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 FDEA202201260132Skin · dentedLWR FUSELAGE SKIN FR33 STGR41-42LH FOUND DENT REPAIRED THE DEFORMED LWR FUSELAGE SKIN AT FR33 STGR41-42LH PER A300-600F SRM53-10-12 FIG210. THIS IS CATEGORY B REPAIR. IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-10-12-2-004-00. FIRST INSPSDR CALA2022012600240Frame · crackedA3NB-53-3-6132 RH FWD EMERGENCY EXIT DOOR LH I/B BEAM FRAM CRACK ED DOT 42-054 () RH FWD EMERGENCY EXIT DOOR LH I/B REMOVED ANGLE CRACKED IAW SRM 51-42-11/001 AND INSTALLED NEW ANGLE IAW SRM 51-42-11/001 PN#D52 237902620451 BATCH#0003892709 PAINTED AS NEED IAWSDR SWAA2022022164206Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / [01] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D; STR 19R; WL 193 IAW SRM 51-40-02-0G-0;[02] NO ALLOWABLE DAMAGE ON SRM; PART WILL TO BE BY REPLACEMENT IAW SRM 5SDR SWAA2022022164205Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / [01] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D; STR 219L; WL 177 IAW SRM 51-40-02-0G-0;[02] NO ALLOWABLE DAMAGE ON SRM; PART WILL TO BE BY REPLACEMENT IAW SRM SDR AALA202201278682Skin · damagedAIRCRAFT IN BASE MAINTENANCE UPON REMOVAL OF LAV A, FOUND DOOR HINGE PIN MIGRATED UP INTO CONTACT WITH FUSELAGE SKIN BETWEEN BS 277 AND BS 294.5, BETWEEN S2L AND S3L. REPAIRED SKIN PER SRM 53-00-01-2R-20.SDR DALA2022012600523None · noneSHIP 3226 DURING WALK AROUND FOUND CORROSION ON FUSELAGE SKIN AROUND BOTTOM OF LAVATORY FAN EXHAUST. CORRECTIVE ACTION: COMPLIED WITH ERA 596785-14AD REV A. (8476486)SDR DALA2022012500507None · noneSHIP 3267 EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC BTW FR 60 TO FR 61 BTW STR 43R TO STR 44 AT LOWER FUSELAGE (SRM REPAIR) CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A320 SRM 53-00-11. (2098055)SDR DALA2022012500506None · noneSHIP 3267 EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 61 TO FR 62 BTW STR 43R TO 44 AT LOWER FUSELAGE. (SRM REPAIR) PERFORMED PERMANENT REPAIR PER A320 SRM 53-00-11. OK FOR SERVICE. (2098048)SDR DALA2022012500509None · noneSHIP 3226 NEED TO INSPECT REPAIR ER/A 596785-14AD. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. OK TO CONTINUE. (2097699)SDR FDEA202201240126Doubler · noneAPU COMPARTMENT STA 1885.2 RIGHT HAND SIDE LOWER REPAIR IS CHAFFED. AT APU COMPARTMENT STA 1885.2 RIGHT HAND SIDE LOWER REPAIR , REMOVED, FABRICATED AND INSTALLED NEW DOUBLER REPAIR IAW FED EX B757 SRM 53-80-08-2R.SDR YENA2022031100157Frame · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 41L LOCATED NWT FR 28 TO FR 30 INTERNAL AREA IN FWD CARGO COMPARTMENT; REF AEROMABN N/R 2021-491693, - PERFORMED REPAIR OF STRINGER 41L LOCATED BTW FRAME27 AND FRAME 31 IN FORWARD CARGO COMPARTMENT IAW A320 SRM 53-0SDR YENA2022031100143Pressure Panel · crackedDURING HEAVY MAINTENANCE, (E/C A21-1367-01) FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FRAME 35-36 / LHS ONLY / PRESSURE PANEL ATTACHMENT HOLES - MODIFICATION (REPAIR SOLUTION FOR CRACK DAMAGES) (CONSIDERED A MAJOR REPAIR)SDR YENA2022031100141Shear Plate · crackedDURING HEAVY MAINTENANCE, (E/C A21-1260-01) FUSELAGE/ WFF SUPPORT STRUCTURE/ A320-53-1259 KEEL BEAM SHEAR PLATE & TI ANGLE FR41-42R/ CRACKS- PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2022012600026None · noneFLT#1748, HDN-FLL (DIVERTED TO DEN). 