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 DALA2021021800935None · noneSUPPLEMENTAL INFORMATION - MAINTENANCE COMPLIED WITH ER/A 590042-14 REV ORIG, SEC 1. TIME LIMITED REPAIR. SHIP 9547 - WHILE TAXIING IN PIT AND TRANSITIONING FROM TAXIWAY TO RUNWAY, THE AIRCRAFT EXITED THE HARD SURFACE. THE NOSE GEAR IS OFF OF THE TAXIWAY ANDSDR SWIA202157477Skin · corrodedEXTERNAL FUSELAGE LOWER SKIN HAS CORROSION BETWEEN FS 559.00+80 AND FS 589, STR 23L AND STR 24R. (C-CHECK RO 4/12/2021) REPAIRED EXTERNAL FUSELAGE LOWER SKIN CORROSION BETWEEN FS 559.00+80 AND FS 589 STR 23L AND 24 R IAW BOMBARDIER REO 601R-53-00-834 RESDR MASA20210322104Doubler · crackedCRACK IN DOUBLER BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT STRUCTURE. CORRECTIVE ACTION: DOUBLER BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01SDR HNAA2021030200071Skin · crackedPOSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 79 BTW STR 6L-7L....PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED....REMOVED THE CRACK AREA ON FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 7SDR HNAA2021030200070Skin · crackedPOSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 77 BTW STR 4L-5L....PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED.REMOVED THE CRACK AREA ON FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 77 BSDR HNAA2021030200069Skin · crackedPOSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 77 BTW STR 8L-9L... PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED....REMOVED CRACKED AREA ON EXTERNAL FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET SDR HNAA2021030200068Skin · crackedPOSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR 77 BTW STR 8R-9R....PERFORMED PT INSPECTION IAW EASI NDTM. EASI 0452. CRACK ENDS MARKED....REMOVED THE CRACK AREA ON FUSELAGE SKIN AND INSTALLED SKIN BUSHING ON EXTERNAL FUSELAGE SKIN AT RIVET AT FR 7SDR JJBA20210214024Skin · crackedTWO CRACK SUSPECTED ON EXTERNAL SKIN FR 78 BTW RT STR 4-7. RT REAR FUSELAGE SKIN AT FR 78 BTW STR 4R-7R REPAIRED.SDR CALA2021021500174Skin · corrodedB767-53-3-7154 AFT CGO - STA 1197+132 TO 1219 S-33R SKIN FOUND C ORRODED AS MARKED REF NR LP 9131154 AFT CGO STA 1197+132 TO 1219 S-33R SKIN REPAIRED AS PER EC/RA NO . 5360-01582 REV-. ATTACHED FORM 44.0008 ITEM 1-14 ACCOMPLISHED.SDR SWIA202157157Doubler · corrodedMAIN AVIONICS BAY FWD DRAIN MAST DOUBLER AFT O/B ATTACH ANGLE AT FS349.00 CORRODED (C-CHECK RO 4/1/2021) REPLACED THE FWD DRAIN MAST DOUBLER AFT OUTBD ATTACH ANGLE. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32278 REV NC AND DWG SH670-32250 REV K. SDR SWIA202157156Doubler · corrodedMAIN AVIONICS BAY FWD DRAIN MAST DOUBLER AFT I/B ATTACH ANGLE AT FS349.00 CORRODED (C-CHECK RO 4/1/2021) REPLACED FWD DRAIN MAST DOUBLER AFT INBD ATTACH ANGLE AT FS349.00. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32250 REV K. COMPLIED WITH TASK SDR SWIA202157149Doubler · corrodedFORWARD WATER DRAIN MAST SUPPORT DOUBLER, FS333.00 €“ FS349.00 STGR25R -STGR24R, HAS CORROSION AT MULTIPLE AREAS. (MARKED) (C-CHECK RO 4/1/2021) INSTALLED NEW DRAIN MAST DOUBLER FROM FS333 TO FS349. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32250SDR MASA20210323107Skin · damagedSKIN SECTION WITH PREVIOUS BLEND OUTS BTW FS 202.75-280 AND STGR 10L-16L WAS REPLACED WITH A NEW SKIN SECTION PER EA 32-2021-005 REV. IR. AND CRJ900 SRM 51-42-06-001-A01 AND SRM 51-42-21-001-001-A01SDR MASA20210322101Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E).
