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 VNAA202402010002Skin · dentedWHILE PERFORMING EXTERIOR PAINT INSPECTION FOUND LARGE DENT ON EXTERIOR OF AC AT L/H FS 202 JUST UNDER THE PITOT TUBE . REMOVED DAMAGED LH NOSE SKIN PANEL PN: CC670-33105-1 IAW CRJ-900 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE LH NOSE SKIN PANEL PNSDR SWIA2024032500131Landing · crackedTRU PANEL 212AR LOWER LANDING ANGLE ON FUSELAGE HAS POSSIBLE CRACK AT THE AFT LATCH CUT OUT RADIUS (MARKED) (C-CHECK RO 3/23/2024) INSTALLED NEW LANDING ANGLE CC670-33151-6 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING CC670-33040 REV G AND REO 670-53-SDR AALA202402051082Skin · crackedAIRCRAFT IN BASE MAINTENANCE CRACK IN FUSELAGE SKIN NEAR VACUUM BLOWER EXHAUST AT BS 1967, BETWEEN S35L AND S36L. REPAIRED SKIN PER 53-70-01-2R PROCEDURE 1.SDR A6WA202401318710Skin · dentedEXTERNAL SKIN ON FUSELAGE HAS 3 DENTS WITH CREASE AT FS 589 TO FS621 BETWEEN STRG21R AND STRG22R. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REPAIRED FWD AND AFT FUSELAGE SKIN AT FS 589.00 STR17R REF REO 601R-53-61-8146 REV -- DATED 2024-01-25.SDR A6WA202401318709Skin · dentedREF WO 332477 MXWC #4 DAMAGE TO FUSELAGE AT FS587 BETWEEN STR17R-STR18R DENT MEASURES 3" X 3.2" X .045 DEPTH. DAMAGE TO UNDERLYING FRAME SECTOR AT FS589 AND STRINGER 17R ALSO NOTED. TROUBLE SHOOT AND REPAIR AS REQUIRED. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. SDR CALA2024020200297Skin · crackedEA 5315-01152 SEQ 1331, R1 DOOR CUTOUT FUSELAGE SKIN AFT LOWER CORNER STA 335 JUST ABOVE STRINGER 20R LOWER HOLE HAS CRACK INDICATIONS IN BOTH THE SKIN AND BEAR STRAP WHILE PERFORMING HFEC SCAN.SDR CALA2024020200296Skin · crackedEA 5315-01152 L1 DOOR LOWER AFTER CORNER FUSELAGE SKIN ONLY AT STA 335 JUST ABOVE STRINGER 20L LOWER FASTENER HOLE HAS A CRACK INDICATION WHILE PERFORMING HFEC OPEN HOLE SCAN.SDR DALA2024020101460Skin · handler error(LOG 5034554) GROUND SERVICE CATERING TRUCK IMPACTED AIRCRAFT BELOW FORWARD SERVICE DOOR. C/W ERA 615488-14 AND BLENDED GOUGES PER B737 SRM 51-10.SDR SWIA202403250259Landing · crackedTRU PANEL 211AL LOWER LANDING ANGLE ON FUSELAGE HAS POSSIBLE CRACK AT THE AFT LATCH CUT OUT RADIUS (MARKED) (C-CHECK RO 3/23/2024) PERFORMED DVI ON UPPER ELECTRICAL LH ACCESS LOWER LANDING ANGLE AT AFT LATCH CUT OUT RADIUS, IT WAS FOUND A VISIBLE CRACK OFSDR SWIA202403250258Skin · crackedPOSSIBLE CRACK ON THE RH SIDE OF THE FUSELAGE SKIN AT TRU PANEL 212AR LOWER AFT CORNER AREA (MARKED) (C-CHECK RO 3/23/2024) ON THE RH SIDE OF THE FUSELAGE SKIN AT TRU PANEL CRACK LENGTH = 0.250", CRACK LENGTH PERMITTED = 0.5D = 0.081" (WHERE D IS THE NEARESDR SWIA202403250257Skin · crackedPOSSIBLE CRACK ON THE LH SIDE OF THE FUSELAGE SKIN AT TRU PANEL 211AL LOWER AFT CORNER AREA (MARKED) (C-CHECK RO 3/23/2024) INSTALLED NEW SKIN PANEL ON AIRCRAFT FROM FS169 TO FS202, BETWEEN STGR 24L TO STGR 16L PER REF CRJ 700 SRM 51-42-06-001-001-A01, CRSDR FDEA202401300354Skin · cracked1EA CRACK INDICATION WAS FOUND AT R/H FR54, STR44 FASENTER HOLE. ACCOMPLISHED THE TRIM-OUT REPAIR AND REINFORCED WITH SHIM & EXTERNAL DOUBLER AT FR54 S-44R, THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5330- T0378095 P1, SEQ NO:974, TITLSDR SWAA2024030446406Skin · debondedPANEL 192AR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 192AR OUTER SKIN DISBOND WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] JOB COMPLETE.SDR SWAA2024022646581Skin · crackedFED FWD SIDE FRAME SKIN HAS CRACK COMMON TO THE 7TH STOP FITTING. (MARKED) FED AFT SIDE FRAME SKIN HAS CRACK COMMON TO THE 7TH STOP FITTING.