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 SWAA2020081707808Skin · dentedDEFT TRANSFERRED FROM CARD 9841860=FUSELAGE EXTERNAL SKIN HAS A DENT LOCATED AT BS 1016+5'; 1' ABOVE STRINGER 14 L/H; DENT MEASURES L=2.7'; W=1.1'; Y=0.026' W/Y=42 / DENT TRANSFERD FROM CARD 9841860; FUSLAGE EXTERNAL SKIN HAS DENT LOCATED @ BS 1016+5'; 1' ABOVSDR SWAA2020081707535Skin · dentedFUSELAGE EXTERNAL SKIN HAS A DENT LOCATED AT BS 1016+6'; 1' BELOW STRINGER 14 L/H; DENT MEASURES L=0.9'; W=0.7'; Y=0.009' W/Y=77 / FUSELAGE EXTERNAL SKIN DENT @ BS 1016+6'; 1' BELOW STR 14L/H DAMAGE REPAIRED & EVALUATED PER EA 20-153-01365 REV IR DATED 08/09/2SDR K11A2020080300005Skin · corrodedCORROSION ON INTERNAL SKIN BY #1 FASTENER HOLE OF REMOVED DRAIN MAST LOCATED @ STA 986-1006 BETWEEN STR 24L & 25LSDR SWAA2020081707807Skin · dentedFUSELAGE SKIN HAS A DENT BS 420+12; 2' BELOW STR 18L. DENT MEASURES L= 1; W= 1; Y= .026'; W/Y= 38 / REPAIRED SKIN DENT AT BS 420+12; 2' BELOW STR18L PER EA 20-153-01372 REV IR AND ER 20-03032 REV.IR.SDR A8ZR20200723001Skin · damagedAPU COWLING ASSY FWD MID SKIN LAP LWR CORNER EDGE HAS CURLED UP EDGE AT STA 26461.57. STRAIGHTENED SKIN, PERFORMED HFEC NO DEFECTS NOTED AT THIS TIME. INSTALLED DOUBLER 2.1" X 2.4" REF EMBRAER TECHNICAL DISPOSITION ETD2020-145-022629 REV.:/ DTD JULY 21, 2020. SDR KCSA202007221126Skin · corrodedAFT CARGO BILGE, APROXIMATELY BS 1630, LBL 6, HAD CORROSION AROUND A DOME NUT ON FUSELAGE SKIN.SDR IPXA2020072258102Skin · dentedINSPECTION TYPE: SEG1, FUSELAGE LT SIDE, HAD A DENT IN THE SKIN AT BS 215.25, WL 214.48. REPAIRED IAW EO B757-5330-77084.SDR MASA20200722055Skin · gouged(C-CHECK) GOUGE FOUND ON SKIN UNDER TCAS ANTENNA FS-295-FS310 STGR 27. REPAIRED I/A/W EA 70-2020-118.SDR MASA20200722054Buttstrap · corroded(C-CHECK) CORROSION ON BUTTSTRAP BS 280, STGR 25L-25R. REPAIRED IAW EA 70-2020-120.SDR SWAA2021081002897Doubler · corroded***CORROSION*** ON FORWARD CARGO BAY ANTENNA DOUBLER AT B.S. 500A+11; B.L. 0; W.L. 147. / REMOVED AND REPLACED ANTENN DOUBLER AT BS500A+11; BLO; IAW SRM 51-40-2; SRM 51-40-05; SRM 51-40-06; DWG 143A3233SDR SWIA202008252058Skin · dentedDENT ON FUSELAGE SKIN LOCATED AT APPROXIMATELY AT FS348 STRG24L. REPAIRED DENT AREA PER WITH REO.SDR SWIA2020082552057Skin · dentedDENT ON FUSELAGE SKIN LOCATE BEWEENT FS280 & FS295 AND STRG25R & STRG26R. REPAIRED THE SKIN, COMPLIED WITH ALL STEPS OF REO.SDR SWIA202008252056Skin · dented4EA DENTS ON FUSELAGE SKIN LOCATED BETWEEN FS310 & FS333 AND STRG24R & STRG26R. CUT OUT DAMAGE, DRESSED BACK DENTS, AND INSTALLED DOUBLER REF REO.SDR SWIA202008252055Skin · dentedDENT LOCATEDON ON FUSELAGE SKIN BETWEEN FS333 & FS349 AND STRG25R & STRG26R. ) / CUT OUT DAMAGE, DRESSED BACK DENT, AND INSTALLED DOUBLER REF REO COMPLIED WITH SKY CARDSDR IPXA2020082159277Skin · corrodedL/H