JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 DALA2024070506769Doubler · corroded(LOG 0423759) SKIN DOUBLER, AT STA 1040, STR 2L-2R, HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED DOUBLER AT STA 1040 STR 2L-2R I.A.W. B737 SRM 51-40-02-0G AND DWG # 148A3110.SDR DALA2024070206725Skin · crackedAIRCRAFT 9567, DURING HCK AT QRO, WHILE PERFORMING THE AFT FUSELAGE AND EMPENNAGE INSPECTION PER WC 5300-2019, A CRACK WAS FOUND AFFECTING THE FUSELAGE SKIN AT Y=1087 AND L-14R. AN EXISTING SKIN SPLICE REPAIR IS ADJACENT TO THE DAMAGE REPORTED. CORRECTIVE ACTISDR FDEA202406300893Skin · gougedSKIN GOUGE AT FS 287 9.75 JUST INBOARD OF S-38L SHGN 26JUN24 06:50 IND SRM: 53-00-01-1A DAMAGE MEASURES 0.1 X 0.4 AND 0.075 DEEP. DAMAGE FOUND TO BE OUT OF LIMITS REF ABOVE SRM. INFO 26JUN24 21:35 ** ATTACHED TO WORK ORDER 00088805 ** REPAIRED GSDR CALA2024071602044Skin · dentedBIRD STRIKE. INSPECTION REQUIRED PER AMM. HIT UNDER CAPT NOSE UNDRSCREEN AT 210KTS 7K FT. FWD DENT EDGE IS X = 13" AND Y = 10" FROM THE CENTER AREA OF THE STATIC PROBE PORT CLOSE UP DENTS ARE ABOUT 6 IN LONG 3IN WIDE 1/4 DEEP AND 5 IN APART DENT 1 FWD DENT SDR R61A2024070400297Skin · handler errorAIRCRAFT DAMAGED FROM BELT LOADER AT FWD LH FUSELAGE BELOW L 1 DOOR FROM FRA 18 TO FRA 20 AND STR 20L TO 21L. REPAIRED IAW ETD2024-170-018077 ALSO REF VP-027009-2024 FOR WORK PERFORMED.SDR CALA2024090302344Skin · dentedDENT AT APPROX. STA 500G ON LT SIDE OF AIRCRAFT INSTALLED REPAIR PER SRM 53-00-01-2R-1 CREATED A DIP PER SRM PER TABLE 207, DIP 53-DIP THIS ITEM MUST BE MARKED AS A MAJOR REPAIR. DENT AT APPROX. BS 500G ON LT SIDE OF AIRCRAFT, ALL WORK ACCOMPLISHED FOR DENT SDR SWAA2024080507067Angle · crackedCRACK ANGLE LOCATED BS500I; STRINGER 28L; LBL 7 FWD CARGO COMPARTMENT 2024-402125<[01] REPLACED ANGLE LOCATED BS500I; STRINGER 28L; LBL 7 FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 SHEET 160 REV B SEE INDIVIDUAL SSDR SWAA2024071806641Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] CRACK WAS FOUND TO BE OUT OF LIMITS AS PER SRM 53-10-15-1A-5. TRIMMED OUT THE DAMAGED AREA OF THE EGPR SURROUND DOUBLER BS233 WL 175 8' ABOVE S-24R IAW SRM 53-10-15-2R-4 REPAIR 4 PARA 4(A-SDR SWIA202407120628Skin · puncturedTRANSFER FROM EAML 1373809 : FOUND PUNCTURE DAMAGE TO THE LEFT FWD FUSELAGE AFT PLUG SKIN PANEL AND STRINGER 22L.THE DAMAGE IS LOCATED BETWEEN FR 21 AND THE AFT PLUG FWD SKIN JOINT AND BETWEEN STRG 22L AND STRG21L. THE VERTICAL PUNCTURE IS 7.4" LONG AND 2.5" WSDR SWAA2024070307054Skin · delaminatedFUSELAGE PANEL 191D DELAMINATED AROUND PREVIOUS REPAIR.<[01] REMOVED DAMAGE PER SRM 51-70-05-2R-2.;[02] REPAIRED PANEL PER SRM 51-70-0502R-2.;[03] REQUIRES FINISH TOPCOAT.;[04] 1. DANIEL BATES (TECHNICIAN); 28-JUN-2024 17:56 UTC<BR>REMOVED DAMAGE PER SRM 51-70SDR SWAA2024070206840Doubler · crackedEGPR DOUBLER CRACKED AT DOOR CUTOUT<[01] PERFORMED REPAIR AT EGPR DOOR DOUBLER IAW SRM 53-10-15-2R-4 FIGURE 204 REPAIR 4. SEE BARCODE NUMBER TTG8Q00U2Y1K FOR MATERIAL ORDERED.SDR DALA2024070106641Access Panel · perforatedSHIP 