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 REXA2025041700440Skin · corrodedFOUND CORROSION ON INNER SKIN AROUND WHAT APPEARS TO BE A SKIN PLUG RIVET AT APPROXIMATELY F.S. 286 BETWEEN STGR 26R AND STGR 25R. RECEIVED AND COMPLIED ALL STEPS OF OF ENDEAVOR AIR EA NO: CRJ753-18599 REV. IR DATED 3/11/2025.SDR SWI2025F00432Skin · gougedGOUGE FOUND ON PAX DOOR SURROUND, FWD LOWER CORNER. (C-CHECK RO 04/04/2025)COMPLIED WITH REO 670-53-21-2589 REV -- DATED 2025-03-12 STEP 1 TO 3. ON FWD LOWER CORNER. ENSURED BLEND OUT HAS SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVAL, ENSURED MINIMUM REMAINISDR R61A2025031300137Skin · damagedWHILE IN HEAVY CHECK - CREASE - EXTERNAL SKIN BETWEEN FR76/77 AND STR24R/25R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER REPAIR AT EXTERNAL SKIN BETWEEN FR76/77 AND STR24R/25R IAW ETD2025-170-902714.SDR ASAA2025021956236Skin Panel · corrodedCORROSION ON FUSELAGE SKIN STA 500I AND SAT 500H AT STGR 14R LAP SEAM SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON SKIN PANEL P/N 143A3252 AT STA 500I AND STA 500H STGR 14R IAW EA 800-53EA-28266 REV 00 SRXR430X.SDR CALA2025022600445Skin · gouged(B757-53-4-1480) MAIN CABIN INTERNAL SURFACE OF THE FUSELAGE SKIN IS GOUGED AT THE CHEM MILL STEP UNDER THE PENETRATION DOUBLER ON THE AFT SIDE OF STA 727E BETWEEN S2R AND S3R. TRANSCRIBED FROM HAECO GSO NRC 9288543 FABRICATED AND INSTALLED REPAIR ER EC/RA 536SDR SIMA20250218002Skin · dentedFOUND 2 PROTRUSIONS LOCATED BETWEEN FR29 AND FR30 AND STGR 24R AND 25R. (MAJOR REPAIR) REPAIRED SKIN BETWEEN FR29-30, STGR 24R-25R IAW ERS-EJ-53MR-5153.SDR SWIA202503110218Skin · damagedFASTNER BETWEEN FS517 - FS533 ON STRINGER 27 HAS LIGHTNING DAMAGE THAT IS BEYOND SRM 53-00-00 LIMITS (MARKED WITH TAPE AND STREAMER) (FILED CLOSED) REPAIR WAS DETERMINED TO BE A MAJOR REPAIR REF CP29667504-1 FOR DETERMINATION. REF CP2970039-1 FOR COMPLISDR IPXA2025022200461Skin Panel · dentedDENT - SKIN, L/H FORWARD LOWER FUSELAGE, NEAR CREW ENTRY DOOR, STA 315, S-30L~S-31L. (REPAIR). ENSURE ALL DATA REQUIRED IN GMM-MTX 03.43.01.04 HAS BEEN CORRECTLY DOCUMENTED. A. ORIGINAL SKIN (P/N:141T3231-7) MADE FROM 2024-T3 CLAD REPAIR AREA THICKNESS 0.07SDR DALA2025022001336Skin · damaged(LOG 0817841) FUSELAGE / SKIN PANEL / BTW BSTA 177 & BSTA 188 / BL 0 & RBL 10 / BURN MARK. REPAIRED DAMAGE PER ERA 624312-14.SDR DALA2025021901240Skin · wornSHIP 3361 BELLY FAIRING 198GB AND FUSELAGE TOUCH SURFACE FOUND WORN. CORRECTIVE ACTION: COMPLIED WITH PRI 623760-14. (0816963)SDR N6WA2025021802Doubler · corrodedCORROSION ON TCAS DOUBLER BETWEEN