FUSELAGE SKIN HAS CORROSION AROUND HORZ, BODY FAIRING BETWEEN STA. 2140-2163 @ L33L. REPAIRED CORRODED SKIN ON L/H FUSELAGE SKIN BETWEEN STA. 2140-2163 @ L33L IAW SRM 53-70-01 REPAIR 3 FIG. 201. (MAJOR)SDR IPXA2020081459039Skin · corrodedINSPECTION TYPE:3CRT AFT FUSELAGE SKIN BETWEEN STA 1997.750 - 2163.681 AND BETWEEN LONGERONS 31R - 35R HAS CORROSION.REPAIRED RT AFT FUSLAGE SKIN CORROSION BETWEEN STA 1997.750 - 2163.681 AND BETWEEN LONGERON 31R - 35R IAW VT-SAA EA 011-5330-01-A8459 REV. IR ASDR IPXA2020081098821Skin · corrodedINSPECTION TYPE:C3, LT FUSELAGE SKIN HAS CORROSION AROUND HORIZONTAL BODY FAIRING BETWEEN STA 2140 - 2163 LONG 33L.REPAIRED CORRODED SKIN ON LH FUSELAGE SKIN BETWEEN STA 2140 - 2163 LONG 33 IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)SDR SWIA2020090152089Skin · corroded* EXTERNAL FUSELAGE SKIN LOWER CENTER AREA APPROX. FS 559.00 + 96 HAS CORROSION AROUND DRAIN HOLE. (C-CHECK) RO 8/28/2020 REMOVED CORROSION AROUND DRAIN HOLE AT APPROX. FS 559.00+96 EXTERNAL FUSELAGE SKIN LOWER CENTER AREA. REF: CRJ-200 SRM. ORIGINAL THISDR SWIA2020090152088Skin · corroded* EXTERNAL FUSELAGE SKIN LOWER CENTER AREA APPROX. FS 559.00 + 16 HAS CORROSION AROUND DRAIN HOLES AND RIVETS. ( MARKED ) (C-CHECK) RO 8/28/2020 REMOVED CORROSION AT EXTERNAL FUSELAGE SKIN LOWER CENTER AREA FS 559.00+16 AROUND DRAIN HOLES AND RIVETS. REF:SDR FDEA2020081201865Skin · damagedUPPER CARGO DOOR JAMB, FUSELAGE SKIN DAMAGED AT FWD LWR AREA REAIRED PER SRM 53-50-00 FIG.026SDR SWAA2021041502386Doubler · crackedDVI OF EGPR PER EA 20-153-01146 FOUND NO DAMAGE GEYOND THAT NOTED GVI OF AREA AROUND EGPR HAS POSSIBLE CRACK ON LOWER DOUBLER / REPAIRED LOWER DOUBLER REF SRM 53-10-15-2R-4SDR SWAA2020072202385Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER IS CRACKED ON FWD SIDE BETWEEN DOOR HINGES. TRIMED OUT DAMAFED OFTHE EGPR DOUBLER PER EA 20-153-01146 PART 1.SDR SWIA2020090152087Skin · corroded* MILD SURFACE CORROSION DETECTED ON (L & R) SIDES OF THE FWD JACKING FITTING FWD OF F.S. 280.00 IN (3EA) PLACES. (1EA) AT L/H SIDE FITTING INTERCOSTAL "FLANGE" AND F.S. 280.00 "FLANGE" INTERSECTION, (1EA) AT L/H FITTING INTERCOSTAL "FLANGE" APROX 2" FWD OF F.SDR SWAA2020080302162Skin · damagedDAMAGED FASTENER HOLE COMMON TO UPPER FLANGE OF FRAME AT BS 480; STRINGER 26L; WL 162. / REPAIRED DAMAGED FASTENER HOLE COMMON TO UPPER FLANGE OF FRAME AT BS480; STRINGER 26L; WL162 IAW SRM 53-30-07-2R-1 56693U 24JUL2020SDR CALA2020072001066Skin · dentedUPPER FUSELAGE FWD OF THE L1 DOOR WAS DENTED AT FRAME 15. EVALUATED DENT IAW SRM 53-00-11-283-005. DENT MEASURES 1.1"X1.1" X .020" DEEP. DENT IS IN RIVETED STIFFENED AREA AND IS CATEGORY C. DENT MUST BE REPAIRED WITHIN 200 FLIGHT CYCLES IAW PARAGRAPH 2.A.