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 UIEA2022042600396None · noneL/H BS 880 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT UPPER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP THRU THICKNESS(<P>STA 880 LH TENSION TIE FORWARD CHANNEL AND FORWARD DOUBLER FASTENER HOLES CRACK AREA REPAIRED IAW RI-53-00-155SDR UIEA2022042600397None · noneL/H BS 900 MOST INNER ROW OF FASTENER HOLES AT TENSION TIE TO FRAME ATTACHMENT UPPER HOLE CRACK WAS FOUND ON FWD CHANNEL RUNNING UP AND DOWN APPROX 0.030 AND 0.040".(<P>STA 900 LH TENSION TIE FORWARD CHANNEL AND FORWARD DOUBLER FASTENER HOLES CRACK AREA REPAIRSDR UIEA2022042200364Bushing · noneM/D STA 1000 RBL 11.33 FLOOR SUPPORT I/B CROSS BOLT HOLE FOUND ENLARGED(<P>M/D STA 1000 RBL 11.33" LUG FTG P/N : 366-53-15-A1364-102 REPLACED IAW SRM 51-10-02 AND P/N : 366-53-15-A1364-104 ATT BUSHING REPLACED IAW SOPM 20-50-03.</P>)SDR UIEA2022042200363Bushing · noneM/D STA 1000 LBL 11.33 FLOOR SUPPORT IB CROSS BOLT HOLE FOUND ENLARGED(<P>M/D STA 1000 LBL 11.33 LUB FTG P/N : 366-53-15-A13641-101 REPLACED IAW SRM 51-10-02 AND P/N : 366-53-15-A1364-103 ATT BUSHING REPLACED IAW SOPM 20-50-03.</P>)SDR UIEA2022042000346None · noneFX - APU TAIL CONE RH FRAME AND UPPER OF WL 310 FOUND CRACKED ( UPR OF PREVIOUS REPAIR AREA )(<P>APU COMP STA 2680.18 RH FRAME ON EXISTING REPAIR SEGMENT CRACK AREA REPAIRED IAW RI-53-80-15504 REV B</P>)SDR UIEA2022042000345None · noneU/D STA 680 - 700 STR 12R - STR 13R, FLOOR WEB ATTACHED STIFFENER FOUND HEAVY CORROSION.(<P>U/D STA 685 RBL 80 - RBL 95 WL 307.5 STIFFENER P/N : 65B06144-882 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)SDR UIEA2022042000344None · noneLH STA 2231 FRAME STR 25L 1EA HOLE FOUND CRACK.(<P>M/D STA 2231 STR 25L, 1EA FASTENER HOLE CRACK AREA OVERSIZE REPAIRED IAW RI-53-00-15534 REV B</P>)SDR UIEA2022042000343None · noneFX - APU TAIL CONE RH STA 2640 - 2680 RIVET FOUND LOOSE.(<P>APU COMPARTMENT STA 2670 - STA 2690 WL 305 - WL 315, ELONGATE FASTENER HOLE REPAIRED IAW RI-53-80-15497 REV B.</P>)SDR UIEA2022042000341None · noneSTA 2598 HINGE SUPPORT FRAME MOD AND STA 2598 LH LOWER LEFT CORNER MOD DOUBLER FASTENER S.E.M REPAIR.(<P>STA 2598 HINGE SUPPORT FRAME MOD AND STA 2598 LH LOWER LEFT CORNER MOD DOUBLER 1EA FASTENER S.E.M REPAIRED IAW RI-53-00-15537 REV A</P>)SDR UIEA2022042000340None · noneEMP - VERTICAL FIN L/H L/E FIXED PNL AT FS 245 AND FS 270 FAIRING 321D AREA RIVET FOUND LOOSE.(<P>EMP - VERTICAL FIN L/H L/E FIXED PNL AT FS 245 AND FS 270 AREAS LOOSE RIVET REPLACED IAW RI-55-00-15535 REV A</P>)SDR UIEA2022042000337None · noneLH BS 800 FRAME AREA, 2EA CRACKS FOUND AT STA 14L. STRAP APPROX 1/8 INCH RUNNING FWD. 1/4 INCH RUNNING AFT.(<P>M/D STA 800 STR 14L. FRAME STRAP P/N : 65B26468-1, 1EA FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-15527 REV A.