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 SWAA2020051878116Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND BS 360+12; 4' BELOW STR 27R / PREVIOUS BLEND ON FUSELAGE SKIN BS 360+12; 4' BELOW STR 27R REPAIRED IAW ATS ER 20-02521; REV IR; DATED 12-MAY-2020 AND PER EA NO: 20-153-00497 REV IR 55981U 13MAY20SDR SWAA2020051445117Skin · gougedEXTERNAL FUSELAGE SKIN HAS A GOUGE AT BS 1006 + 9.5'; 1' BELOW STRINGER 14 L/H / EXTERNAL FUSELAGE SKIN GOUGE AT BS 1006+9.5'; 1 BELOW STRINGER 14 L/H REPAIRED IAW ATS ER 20-02505; REV IR; DATED 11-MAY-2020 AND PER EA NO:20-153-00493 REV IR. 55981U 11MAY20SDR UIEA2020042800852Doubler · damagedINSPECTION REPAIR #2 AND #3 AT STA 480-505 STR 37R-38R.(<P>FUSELAGE SKIN AT STA 480 TO STA 505, STR 36R-39R, 2 EA EXISTING DOUBLER REPAIRED AND INSPECTION IAW RI-53-10-14009 REV. A.</P>)SDR UIEA2020042800874Rivet · burnedFX-LH FWD UPPER STA 134.75 - STA 140 STR 19L, 1 EA RIVET HEAD FOUND BURN MARK.(<P>FX-STA 136 LH STR 19, 1 EA FASTENER HEAD BURN MARK REPAIRED IAW RI-53-10-14000 REV. A. </P>)SDR UIEA2020042800875Skin · burnedFX-LH FWD UPPER STA 140-160, STR 14B-14C, SKIN FOUND BURN MARK.(<P>FX-STA 157 LH, STR 14B-14C, SKIN BURN MARK REPAIRED IAW RI-53-10-14000 REV. A. </P>)SDR UIEA2020042800876Rivet · burnedFX-LH FWD UPPER STA 140-160, STR 14E- STR 19L, 2EA RIVET HEAD FOUND BURN MARK.(<P>FX-STA 146 AND STA 149 LH STR 14E-19, 2EA FASTENER HEAD BURN MARK REPAIRED IAW RI-53-10-14000 REV. A.</P>)SDR UIEA2020042800877Rivet · burnedFX-LH FWD UPPER STA 140-160, STR 19L - STR 20L, 1EA RIVET HEAD FOUND BURN MARK.(<P>FX-STA 152 LH STR 20L, 1 EA FASTENER HEAD BURN MARK REPAIRED IAW RI-53-10-14000.</P>)SDR UIEA2020042800885Skin · burnedFX-LH FWD UPPER STA 160-180, STR 14B-14C, SKIN FOUND BURN MARK(<P>FX-STA 167.5 LH, STR 14B-14C, SKIN BURN MARK REPAIRED IAW RI-53-10-14000 REV A.</P>)SDR UIEA2020042800886Rivet · burnedFX-LH FWD UPPER STA 160-180, STR 14E, 1EA RIVET HEAD FOUND BURN MARK.(<P>FX-STA 175 LH STR 14E, 1EA FASTENER HEAD BURN MARK REPAIRED IAW RI-53-10-14000 REV A. </P>)SDR UIEA2020042800887Skin · burnedFX-LH UPPER ST 160-180, STR 15L-19L, SKIN FOUND BURN MARK.(<P>FX-STA 71 LH, STR 15-19, SKIN BURN MARK REPAIRED IAW RI-53-10-140000 REV. A. </P>)SDR UIEA2020042800888Skin · burnedFX-LH FWD UPPER STA 180-300, STR 14D-14E, SKIN FOUND BURN MARK.(<P>FX-STA 201 LH, STR 14D-14E, SKIN BURN MARK REPAIRED IAW RI-53-10-14000 REV A.</P>)SDR UIEA2020042800889Skin · burnedFX-RH FWD UPPER STA 180-200, STR 14B-14C, SKIN FOUND BURN MARK.(<P>FX-STA 189.5 RH, STR 14B-14C, SKIN BURN MARK REPAIRED IAW RI-53-10-14000 REV A. </P>)SDR UIEA2020042800890Skin · burnedFX-RH FWD UPPER STA 180-200, STR 16R, SKIN FOUND BURN MARK.(<P>FX-STA 185.5 RH, STR 15R-16R, SKIN BURN MARK REPAIRED IAW RI-53-10-14000 REV. A.