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 SWIA202005210857Doubler · corrodedAFT LAV WATER DRAIN SURROUND STRUCTURE CORRODED BETWEEN FS605 AND 621.00 AND STGR25R TO STGR26R. (C-CHECK) RO 5/16/2020 PERFORMED A MAJOR REPAIR BY REPLACING A DOUBLER BETWEEN FS605 AND 621.00, AND BETWEEN STGR25R TO STGR26R. P/N 601R43216-9 IAW CRJ200 SRSDR ASOA2020051103039Skin · damagedDURING C CHECK INSPECTION FOUND APU LOWER MOUNT STRUCTURE HAD CHAFE ON RIGHT SIDE CORNER AND 2 DENTS ON RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED DAMAGED SKIN ON APU MOUNT STRUCTURE.SDR DALA2021030101151Skin · damagedDURING CURRENT H CHECK A ROCK CHIP DAMAGE WAS FOUND ON FUSELAGE SKIN (P/N 141T3221-5) AT BS 385 AND S-38R. THE DAMAGE WAS OUT OF LIMITS OF B767-300 SRM 53-00-01-1A-1 AND IT WAS REMOVED BY TRIMMING THE SKIN. C/W ERA 585636-14. (LP 1535035)SDR CALA2020032100671Skin · crackedSUPPORT TASK - EA 5380-01178 REV A OP004, CRACKS FOUND AT STR 13AR BETWEEN STA 1660 AND 1665 APPROX 4.5" IN LENGTH. DETAIL REFER ATTACHED FIGURE REFER NR LP 9130664 (VENDOR) FX STA 1654 - 1668 STR 13AR SKIN REPAIRED AS PER SRM 53-80-01 REPAIR T DETAIL IV FIG 2SDR SWIA202005210838Plug · migrated3 EACH FREEZE PLUGS FOUND MIGRATED AROUND PANEL CUTOUT 132AL (C-CHECK) RO 5/19/2020 REPAIRED 3 OFF DISCREPANT FREEZE PLUGS COMMON TO PANEL CUTOUT 132AL IAW BOMBARDIER REO.SKYCARD AND FORM M-337 ATTACHED.SDR SWIA202005190829Skin · chafed* CHAFING ON EXTERNAL SKIN BETWEEN FS 349.00 AND FS 369.00, ABOVE AND BELOW STRG 23 (UNDER FWD SIDE POTABLE WATER SERVICING DOOR CUTOUT) (C-CHECK) RO 5/16/2020 BLENDED DAMAGED AREA ON RH EXTERNAL SKIN BETWEEN FS349.00 AND FS369.00 ABOVE AND BELOW STRG 23R SDR SIMA2020042218007Skin · damagedCHERRY MAX FOUND ON SKIN AT FR 28 AND STR 17 LH.-C/A-PAINT STRIPPED SKIN AT FR 28 AND STR 17 L/H AS PER 51-21-01. AIR CONDITIONING DUCTS BETWEEN WINDOW L/H #4-5 REMOVED FOR ACDCESS IAW AMM 21-20-04. BUSHING FABRICATED IAW ETD 2020-145-014213 AND SRM 51-10-07 (SDR SIMA2020042118006Skin · damagedCHERRY MAX FOUND ON SKIN AT FR 25 BTW FR 18-19LH.