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 R61A2022102100647Intercostal · corrodedFLOOR SUPPORT ANGLE ON INTERCOSTAL BTWN FR 90-92 L/H I/B SIDE CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.SDR YENA2022100601005None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 RH SIDE UPPER CORNER WEB JOINT AFT FACE BETWEEN UPPER FASTENER AND STRINGER 8 RADIUS, CRACK LENGTH IS 0.2 50 INCH APPROX AT AFT GALLEY AREA (1 E/A); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00014 ) RESDR YENA2022100601002None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16RH SIDE IN OPEN FASTENER HOLE 2 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS AREA 6 AND 8 O CLOCK AT FWD GALLEY AREA (2EA); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00019 ) REF TO AEROMAN WO 2022 181/1 SDR YENA2022100601001None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 8 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481996, REMOVED AND REPLACED INTERCOSTSDR YENA2022100601000None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 2 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 2, 5, 8, AND 11 OCLOCK AT THE FWD GALLEY AREA (4 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481998, REMOVED AND REPLACESDR YENA2022100600999None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 1 AND 4 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2020 181/1 NR 2022-481999, REMOVED AND REPLACED INTERCOSTSDR YENA2022100600998None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2022-181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITYSDR GTIA2022100636711None · noneSTRONG PLASTIC ODOR IN COCKPIT DESCENDING THROUGH 21000FT WITH THRUST IDLE. SELECTED XBLEED OFF AND PACK 1 OFF AND ODOR DISSIPATED COMPLETELY.-PERFORM TSM 05-50-00-810-831. RAN PACK 1&2 & INSPECTED FOR CONTAMINATION I.A.W AMM 21-51-00. FOUND NO EVIDENCE OF CONSDR R61A2022102100646Seat Track · corrodedL/H I/B SEAT TRACK FOUND CORRODED AT FR 16. R&R IAW SRM 53-10-10 REPAIR 01.SDR R61A2022102100645Intercostal · corrodedCABIN FLOOR INTERCOSTAL BTWN FR 90-92 R/H I/B SIDE CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.SDR GTIA2022100636707None · noneON SHORT FINAL F/A REPORTED SMELL LIKE DIRTY SOCK-ACCOMPLISHED TSM 05-50-00-810-831 AND RAN ENGINES WITH CREW..ODOR ISOLATED TO PACK 2. SEE LP 2883717-2 FOR CORRECTIVE ACTION.SDR R61A2022102300668Fitting · corrodedL1 DOOR SILL FWD GIRT BAR FITTING WELL CORRODED AROUND 3 EA RIVETS IN BOTTOM OF WELL. REMOVED AND REPLACED L1 DOOR SILL
BEAM REF EMB SRM 51-40-08 SEE WIP'S AND TASKS FOR WORK ACCOMPLISHEDSDR GTIA2022100636705None · noneFUME EVET AT FL 380 SUSPECTED ON PAACK 1. ISOLATED AND FUMES DISPERSED, UPON DESCENT PACK #1 WAS TESTED AGAIN AND FUMES RETURNED. ISOLATED AGAIN WITH NO FURTHER FUMES. ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCEDSDR JR2R20221004848Skin · crackedLH SIDE OF FUSELAGE SKIN AFT OF RADOME DAMAGED BETWEEN FR1 AND FR2SDR SWIA202266581None · damagedREF AML 1005421 CATERING TRUCK HITTING AC: FOUND DAMAGE IS A HOLE APPROXIMATELY 6.25 INCHES LONG BY APPROXIMATELY 4.5 INCHES WIDE IN TOTAL WIDTH LOCATED ON THE BOTTOM OF THE TAIL CONE. IN ADDITION TO THE HOLE, THERE IS BUCKLING IN THE AREA OF THE HOLE, WITH THSDR SWIA202266582None · damagedDAMAGE EVALUATED AND DETERMINED TO BE OUT OF LIMITS PER SRM 53-00-00-01 AND SRM 53-00-31-01. DAMAGE TO LOWER SKIN AND STRINGERS 25 AND 26 ON BOTH SIDES OF THE CENTERLINE JUST AFT OF FS755 DETERMINED TO BE A MAJOR REPAIR / REFER TO CP 25583746-1 (FILED OPEN) SDR GTIA2022100336702None · noneSTRONG SMELL IN FLIGHT DECK AT FL180 DESCENDING. AFTER PACK 1 TURNED OFF SMELL WENT AWAY. FA DIDNT NO REPORT A SMELL.