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 EE4Y2021072913435Skin · damagedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT CENTER FUSELAGE II UPPER SKIN PANEL, EXTERNAL SKIN WITH REWORK LOCATED BETWEEN FR60 AND FR61, BETWEEN STR- 03L/05L, THE DAMAGE WAS REPAIRED INSTALLING EXTERNAL DOUBLER REPAIR AS PER E.O. # COO-EO-2021-13213 R00,SDR 2021F00270Skin · chafedLWR SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. ACCOMPLISHED STEP 1 THROUGH 5 OF TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA-53-22175 DATED 7-19-2019, 680A ALL S/N LWR SKIN CHAFE FROM ANTI-ICE CROSS FLOW VALVE. STEP 6 THROUGH 8 NOT COMPLETED DUE TO ACCOMPLISHMSDR 2021FA0000217Skin · chafedLOWER SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. REFERENCE STEPS 1-5 TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 REV -.SDR HNAA2021083100394Skin · crackedL/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVETS FR-77 IN THREE (3) PLACES. REPAIRED THE L/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVET AT FR-77 AT ONE (1) LOCATION IAW PIEDMONT EO1-53-21-0223, TWO (2) LOCATIONS FOUND NOT TO BE CRACKED,SDR HNAA2021083100393Skin · crackedL/H EXTERNAL FUSELAGE SKIN CRACKED AROUND RIVETS FR-78 IN THREE (3) PLACES. REPAIRED THE L/H EXTERNAL FUSELAGE SKIN AROUND RIVET AT FR-78 AT ONE (1) LOCATION IAW EO1-53-21-0223, TWO (2) LOCATIONS FOUND NOT TO BE CRACKED,SDR DALA2021072904266Skin · corrodedSHIP 3217 SKIN CORRODED AND FASTENERS PULLING THROUGH AT FRAME 70 R/H BETWEEN STRG 31 AND 32 R/H, APPROX 13 INCHES AFT OF LAV VENT OUTLET. CORRECTIVE ACTION: COMPLIED WITH ER/A 592914-14 REV ORIGINAL. (1891186)SDR CALA2021072801214Skin · damagedFUSELAGE SKIN DAMAGE STA.220 S-27R REFERENCE ECRA 5311-02609 AND LOG PAGE 6632591 FOR WORK ACCOMPLISHED. PERFORMED INTERIM REPAIR PER ECRA 5311-02609 PART 1. ACCOMPLISH PART 3 PERMANENT REPAIR AT OR BEFORE 50,000 TOTAL AIRFRAME CYCLES. APPROVED INTERIM REPAIR SDR DALA2021120307461None · noneSHIP 3217 ERA 592914-14 SECTION I ISSUED FOR REPAIR TO SKIN CORROSION AT FRAME 70 RHS. CORECTIVE ACTION: COMPLIED WITH ERA 592914-14. (1890680)SDR U2RA2021101100060Skin · corrodedWHILE ACCOMPLISHING T/C 53-830-01-01, FOUND CORROSION ON SKIN DOUBLER, R/H SIDE AT WATER OVERFLOW VALVE AREA. ACCOMPLISHED MAJOR REPAIR R/H FUSELAGE SKIN DOUBLER P/N 65B04118-22,CORROSION AT R/H WATER OUTFLOW VALVE STA 980 IAW EA 747-5320-56-A9230 REV. I/R. 8SDR FDEA202107272005Doubler · gougedDURING PFM WORKCARD:E6-5100-7-5000 D7 PT1, FOUND GOUGE ON THE EXISTING REPAIR DOUBLER SURFACE AND SKIN CUTOUT EDGE AREA AT FR20A BETWEEN S-38R TO S-41R. GENERTAING FROM EO:E6-5100-7-5000 D7 PT1 & WO/NRC:00080535/N00132, ACCOMPLISHED THE WORK I.A.W. E.A:T6-SDR CALA2021072801202Skin · bulgedSKIN IS