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.

SDR DALA2021091405484Skin · dentedSHIP 649 PROTUBERANCE (01 EA) FUSELAGE SKIN BTW STRINGERS 19 TO 20 STATIONS=686 FUSELAGE LH SIDE. CORRECTIVE ACTION: SUMMARY OF NRC 00043: PROTUBERANCE (01 EA) FUSELAGE SKIN BTW STRINGERS 19 TO 20 STATIONS=686 FUSELAGE LH SIDE WAS REPAIRED PER ER/A 593738-14 RSep 10, 2021 · N649DL · Boeing 757232SDR DALA2021091505516Skin · dentedSHIP 649 PERFORM REPAIR:MON, 56 REP, 0951234;INSP;DECAL;BLW R4 DOOR; DENT ON FUSELAGE AFT AND BELOW AND 4IN AFT OF SERVICE DOOR. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00981. DENT ON FUSELAGE AFT AND BELOW AND 4IN AFT OF SERVICE DOOR WAS REPAIRED. PER. ETI-57-21Sep 9, 2021 · N649DL · Boeing 757232SDR REXA2021092300757Seat Track · corroded"RH FLOOR SEAT TRACK FS 847-1000 CORRODED. " " REMOVED & REPLACED RH FLOOR SEAT TRACK FROM FS 847-1000 FOUND NO CORROSION NOTED ON RBL9 SEAT TRACK FS 847.00-FS 901.00 WVAC EMP STAMP # 796 MTC. "Sep 8, 2021 · N901XJ · Cndair CL6002D24SDR YENA2021091700593Doubler · corrodedDURING HEAVY MAINTENANCE, CORROSION DISCOVERED ON WASTE BOX INNER DOUBLER; (REF TOMX NR 00394) REPAIRED WASTE BOX INNER DOUBLER IAW SRM 53-23-60 / REPAIR 51P.Sep 8, 2021 · N238JB · Emb ERJ190100IGWSDR DALA2021091005358Doubler · out of limits(LOG 1941533) DURING INSPECTION FOUND DURING RIVETS INSTALLATION CHECK ON F.S. (WHERE THE IDTV ANTENNA WAS REMOVED) PER AMDS 2332-01125-42 STEP 60. RIVET HOLES DOES NOT MEET WITH EDGE DISTANCE FROM THE CENTER OF HOLES TO THE INNER SKIN DOUBLER EDGE AT STA 727GSep 8, 2021 · N828DN · Boeing 737932ERSDR SWAA2021110915577Doubler · corrodedCRACK INDICATIONS OBTAINED EMANATING FROM FASTENER HOLE OPPOSITE FITTING LATCH AT R1 DOOR CUTOUT STA 294.5 BETWEEN S-8R AND S-9R. THERE ARE 2 CRACKS (1) LENGTH 0.197' AND (2) 0.118' ; / [01] INSTALLED EWIS PROTECTION AT RT FUSELAGE REPAIR AREA REF BI37-7 AMM 2Sep 7, 2021 · N783SW · Boeing 737*SDR SWAA2021100815431None · brokenBROKEN EXTERNAL GROUND ELECTRICAL POWER SKIN CUT OUT AT LOWER FUSELAGE ; 2021-417559 / [16] OK TO INSTALL REPAIR PARTS DOUBLER; FILLER; RUBBING BLOCK; LAMINATED SHIM; FASTENERS AND WASHER ON EXTERNAL GROUND ELECTRICAL POWER SKIN CUT OUT AT LOWER FUSELAGE; [17]Sep 7, 2021 · N760SW · Boeing 7377H4SDR REXA2021092100735Stringer · chafedSTRINGER NUMBER 6 FS 1148.18 CHAFED .400 INCHES DEEP .500 INCHES WIDE. - THIS IS A MAJOR REPAIR. STRINGER 6 REPAIRED IAW EA CRJ753-12072.SEE EA FOR DETAILSSep 7, 2021 · N390CA · Cndair CL6002C10SDR REXA2021092100734Stringer · chafedSTRINGER NUMBER 7 FS 1148.18 CHAFED .400 INCHES DEEP .500 INCHES WIDE. - STRINGER #7 REPAIRED IAW EA CRJ753-12073. SEE EA FOR DETAILS.Sep 7, 2021 · N390CA · Cndair CL6002C10SDR FDEA202109072235Skin · dentedUPPER FUSELAGE SKIN STA212.5 - STA220.5 S2R-S3R FOUND 1EA DENT. PERFORMED THE REPAIR ON UPPER FUSELAGE SKIN STA212.5 - STA220.5, S2R-S3R PER FEDEX EA # : H-5330-T0363972 P1. TITLE : FUSELAGE - PLATES & SKINS - STA212.5 - STA220.5, RBL15.10 - RBL22.19, DENSep 7, 2021 · N128FE · Boeing 7673S2FSDR R61A2021090980723Skin · dentedFWD FUSELAGE FWD LOWER SKIN PANEL HAS 1X DENT WITH A CREASE FR4 TO FR7 STGR 20L TO STGR 22L. ACCOMPLISHED REPAIR IAW ETD2021-170-029303Sep 7, 2021 · N726YX · Emb ERJ170200LRSDR DALA2021090805302Skin · damaged(LOG 1939722) DURING INSPECTION FOUND DAMAGE AT STA 500C+20, .3" BELOW STR 26L ON EXTERIOR FUSELAGE SKIN. REPAIRED DAMAGE ON FUSELAGE EXTERIOR SKIN AT STA 500C+20, .3" BELOW STR 26L IAW B737 SRM 53-00-01-2R PROCEDURE 1 REPAIR 1.Sep 7, 2021 · N390DA · Boeing 737832SDR CALA2021090801529Skin · crackedSUPPORT TASK - EA 5380-01178 REV A OP 003 L/H FUSELAGE SKIN BETW EEN 1654 TO 1678 FOUND 2EA CRACK AT STR 13AL APPROX 3/8" AND 5/8 " IN LENGTH. N/R L/P 9130401 AND ORIGINATED BY EMP V924736 CREATE REPEAT INSPECTION AS PER SRM 53-80-01-2R-7 REPAIRT TABLE 202 DETSep 7, 2021 · N66056 · Boeing 767424ERSDR DALA2021090805287Skin · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BODY SKIN AT STA1197 TO 1197+22, S-36R. REPAIRED PER ERA 593684-14. (LP 1938045)Sep 6, 2021 · N186DN · Boeing 767332SDR DALA2021090705231Skin · corrodedSHIP 3250 CORROSION INTERNAL SKIN LOCATED BETWEEN FR64 TO FR65 AND FROM STR 44 TO STR 43R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: INSPECTED AND FOUND DAMAGE TO BE NEGLIGIBLE. (1938661)Sep 6, 2021 · N350NA · Airbus A320212SDR MASA20210907396Skin · corrodedFUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE BETWEEN FS 927 - FS 942, STR 21R -STR 22R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-101-003-A04, IPC 53-82-83 FIGURE 10, EA 20-2021-161.Sep 6, 2021 · N244LR · Cndair CL6002D24SDR FDEA202109052220Skin · dentedFUSELAGE SKIN BETWEEN STATION 615 TO STATION 629.542, LONGERON 31L - LONGERON 32L FOUND DENT FUSELAGE SKIN BETWEEN STATION 615 TO STATION 629.542, LONGERON 31L - LONGERON 32L DENT AREA REPAIR CARRIED OUT AS PER EA # : 1-5330-T0363977 P1 TITLE : FUSELAGE -Sep 5, 2021 · N584FE · Doug MD11FSDR CALA2021090601513Skin · crackedFUSELAGE SKIN 4 EACH CRACKS FOUND AT STA1630-1654 STR 14AR WHILE PERFORMING INSPECTION BY EA 5380-01178 OPS 004. INSTALLED DOUBLER REPAIR STA 1630-1654 STR 14AR IAW SRM 53-80-01-2R-7 REPAIR 7 FIG 201. REPAIR IS PERMANENT CAT B. INSPECTION THRESHOLD IS 30,000 FSep 5, 2021 · N77066 · Boeing 767424ERSDR CALA2021090601512Skin · crackedSUPPORT TASK EA 5380-01178 REV A OP 4 4EA CRACKS FOUND BETWEEN B S1630 AND BS 1654 STR -14AR FUSELAGE SKIN TRANSFER REF NR LP 913 0582 AND ORIGINATED BY EMP V924736 FX- SKIN BETWEEN BS1629-BS1654 S-14AR PERMANENT REPAIRED (CAT B) AS PER SRM 53-80-01-2R-7 REPAISep 5, 2021 · N77066 · Boeing 767424ERSDR FDEA202109042213Skin · crackedSURFACE HFEC INSPECTION FOUND 02EA CRACKS(FWD CRACK APPROX 0.700INCH IN LENGTH AND AFT CRACK APPOX 0.950INCH IN LENGTH)ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN AROUND THE 2 HOLES COMMON TO THE