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 DALA2021061103194Skin · gouged(LOG 1833717) DURING INSPECTION FOUND TWO GOUGES ON FUSELAGE SKIN, AT STA 845 AND ST 20 RH. TWO GOUGES ON FUSELAGE SKIN, AT STA 845 AND ST 20 RH WERE REPAIRED PER ETI-37-21-366 REV. ORIGINAL AND ER/A NO. 592035-14.SDR JJBA20210608014Skin · crackedRF1 RH EXT FUSE SKIN AT FRAME 75 ONE RIVET HOLE CRACKED JUST BELOW STR 2R. RF1 EXT FUSE SKIN AT FR 75 SKIN STRIPPED. RIVETS REMOVED AND SKIN + ANGLE CUTOUT CARRIED OUT. RF1 EXT FUSE SKIN AT FR 75 REPAIRED. NR # 53-2238SDR FDEA202106071865Skin · wornLH FUSELAGE STA 695 SKIN HAS GOUGE AT MAIN CARGO DOOR CUTOUT. MRKD AT LWR JAMB AFT OF LATCH SPOOL #4 REPAIRED PER EA # 8-5330-T0362732 P1SDR CALA2021060700808Skin · damagedB777-06-3-7176 - LH UPPER FUS STA212.5-STA220.5 AREA AFT OF FLIGHT COMPT WINDOW FOUND 1EA PREVIOUSLY BLEND. REF NR LP 9131391 LH UPPER FUSELAGE STA217 WL251.8 AFT AFT OF FLIGHT COMPT. WINDOW PREVIOUSLY BLEND AREA REPAIRED AS PER ECRA 5311-02578 REV- ATTAC H FOSDR P5CA2021051900173Skin · crackedM/D STA 1780 - 1840 RBL 55 - 77 CASTER PANEL SKIN FWD CORNER FOUND CRACK. M/D STA 1780 - 1840 RBL 55 - 77 CASTER PNL SKIN FWD CORNER REPAIRED AS PEREO 4425A500, SRM 51-70-13 AND COMPONENT SB AND CMM.SDR P5CA2021051900174Skin · crackedM/D STA 1840 - 1920 RBL 77 - 99 CASTER PANEL SKIN FWD CORNER FOUND CRACK.(<P>M/D STA 1840 - 1920 RBL 77 - 99 CASTER PANEL SKIN FWD CORNER REPAIRED AS PER EO 4425A500, SRM 51-70-13 AND COMPONENT SB AND CMM.SDR P5CA2021051900175Skin · crackedM/D SCD AFT DOOR SILL O/B PANEL UPPER SKIN FOUND CRACK.(<P>M/D SCD AFT DOOR SILL O/B PANEL UPPER SKIN REPAIRED AS PER <SPAN>EO 4425A500, SRM 51-70-13 AND COMPONENT SB AND CMM.</SPAN></P>)SDR P5CA2021052600197Skin · crackedNLG LH FWD CORNER SKIN FOUND 1EA FASTENER HOLE CRACK.(<P>NLG LH FWD CORNER SKIN 1EA FASTENER INSTALLED AS PER RI 53-10-14631 REV A.</P>)SDR UIEA2021052601201Bear Strap · corrodedC-1 DOOR CUT-OUT , UPPER FWD CORNER HAS EXFOLIATING CORROSION ON INNER SKIN.(<P>REMOVED CORROSION FROM C-1 DOOR CUT-OUT UPR BEAR STRAP FWD CORNER AND FOUND OUT OF LIMITS IAW B767 SRM 53-00-01-1A-1. REPAIRED UPR BEAR STRAP FWD CORNER IAW FAS EA 21050 REV. IR</SDR UIEA2021052701204Skin · corrodedBUBBLE PAINT EXTERIOR SKIN STA. 1310 STR. 34L SECTION 48. DOT 88-003(<P>UPON EVALUATION FUSELAGE SKIN AT STA. 1310 STR. 34L FOUND TO BE EXFOLIATED 100% MATERIAL LOSS. CUTOUT DAMAGE AND APPLIED A FILLER/DOUBLER REPAIR IAW B767 SRM 53-00-01-2R-1, 53-00-01, 51-10SDR CALA2021060700799Skin · scratchedA3NB-53-4-6229 DURING INSPECTION OF LOWER FUSE EXTERNAL SURFACE FR47-FR70 FOUND SCRATCH FUSE SKIN FR53-54 STGR29L-30L. EVALUATE IAW THE CURRENT SRM STANDARDS. SEQ 461 ZONE 100. 