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 SWAA2021032458179Skin · dentedDENT EXTERNAL SKIN LOCATED AT BS363 AND 7 INCHES BELOW STR 6R UPPER FUSELAGE EXTERIOR / REPAIRED DENT ON EXTERNAL FUSELAGE SKIN LOCATED BETWEEN BSTA 360 AND BSTA 380 AND BTW S-6R AND S-7R UPPER FUSELAGE IAW E.A.#53-0089-21 REV.0 AND SWA E.A. NO.21-153-00680 RESDR JJBA20210301005Skin · canningOIL CAN FOUND ON LH SKIN BTW FR 22-23 AND STR 11L-12L. DAMAGE REPAIRED.SDR DALA2021030401219Access Panel · corrodedDURING INITIAL INSPECITON MANTENANCE FOUND LEVEL 2 CORROSION ON ACCESS PANEL 165BL (POTABLE WATER SERVICE) SKLIN. REPAIRED PER ERA 590285-14. (LP 1742922)SDR SWIA2021071459502Tripler · chafedREPAIR TRIPLER CHAFED AT FS 969.00 TO FS 985.00 STRGR 27 CHAFED AREA .042" DEEP. (C-CHECK RO 7/10/2021) REPAIRED TRIPLER CHAFE AT FS 969.00 TO FS 985.00 STR 27 IAW REO 670-53-00-290 REV F, DATED 2019/04/26. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHSDR CALA2021030100247Skin · cracked63-5530-1-2500 L/H EXTERIOR FUSELAGE SKIN STA 1654.5 BETWEEN STR INGER 3L-4L IS CRACHED VERIFIED WITH HFEC REPAIRED CRACKS AT STA 1654.5 BETWEEN S3-4LT IAW 767 SRM 53-80-0 1REPAIR 4 AND REA 47451REA 05 AND ECRA 5380-01277.SDR CALA2021030100246Skin · crackedRH EXTERIOR FUSELAGE SKIN AT STA 1660 STRINGER 13R SKIN IS CRACK ED REPAIRED CRACK AT STA 1660 AND 13R IAW 767 SRM 53-80-01 REPAIR 7 .SDR CALA2021030100245Skin · crackedSUPPORT TASK AFT EXTEROR R/H FUSELAGE SKIN STA 1654.5 BETWEEN STRIGNER 3R-4R IS CRACKED.(VERIFIED WITH HFEC SURFACE SCAN) AFT EXTERIOR RH FUSELAGE SKIN STA 1654.5 TO STRINGER 3R-4R ID 0717075T6 PO# 0167028 TAG# 2760222 FILLER MAT''L ID .032 707ST6 IAW B767 SRSDR JR2R20210228688Spacer · corrodedACCESS PANEL 192BL SPACER CORRODED BEYOND LIMITSSDR JR2R20210228Panel · corrodedACCESS PANEL 192CR CORRODED OUT OF LIMITSSDR SWIA2021071459469Skin · dentedTRANSFERED FROM CAMP # 22354978 - AFT FUSELAGE LOWER SKIN AT FS 1035.00 STR L 22 AND STR L 23 SKIN IS DENTED 1 INCH LONG X .7 X .040 DEEP. (C-CHECK RO 7/10/2021) REPAIRED DENT ON AFT FUSELAGE LOWER SKIN AT FS 1035.00 STR 22L AND 23L IAW CRJ 700 SRM 53-0SDR SWIA202157026Skin · gougedMULTIPLE SKIN GOUGES AROUND THE LP GROUND AIR CONNECTION ACCESS DOOR 182BR FILED CLOSED REPAIRED MULTIPLE SKIN GOUGES AROUND THE LP GROUND AIR CONNECTION ACCESS DOOR 182BR IN REF. TO REO 670-53-61-1836 REV. -- DATED 2021-03-22. COMPLETED 51-900-1002-SKYSDR ASAA2021022734347Doubler · corrodedANTENNA DOUBLER IS CORRODED BETWEEN F/S 500 TO F/S 500A AND BETWEEN S28L & S28R ON INNER SURFACE GROUNDED - YES. REMOVED & REPLACED ANTENNA DOUBLER IAW 737-700 SRM 51-40-02-0G-0 W=1.5 O=.040 R=.033 L=3 D=.067SDR FDEA202102270498Splice · corrodedUPON REMOVAL OF SHEAR TIE STA 1400 BETWEEN S26L - S27L,FOUND CORROSION ON INTERNAL FUSELAGE SPLICE STRAP. REMOVED INTERNAL FUSELAGE SPLICE STRAP AT AFT CARGO STA 1400 BETWEEN STR 26L TO TO 27R IAW B 757 SRM 51-40-02-OG,UPON EVALUATION FOUND CORROSION 100% MSDR SWIA202156592Skin · puncturedPUNCTURE HOLE