<[01] COMPLETED STEP 1.<BR>TASK COMPLETED ON ATS COMPONENTS WORK ORDER; RO NUMBER P8012885-1;[02] VERIFIED CORRECTIVE ACSDR SIMA20240130002Skin · corrodedCORROSION FOUND ON AFT FUSELAGE SKIN AROUND AFT LAVATORY SERVICE BUCKET EXTERIOR AREA (LEVEL 2 CORROSION). PERFORMED PERMANENT REPAIR TO AFT FUSELAGE SKIN AROUND AFT LAVATORY SERVICE BUCKET IAW EMB 175 SRM 53-23-60/REPAIR 01P.SDR IPXA2024020284515Skin Panel · dentedMAJOR REPAIR, DENT, FUSELAGE SKIN BETWEEN STA 360 - STA 384, S-16L - S-17L (REPAIR). ACCOMPLISHED REPAIR IAW SRM 53-00-01-2R-12 REV.88 AND EO-89370-REQ 1 REV. 1. JOB COMPLISHED. REVIEW COMPLETESDR CALA2024013000258Skin · dentedDIP DENT AFT OF POTABLE WATER DOOR. ACCOMPLISHED PERMENANT REPAIR ON DENT AFT OF POTABLE WATER DOOR (12.375" AFT OF AFT SIDE) IAW A320 SRM 53-41-11-283-059 AND 53-4 1-11-300-093 REPAIR LOCATED AT FR 66-67 STR 39L-40LSDR DALA2024013001346Skin · damagedSHIP 3159 FOUR (4) ELONGATED HOLES LOCATED AT FR59 AND STR 2-3R. CORRECTIVE ACTION: REPAIRED PER ERA 605637-14. (0178041)SDR ASAA2024012849590Skin · corrodedFUSELAGE SKIN EXTERIOR BETWEEN STR 1L AND 1R, UNDER ADF2 ANTENNA CUTOUT HAS CORROSION AROUND FASTENER HOLE (2EA) AS MARKED. (DOT ATTACHED UNDER TAPE) GROUNDED - YES. BLENDED DAMAGED AREAS, 1) L=1.30", WIDTH=.800", ORIGINAL THICKNESS IS .087" REMAINING=.078", RSDR CALA2024020200281Skin · dentedPERFORMED PERMANENT REPAIR AT UPPER FUSELAGE SKIN STA 360 BTW STR 8L AND 7L.PER LP#8612412( REF AAR NR 99998516) SFR #1034970 REMOVED DAMAGE DENT AND PERFORMED PERMANENT REPAIR AND 51-21-73-370-801 UPPER FUSELAGE SKIN STA 360 BTW STR 8L AND STR 7L. IAW A-30 SRSDR DALA2024020101442Skin · crackedCRACK AT FWD UPPER CORNER OF R1 DOOR ON FUSELAGE SKIN. REMOVED PAINT AND FASTENER FOR FURTHER EVALUATION PER B717 SRM 51-22-01 AND SRM 51-40-02-06. VERIFIED CRACK PER BHEC AND HFEC INSPECTION, NDTSPM PART 06-10-01.003 AND PART 06-10-01.001. TWO CRACKS MARKED ASDR DALA2024013001396Skin · damagedSHIP 665 LIGHTNING STRIKE ON FUSELAGE SKIN AT STA 756 BETWEEN STR 28R AND 29R CORRECTIVE ACTION: REPAIRED LIGHTNING STRIKE DAMAGE PER B757 SRM 53-00-01 (0175584)SDR DALA2024012901337Skin · damagedSHIP 665 LIGHTNING STRIKE ON FUSELAGE SKIN AT STA 717 BETWEEN STR 28R AND 29R. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 004-0001:0514-2001/006 00006 REPAIRED LIGHTNING STRIKE DAMAGE PER B757SRM 53-00-01-2R PROCEDURE 28. (0175598)SDR DALA2024012901229Doubler · corrodedCORROSION ON DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT. SUMMARY OF NRC 00535: CORROSION LEVEL 2. DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 FIG 201 AND 51-41-05-0G. SDR FDEA202401270177Skin · damagedFOUND LIGHTNING STRIKE TRACE AT FR28 PLUS 7", S-46L ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600F SRM 53-10-12-201, PARA.11, PAGE.279-288, FIG.208 (SHEET-2) & SRI:53-10-12-201, IIR:53-10-12-2-002-00, PARA.3B, TABLE.205. MAJOR REPAIR.SDR NACA2024013170001Skin · crackedCRACK INDICATIONS AT STR 10R BS 827+6 5/8 INCHES LONG, AND BS 827+10 11/16, 1/2 INCHES LONG. REPAIRED PER BOEING SB 737-53A-1234SDR DALA2024012901222Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN. SUMMARY OF NRC 00395: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN WAS REPLACED PER B717 SRM 5SDR 2024FA0000077Skin · corrodedREPAIR OF UPPER FUSELAGE SKIN CORROSION. REPORT NO. ERO-978708 DATED JAN. 27, 2024 WITH FAA FORM 8110-3.SDR 2024FA0000178Stiffener · crackedAFT FUSELAGE LOWER SKIN STIFFENER FOUND CRACKED. REPLACED WITH NEW STIFFENER.SDR CALA2024013100267Skin · crackedRAMP REPORTED LARGE PUNCTURE ON LEFT FUSELAGE BY JETWAY DOOR AREA. DENT DIMENSIONS: LENGTH(2.5"), HEIGHT(2") AND DEPTH(1/4"). LOCKED FOR MX FERRY ACCOMPLISHED VISUAL INSPECTION OF STRUCTURE INSIDE AND AROUND DAMAGE IS APPROXIMATELY AT STA 448 AND STRINGER 1SDR SWIA2024032600125Skin · damagedEXTERNAL SKIN DAMAGED ALONG THE EDGE OF NOSE LANDING GEAR BOX CUT OUT, LEFT SIDE APPX. FS210.00. (C-CHECK RO 3/23/2024) BLENDED OUT EXTERNAL SKIN DAMAGE ALONG THE EDGE OF NOSE LANDING GEAR BOX CUT OUT, LEFT SIDE APPX. FS210.00. REF: CRJ-700 SRM 51-12-00-001-SDR ASAA2024012547557Skin · gougedDURING RIG OF L1 DOOR FOUND DAMAGE TO FWD DOOR SURROUND SKIN PANEL. GROUNDED - YES. ACCOMPLISHED FABRICATION OF NEW SKIN PANEL PER BOEING DWG 141A3112 SHEET 7. REPAIR ACCOMPLISHED ON MIG-5 300010924 CLOSED MIG 5 SERIES 300010925.SDR R612024F00001Skin Panel · dented"3 DENTS ON EXTERNAL FUSELAGE, FR 19-20, STGR 24L-25L. EVALUATED 2 EA DENTS (IDENTIFIED AS DENT# 1 AND 3) ARE FOUND TO BE ACCEPTABLE. PERFORMED REPAIR ON DENT# 2 BY CUTTING OUT DAMAGE AND INSTALLING REPAIR DOUBLER. REF EMB ETD2024-170-001185 REV B."SDR DALA2024012501109Finger Doubler · corrodedCORROSION ON FINGER DOUBLER STA 944, 972, 1001, AND 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00194: CORROSION LEVEL 2. FINGER DOUBLER BTW STA 944 AND STA 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-SDR ASAA2024012448262Skin · corrodedAFT AVIONICS BAY AT SKIN AIR INLET VALVE LOCATION, INTERNAL DOUBLER AROUND CUTOUT CORRODED. GROUNDED - YES. NO ALLOWABLE DAMAGE FOR AREA. CORROSION LOCATION ON FLANGE AT 2 LOWER FORWARD HOLE LOCATIONS 3.5"L X .5"W. LOCATED, DRILLED AND DEBURRED P/N D5311362220SDR SWAA2024022244598Bear Strap · crackedCRACK ON BEAR STRAP LOCATED BTW BS291.5 TO BS294.5 STR8R AND STR9R PASSENGER CABIN 2024-68196<[01] TOOL USED STEP 3: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24 AND DIGITAL CALIPER; P/N: 500-197-30; S/N: A21147758; DUE SDR SWAA2024022044355Doubler · crackedFAULT CREATED TO CAPTURE RII ITEMS ON EXTERNAL GROUND POWER RECEPTACLE DOOR SURROUND DOUBLER BENT AND CRACKED AT LOWER TAB [TTG8Q00QTQ6A]<[01] FABRICATED AND INSTALLED REPAIR IA B737-800 SRM 53-10-15-2R-4;[02] VERIFIED REPAIR PER REF.;[03] COMPLIED WITH C/W EASDR DAL2024F00000Skin · dentedSHIP 671 FUSELAGE / SKIN / DENT / BS 1720, S28L. CORRECTIVE ACTION: REF ERA 501946-14. (0169641)SDR DALA2024012501131Skin · corrodedSHIP 3234 DISC: CORROSION EXTERNAL SKIN DRAIN VALVE