LEFT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS MARK ASSep 4, 2021 · N892FD · Boeing 777FS2SDR FDEA202109042211Skin · crackedSURFACE HFEC INSPECTION FOUND 02EA CRACKS(FWD CRACK APPROX 0.900INCH IN LENGTH AND AFT CRACK APPROX 0.700INCH IN LENGTH) ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN AROUND THE 2 HOLES COMMON TO THE RIGHT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS MASep 4, 2021 · N892FD · Boeing 777FS2SDR SWAA2021092714680Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENERS FROM BS887+3' TO BS927+15' BL0 WL 306.5 ON FUSELAGE SKIN UNDER DORSAL FIN ; / [01] RECEIVED ENGINEERING P1 TTG8Q006F9CT FOR REPAIR DISPOSITION.; [02] 'REFER TO FAULT TTG8Q006DPMC WHERE EA 21-153-02635 WAS ADSep 3, 2021 · N208WN · Boeing 737SDR IPXA2021101675006None · corrodedINSPECTION TYPE:CK12** SUPPLEMENTAL SDR **AFT CARGO TRANSITION PANEL LOCATED BETWEEN STA. 1529.0 AND 1640.0 HAS CORROSION. REPAIR IAW SRM. REPAIR IAW SRM 51-40-02-0G.Sep 3, 2021 · N470UP · Boeing 75724APFSDR HNAA2021100600475None · noneE878917 - STRINGER 19R GOUGED AFT OF FRAME 52 .... REPAIRED STRINGER 19R AFT OF FRAME 52 IAW PIEDMONT EO1-53-21-0256Sep 3, 2021 · N636AE · Emb EMB145LRSDR SWAA2021100426165None · crackedFWD CARGO COMPARTMENT CLIP CRACKED AT STA 400 AND S-25L (UNDER ZEE ANGLE) ; / [01] REMOVED CLIP AND INTERCOSTAL CRACKER AT FWD. CARGO COMPARTMENT STA. 400 TO STA. 420 AND S-25L IAW B-737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW BAFFLE AND CLIP PER Sep 3, 2021 · N225WN · Boeing 7377H4SDR ASAA2021090236140Cargo Track · crackedAFT PIT R/H CARGO TRACK IS CRACKED AT STA 727B AND 727E. GROUNDED - YES. REPAIRED AFT PIT RH CARGO TRACK FROM STA 727 TO 767 IAW B737-700 SRM 53-00-53-2R-3.Sep 2, 2021 · N615AS · Boeing 737790SDR ASAA2021090236136Cargo Track · corrodedAFT PIT CARGO TRACK HAS SPOTS OF CORROSION AT STA 787-847. GROUNDED - YES. REMOVED CORROSION ON AFT PIT CARGO TRACK RH OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 REPAIRED TRACK FROM STA 767-867 IAW B737-700 SRM 53-00-53-2R-3. W=1.0" O=.080" R=.063" L=22" D=.Sep 2, 2021 · N615AS · Boeing 737790SDR SWIA202161084None · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT CIRCUMFERENTIAL SPLICE BETWEEN FR 12-13 AND STG 3R-4R AS MARKED. (C-CHECK RO 09/19/2021) REPAIRED LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT CIRCUMFERENTIAL SPLICE BETWEEN FR 12-13 AND STG 3R-4R BY MEANS OF CUTSep 2, 2021 · N188SY · Emb ERJ170200LRSDR 2021F00289Skin · chafedREPAIR OF CHAFE IN LOWER FUSELAGE SKIN ABOVE ANTI-ICE CROSS-FLOW VALVE. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED: 07/19/2019 WITH FAA FORM 8100-9 DATED: 07/19/2019, 680A ALL S/N LWR CHAFE FROM ANTI-ICE CROSS-FLOW VALVE.Sep 2, 2021 · N511QS · Cessna 680ASDR DALA2022082905794Unknown · unknownSHIP 5643 DTA MONITOR INSPECTION LOG REF ERA 593624-14 REV. B. CORRECTIVE ACTION: REF ERA 593624-14 REV B. (1932962)Sep 1, 2021 · N543US · Boeing 757251SDR SWAA2021092713929Skin · corrodedSUPPLEMENTAL INFORMATION: CORROSION AROUND FASTENER AT B.S. 927+4; B.L. 0; W.L. 306.5. ; / [01] REMOVED 1 EA FASTENER PER SRM 51-40-02. REMOVED CORROSION AT DISCREPANCY AREA L=0.7' W=0.6'.PERFORMED VISUAL INSPECTION WITH A 10- POWER MAGNIFYING GLASS TO MAKE SUSep 1, 2021 · N208WN · Boeing 737SDR REXA2021092300758Seat Track · corroded"L/H FLOOR SEAT TRACK FS 995 TO 1002 CORRODED. " "REPLACED LH FLOOR SEAT TRACK AT FS 995 TO 1002 IAW CRJ 900 AMM 53-00-49-000/400-802-A02. WVAC EMP # 6449. "Sep 1, 2021 · N901XJ · Cndair CL6002D24SDR REXA2021092300748Drag Angle · cracked"L/H VERT. STAB AFT DRAG ANGLE TO TAIL CONE APPEARS TO BE CRACKED. " "REMOVED AND INSTALLED NEW AFT DRAG ANGLE (LH SIDE) VER. STAB TO TAIL- CONE IAW CRJ-900 SRM 51-42-13-001-001-0A01 AND SRM 51-42-21-001-001- A01 WVAC EMP STAMP # 796 MTC Sep 1, 2021 · N901XJ · Cndair CL6002D24SDR ASAA2021090135843Skin · corrodedFOUND SKIN CORROSION JUST BELOW THE WASTE TANK VENT PORT. GROUNDED - YES. REPAIRED FUSELAGE SKIN IAW 737-800 SRM 53-70-01-2R-3 THIS IS A CAT B REPAIR WITH AN INSPECTION INTERVAL OF 5,000 FLT CYCLES AND A THRESHOLD OF 50,000 FLT CYCLES A/C TOTAL FLT CYCLES AT TSep 1, 2021 · N546AS · Boeing 737890SDR DALA2021090205181Skin · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION ON THE FUSELAGE SKIN AT S-36R, BETWEEN STA 1175 AND 1197+6. C/W ERA 593684-14.Sep 1, 2021 · N186DN · Boeing 767332SDR HNAA2021091300469Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS ON FR 77 RH SIDE BELOW VERTICAL STAB. FABRICATED, PERFORMED CUTOUT. INSTALLED AND EDGE SEALED 1 EA. SKIN BUSHING ON FR. 77 RH SIDE IAW EMB 145 SRM 53-32-01 ITEM #9 FIG. 213 SHEET 2 SRM 51-20-01 AND PIEDMONT Aug 31, 2021 · N657AE · Emb EMB145LRSDR HNAA2021091300466Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS ON FR 77 LH SIDE BELOW VERTICAL STAB. FABRICATED, PERFORMED CUTOUTS, AND INSTALLED EDGE SEALED 2 EA SKIN BUSHINGS ON FR 77 LH SIDE IAW EMB 145SRM 53-32-01 ITEM #9 FIG 213 SHEET 2, 51-20-01 AND EO1-53-21-0242Aug 31, 2021 · N657AE · Emb EMB145LRSDR HNAA2021091300464Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS ON FR 79 RH SIDE BELOW VERTICAL STAB. INSTALLED AND EDGE SEALED 2 EA SKIN BUSHINGS ON FR 79 RH SIDE IAW EMB 145 SRM 53-32-01, ITEM 9, FIG. 213, SHEET 2, EMB 145 SRM 51-20-01, AND PIEDMONT EO1-53-21-0243.Aug 31, 2021 · N657AE · Emb EMB145LRSDR IPXA2021091073772Doubler · chafedINSPECTION TYPE:S/VINTERNAL DOUBLER HAS DAMAGED HOLES AND CHAFE DAMAGE BETWEEN STA. 1958 TO 1997 AND BETWEEN L48L TO 50L.REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG. AGA7167 AND SRM 51-33-01. (MINOR)Aug 31, 2021 · N296UP · Doug MD11FSDR SWAA2021090713131Skin · damagedDAMAGED FASTENER HOLES AROUND ANTENNA DOUBLER AND THE REPAIR AREA AFT OF THE NOSE L/GEAR DOOR CUTOUT SEE PIC FOR HOLE LOCATIONS. ; / [01] REPAIRED/OVERSIZED HOLES AROUND ANTENNA DOUBLER AS REQUIRED PER EA 21-153-02535; [02] REPAIRED/OVERSIZED HOLES AROUND ANTEAug 31, 