-PERFROMED TSM 05-50-00-810-832-A. PERFROMED SUBTASK A PARAGRAPH 3 (3) IAW AMM 49-00-00-200-812-A. NO SMELS NOTED. A/C OK FOR SERVICE AT THIS TSDR GTIA2022100336699None · noneHEARD LOUD POP , FOLLOWD BY A SMELL OF BURNING E;EC ON CLIMB OUT AR 22,000 FT . DIVERTED TO RIC. ON TAXI WAY WAITING FOR GATE SMELL AND NOISE GOT WORSE , NO ECAM AT THIS TIME .. ANOTHER LOUD NOISE HAPPENED AND SMELL OF BURNING. AT THAT TIME GOT ECAM FAULT -PERSDR 2022FA0000560None · asymetricAT 400 HOUR ENGINE VIBRATION CHECK, RESULTS EXCEED LIMITS BY 4X. ENGINE REMOVED AND SENT TO DALLAS AIR MOTIVE. WHEN RUN ON TEST, CELL. ALL VIBRATIONS WITHIN LIMITS. MRO (DALLAS AM) PREFORMED RUNOUT CHECK AS DESCRIBED IN RMM ON PAGE 18.35, #4, B. FOUND TO BE 0.SDR YENA2022100400983None · noneDURING HEAVY MAINTENANCE: CORROSION LOWER SILL AT LEVEL FR68 AND STR 23L AFT GALLEY AREA (CPCP RELATED MPD TASK 534195-01): PERFORMED REPAIR AT LOWER SILL AND STR23L AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001. THIS REPAIR IS CATEGORY A AND NO FURTHER INSPESDR CALA2022100302628Structure · cracked( AD2022-06-07 ) SUPPORT TASK - EA 5380-01113 REV B OP.017 LH BS 2370 PIVOT B/H FWD CHORD FOUND CRACKED AS MARKED , PLS GENERATE EA 5380-0113 REV B OP.025 , TRANSFER TO NR WO.1085050 AND ORIGINATED BY V934412 LH BS2370 PIVOT BULKHEAD FORWARD CHORD REPLACED AS SDR CALA2022100302626Structure · cracked( AD2022-06-07 ) SUPPORT TASK - EA 5380-01113 OP.18 RH BS 2370 PIVOT B/H FWD CHORD FOUND CRACKED AS MARKED , PLS GENERATE EA 5380-0113 REV B OP.26 , TRANSFER NR WO.1085052 AND ORIGINATED BY V934412 RH BS2370 PIVOT BULKHEAD FORWARD CHORD REPLACED AS PER EA5380-SDR GTIA2022100336696None · noneSTRONG SMELL IN THE FLIGHT DECK AT 6000FT IDDLE POWER. SMELL WENT AWAY 1 MIN AFTER PACK 1 WAS TURNED OFF. FLIGHT ATTENDANTS DID NOT SMELLED ANYTHING. NO FURTHER SMELL AFTER PACK 1 OFF. -PERFORMED TROUBLESHOOTING PER TSM 05-50-00-810-831-A. PERFORMED LEVEL B DESDR YENA2022100300981None · noneFLT#170, FLL-BOS. 'LEVEL 1 ODOR EVENT. FCOM ODER ISOLATION PROCEDURE COMPLIED WITH. PACK 1 SUSPECTED. ODOR NOT DETECTABLE AFTER 3-5 MIN AIRCRAFT ENVIRONMENTAL SYSTEM ODER; PERFORMED LEVEL A DECONTAMINATION AND REPLACED BOTHH RECIRCULATION FILTER OER E 30905. RSDR CALA2022100302587Door · corrodedR2 DOOR AND FR68 FWR FACE LOWER AREA HAVE CORROSION PER HAECO LC Q N/R 9290381/30381 GEN BY V061682 SEE LP''S 9647687 AND 9647706 FOR DIPS AND REPETITVE INSP REQUIREMENT FOR THE REPAIR OF THE R2 DOOR AND FR68 FWR FACE LOWER AREA HAVE CORROSION PER ECRA 5341-01SDR GTIA2022100336687None · noneFUNKY SMELL DESCENDING THRU 5000'-4000' COMING FROM PACK 2 AND GOT IT ALSO FROM APU BLEED-REF. TSM 05-50-00-810-851-A INSP AND FOUND APU LEAKING OIL AT GEARBOX FLANK SEE L.P. 3079806-1 APU OIL LEAK. R/R RECIRC FILTERS IW AMM 21-21-41 PERF. DECONTAMINACION