FS295 TO FS310. REMOVED AND REPLACED TCAS DOUBLER BETWEEN FS295 TO FS310 IAW CRJ SRM 51-42-06.SDR SWAA2025031997078Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED <[01]. FWD CARGO BAY FWD CORNER SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1.SDR ASAA2025021756548Skin · dentedBS.727F+12 STR.7L TO STR. 8L EXTERIOR SKIN HAS DENT. GROUNDED - YES. EVALUATED DENT IAW B737-900 SRM 53-00-01 FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR 35 IAW B737-900 SRM 53-00-01-2R-35. . REPAIR IS CAT B, INSPECTION THRESHOLD IS 50,000 FLIGHT CYCLES AFTER SDR DALA2025022001348Skin · pilot errorSHIP 673 ER/A 624217-14 REV. ORIG. - FUSELAGE / SKIN / STA. 1743.85 / STR . 29L - STR. 29R / TAIL STRIKE / PERMANENT REPAIR. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:0514-2001/009 00009 COMPLY WITH E/RA 624217-14 REV. ORIG / PERMANSDR DALA2025022001284Skin · damagedLIGHTNING STRIKE AT STA 390 STRINGER 27 LEFT. REMOVED PAINT AND PRIMER PER B-767 SRM 51-10-08. REMOVED FASTENERS WITHIN DOUBLER FOOTPRINT. DOUBLER AND FILLER FABRICATED AND DRILLED. TREATED, PRIMED, AND PAINTED REPAIR PARTS. FILLER WASHERS INSTALLED ON A/C. PESDR DALA2025021901241Skin · chafedSHIP 3361 CHAFFING DAMAGE WAS FOUND ON THE FUSELAGE SKIN PANEL BETWEEN FR 54 AND FR 55, COMMON TO THE WING TO BODY FAIRING PANEL 198GB. CORRECTIVE ACTION: COMPLIED WITH ERA 623760-33. (0816372)SDR SWI2025F00565Skin · chafedTHE SKIN ON THE REAR FUSELAGE UNDER THE LH VENTRAL FIN FAIRING HAS MULTIPLE LOCATIONS OF CHAFING. (C-CHECK RO 04/26/2025)REPAIRED CHAFING TO FUSELAGE SKIN UNDER LH VENTRAL FAIRING PER MHIRJ BLEND REPAIR REO 690-53-00-590 REV -- DATED 2025-02-28, REO FINDS BLSDR SWIA20250216Skin · chafedTHE SKIN ON THE REAR FUSELAGE UNDER THE RH VENTRAL FIN FAIRING HAS MULTIPLE LOCATIONS OF CHAFING. (C-CHECK RO 04/26/2025)REMOVED CHAFING ON THE SKIN ON THE REAR FUSELAGE UNDER THE RH VENTRAL FIN FAIRING REF REO 690-53-00-590 REV -- DATED 2025-02-28. SEE CONTISDR IPXA2025061668615Skin · dentedMAJOR REPAIR, FOUND DENT AT STA 570 A/C LEFT 13.5" BELOW SKIN LAP JOINT REPAIRED DAMAGE IAW EO-92838-REQ2SDR SWI2025F00570Skin · corrodedFUSELAGE LOWER SKIN AT APPROXIMATELY FS597-FS581 FROM STGR26L-STGR26R COMMON TO ADF ANTENNA IS CORRODED. (C-CHECK RO 04/26/2025)COMPLIED WITH THE DISPOSITION FOR BLENDED CORROSION DAMAGE TO FUSELAGE SKIN BETWEEN FS565.00 - FS613.00 & STR26L - STR26R (UNDERNEASDR DALA2025021901265Skin · not reportedSHIP 673 ER/A 624191-14 REV. ORIG. - FUSELAGE / SKIN / STA. 1720 FWD / STR. 29L - STR. 29R / TAIL STRIKE / PERMANENT REPAIR. CORECTIVE ACTION: REF ERA 