-C/A-PAINT STRIPPED SKIN AT FR 75 BTW FR 18-19 L/H AS PER CPM 51-21-01. CHERRY MAX REMOVED AND CUT OUT PERFORMED ON SKIN TO REMOVE DAMAGE. L/H FUSELAGE SKIN AT FRAME "25 BTW STRINGER "18 & 19, REPAIRED IAW. ETD2SDR 2020F00117Skin · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N514 DISCREPANCY: AFT CARGO BULK AREA, HAVE CORROSION ON SKIN AT BS 1540 THRU 1562, STRINGERS S28R-S29R CORRECTIVE ACTION: REPAIRED AFT CARGO BULK AREA SKIN AT B$ 1540-1562 IAW EO CONTROL # 19124SDR KCSA202003181026Skin · damagedEXTERNAL EMPANNAGE SKIN SHOWS DAMAGE @ STA 2521 TO 2595 RIGHT STRINGER 2 TO 3SDR KCSA202003181025Skin · damagedEXTERNAL EMPANNAGE SKIN SHOWS DAMAGE @ STA 2521 TO 2628 STRINGER 2 TO 3 LEFTSDR KCSA202003181024Skin · chafedSTA 2620 R/H VERT STAB TO BODY INTERFACE BODY SKIN IS CHAFFEDSDR SWAA2020042032529Skin · damagedDAMAGE ON FUSELAGE SKIN BS500C+9 BL0 UNDER ACCESS PANEL 191D. MARKED / REPAIRED PER: EA 20-153-00179 REV IR AND ATS ER 20-02254 REV IRSDR SWAA2020041437396Skin · dentedFUSELAGE SKIN HAS A PROTRUDING DENT AT BS400+6; 2.5' ABOVE S-18L. DENT MEASURES AT L=1.1'; W=.6'; Y=.006'; W/Y=100 / 'DAMAGE INSPECTED AND EVALUATED PER EA 1-753-36799 REV IR (ATS ER 20-02220 REV IR). REFER TO NRC U138485 FOR TRACKING.'SDR SWAA2020041441031Doubler · damagedEXISTING REPAIR DOUBLER INSTALLED HAS A MULTIPLE TOOLING MARK AT BS 377 TO BS 404 BETWEEN S-17L AND S-18L / EXISTING REPAIR DOUBLER AT BS 377 TO BS 404 BETWEEN S17L AND S18L WAS REPAIRED IAW ATS ER 20-02220 REV IR DATED 07APR20 AND EA 1-753-36799 REV IR.SDR SWAA2020041332277Skin · damagedFUSELAGE EXTERIOR SKIN REPAIR AT BS 302-310; STRINGER 17R-18R DOES NOT MEET SRM CRITERIA FOR FASTENER INSTALLATION AND ADEQUATE DAMAGE REMOVAL. / REMOVED FUSELAGE EXTERNAL SKIN REPAIR BS. 302-310 STR 17R/H-18R/H. REPAIRED PER ATS ER #20-02206 REV IR AND SWA EASDR FDEA202003170583Skin · gougedFUSELAGE EXT SKIN STA 1280 TO 1400 AND FROM S26L TO S26R HAS SEVERAL PREVIOUS BLENDS REPAIRED AREA PER EA# F-5310-T0352664-P1SDR SWIA2020042850412Skin · damagedLARGE AREA OF SKIN DAMAGE AFT OF LOW PRESSURE AIR ACCESS DOOR (172BR) RH SIDE BETWEEN FS 589.00 AND FS 605.00 FROM STGR 21R TO STGR 26R (48 MO INSP) RO 4/23/2020 ACCOMPLISHED CUTOUT AND REPAIR OF SKIN DAMAGE TO FUSELAGE SKIN BETWEEN FS 574 AND FS 621, STRISDR SWAA2020032634348Skin · crackedRES NRC D393391 CRACK IND FROM BS 706+7 TO 706+10 1' TO 2' ABOVE S-4L USING C SCAN 737 NDT MANUAL PART 6; 53-30-25 AND 737 NDT MANUAL PART 6; 53-30-18 / C/W