CORRECTIVE ACTION: INTERNAL PRODUCTION DOUBLER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.SDR SWAA2021021748794Skin · crackedGROUND POWER EXTERNAL DOOR WTOUT HAS CRACK AT LOWER CENTER POSITION. COMPLETED REPAIR ON GROUND POWER INTERNAL DOOR PULL OUT PER SRM 53-10-15-2R-4.SDR DALA2021021500829Skin · corroded(LOG 1729707) DURING INSPECTION FOUND CORROSION ON FUSELAGE SKIN AROUND OF WASTE TANK VENT PORT BTW STA 905 AND STA 927 AND BTW S20L. FUSELAGE SKIN AROUND OF WASTE TANK VENT PORT BTW STA 905 AND STA 927 AND BTW S20L WAS REPAIRED PER B737-800 SRM 53-70-01-2R RESDR WX0A2021021573643Skin · dentedCONE REAR LOWER FUSELAGE 70MM AFT OF FR73, 55MM BELOW OF THE STR 28RH SKIN WITH DENT. / PERFORMED PERMANENT REPAIR AT REAR CONE LWR FUSELAGE AFT FR73, SGTR28R, STGR31R I.A.W ERO # R5341-0039 REV 00. THIS IS A MAJOR PERMANENT REPAIR.SDR WX0A2021021573642Skin · dentedUPPER REAR FUSELAGE BETWEEN FR69 - FR69+300MM AND STR 19LH - STR 20LH SKIN WITH DENTS. / PERFORMED TEMPORARY REPAIR AT AFT FUSELAGE FR69-70, STGR 18LH-21LH MULTIPLE DENTS IN SKIN I/A/W ERO NO. R5341-0038. IS A MAJOR TEMPORARY REPAIR.SDR WX0A2021021573647Skin · dentedCONE REAR LOWER FUSELAGE 180MM AFT OF FR73, 55MM BELOW OF THE STR 30 RH SKIN WITH DENT. / PERFORMED PERMANENT REPAIR AT REAR CONE LWR FUSELAGE AFT FR73,STGR28R, STGR31R I.A.W ERO. # R5341-0039. THIS IS A MAJOR PERMANENT REPAIR CATEGORY A.SDR WX0A2021021573646Skin · dentedCONE REAR LOWER FUSELAGE 70MM AFT OF FR73, 55MM BELOW OF THE STR 28RH SKIN WITH DENT. / PERFORMED PERMANENT REPAIR AT REAR CONE LWR FUSELAGE AFT FR73, SGTR28R, STGR31R I.A.W ERO # R5341-0039 . THIS IS A MAJOR PERMANENT REPAIR "SDR WX0A2021021573645Skin · dentedUPPER REAR FUSELAGE BETWEEN FR69 - FR69+300MM AND STR 19LH - STR 20LH SKIN WITH DENTS. /PERFORMED TEMPORARY REPAIR AT AFT FUSELAGE FR69-70, STGR 18LH-21LH MULTIPLE DENTS IN SKIN I/A/W ERO NO. R5341-0038. THIS IS A MAJOR TEMPORARY REPAIR CATEGORY C"SDR WX0A2021021573644Skin · dentedCONE REAR LOWER FUSELAGE 70MM AFT OF FR73, 55MM BELOW OF THE STR 28RH SKIN WITH DENT. / PERFORMED PERMANENT REPAIR AT REAR CONE LWR FUSELAGE AFT FR73,STGR28R, STGR31R I.A.W ERO. # R5341-0039. THIS IS A MAJOR PERMANENT REPAIR .SDR SWIA202157554Skin · corrodedFUSELAGE EXTERIOR SKIN IS CORRODED BETWEEN STGR20L AND 20R UNDER FAIRING 195BB CONTOURING SEALANT BED. (C-CHECK RO 4/12/2021) UPON FURTHER INVESTIGATION FOUND THE CORROSION TO BE ON THE LOWEER SKIN BETWEEN STR 23L AND STR 24R COMMON TO BELLY FAIRING 195SDR SWIA202157553Skin · corrodedFUSELAGE EXTERIOR SKIN IS CORRODED IN MULTIPLE PLACES BETWEEN FS559+80 AND FS574 FROM STGR 26L TO STGR 26R. (C-CHECK RO 4/12/2021) REMOVED CORROSION FROM THE EXTERNAL FUSELAGE SKIN BETWEEN FS 559.00+80 AND FS 574, STR 26L AND STR 26R IAW CRJ-200 SRM 51-SDR SWIA202157552Skin · corrodedFUSELAGE EXTERIOR SKIN IS CORRODED ALONG FS559+112 CIRRCUMFERENTIAL