWD DRAG ANGLE, AND PREVIOUS REPAIR ANGLE AND SHIMS AT FRAME 75 STRINGER 2R IAW EMB145 SRM 51-40-02, 53-31-01 ITEMSDR HNAA2022010400036None · noneE893075 - L/H CABIN FLOOR BEAM SEAT TRACK #4 IS CORRODED ... RAR L/H CABIN FLOOR BEAM SEAT TRACK #4 IAW EMB 145 AMM 53-01-06SDR HNAA2022010400035None · noneE893073 - L/H FLOOR BEAM SEAT TRACK GUESSET #4 IS CORRODED ... REMOVED AND REPLACED L/H FLOOR BEAM
SEAT TRACK GUSSET #4 IAW EMB-145 SRM 51-40-02.SDR HNAA2022010400034None · noneE893072 - CENTER FLOOR BEAM SEAT TRACK GUESSET #3 IS CORRODED. ... REMOVED AND INSTALLED SERVICEABLE CENTER FLOOR BEAM SEAT TRACK GUSSET #3 IAW EMB145 SRM 51-40-02.SDR HNAA2022010400033None · noneE893071 - L/H CABIN FLOOR SILL #4 IS CORRODED ... RAR LH #4 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2022010400032None · noneE893062 - L/H CABIN FLOOR SILL #7 IS CORRODED ... RAR CABIN FLOOR SILL #7 IAW EMB 145 SRM 51-40-02.SDR HNAA2022010400031None · noneE893044 - CORROSION IN GALLEY AREA ON CROSS FLOOR BOARD SUPPORT AT FRAME 19 ... REMOVED AND REPLACED CROSS FLOOR BOARD SUPPORT AT FRAME 19 IN GALLEY AREA IAW EMB145 SRM 51-40-02.SDR HNAA2022010400030None · noneE893043 - CORROSION IN GALLEY AREA ON HAT BEAM AT FRAME 18 PREVIOUS REPAIR ... ACCOMPLISHED REPAIR DOUBLER ON R/ H HAT BEAM AT FRAME 18 IAW ETD2021-145-041321 AND PIEDMONT EO1-53-21-0348.SDR HNAA2022010400029None · noneE893042 - CORROSION ON PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT ... REMOVED DAMAGED SUPPORT AND INSTALLED SERVICEABLE PASSENGER DOOR ENTRY AFT FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.SDR HNAA2022010400028None · noneE893041 - CORROSION ON PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT ... REMOVED DAMAGED SUPPORT AND INSTALLED SERVICEABLE PASSENGER DOOR ENTRY FWD FLOOR BOARD SUPPORT IAW EMB 145 SRM 51-40-02.SDR HNAA2022010400027None · noneE893034 - CORROSION IN GALLEY AREA ON CROSS BEAM AT FRAME 20 ... REMOVED CORRODED CROSSBEAM, DRILLED UP AND INSTALLED NEW FLOOR CROSS BEAM AT FRAME 20 IN GALLEY AREA IAW EMB 145 SRM 51-40-02.SDR HNAA2022010400026None · noneE893033 - CORROSION IN GALLEY AREA ON CENTER GUSSET AT FRAME 22 ... REMOVED AND REPLACED CENTER GUSSET AT FRAME 22 IAW EMB 145 SRM 51-40-02SDR HNAA2022010400025None · noneE893029 - CORROSION IN GALLEY AREA ON SERVICE DOOR CENTER SILL ... INSTALLED INTERNAL DOUBLER AT GALLEY SERVICE DOOR CENTER SILL AT FWD NUTPLATE HOLE IAW EMB 145 SRM 53-21-02 RE, ITEM 2, FIG. 201 AND PIEDMONT EO1-53-21-0362.SDR HNAA2022010400015None · noneE892916 - RH FLOOR SEAT TRACK PITTED BETWEEN FR27-28 ... RAR RH FLOOR SEAT TRACK IAW EMB 145 AMM 53-01-06.SDR HNAA2022010400014None · noneE892915 - LH FLOOR SEAT TRACK PITTED BETWEEN FR29-30 ... REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FR 29-30 IAW EMB 145 AMM 53-01-06. TQW USED EASI# 4401.SDR HNAA2022010400013None · noneE892912 - LH CABIN #3 FLOOR SILL CORRODED. ... RAR LH #3 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2022010400012None · noneE892911 - LH CABIN #2 FLOOR SILL CORRODED ... REMOVED AND REPLACED LH CABIN #2 FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2022010400011None · noneE892910 - RH CABIN #2 FLOOR SILL CORRODED ... REMOVED AND REPLACED RH CABIN #2 FLOOR SILL IAW EMB 145 SRM 51-40-02SDR HNAA2022010400010None · noneE892909 - RH CABIN #1 FLOOR SILL CORRODED. ... RAR RH CABIN #1 FLOOR SILL IAW EMB1145 SRM 51-40-02SDR HNAA2022010400009None · noneE892893 - CARGO DOOR SILL CORRODED ...REMOVED DRILLED AND INSTALLED SERVICEABLE CARGO DOOR LRW CENTER SILL IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02.SDR HNAA2022010400001None · noneE891811 - LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 26-27 AND STR 17R-16R ... ACCOMPLISHED RIVET REPAIR OF LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 26-27 AND STR 17R-16R IAW EMB 145 SRM 53-00-01 ITEM 2B AND PIEDMONT EO1-53-21-0368.SDR HNAA2022010400000None · noneE891808 - LIGHTNING STRIKE ON FUSELAGE SKIN AT FR 24-25 AND STR 17R-18R ... PERFORMED REPAIR ON FUSELAGE SKIN AT FR 24-25 AND STR 17R-18R. IAW EMB 145 SRM 53-22-01 FIG 204 SHEET 1 AND PIEDMONT EO1-53-21-0369.SDR MASA20220103063None · corroded"CORROSION ON LOWER MOUNTING ANGLE AT GALLEY SERVICE DOOR SURROUND STRUCTURE.