'FLT # 1748, HDN-FLL(DIVERTED TO DEN). TAKE-OFF ROLL / ROTATION. POSSIBLE TAILSTRIKE. ON POST-FLIGHT WALKAROUND TAIL STRIKE NOTED MARKS ON UNDERCARRIAGE, NEAR; REF DEFECT 3135240-1 PRESSURE BULKHEAD SEAM FR 70 BETWEEN STR 3SDR SWAA2022012663134Web · crackedSUPPLEMENTAL INFORMATION: FWD. CARGO COMPT. UNDER SHIELD; WEB IS CRACKED AT FLOOR STRUT. AREA; BS 440;RBL 21. / [01] REMOVED FWD CARGO COMPT UNDER SHIELD WEB AT FLOOR STRUT. AREA BS 440RBL 21. AS PER B-737-7 SRM-51-40-02-0G-0;[02] VERIFIED STEP 1;[03] LOCATED SDR DALA2022030101315None · noneDENT FOUND LH SIDE OF FUSELAGE AFT OF L1 DOOR. DENT IS BETWEEN FR 23&24 LH SIDE 32" BELOW FIRST CLEAR WINDOW. DENT IS 3" TALL, 1" WIDE, .059 DEEP. ALLOWABLE DAMAGE PER SRM 53 -00-11-283-005 FIG 2. REPAIR CATEGORY C REPAIR WITHIN 200 FLIGHT CYCLES FROM FLIGHT 1SDR DALA2022012600544None · none(LOG 2094574) DURING INSPECTION FOUND ELONGATED HOLES COOMON TO SKIN AND BONDED DOUBLER AT STRINGER S-1, S2R AND CRACK AND MISSDRILLED HOLES ON SKIN. MAINTENANCE REPAIRED DAMAGE PER ERA 592112-14.SDR DALA2022012500495None · noneCRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R. SUMMARY OF NRC 00057: CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R WAS REPAIRED PER ETI-17-22-001 REV. 3 AND ER/A 596558-14AD SECTION I. PERMANENT REPAIR REPAIR APPROVAL IS LIMITED TO 60,000 FSDR SWIA202265403Skin · corrodedNUMEROUS AREAS OF FRETTING CORROSION ON EXTERIOR FUSELAGE SKIN AROUND NUT PLATE HOLES FOR APU EXHAUST SHIELD BETWEEN F.S.651.5 TO F.S.690. (C-CHECK RO 4/20/2022) REMOVED CORROSION FROM R/H EXTERNAL FUSELAGE SKIN COMMON TO THE APU EXHAUST SHIELD IAW MHIRSDR AALA202202115545Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: AT FUSELAGE CUTOUT FOR PANEL 312AR FOUND CORROSION AT FR 71 AND S28R. REPAIRED CUT OUT PER EA 333617.SDR REXA2022020900189Floorbeam · corroded"FLOORBEAM AT LBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO
FS 1098 TCI-53-30-306 "
"LOCATED AND DRILLED NEW FLOORBEAM P/N S6283 NAD INSTALLED @ F.S. 1000
TO F.S. 1088 LBL 9 IAW CRJ-900 SRM 53-00-41-201-0SDR DALA2024073007620Panel · dented(LOG 8325478) DENT 4FT FWD OF LAV SVC PANEL. COMPLETED REPAIR PER B737-900 SRM 53-00-01-2R-36.SDR REXA2022042000664Door Sill · corrodedAFT CARGO DOOR CUTOUT SILL HAS CORROSION IN VARIOUS LOCATION JC:900-53-280-506 - REMOVED AND REPLACED AFT CARGO DOOR SILL IAW CRJ900 SRM 51-42-13SDR SWAA2022013162298Light · inoperativeINOP EMERGENCY LIGHT POWER SUPPLY ASSY ROW 11 RT SIDE AT PASSENGER CABIN ; 2021-567452 / [01] REPLACEMENT EMERGENCY LIGHT POWER SUPPLY ASSY ROW 11 RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805.; [02] CORRECTED STEP 1: REPLACEMENT EMERGENCY LIGHTSDR