2 SCRATCHES FOUND ON FUSELAGE SKIN BTW FR53-54 STR29-30 LH. SCRATCHES BLENDED IAW SSDR SWIA2021081060231Doubler · corroded*CORROSION ON AFT CARGO UNDERFLOOR ANTENNA MOUNT DOUBLER LOCATED BETWEEN 1031.00 €“ 1069.70, STGR 27 €“ STGR 26L. AREAS MARKED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED 1EA AFT CARGO UNDERFLOOR ANTENNA MOUNT DOUBLER LOCATED BETWEEN 1031.00 - 1069.70SDR SWIA2021073059821Skin · dented* DENTS IN FUSELAGE SKIN FS625.30-FS640.00 BETWEEN STGR22L & STGR21L (C-CHECK RO 7/27/2021) REPAIRED DENTED FUSELAGE SKIN FROM FS621.00 TO FS640.00 BETWEEN STGR21L & STGR22L. REF REO 601R-53-61-7677 REV -- DATED 2021-07-05, CRJ200 SRM 51-42-21, & CRJ200SDR EE4Y2021071313375Skin · damagedDURING THE MAINTENANCE INSPECTION IT WAS FOUND AT FORWARD FUSELAGE SKIN, THE SKIN SECTION LOCATED BETWEEN FR6 AND FR7 AND BETWEEN STRG-13L/15L, WITH EXISTING TEMPORARY THROUGH DAMAGE REPAIR BEYOND SRM LIMITS. THE SKIN SECTION WAS REPAIRED BY INSTALLING AN EXTESDR SWAA2021071280280Skin · corroded**CORROSION** ON FUSELAGE SKIN AT BODY STATION 696; RBL 5; WL 305. / [01] REMOVED CORROSION ON FUSELAGE SKIN BS696 RBL5 WL305;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [02] VERIFIED REMOVED CORROSION ON FUSELAGE SKIN BS696 RBL5 WSDR SWAA2021071280279Skin · corroded**CORROSION** ON FUSELAGE SKIN AT BODY STATION 694; RBL 1; WL 306. / [01] REMOVED CORROSION ON FUSELAGE SKIN BS694 RBL1 WL306;1'X1' AREA I.A.W SRM 51-10-02-0G-01 AND ARM90-7023-01 TABLE 3001 ZONE 1; [02] VERIFIED REMOVED CORROSION ON FUSELAGE SKIN BS694 RBL1 WSDR SWIA2021073059817Access Panel · elongatedFASTENER HOLES AROUND LH FWD ACCESS PANEL 131AL ARE ELONGATED AS MARKED (C-CHECK RO 7/27/2021) REPAIRED FASTENER HOLES AROUND LH FWD ACCESS PANEL 131AL REF REO 601R-53-11-3703 REV €“ DATED 2021-06-18 STEPS 1-11. ALL STEPS COMPLIED WITH. COMPLIED WITH SDR SWAA2021071280239Skin · corrodedCHAFING DAMAGE ON INTERNAL FUSELAGE SKIN AT AFT CARGO BAY BS727D+16 LBL11 WL149. ; / [01] BLENDED CHAFE DAMAGE ON SKIN 3.3'X1.1' PER SRM 53-00-01-1A-5; [02] VERIFIED BLENDING ON CHAFE DAMAGE AREA ON SKIN 3.3'X1.1' PER SRM 53-00-01-1A-5; [03] HFEC INSP BLENDED SDR DALA2021060403092Skin · damaged(LOG 1827978) DURING INSPECTION FOUND PROTUBERANCE ON EXTERNAL FUSELAGE SKIN BTW STA= 485 AND STA= 495 STRINGERS 15 AND 16 RH SIDE. PROTUBERANCE ON EXTERNAL FUSELAGE SKIN BTW STA= 485 AND STA= 495 STRINGERS 15 AND 16 RH SIDE WAS REPAIRED PER ER/A 591999-14 REVSDR SWAA2021072279519Skin · corrodedCORROSION ON FUSELAGE SKIN AROUND WASTE TANK EXHAUST PORT AT B.S. 919; BETWEEN STRINGERS 21L AND 22L. ; / [01] REMOVED DECORATIVE