(1) SDR NACA2020080500013Skin · cracked3 CRACKS DISCOVERED AT BS460+6.5 ABOVE STR10R, BS500A+8.5 AND BS500A+12.5 DURING THE ACCOMPLISHMENT OF AD 2012-26-02. REPAIRED SKIN IAW EA-PD37-53-3157, REV B.SDR NACA2020080500012Skin · crackedDISCREPANCY: 3 CRACKS INDICATED AT BS620+4 BELOW STR2R 1 5/8" LONG DISCOVERED DURING ACCOMPLISHMENT OF AD 2011-24-12. REPAIRED IAW EA PD37-53-3173, REV 1R.SDR 2020FA0000336Skin · dentedON POST FLIGHT INSPECTION, FOUND A DENT ON BELLY OF THE ACFT AT BS 1793. REMOVED & REPAIRED THE STRINGERS 39R & 39L & INSTALL EXTERNAL DOUBLER REPAIR IAW SRM 53-00-05, 51-40-02 & EO 20306 REV. ASDR SWAA2020080600993Skin · damagedBS 927 - 947 INTERCOSTAL LOWER FLANGE FWD 2 HOLES COMMON TO SKIN ELONGATED / DRILLED (2EA) HOLES AT INTERCOSTAL FLANGE IAW SRM 51-40-05 FIG. 3+0 .228. 91195U 7-16-20. AT STA. 927-947 RBL3 WL175 91195U 7.16.20. 2EA HOLES WILL BE INSTALLED ON NRC U192866. 91195USDR IXXA20200720033Skin · dentedAIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. ON POST FLIGHT, FOUND A DENT ON THE BELLY OF THE AIRCRAFT AT BS 1793 BETWEEN STRINGERS 39L AND 39R. REPAIRED IAW SRM 53-767-7169.SDR SWAA2021082510156Skin · corrodedADF NO. 1 ANTENNA FASTENER HOLES HAVE CORRROSION - BS679-BS701; RBL1-RBL9; WL308.5 / REPAIRED SKIN UNDER ADF ANTENNA BS679-701 RBL1-RBL9 IAW EA 20-153-01236 REV IR AND ER 20-02930 REV IR.SDR SWAA2020081006553Skin · dentedDENT ON FUSELAGE SKIN BS360+2' 5' BELOW STR 4L REF NRC V474386 / DAMAGE REPAIRED PER EA 20-153-01291 REV IR AND ATS ER 20-02933 REV IR. REFER TO NRC U188571 FOR TRACKINGSDR SWAA2020072001657Skin · dentedON WALKAROUND FOUND DENT IN FUSELAGE. DENT IS LOCATED AT STA 259 AND STR 17L. DENT MEAUSURES 6.5 INCHES LONG; 5 INCHES WIDE; AND 0.120 INCHES DEEP. W/Y=41.7 SEE NRC #D418059 FOR OPEN-UP / REPAIRED DENT PER EA 20-153-01123SDR CALA2020072001057Skin · dentedLH NOSE FUSELAGE SKIN FWD AND ABOVE THE L1 DOOR BETWEEN S-5L AND S-6L AT APPROX STA 272 HAS A DENT THAT MEASURE 1.7"X 3.7" X .022" DEEP. ACCOMPLISHED PART 1 AND PART 1A OF ECRA 5330-06406.SDR DALA2020071762600Skin · damagedUPPER FUSE SKIN FASTENER HOLE OVERSIZED AT IDTV ATTACHMENT HOLE NR 6, FS 1370. REPAIRED PER ERA 587209-14.SDR SIMA202007165003Skin · gougedEXTERNAL FUSELAGE SKIN IS GOUGED BETWEEN FRAMES 74-75 AND STR 12L-13L. PERFORMED PERMANENT REPAIR ON LT FUSELAGE EXTERNAL SKIN BETWEEN FR 74-75 AND STR 12L-13L IAW ERS-EM-53MR-4132. REPAIR MATERIALS: DOUBLER AL2024-T3, 0.050 FILLER - AL2024-T3, 0.040.SDR EE4Y2020071511498Skin · nickedDURING THE AIRCRAFT STRUCTURAL INSPECTION, WAS FOUND AT SECTION 43 FUSELAGE SKIN BETWEEN BS 360 AND BS 420 AND BETWEEN STRINGER 27R-27L SKIN WITH NICKS. IT WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER SERVICE REQUEST 4-4703561547 AND EO NUMBER COO-EO-2020SDR FDEA2020081841902Access Panel · debondedDEBONDED ACCESS PANEL 121CF IN FWD AVIONIC COMPARTMENT MANUFACTURED ACCESS