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 MASA20220112039None · noneTHE FUSELAGE SKIN PANEL BETWEEN FS 897.70 AND FS 969, STR 13L-STR 18L WAS FOUND WITH DAMAGE DUE TO NICKS AT (31) LOCATIONS. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 53-51-01-001-002-A02 STRUCTURAL IDENTICATION. B)CRJ7/9 SRM 53-51-01-101-002-A04 / 53-00-01-101-0SDR MASA20220112037None · dented"THE FUSELAGE SKIN PANEL BETWEEN FS1051.3-FS1069.75, STR 19R-STR 20R WAS FOUND WITH A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-001-004-A02 STRUCTURAL ID.
B) CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-101-004-A02 ASDR MASA20220112036None · dentedTHE LOWER FUSELAGE SKIN PANEL (P/N: MM690-35146-005) BETWEEN FS1015.00-FS1031.00 AND STGR23L-STGR24L WAS FOUND TO HAVE A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-001-003-A02, FIGURE 53-61-01-991-806, ITEMS 1 AND E (REV.SDR MASA20220112035None · noneTHE FUSELAGE SKIN BETWEEN FS 1031.00 TO FS1051.00 AND STRINGER 21R TO STGR 26R WAS REPORTED WITH MULTIPLE DAMAGES CONSISTING OF NICKS THAT WERE BLENDED SMOOTH AND GROUPED IN LOCATIONS DENOTED AS DETAILS A THROUGH L. PERFORM PERMANENT REPAIR JAW CRJ7/9 STRUCTURSDR MASA20220112034None · noneMAINTENANCE DISCOVERED GOUGES ON THE SIDE SKIN PANEL OF THE FUSELAGE, BETWEEN FS1000.00-FS1051.00 AND STGR16L-STGR19L. PERFORM PERMANENT REPAIR IAW CRJ7/9 53-61-01-001-002-A02, FIGURE 53-61-01-991-804, ITEM 1, A, AND B (REV. 33 DATED JUN. 25, 2017).SDR CALA2022011200118Beam · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACSDR SWAA2022020860837None · corrodedPLATE-HINGE CLOSEOUT BELOW LAVATORY SERVICE ACCESS DOOR CUTOUT HAS CORROSION AT AFT SIDE ; / [01] REMOVED CORROSION ON THE AFT SIDE OF THE PLATE HINGE CLOSEOUT BELOW LAVATORY SERVICE ACCESS DOOR CUTOUT IN 2.4'LX0.7'W AREA IAW SRM 51-10-02; [02] VERIFIED CORRECSDR IPXA2022012578263None · noneINSPECTION TYPE:1CMAIN CABIN R-3 PLUG DOOR AFT JAMB WEB(INNER SKIN) CRACK AT STA.Y=1307 & Z=-17.5.REPAIRED MAIN CABIN R-3 PLUG DOOR AFT JAMB CRACKED WEB(INNER SKIN) AT STA.Y=1307 & Z=-17.5 IAW MD-11 SRM 53-40-15,REPAIR 3 FIG 201,REV.68.01 (MAJOR).SDR DALA2022011300271None · none(LOG 2082909) DURING LINE OPERATIONS A LAVATORY SERVICE TRUCK IMPACTED THE FUSELAGE SKIN AT STATION BS 870, BETWEEN S23L-S24L. MAINTENANCE REPAIRED DAMAGE PER ERA 596297-14.SDR MASA20220111031None · dented"THE FUSELAGE SKIN, BETWEEN STA. 169-STA.173,STR. 0-STR 1 L WAS FOUND WITH A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-11-01-001-004-A01. SKIN, TOP PANEL. STRUCTURE IDENTIFICATION.