3161 PERFORATION ON ACCESS PANEL 192KB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 592345-14 REV. ORIGINAL. (0418528)SDR KCSA202406281084Skin · damagedLOWER HALF OF FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE RIGHT SIDE APPROX STA 200 AND S-31ASDR SWIA2024092000019Skin · dentedMULTIPLE DENTS,NICKS, GOUGES ,ON AFT FUSELAGE SKIN IN BETWEEN APPROX FS 1000 TO FS 1051 BETWEEN STR 21R AND STR 27 IN AREA OF GROUND A/C SERVICE DOOR. (C-CHECK RO 9/19/2024) REPAIRED MULTIPLE DENTS,NICKS, GOUGES ,ON AFT FUSELAGE SKIN BETWEEN FS 1000 TO SDR CALA2024062801915Skin · dentedFUSELAGE SKIN DENTED BETWEEN STA 807 AND 827 AND BETWEEN STR 24L AND 25L. AN INTERIM REPAIR WAS ACCOMPLISHED PER ECRA 5360-01826 PART 1. PERMANENT REPAIR NEEDS TO BE ACCOMPLISHED ON OR BEFORE DEC 21, 2025 PER ECRA 5360-01826 PART 1 ITEM # 2. CREATING DIP PER ESDR SWAA2024080905721Skin · crackedCUSTOMER REQUEST- CRACK LOCATED ON CUTOUT ACCESS DOOR 114AR AT LOWER SIDE AT LOWER FUSELAJE 2024-414597<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC 500D S/ N 500X1693P030457 DUE DATE: 15-OCT-24.;[02] PERFORMED PERMANENT REPAIR LOCATED ON CUT OUT ACCESS DSDR R61A2024071800310Finger Doubler · corrodedWHILE IN HEAVY CHECK - FWD CARGO- DOOR CUTOUT LOWER FWD FINGER DOUBLER AREAS OF POSSIBLE CORROSION AS MARKED. REMOVED AND REPLACED FWD CARGO-DOOR CUTOUT LOWER FWD FINGER DOUBLE REF EMB SRM 51-40-08SDR GTIA2024062938199Skin · dentedLEFT SIDE OF FUSELAGE DENT JUST FORWARD OF FRAME 3 JUST BELOW LEFT SIDE STRINGER. RAF-01 CREATED-ACCOMPLISHED INSPECTION SOLUTION PER AIRBUS RDAF 81417892/002/2024 A. NO ADDITIONAL REQUIREMENTS. CAT A PERMANENT REPAIR PER AIRBUS RDAF 8141792/002/2024 A PAGE 2 SDR JR2R20240626127Doubler · corrodedSURFACE CORROSION AROUND WASTE BOX IN AFT CARGO COMPARTMENT AREA, I/B FORWARD CORNER OF BOX. REPAIRED.SDR FDEA202406260870Skin · crackedLOWER FUSELAGE SKIN CRACKED APPROX 1" LOCATED 10" FWD OF BS 1654.5 AND OTBD OF S36L. COMPLIED WITH E.A. # H-5310-T0379685 PT 11808. TITLE - FUSELAGE - MAINFRAME - REPAIRS DUE TO CONTAINER STRIKE, FUSELAGE SKIN, ST 1629-1702, S-36L TO S-36R AND STA 1678 FRASDR IXXA2024073102Skin · crackedCRACK FOUND IN FORWARD ENTRY DOOR AFT LOWER CORNER FUSELAGE SKIN EXTENDING FROM FASTENER IN 10 O'CLOCK POSITIONSDR IXXA202407310001Skin · crackedCRACK FOUND IN SKIN OF FORWARD SERVICE DOOR AFT LOWER CORNER EXTENDING OUT FROM FASTENER IN 2 O'CLOCK AND 8 O'CLOCK POSITIONSDR SWAA2024073005544Doubler · corrodedCORROSION ** AFT CARGO COMPARTMENT BILGE SKIN PREVIOUS DOUBLER REPAIR @ S-26R STA 807+5' MKD DOT<[01] ACCOMPLISHED REPAIR PER EA -24-153-01888 AT AFT CARGO COMPARTMENT BILGE STR 26R STA 807'+5'.;[02] VERIFIED STEP 1; 2<BR>TREAT AND PRIME C/W ON EA 24-153-01880SDR R61A2024070800301Skin · unknownDURING HEAVY CHECK MAINTENANCE FOUND PREVIOUS REPAIR SKIN AT JACK POINT REQUIRES INVESTIGATION. PREVIOUS REPAIR PATCH AT AFT JACK POINT HAS BEEN REMOVED AND NEW REPAIR INSTALLED IAW ETD2024-170-017068, HFEC INSP CARRIED OUT AT CUT -OUT AREA WITH NO FAULTS FOUNSDR DALA2024070106610Skin · corrodedL1 SERVICE DOOR, SKIN PANEL UNDER DOOR SILL HAS SEVERAL ATTACH FASTENER HOLES WITH CORROSION. REFERENCE SSI 53-61-23-02. NO PREVIOUS CORROSION REPAIRS ARE EVIDENT. COMPLIED WITH PRI 618803-14 REVISION O, 1, AND ER/A 618803-14 REVISION ORIGINAL. SEE NR 260 FOR SDR DALA2024070106609Skin · corrodedR2 SERVICE DOOR, SKIN PANEL UNDER DOOR SILL HAS SEVERAL ATTACH HOLES THAT ARE CORRODED. REF. SSI 53-61-24-02. NO PREVIOUS CORROSION REPAIRS NOTED. LOG-PAGE UPDATED @ 25JUN24 1314 UTC 02 CORR BY WOG 00227037 MSP 25JUN24 ATA 5331 RII: N ENTR 00015582 W SCEPTRE LSDR DALA2024062706577Skin · damagedAIRCRAFT 9567, FUSELAGE/SKIN/L1 DOOR GUST LATCH/CUTOUT/EDGE DAMAGE REPAIR. CORRECTIVE ACTION: ACCOMPLISH ER/A 618643-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. (LP 0413016)SDR DALA2024062606514Skin · gougedGOUGE WAS FOUND ON SKIN BS 1013. THE SKIN WAS REPAIRED IAW SRM 53-02-01-2R REP 1 PAR 5.B(5)(C) FIG 202 SHEET 15. PERFORMED VISUAL INSPECTION, INITIAL AND REPETITIVE, EVERY 8,000 CYCLES PER B717-200 SRM 53-02-01-2R PROCEDURE 1, REPAIR 1, STEP 6.A, TABLE 202. MSDR YENA2024062500905Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / LH SKIN / FR 13-15 / CANOPY AREA / DENT & GOUGE DAMAGE – TIME LIMITED REPAIR; REFERENCES: /1/ JETBLUE ECA-261 /2/ AIRBUS CANADA REO 500-53-11-240 /3/ AIRBUS CANADA CASE # 00155896 DESCRIPTION: ON 6/3/2024 IN BOS, A/C N3138JSDR SWIA2024070500624Skin · dentedFIVE DENTS/GOUGES LOCATED IN SKIN BAYS FORMED BY S29L AND S29R, FRAMES 91 AND 93. DAMAGE IS LABELED €ŒDAMAGE AREA 3€? FOR IDENTIFICATION PURPOSES. DAMAGE MEASUREMENTS ARE AS FOLLOWS:GOUGE/DENT #1- L= 1.09€?, W= 0.328€?, D= 0.027€? MAX DEPTHGOUGE #2- L= 0.SDR VNAA2024062711101Skin · puncturedPUNTURE/GASH IN AIRCRAFT SKIN NEAR PANEL 196DR. / REO 670-53-61-2302 REPAIR TO FUSELAGE SKIN PANEL AND FRAME BTW FS985.00 - FS1015.00 & BTW STR19R - STR22R.SDR DALA2024062406344Skin · crackedCRACK ON INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00307: INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R-1, CATEGORY A REPAIR. (LP #0409764SDR QXEA2024062500165Access Panel · damagedTAIL STRIKE DURING BALKED LANDING AND GO AROUND. REMOVED FROM SERVICE. APU FWD ACCESS PANEL (351GL) HAS DAMAGE FROM TAIL STRIKE CONTACT. APU AFT ACCESS PANEL (351HL) HAS DAMAGE FROM TAIL STRIKE CONTACT. FWD BOTTOM EDGE OF APU TAILCONE HAS DAMAGE FROM TAIL STRISDR FDEA202406230854Skin · damagedLOWER HALF OF FUSELAGE, BTW STA 1417 AND STA 1439, BTW STRG 33L AND 38L, WITH SCRATCH. LOWER FUSELAGE SKIN BTWN STA 1417/1439 AND STGR 33L/37R WAS REPAIRED IAW E.A. #:H- 5330-T0379538 (P1).SDR VNAA202406230011Skin · dentedFOUND PAINT/DENT DAMAGE BETWEEN FS 394 AND FS 409, STGR 18R TO STGR 19RSDR SWIA202409200018Skin · dentedFOUND DENT ON RHS OF REAR FUSELAGE, AFT OF GROUND AIR DOOR, APPROXIMATELY 13 INCH, PARALLEL TO AFT LOWER CORNER RADIUS.OF DOOR CUT-OUT. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. SDR DALA2024062506507Skin · dentedRIGHT SIDE BETWEEN BS 1621-1640 EXTERNAL SKIN DENTED AT INTERCOSTAL 13. DUE TO PREVIOUS REPAIR. REPAIRED IAW PRI 569586-14AD REV 0, PRI 569586- 14AD REV 1, PRI 569586-14AD REV 2, & ER/A 569586-14AD REV B.SDR AALA202406241776Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION WITH CRACK IN FUSELAGE SKIN AROUND LAVATORY BLOWER VENT AT STA 917, BETWEEN S21L AND S22L. REINFORCING REPAIR ACCOMPLISHED PER SRM 53-70-01-2R, REPAIR 3 AND EA 355418.SDR CALA2024062601904Skin · noneEXISTING DOUBLER AT FUSELAGE EXTERNAL SKIN FR 34 STR 43 REQUIRES INFORMATION/ECRA ABOUT EXISTING DOUBLER PER HAECO LCQ N/R 9298217/26217 GEN BY V080280 53-00-11-300-043 CRITERIA. NO DEFECTS NOTED ON DOUBLER. REPLACE SRI 53-21-11-205-073 TABLE 2, ZONE A, INSPECSDR R61A2024062600292Skin · corrodedDURING BI-WEEKLY INSPECTION FOUND WASTE DOOR CUTOUT SKIN CORRODED. REMOVED AND REPLACED CORRODED SKIN IAW ETD2024-170-017358 AND EMB 170/175 SRM 51-41-01 AND 51-41-02. ALSO REF VP-022217-2024 FOR WORK PERFORMED.SDR DALA2024062406453Skin · corrodedCORROSION EXTERNAL SKIN LOCATED ON DRAIN BTW FR 69 TO FR 70 AND STR 31R TO STR 32R AT LOWER FUSELAGE. REPAIRED PER A319 SRM 51-74-00.SDR DALA2024062406414Skin · nickedFUSELAGE SKIN JUST FWD OF RT AFT PAX DOOR NICKED. REPAIRED THE SKIN IAW PRI 618681-14 REV 0, PRI 6181681-14 REV 1, PRI 6181681-14 REV 2 AND ERA 618681-14 REV A.SDR KCSA202406211078Skin · damagedLOWER HALF OF FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE RIGHT SIDE APPROX STA 160 AND S-47SDR KCSA202406211077Skin · damagedLOWER HALF OF FUSELAGE SKIN HAS EVIDENCE OF LIGHTNING STRIKE RIGHT SIDE APPROX STA 160 AND S-39SDR SWIA20240620Skin · corrodedCORROSION AROUND MULTIPLE RIVET HEADS ON EXTERNAL SKIN FS939.00 - FS992.00 BETWEEN STGR20R & 22L. (MARKED IN RED) 28413806 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED CORROSION FROM FASTENER HOLES (6 PLACES), AND EVALUATED AS 'OUT-OF-LIMITS'. RECIEVED AND COMPLSDR 6RNA202408120001Skin · corrodedLEVEL 3 CORROSION FOUND BEHIND RIGHT PYLON LOWER DRAG ANGLE.SDR SWAA2024080503706Skin · corrodedCUSTOMER REQUEST-CORROSION PIT IN FUSELAGE SKIN BY FASTENER HOLE BS 907 S-25L. 8-16<[01] REMOVED CORROSION AT FUSELAGE SKIN BY FASTENER HOLE BS 907 S-25L FOUND TO BE WITHIN LIMITS PER REF SRM 53-00-01-1A-1; REMOVED AND INSTALLED NEW FASTENER; TREATED; PRIMED ASDR CALA2024062601903Skin · damagedFUSELAGE REPAIR AT BS 264-275 STR 4-6 LH REQUIRES A CATAGORY B REPAIR INSPECTION PER SRM 53-00-01-2R-3 REPAIR 3 TABLE 204. MAJOR REPAIR.SDR CALA2024062400066Skin · gougedFOUND DENT AND GOUGE ON LT AFT FUSELAGE JUST BEHIND PRESSURIZED AREA. APPROX STA 1040 STGR 11-12. PERFORMED REMOVAL OF DAMAGE PER SRM 53-80-01 REPAIR 7 REMOVAL OF DAMAGE. COMPLIED WITH STEP 4F HFEC INSPECTION REF NDT PART 6-51-00-00-23 OF CUTOUT EDGE, NO CRACSDR DALA2024062106308Doubler · corroded(LOG 0403864) CORROSION ON INTERNAL PRODUCTION DOUBLER BS 757 AND BS 797 BTW STRINGER 27LH-27RH AT AFT CARGO COMPARTMENT. INTERNAL PRODUCTION DOUBLER BS 757 AND BS 797 BTW STRINGER 27LH-27RH AT AFT CARGO COMPARTMENT WERE REPAIRED PER ER/A 618489-14 REV. ORIGIN
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