JOINT FROM STGR 25L TO 25R. (C-CHECK RO 4/12/2021) REMOVED CORROSION FROM THE EXTERNAL FUSELAGE SKIN AT FS 559.00+112 IAW CRJ-200 SRM 51-21-06 AND FOUND TO BE OUT OF LLOWABLE LIITS IAW SDR SWIA202156473Skin · dentedREFERENCE CP 22296913 FOR ORIGINAL DISCREPANCY.ADG SKIN P/N: CC670-33109-5 REQUIRES REPLACEMENT DUE TO OUT OF LIMITS DENT DAMAGE MEASURING 0.43" DEPTH WITH EVIDENCE OF BURN AND DEFORMATION.THIS IS CLASSIFIED AS A MAJOR REPAIR. COMPLY WITH FORM M-337. FILEDSDR 2A6R2021021259202Skin · crackedFWD SKIN OF TAILCONE, RIGHT ENGINE BAY INBD FWD CORNER AT ATTACH ANGLE FS 4800 RBL80 FOUND 1.5" CRACK DURING 1000HR INSPECTION. CRACK RUNS FROM THE FWD EDGE OF THE TAILCONE SKIN THROUGH TWO RIVETS THAT ATTACH THE SKIN TO THE BULKHEAD ANGLE.SDR SWIA202157144Skin · dentedDENT FOUND AT APPROXIMATELY FS 240 STRINGER 19/20L. (C-CHECK RO 4/1/2021) DENT ON EXTERNAL FUSELAGE SKIN AFT OF FS250 ABOVE STGR 25L REPAIRED. REF REO 670-53-11-1670 REV -- DATED 2021-03-08.. COMPLIED WITH 51-900-1002-SKY.SDR AALA202102189017Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN FROM CONTACT WITH APU DOOR HINGE ARMS BETWEEN STA 1101 AND STA 1149 AT STR 20R, MEASURING L=0.5 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW SRM 53-80-01-2R-1.SDR DALA2021021200822Skin · dentedSHIP 3316 DENT EXTERNAL SKIN FROM FR 30 TO FR 31 BTW STR 28L / STR 29L AT FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON DENT AREA LOCATED FROM FR30 TO FR31 AND BTW STR 28L TO STR 29L AT LOWER FUSELAGE AS PER ER/A 589910-14 PRI REV. 0 AND ER/A 5SDR DALA2021021200821Skin · dentedSHIP 3316 DENT EXTERNAL SKIN FROM FR 30 TO FR 31 BTW STR 27L / STR 28L AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON DENT AREA LOCATED FROM FR30 TO FR31 AND BTW STR 27L TO STR 28L AT LOWER FUSELAGE AS PER ER/A 589910-14 PRI REV. 0 AND SDR DALA2021120807567None · none(LOG 1727305) DURING INSPECTION FOUND ELONGATED HOLES BETWEEN STA 7 27L AND 727J, STRINGERS 2L AND 2R. MAINTENANCE REPAIRED DAMAGE PER ERA 589997-14.SDR IPXA2021031366776Skin · corrodedINSPECTION TYPE:3CR/H AFT FUSELAGE SKIN BETWEEN STA 2119.685 - 2163.681 AND BETWEEN LONGERONS 32R - 35R HAS CORROSION.REPAIRED CORRODED R/H AFT FUSELAGE SKIN BETWEEN STA 2119.685 - 2163.681 AND BETWEEN LONGERONS 32R - 35R IAW VT-SAA EA 011-5330-01-A8909 REV. ISDR VNAA202102131112Skin · dentedDURING ROUTINE OVERNIGHT MAINTENANCE IN PENSACOLA, FL (PNS), MAINTENANCE NOTED THAT THERE IS A DENT COMMON TO THE FUSELAGE SKIN BETWEEN FS 245, AND BETWEEN STRINGERS 22L AND 23L. THE DENT MEASURES .780Ï¿½ LONG X .330Ï¿½ WIDE X .035Ï¿½ DEEP. ITÏ¿½S WIDTH TO DEPSDR KCSA202102101009Skin · out of limitsVERTICAL STAB TO FUSELAGE INTERFACE BLENDID OUT OF LIMITS AT STA 2597 RHSDR SWIA202156968Skin · dentedFOUND DENT IN SKIN AT FS193 AND STR23R. FILED CLOSED REPAIRED FUSELAGE SKIN BETWEEN FS 185 AND FS 202.75 AT STR 23R IAW REO 670-53-11-1649 REV -- DATED 3/12/21 & REO 670-51-00-085 REV A DATED 8/23/17. C/W TASK CARD 51-900-1002-SKY AND M-337.SDR SWAA2021031152616Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FASTENER BS 294.5 2' ABOVE STR 21R / REMOVED LIGHTNING STRIKE DAMAGE AT FASTENER BS294.5. 