B) CRJ7/9 SRM 53-11-01-101-004-A01 ALLOWABLSDR DALA2022011200233None · noneSHIP 3247 DENT EXTERNAL SKIN LOCATED FROM FR19 TO FR20 AND 11 INCHES ABOVE LOWER STRINGER RH AT LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED PER A320 SRM 51-73-11 AND FOUND DENT TO BE WITHIN LIMITS. (2082868)SDR CALA2022011200114Skin · noneSTA.351 STR. 2L DENT OUT OF LIMITS. (REF. F/C N/R 9796454) BEFORE 50,000 TOTAL AIRCRAFT FLIGHT CYCLES". REPAIRED PER ECRA 5330-06900 . ALL WORK PERFORMED ON F/C N/R 9796454. PLACED ON DIP TO "ACCOMPLISH A PERMANENT REPAIR ON ORSDR DALA2022011100231None · noneSHIP 3325 INDICATION OF LIGHTING STRIKE STA. FR45+8 BETWEEN STRINGER 7 AND 8. CORRECTIVE ACTION: INSTALLED TEMPORARY REPAIR PER 53-11-11-300 CATEGORY C REPAIR. (2082027)SDR IPXA2022013078449None · crackedINSPECTION TYPE:3CAFT CARGO COMP. VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LBL 26.REMMOVED, FABRICATED AND REPLACED STIFFNER IAE DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2022013078448None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER AT STA. 1841 AND RBL 36 IS CRACKED.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR SWAA2022011359870Shield · corrodedCORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 TO BS500A RBL23. MARKED. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] LOCATED AND DRILLED NEW SHIELD BS490- BS500SDR MASA20220110020None · noneTHE FUSELAGE SKIN PANEL BETWEEN FS 897.70 AND FS 969, STR. 13L - STR. 18L WAS FOUND WITH DAMAGE DUE TO NICKS AT (31) LOCATIONS. PERFORM PERMANENTE REPAIR IAW CRJ7/9 SRM 53-51-01-001-002-A02 B) CRJ7/9 SRM 53-51-01-101-002-A04/ 53-00-01-101-001, ALLOWABLE DAMAGESDR DALA2022011100216Skin · dentedSHIP 3247 DENT EXTERNAL SKIN LOCATED AT FR 63 BTW STR 40R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED PER A320 SRM 53-41-11. OK FOR CONTINUED SERVICE. CONTINUE ON MON. (2081599)SDR DALA2022011100215Skin · dentedSHIP 3247 DENT EXTERNAL SKIN LOCATED AT FR 62 AND BTW STR 40R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: INSPECTED PER A320 SRM 53-41-11. OK FOR CONTINUED SERVICE. CONTINUE ON MON. (2081596)SDR SWAA2022022159711None · crackedCRACK SERVICE DOOR CUT OUT REVEAL LOCATED BS294.5 AND BTW STR 7R TO STR 9R AT FWD GALLEY AREA 2022-15910 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A21043164 DUE DATE: 01-SEP-22;[02] REPLACED REVEAL LOC. SERVICE DOOR CUT OUT BS294.5 AND BTW STR 7R TO STR 9RSDR REXA2022012600134Floorbeam · corroded"FLOORBEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 1000
TO FS 1031. "
"REPAIRED FLOOR BEAM AT LBL27 BETWEEN FS 1000 AND FS 1031 PIAW CRJ
900 SRM 53-00-41-201-001-A03. WVAC EMP "SDR DALA2022011100228None · nonePERMANENT REPAIR INSTRUCTIONS : GROUND DAMAGE LEFT FUSELAGE / FR30-32 STR26L - STR27L ( REFERENCE ERA 596397-14 REV. ORIG ). COMPLIED WITH SKIN REPAIR ERA 596427-14 REV. ORIG ON NR 00001 ASSOCIATED ER/A 14-596427 ADDED FOR AC 3062. (LP# 2080234)SDR IPXA2022010977679None · damagedINSPECTION TYPE:N/AFUSELAGE SKIN DAMGE FOLLOW ON ACTIONS TO ZERO TIME FASTENER HOLESACCOMPLISH FOLLOW-ON ACTIONS PER EO MD11-5330-50064-ESDR CALA2022011000088Skin · 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 SWAA2022021159612Angle · crackedCRACK ANGLE - CLIP LOCATED AFT FACE BS400 AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2022-11269 / [01] TOOL USED DIGITAL CALIPER P/N:500-196-30 S/N:A20226522 DUE DATE 11-AUG-22.; [02] REPLACED ANGLE CLIP