EA 1-753-36731 REV IR; THIS IS A STAGE 1 APPROVED; CONTACT SERVICE ENGINEERING PRIOR TO THRESHOLD FOR SSDR JJBA2020032616018Skin · not reportedLOCATE THE CIRCULAR DOUBLER REPAIR AT FRAME 28, STRINGER 16R. REMOVE THE DOUBLER, REPORT THE SKIN CONDITION TO RTS FOR PERMANENT REPAIR INSTRUCTIONS AND DAMAGE TOLERANCE-BASED SUPPLEMENTAL INSPECTION REQUIREMENTS, AS NEEDED. ACCOMPLISH THE PERMANENT REPAIR. RESDR CALA2020032100659Skin · corrodedIN AFT CARGO AFT BULKHEAD ABOVE WATER DRAIN MAST HAS CORROSION REMOVE MAST AND CHECK LIMITS. (REF AAR NR 9759301) REMOVED DRAIN MAST. REMOVED CORROSION, HFEC AREA, NO CRACK ON DEFECT FOUND, TREATED, PRIMED AND TOP COAT AREA. FILL ALL VOIDS WITH POTTING COMPOUNSDR 2020F00115Skin · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N497 DISCREPANCY: AFT LOWER CARGO HAS CORROSION APROX S-35R STA. 1241 BELOW BODY DOOR OPEN PANEL INTERNAL CORRECTIVE ACTION: INSTALLED FILLER, DOUBLER & TRIPLER AFT LOWER CARGO APROX S355R STA 1241 BELOW BODY DOOR OPEN PANEL INTSDR FDEA2020031760574Skin · gougedFUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S30 TO S26L HAS SEVERAL PREVIOUS BLENDS AREA REPAIRED PER EA # F-5310-T0352664 P1SDR FDEA2020031760573Skin · dentedFUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S27R TO S29R HAS 4EA DENTS. REPAIRED AREA PER EA# F-5310-T0352664-P1SDR FDEA2020031760569Doubler · gougedFUSELAGE EXT BETWEEN STA 1540 AND STA 1560 AND BETWEEN S20L AND S22L PREVIOUS REPAIR HAS SEVERAL TOOLING MARKS REMOVED REPAIR AND REPAIRED AREA IAW FEDEX EA # F-5330-T0352692-P1SDR IPXA2020042054379Skin Panel · dentedINSPECTION TYPE:CEXTERIOR FUSELAGE HAS DENT FWD OF FR-3CHECKED SRM LIMITS IAW SRM 53-10-12 VERIFIED NO CRACKS IAW NTM 51-10-08SDR JJBA2020032615021Skin · damagedFOUND SEVERAL TOOLING MARKS BELOW ADF ANTENNA. INSTALLED REPAIR DOUBLER TO INTERNAL FUSELAGE BETWEEN FR42-FR44 STR1RSDR SWAA2020031742541Skin · crackedFUSELAGE SKIN HAS A CRACK INDICATION AT RIVET HOLE (FS 727C + 16") (STRINGER 4L) OF THE LOWER SKIN, LOWER FASTENER ROW REMOVED FASTNER, PERFORMED BOLT HOLE INSPECTION PER 737 NDT MANUAL 51-00-00, PROCEDURE 16, AND 53-30-05. CRACK CONFIRMED .040" LONG. SDR HNAA2020041500135Skin · crackedRH FR. 75 AREA HAS A SKIN CRACK ABOVE STR., 2R MARKED, SETTINGS: FREQ.
