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 SWIA202411120726Skin · dentedFOUND DENT TO BE 2 FEET ABOVE FORWARD CARGO DOOR. DENT MEASURES 3IN LONG BY .125 WIDE AND .004 DEEP SRM 53-00-01-101-001-A01 (C-CHECK RO 11/9/2024) REPAIRED AREA IAW REO 670-53-31-925 TASK CARD 53-900-1002 COMPLETE, M-337 ATTACHEDSDR SWIA202409160826Skin · crackedLH TRU DOOR FUSELAGE SKIN CUT OUT, THE AFT LOWER CORNER POSSIBLY CRACKED IN THE RADIUS (C-CHECK RO 9/15/2024) LH TRU DOOR FUSELAGE SKIN FOUND TO BE CRACKED, REMOVED AND REPLACED LH TRU SKIN WITH SERVICEABLE UNIT REF REO 690-53-11-1827 REV -- DATED 2024-SDR DALA2024072907536Skin · corrodedSEVERAL SPOTS OF CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, Y=674 TO 696, Y=696 TO 715, AND BTW X=45 TO X=60 AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00346: CORROSION LEVEL 2. WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, YSDR IXXA20240726001Skin · crackedR1 DOOR CUTOUT, AFT LOWER CORNER, ROTO SCAN SHOWS INDICATION AT SECOND HOLE FROM BOTTOMSDR HNAA2024091700828Skin · gouged00104 FUSE SKIN IS GOUGED AT FR73 STR20L. REPAIRED IAW EO1-53-24-0478SDR HNAA2024091100743Doubler · corroded53-2022 CORROSION ON EXTERNAL POTABLE WATER DOUBLER. RAR DOUBLER IAW SRM 51-40-02SDR HNAA2024081300692Skin · crackedE047453 EXTERNAL FUSELAGE SKIN HAS A CRACK AT RH DV WINDOW CUTOUT AFT UPPER CORNER. ACCOMPLIHSED FCD1-53-23-0183 CRACK AT RH DV WINDOW CUTOUT AFT UPPER CORNER DAMAGESDR DALA2024072507463Skin · damagedSHIP 3140 DAMAGED NOSE FWD FUSELAGE FR & SKIN AT FR8 LEVEL, BTWN Y175 & Y520, CLOSE TO JACKING POINT. CORRECTIVE ACTION: REPAIRED PER ER/A # 619030-14. (0463750)SDR YENA2024072501041Skin · corrodedDURING HEAVY MAINTENANCE: AFTER REMOVAL STRINGER 29RH CORROSION ON SKIN BTW FR73-74RH WAS FOUND; REF TOMX WO 2563 NR 00273. SKIN BTW STRINGER 29RH FR73-74 WAS REPAIR PER EMB 190 ETI-190-24-211 REV.: 1, ETD2024-190-018554 REV.: /, EC: E-24-895-01. COMPLETED BY:SDR YENA2024072501040Skin · corrodedDURING HEAVY MAINTENANCE: CPCP FINDING: CORROSION ON SKIN BTW FR 73/74 AND STGR 28R/28L AT AFT CARGO; REF TOMX WO 2563 NR 00158. CORROSION ON SKIN BTW FR 73/74 AND STGR 28R/28L AT AFT CARGO WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB 190 SRM 51-12-01, SRMSDR YENA2024072501036Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE II & III / FR 73-74 / STGR 28 RH TO 29 LH / LOWER SKIN / CORROSION – PERMANENT REPAIR; REFERENCES: /1/ TOMX ETI-190-24-211 REV 01 /2/ EMBRAER ETD2024-190-018554. DESCRIPTION: AT CURRENT (7/2024) BASIC 6 CHECSDR DALA2024072407439Skin · scratchedSHIP 3140 SCRATCH EXTERNAL SKIN LOC BTW FR 7 TO FR 8 LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 619030-14. (0462841)SDR SWAA2024090316061Skin · corrodedCORROSION AT AFT CARGO BILGE DOUBLER REPAIR INNER SKIN BETWEEN S-26L & 27L STA 847+11'INC MKD DOT<[01] ACCOMPLISHED REPAIR AT STA 847 BETWEEN S-26L AND S-27L AS PER EA 24-153-02189; REF: TTG8Q00VE474;[02] VERIFIED STEP 1SDR DALA2024072407441Skin · crackedCRACK ON EDGE EXTERNAL FUSELAGE SKIN STA Y=991 BTW LONGERON 26-24R AT FUSELAGE. SUMMARY OF NRC 00075: CRACK ON EDGE EXTERNAL FUSELAGE SKIN STA Y=991 BTW LONGERON 26-24R AT FUSELAGE WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 12. (LP #0461829)SDR CALA2024072402095Skin · dentedB757-06-3-0221 2 DENTS LWR AFT FUSELAGE STA 1480 AT KEEL BEAM DO OR. DOT 140-005. EVALUATED DENTS AT LWR AFT FUSELAGE STA 1480 DENT #1 L=1.870" W= 53-00-01-2R-28. .900" D=0.017" A/Y=52.9", DENT #2 L=1.480" W=.860" D=0.012" A/Y= 66.1, DENTS FOUND TO BE OUT OF LSDR U2RA2024110400066Skin · dentedDENT FOUND ON EXTERNAL FUSELAGE SKIN BTWEEN FR 28/29 STR 12/13LH. ASSEMENT WAS PERFORMED IAW 53.24.11.28.006 