EXTERIOR PAINT TO F.O.M. AT DISCREPANCY AREA PER AMM 51-21-11; [02] REMOVED FASTENERS COMMON TO DAMAGE AREA TO F.O.M PER SRM 51-40SDR SWAA2021072279520Skin · corrodedCORROSION ON FUSELAGE SKIN AT B.S. 1091; BETWEEN STRINGERS 24L AND 24R. ; / [01] REMOVED DECORATIVE EXTERIOR PAINT TO F.O.M. AT DISCREPANCY AREA PER AMM 51-21-11; [02] REMOVED CORROSION BY BLEND OUT AT DISCREPANCY AREA AND<BR>PERFORMED VISUAL INSPECTION WITH ASDR SWAA2021070679222Bear Strap · crackedCRACK INDICATION FOUND AROUND FASTENER LOCATED ON BEAR STRAP AT STA 295 AND 4 INCHES BELOW OF S-8R. L=0.200 INCHES APPROX ; 2021-247728 / [01] TOOL USED PN NORTEC600D SN 60009161631 DUE DATE DEC-01-21; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATESDR IPXA2021062871034Skin · corrodedINSPECTION TYPE:3CL/H EXTERIOR FUSELAGE SKIN HAS CORROSION BETWEEN STA. 2153 TO 2163 AND BETWEEN L33L TO 35L.REPAIRED CORRODED FUSELAGE SKIN BETWEEN STA. 2153 TO 2163 AND BETWEEN L33L TO 35L IAW SRM 53-70-01 REPAIR 3 FIG. 201. (MAJOR)SDR IPXA2021061770716Skin · crackedINSPECTION TYPE:SEGMID LOWER EXTERNAL FUSELAGE LH AFT AIR CON PANEL 143FR LANDING SUPPORT HAS A CRACKREMOVED AND INSTALLED REPLACEMENT LANDING PER SRM 51-40-21SDR IPXA2021061770714Panel · crackedINSPECTION TYPE:SEGMID LOWER EXTERNAL FUSELAGE LH AFT AIR CON PANEL 143FL LANDING SUPPORT HAS A CRACKREMOVED AND INSTALLED REPLACEMENT LANDING PER SRM 51-40-21SDR SWAA2021060778921Skin · crackedGROUND POWER DOOR CUTOUT LOWER SECTION CRACKED / ACCOMPLISHED REPAIR #4 ON THE ELECTERICAL GROUND POWER RECEPICALE SURROUND DABLER IAW SRM 53-10-2R-4.SDR DALA2021060403094Skin · dented(LOG 1827864) DURING CCK AT QRO, A FUSELAGE SKIN DENT WAS NOTED AT STA 500, BETWEEN S15R-S16R. MAINTENANCE REPAIRED DAMAGE PER ERA 591999-14.SDR DALA2021060403093Skin · gouged(LOG 1827644) DURING CCK AT QRO, WHILE PERFORMING A BASE ZONAL INSPECTION PER WC 5300-2422, TWO GOUGES WERE FOUND AFFECTING THE FUSELAGE SKIN BETWEEN STATION 807 827 AND S25L S27L. MAINTENANCE REPAIRED DAMAGE PER ERA 591986-14.SDR DALA2021060403090Skin · gouged(LOG 1827767) DURING INSPECTION FOUND GOUGE ON FUSELAGE SKIN ( 2 E A ) BTW STA =807 AND 827 BTW STR=27L / 25L AT FUSELAGE. GOUGE ON FUSELAGE SKIN ( 2 E A ) BTW STA = 807 AND 827 BTW STR=27L / 25L AT FUSELAGE ( FUS ) WERE REPAIRED PER ER/A 591986-14 REV ORIGINASDR EE4Y2021052412851Skin · damagedDURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THE LOWER FUSELAGE AT FR24+385MM, BETWEEN STRG 42R AND STRG 43R SKIN WITH NICKS, THE DAMAGE REMOVAL WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 SRM TSDR 2A6R2021060260603Skin · corrodedDURING 1000 HR INSPECTION, FOUND CORROSION AROUND PREVIOUS