</P>)SDR KCSA202004241051Skin · crackedEVIDENCE OF CRACK AT FASTENER LOCATION AT L/H NWW CUTOUT AFT CORNERSDR IPXA2020052635671Skin · corrodedINSPECTION TYPE:3CRT AFT FUSELAGE EXTERIOR SKIN HAS CORROSION BETWEEN STA 2140 - 2163.ACCOMPLISH PERMANENT REPAIR ON CORRODED RT AFT FUSELAGE SKIN BETWEEN STA 2140 - 2163 IAW MD-11 SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)SDR SWAA2020051844761Doubler · crackedEXTERNAL POWER DOOR CUTOUT LOWER AFT CORNER OF EXTERNAL POWER CUTOUT SURROUND DOUBLER IS CRACKED / REPAIRED EXTERNAL POWER DOOR CUTOUT LWR AFT CORNER PER ER 20-02517 REV IR AND EA 20-153-00519 REV IRSDR SWAA2020051878115Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND AT BS 224.8'; 13' ABOVE S-24R / FUSELAGE SKIN PREVIOUS BLEND AT BS 224.8'; 13' ABOVE S-24R REPAIRED IAW ATS ER 20-02509; REV IR; DATED 12-MAY-2020 AND PER EA NO: 20-153-00523 REV IR 55981U 13MAY20SDR SWAA2020051877663Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND AT BS 312; 3' BELOW S-26R / PREVIOUS BLEND ON FUSELAGE SKIN BS312; 3' BELOW S-26R REPAIRED IAW ATS ER 20-02538; REV IR; DATED 12-MAY-2020 AND EA NO:20-153-00420 REV IR. 55981U 12MAY20SDR SWAA2020051877664Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND AT BS 312; 3' BELOW S-27L / PREVIOUS BLEND ON FUSELAGE SKIN BS312; 3' BELOW S-27L REPAIRED IAW ATS ER 20-02533; REV IR; DATED 12-MAY-2020 AND EA NO:20-153-00417 REV IR. 55981U 12MAY20SDR CALA2020042400871Skin · chafedFUSELAGE CROWN SKIN BSTA2112 TO BSTA2150 STR 2L FOUND CHAFING MA RK - REFER NON-ROUTINE L/P 9411578 - ORIGINATED S PEC NO.B777-06-3-7179. PERFORMED FUSELAGE CROWN SKIN STA2108-STA2150 ST R1L-STR3L REPAIRED AS PER SRM 53-70-01 REPAIR 2 FIG 202 REV 82 A ND ECRA SDR CALA2020042400870Skin · chafedFUSELAGE CROWN SKIN STA2108 TO STA2150 FOUND CHAFING MARK - REFE R NON-ROUTINE L/P 9411580 - ORIGINATED SPEC NO.B 777-06-3-7179. UPDATE INFO. THE POSITION IS BSTA2108 TO BSTA2150 STR 2R. PERFORMED FUSELAGE CROWN SKIN STA2108 TO STA2150 STR 2R AREA CARRIED OUT SDR IXXA20200519014Skin · crackedAIRCRAGT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-53-730-00-02 "GVI - EXTERNAL - EXTERIOR SECTION 48 - RIGHT SIDE", THE FOLLOWING FINDINGS WERE NOTED: AFT RIGHT EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. REPAIRED EXTESDR SWIA202005190785Skin · damagedCOMPLY WITH REPAIR TO FUSELAGE SKIN FOR CAMPS 20724547 (91509244/111), 20724552 (91509244/112), 20724556 (91509244/113), 20840027 (91509244/182) (C-CHECK) RO 5/16/2020 COMPLIED WITH PERMANENT REPAIR FUSE SKIN REF REO, VERIFIED ALL STEPS COMPLIED WITH, COMPSDR CALA2020042400863Skin · crackedFOUND CRACK AT EXTERNAL POWER RECEPTACLE FWD FLANGE APROX 3/4DOWN FROM TOP TO BOTTOM REPAIR EXTERNAL POWER RECEPTACLE IN REF SRM 53-10-15 REPAIR 5. DIP ITEM PER SAME SRM REFERENCE STEP 5 A(1)(2)(3) . AT A THRES HOLD OF 50.000 FLIGHT CYCLES AFTER AIRPLANE DELIVSDR FDEA2020042310767Skin · dentedLOWER FUSELAGE EXTERNAL SKIN ,STA 1592.7 BETWEEN S22R-S23R DENTED REPAIRED PER B757 SRM 53-00-01-2R REPAIR 29SDR FDEA2020042310763Skin · dentedOBSERVED SMALL DENT AND SCRATCH ON FUSELAGE. LEFT HAND SIDE BELOW CAPTS L2 WINDOW. REF WRI 56-10-5113, HFEC THE DENT ON NOSE SECTION OF