ON RIGHT SIDE OF FUSELAGE BETWEEN THE SERVICE DOOR AND WING. APPROXIMATELY 2 INCH BY 2 INCH HOLE. FLIGHT 5217 - FILED CLOSED INSPECTED AND FOUND CRACK/PUNCTURE DAMAGE TO SIDE FUSELAGE SKIN (DWG 601R38321, 0.045" / THK IN CHEM MILL POCKET & SDR IPXA2021022766156Skin · damagedINSPECTION TYPE:N/ART FUSELAGE SKIN REPAIR AT STA 2598 & BELOW STR 26RREPAIRED IAW UPS E.O. B747-5330-79437-A, ITEM IS TIME LIMITED PER THE E.O. AND WILL BE DEFERREDSDR SWIA2021071459501Skin · dentedTRANSFERED FROM CAMP 22355031 AFT FUSELAGE LOWER SKIN AT FS 1015.00 TO FS 1051.30 STR 27 TO STR 24R MULTIPLE DENTS IN FUSELAGE SKIN. (C-CHECK RO 7/10/2021) REPAIRED RH AFT FUSELAGE SKIN AT FS 1015.00 TO FS 1051.30 AT STG 27 TO STG 24R IAW REO 670-53-61SDR AALA202103029026Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION AROUND AFT LAVATORY EXHAUST VENT. CORROSION OF FUSELAGE SKIN AROUND AFT LAVATORY EXHAUST VENT AT STA 1968 BETWEEN STR 35L AND STR 36L, MEASURING L=5.0 IN, W=2.5 IN, D=0.1 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR ISDR DALA2024080407738Skin · crackedSHIP 3236 DISC: WHILE WORKING 5312-01183 (A320-53-1372), VISIBLE CRACK FOUND IN FR35 AFFECTING HOLES #6,#7,#16, AND #17. IN ADDITION, CRACKS FOUND IN EXTERNAL FWD SKIN PANEL AND AFT (SIDE) PANEL. C/A: DTE REQUIRED PER SECTION DTE II OF 589595-14AD, THE AFT SKISDR DALA2021072804239Skin · crackedCRACK FOUND IN HOLE #16 IN FWD SKIN PANEL AND AFT (SIDE SHELL) PANEL. CORRECTIVE ACTION: INSPECTED PER ERA 589749-14AD REV A. OK FOR CONTINUED SERVICE. CONTINUE ON MON. (1739780)SDR N6WA2021022505Doubler · corrodedCORROSION LEVEL 2 ON ANTENNA (ATC) DOUBLER BETWEEN FS295 AND FS310 @ STRINGER 27.R&R ANTENNA DOUBLER BETWEEN FS295 AND FS310 & STR 27 IAW CRJ 700 SRM 51-42-06.SDR UIEA2021022200390Skin · dentedAIRCRAFT DAMAGE LOG ITEM D19-001 - DENT 1.5" X 0.03" SMOOTH CRACK FREE W/I LIMITS PER SRM 53-00-01-1A STICKER INSTALLED #30369.(<P>DENT AREA REPAIRED AS PER RI-53-11-14364 REV A.</P>)SDR CALA2021022500228Skin · crackedEXTERNAL POWER RECEPTACLE DOOR CUT-OUT CRACKED AT LOWER SIDE. (REF NR 9613289) ACCOMPLISHED REPAIR AT EXTERNAL POWER RECEPTACLE CUT-OUT LOWER SIDE IAW B737-900 SRM 53-10-15 REPAIR 4 PG 211 ADD EMP:V900442.SDR JR2R20210225815Spacer · corrodedACCESS PANEL 192BL SPACER CORRODED OUT OF LIMITSSDR SWIA202157784Skin · damagedUPON REMOVAL OF FWD FUSE SKIN PANEL 600-33052-145, FOUND ELONGATED HOLE IN FWD CORNER OF SKIN PANEL AT APPROX FS 173, WL 73.50. (C-CHECK RO 4/25/2021) REPAIRED IAW MHIRJ REO 601R-53-11-3669 REV-- DATED 2021-03-22 COMPLETED SKYCARD 51-900-1003-SKY (CL600SDR NACA2021032200004Skin · crackedDISCREPANCY: 1.25 INCH CRACK AT BS907+7.25 INCHES, STR25R. CORRECTIVE ACTION: INSTALLED REPAIR PER SRM 53-00-01, REPAIR 31 DETAIL XXVIII.SDR NACA2021032200003Skin · crackedDISCREPANCY: 1 7/8 INCH CRACK AT BS927 + 6 3/4 INCHES, STR25R. CORRECTIVE ACTION: INSTALLED REPAIR PER SRM 53-00-01 REPAIR 31 DETAIL XIX.SDR KCSA202102241012Skin · damagedEVIDENCE OF DAMAGE ON RIGHT EXTERNAL FUSELAGE SKIN AT APPROXIMATELY BS 2450 WL 280.SDR KCSA202102241011Skin · damagedEVIDENCE OF DAMAGE ON LEFT EXTERNAL FUSELAGE SKIN AT APPROXIMATELY BS 2450 WL 280.SDR SWIA2021071459473Skin · corrodedAFT FUSELAGE LOWER SKIN AT FS 1051.00 STR 27 TO STR R 26 JUST AFT OF REAR HEATED MAST SKIN IS CORRODED. REPAIRED DAMAGE IAW REO 670-53-1848 REV -- DATED 2021-04-23. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHEDSDR IXXA20210402333Skin · corrodedAFTER CLEANING INBOUND SIDE OF CENTER TANK AREA FOUND CORROSION ON UPPER SKIN AREA AT STA 952, BETWEEN 8 TO 12 INCH FROM FUSELAGE SKIN TO INBOUND SIDE. ACCOMPLISHED REPAIR ON CENTER WING SKIN AT STA 952 IAW FAS EA 21019 REV 1R, FVCI E0 21011-4 REV B AND 8110-3SDR SWAA2021040152239Skin · wornWEAR ON EXTERNAL SKIN CLOSURE ANGLE LOCATED BS 1132.02 APPROX RH SIDE AT UPPER FUSELAGE / PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN CLOSURE ANGLE LOC BS 1112 TO BS 1132 RH SIDE AT UPPER FUSELAGE IAW B737-700 53-80-71-2R-6 REPAIR 6 AND SRM 51-40-02 MATERIAL USDR SWIA202157024Skin · gouged*GOUGE ON INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS 559.00+16 - 559.00+32 (C-CHECK) RO 3/24/2021 BLENDED OUT GOUGE ON INTERNAL FUSELAGE SKIN BETWEEN STGR 27 - 26R, FS559.00+16 - 559.00+32. REF: CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF CRSDR DALA2021030101121Skin · dentedDURING DECAL INSPECTION MAINTENANCE FOUND DENT OUT OF LIMITS BTW STA 590-620 AT FWD CARGO DOOR IN REF LOG 3525323. REPAIRED PER SRM 52-30-01. (LP 1736433)SDR DALA2021022301053Skin · gougedSHIP 3252 GOUGE EXTERNAL SKIN LOC. BTW FR 50 TO FR 51 STR 40L TO STR 42 AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-42-11 AND A320 SRM 51-72-11 AND ER/A 589897- 14 REV. ORIGINAL AND PRI 589897-14 REV.0. OK FOR SERVICE. (1737427)SDR IPXA2021022265932Skin · dentedINSPECTION TYPE: SEG 2 FUSELAGE SKIN AT STA 500-530 STR 19L-20L HAS INCOMING DENT DAMAGE. REPAIRED PER EA 757-5330-27-A2548 REV-.SDR CALA2021022200211Skin · crackedRIGHT EXTERIOR FUSELAGE SKIN AT STA 1660 STRINGER 13R SKIN IS CRACKED. REPAIRED CRACK AT STA 1660 AND 13R IAW 767 SRM 53-80-01 REPAIR 7. SEE PARTIAL WORK ACCOMPLISHED FOR WORK PERFORMED. LOG PAGE OPEN. MORE DETAILS AWAITED.SDR DALA2024072907591Skin · unknownSHIP 5813 ERA 590190-14 ISSUED FOR REPAIR TO FUSELAGE SKIN AT STATIONS 154 0-1560, BETWEEN STRINGERS 27R TO 29R. CORRECTIVE ACTION: REF ERA 590190-14. (1736037)SDR SIMA20210221005Skin · not reportedSKIN SECTION FROM FRAME 11 (FACTORY SPLICE) TO FRAME 18 (FACTORY SPLICE) AND FROM STRINGER 20L TO BETWEEN STRINGERS 24L-25L REQUIRES REMOVAL PER ETD2021-170-004959.