REPAIRS ON L/H AND R/H MAINTENANCE STEPS. PREVIOUSLY REPAIRED ON FAA FORM 337 DATED 16 SEPTEMBER 2013.SDR 2A6R2021060260602Skin · corrodedDURING 1000 HR INSPECTION, FOUND CORROSION AROUND AND UNDER DATA TAG. PREVIOUSLY REPAIRED ON FAA FORM 337 DATED 16 SEPTEMBER 2013.SDR JR2R202106027579Skin · dentedFWD FUSELAGE SKIN DENTED FROM APPARENT BIRD STRIKE BETWEEN FR01 AND FR02 AND STRINGER 2R TO STRINGER 6R. REPAIRED SKIN IAW EMBRAER ETD2021-170-015527.SDR 4AER2021100500001None · noneFOUR DENTS FOUND AT FS 755.0 + 3”-3.5”. DENT #1 AT FS 755.0 + 3.5” BETWEEN STR 26 - 27, 2.1” (L) X 1.5” (W) X .024” (D). DENT #2 AT FS 755.0 + 3.5” BETWEEN STR 25L – 26L, 2.4” (L) X 2.3” (W) X .008” (D). DENT #3 AT FS 755.0 + 3” BETWEEN STR 26 – 27, 2.4” (L) XSDR 4AER202108311001Skin · gougedFOUR DENTS LOCATED AT FS759.0, DENT #1 BETWEEN STR 25L-26L MEASURES 2.400(L) X 2.300(W) X .008(D), DENT#2 BETWEEN 26L-27 MEASURES 2.100” (L) X 1.500” (W) X .024” (D) DENT #3 BETWEEN STR 27-26R 2.400” (L) X 1.200” (W) X .022” (D) DENT #4 BETWEEN STR 25R-26R MESDR 4AER2021083100101Drag Angle · crackedPAX DOOR AFT DRAG ANGLE FS339.0 BETWEEN DATUM 3 AND DATUM 5 HAS A 5” CRACK BY THE ASSIST MOTOR PULLEY BRACKET. CUT AWAY 16.5” OF DRAG ANGLE. AND SPLICED IN 20” REPAIR DRAG ANGLE. REF. MHI RJ AVIATION REO 601R-52-11-513SDR EE4Y2021071313374Skin · dentedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT FWD LOWER FUSELAGE LH SIDE, AN EXISTING EXTERNAL DOUBLER REPAIR WITH DENTS SURROUNDING IT, A NEW EXTERNAL DOUBLER REPAIR WAS INSTALLED AS PER E.O. # COO-EO-2021-1296 R01, ETD2021-190-017944A AND APPROVED UNDER ASDR EE4Y2021071313373Skin · dentedDURING THE STRUCTURAL INSPECTION IT WAS FOUND AT FORWARD FUSELAJE, THE SKIN LH SIDE WITH EXISTING OIL CAN. THE OIL CAN WAS LOCATED COMMON TO AN EXISTING REPAIR AS PER SRM 53-10-01 REPAIR 64P AT FR12 BETWEEN STRINGER 21L AND STRINGER 23L. ALSO, THERE WERE TWO SDR SWAA2021061678827Skin · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER ACCESS DOOR CUT OUT LOWER AT LOWER FUSELAGE ; 2021-215742 / REPAIRED EXTERNAL GROUND ELECTRICAL POWER ACCESS DOOR CUT OUT LOWER AT LOWER FUSELAGE IAW SRM B737-700 53-10-15-2R-4 FIGURE 204 SHEET 1;REPAIRED EXTERNAL GROUND SDR DALA2021060403085Skin · damagedSHIP 685 INITIAL INSPECTION: PROTUBERANCE ON SKIN STA 1679 AND BTW STR 22/23 RH AT FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00103: PROTUBERANCE ON SKIN STA 1679 AND BTW STR 22/23 RH WAS REPAIRED PER ER/A: 591529-14 REV. ORIGINAL SECTION I.(1826741)SDR CALA2021053100762Skin · corrodedA3NB-57-3-6007. CORROSION ON CENTER WING BOX, UPPER SKIN UPPER S URFACE BETWEEN FR41-FR42 APPRX Y1550.