BULGING AND HAS PULLED THROUGH FASTENER AT STA 246, OUTBD OF RIGHT NOSE LANDING GEAR DOOR. TOMC LOCKING FOR MX FERRY REMOVED FASTENERS AND REMOVED CORROSION. FLANGE IS 100% CORRODED. UNLOCKING NEED TO PERFORM DVI OF LOWER CHORD AND SURROUNDING AREA REFSDR SWIA202161093None · dented*PROTRUDING DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 280.00 €“ 295.00, STGR 25R €“ 26R (C-CHECK RO 9/21/2021) PERMANENTLY REPAIRED PROTRUDING DENT AND GOUGE ON INTERNAL AND EXTERNAL SKINE BETWEEN FS280-FS295 STGR 25R TO 26R REF REO 670-53-21-2117 REVSDR SWIA202161092None · dented*PROTRUDING DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 280.00 €“ 295.00, STGR 24R €“ 25R (C-CHECK RO 9/21/2021) PROTRUDING DENT AND GOUGE ON EXTERNAL FUSELAGE SKIN BETWEEN FS 280.00 €“ 295.00, STGR 24R €“ 25R PERMANENTLY REPAIRED REF REO 670-53-21-21SDR DALA2021072904272Skin · cracked(LOG 1889082) DURING INSPECTION FOUND CRACKS ON FOUR HOLES ON SKIN TO ATTACH THE ADAPTER RING AND ELONGATED HOLE BTW STRG 2 LH STA 727F. AREA WAS REPAIR PER ETI-37-21-434 REV 12 AND ERA 593033-14.SDR IPXA2021072672122Skin · corrodedINSPECTION TYPE:N/ACORROSION ON FUSELAGE SKIN UNDER AFT VHF ANTENNA STA 1726 STR 52-51RREPAIRED PER SRM 53-00-00 FIG 202 SHEET 4/4SDR SWAA2021091548253Bear Strap · crackedCRACK INDICATION FOUND AROUND FASTENER LOCATED BEAR STRAP AT LEVEL FITTING-LATCH; STA 294.5 BETWEEN S-8R AND S-9R. ; 2021-341948 / [01] TOOL USED. P/N: NORTEC 500D. S/N: N500X12101V022233. DUE DATE: 02-JUN-2; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DSDR IPXA2021080272338Skin · dentedINSPECTION TYPE:C4DENTS ON SEC 41 FUSELAGE SKIN(P/N:141T3231-10) BETWEEN STA 287 AND STA 303,S-31R.REPAIR I.A.W BOEING SR 3-5063128792 AND UPS EO B767-5330-81169-ASDR SWAA2021091597564Skin · chafedPANEL 194CR INNER SKIN MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 194CR / MATERIAL IAW SRM 53-60-70-0I-1 FIG. 2 TABLE 2 ITEM [6]. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4. B. (8). FIG. 105. <BR><BR>REPAIR TO BE ACCSDR SWIA2021091360952Skin · corrodedMAIN AVIONICS BAY INNER SKIN FROM FS360.00 TO FS364.00 BETWEEN STR 26L AND STR 26R HAS SPOTS OF CORROSION (C-CHECK RO 9/8/2021) CORROSION ON INNER SKIN FROM FS360.00 TO FS364.00 BETWEEN STR26L AND STR 26R WAS REMOVED AND FOUND TO BE WITHIN LIMITS AND FINISDR SWIA2021091360949Doubler · corrodedMAIN AVIONICS BAY FWD DRAIN MAST DOUBLER FROM FS333.00 TO FS349.00 BETWEEN STR 25R AND STR 24R CORRODED (C-CHECK RO 9/8/2021) FOUND CORROSION TO BE OUT OF LIMITS ON MAIN AVIONICS BAY FWD DRAIN MAST DOUBLER FROM FS333.00 TO FS349.00 BETWEEN STGR 25R AND STSDR SWAA2021090398064Bear Strap · crackedCRACK NOTED AT R-1 DOOR BEAR STRAP BS-294.5 5' ABOVE STR-9R. CRACK APPROXIMATELY 1/4' - 1/2' INCH LONG