LOC. FR 69 TO FR 70 AT LEVEL STR 31 TO STR 32 R/H AT LOWER FUSELAGE. C/A: PERFORMED REPAIR LOC. FR 69 TO FR 70 AT LEVEL STR 31 TO STR 32 R /H AT LOWER FUSELAGE AS PER A320 SRM 53-41-11-300-004 STEP 2FIGURE 00SDR FDEA202401240105Skin · dentedDENT FOUND AT FUSELAGE SKIN BTW STA 480-500, STR 22-R TO 23R. EVALUATED DENT ON FUSELAGE SKIN BETWEEN STA 480-500, STR 22R TO 23R FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-01-1A, FIG 101 DETIAL III, CUT DAMAGED AREA IAW B757 SRM 53-00- 01-2R PAR 4 D, PERSDR DALA2024012401100Skin · damagedCREASES WERE FOUND ON REPAIR SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH PER B717 SRM 53-00-01-02 REPAIR 6 PAR. 7. SUMMARY OF NRC 00270: SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH WAS REPAIRED PER B717-200 SRM 53-00-01-2R REP 6. SPECIFICSDR VNAA202402290028Skin · crackedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 18 RH TO 19 RH AND AT FS629. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 18 RH TO 19 RH AND AT FS629 WAS REPAIRED PER REO 690-53-31-816 REV - -SDR UATA202402023312Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.070" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, HE SITUATION REPORTED, AND A REPAIR SCHEME REQUESTSDR DALA2024012501122Doubler · corroded(LOG 0168410) CORROSION AT FWD CARGO BAY LOWER ANTENNA BLACKOUT DOUBLER STA 500C TO 500D BL0. REMOVED AND REPLACED DAMAGED SKIN DOUBLER LOCATED AT FWD CARGO COMPARTMENT LOWER INNER SIDE OF SKIN FUSELAGE BETWEEN BS 500C TO BS 500D BL0 I.A.W B737-900 S.R.M 51-40SDR DALA2024012401098Skin · damagedAIRCRAFT 1028, GSE RAILING CONTACTED AIRCRAFT SKIN JUST AFT OF THS DOOR. CORRECTIVE ACTION: CRACK .25" LONG IN A 1" DENT FOUND AT FRAME 73/74 AT STR 28/29L. REMOVED DAMAGE AND INSTALLED A DOUBLER PER A321-200 SRM 53-00-11-300-029. FIG 001. PAGE 9. DEFERRED TO SDR FDEA202401230102Skin · gougedMAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 497 1 1/8" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND IN LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINATINSDR FDEA202401230101Skin · gougedMAIN CARGO DOOR LOWER EXTERIOR SKIN APROX. STA/ 482-500 SKIN HAS GOUGE. EVALUATED AND REWORKED MCD LOWER EXTERIOR SKIN AT STA 490 0.787" BELOW S-10 IAW B757-200 SRM 52-30-01-1A FIG 101 SHEET 1 TO 5 FOUND OUT OF LIMIT. SEE EA F-5330-T0377806 A P1 FOR TERMINSDR DALA2024012301009Skin · gougedGOUGE AND DENT ON FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L. SUMMARY OF NRC 00615: FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L WAS PERMANENT REPAIRED PER B717-200 SRM 53-02-01-2R-1 FIG 202. THE PERMANENT REPAIR SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSSDR VNAA202402290026Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 16 LH TO 17 LH AND BTW FS 501 TO FS 517. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 16 LH TO 17 LH AND BTW FS 501 TO FS 517 WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03SDR VNAA202402290024Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 14 RH AT FS 379. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 14 RH AT FS 379 WAS REPAIRED PER REO 690-53-21-1726 REV. - -
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