PANEL 121CF AS PER DWG SRZ 25-005 REV. RSDR SWAA2020072700652Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 679 RBL 5 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.SDR SWAA2020072700651Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 683 RBL 2;RBL 9 AT FASTENER HOLES. INBETWEEN STRINGER 1R AND 2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.SDR SWAA2020072700650Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 694;RBL 9 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND STR2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.SDR SWAA2020072700649Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 701; RBL3 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / REPAIRED UPPER EXTERIOR FUSELAGE SKIN PER ATS ER 20-02895; REV IR; PER EA 20-153-01151; REV IR.SDR SWIA2020091652496Skin · dentedCOMPLIED WITH SCHEDULED MAINTENANCE CODE: RA, DENT ON RT FWD FUSELAGE SKIN BETWEEN FS 202.75 AND FS 220.00 AND BETWEEN STR 16R AND STR 17R. COMPLIED WITH TEMPORARY REPAIR PER REO. PERMANENT REPAIR WITHIN 2600 FLIGHT HOURS DUE BY TAT 34476.7, PART NUMBER: - ,SDR SWIA2020090252163Skin · damagedAFTER DETAILED INSPECTION ON THE FUSELAGE SKIN SURROUND FOR ATTACHING PNL. 131 AL, FOUND ONE EACH REPAIRED HOLE'S FREEZE PLUG NOT SEATED. REQUIRES REPAIR. C-CHECK RO 8/29/2020. PANEL 131AL HAD A DAMAGED/LOOSE FREEZE PLUG AND REPAIRED IAW BOMBARDIER REO. COMSDR SIMA202007162004Skin · chafedFUSELAGE SKIN INSIDE RT PYLON ACCESS PANEL 424DB IS CHAFFED. REPAIRED FUSELAGE SKIN CHAFE INSIDE RT PYLON ACCESS PANEL 424DB IAW ERS-EM-53MR-4134 REV ORIGINAL.SDR U2RA202007110001Skin · corrodedDURING ACCOMPLISHMENT OF DAMAGE TOLERANCE INSPECTION FOR SATELITE COMMUNICATION SYSTEM ANTENNA DOUBLER, CORROSION WAS NOTED ON THE SKIN INTERIOR AT BODY STATION 1480 FROM STRINGER S-10L TO STRINGER S-11L. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLESSDR U2RA202007100001Skin · damagedDURING ACCOMPLISHMENT OF TASK CARD 53-804-01-01, EXISTING BLEND REPAIR NOTED ON SKIN AT LOWER FUSELAGE STA 1801 S-38R TO S-39R. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC, ENGINEERING ORDER NUMBER 20288.SDR SWAA2020081005317Skin · dentedDENT ON FUSELAGE SKIN BS259+6' 2' ABOVE STR 17L REF L110399 AND C029806 / REPAIRED PER EA 20-153-01179 REV IR AND ATS ER 20-02868 REV IRSDR SWAA2020081005316Skin · dentedDENT ON FUSELAGE SKIN BS 328+8.5' 1' ABOVE STR 26R REF 9667278 / REPAIRED PER: EA 20-153-01183 REV IR AND ATS ER 20-02869 REV IRSDR U2RA202007090001Skin · crackedDURING ACCOMPLISHMENT OF BOEING SERVICE BULLETIN 747-53A2390, CRACKED FASTENER HOLES WERE NOTED AT SKIN PANEL UNDER LONGERON EXTENSION FITTING 1 EACH BODY STATION 1480 STRINGER S-32L AND 1 EACH AT BODY STATION 1480 BETWEEN STRINGERS S-32R AND S-34R. REPAIR AC
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