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 SWAA2022011850326Gusset · crackedFWD CARGO COMPT STA 500D STR 18 R/H GUSSET CRACKED ; / [01] REMOVED R/H GUSSET AT FWD CARGO COMPT STA 500D STR 18 IAW B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES AT NEW GUSSET AT FWD CARGO COMPT SAT 500D STR 18 R/H. IAW B737-700 SRM 51-40-05-0G-SDR CALA2021120602267None · corrodedTRANSCRIBED FROM HAECO NR 9286539. B757-06-3-0244: AFT CARGO INT ERCOSTAL BETWEEN STA.1360-1380, STRINGER S26R-S27R CORRODED. TRANSCRIBED FROM HAECO NR 9286539.REMOVED CORRODED INTERCOSTAL IAW B757-200 SRM51-40-02. FABRICATED NEW INTERCOSTAL PER BAC DWG 146N32SDR CALA2021120602264Door · corrodedTRANSCRIBED FROM HAECO NR 9286297. (B757-53-3-0526) AFT CARGO COMPARTMENT DOOR SURROUNDING SUPPORT STRUCTURE - INTERCOST AL TO FORWARD FRAME 1380 ATTACH BRACKET EXFOLIATED. STREAMER FS 1360- FS 1380, STR S25R STR S26R. TRANSCRIBED FROM HAECO NR 9286297. REMOVESDR CALA2021120602260Floor Mat · corrodedTRANSCRIBED FROM HAECO GSO TASK CARD 9286698--SUPPORT TASK CBN F LOOR SHEAR WEB CORRODED BS 1681 BL LBL-0 REMOVED CORROSION IAW B757-2 SRM 53-60-51 AT STA 1681 LBL 10-55 REPAIR III. REF HAECO GSO MECH V933620 INSP QC418 ORIGINAL MATERIAL THICKNESS .156, REMOVSDR DALA2021120707544None · noneSHIP 3303 UPON LIGHTNING STRIKE INSPECTION FOUND DMG AT FRAME 14C STRINGER 1R. CORRECTIVE ACTION: REPAIRED PER ERA 595842-14. (2041958)SDR R61A2021120400977Doubler · corrodedCORROSION ON INTERNAL SKIN BETWEEN FRAME 90/91 STRG 29R/28R. REMOVED AND REPLACED INTERNAL DOUBLER REF EMB ETD2021-170-039289 RESTORE FINISH REF EMB SRM 51-23-04, 51-23-05 & 51-23-06 ON SKIN. MAJOR REPAIR.SDR R61A2021120400973Doubler · corrodedCORROSION ON WASTE BOX DOUBLER AFT OF FR88, O/B OF STR 28R. MAJOR REPAIR. REMOVED, LOCATED, DRILLED, AND ALODINED NEW WASTE BOX DOUBLER. INSTALLED NEW WASTE BOX DOUBLER. REF. SRM 53-23-60, 51-23-06, 51-40-02, 51-23-04, 51-40-08.SDR SWAA2021123049689Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY GUSSET IS CRACKED AT BS500D COMMON TO STR 21R ; / [01] EVALUATED GUSSET; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED GUSSET; FOUND TO BE OSDR SWAA2021123049687Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY GUSSET IS CRACKED AT BS 500D COMMON TO STR 23L ; / [01] CORRECT LOCATION OF CRACKED GUSSET IS BS 500D STRINGER 19 L/H; [02] EVALUATED GUSSET; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENTSDR SWAA2021123049686Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY GUSSET IS CRACKED AT BS 500D COMMON TO STR 19R ; / [01] EVALUATED GUSSET; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED GUSSET; FOUND TO BE SDR CALA2021120602246Skin · noneSUPPORT TASK, DURING AAI RECORD REVIEW, NO RECORD OF REPAIR AND NO RECORD TO ACCOUNT FOR THE REINSPECTION OF THE FUSELAGE DOUBLER REPAIR AT FUSELAGE STATION 1582 TO 1605 AND S-38R TO S-39L.. HAECO LOG 9132200, V913166 ON OR BEFORE THE ACFT ACCUMULATING 37500 TSDR CALA2021120602245Plate · crackedFRAME 36 PRESSURE PANEL HOLES 102,103,106 AND 120 BETWEEN Y765 A ND Y1292 HAVE CRAC INDICATIONS IN THE PRESSURE PANEL. A3NB-53-4- 6324; AD2019-23-01 PER HAECO LCQ N/R 9297008/31008 GENERATED BY V061633. ECRA 5331-02786 & REO-L23431 REV I & ECRA 5330-05216 OP00SDR SWAA2022011849610Doubler · crackedEXTERNAL POWER RECEPTACLE DOOR LOWER CUT OUT SKIN DOUBLER IS CRACKED. PROTECTED EWIS AREA AT EXTERNAL POWER RECEPTACLE DOOR. IAW AMM 20-60-07-913-801. REMOVED DOOR PANEL 114 AR FOR GAIN ACCESS. IAW SRM 51-40-02-0G-0. REMOVED THE INITIAL RUBBING BLOCK; THE LASDR SWAA2022010449600Angle · crackedCRACK ANGLE - CLIP LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT ; 2021-549817 / [01] REPLACED CLIP AND FASTENERS LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02. DGW: 143A7505 REV: A.; [SDR FDEA202112022957None · noneAGING AIRCRAFT - EXISTING REPAIR AT FWD CARGO DOOR CUTOUT - AFT JAMB SKIN EXTERIOR STATION 1009, LONGERON 39 RIGHT HAND TO 41 RIGHT HAND. EXISTING REPAIR AT FWD CARGO DOOR CUTOUT - AFT JAMB SKIN EXTERIOR STATION 1009, LONGERON 39 RIGHT HAND TO 41 RIGHT HANSDR SWAA2021120649603Skin · corrodedFUSELAGE SKIN UNDER DORSAL HAS MINOR CORROSION SPOTS BS 882-893 LBL 6- RBL 5. 8-143. REMOVED MINOR CORROSION ON AREAS IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREAS IAW NDT P4 51-00-00 PROC.3. FOUND WITHIN LIMITS IAW SRM 53-00-01-1A-1SDR DALA2021120307476None · noneDENT ON FUSELAGE SKIN AT FWD SIDE OF FRAME 5, APPROX. 8" ABOVE S39-L. REPAIRED DAMAGE ON FUSELAGE SKIN FWD SIDE OF FRAME 5 APPROX. 8" ABOVE S39-L IAW A321 SRM 53-11-11-991-003. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT OF 60,000FC OR 120,000FH WHSDR SWAA2021120349385Skin · crackedFUSELAGE SUBSURFACE CRACK INDICATION AT BS 500D+9 ABOVE STR4R ; FSELAGE SSRFACE CRACK INDICATION AT BS 500D+9 AOVE STR4R SING 737NDT PART 6; 53-30-25. VERIFIED FSELAGE SSRFACE CRACK INDICATION SING 737NDT PART 6; 53-30-18 AND 737NDT PART 4; 53-30-07. (CRACK INSDR NACA2021120100001None · noneCORROSION FOUND AT FRAME STATION 785.9 STRINGER S13 LEFT. REMOVED TREATED AND REPAIRED LEFT SIDE SECTION 43/45 SKIN PANEL ASSEMBLIES PN 145T3310 AND 143T3351 AT STA 785 PER AMES DOC# 47303REA20 REV A DATED 12/3/2021. ALL STEPS ACCOMPLISHED WITHOUT DEVIATION.SDR GTIA2021120236158Skin · dented"DENT FOUND ON LATERAL FWD FUSELAGE SKIN FR3-4 STR RH & LATERAL EDGE/ STRUCTURE -Z250. RAF01 2871822-02 CREATED-COMPLIED WITH E.O. 25311-2147"SDR GTIA2021120236155Skin · dented"DENT FOUND ON LATERAL FWD FUSELAGE UPPER CROWN RH FR11-12 STR RH & LATERAL EDGE/ STRUCTURE -Y511. RAF01 2871823-01 CREATED-COMPLIED WITH E.O 5311-2149"SDR CALA2021120202237Intercostal · corrodedTRANSCRIBED FROM HAECO NR 9286539. B757-06-3-0244: AFT CARGO INT ERCOSTAL BETWEEN STA.1360-1380, STRINGER S26R-S27R CORRODED. TRANSCRIBED FROM HAECO NR 9286539.REMOVED CORRODED INTERCOSTAL IAW B757-200 SRM51-40-02. FABRICATED NEW INTERCOSTAL PER BAC DWG 146N32SDR CALA2021120202236Bracket · noneTRANSCRIBED FROM HAECO NR 9286297. (B757-53-3-0526) AFT CARGO COMPARTMENT DOOR SURROUNDING SUPPORT STRUCTURE - INTERCOST AL TO FORWARD FRAME 1380 ATTACH BRACKET EXFOLIATED. STREAMER FS 1360- FS 1380, STR S25R STR S26R. TRANSCRIBED FROM HAECO NR 9286297. REMOVESDR CALA2021120102216Skin · dentedDENT IN SKIN PANEL 143A3111-29 NEAR STA 500A AND S-2R...REQUIRES A REPAIR DOUBLER TO BE INSTALLED REFORMED DENT, PERFORMED ALL REQUIRED INSPECTIONS, FAB''D REPAIR PARTS, TREATED, PRIMED, INSTALLED AND PAINTED IN REF TO ECRA#5331-02790 CONFIRMED COMPLIANCE WITHSDR NACA2021113000001None · noneCORROSION FOUND AT FRAME STATION 785.9 STRINGER S11 LEFT. REMOVED CORROSION AND TREATED AREA PER AMES INTERIM REPAIR 47303REA19 REV 1R DATED 12-1-2021. ALL STEPS COMPLIED WITH.SDR CALA2021120102210Skin · corrodedREFERENCE ECRA 5330-06888 FUSELAGE SKIN AT FR27-FR28 BETWEEN STR 43R-STR44 CORROSION INTERIM REPAIR. PER PART 1 STEP 2 GENERATE DIP, "ACCOMPLISH A PERMANENT REPAIR ON THE FUSELAGE SKIN AT FR27 -FR28 STR43R-STR44 PER PART 3 OF THE LASTEST REV OF ECRA5330-068 88SDR DALA2021120107403None · noneSHIP 3263 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR60 TO FR61 AND STR 43R TO STR 44 LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH AA 2335-01033, SRM 53-00-11-300-029, SRI 53-00-11-205- 017, TABLE 002 AND ER/A #575637-14 REV SDR DALA2021120107402None · noneSHIP 3263 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR61 TO FR62 AND STR 43R TO STR 44 LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH A320 SRM 53-00-11-300-029, SRI 53-00-11-205-017, TABLE 002 AND ER/A #575637-14 REV.A. (2033495SDR DALA2021120107389None · noneSHIP 6812 GOUGE AT LWR EXTERNAL FUSELAGE SKIN, STA. 1400-1420, BTW S-30 AND S-29R. CORRECTIVE ACTION: SUMMARY OF NRC 00023: GOUGE AT LWR EXTERNAL FUSELAGE SKIN, STA.1400-1420, BTW S-30 AND S-29R WAS REPAIR PER ETI-57-21-566 REV. 2 AND ER/A 595654-14 REV. ORIGISDR DALA2021120107382None · noneSHIP 3161 - DURING BIRD STRIKE INSPECTION FOUND DENT TO LOWER LEFT FUSELAGE BETWEEN FR5-FR7 17 INCHS FWD OF #3 PITOT PROBE & ABOVE #1 TAT PROBE. CORRECTIVE ACTION: C/W INSPECTION & TEMPORARY REPAIR PER ER/A 595586-14 (8358889)SDR DALA2021113007352None · noneSHIP 3331 RED LADDER CONTACTED BELLY OF A/C NEXT TO WATER SVC PANEL. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN REF A330-300 SRM 53-41-11-300-006. (8401270)SDR DALA2021112907298None · none(LOG 2032707) WHILE IN MSP FOR THE VIASAT MODIFICATION PER WORK CARD: 4430-01003-01D, MTC FOUND AN EXISTING SRM REPAIR (REF. LOG PAGE 2894467) COMMON TO FRAME STA 727D WHICH INTERFERE WITH THE SHEAR TIES INSTALLATION. THE FASTENER HOLES OF THE INTERNAL TEAR STSDR FDEA202111282943None · noneTHIS CARD IS CREATED FOR TRACKING PURPOSES TO CREATE A RDR/SDR FOR THE REPAIR DONE TO MCD LOWER JAMB AT STA. 697.87 UNDER E.A.8-5330-T0365660 B PART 2 CREATED RDR/SRD FOR MCD LOWER JAMB REPAIR USING E.A. 8-5330-T0365660 B PART 2.SDR VNAA2021112899991Skin Panel · damagedDENT AND GOUGE DAMAGE ON FUSELAGE SKIN AT FS 518 STR 16LSDR SWAA2021122748008Intercostal · crackedCRACKED CABIN INTERCOSTAL; BS 277-290; RBL 1; WL 208 (MARKED) ; / [01] REMOVED DAMAGED INTERCOSTAL FROM BS 277 TO BS 294 ; RBL 1 ; WL 208 IAW B737 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED INTERCOSTAL AT FLOOR STRUCTURE BS 277 TO BS 290 RBL 1 WL 208 PER SRMSDR DALA2021120107390None · noneSHIP 5639 DURING GVI WERE FOUND MISSING THREE (3EA) HOLES ON THE ANTENNA GOGO RING ATTACHMENT AND SKIN DOUBLER IN REF CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00320. AREA WAS REPAIRED PER ETI-57-21-554 REV. 1 AND ER/A 595659-14 REV ORIGINAL. SECTION II: PERMANESDR DALA2021113007362None · noneSHIP 5639 AWR. AA. CORROSION ON SEVERAL POINTS OF EXTERNAL DOUBLER BTW STA 690 TO STA 760 AND BTW S-3R TO S-3L. CORRECTIVE ACTION: SUMMARY OF NRC 00215. AREA WAS REPAIRED PER ETI-57-21-550 REV. 4 AND ER/A 595659-14 REV ORIGINAL. SECTION I: PERMANENT REPAIR. (2SDR FDEA202111262935Stringer · corrodedEXTERIOR FUSELAGE SKIN IS BUCKLED BETWEEN FASTENERS ON S-28L @ STATION 1468 AFTER FURTHER EVALUATION, "BUCKLE" IN SKIN FOUND TO BE TRAPPED FOD BETWEEN THE SKIN & STRINGER 28L NO DAMAGE NOTED TO SKIN, ONLY STRINGER. REPAIRED STRINGER 28L IAW FEDEX EA # F-5310SDR DALA2021112907323None · noneSHIP 6820 [A.A] INITIAL. DURING LFEC INSPECTION, CORROSION AND FLACKED PAINT WAS FOUND ON EXTERNAL DOUBLER CUT-OUTS AND SURROUNDING RIVETS BTW FUS STA 720-740 AND STGR 2L-2R. CORRECTIVE ACTION: SUMMARY OF NR 00487: PAINT ON EXTERNAL DOUBLER AT STA. 720-740 ANDSDR DALA2021112907296None · none(LOG 2030715) DURING INSPECTION CRACK OF 0.2IN OF LENGTH AT 03:00 HRS O?CLOCK POSITION WAS FOUND ON RH FUSELAGE SKIN AT FRAME STATION 540. FUSELAGE SKIN AT FRAME STA 540, IN REF. 5331-01278-01B, STEP 