</P>)SDR UIEA2022041900314None · noneSTA 1480 RH WEB SPLICE AREA 1EA CRACK FOUND AT WEB SPLICE PLATE #15 HOLE RUNNING 2 O'CLOCK APPROX 0.050IN.(<P>STA 1480 R/H B/H WEB SPLICE AREA, #15 HOLE WEB SPLICE PLATE CRACK AREA OVERSIZE ( 0.4057" ) REPAIRED AND BUSHING REPAIRED ( 0.502" ) IAW SB 747-53A239SDR UIEA2022041900313None · noneSTA 1480 RH WEB SPLICE AREA 1 EA CRACK FOUND AT WEB PANEL #14 HOLE RUNNING 7 O'CLOCK APPROX 0.050IN.(<P>STA 1480 RH B/H WEB SPLICE AREA, #14 HOLE WEB PANEL CRACK AREA OVERSIZE ( 0.4057" ) REPAIRED AND BUSHING REPAIRED ( 0.502" ) IAW SB 747-53A2390 REV 1 AND FISDR UIEA2022041100291None · noneEO 4453A797 PART 3 - PART 6, SKIN AND BEAR STRAP CRACK AT THE AFT UPPER CORNER OF THE M.E.D 5 CUTOUT - MODIFICATION - SB 747-53A2839.(<P>EO 4453BA797 PART 3 - PART 6, SKIN AND BEAR STRAP CRACK AT THE AFT UPPER CORNER OF THE M.E.D 5 CUTOUT - MODIFICATION - SB 7SDR UIEA2022040900274None · noneRH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #26 AT BULKHEAD CHORD.(<P>RH BS 1480 LONGERON WEB SPLICE AREA AT FASTENER HOLE #26 CRACK HOLE REPAIRED AS PER SB 747-53A2390 REV 1. #26 FASTENER HOLE OVERSIZE ( 0.500" ) REPAIRED IAW SB 747-5SDR UIEA2022040900273None · noneRH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #21 AT WEB PANEL(<P>RH BS 1480 LONGERON WEB SPLICE AREA FASTENER HOLE #21 CRACKED HOLE REPAIRED AS PER SB 747-53A2390 REV 1, #21 FASTENER HOLE OVERSIZE ( 0.500" ) REPAIRED IAW SB 747-53A2390 SDR UIEA2022040900272None · noneLH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #16 AT WEB PANEL.(<P>LH BS 1480 LONGERON WEB SPLICE AREA FASTENER HOLE #16 CRACKED HOLE REPAIRED AS PER SB 747-53A-2390 REV 1. #16 FASTENER HOLE OVERSIZE ( 0.4682 ) REPAIRED IAW SB 747-53A239SDR UIEA2022040900271None · noneRH BS 1480 LONGERON WEB SPLICE AREA CRACK WAS FOUND AT FASTENER HOLE #20 AT BULKHEAD CHORD.(<P>RH BS 1480 LONGERON WEB SPLICE AREA AT FASTENER HOLE #20 CRACKED HOLE REPAIRED AS PER SB 747-53A-2390 REV 1. #20 FASTENER HOLE OVERSIZE (0.500") REPAIRED IAW SB 747-SDR UIEA2022033000259None · noneM/D STA 1800 - 1820 LBL 90 SEAT TRACK CROWN FOUND CORROSION(<P>M/D STA 1800 - 1820 LBL 99 SEAT TRACK CROWN CORROSION REMOVED IAW IAI SRM 51-10-02 AND REPROTECTED IAW IAI SRM 51-20-01, CHECKED WITHIN IAI SRM 53-00-52 ADL 1, FIG 101.</P>)SDR JJBA20220429033None · noneRH FLOOR SILL JUST AFT LAV BULKHEAD HAS SIGNS OF CORROSION FR61 TO FR65. REMOVED AND REPLACED RH FLOOR SILL.SDR JJBA20220429031None · wrong partINCORRECT EXIT MARKER INSTALLED ON FLOOR PROXIMITY LIGHT ALONGSIDE SEAT 24A. REMOVED AND REPLACED EXIT MARKER. NO DEFECTS NOTED.SDR YENA2022050200430None · noneFLT#2637, JFK-STI. 