AIRCRAFT, LEFT SIDE BELOW L3 WINDOW. MEASURED SDR SWIA2020072951562Doubler · corrodedDURING REMOVAL OF WASTE PANEL ACCESS DOOR, FOUND CORROSION ON DOUBLER SURROUNDING WASTE PANEL CUTOUT. COMPLIED WITH TEMPORARY REPAIR PER ETD.SDR IPXA2020052255603Panel · crackedINSPECTION TYPE:3CL/H UNDERWING BARREL CANTED PANEL CRACKED AT STA X=1236.8 Z=100.ACCOMPLISHED PERMANENT REPAIR OF CRACKED LH UNDERWING BARREL CANTED PANEL AT STA 1236.8 IAW EO.MD11-5310-76331-A REV 05/18/2020. (MAJOR)SDR IPXA2020052255567Skin · dentedINSPECTION TYPE:2CL/H FUSELAGE SKIN DENT AT STA 337 REQUIRES PERMANENT REPAIR.REPAIRED L/H FUSELAGE SKIN DENT BETWEEN STA 322 - 339 AND BETWEEN Z=-2 - Z=-20 IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 201. (MAJOR)SDR IPXA2020052255626Skin · dentedINSPECTION TYPE:2CRT FUSELAGE SKIN DENT BETWEEN STA 330 - 348 AND Z=-2.9 - Z=9.312 REQUIRES PERMANENT REPAIR.REPAIRED RT FUSELAGE SKIN DENT BETWEEN STA 330 - 348 AND Z=-2.9 - Z=9.312 IAW VT-SAA EA 011-5330-01-A8172 REV IR AND UPS EO MD11-5330-76584-A. (MAJOR)SDR IPXA2020052255625Skin · dentedINSPECTION TYPE:2CLT FUSELAGE SKIN HAS A DENT AT STA 357 ABOVE Z=-2.9 REQUIRES PERMANENT REPAIR.REPAIRED LT FUSELAGE SKIN DENT BETWEEN STA 339 - 357 ABOVE Z=-2.9 IAW VT-SAA EA 011-5330-01-A8179 REV IR AND UPS EO MD11-5330-76576-A. (MAJOR)SDR IPXA2020052055565Skin · dentedINSPECTION TYPE:2CL/H FUSELAGE SKIN DENT AT STA 330 REQUIRES PERMANENT REPAIR.REPAIRED L/H FUSELAGE SKIN DENT BETWEEN STA 322 - 348 AND Z=-30 - Z=-40 IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 201. (MAJOR)SDR IPXA2020052055564Skin · dentedINSPECTION TYPE:2CL/H FUSELAGE SKIN DENT AT STA 283 REQUIRES PERMANENT REPAIR.REPAIRED L/H FUSELAGE SKIN DENT BETWEEN STA 280 - 308 AND BETWEEN Z=5 - Z=22 IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 201. (MAJOR)SDR SWAA2020050543660Skin · canningRAMP REPORTED SMALL DENT UNDER APU INLET STA 1052 BETWEEN STRINGER 20R AND 21R / FUSELAGE SKIN REPAIRED DUE TO OIL CANNING CONDITION AT DENT LOCATION STA 1052 BETWEEN S-20R AND S-21R IAW SRM 53-80-01-2R-5 REPAIR 5.SDR MASA20200420010Skin · damagedFUSELAGE SKIN DAMAGE BETWEEN STGR 6R -STGR 7R FROM RAM AIR WATER TUBESDR SWAA2020042043487Doubler · crackedEXTERNAL POWER DOOR CUTOUT DOUBLER IS CRACKED AT THE AFT LOWER CORNER / REMOVED DAMAGE AT EXTERNAL POWER DOOR CUTOUT DOUBLER AT THE AFT LOWER CORNER PER REF B737 SRM 53-10-15-1A-4SDR ASAA2020041846291Skin · dentedRAMP REPORTS DENT NEAR AFT L/H FUSELAGE, FR 59 THRU FR 60 STRG 39-40, MEASURES 0.017" DEEP. 1.5" FROM FR. GROUNDED - YES. EVALUATED DENT, DEPTH .009, LENGTH 1.00, WIDTH 1.3, NEAREST STIFFNER 1.6, LOCATION BETWEEN FR 59 AND FR 60 AND STR 36L AND STR 40L AT WATESDR YENA2020042280315Skin · dentedDURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN LOC FR 4 TO FR 5 AND 5 INCHES BELOW R/H SIDE STRINGER AT LOWER FUSELAGE; REF AEROMAN N/R 2020-100283, PERFORMED PERMANENT REPAIR IAW EC NO. A20-401-01 AND EA # 53-0291-20 PART 1 AND PART 2 AND AIRBUS