IPXA2022012878388None · noneINSPECTION TYPE:C12CRACK ON FUSELAGE SKIN (P/N:148T3121-2) ON STA 1725.5 , NEAR S-7R.REPAIR I.A.W UPS EO B767-5330-24301-K AND 767-300F SRM 53-80-01-2R REPAIR 5 ,REV82.01.SDR CALA2022011800182Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR30 STR40R-42R ARE COR RODED (REPLACE SHEAR TIES/CLEATS) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR30 STGR 40R TO 42R IA W A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROS PACE MOBILE NR#0020647SDR CALA2022011800177Shear Tie · corroded(A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR31 STR 40R-42R ARE CO RRODED (REPLACE SHEAR TIES/CLEATS.) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR 31 STRG 40R TO 42R I AW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AERO SPACE MOBILE. NR#0020646SDR MASA20220118054None · none"THE FUSELAGE SKIN PANEL BETWEEN 43.75% MID SPAR DATUM AND 55.63%, STR 4L TO STR SL WAS FOUND WITH A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM). 53-71-01-991-828, ITEM 1 (REV. 38 DATED 9 JUL 2021 ). "SDR SWAA2022021462051Depressor · crackedCRACK ON DEPRESSOR LOCATED AT BS 294.5 AT LEVEL S-9R CUT OUT SERVICE DOOR AT PASSENGER CABIN ; 2022-11536 / [01] REPLACED DEPRESSOR LOCATED AT BS294.5 AT LEVEL S-9R CUT OUT SERVICE DOOR AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.; [SDR SWAA2022021161955Gusset · crackedFWD CARGO COMPARTMENT;RH GUSSET AT STA 500D;STR 18R IS CRACKED. ; / [01] REMOVED AND REPLACED R/H GUSSET AT FWD CARGO STA 500D ; STR 18R IRW B737-700 SRM 51-40-02-0G-0; [02] VERIFIED 1;COMPLETESDR MASA20220117051None · noneTH LH SKIN PANEL (P/N: SH690-33102.15)BETWEEN FS661.00+90.00-FS661.00+98.40 AND STGRL8L-STGR9L WAS FOUND TO HAVE A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-31-01-001-002-A02, FIGURE 53-31-01-991-804, ITEMS 1A AND D (REV. 37 DSDR MASA20220117050Stringer · none"THE STRINGER 21LH, BETWEEN FS 1126-FS1144 WAS FOUND WITH A SMALL NICK ON THE EDGE OF THE STRINGER, OUTBOARD OF THE ATTACHING FASTENERS. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-001-004-A02 STRUCTURAL ID.
8) CRJ7/9 STRUCTURSDR DALA2022011700298None · noneCRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L. SUMMARY OF NRC 00056: CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L WAS REPAIRED PER B717-200 SRM 53-03-01-2R, REPAIR 1 STEP 6 PAR G, FIG 20. REQUIRES VISUAL REPETITIVE (8,000 CYCLES) INSPECTSDR IPXA2022020378622Floor Panel · brokenINSPECTION TYPE:A300PNL 132MG IS BROKEN.FABBED PER SREO A300-5320-16407-E.SDR IPXA2022020378621Floor Panel · brokenINSPECTION TYPE:A300PNL 132AH IS DAMAGED.FABBED PER SREO A300-5320-16407-E.SDR IPXA2022020378620Floor Panel · brokenINSPECTION TYPE:A300PNL 132SG DAMAGED.FABBED PER SREO A300-5320-16407-E.SDR IPXA2022013178504Floor Panel · damagedINSPECTION TYPE:A300FWD CARGO COMPT. FLOOR PANEL 11GE DAMAGED/BROKEN.COMPLIED WITH SREO A300-5320-42722-F.SDR IPXA2022013178502Floor Panel · noneINSPECTION TYPE:A300FWD CARGO COMPT FLOOR PANEL 131MG DAMAGED BROKEN.COMPLIED WITH SREO A300-5320-42722-F.SDR HNAA2022011700052None · nonePDIS 655 05-51 2711371 14JAN22 SBY ASSGN
