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 DALA2025033102358Skin · damagedSHIP 6708 INITIAL AD//AA: DURING HFEC INSPECTION ELONGATE HOLE WAS FOUND ON FUSELAGE SKIN AT LOWER FWD CORNER THE CARGO # 1 DOOR CUTOUT OF: STA: 560. CORRECTIVE ACTION: SUMMARY OF NRC 00232: ELONGATE HOLE ON FUSELAGE SKIN AT LOWER FWD CORNER THE CARGO # 1 DOORSDR FDEA202503290537Skin · not reportedWHILE ACCOMPLISHING GVI OF STRINER S-14L LAP SPLICE ON EO F-5330-E0344603 P1 STEP 3.A A SKIN REPAIR DOUBLER WAS FOUND INSTALLED AT STA. 1600-STA 1620 STRINGER S-12L TO S-14L ACCOMPLISHED WITH REPAIR ON EA F-5330-T0382552 P1 FUSELAGE-PLATES & SKINS-STA1600 SDR DALA2025033102354Repair · crackedCRACKED PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH. SUMMARY OF NRC 00334: PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH, WERE REPLACED PER B717-200 SRM 5SDR DALA2025033102344Skin · cracked-AD- OPEN HOLE HFEC INSPECTION FOUND 01 EA THROUGH CRACK AT 2 O'CLOCK POSITION AT #3 FASTENER LOCATION AND FOUND 02 EA THROUGH CRACKS AT 2 O'CLOCK AND 7 O'CLOCK POSITION AT #4 FASTENER LOCATION ON BOTH FUSELAGE SKIN AND BEAR STRAP LAYERS AT THE FORWARD SERVICESDR DALA2025033102343Skin · cracked-AD- OPEN HOLE HFEC INSPECTION FOUND 01 EA THROUGH CRACK AT 10 O'CLOCK POSITION AT #3 FASTENER LOCATION AND 01 EA THROUGH CRACK AT 4 O'CLOCK AT #4 FASTENER LOCATION ON THE FUSELAGE SKIN LAYER ONLY AT THE FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AS MARK. (LOOSDR AALA202508012249Skin Panel · not reportedAIRCRAFT IN BASE MAINTENANCE: TEMPORARY REPAIR LOC BTW FR12 TO FR16 RH SIDE ON UPPER FUSELAGE.MEASURED EXISTING CUT OUT L=6.100IN AND W=5.500IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOCATED ON FUSELAGE RH SIDE FR 12-16 FWD SKIN PANEL/ DOOR SURROUND PANEL SDR VNAA20250525014Skin · dentedDENTS (6EAS) ON FUSELAGE SKIN LOCATED BTW FS349/ FS421 AND STGR18R / STGR19R. PREVIOUS BLEND OUT ON AREA (1 EA) BTW FS 364 TO FS349 STGR 18R TO STGR 19R AND AREAS (3 EAS) BTW FS379 TO FS 394 STGR18R TO STGR 19R WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53SDR VNAA20250525012Skin · wornPROTUBERANCE ON FUSELAGE SKIN LOCATED BTW FS1000 / FS1015 AND STGR1R / STGR2R. PROTUBERANCE ON FUSELAGE SKIN LOCATED BTW FS1000 / FS1015 AND STGR1R / STGR2R WAS REPAIRED PER REO 670-51-00-085 REV - A AND PER REO 670-53-61-2496 REV. - .SDR JJBA20250408039Skin · crackedRF2, RH EXTERNAL SKIN, CRACK SUSPECTED BTW FR 77-78 AND BTW STR 5R-8R. REPAIR DOUBLER ON RH REAR FUSE II SKIN, AT FR78 BTW STR 5R-7R CARRIED OUT.SDR CALA2025040103394Skin · crackedINSTALL REPAIR PARTS REF AVO 14374 REV A THIS IS A STEP IN A MAJOR REPAIR, REQUIRES INSPECTION, RII INSTALLED REPAIR PER AVO14374 WITH NO DEVIATIONS TO AVO. REPAIR WAS INSTALLED USING AVO14374 REV C. ACCOMPLISHED RII REQUIREMENTS FOR FUSELAGE REPAIR IN REF TOSDR DALA2025040102439Repair · unknownSHIP 6708 REPAIR TO FUSELAGE SKIN AT C1 DOOR CUTOUT LOWER FWD & AFT CORNERS. FUSELAGE / SKIN / FWD CC DOOR NO. 1 CUTOUT / LOWER FWD & AFT CORNERS / BTW BSTA 560 & 620 AND BTW S-25R & S-26R / ELONGATED HOLES IS PENDING DTE STAGE III APPROVAL PRIOR TO 33,000 TOTSDR DALA2025033102352Skin · crackedCRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00035: CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 624820-14 REV 3 AND ER/A 624820-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GVI EVERY 24 MONTSDR DALA2025033102350Skin · crackedCRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L. SUMMARY OF NRC 00444: CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L WAS REPAIRED PER PRI 625028-14 REV 1 AND ER/A 625028-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GENERAL VISSDR FDEA202503280530Skin · corroded(DOT 38-24) RH LOWER FUSELAGE SKIN CORRODED STA 1788 APPROX 4" AREA, 3" ABOVE THE APU RH DOOR CUTOUT. COMPLIED WITH REPAIR ON EA F-5330-T0382463 P1 FUSELAGE-PLATES & SKINS-SKIN REPAIRS AT STA 1885 RHS AND STRINGER S-17R FOR CORROSION MAJOR REPAIRSDR DALA2025032802308Skin · damagedSHIP 3360 FOUND TWO FASTENERS HOLE OVERSIZED AT FR 49 AND FR 50; BETWEEN STR 25R AND STR 26R. CORRECTIVE ACTION: REPAIRED TWO OVERSIZED FASTENER HOLES IN THE FRAME AT FR49 AND FR50, BETWEEN STGR25 RH AND STGR26 RH PER ER/A 625272-14 REV ORIGINAL (0881713)SDR HNAA2025041700211Doubler · corroded53-2207 RH LATERAL DOUBLER PARTITION CORRODED AT FR61. RAR PARTITION IAW SRM 51-40-02SDR JJBA20250404036Skin · crackedRF2, LH EXTERNAL SKIN, SEVERAL CRACKS SUSPECTED AT FR 77, 78, 79, 80 AND BTW STR 3L-7L. 2 REPAIR DOUBLER ON LH REAR FUSE II SKIN. DOUBLER #1 IS LOCATED AT FR77 BTW STR 3L-5L. DOUBLER #2 IS LOCATED AT FR 78 BTW STR 5L-7LSDR DALA2025033102348Skin · dentedPERFORM REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP. SUMMARY OF NRC 00637: SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP WAS REPAIRED PER ER/A 624583-14AD REV ORIGINAL SECTSDR DALA2025032802309Skin · chafedSHIP 3360 DURING HCK AT STAG (CAN), CHAFING WAS FOUND ON THE FUSELAGE SKIN FROM FR 54 TO FR 55, STR 47R TO STR 50R COMMON TO THE 198GB WIN GTO BODY FAIRING. CORRECTIVE ACTION: COMPLIED WITH ERA 624941-33. (0880885)SDR CALA2025032803292Skin Panel · crackedIT WAS FOUND CRACK IN OPEN HOLE, AT AFT LOWER CORNER FUSELAGE SKIN, FWD SERVICE DOOR,DURING INSPECTION ROTARY SCANNER PER 767 NDT MANUAL PART 6, 51-00-16. IT WAS PERFORMED PERMANENT REPAIR AS PER SRM 53-10-01-2R-1, DETAIL III, FIGURE 201. THIS IS A CATEGORY BSDR WRXR20250327001Skin · gougedGOUGES FOUND IN METAL NUTPLATE BRACKET AND STRUCTURE AT MID CARGO DOOR SURROUND AT F.S. 661.00+5.00 AND 661.00+8.00. REMOVED GOUGE FROM STRUCTURE AT MID CARGO DOOR SURROUND FS 661.00+8.00. NDT EVALUATE BLENDED AREA ON STRUCTURE AT MID CARGO DOOR SURROUND AT SDR DALA2025100207189Skin · corrodedCORROSION INTERNAL SKIN LOCATED AT LEVEL FR20 AND BETWEEN STR28L TO STR29L IN LATERAL AVIONIC COMP LH. REPAIRED PER ER/A 624546-14. (0879376)SDR DALA2025100207188Skin · corrodedCORROSION INTERNAL SKIN LOCATED AT LEVEL FR16 AND BETWEEN STR28L TO STR29L IN LATERAL AVIONIC COMP LH. REPAIRED PER ER/A 624546-14. (0879365)SDR FDEA202503260555Skin · corrodedLH FWD FUSELAGE TOILET SERVICE PANEL CUTOUT SKIN STIFFENER CORRODED. REPLACED THE HEAVY CORRODED STIFFENER (SKIN) ON LH FWD FUSELAGE TOILET SERVICE PANEL CUTOUT PER A300-600F SRM 51-40-21. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR DALA2025032702276Skin · chafedSHIP 3141 CHAFING MARKS ON EXTERNAL FUSELAGE SKIN PANEL AT FR34 BTW STR 43 LH AND 43 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 624730-14AD. (0879393)SDR SWI2025F01260Skin · corrodedCORROSION ON INNER SKIN BETWEEN FS847.00 +16.00 AND FS 847 +32.00 AND BETWEEN STGR26R AND STGR26L. (MARKED). (C-CHECK RO 09/07/2025)COMPLIED WITH ALL THE STEPS OF REO 690-53-51-452 REV-- DATED 2025-04-02. ENSURED BLEND OUT ON INNER SKIN (DOUBLER) BETWEEN FS8SDR HNAA2025042800234Skin · dented53-2092 SKIN DENT AT FR19-20 BTW STR20-21R. REPAIRED SKIN IAW SRM 53-21-01 AND EO 1-53-25-0134SDR IPXA202504220161Skin · crackedDURING PERFORM T/C NO. EO-24301-JIC001 FOUND SKIN CRACK. (REPAIR). .REPAIR DAMAGE AREA I.A.W SRM 53-80-01-2R-5 REV.91 AND EGAT WORK SHEET NO. 50216 AND UPS EO-24301-JIC003 REV4 (T3F18E006BF6P) AND EO-24301-REQ 002 (T3F18E006BF6N). JOB COMPLETED.SDR SWI2025F00450Skin · corrodedAFT FUSELAGE BETWEEN FR 88 AND FR 89 STGR 28R RIVETS CORRODED AROUND WASTE BOX FWD I/B CORNER (C-CHECK RO 4/11/2025) REMOVED AND REPLACED 13EA.RIVETS ON AFT FUSELAGE BETWEEN FR 88 AND FR 89 STGR 28R AROUND WASTE BOX FWD I/B CORNER REF. EMB SRM 51-40-08SDR SCNA20250415115Skin · gougedAFT CARGO DOOR CUTOUT HAS GOUGE ON EXTERNAL PLATING UPPER AFT CORNER MARKED. UPON FURTHER EVAULATION DEFECT WAS CONTAINED WITHIN PAINT AND PRIMER AND DID NOT PENERATRATE INTO THE FUSELAGE SKIN IAW ESR RESPONSE 25-10536 RESTORED EXTERIOR FINISH AT AFT UPPER COSDR R61A2025041400179Doubler · corrodedCENTER FUSELAGE 3 INTERMAL, FOUND CORRODED FLOOR DOUBLER ON FR 84 RML 12. MX REPLACED DOUBLER PN 170-92856-001 IAW SRM 52-42-04.SDR JJBA20250403014Skin · dentedFF2 LH LOWER SKIN DENT FOUND UPPER EXTERNAL POWER RECEPTACLE. ON FF2 LH LOWER SKIN UNDER EXTERNAL RECEPTACLE PAIN STRIPPED. FF2 LH LOWER SKIN UNDER EXTERNAL POWER RECEPTACLE REPAIRED.SDR DALA2025032702275Skin · corrodedSHIP 3141 CORROSION FOUND ON INTERNAL SURFACE OF FUSELAGE SKIN PANEL BETWEEN FR15-FR21 AT LATERAL STR ON THE LHS. CORRECTIVE ACTION: REPAIRED PER ER/A 624546-14. (0876789)SDR DALA2025032702274Skin · corrodedSHIP 3141 DURING M2 AND WHILE INSPECTING PER 5320-3013, CORROSION FOUND ON INTERNAL SURFACE OF FUSELAGE SKIN PANEL BETWEEN FR15-FR21 AT LATERAL STR ON THE LHS. CORRECTIVE ACTION: COMPLIED WITH ER/A 624546-14. (0876782)SDR VNAA2025032711102Skin · dentedFOUND DENT ON RH SIDE AFT OF RVSM AREA. DENT MEASURES FS 202.75-FS220 STGR 12A-STGR13A - 0.2 INCHES FWD OF FASTENER LINE AND 0.2 INCHES UNDER FASTENER LINE 1.3 INCHES WIDE AND 1.3 INCHES LONG. HAS A DEPTH OF .13 INCHES. / PERFORMED PERMANENT REPAIR ON RIGHT HASDR CALA2025032703253Skin · damagedL1 DOOR CUTOUT MOD. THERE ARE DISCREPANCIES BETWEEN THE INSTALLATION DRAWING AND ACTUAL FASTENER LOCATIONS FOUND DURING LAYOUT OF DOUBLER AND TRIPLER. L1 DOOR SURROUND - REPAIR / PREVENTATIVE MODIFICATION PER EA 5330-04213 AND ECRA 5330-07490 VERIFIED L1 DOOR SDR R61A2025032600160Skin · damagedLIGHTING STRIKE DAMAGE WITH CUTOUT FWD OF FR 24 AT STR 22L & FWD FR 25-26 AT STR 22L-21L. REPAIRED IAW SRM 51-23-01.SDR IPXA2025032554643Skin · chafedFUSELAGE SKIN UNDER RIGHT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. [SDR JR2R20250325827Skin · dentedFORWARD FUSELAGE, NOSE SKIN IS DENTED OUT OF LIMITS BETWEEN STRINGERS 2R AND 4R AND FRAMES 3 AND 4.SDR DALA2025040202492Skin · damaged(LOG 6521776) DURING WALK AROUND FOUND SKIN DAMAGE CORROSION AT VACUUM WASTE CUTOUT 6 O'CLOCK POSITION. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN AT STA 917 BETWEEN STR 21L & STR 22L AROUND LAV DUCT VENT NOZZLE ASSY PER DELTA ER/A 625307-14 AND B737-800 SSDR DALA2025032702261Skin · damagedSHIP 1018 DAMAGE BETWEEN FR 23 AND FR 24 BETWEEN STR 35L,36L .09375 INCH DIAMETER RIVET AND SKIN DAMAGE. CORRECTIVE ACTION: REPAIRED DAMAGE. REF A321 SRM 53-11-11. (0875575)SDR UIEA2025030600220Skin · crackedFWD ENTRY DOOR, AFT LOWER CORNER, HOLE 4 WITH CRACK INDICATION ON BEAR STRAP APPROX 10 O'CLOCK, AND HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 10 O'CLOCK, 4 AND 11 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 & SRM 51SDR UIEA2025030600221Skin · crackedSERVICE DOOR, AFT LOWER CORNER, HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 2 AND 8 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 & SRM 51-40-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030800239Skin · corrodedUPPER FUSELAGE SURFACE WITH CORROSION AT THE BASE OF THE TOP TCAS ANNTENA.(<P>UPPER FUSELAGE SURFACE CORROSION AT THE BASE OF THE TOP TCAS ANNTENA. REPAIR WAS PERFORMED IN ACCORDANCE WITH TRE6753716 FEB 24, 2025. FVC TITLE REPAIR- FUSELAGE SKIN- CROWN AREA-CORSDR UIEA2025030800245Skin · dentedLOWER HALF OF FUSELAGE, BTW STA 654+44 AND 654+66, BTW STR 34L AND 33L, DENT ON SKIN.(<P>THE DENT WAS EVALUATED AND FOUND OUT OF LIMIT. IT WAS REPAIRED IAW SRM 53-00-01-2R-29 REPAIR 29. NO FURTHER DEFECTS NOTED.</P>)SDR CALA2025032603217Skin · stainedFWD CARGO PIT L/H SIDE FROM STA 640 TO STA 845 AND FROM S-28L TO S-21L FUSELAGE SKIN CONTAMINATED BY BLUE WATER. CLEANED FWD CARGO PIT L/H SIDE FROM STA 640 TO STA 845 AND FROM S-28L TO S-21L IAW ECRA 2011-01000 REV AD.SDR DALA2025032502216Skin · corrodedFOUND BULGE ON SKIN AT STA 420 13L TO 14L. CORRECTIVE ACTION:THE EVALUATION OF BULGE AT ST 420 STR 13L TO 14L FOUD IT TO BE OUT OF LIMITS IAW B757-200 SRM 53-00-01 DETAIL III. DAMAGE WAS REMOVED AND REPAIRED IAW ER/A 625043-14.SDR DALA2025032702259Skin · chafedSHIP 6805 DTE, ERA 625043-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN AT STA 420-440 & S-14/15L. CORRECTIVE ACTION: REF ERA 625043-14. (0873043)SDR CALA2025032703252Skin · corrodedAFT CARGO LH FR58, STRG 43L HAS CORROSION. BLENDED CORROSION ON FR58, STRG 43L. DETERMINED TO BE OUT OF LIM ITS IAW SRM 53-41-13-283-002, FIG 1, SHEET 1. MAX REWORK DEPTH B EYOND 10 PERCENT OF NOMINAL THICKNESS. FLOW CHART TAKES YOU TO S RM 53-41-13 BUT FR58 NSDR SWIA20250326003Skin · dentedFUSELAGE SKIN HAS TWO SMALL DENTS LOCATED BETWEEN FS654.50 & FS672.00 AND STGR'S 0 & 1L. (C-CHECK RO 03/25/2024)COMPLIED WITH TEMPORARY DISPOSITION FOR DENTS TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.00 AND STR 0 - STR 1L WITH REFERENCE TO REO 601R-53-61-8308
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