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 CALA2021031200301Doubler · corrodedFUSELAGE REIENFORCEMENT DOUBLER AT AVIONICS COMPARTMENT INLET VA LVE HAS CORROSION AT 6 O''CLOCK POSITION ON HAECO LCQ REF 9290312 GENERATED BY MECH V899045 REMOVED AND REPLACED AVIONICS COMPARTMENT REINFORCEMENT DOUBLER IAW A320 SRM 51-72-11 MECH BY V914162 ISDR CALA2021031200300Skin · corrodedR-2 AFT ENTRY DOOR CUTOUT FWD FR68 AREA UNDER PLANKING PLATE HAS AREAS OF CORROSION A3NB-53-3-6299. PER HAECO LCQ N/R 9296482/22 482. GENERATED BY MECH V311118. REMOVED AND REPLACED R-2 DOOR SILL @ FR 66-68 PER A319 SRM 51-42 -11-801 & D53480009002 REV A. REMOSDR DALA2021031101385Skin · scratchedSHIP 3235 SCRATCH ON EXTERNAL SKIN STATIC PORT RH SIDE BTW FR23 TO FR24 AT LOWER FUSELAGE. CORRECTIVE ACTION: REWORKED AREA AS PER A320 SRM 51-73-11. OK FOR SERVICE. (1751251)SDR DALA2021031101380Skin · dentedDURING CHECK MAINTENANCE FOUND FUSELAGE SKIN STATION 600 TO 640 STRINGER 16L DENTS. REPAIRED PER ERA 532855-14. (LP 1751578)SDR SWIA202157715Skin · corroded* THE FUSELAGE SKIN'S EXTERNAL SURFACE BENEATH THE TCAS ANTENNA HAS MULTIPLE SHALLOW NICKS THROUGH THE CLADED SURFACE AND SURFACE CORROSION AROUND THE ATTACH FASTENER HOLES. (C-CHECK RO 4/21/2021) REMOVED DAMAGE ON FUSELAGE SKIN EXTERNAL SURFACE BENEATHSDR JJBA20210309025Skin · corrodedCF1, BTW FR 17-18 AND BTW STR 21L-21R, SKIN CORRODED. CF1, BTW FRAMES 17-18 AND BTW STR 21L-21R CORRODED SKIN REPAIRED.SDR JJBA20210309024Skin · misrepairedRH FUSELAGE BTW FR 16-17 BTW STR 10-12, REPAIR DOUBLER NOT PROPERLY INSTALLED. RH FUSELAGE BETWEEN FRAME 16-17 AND BTW STR 10R-12R REPAIR DOUBLER NOT PROPERLY INSTALLED. REPAIR REWORKED.SDR UIEA2021030100427Panel · crackedM/D STA 1620 - 1720 LH DADO PANEL FOUND CRACK.(<P>M/D STA 1620 - 1720 LH DADO PANEL REPAIRED AS PER RI-25-00-14384 REV A.</P>)SDR UIEA2021030100433Skin · crackedUPPER FUSELAGE DURING HFEC FOUND CRACKS BETWEEN RIVETS ON I/B SIDE OF ELT ANTENNA CUT OUT. NOTE OUTER SKIN(<DIV> / </DIV><P STYLE="MARGIN:0IN;MARGIN-BOTTOM:.0001PT"><SPAN>COMPLIED WITH WORK INSTRUCTIONS / BELOW AND EO6753A923</SPAN></P><P CLASS="XXMSOLISTPARAGSDR UIEA2021030100435Skin · damagedBS 938-1000 S38L DRAG SPLICE LOWER FITTING AREA, SKIN REPAIR CRACK REPAIR.(<P>EO 4453A705 ' CAT B ' PERMANENT REPAIR ACCOMPLISHED ON SKIN ASSEMBLY 65B04116 PER 747-400F SRM 53-20-01 REPAIR 2 AT BS 950 - BS 990, S38L.</P>)SDR UIEA2021030100436Skin · dentedBS 1700 S-41L, SKIN DENT, INSPECTION AND CAT B PERMANENT REPAIR.