BIRD STRIKE CAPTS SIDE OF NOSE FWD OF WIPER DURING ROTATION. (NO ENGINE OR AIRSPEED ISSUES)
HISTORY: NO
AIRCRAFT CURRENTLY RECEIVING STRUCTURAL REPAIR TO DENTED AREA UNDER THE GUIDANCE OF EMBRAERSDR DALA2022011700309None · noneSHIP 3261 FUSELAGE / SKIN / FRAME 20 LH AT DOOR STOPS NUMBER 7/ DOUBLE JOGGLE / HOLE 8 SKIN / CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 595833-14 SECTION II INSPECTION. OK FOR CONTINUED SERVICE. (2086503)SDR CALA2022011700157Skin · damagedAIRCRAFT SKIN HAS GROUND DAMAGE STA.400 TO STA.420, S-20L TO S-22L. VISUALLY INSPECTED AREA OF REMOVED FUSELAGE SKIN STA 400-420 BETWEEN S20L AND S22L. NO FURTHER DAMAGE NOTED. OK TO CONTINUE. CUT AND REMOVED DAMAGE TO SKIN FROM STA.400 TO STA.420 BETWEEN S-SDR MASA20220114048None · dentedTHE LH FUSELAGE SKIN PANEL (P/N: SH690-33102-15) BETWEEN FS661.00+90.00-FS661.00+98.40 AND STGR8L-STGR9L WAS FOUND TO HAVE A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-31-01-001-002- A02,FIGURE 53-31-01-991-804, ITEMS 1A AND D SDR IPXA2022020478633Seat Track · corrodedINSPECTION TYPE:1CFORWARD MAIN CABIN SEAT TRACK CORRODED AT STA 475 X=-17.000.REMOVED,FABRICATED AND REPLACED CORRODED SEAT TRACK IAW MD-11 SRM 51-33-01 AND 51-21-01 (MINOR).SDR 2022FA0000058None · noneLIGHTNING STRIKE IN FUSELAGE SKIN @STA. 277, 1.5" ABOVE STR. 16R. REMOVED DAMAGE AT BS 277 1.5" ABOVE STR
16R IAW B737-800 53-00-01 REPAIR 36 REV 74 CUT OUT MEASURES 1.00" WIDE BY 4.00" LONG. FABBED DOUBLER FROM .040" 2024-T3, TRIPLER FROM .063" 2024-T3 AND FSDR IPXA2022012678307Floor Panel · noneINSPECTION TYPE:A300PANEL 242SN BROKENFABBED IAW SREO A300-5320-40552-BSDR IPXA2022012678305Floor Panel · damagedINSPECTION TYPE:A300PNL 242CN BROKENFABBED IAW SREO A300-5320-40552-BSDR IPXA2022012578264Floor Support · corrodedINSPECTION TYPE:1CMAIN CABIN LAV FLOOR SUPPORT CORRODED BETWEEN STA.Y=392-Y=440 AND X=-8.5-X=-27.5.REMOVED AND REPLACED CORRODED MAIN CABIN LAV FLOOR SUPPPORT BETWEEN STA.Y=392-Y=440 AND X=-8.5-X=-27.5 IAW MD11 SRM 51-31-01 AND 51-33-01 (MINOR).SDR SWAA2022012760871Baffle · crackedSUPPLEMENTAL INFORMATION: CRACKED BAFFLE FWD CARGO BAY BS459 LBL20 WL156 ; / [01] CRACKED FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION 1.; [03] REMOVED BAFFLE CARGO BAY 459 LBL20 WL156 PER SRM 51-40-02-0G-0;SDR SWAA2022013160883Angle · crackedCRACK ON FWD CARGO BAY FRAME TO INTERCOSTAL ATTACH ANGLE AT LBL 23 BS 400. ; / [01] DAMAGE FOUND ON INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL23; FOUND TO BE OUT OF LIMITS DUE TO O LIMITS ON SRM PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0GSDR SWAA2022012764618Baffle · crackedCRACKED BAFFLE FWD CARGO BAY BS418 LBL20 WL156 ; / [01] CRACKED FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION 1.; [03] REMOVED BAFFLE PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW BAFFLE P0# 782323/1 PE
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