AT TYPICAL LOCATION (SEE FIGURE 4 ON TASK TTG8Q001VJ2Y FOR TYPICAL LOCATION) ; / CUT AND REMOVED THE DAMAGED PART OF THE BEARSTRAP BY 2.2' LX1.0'W IAW SRM 53SDR DALA2021072704220Skin · damaged(LOG 1886918)DURING CCK AT QRO, WHILE PERFORMING STEPS 17 & 18 OF WORK CARD 2330-01337-1001, FOUR (4) CRACKED HOLES AND TWO (2) ELONGATED HOLES WERE FOUND ON FUSELAGE SKIN BETWEEN STA. 727E & 727H, STRINGER S-3R & STRINGER S-3L. ADDITIONALLY, A DENT ON FUSELAGSDR CALA2021072601178Skin · buckledAFT LOWER FUSELAGE SKIN BUCKLED AT FR73 AND FR 74 AT ALL 4 CORNE RS OF AFT JACK POINT STRUCTURE. REF TO AIRBORNE/PEMCO NR 11080.0025 REMOVED DAMAGED SKIN AND SUPPORTING SHEAR TIES AT FR 73-74, STR. 31L-31R IAW A319- SRM 53-51-29. FABRICATED NEW REPAIR DOUBLER SDR JJBA20210723065Doubler · not reportedEXTERNAL SKIN EXISTING DOUBLER REPAIR BETWEEN FR19 AND FR20 BETWEEN STR 6L AND STR 8L. REPAIRED EXTERNAL SKIN BETWEEN FR19 AND FR20 BETWEEN STR 6L AND STR 8L.SDR A6WA202108047849Skin · corrodedSKIN SURFACE CORROSION AT ADF ANTENNA SKIN SURFACE FS409.00 + 63 TO FS409.00 + 73 AND AROUND 3 BOLT HOLES AT FS409.00 + 73 AND FS409.00 + 82. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT ADF SKIN SURFACE FS409.00 + 63 TO FS409.00 + 73 AND AROUND SDR FDEA202107231843Skin · dentedAFT CARGO - EXTERIOR STATION 1964 LONGERON 38 LEFT TO LONGERON 39 LEFT FOUND DENT . AFT CARGO - EXTERIOR STATION 1964 LONGERON 38 LEFT TO LONGERON 39 LEFT DENT DAMAGE CARRIED OUT REPAIR AS PER SRM 53-00-15-2R REPAIR 8 FIGURE 202 . REPAIR CLASSIFIED AS MASDR VNAA2021072701111Skin · dentedDURING MX OPERATIONS IN CANTON OH, (CAK) MX REPORTS TWO DENTS LOCATED UNDER CAPTAIN'S WINDSHIELD ABOVE RVSM AREA. LOCATED ON L/H SKIN PANEL (FS202.75-FS280.00). BOTH DENTS ARE ABOVE STGR12A BETWEEN FS220.00 AND FS202.75. FWD DENT MEASURES .8125" LONG, .5937" WSDR DALA2021072604194Skin · corrodedSHIP 3138 - AFT R/H FUSELAGE FR69 @ STR 26R FWD OF ACCESS DOOR 312AR VENT FITTING IN SKIN HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REPAIRED AREA IAW A319 SRM 53-41.(1885431)SDR CALA2021072601176Skin · gougedRT FUSALAGE SKIN BETWEEN STA. 219.5 - 224.8 SKIN GOUGED LOCATED 3" ABOVE S-27R AND GRID MAP OF AREA REQUIRES ULTRASONIC TEST NDT. COMPLIED WITH STEPS 1 THRU 4 OF AVO9055, BURNISHED DAMAGED AREA PERFORMED ULTRASONIC THICKNESS MEASUREMENTS FOR THIS AREA IAW 737NSDR SWAA2021091597509Bear Strap · crackedFORWARD GALLEY DOOR BEAR STRAP; BETWEEN S-8R AND 9R; BS291.- BS294.5 CRACKED APROX. 