RDAS 8076776010SDR ABXR2020050600031Skin · crackedAFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01 REPAIR 4.SDR SWAA2020050445931Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND BS 420+6.5; 1.5' ABOVE STR 26 L/H / BLEND ON FUSELAGE SKIN AT BS420+6.5; 1.5' ABOVE STR26L WAS REPAIRED IAW ATS ER 20-02461 REV IR DATED 29APR20 AND EA 20-153-00381 REV IRSDR SWAA2020050445932Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND BS 420+16; 1.5' ABOVE STR 26 L/H / 'DAMAGE REPAIRED AND EVALUATED PER EA 20-153-00381 REV IR (ATS ER 20-02461 REV IR). REFER TO NRC U151409 FOR TRACKING.'SDR SWAA2020050445933Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND BS 400+6; 1' ABOVE STR 26 L/H / PREVIOUS SKIN BLEND AT BS400+6; 1' ABOVE STR 26L WAS REPAIRED IAW ATS ER 20-02461 REV IR DATED 29APR20 AND EA 20-153-00381 REV IRSDR SWAA2020050445935Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND BS 500+10; STR 25 L/H / PREVIOUS SKIN BLEND AT BS500+10; STR25L WAS REPAIRED IAW ATS ER 20-02461 REV IR DATED 29APR20 AND EA 20-153-00381 REV IR.SDR SWAA2020050445936Skin · damagedFUSELAGE SKIN HAS A PREVIOUS BLEND BS 500A+8; .7' ABOVE STR 25 L/H / PREVIOUS BLEND ON FUSELAGE SKIN AT BS500A+8; .7' ABOVE STR25L WAS REPAIRED IAW ATS ER 20-02461 REV IR DATED 29APR20 AND EA 20-153-00381 REV IRSDR SWAA2020043042830Skin · corroded***CORROSION*** FUSELAGE SKIN HAS CORROSION AROUND BELLY DRAIN VALVE; BS 500B+6; BELOW STR 27 L/H / FUSELAGE SKIN DAMAGE AROUND BELLY DRAIN VALVE; BS 500B+6 BELOW STR 27 L/H. REPAIRED PER 737-700 SRM 53-30-01-1A-1. INSTALLED DENT DOT PER MPM 52.03.01.02SDR SWAA2020043042831Skin · corroded***CORROSION*** FUSELAGE SKIN HAS CORROSION AROUND BELLY DRAIN VALVE; BS 500B+2.5; 6.5' BELOW STR 28 L/H / FUSELAGE SKIN DAMAGE AROUND BELLY DRAIN VALVE; BS 500B+2.5'; 6.5' BELOW STR 28 L/H. REPAIRED PER 737-700 SRM 53-30-01-1A-1. INSTALLED DENT DOT PER MPM 52SDR ABXR2020042300020Skin · corrodedALC STA 1065 LOWER INTERNAL SKIN AND STRINGERS BETWEEN FUSELAGE DRAINS HAVE SURFACE CORROSION. BLEND OUT REQUIRED AT CORRODED AREA, REMOVED CORRODED AREA AT LOWER FUSELAGE SKIN STA 1080 TO STA 1131, STRINGER 38L TO 38R IAW B767-200 SRM 53-60-01 ALLOWABLE DAMAGSDR SWAA2021081043131Access Door · corrodedCORROSION ACCESS DOOR 311BL INTERNAL LOCATED ON 4 INCH LOWER EDGE; 9 INCH AFT EDGE AND 13 INCH UPPER EDGE AT LOWER FUSELAGE / REPLACED ACCESS DOOR 311BL AFT LOWER FUSELAGE IAW AMM B737-700 52-49-11-400-802 AND SRM B737-700 51-10-02 ITEM 9SDR COEA2020050409901Skin · corrodedWO 212701 NR 200141 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE AFT CROWN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN STRINGERS 4R-4L. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0118056_01...16219 ISSUE A, DATED 4/29/2020.SDR 2A6D20200415001Deck Plate · chafedTHE TRANSMISSION DECK SKIN HAS CHAFING DAMAGE. THE CHAFE LOCATION IS LOCATED ON THE UPPER SIDE OF THE TRANSMISSION DECK SKIN
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