'DIRTY SOCK ODOR THROUGHOUT FLIGHT DECK; ODOR EVENT VERIFIED TO BE TYPE 10 (A)1C. AMBIENT AIR. COMPLIED WITH INFO NOTICE 2017-T15 SECTION A(A) ISOLATED FAULT TYPE 10(A)1 PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-085D. A/C OK FOR SERVICE. ASDR YENA2022050200428None · noneFLT#365, BOS-RSW. ' FUMES ODOR A-B PERSISTENT FROM 7000 TO 4000 FT PASSED THROUGH THIN CLOUD LAYER THROAT IRRITATION AND DISCOMFORT EXPERIENCED BY BOTH PILOTS; ACCOMPLISHED TASKS AS REQUIRED BY INFORMATION NOTICE 2017-T015I PERFORMED VISUAL INSPECTION OF APU FSDR CALA2022050201110Beam · corrodedSTA 365BLO FLOOR SUPPORT STRUCTURE HAS CORROSION. REPORTED BY V9 21209 FOUND AREA ON FLOOR SUPPORT TO BE OUT OF LIMITS. REMOVED AND REP LACED FLOOR SUPPORT FROM STA 365B BLO IAW B757 SRM 51-40-02 PARA GRAPH 7. REF NON-ROUTINE 145078-0100-0161 FOR INFOSDR 2A6D20220429002Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE RH SIDE OF THE TRANSMISSION DECK. THE DEEPEST DEPTH IS 0.015" WITH A LENGTH OF 2.1" AND WIDTH OF 0.1.SDR YENA2022042900422None · noneFLT#365, BOS-RSW. 'FUMES ODOR A-B PERSISTENT FROM 7000 TO 4000 FT PASSED THROUGH THIN CLOUD LAYER THROAT IRRITATION AND DISCOMFORT EXPERIENCED BY BOTH PILOTS; ACCOMPLISHED TASKS AS REQUIRED BY INFORMATION NOTICE 2017-T015I PERFORMED VISUAL INSPECTION OF APU FOSDR IXXA2022040910Floor Support · corrodedFLOOR SUPPORT CORRODEDSDR IXXA2022042909Fitting · corrodedFITTING CORRODED BEYOND LIMITSSDR IXXA2022042908Failsafe · corrodedRH FAILSAFE STRAP CORRODED AT KICK LOAD FITTINGSDR IXXA2022042907Intercostal · corrodedINTERCOSTAL FLOOR SUPPORT CORRODEDSDR IXXA2022042906None · corrodedFRAME CHORD CORRODED.SDR IXXA2022042905Web · corrodedCORROSION ON CARGO GUIDE SUPPORT BEAMSDR IXXA2022042904Floor Support · corrodedFLOOR SUPPORT CORRODED.SDR IXXA2022042903Floor Support · corrodedFLOOR SUPPORTS CORRODEDSDR MK1Y20220429011None · noneEXTERNAL FUSELAGE SKINS, STA 390, STR-24R; STA 396, STR-22R; STA 1420, STR-31L – STR-32L; STA 1351, STR-31R: DURING MAINTENANCE INSPECTION AT IAI, A FEW BLENED OUTS WERE FOUND ON FUSELAGE SKINS 141T3330, 146T3230, 146T3530 AT LOCATIONS AS MENTIONED ABOVE. SEE SDR MK1Y20220429010None · noneDURING MAINTENANCE INSPECTION, LIGHTNING STRIKE DAMAGE WAS FOUND ON EXTERNAL FUSELAGE SKIN AT DATUM LOCATION. THE DAMAGE WAS REMOVED BY BLENDING IN THE FASTENERS AREA.SDR MK1Y20220429009None · noneTAILCONE ASSY, STA 1943.50 TO STA 1952.00: DURING MAINTENANCE INSPECTION MULTIPLE LIGHTING STRIKES WERE FOUND ON TAILCONE ASSY 148T8301-1 (148T8301-1 7 -2 SKINS). THE DAMAGES WERE BLENDED OUT AS REQUIRED, AND NDT HAS PERFORMED REMAINING MATERIAL THICKNESS AND SDR MK1Y20220429007None · noneFUSELAGE FRAME, STA 1461, STR-4R – STR-5R: DURING MAINTENANCE INSPECTION AT IAI, CRACKS WERE FOUND AT DATUM LOCATION. SEE RFTA 02815-0223. THE DAMAGE WAS REMOVED PER J/C MF02815R0223-01 INSTRUCTIONS. THE CUTOUT IS ABOVE 1.99X0.73 INCH.SDR MK1Y20220429004None · noneEXTERNAL FUSELAGE SKIN, SECTION 41, STA 168, BELOW STR-21R; 141T3211: DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLENSDR MK1Y20220429003None · noneSTA 132.5 – STA 172.5, ABOVE STR-21L:
DURING MAINTENANCE INSPECTION AT IAI, MULTIPLE EXISTING UNDOCUMENTED BLEND OUTS WERE FOUND ON THE EXTERNAL FUSELAGE SKIN. ALSO, A GOUGE WAS FOUND ON THE EDGE OF THE DATUM SKIN, STA 132.5.SDR MK1Y20220429002None · noneEXTERNAL FUSELAGE SKIN, SECTION 46, STA 1485, STR-37R; 146T3240:
DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND ON THE EXTERNAL FUSELAGE SKINS AT STA 1485, STR-37R. THE AFFECTED FASTENER IN THE BLEND OUT AREA WAS REMOVED. AFTER INSPECTISDR MK1Y20220429001None · noneEXTERNAL FUSELAGE SKIN - STA 1261.5, STR 28R-STR 29R:DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND , COMMON TO THE FASTENER, THAT IS NOT ALLOWED PER B767-300 SRM 53-00-01, AD1.SDR SWIA202265996None · crackedFWD EQUIPMENT COMPARTMENT - RIGHT SIDE COMPARTMENT DECK CRACKED AT FRAME - FS220 WL79 (C-CHECK RO 7/8/2022) CRACKED DAMAGE ON FLOOR DECK LOCATED AT RH FWD EQUIPMENT COMPARTMENT AT FRAME FS 193.00 WL 79 (INSTEAD OF FS 220.0 ) . CUT OUT DAMAGED AREA ON RHSDR SWIA202265995None · crackedFWD EQUIPMENT COMPARTMENT - LEFT SIDE COMPARTMENT DECK CRACKED AT FRAME - FS220 WL79 (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED FABRICATED REPAIR DOUBLER -1 AND SHIM -3 AND FABRICATED REPAIR CLEAT -2 ON FWD EQUIPMENT COMPARTMENT FLOOR DECK LH AT FS 19SDR SWIA202265993None · crackedFWD EQUIPMENT BAY - R/H DOOR - AFT LATCH - EQUIPMENT BAY FLOOR SILL CRACKED @ UPPER RADIUS OF AFT LATCH RECEPTICAL (C-CHECK RO 7/8/2022) SEE ATTACHED CERTIFICATE FOR MHIRJ GEOMETRIC CONTOUR ANALYSIS APPROVAL. / COMPLIED WITH SKYWEST TASKCARD 51-900-1002SDR IXXA2022053004Intercostal · corrodedCORROSION AROUND NUTPLATES ON UNDERSIDE OF INTERCOSTAL AT RBL 21 BETWEEN STA 588-610SDR SWIA202265626None · damagedWARRANTY: P/N 170-2365-02-401-111 STIFFENER, AFT ATG ANTENNA WAS MISS TRIMMED DURING ACCOMPLISHMENT OF TASK 1086:ERJ3095B-23-ERJ3095B-23. (C CHECK RO 5/20/22) AQUIRED NEW P/N 170-2365-02-401-111 STIFFENER TO REPLACE MISS TRIMMED ONE. REF CP # 24612025 FOR SDR YENA2022050200436None · noneFLT#38, SJO-FLL. ' CABIN CREW REPORTS DIRTY SOUR SMELL FROM 10,000 FEET TO GEAR DOWN ON APPROACH; COMPLIED WITH INFO. NOTICE 2017-T015, SECTION A, ISOLATED TO TYPE 10,(A), 1,C PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-085D. AIRCRAFT OK FOR SERVICE.'SDR YENA2022050500441Nonskid · noneDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC BTW FR81 AND FR 82 AT STR 2RH AND 3RH ON UPPER FUSELAGE; REF AEROMAN WO 2022 71/1, NR 2022-205434, PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTW FR81 AND FR82 AT STR 2RH AND 3RH ON UPPER FUSELAGE IAW SRM 53-5SDR GTIA2022042836402None · noneDOOR R2 EMER ASSIST BOTTLE REQ SERVICE-SERVICED R2 DOOR EMER ASSIST BOTTLE IAW AMM 52-10-00
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