(UNDER APU FUEL FEEDLINE). RECEIVED FINAL EC/RA #5310-07880 VERIFIED ALL STEPS COMPLIED WIT H AND DEVIATIONS NOTED LP CREATED FOR ACCOMPLISHMENT OF ESFR ENTRYSDR CALA2021053100754Skin · damagedLIGHTNING STRIKE DAMAGE FUSELAGE CROWN STA462 S-1 (MARKED 18) STRIKE DAMAGE OCCURED ON SKIN DIRECTLY OVER STRINGER. DAMAGE BEYOND LIMITS OF BLEND OUT AS PER SRM 53-00-01-2R-38 PAR 4D. CUT OUT DAMAGED AREA AS PER SRM 53-00-01-2R-35 REPAIR 35 HFEC INSPECTION OFSDR WX0A1900010073964None · noneNRC 1000-0043: 031-37 EXTERNAL FUSELAGE BILGE SKIN, LIGHTNING STRIKE FOUND AT PRODUCTION FASTENER + INTERFACE SKIN AREA OF 1"" FWD OF FRAME 68 AND 1"" ABOVE STRINGER 42R. / EXTERNAL FUSELAGE BILGE SKIN, LIGHTNING STRIKE AT PRODUCTION FASTENER + INTERFACE SSDR SWIA2021080560032Skin · dented*PROTRUDING DENT NOTED AT APPROX FS643.00 BETWEEN STRG25L-STRG26L (MARKED) (C-CHECK RO 8/1/2021) REPAIRED FUSELAGE SKIN AT APPROX FS643.00 BETWEEN STRG25L-STRG26L. REF REO 601R-53-61-7673 REV. -- DATED 2021-06-27. COMPLIED WITH 51-900-1003-SKY AND SEE SDR DALA2021060203014Skin · dentedSHIP 676 ACCOMPLISHED SECTION II OF ER/A 565228-14 REV C, AT STA 580-620 STR 1R-4R. CORRECTIVE ACTION: ACCOMPLISHED SEC II OF ER/A 565228-14 REV C AT STA 580-620 STR 1R-4R RECIEVED REPAIR INSTRUCTIONS AND ACCOMPLISHED REPAIR FOR DENTS AT STA 580-620 BTWN S-1 ASDR DALA2022052603657None · noneSHIP 676 DTA MONITOR INSPECTION LOG REF ERA 565227-14 REV.C. CORRECTIVE ACTION: REF ERA 565227-14 REV C. (1823745)SDR SWIA2021081060164Skin · dentedACFT EXTERIOR SKIN DENTED FROM INSIDE - BTWN FS'S 280/295 AND STGRS 24L/25L (C-CHECK RO 8/6/2021) REPAIRED ACFT EXTERIOR SKIN BETWEEN FS 280.00 - FS 295 AND STGR 24L - STGR 25L REF REO 670-53-21-2069 REV -- DATE 2021-07-01. COMPLIED WITH TASK CARD 51-90SDR ASAA2021052935072Skin · corrodedFUSELAGE SKIN CORRODED AROUND WASTE VACUUM EXHAUST VENT. GROUNDED - YES. REMOVED CORROSION FROM THE FUSELAGE SKIN AT STA 917, BETWEEN STR-21L AND STR-22L, ORIGINAL THICKNESS 0.125", REMOVED 0.023", REMAINING THICKNESS 0.102" AREA FOUND TO BE OUT OF LIMITS IAW SDR REXA2021060700407Doubler · corrodedINTERNAL STRUCTURE LOWER TCAS ANTENNA DOUBLER AT FS 300.00, STR 27 AREA CORRODED. REMOVED TCAS ANTENNA DOUBLER AND DRAME CLEET, LOCATED DRILLED, INSTALLED AND SEALED DOUBLER AND FRAME CLEET IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-SDR UIEA2021060101226Skin · dentedDENT STA 2596 IN BETWEEN STRUCTURE (DMI 101008) (UPGRADE THE EXISTING REPAIRS AND COMBINE WITH NEW DENT DAMAGE ON FUSELAGE SKIN NEAR STA 7598. S-26R RO S-46R (<P>ACCOMPLISHED EI NO T2021A53M-1401 REV.1.</P><P>CONDITION CHECK NORMAL.</P>)
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