400KHZ, ANGLE: 291.1 DEG., H-61.3DB., V-77.6DB., FILTER: LO-PASS 500HZ.,
PROBE: 100-500KHZ....ACCOMPLISHED REPAIR OF FUSELAGE SKIN AT FR 75
STGR 2R IAW EMB 145 SRM 53-31-01 AND EO1-53-20SDR JJBA2020032614017Skin · not reportedLOCATE THE CIRCULAR DOUBLER REPAIR AT FRAMES 19-20, STRINGERS 15L-17L REMOVE THE DOUBLER, REPORT THE SKIN CONDITION TO RTS FOR PERMANENT REPAIR INSTRUCTIONS AND DAMAGE TOLERANCE-BASED SUPPLEMENTAL INSPECTION REQUIREMENTS, AS NEEDED. ACCOMPLISH THE PERMANENT RESDR SWIA202053700Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA-THERE IS A DENT ON RIGHT SIDE OF THE AIRCRAFT BELOW AND SLIGHTLY AFT OF THE APU EXHAUST. COMPLIED WITH TEMPORARY REPAIR, PER REO. PERMANENT REPAIR DUE IN 4000 FLT HRS. DUE BY TAT 41463.9, PART NUMBER: -, SERIAL NUMSDR CALA2020032100648Skin · corrodedCORROSION DAMAGE FOUND ON THE THE FUSELAGE SKIN AFT LAV SERVICE PAN, AT BS 1701 AND BETWEEN STRINGER 28R AND 29R. REMOVED AFT SE RVICE PAN. REMOVED CORROSION AND FABRICATED AND INSTALLED RPR DOUBLER PER ECRA 5331-02645. ALL WORK ACCOMPLISHED ON AAR-MIA NR 9759SDR U5QA202003130096Skin · corrodedDURING A,B,C INSPECTION DISCOVERED CORROSION ON BELLY OF ACFT, ALSO UNDER BASE OF SOME STATIC WICKS ON DELTA FIN. MX VENDOR WORKING WITH LOCAL DER FOR RESOLUTION/MAJOR REPAIRS AS REQUIRED. IN WORK AT THIS TIME.SDR P5CA2020031600065Skin · damagedFX STA 1840 - 1900 S-42L TO S-43L SKIN DAMAGED.(<P>FX STA 1840 - 1900 S-42L TO S-43L SKIN REPAIRED AS PER SRM 53-00-01-2R-1 AND RI 53-60-13958 REV A.</P>)SDR SWIA2020042750328Doubler · corrodedDOUBLER FOR ANTENNA IS CORRODED BETWEEN F.S. 295.00 TO F.S. 310.00AT STRG. 27 (C-CHECK) RO 4/23/2020 REPLACED ANTENNA DOUBLER BTWN FS295.00 & FS310.00 AT STGR 27 REF BOMBARDIER DWG, CRJ-900 SRM. COMPLIED WITH SKY CARD (CL600-2D24) STRUCTURAL MAJOR REPAIR SDR SWAA2020031942582Skin · crackedFOUND 12" CRACK ON FUSELAGE CROWN AT BS 500D-520 ABOVE STR 4R TRANSFERED FROM LOGBOOK 1096404 REPAIRED DAMAGE ON FUSELAGE CROWN AT BS 500D-D-520 ABOVE STR 4R IAW EA 1-753-36703 AND EA 1-753-36704 FACT AS A RESULT OF POST REPAIR INSPECTIONSDR UIEA2020031300382Skin · corrodedCORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1562/1582 AND STRINGER S-24L / S-25L, AT THE VACUUM OUTLET NOZZLE.(<P ><SPAN>FUSELAGE SKIN REPAIRED / PER SRM 53-60-01-2R-3 REPAIR 3. SEE RAM FORM N662GT-20-02.</SPAN></P>)SDR UIEA2020031300383Skin · dentedAN EVIDENT DENT DAMAGE WAS FOUND DURING THE INITIAL INSPECTION ON FUSELAGE SKIN STA 1197+88 / STA 119+110, AND BETWEEN STRINGER S-22L / S-24L.(<P >THE DAMAGE WAS REPAIRED IN / ACCORDANCE WITH B767-300 SRM 53-00-01-2R-1 REPAIR 1. SEE RAM FORM / N662GT-20-01.