(<P>EO 4453A541 CAT B PERMANENT REPAIR ACCOMPLISHED AT HKG DURING FEB 2016 C1A1 CHECK BY HAECO.</P>)SDR AALA202103129011Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF FUSELAGE SKIN AROUND VACUUM BLOWER EXHAUST VENT AT STA 1968 BETWEEN STR 35L AND STR 36L, MEASURING L=4.7 IN, W=7.9 IN, D=0.12 IN. ACCOMPLISHED PERMANENT REINFORCING TRIPLER REPAIR IAW SRM 53-70-01-2R. (DUPLICATE SUBMISDR MASA20210408163Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA:FS=295 TO FS=310 BTW STGR:26LH TO 26 RH. AT MAIN AVIONICS COMPARTMENT ACTION CORRECTIVE REPLACE PER CRJ-900 SRM 51-42-06-001-001-A01. PAR.6.C.
PART DEFECT LOCATION: IN STA.FS=295 TO FS=310 BTW STGR 26LH TO 26RHSDR SWAA2021033154509Skin · corrodedCORROSION LOWER SKIN BS 545.8 STR 14 LT AND WING CENTER SECTION FRONT SPAR LBL 49 IN CENTER FUEL TAN. PERFORMED INTERIM REPAIR LOWER SKIN LOCATED BTW BS540 TO BS545.8 STR 14L AND WING CENTER SECTION FRONT SPAR LBL 49 IN CENTER FUEL TANK IAW EA # 57-0104-21 RESDR ASAA2021030734281Skin · corrodedSKIN CORRODED JUST FWD OF LAV WASTE VENT AT FUSELAGE R/H SIDE GROUNDED - YES. SKIN REPAIRED PER EA # A320-53EA-00851SDR DALA2021030801328Skin · crackedDURING HCK FOUND EXSISTING REPAIR WITH CRACKS ON FUSELAGE SKIN BTW STA 1600 TO STA 1660 AND BTW S-17R & S-29R. REPAIRED PER ERA 590453-14AD. (LP 1748852)SDR DALA2021030801324Service Panel · corrodedDURING INITIAL INSPECITON MAINTENANCE FOUND CORROSION LEVEL 2 ON FWD LAVATORY SERVICE PANEL INNER SIDE BTW FS400 TO FS420 AND STGR 26L TO 29L AT FWD FUSELAGE. REPLACED SERVICE PANEL. (LP 1748114)SDR IPXA2021030766520Skin · damagedINSPECTION TYPE:N/ALH FUSELAGE SKIN DAMAGE REPAIR BETWEEN STA 272 AND STA 305 AND BETWEEN S-21L AND S-23L.CUT OUT DAMAGE AND REPLACED DAMAGED SKIN PER EO B757-5330-79526.SDR DALA2024080107706Skin · unknownSHIP 5814 ER/A 590453-14AD IS REQUIRED FOR THE FUSELAGE SKIN BETWEEN STA 1600 - 1660 AND STR 17R TO 29R. CORRECTIVE ACTION: REF ERA 1748131. (1748131)SDR SWAA2021030953549Skin · damagedAIRCRAFT FUSELAGE SKIN IS CREASED AT STA 807 BETWEEN STR 25L-26L / ACOMPLISHED REPAIR OF FUSELAGE SKIN AT STA. 807 BETWEEN STR. 25L-26L PER E.A. 21-153-00515. 'AFT BAG BIN' 'CHOSE UP?' WILL BE ACCOMPLISHED ON N/R # D460281. REF L/P'S 1062354;1180648;1180649. RSDR CALA2021030800274Skin · crackedCRACK FOUND APPROX 1.125" LONG AT STR13AL BETWEEN BS1654-1674 WHILE ACCOMPLISHING EA 5380-01178 OPS 001 SKIN INSPECTION. FUSELAGE SKIN CRACK REPAIRED BETWEEN STA1654-1674 STR 13AL IAW SRM 53-80-01 REPAIR 7 FIG 201 DETAIL VII CAT B REPAIR. REF TABLE 202 FOR