2' ABOVE STR 21 R/H; FABRACATED AND INSTALLED A REPAIR IAW SRM 53-00-01-2R-36SDR IPXA2021030366384Skin · corrodedINSPECTION TYPE:C3MAIN CABIN CENTER WING BOX SKIN HAS CORROSION BETWEEN STA.XCW = 80 AND XCW=-80 STR 15.REPAIRED MAIN CABIN CORRODED CENTER WING BOX SKIN IAW VTSAA EA 011-5710-01-A8888 REV I/R AND UPS EO MD11-5710-79511-A (MINOR).SDR IPXA2021030166224Skin · corrodedINSPECTION TYPE:C3MAIN CABIN CENTER WING BOX SKIN HAS CORROSION BETWEEN XCW=-81 AND XCW =-85 STRINGER 16.REPAIRED CORRODED CENTER WING BOX SKIN IAW SAA EA 011-5710-01-A8889 REV I/R AND UPS EO MD11-5710-79458-A (MINOR)SDR A6WA202102287670Skin · dented3 EACH OUTWARD DENTS IN SKIN AT FUSELAGE STATION 625.30+7 TO FUSELAGE STATION 625.30+10 S23R-S24R ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED REPAIR LOCATED IN SKIN AT FUSELAGE STATION 625.30+7 TO FUSELAGE STATION 625.30+10 S23R-S24R REF EA # AWAC - CRH-SDR IPXA2021022466062Skin · crackedINSPECTION TYPE: C13 CRACK FOUND ON FUSELAGE SKIN AT STA 1654.5, S-13AR. REPAIR IAW SRID: 3-4978953707 AND UPS EO B767-5330-79406-A.SDR JJBA20210209022Skin · damagedREAR FUSELAGE II, LT SIDE, AT FR 77-78-79, BTW STR 3-8 MULTIPLES REPAIR BUSHING. REAR FUSE II AT FR 77 BTW STR 3-4L SKIN REPAIRED AT THE 2 CONSECUTIVE REPAIR BUSHING LOCATIONS.SDR JJBA20210209017Skin · dentedON RH FUSE SKIN BTW FR 12-11 AND STR 20-21 2 DENTS FOUND. DENT #1 ON RH FUSE SKIN FROM 0650 FWD FR 11 AND 2100 ABOVE STR 21R DENT DRILLED 0185 AND INSTALLED RIVET PLUG. RH FUSE SKIN BTW FR 12-11 AND STR 20-21R DENT #2 IS AN EXISTING BLEND REMAINING 025 AND 032SDR JJBA20210209015Skin · dentedRH FUSE BTW FR 2-3 AND BTW STR 11-13, SKIN DENTED. RH FUSE SKIN BTW FR 2-3 STR 11-13 REPAIREDSDR JJBA20210209013Skin · dentedON RH FUSE DENT FOUND BTW FR26 AND FR25 AND BTW STR 13R AND 14R. DENT IS OUT OF LIMITS. DENT DIMENTION L 0.800 W 0.600 H 0.020. RH FUSE SKIN BTW FR26 & FR25 BTW STR 13R & 14R REPAIRED.SDR SWIA202156194Door Frame · gougedOUT OF LIMITS, 1-OFF GOUGE DAMAGE TO LOWER FWD LAND (DWG CC670-33472, 2024-T42, / NOMINAL THICKNESS .050", REF) OF ADG DOOR SURROUND. DAMAGE IS LOCATED BTW FS177.00 & / FS185.00 AND APPROXIMATELY 2.00 AWAY FROM AFT EDGE OF THE PART.HAS BEEN DETERMINED TO BE A SDR DALA2021021000788Skin · damaged(LOG 1726670) DURING INSPECTION FOUND SKIN DAMAGE INCURRED AT FS 807 BTWN S-25L AND S-26L. DAMAGE REPAIRED PER ERA 589965-14.SDR 2021F00024Skin · chafedLOWER SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 REV - DATED 7/19/2019; STANDARD REPAIR - 680A ALL S/N LWR SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE.SDR A6WA202102227666Skin · dentedOUTWARD DENT IN SKIN AT FUSELAGE STATION 672.20+5, STRINGER 24R+3. AIRCRAFT REMOVED FROM SERVICE. PERFORMED DOUBLER REPAIR AT FS 672.20 TO FS 682.00 STR 24R. FABRICATED DOUBLER FROM 2024T3 0.063". HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASDR A6WA202102197664Skin · corrodedCORROSION UNDER ADF ANTENNA ON THE TOP OF THE FUSELAGE AT FS 409.00+64.000 - 409.00+86.750 BL 0-5.3000 - BL 0+5.000: AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION BY BLENDING TO A SMOOTH CONTOUR ON 6 DAMAGE AREAS ON TOP OF FUSELAGE FS 409.00+64.000 - 409.
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