2.800' ; / [01] TRIMED OUT AND REMOVED THE DAMAGED AREA AT BEARSTRAP FWD GALLEY DOOR BETTWEEN S-8R AND S-9R BS 293 L=3.4; W=3 PER SRM 53-10-01-2R-6 REP. 6; [02] DO A HEFC EDDY SDR R61A2021081400638Access Door · corrodedCF III WASTE ACCESS DOOR HAS CORROSION. REPLACED IAW AMM 20-10-01-910-801-A.SDR JJBA20210722005Doubler · not reportedREPAIR DOUBLER ON LH CENTER FUSE 1, BTW FR 20-21 AND BTW STR 11L - 12L. REPAIR DOUBLER ON LH CENTER FUSE 1 BTW FR 20-21 AND STR 11L-12L REMOVED FOR INVESTIGATION. AFTER INVESTIGATION, CUT OUT NOT CONFORM. CUT OUT ON L/H FUSE, CF1, BTW FR20-21 AND BTW STR 11L-1SDR A6WA202108047848Skin · dentedAFT FUSELAGE DENT AT FS590.00 + 3Ï¿½ STR23L + 1Ï¿½ AND FS590.00 + 2Ï¿½ STR22L + 5Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENTS AT FS590.00 + 3Ï¿½ STR23L + 1Ï¿½ AND FS590.00 + 2Ï¿½ STR22L + 5Ï¿½. PART NUMBER 601R35005 SKIN THICKNESS 0.063Ï¿½. DSDR A6WA202108037844Skin · dentedAFT FUSELAGE HAS 3 SKIN DENTS AT FS654.50 THROUGH FS672.00 AND S21R Ï¿½ S23R. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED AFT FUSELAGE SKIN AT FS654.50 THROUGH FS672.00 AND S21R Ï¿½ S23R TO ORIGINAL CONTOUR. DIMENSIONS DENT #1 - L = 1.600Ï¿½ X W = 0.600Ï¿½ SDR A6WA202108037845Skin · dentedAFT FUSELAGE SKIN DENT AT FS636.5, S27R-3.5Ï¿½. *AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT FS636.5 S27R-3.5Ï¿½ TO ORIGINAL SKIN CONTOUR. DIMENSIONS L = 1.700Ï¿½ X W = 1.00Ï¿½ D = 0.023Ï¿½. PART NUMBER 601R35005 AND SKIN THICKNESS 0.063Ï¿½. HFEC SDR FDEA202107221833Skin · dentedFUSELAGE - DENT FOUND AT RIGHT HAND FUSELAGE SKIN APPROXIMATE STATION 1835 LONGERON 33 RIGHT HAND AREA. FUSELAGE - AT RIGHT HAND FUSELAGE APPROXIMATE STATION 1835 LONGERON 33 RIGHT HAND DENTED SKIN AREA REPAIRED AS PER SRM 53-00-01-2R FIGURE 201 REPAIR 1. SDR SWAA2021072697321Doubler · crackedTHE ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS A 2 CRACK IN ZONE 2 AND ADJACENT TO TWO FASTENERS. ; / [01] C/W 10X VISUAL INSPECTION OF THE TRIMMED OUT AREA.; [02] C/W HFEC INSPECTION OF TRIM OUT EDGE AND INTERIOR STRUCTURE PER NDT PART 6 51-00-00SDR DALA2021072304156Skin · damagedSHIP 3233 NEED TO PERFORM INSPECTION ON FASTENER HOLE LOC. ON STR 7R BTW FR 60 TO FR 59 UPPER SKIN. CORRECTIVE ACTION: PERFORMED INSPECTION PER A320 SRM 53-41-11-300-014 AND SRM 53-41-11. CONTINUE ON MON. (1884310)SDR CALA2021072301163Skin · dentedDAMAGE ON SKIN R/H SIDE NOSE AREA FS251.6 PER AVO9056 REV.A STEP1 COMPLETED ON L/P 6612667. STEP 4 COMPLETED PER NDT PART 4-51-00-00-03. STEP 5 HFEC EXTERNALLY COMPLETED PER NDT PART 6-51-00-00-23 WITH NO FINDINGS. STEP 6 COMPLETED WITH A CREASED DENT FOUND. SSDR DALA2021072204143Skin · dentedSHIP 3329 DENT EXTERNAL SKIN FR 26.3 AND BTW STR 38R TO STR 39R AT LOWER FUSELAGE. CORRECTIVE ACTION: EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS AS PER A330 SRM 53-21-11-283-003, FIGURE 003, SHEET 01. MEASURES OF REWORK ARE: L= 2.418IN, W= 1.934 IN. (1883SDR DALA2021072204142Skin · gougedSHIP 3329 GOUGE EXTERNAL SKIN FR 83 AND BTW STR 39R TO STR 40R