IQ SDR SWIA2021071459506Doubler · corrodedANTENNA DOUBLER CORRODED BETWEEN FS349.00 AND FS364.00 STRGR 25R AND 26R. (C-CHECK RO 7/10/2021) REMOVED AND REPLACED ANTENNA DOUBLER BETWEEN FS 349.00 AND 364.00 STR 25R AND 26R IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. COMPLETED TSDR SWIA202157666Doubler · corrodedCORROSION FOUND ON INTERNAL DOUBLER AT FWD OMNIDIRECTIONAL TSS ANTENNA (C-CHECK RO 4/21/2021) REMOVED CORRODED ATENNA DOUBLER AND INSTALLED NEW ANTENNA DOUBLER REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32364 REV-NC. PRESSURE CHECK GOOD. COMPLIESDR SWIA202157665Skin · corrodedFUSELAGE SKIN CORRODED UNDER AFT DRAIN MAST CHANNEL AT FS1040.00 AT STR26R (C-CHECK RO 4/21/2021) REPAIRED FUSELAGE SKIN CORRODED UNDER AFT DRAIN MAST CHANNEL AT FS1040.00 AT STR26R REF REO 670-53-61-1852 REV -- DATE 2021-03-27. COMPLUIED WITH TASK CARDSDR SWIA202157368Doubler · corroded*CORROSION ON RAD ALT ANTENNA DOUBLER BETWEEN FS 1000.00 - 1015.00, STGR 27 - 26L (C-CHECK RO 4/3/2021) REMOVED 2EA. CORRODED SHIMS ON RAD ALT ANTENNA DOUBLER AND INSTALLED 2EA NEW SHIMS WITH PN MM670-70327-001 AND MM670-70329-001 WERE INSTALLED ON RAD ANSDR SWAA2021033154498Bear Strap · crackedCRACK INDICATION FOUND (2 E/A) ON THE BEAR STRAP. LOC FWD GALLEY DOOR R1 BS CUT OUT FROM BS 290 TO BS 296 BTW S-8R AND S-9R. CRACK 1 DIRECTION IS 9 O’CLOCK OF FASTENER AND LENGTH 0.240 INCH. CRACK 2 DIRECTION IS 3 O’CLOCK OF FASTENER AND LENGTH 0.400 INCH. SDR A6WA202103097708Skin · corrodedCORROSION ON LOWER RIGHT HAND TCAS ANTENNA AREA ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION AT LWR R/H TCAS ANTENNA AREA, 5.5"L X 2.20"W X 0.008"D. IN LIMITS IAW ASAP EA# AWAC CRJ253-01583 REV IR DATED 3/8/2021. HFEC INSPECTION PERFORMED WITH NO ISDR SWAA2021033153388Skin · dentedDENT EXTERNAL SKIN LOC. AT BS 420 MORE 8 INCHES AND 2 INCH BELOW STR 21R AT LOWER FUSELAGE (1 EA).SDR AALA202103089024Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION OF FUSELAGE SKIN NEAR WASTE SYSTEM OVERBOARD EXHAUST AFT VENT. **SUPPLEMENTAL REPORT: CORROSION OF FUSELAGE SKIN AROUND VACUUM BLOWER EXHAUST VENT AT STA 1968 BETWEEN STR 35L AND STR 36L, MEASURING L=4.7 IN, W=7.9 IN, D=0.12 INSDR SWIA202156723Skin · damagedREPORT OF AIRCRAFT MAJOR REPAIR" FOR DAMAGE TO FUSELAGE LOCATED UNDER 3RD PASSANGER WINDOW ON LH STGR 21 & STGR 23 AND FR25 & FR27 FILED CLOSED REVIEWED AND SIGNED FORM M-337SDR VNAA202103081111Skin · dentedDURING OVERNIGHT MAINTENANCE, A DENT WAS DISCOVERED ON THE RH FUSELAGE SKIN JUST FORWARD