-C/A-REPAIRED IAW ERS-EJ-53MR-4290.SDR MK1Y20210221035Skin · dentedEXTERNAL FUSELAGE SKIN – 3 BULGES AND A DENT WERE FOUND ON EXTERNAL FUSELAGE SKIN BETWEEN STA 434-456 STR 26L-28L. THE DAMAGES ARE LOCATED WITHIN THE EXTRA CRITICAL AREA AROUND THE STATIC PORT AS NOTED IN SRM 51-10-01 GENERAL FIG 3 (SHEET 3 OF 4) DETAIL IV EXSDR MK1Y20210221032Skin · damagedREPAIR – FUSELAGE SKIN STA 1263 – 1270, STR-32R-33R & 27R-29R, SECTION 46; PN 146T3510. SHOP FOUND EXISTING BLEND OUT AREAS NAMED M0054 AND M0055 AT FUSELAGE SKIN IN THE NOTED LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLSDR MK1Y20210221029Skin · damagedREPAIR EXTERNAL FUSELAGE SKIN BETWEEN STA 287 – STA 406, STR - 1R/4R, AND STA 266 – STA 348, STR 5R-7R, (SECTION 41). MULTIPLE BLEND OUTS AND LIGHTNING STRIKES WERE FOUND ON EXTERNAL FUSELAGE SKIN BETWEEN STA 287-406 STR 1R-4R AND STA 266 – STA 348, STR 5R-7RSDR MK1Y20210221028Skin · damagedINNER FUSELAGE SKIN PANEL STA 1193 BETWEEN STR-28L AND 29L, PN 146T3252-1: AN EXISTING DEEP GOUGE WAS FOUND AND WAS BLENDED OUT AS PER SRM B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. AFTER THE BLEND AND DRILL OUT (0.250"), THE MEASURED MINIMUM FUSELAGE SKIN THSDR MK1Y20210221027Skin · damagedEXTERNAL FUSELAGE SKIN AT STA 1417, BETWEEN STR-31L/33L, SECTION 46. SHOP FOUND 9 BLEND OUTS IN FASTENERS ZONE IN FUSELAGE SKIN AT THE DATUM LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENERS AREA.SDR MK1Y20210221026Skin · damagedFUSELAGE SKIN EXTERNAL FUSELAGE SKIN AT STA 632, STR-26R SECTION 43. SHOP FOUND BLEND OUT IN FASTENERS ZONE IN UPPER SKIN OF LAP JOINT IN FUSELAGE SKIN AT THE DATUM LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENSDR MK1Y20210221024Skin · corrodedREPAIR – FUSELAGE SKIN (SECTION 45), BETWEEN STA 999 AND STA 1043, BETWEEN STR 2L AND STR 2R AS PER COSTUMER REQUEST SATCOM ANTENNA WAS DEACTIVATED AND DISMANTLED FROM THE AIRCRAFT. THE ANTENNA WAS MOUNTED TO AN ADAPTER PLATE AT DATUM LOCATION. UNDER ANTENNASDR MK1Y20210221023Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 1347 AND STA 1387, BETWEEN STR-28R AND STR 33R, SECTION 46. SHOP FOUND FIVE (5) EXISTING BLENDOUTS AREAS NAMED NRC: M0062, M0065, M0066, M0069 AND M0151 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERSDR MK1Y20210221021Skin · damagedEXTERNAL FUSELAGE SKIN, STA 1535, STR 20L – 22L P/N 146T3340. SHOP FOUND AN EXISTING BLENDOUT AREA NAMED M0153 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUT FALL ON ASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLESDR MK1Y20210221020Skin · damagedEXTERNAL FUSELAGE SKIN AT STA 1417 STR 36L AND STA 1567, STR-37L, (2EA REPAIR LOCATIONS) SECTION 46. SHOP FOUND EXISTING BLENDOUTS AREAS NAMED NRC: M0086 AND M0099 AT FUSELAGE SKIN IN THE NOTED LOCATION. BLENDOUT M0086 IS LOCATED 1.1 INCHES FROM SPLICE JOUNT.SDR MK1Y20210221019Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 343 AND STA 350, STR-22R, SECTION 41. SHOP FOUND FORE (4) EXISTING BLENDOUTS AREAS NAMED NRC : M0048 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1SDR MK1Y20210221018Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 450.5 AND STA 478, STR-26R/32R, (3EA REPAIR LOCATIONS), SECTION 43. SHOP FOUND THREE (3) EXISTING BLENDOUTS AREAS NAMED NRC : M0032, M0038 AND M00040 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZO
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