2021 · N245WN · Boeing 7377H4SDR DALA2021090705249Skin · dentedSHIP 5643 DTA MONITOR INSPECTION LOG REF ERA 593633-14 REV. B. , SEVERAL DENTS (5EA) WERE FOUND ON EXTERNAL SKIN. CORRECTIVE ACTION: REF ERA 593633-14 REV B AND REF 593560-14. (1932028)Aug 31, 2021 · N543US · Boeing 757251SDR UIEA2021090301951Skin · dentedEMP - TAIL JACK POINT SKIN FOUND DENT MARK ( STA 2595 S-25R TO S-26R ). EMP TAIL JACK POINT SKIN DENT AREA REWORKED AS PER RI-53-14813 REV A</SPAN></P>)Aug 31, 2021 · N451PA · Boeing 74746NFSDR MASA20210831394Skin · dentedFUSELAGE SKIN PANEL BETWEEN FS1051.30-FS1069.75, STGR18R-STGR19R WAS FOUND TO HAVE DENTS. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 53-60-01-001-004-A02, ITEMS 1F AND G, EA 84-2021-001.Aug 31, 2021 · N957LR · Cndair CL6002D24SDR IPXA2021090973749Doubler · damagedINSPECTION TYPE:SVAFT FUSELAGE SKIN DOUBLER HAS 3EA ELONGATED HOLES BETWEEN STA.1975-1986 LON 48L-49L.REPAIRED 3EA ELONGATED HOLES AT AFT FUSELAGE SKIN DOUBLER BETWEEN STA.1975-1986 LON 48L-49L IAW VT-SAA EA 011-5330-01-A9341 REV I/R AND UPS EO MD11-5330-81536Aug 30, 2021 · N296UP · Doug MD11FSDR V0XD202109050001Skin · gougedRIGHT HAND FWD FUSELAGE AT F.S. 250.00 BETWEEN STGR 23R AND 24R THERE ISA GOUGE. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW STS ENGINEERING SOLUTIONS ENGINERING AUTHORIZATION 72-2021-148 P1, P2, AND IRAug 30, 2021 · N954LR · Cndair CL6002D24SDR DALA2021090305204Skin · damaged(LOG 1930827) DURING INSPECTION ELONGATED HOLES WERE FOUND (3EAS) ON FUSELAGE SKIN LH SIDE AT NLG JACK POINT AREA. PERMANENT REPAIR ON HOLES (3EAS) OF FUSELAGE SKIN LH SIDE AT NLG JACK POINT AREA WAS PERFORMED PER ETI-37-21-484 REV. 3 AND ER/A 593769-14.Aug 30, 2021 · N3731T · Boeing 737832SDR MASA20210831392Skin · damagedFUSELAGE SKIN BETWEEN FS1000.00- FS1031.00 & STGR22R - STGR24R WAS FOUND TO HAVE SEVERAL NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01, FIGURE 53-61-01-991-806, ITEM 1D, EA 69-2021-136. DEFECT LOCATION: FUSELAGE/FS 1000,00-FS1031.00 & STGR.22RAug 30, 2021 · N957LR · Cndair CL6002D24SDR MASA20210831391Skin · damagedFUSELAGE SKIN AT FS288.00-FS295.00 BETWEEN STGR17R-STGR18R WAS FOUND TO HAVE AN UNDOCUMENTED BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1, EA 72-2021-144. DEFECT LOCATION: FUSELAGE FS288.00-FS295.00 & STGR1Aug 30, 2021 · N957LR · Cndair CL6002D24SDR MASA20210831390Skin · damagedLOWER FUSELAGE SKIN PANEL WAS FOUND WITH BURN DAMAGE AT FS565.00 BETWEEN STR 24R & STR 25R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-991-806, ITEM 1B, EA 69-2021-129.Aug 30, 2021 · N244LR · Cndair CL6002D24SDR DALA2021090205193Skin · dentedSHIP 5643 FUSELAGE SKIN UPPER CROWN HAS 5 EACH LOCATIONS WITH DENTS AND REQUIRES REPAIRS STA 760-780 S-4R TO S-4L. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN FROM STA 760 TO 780 STR 4L TO STR 4R IAW ERA # 593633-14 REV ORIGINAL. (1929442)Aug 29, 2021 · N543US · Boeing 757251
Back to JASC 5330