OF FS 220 ABOVE THE RH PITOT PROBE BETWEEN STGR 13A AND 14A. THE DENT MEASURES 2.05Ï¿½ X 2.0Ï¿½ X 0.016Ï¿½ DEEP AND IS NOT WITHIN ALLOWABLE DAMAGE LIMITS DUE TO EDGE OF DESDR A6WA202103087693Skin · corrodedCORROSION COMMON TO PRESSURE FLOOR SILL AT FS439.00+2, RBL 42 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON PRESSURE FLOOR SILL FS439.00+2, RBL 42, PERFORMED HFEC INSPECTION WITH NO INDICATIONS, PERFORMED UT THICKNESS CHECK, REMAINING MATERIAL WITSDR SWIA202157933Skin · dentedMULTIPLE DENTS IN AREA BELOW AND BEHIND LOW PRESSURE AIR ACCESS DOOR. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICE/PROCEDURES. (C-CHECK RO 5/3/2021) CUT OUT DAMAGE AND SDR SWIA202157932Skin · crackedTRANSFER FROM EAML 588779 : CRACK/PUNCTURE DAMAGE TO SIDE FUSELAGE SKIN (DWG 601R38321, 0.045" / THK IN CHEM MILL POCKET & 0.058" THK IN PAD UP AREA, REF) BETWEEN FS409.00+48 - FS409.00+64 / AND STR 16R - STR 18R (C-CHECK RO 5/3/2021) REMOVED TEMPORARYSDR R61A2021032700293Access Door · corrodedCF III WASTE ACCESS DOOR HAS CORROSION. REPLACED IAW AMM 53-03-60SDR SWAA2021032355737Skin · chafedCHAFING DAMAGE ON FUSELAGE SKIN AT AFT CARGO BAY BS727E - BS747 BL0 WL149. / ACCOMPLISHED REPAIR TO FUSELAGE SKIN CHAFFING DAMAGE AT AFT CARGO BAY BS 727E-BS747 BL0 WL149 IAW EA. 21-153-00661 REV IR AND ATS ER 21-01459 REV IRSDR AALA202103129010Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: 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 IAW B777 SRM 53-70-01-2R-1. (DUPLICATE SDR A6WA202103097707Skin · dentedOUTWARD DENT COMMON TO SKIN AT FS 625.3+5 TO 625.30+5.6, STR24L+4 TO STR ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED 2 OUTWARD DENTS: DENT 1) 0.200Ï¿½L X 0.200Ï¿½W X 0.004Ï¿½D. DENT 2) 0.500Ï¿½L X0.300Ï¿½W X 0.007Ï¿½D. FOUND TO BE WITHIN LIMITS PER SUPPLESDR A6WA202103097709Skin · dented1 OUTWARD DENT COMMON TO SKIN AT FS672.20+6, STR 24R+ 2.5, 2 OUTWARD DENTS COMMON TO SKIN AT FS672.20+4.4 Ï¿½ FS672.20+6, STR 25R+1.8 - STR 25R+2.8. ***AIRCRAFT REMOVED FROM SERVICE*** ACCOMPLISHED FS REPAIR BETWEEN FS62.20 AND FS682.00, BETWEEN STR 24R AND SDR A6WA202103087681Skin · dentedOUTWARD DENT COMMON TO SKIN AT FS 625.30+17 TO STR22R+3.5 ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED OUTWARD DENT IN SKIN AT FS 625.30+17 AND STR 22R+3.5. HAND DRESSED DENT MEASURED 0.2"L X0.2"W X 0.004"D TO ORIGINAL CONTOUR REF ASAP EA # AWAC - CRJ253- SDR A6WA202103087682Skin · dentedDENT IN FUSELAGE SKIN AT FRAME VS55.625% SPAR DATUM AND STR 10+1.5 ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT AT FRAME VS 55.625% SPAR DATUM, DENT MEASURED .760"L X .420"W X .009"D. PERFORMED HAND DRESS ON FUSELAGE SKIN AT VS 55.625% BETWEEN STR1SDR A6WA202103087704Skin · dentedINWARD DENT COMMON TO FS640.00+4 STR24+2.5 TO STR24+3.6. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED EXTERNAL DOUBLER REPAIR FROM 0.063" 2024 T3 ON FUSELAGE SKIN AT FS 640.00+4 STR24+2.5 TO STR24+3 REF EA# AWAC - CRJ253-01577 REV IR DATED 3/6/2021.SDR A6WA202103087706Skin · dentedINWARD DENT COMMON TO SKIN AT FS718.00+14 TO FS718.00+16 STR16+1 AT FWD END TO STR16+.5 AT AFT END OF DENT. ***AIRCRAFT REMOVED FROM SERVICE*** HAND PASSED DENT COMMON TO SKIN AT FS 718.00+14 TO FS718.00+16, STR16+1 AT FWD END TO STR16+.5, REF EA# AWAC - CRSDR IPXA2021030366341Skin · crackedINSPECTION TYPE:N/AFUSELAGE SKIN P/N# ACA3108-503 AT STA 535 ABOVE S-33R HAS A 1.55" CRACKCOMPLETED PERMANENT REPAIR PER EO MD11-5330-79121-B THIS IS A MAJOR REPAIRSDR AALA202103049012Doubler · crackedAIRCRAFT WAS GROUNDED: EGPR DOUBLER CRACKED, 1/4 INCH LONG, LOCATED ON BOTTOM OF EXTERNAL POWER DOOR LANDING. COMPLIED WITH TIME LIMITED REPAIR TO THE EGPR DOUBLE IAW AARD 53-10-00-4 REPAIR 4.SDR SWIA202156970Skin · dentedTRANSFER FROM EAML 588661 : FOUND DAMAGE TO LT SIDE OF AC LOCATED 2FT AFT OF THE PAX DOOR BETWEEN FS364.00 TO FS394 AND STR14L, STR15L, AND STR16L. 3 DENTS TO FUSELAGE #1. BTWN FS364.00-FS379.00, STR15L - STR16L: 15" L X 6" W X 0.132" MAX DEEP, # 2. BTWN FS364SDR SIMA20210302003Skin · damagedTRANSFERRED FROM NRWC 038-ORD-01910 "FUSELAGE SKIN ABOVE GPU RECEPTACLE HAS SIGNIFICANT HEAT DAMAGE DUE TO FIRE. (REF AML PG 4675896 ITEM 2) UPGRADED TO A MAJOR REPAIR-C/A-RERPAIRED IAW ERS-EJ-53MR-4290SDR DALA2021030401241Skin · gougedDURING INSPECTION MAINTENANCE FOUND GOUGE AT UPPER FUSELAGE STA 570 BTW S-3R TO S-4R.(FUS). REPAIRED PER ERA 590228-14AD. (LP 1744256)SDR CALA2021030300253Skin · corrodedL-2 AFT ENTRY DOOR CUTOUT FWD FR68 AREA UNDER PLANKING PLATE HAS AREAS OF CORROSION (3NB-53-3-6299). REMOVED CORROSION AT L-2 ENTRY DOOR CUTOUT. HFEC OF BLENDED AREA HICKNESS OF BLENDED AREA IAW NTM 51-10-04 FOUND TO BE IN LIMITS IAW A319 SRM 53-41-14-283-002SDR SWIA202157820Doubler · corrodedFS379 SKIN BUTTJOINT DOUBLER IS CORRODED AT STR 23L (C-CHECK RO 4/25/2021) REPAIRED FS379 SKIN BUTTJOINT DOUBLER AT STR 23L IAW MHIRJ REO 601R-53-21-3420 REV. -- DATED 2021-03-29, SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY AND ATTACHED FORM
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