</PSDR C77A2020031200028Skin · damagedEO E175-53MR-282 REV IR WAS ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III LOWER SKIN BETWEEN FR77/FR78 AND S-29L/S-29R. THE CORROSION WAS FOUND AROUND 26 FASTENER HOLES AND WAS REMOVED BY BLEND OSDR SWAA2020032442724Doubler · damaged** CUSTOMER REQUEST ** EGPR EXTERNAL POWER RECEPTACLE DOUBLE (P/N 141A3722-12) IS DAMAGED AT LOWER HINGE ATTACHMENT REMOVED DAMAGE AND REPAIRED EGPR DOUBLER AND SKIN AT LOWER HINGE ATTACHMENT PER SRM 53-10-15-2R-5 REPAIR 5 FACT AS A RESULT OF POST REPASDR 2020FA0000207Skin · corrodedAIRBORNE/PEMCO NON-ROUTINE 2387N1046 DISCREPANCY: STA. 1417, STRGS 29L TO 33L BULK CARGO DOOR CUT OUT AT FUSELAGE SIDE HAS MULTIPLE AREAS OF CORROSION. CORRECTIVE ACTION: WORK ACCOMPLISHED IAW EA# 47359REA04 REV. IRSDR FDEA2020031210535Doubler · damagedAGING AIRCRAFT - EXISTING REPAIR AT FUSELAGE EXTERIOR - STATION 1019, LONGERON 37 RIGHT HAND TO LONGERON 38 RIGHT HAND. EXISTING REPAIR AT FUSELAGE EXTERIOR - STATION 1019 LONGERON 37 RIGHT HAND TO LONGERON 38 RIGHT HAND EVALUATED AND FOUND REPAIR DOUBLER SDR VNAA202003119991Skin · corrodedCORROSION FOUND ON OUTER SKIN UNDER FWD WATER DRAIN MAST. 2/15/20 (PCC) M/A: 1. CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-00-31. 2/15/20 C/A: 1. REMOVED CORROSION IAW CRJ200 SRM 51-21-06. 2/15/20 M/A: 2. UT INSPECTION REQUIRED TO DETERMINE REMAININSDR SWIA2020041750131Skin · corroded*FS559.00 €“ FS559.00+32 STGR 26LH €“ 26RH EXTERNAL SKIN HAS SEVERAL FASTENERS WITH CORROSION AROUND THEM (MARKED) (C-CHECK) RO 4/16/2020 REPAIRED CORRODED SKIN AND FASTENERS @ FS559.00 €“ FS559.00+32 STGR 26LH €“ 26RH REF REO. LEAK CHECK GOOD AT THISSDR SWAA2020041441030Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND AT BS 460; 1' BELOW S-26R / PREVIOUS BLEND AT BS 460; 1' BELOW S-26R REPAIRED IAW ATS ER 20-02222; REV IR; DATED 03-APR-2020 AND PER EA NO: 1-753-36794 REV IR 55981U 07APR20SDR SWAA2020033022256Skin · corroded***CORROSION*** ON LOWER BELLY SKIN OUTER SURFACE BS 500A+14 BETWEEN STR 28R-28L; BL0; WL 148 / REPAIRED FUSELAGE BELLY SKIN BS 500A+14 BETWEEN STR 28R-28L BL0 WL148 PER ER 20-02135 REV IR AND EA 1-753-36786 REV IRSDR IPXA2020033053633Skin · damagedINSPECTION TYPE:SVFUSELAGE SKIN DAMAGED BETWEEN STA Y= 1801 AND Y=1841 AND BETWEEN L-11L AND L-17L. PART # AFA3031-1 AND AGA3025-1.REPAIRED FUSELAGE SKIN BETWEEN STA Y= 1801 AND Y=1841 AND BETWEEN L-11L AND L-17L IAW VT-SAA EA# 011-5330-01-A8078-IR AND UPS EOSDR SWAA2020032442701Doubler · damagedEXTERNAL POWER DOOR DOUBLER IS DAMAGED REMOVED AND REPAIRED EXTERNAL POWER DOOR DOUBLER IAW ER 20-02141 REV IR AND EA 1-753-36764 REV IR FACT AS A RESULT OF POST REPAIR INSPECTIONSDR 7C7A2020032300005Skin Panel · gougedSKIN PANEL ON LEFT SIDE OF FUSELAGE HAS A DENT WITH A GOUGE. X387.35-X405.737 AND STR. 30P-31PSDR 7C7A2020032300004Skin · gougedFUSELAGE SKIN PANEL ON RIGHT SIDE HAS GOUGE DAMAGE.
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