AT LOWER FUSELAGE. CORRECTIVE ACTION: EVALUATED REWORKED AREA LOCATED ON EXTERNAL SKIN ON FR83 AND BTW STR 39R TO 40R AND FOUND WITHIN LIMITS AS PER A330 SRM53-51-11-283-001 FIGURE 003 SHEET 01. MESDR SIMA20210721013Skin · corrodedEXTERIOR FUSELAGE SKIN IS CORRODED BETWEEN FR 57 RT AND 58 RT AND BETWEEN STR 19 RT AND STR 20 RT (LEVEL2 CORROSION) (MAJOR REPAIR)-C/A-COMPLETE:RAR POTABLE WATER FILL/OVERFLOW NIPPLE DOUBLER IAW SRM 51-40-02.SDR IPXA2021080572484Skin · corrodedINSPECTION TYPE:2CCENTER WING UPPER SKIN AT STRINGERS 9, 10 AND 12 BETWEEN XCW 101 TO XCW 110 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN AT STRINGERS 9, 10 AND 12 BETWEEN XCW 101 AND XCW 110 IAW VT-SAA EA 011-5730-01-A9262 REV. IR AND UPS EO MD11-573SDR IPXA2021080572474Skin · corrodedINSPECTION TYPE:2CCENTER WING UPPER SKIN AT STRINGER 15 AND BETWEEN XCW 101 TO XCW 110 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN AT STRINGER 15 AND BETWEEN XCW 101 TO XCW 110 IAW VT-SAA EA 011-5730-01-A9256 AND UPS EO MD11-5730-81179-A. (MINOR)SDR AALA202107277247Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: EXTERNAL POWER DOOR CUTOUT DOUBLER CRACKED. REPLACED DOUBLER PER SRM 51-40-02 AND DWG 141A3702.SDR HNAA2021072700334Skin · crackedEXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 13 RIVETS ON FR 79 BTW STR 3R-8R. .... REPAIRED EXTERNAL FUSELAGE SKIN CRACK AROUND 1 RIVET ON FR 79 BETWEEN STRINGERS 8R AND 9R. 12 RIVETS WERE FOUND NOT TO HAVE CRACKS AROUND THEM, SEE TASK 1.SDR HNAA2021072700333Skin · crackedEXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 26 RIVETS ON FR 77 BTW STR 2R-8R. REPAIRED EXTERNAL FUSELAGE SKIN CRACKS AROUND 3 RIVETS ON FR 77 BETWEEN STRINGERS 04R AND 08R IAW PIEDMONT EO1-53-21-0178 (BUSHING REPAIRS), REPAIRED EXTERNAL FUSELAGE SKIN CRSDR HNAA2021072700332Skin · crackedEXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 26 RIVETS ON FR 77 BTW STR 2R-8R. ... REPAIRED EXTERNAL FUSELAGE SKIN CRACKS AROUND 3 RIVETS ON FR 77 BETWEEN STRINGERS 04R AND 08R IAW PIEDMONT EO1-53-21-0178 (BUSHING REPAIRS), REPAIRED EXTERNAL FUSELAGE SKSDR HNAA2021072700331Skin · crackedE867326 - EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 13 RIVETS ON FR 79 BTW STR 3L-9L. ... FURTHER INVESTIGATION OF THE 13 POSSIBLE EXTERNAL FUSELAGE SKIN CRACKS ON FR 79 BTW STR 3L-9L, ONLY 2 EA. CRACKS WERE FOUND. SEE TASK ENTRY #1 FOR NDT RESULTS. 1 SDR HNAA2021072700330Skin · crackedE867325 - EXTERNAL FUSELAGE SKIN HAS POSSIBLE CRACKS AROUND 14 RIVETS ON FR 78 BTW STR 3L-8L. ... FURTHER INVESTIGATION OF EXTERNAL FUSELAGE SKIN POSSIBLE CRACKS AROUND 14 RIVETS ON FR 78 BTW STR 3L-8L FOUND ONLY 1 CRACK. SEE WIPS AND TASKS FOR NDT DETAILS. RE
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