LOWER MOUNTING ANGLE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. "SDR FDEA202201030026None · corrodedMAIN DECK SEAT TRACK STRUCTURE FOUND CORROSION BTWN FR11~12A , Y730 REPLACED THE CORROSION SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE2SDR JJBA20220103004Not Reported · not reportedALL SEAT TRACKS GOUGED / POSSIBLE CORROSION. BLENDED CORROSION / GOUGES ON ALL SEAT TRACKS LH UPPER, CENTER FLOOR FRAMES 19-59 AND RH UPPER, CENTER FLOOR FROM FRAME 23-59. ALL SEAT TRACKS WITHIN LIMITS. REMOVED AND REPLACED 2 SEAT TRACKS AT FRAME 26-28 LH FLOOSDR MK1Y202201025None · noneTHE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE RIGHT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR.
RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTISDR MK1Y202201024None · noneTHE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE LEFT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR.
RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIFSDR MK1Y202201018None · noneFUSELAGE SKIN (SEC 45), STA 999 AND STA 1043, STR-2L AND STR-2R: DURING CONVERSION PROCESS, AIRCRAFT MAINTENANCE WAS REQUIRED TO DEACTIVATE AND REMOVE THE HIGH GAIN SATCOM SYSTEM PER CUSTOMER REQUEST THAT WAS INSTALLED BY THE PREVIOUS OPERATOR. THE LARGE EXTERSDR CALA2022010300008Bracket · corrodedB767-53-3-7077 CABIN - LH STA999 S-16L TO S-17L SHEAR TIE FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130759 AND ORIGINATED BY EMP V926653 CABIN BS999 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FSDR CALA2022010300006Stringer · corrodedAFT CARGO FR56 - FR59 STGR 42L. A3NB-53-4-6179. GENERATED BY V06 61629 AT HAECO LCQ PER NR 9290618 (28618) CUT OUT CORRODED STRINGER SECTION AND REMOVED 1EA SHEAR WEB IAW 53-41-13-300-010, SRM 51-21-11/001, SRM 51-23-11/001 ANDSRM 51-4 A320 SRM 53-41-13-300-01SDR JR2R20220102857Shear Panel · corrodedLH FLOOR SHEAR PANEL FOUND TO BE CORRODED AT FR87-FR88SDR JR2R20220102850None · corrodedRH FLOOR SILL CORRODED AT FR90SDR JR2R20220102852Shear Panel · corrodedRH FLOOR SHEAR PANEL CORRODE AT FR87SDR JR2R20220102856Shear Panel · corrodedCENTER FLOOR SHEAR PANEL IS CORRODED AT FR88SDR JR2R20220102909Bracket · corrodedFLOOR SUPPORT BRACKET CORRODE AT FR87 AND APPROX RBL20SDR JR2R20220102851Gusset · corrodedFLOOR GUSSET CORRODED AT FR90 AND RBL 48SDR JR2R20220102853Gusset · corrodedFLOOR GUSSET CORRODED RBL9 AND FR89SDR R61A202201020003Shear Tie · crackedRH FRAME 9 STRINGER 11R HAS CRACKED SHEAR CLIP UNDER RH D.V. WINDOW. : INSTALLED NEW SHEAR CLIP AT FRAME 9 STR 11R UNDER RH D.V. WINDOW. REF SRM 51-40-08.COMPLIED WITH SURFACE PROTECTION. REF SRM 51-23-06. MAJOR REPAIRSDR R61A202201020002Shear Tie · crackedFRAME 9 STR 11L CRACKED SHEAR CLIP UNDER LH D.V. WINDOW. INSTALLED NEW SHEAR CLIP AT FRAME 9 STR 11L UNDER LH D.V. WINDOW. REF SRM 51-- 40-08. COMPLIED WITH SURFACE PROTECTION AS REQUIRED. REF SRM 51-23-06. MAJOR REPAIRSDR MK1Y202201008None · none. DURING A/C SURVEY AT TLV, MAINTENANCE DISCOVERED EXISTING BLENDOUT AT THE EDGE OF AN EXISTING FLUSH REPAIR CUTOUT LOCATED ON THE FUSELAGE SKIN AT STA 616 BETWEEN S38L AND S39L. THE EXISTING FLUSH REPAIR WAS FOUND TO BE INSTALLED BY THE PRIOR OPERATOR, AMERISDR MK1Y202201006None · noneNLG SUPPORT STRUCTURE, AFT VERTICAL STIFFENERS, UPPER EDGES, STA 287, L/RBL 13.10 DURING THE MAINTENANCE INSPECTION AT IAI, TWO CRACKS WERE FOUND AT DATUM LOCATIONS WITH 0.6 INCH LENGTH EACH ONE. THERE IS NO APPLICABLE DAMAGE EXISTING.
VERTICAL STIFFENERS PI
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