6 WAS REPAIRED PER ERA 595574-14AD.SDR DALA2021112907295None · none(LOG 2030575) DURING INSPECTION CRACKS WERE FOUND OF: 1) 0.100IN OF LENGTH AT 02:30 HRS O?CLOCK POSITION ON SKIN ON THE FIRST OPEN HOLE, 2) 0.100IN OF LENGTH AT 02:30 HRS O?CLOCK POSITION ON FRAME ON THE FIRST OPEN HOLE AND 3) 0.020IN OF LENGTH AT 06:30 HRS O?SDR DALA2026042902715Skin · not reportedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 61 TO FR 62 BTW STR 43L TO STR 42R AT LOWER FUSELAGE ( REFERENCE DOC NUMB ER AA CARD 5100-01821-01A). AIRCRAFT WAS GROUNDEDSDR FDEA202111242927None · noneLOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT STATION 1707, X= -52 FLANGE FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT DOORWAY DOOR CUT OUT CORROSION AT STATION 1707, X= -52 WORK COMPLIED AS PER EA # 1-5310-T0365753 P1 TITLE: FUSELAGE MAINFRASDR JJBA20211124040Skin · damagedFWD FUSELAGE 1 RH SKIN AT FR 3 BTW STR 01R-13R SEVERAL RIVETS NOT PROPERLY INSTALLED. PAINT STRIPPED ON FWD FUSELAGE I RH, STR 01R-13R FOR INVESTIGATION ON FWD FUSELAGE I RH SKIN AT FR3 BTW STR 01R-13R IMPROPERLY INSTALLED RIVETS REMOVED. RIVETS HOLES FOUND TOSDR JJBA20211124039Doubler · corrodedCORROSION FOUND ON ANTENNA INNER DOUBLER BTW FR 65-66 AND STR 21LH + STR 21RH. REMOVED R. ALT ANTENNA FOR ACCESS, REMOVED INNER AND OTHER DOUBLER FOR INVESTIGATION. AFTER FURTHER INVESTIGATION FOUND OUTER SKIN CRACK OUT OF LIMITS AT R. ALT ANTENNA LOCATION. PESDR QXEA2021112900532None · noneFWD PAX DOOR LOWER THRESHOLD CORRODED BEYOND LIMITS. REPLACED FWD PAX DOOR LWR THRESHOLD IAW SRM 51-42-05-02-01, 51-42-75-02-01 AND 51-23-00-00-01 REV 21.SDR DALA2021112807285None · none(LOG 2029540) DURING CCK AT QRO, WHILE PERFORMING RH FUSELAGE SKIN AT FRAME STA 540 INSPECTIONS PER WC 5331-01278-01B AND WC 5331-01278-2B, CRACKS WERE FOUND ON SKIN AND BULKHEAD SIDE CHORD HOLE. MAINTENANCE REPAIRED CRACKS PER ERA 595574-14.SDR DALA2021112507230None · noneSHIP 3248 DENT EXTERNAL SKIN LOCATED AT FR15 LEVEL STR 30L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-11-11. (2029283)SDR SWAA2021122746820Skin · crackedCORROSION ON CROWN SKIN UNDER VERTICAL STABILIZER STA 1012 TO STA 1044; RBL 8 TO RBL 13. ; / [01] REMOVED CORROSION ON CROWN SKIN UNDER VERTICAL STABILIZER STA 1016 TO 1040 RBL 8 TO RBL 13 REWORKED AREAS A= L: 15.6' W: 1.2' B= L: 9.7' W: 2.2' C= L: 4' W: 3.8' SDR FDEA202111233093Skin · dentedTHE RH FUSELAGE WAS FOUND 1EA DENT AT FR 55 5.5" STRG 36R ACCOMPLISHED DENT SKIN CAT.B REPAIR I.A.W A300-600 SRM 53-10-12-201, PARA5 PAGE.343-346 FIG224(SHEET1) AND SRI 53-10-12-201, IIR 53-10-12-2-004-00, PARA3D TABLE208 FIG204
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