LOCATED AFT FACE BS400 AT LEVEL STR26L FWD CARGO COMPARTMENSDR SWAA2022021159611Angle · crackedCRACK ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26R FWD CARGO COMPARTMENT ; 2022-11266 / [01] REPLACED ANGLE CLIP LOCATED FWD FACE BS500C AT LEVEL STR26R FWD CARGO I.A.W.B737-700 SRM 51-10-02 AND DWG# 143A7505 REV. ?B?. SEE INDIVIDUAL SIGN OFF BELOW; [0SDR SWAA2022021159605Angle · crackedCRACK ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2022-11268 / [01] TOOL USED DIGITAL CALIPER P/N:500-196-30 S/N:A20226522 DUE DATE: 11-AUG-22.; [02] REPLACED ANGLE CLIP LOCATED AFT FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTSDR IPXA2022013078446Intercostal · noneINSPECTION TYPE:3CMAIN CABIN FLOOR WEB/INTERCOSTAL BETWEEN STA. 1341-1364 AT RBL 46 IS BROKEN.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. AEA7204 AND SRM 51-35-01. (MINOR)SDR SWAA2022022159665Bear Strap · crackedCRACK INDICATION FOUND AROUND FASTENER LOCATED BEAR STRAP AT LEVEL FITTING-LATCH; STA 294.5 BETWEEN S-8R AND S-9R 2022-15739 / [01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22.;[02] REPAIRED BEAR STRAP BTW BSTA 277 &SDR SWAA2022021460011Track · crackedCRACK TRACK RBL 13.84 LOCATED BS 500 AT FWD CARGO COMPARTMENT ; 2021-585157 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A21147748 DUE DATE 02-OCT-22; [02] TOOL USED PN: NORTEC 600D; SN: 210138503; CAL DUE DATE: 05-MAR-22; [03] PERFORMED PERMANENT REPAIR ON TSDR SWAA2022013159340Bracket · crackedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET CRACKED BS 420 RBL 25 WL 156 LOCATED; DRILLED; APPLIED CHEMICAL CONVERSION COATING; AND APPLIED PRIMER TO NEW FCB FLOOR TO SIDEWALL SUPPORT BRACKET IAW DWG 143A1212; 143A7505; SRM 51-40-05-0G-0; AMM 51-21SDR SWAA2022013159343Bracket · crackedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET CRACKED AFT BS 500C LBL 25 WL 156 ; / [01] LOCATED AND DRILLED NEW FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET IAW SRM 51-40-05-0G-0 AND DWG 143A7505; ID:9; REV:A; OK TO INSTALL; [02] NOT ALLOSDR SWAA2022013159342Bracket · crackedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET CRACKED FWD BS 500C LBL 25 WL 156 ; / [01] NOT ALLOWABLE DAMAGE PER THE SRM; PART WILL TO BE REPLACE; [02] LOCATED AND DRILLED NEW FWD CARGO BAY COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET IAW SRM 51-40SDR SWAA2022013159341Bracket · crackedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET CRACKED BS 400 LBL 25 WL 156 ; / [01] NOT ALLOWABLE DAMAGE PER THE SRM; PART WILL TO BE REPLACE; [02] LOCATED AND DRILLED NEW FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BRACKET IAW SRM 51-40-05-0G-0 SDR DALA2022011300275None · noneDTE LOGPAGE FOR ERA 596427-14. DTE LOGPAGE FOR ERA 596427-14. ?REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEESDR DALA2022011000160None · none(LOG 2078345) DURING INSPECTION FOUND LOOSE FILLER ON FUSELAGE CUT OUT AT EXTERNAL POWER RECEPTACLE. EGPR DOUBLER ON CUT OUT AT EXTERNAL POWER RECEPTACLE WAS REPAIRED PER ETI-37-21-539 REV. 2 AND ERA 596460-14 REV. ORIGINAL.SDR MASA20220107018None · noneTHE FUSELAGE SKIN WAS FOUND TO HAVE DAMAGE TO AN EXISTING DOUBLER. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 53-51-01, FIG. 53-51-01-991-806 ITEM 1E (REV. 38 DATED 25 JUL. 2020). DEFECT LOCATION: FS 913.00 - 927.00, STGR. 26R - 26LSDR SWAA2022020859094Web · corrodedCORROSION ON FORWARD CARGO BAY SUB WEB THRESHOLD AT B.S. 440-494; R.B.L. 28. ; / [01] REMOVED CORROSION ON FWD CARGO BAY SUB WEB THRESHOLD AT BS; 440-494 RBL 28 IAW SRM 51-10-02 PARAGRAPH 15 ;EVALUATED ALL REWORKED AREAS ;THE DEPPEST AREA BS 440-494 RBL 28 ;DISDR IPXA2022012678295Intercostal · crackedINSPECTION TYPE:3CR/H A/C COMP. AT STA. 605, INTERCOSTAL IS CRACKED.REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG. ACA3804 AND SRM 51-33-01. (MINOR)SDR IPXA2022012078073Floor Panel · corrodedINSPECTION TYPE:3CFWD CABIN FLOOR PANEL WSP0786-501 HAS CORROSION BETWEEEN STA. Y=475.000-Y=503.175 AND X=-17.00-X=27.5.REMOVED AND REPLACED CORRODED FLOOR PANEL IAW SRM 53-21-10 AND 51-21-01 (MINOR).SDR MASA20220107015None · noneTHE FUSELAGE LOWER SKIN PANEL BETWEEN AT FS 364, BETWEEN STR. 26L- STR. 26 R, PERFORM PERMANENT REPAIR IAW CRJ7/9 ESTRUCTURAL REPAIR MANUAL (SRM) 53-21-01-001-006-A02, SKIN, LOWER PANEL FS 333.00 TO FS477.40- STRUCTURAL IDENTIFICATION AND ALLOWABLE DAMAGE.SDR SWAA2022013158743Intercostal · deformedSUPPLEMENTAL INFORMATION: DEFORMED INTERCOSTAL AT FWD CARGO BAY BS 500D+10 LBL 6. ; / [01] REMOVED ; LOCATED AND DRILLED NEW INTERCOSTAL AT FWD CARGO BAY BS 500D + 10; LBL 6 ;WL 158 IAW SRM 51-40-02-0G-0;SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 126; REV: A; OK SDR SWAA2022013158572Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY BULKHEAD GUSSET IS CRACKED AT BS 500D COMMON TO STR19L ; / [01] REMOVED; LOCATED AND DRILL NEW FWD CARGO BAY BULKHEAD GUSSET AT BS 500D; STR 19L IAW SRM 51-40-02-0G-0;SRM 51-40-05-0G AND DWG 143A7902;ID: 174; REV:-; OK TSDR IPXA2022020178547Skin · noneINSPECTION TYPE:3CFWD LWR CARGO DOOR HAS A DENT BETWEEN STA Y=954.8 TO 957.8 AND INTERCOSTAL PLANE C . DENT IS (3"X 2.5" X.176" DEEP)REPAIRED DENT AT THE FWD LWR CARGO DOOR BETWEEN STA Y=954.8 TO 957.8 AND INTERCOSTAL PLANE C IAW MD11 EA 011-5200-01-A9469 REF SDR V0XD20220124001Angle · corrodedPASSENGER DOOR KICK ANGLE IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED KICK ANGLE IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01SDR DALA2022011000173None · noneSHIP 6822 DENT ON FUSELAGE APPROX 2 FT FWD AND 1 FT BELOW 4R DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00202: DENT ON FUSELAGE APPROX 2 FT FWD AND 1 FT BELOW 4R DOOR WAS REPAIRED PER ETI-57-21-578 REV. 3 AND PER ER/A 596371-14 REV. ORIGINAL. (2076284)SDR DALA2022011000172None · noneSHIP 6822 CORROSION ON SIDE PANEL AT LBL 16.10 BETWEEN STA 1310-STA 1410. IN REFERENCE TO NRC 00174. CORRECTIVE ACTION: SUMMARY OF NRC 00716: SIDE PANEL AT LBL 16.10 BETWEEN STA 1310-STA 1410 WAS REPLACED PER B757-200 SRM. (2075646)SDR DALA2022010800150None · none(LOG 2076474) DURING LINE OPERATIONS A LAVATORY SERVICE TRUCK IMPACTED THE FUSELAGE SKIN AT STA 820, S22L-S23L. MAINTENANCE REPAIRED DAMAGE PER ERA 596292-14.SDR DALA2022010700134None · noneFOUND DAMAGE ON RT FWD NOSE FUSELAGE UNDER FO WINDOW. REMOVAL OF SIDE STICK ASSEMBLY IAW A321 27-92-41-000-001-A. A/W REMOVAL UP TO STEP D. (3) (GS 812718). REMOVAL OG THE OXYGEN MASK STOWAGE BOX IAW A321 AMM 35-12-41-000-001-A C/W REMOVAL UP TO STEP D. OPENINSDR DALA2022010600092None · noneFWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. REMOVED EXSITING RIVETS AND CUT OUT DAMAGE FOR REPAIR PER B717 SRM 53-20-15-2R PRC. 11. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53- 20-15-2R PROC 11 OPTION 2 AND INSTALLED CONICAL SEALS. RII COMP
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