OFSDR UIEA2022100101066None · noneREINSPECTION OF DENT AT FWD CARGO FUSELAGE STATION 560 ( 15 INCHES FROM BOTTOM OF DOOR CUT OUT ) (PART II OF EO 4453C212, DUE EVERY 5 FLIGHT CYCLES )(<P>ACCOMPLISHED ATLAS AIR EO # 4453C212 PART # 3 PERMANENT REPAIR AT FWD FUSELAGE BY STA 56SDR CALA2022093002581Panel · crackedCTR FUSELAGE LH FR 36 PRESSURE PANEL CRACKED I/B HOLES #9, #20, #26 ACCOMPLISHED ON VTMAE NR 36413 BY VTMAE EMPLOYEE V933870. N PRESSURE PANEL HOLES AREA PER PART 2 OF THE LATEST REVISION OF OR BEFORE MARCH 23, 2023, PERFORM AN INSPECTION OF THE LH FR 36 ECRA SDR CALA2022093002580Fastener · missingPDA 3 REF LOG PAGE 9639140 CREW REPORTED MISSING FASTENER, REF ORIGINAL LOG PAGE 9639140 MISSING FASTENER REPLACED.SDR CALA2022093002578Bulb · noneF/A REPORTED ELECTRICAL SMELL, MOST NOTICABLE AT DOOR 2L/ 2R. THE TIME THE SMELL WAS NOTICED POSSIBLY CORRESPONDS TO THE START OF THE APU. STARTED APU ON AND OFF SEVERAL TIMES COULD NOT LOCATE A SMELL , FLOOR MAT AND CARPET HAS PLASTIC SMELL, LOOKS NEWLY INSDR CALA2022093002576Radome · noneSTRONG STATIC DISCHARGE /LIGHTNING STRIKE AT NOSE DURING FLIGH T. FOUND BURNED MARKS ON RADOME UPDATING PICTURES. PERFORMED LIGHTING INSPECTION PHASE 1A AND 1B, FOUND SMALL BURN MARKS ON RADOME, NO OTHER AREAS OF DAMAGE NOTED. OPENED RADOME FOUND NO DAMAGE TSDR SWAA2022101749300Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT STA 727E +1;+2;+6;+10;+14;+15 TO 747; LBL 23 TO 25; WL 157. / [01] ENTERED MEASUREMENTS.;[02] B737-700 SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS EVALUATION.<BR>REMOVED CORROSION DAMAGE IAW SRM 51-10-02-0GSDR SWIA202266576Stringer · damagedDAMAGE EVALUATED ON RH SIDE STGR 14A P/N: CC670-33164-6, DEFORMED DAMAGE STGR 14A LOCATED AT FS229.00-FS236.00 MEASURING 6.0"L AND A DENT ON STGR 14A LOCATED AT FS247.00-FS250.00 MEASURING 3.0"L. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR. REMOVED AND RESDR DALA2022093006409None · noneSHIP 655 DENTS ON FRAMES STA 1320 BTW S-27R - S-24R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00241-PREVIOUS REPAIR DOUBLER ON STA 1320 BTW S- 27R - S-24R AT AFT CARGO WAS REPLACED PER B757-200 SRM. (2430419)SDR DALA2022093006408None · noneSHIP 655 DENTS ON FRAMES STA 1320 BTW S-27R - S-24R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00241-PREVIOUS REPAIR DOUBLER ON STA 1320 BTW S- 27R - S-24R AT AFT CARGO WAS REPLACED PER B757-200 SRM. (2430412)SDR UIEA2022091600982None · noneEMP - STA 2598 BULKHEAD STR 11L, LONGERON BULKHEAD FRAME SUPPORT FOUND CRACK(<P>EMP - STA 2598 STR 11L FRAME SUPPORT P/N: 65B02508-3 CRACK AREA REPAIRED IAW RI-53-83-15874 REV.A</P>)SDR UIEA2022091600983None · noneEMP - STA 2598 BULKHEAD STR 11R, LONGERON BULKHEAD FRAME SUPPORT AND SPLICE FTG FOUND CRACK(<P>EMP - STA 2598 STR 11R SPLICE FTG 65B02539-12 REPLACED AND FRAME SUPPORT P/N: 65B02508-4 CRACK AREA REPAIRED IAW RI-53-83-15875 REV.A</P>)SDR UIEA2022091700988None · noneLH NOSE WHEEL SIDE PANEL STA 265 TO 280 WL 170 STIFFENER CRACKED.(<P>LH NOSE WHEEL SIDE PANEL STA 265 TO 280 WL 170, STIFFENER P/N: 65B07942-164 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)SDR UIEA2022091700989None · noneLH NOSE WHEEL SIDE PANEL STA 320 TO 340 WL 140 STIFFENER CRACKED.