REPAIR IS A CAT B INSPECTION REQUIRED AT 32300 FC/107 400 FH FROM TIME OF ADL. HFEC IAW SRM 53.21-11-205-208SDR SIMA20240722001Skin · puncturedDWMS NRWC# E046819 - SKIN PUNCTURED BETWEEN FRAME 93 TO FRAME 94 AND BETWEEN STRINGER 21L TO 23L. (MAJOR REPAIR) REPAIRED IAW ERS-EJ-53MR-5020SDR DALA2024072407433Skin · unknownCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC BTW FR 57 TO FR58 AND BTW STR39LTO STR43L LOWER FUSELAGE ( REFERENCE DOC. AA C ARD 5100-01821-01A). C/A: PERFORMED REPAIR PREVIOUS COMPLETED ON 23-DEC-09. LOCATED BTW FR57 TO FR58 AT LEVEL STR39L SDR DALA2024072307385Access Panel · perforatedSHIP 3138 PERFORATION ON INTERNAL SKIN ACCESS PANEL 192KB AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 529512-14. (0459546)SDR FDEA202407211044Skin · gougedFOUND GOUGE AT TAIL CONE LOWER SURFACE FR92 PLUS 5.6", S-17R PLUS 3" CUT OUT THE DAMAGE AREA, FABRICATED THE REPAIR DOUBLER WET INSTALLED REPAIR DOUBLER WITH BLIND RIVETS AT TAIL CONE LOWER SURFACE FR92~93, S-17R~18R I.A.W A300- 600F SRM 53-19-12-201, PARA.SDR R61A2024072400320Skin · dentedLH FWD FUSELAGE BETWEEN FRAMES 10 AND 11 AND STR 15L TO 17L DENTED. REPAIRED DENT IAW ETD2024-170-004972 REVC, ALSO REF VP-029594-2024 N/R #1 FOR WORK ACCOMPLISHED.SDR CALA2024072502098Skin · corrodedFOUND CORROSION AROUND THE LAVATORY EXHAUST PORT PICTURES ADDED UPDATE PERFORMED HFEC PER 737 NDT PART6, PROCEDURE 23 ,ALONG CUT OUT EDGES. NO DEFECTS NOTED. PERFORMED STEPS A-D PARA 4 OF SRM 53-70-01-2R-3. HFEC REQUIRED AROUND EDGE OF DAMAGE TRIM OUT REF SRM SDR HNAA2024091200817Doubler · cracked2 CRACKS FOUND ON SKIN AT FR75 BETWEEN STR 1R-1L UNDER REPAIR DOUBLER. PERMANENTE REPAIR PERFORMED AS PER ETD2024-145-019639.SDR IPXA2024081766455Skin Panel · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT L/H UNDER FLOOR, STA 1140, MID SPAR (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1. REVIEWEDSDR IPXA2024081766354Skin Panel · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1100, S-20C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1. REVIEWEDSDR IPXA2024081766332Skin Panel · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+11", S-24C~S-25C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1 (REF. T3F18E004ZX7Q) PRIOR TO FURTHER FLIGHT. REVIEWEDSDR IPXA2024081766310Skin Panel · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1040 + 12", S-27C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1. REVIEWEDSDR IPXA2024081766287Skin Panel · corrodedCORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+6" S-25C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1.SDR IPXA2024081166455Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT L/H UNDER FLOOR, STA 1140, MID SPAR (REPAIR) CHECK NORMAL.SDR IPXA2024081166354Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1100, S-20C (REPAIR) CHECK NORMAL.SDR IPXA2024081166332Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+11", S-24C~S-25C (REPAIR) CHECK NORMAL.SDR IPXA2024081166310Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1040 + 12", S-27C (REPAIR) CHECK NORMAL.SDR IPXA2024081166287Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+6" S-25C (REPAIR) CHECK NORMAL.SDR SCNA20240805290Skin · damagedFS400 FWD CARGO DOOR CUTOUT FWD LOWER CORNER HAS DAMAGE. RESOLUTION: ACCOMPLISHED EXTERNAL SKIN REPAIR AT RH SIDE FUSELAGE FWD CARGO DOOR CUTOUT OWER CORNER IAW BOEING SRM 53-00-01-2R-21.SDR DALA2024072307420Skin · brokenSHIP 3731 - BROKEN CUTOUT SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE. SUMMARY OF NRC 00024: SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE WAS REPAIR PER B737-800 SRM 53-10-15-2R-5. (LP #0454660)SDR DALA2024072207352Skin · damaged(LOG 0454672) BROKEN CUTOUT SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE. SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R-5.SDR DALA2024071907296Skin · damagedSHIP 3140 DAMAGED NOSE FWD FUSELAGE FR & SKIN AT FR8 LEVEL, BTWN Y175 & Y520, CLOSE TO JACKING POINT. CORRECTIVE ACTION: REPAIRED PER ERA 619030-14. (0454265)SDR NACA2024071700002Skin · corrodedSURFACE CORROSION ON FUSELAGE EXTERNAL SKIN (AFT LAVATORY ACCESS PANEL1502 R L/E SIDE) BETWEEN BS998 AND BS1006 FROM S24R TO S25R. REPLACED ACCESS PANEL IAW AMM 52-49-6SDR SWIA202409250871Skin · wornLH SIDE APRON HAS WEAR ON EXTERNAL SKIN BETWEEN FS 513.00 - 559.00 FROM CONTACT WITH TRAILING EDGE UPPER AND LOWER SHROUDS (C-CHECK RO 9/24/2024) REPAIRED LH APRON SKIN PER REO 601R-53-41-115 (REV A) DATED 2005-07-20. AND REO 601R-57-51-1051 REV -- DATESDR HNAA2024091100740Skin · gouged53-2012 FR2, GOUGE FOUND 7" FWD OF FR7 2" ABOVE STR15L. REPAIRED IAW EO 1-53-24-0459SDR IPXA2024080449680Skin · corroded**SUPPLEMENTAL SDR**FAULT - CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O-100 BARE TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1821 SEQUENCE A PART A STEP 1.8) REV.0 ASDR IPXA2024080549718Skin · corrodedCORROSION - SKIN, AFT CARGO COMPARTMENT LOWER SKIN AT STA 1197+88~STA 1197+132 S-35R~S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1838 SEQUENCE A PART A STEP 1.8) REV.0 AND SPWPS-HT-008 REV.32 AND SPDS-HT-005 RESDR IPXA2024080249680Skin · corrodedCORRODED SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R. (REPAIR) I.A.W. EGAT EI NO.F2024A53M-1821 REV.2 SEQUENCE:C PAGE:1 OF 9 STEP:3.A.B, COMPLETED TO MACHINE THE BASE DOUBLER/FLAT FILLER THE THICKNESS FROM 0.125" TO 0.11SDR SWAA2024071813920Skin · crackedPERFORMED HFEC ON THE EDGE OF THE FUSELAGE SKIN CUTOUT FOUND; PER WIP1 STEP 6; AND FOUND A CRACK ON LOWER EDGE OF CUTOUT 15 AFT FROM FRAME 440. PERFORMED HFEC ON THE EDGE OF THE FUSELAGE SKIN CUTOUT FOUND PER WIP1 STEP 6 AND FOUND A CRACK ON LOWER EDGE OF CUTOSDR UIEA2024062000561Skin · dentedFUSELAGE SECTION 41 DENT/NICK DAMAGE FOUND ON FUSELAGE SKIN (PN 65B12874) AT STA 284 APPROXIMATELY NEAR STR 10R(<P>DAMAGE AREA REPAIRED AS PER RI-53-10-16982 REV.A (CAT A). NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024071707227Skin · wornWEAR ON EDGE SKIN AROUND HOOK AT L1 DOOR. SUMMARY OF NRC 00111: EDGE SKIN AROUND HOOK AT L1 DOOR WAS REPAIRED PER PRI 619136-14 REV 1 AND ERA 619136-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-619136 ADDED FOR AC 9524. (LP #0451426)SDR ASAA2024071551700Skin · corrodedMAJOR COROSION ON FUSELAGE AND AROUND BLOWER MOTOR EXHAUST. (REF ALASKA CARD NUMBER N/R-00029, HAECO N/R# 9929). GROUNDED - YES. REMOVED REPAIR I.A.W B737-800 SRM 51-40-02, CORROSION FOUND TO BE ON REPAIR PARTS ONLY REPAIR PARTS OUT OF LIMITS WITH MATERIAL LOSSDR HNAA2024080900658Doubler · corrodedE045597 FUSELAGE SKIN INTERNAL DOUBLER BETWEEN FRAME 60 AND FRAME 61 AND STRINGERS 19L AND 20L HAS CORROSION. REMOVED UNSERVICEABLE INTERNAL FUSELAGE SKIN DOUBLER BETWEEN FRAMES 60-61 AND STRINGERS 19L-20L IAW EMB 145 SRM 51-40-02.INSTALLED NEW INTERNAL FUSESDR CALA2024072302091Skin · damagedCUSTOMER PICKUP SHEET PLEASE REMOVE AND REPLACE DOUBLER AT STA 2000-2017 SRE 30L-33L. DUE TO NO RECORD OF REPAIR REFER HX NR WO. 3460850 AND ORIGINAL BY V940359.SDR CALA2024071600205Skin · damagedLIGHTNING STRIKE DAMAGE, 0.5 INCH AFT STATION 500J BTW STRINGER 27L & 27R REMOVED LIGHTNING STRIKE DAMAGE REF. SRM 53-00-01-2R-38 4-D-(2) HFEC REQUIRED REF. SRM 53-00-01-2R-38 4-D-(3) ACP. HFEC IAW WITH SRM 53-00-01-2R-38 STEP 4D (3) & B737 NTM PART 6 51-00-0
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