(<P>LH NOSE WHEEL SIDE PANEL STA 320 TO 340 WL 140 STIFFENER P/N: 65B07942-181 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)SDR UIEA2022091700990None · noneSTA 1000 FRONT SPAR SHEAR TIE AT LBL 11.33 STAND OFF AREA FOUND CRACK APPROX 1.5"(<P>STA 1000 LBL 11.33 FRONT SPAR SHEAR TIE P/N: 69B10957-11 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02 AND DWG 111U0901 SHEET 2</P>)SDR UIEA2022092201032None · noneRH BS 1480 1EA CRACK WAS FOUND AT FASTENER HOLE (20) AT LOWER BULKHEAD CHORD(<P>FX - STA 1480 RH STR 33R - 34R AREAS. LOWER BULKHEAD CHORD 1EA FASTENER HOLE CRACK AREA FREEZE PLUG REPAIRED IAW RI-53-00-15880 REV.A</P>)SDR UIEA2022092201033None · noneRH BS 1480 CRACKS FOUND AT FASTENER HOLE (25) AT LOWER BULKHEAD CHORD RUNNING 12 O'CLOCK APPROX 0.030" IN DEPTH(<P>RH BS 1480 CRACKED FASTENER HOLE (25) AT LOWER BULKHEAD CHORD REWORKED AND A FREEZE PLUG FABRICATED AND INSTALLED AS PER RI-53-00-15880 REV.A</P>SDR UIEA2022092201034None · noneRH BS 1480 CRACKS FOUND AT FASTENER HOLE (25) AT LOWER BULKHEAD OUTER CHORD SPLICE FITTING RUNNING 7 O'CLOCK APPROX 0.060" IN DEPTH(<P>RH BS 1480 CRACKED FASTENER HOLE (25) AT OUTER CHORD SPLICE FITTING REWORKED AND A FREEZE PLUG FABRICATED AND INSTALLED AS PESDR UIEA2022092201035None · noneRH BS 1480 WEB SPLICE PLATE HOLE #15 FOUND CRACK(<P>RH BS 1480 CRACKED FASTENER HOLE (15) AT WEB SPLICE REWORKED AND A FREEZE PLUG FABRICATED AND INSTALLED AS PER SB 747-53A2390 REV.01 FASTENER INSTALLED AS PER SB 747-53A2390 REV.01</P>)SDR UIEA2022092201036None · noneRH BS 1480 WEB PANEL HOLE #15 FOUND CRACK(<P>RH BS 1480 CRACKED FASTENER HOLE (15) AT WEB PANEL REWORKED AND A FREEZE PLUG FABRICATED AND INSTALLED AS PER SB 747-53A2390 REV.01 NEW FASTENER INSTALLED AS PER SB 747-53A2390 REV.01</P>)SDR UIEA2022092201037None · noneRH BS 1480 LONGERON LOWER BULKHEAD 1EA CRACK WAS FOUND AT FASTENER HOLE (26) DETAIL REFER INSPECTION FINDING RECORD(<P>RH BS 1480 CRACKED HOLE (26) REWORKED AT LONGERON LOWER BULKHEAD A FREEZE PLUG FABRICATED AND INSTALLED AS PER RI-53-00-15880 AND SB 747-53A2SDR UIEA2022092201038None · noneRH BS 1480 OUTER CHORD SPLICE FITTING HOLE #18 FOUND CRACK(<P>RH BS 1480 CRACKED HOLE (18) AT OUTER CHORD SPLICE FITTING REWORKED AND A FREEZE PLUG FABRICATED AND INSTALLED AS PER SB 747-53A2390 REV.01 NEW FASTENER INSTALLED AS PER SB 747-53A2390 REV.01</P>)SDR UIEA2022092901062None · noneLH BS 1480 LONGERON EXTENSION FITTING AREA 1EA CRACK WAS FOUND AT FASTENER HOLE #11 AT SKIN PNL DETAIL REFER FINDING RECORD(<P>LH BS 1480 NO.11 FASTENER HOLE OVERSIZE TO DIA 0.562" INCH AND REPLACED NEW BOLT AS PER AMM 20-51-01 REV.105 15 JUL 22 AND SB 747-53ASDR R61A2022102300667Doubler · corrodedCORROSION ON CO-PILOT COCKPIT FLOOR DOUBLER IN MULTIPLE LOCATION BETWEEN FR 07-12 AS MARKED.: REMOVED AND REPLACED CO-PILOT COCKPIT FLOOR DOUBLER REF EMB170 SRM 51-40-08 SEE WIPS AND TASKS FOR WORK ACCOMPLISHEDSDR R61A2022102300666Doubler · corrodedCORROSION ON PILOT COCKPIT FLOOR DOUBLER IN MULTIPLE LOCATION BETWEEN FR 07-12 AS MARKED. : PERFORMED PERMANENT REPAIR ON PILOT COCKPIT FLOOR DOUBLER BY SPLICING IN NEW SECTION BETWEEN FR 07-12. REF EMB ETD2022-170-030432 REV. A. SEE WIPS AND TASKS FOR WORK AC
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