624191-14. (0812893)SDR DALA2025021901263Skin · not reportedSHIP 673 DTE, ER/A 624217-14, REPAIRS AT STA 1720 AND AT STA 1744 (AREA B ) BETWEEN STRINGERS 29L AND 29R. CORRECTIVE ACTION: REF ERA 624217-14. (0813052)SDR DALA2025021901262Skin · damagedSHIP 673 DTE, ER/A 624191-14, REPAIR FWD OF STA 1720 BETWEEN S-29L AND S- 29R. CORRECTIVE ACTION: REF ERA 624191-14. (0812559)SDR DALA2025021901260Skin · dentedSHIP 6705 DENT ON FUSELAGE SKIN BTW S=28-29 STA 1560- 1580. CORRECTIVE ACTION: SUMMARY OF NRC 00076: FUSELAGE SKIN BTW S=28-29 STA 1560-1580 WAS REPAIRED PER PRI 623761-14 REV. 1 AND ER/A 623761-14 REV ORIGINAL. (0812042)SDR DALA2025021901243Skin · damaged(LOG 0811791) TOOL MARKS BTW STA.727D-STA.727E. BTW STG.1. INTERNAL FUSELAGE SKIN. FUSELAGE SKIN BTW STA.727D-STA.727E. BTW STG.1 WAS REPAIRED PER ER/A 623785-14AD REV. A SECTION I: PERMANENT REPAIR AND ER/A 623787-14AD REV. ORIGINAL.SDR SWIA20250422214Skid Shoe · bentGROUND AIR SERVICE DOOR 311AL, FORWARD AND AFT LANDING ON AIRFRAME SIDE ARE BENT (C-CHECK RO 04/21/2025)REPAIRED GROUND AIR SERVICE DOOR FORWARD AND AFT LANDINGS IAW REO 601R-53-61-6078 REV. --, DATED 2018-04-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACSDR DALA2025021901261Skin · dentedSHIP 6705 DTA MONITOR INSPECTION LOG REF ERA 623761-14 FUSELAGE / SKIN PANEL / BETWEEN BSTA 1560 AND BSTA 1580 / BETWEEN S-28R AND S-29R / DENT. CORRECTIVE ACTION: 623761-14. (0811488)SDR JJBA202502265040Repair · damagedREPAIR DOUBLER ON LH CENTER FUSE I SKIN BTW FR20-21 AND BTW STR 13L-14L. LH CENTER FUSE I, SKIN BTW FR 20-21 AND BTW STR 13L - 14L DOUBLER REMOVED. SKIN REPAIRED BTW FR20-21 AND BTW STR 13L-14LSDR ABX2025F00000Skin · crackedDURING C CHECK AIRBORNE MAINTENANCE REPORTED AN EXISTING FLUSH SKIN REPAIR INSTALLED AT STA 440-460 BETWEEN STRINGERS 33R AND 35R. THE REPAIR WAS ACCOMPLISHED BY THE PREVIOUS OPERATOR IN 2008 AND IT WAS DOCUMENTED AS ACCOMPLISHED PER 767-200 SRM 53-00??0L REPASDR SWIA2025062400212Skin · gougedEXTERIOR SKIN GOUGED FS559.00+112.00 AT STGR20R (C-CHECK RO 06/23/2025)PERFORMED BLEND REPAIR OF EXTERIOR SKIN GOUGE AT F.S 559+112 STGR 20R REF. REO 601R-53-51-705 REV. -- DATED 2025-02-28 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR ASAA2025031756600Skin Panel · corrodedCORROSION ON WATER SERVICE PANEL AT FASTNERS ON EXTERNAL HINGE AND ALSO PUSH LATCH, WITH 2 SPOTS ON INTERNAL DOOR. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 BETWEEN STA 907-927 STGR 25R-27R OF WATER SERVICE PANEL CUSDR SWI2025F00282Skin · dentedRA91428-RA91428-ETD2024-170-015605 REV: E EVALUATE AND IMPROVE APPEARANCE DENT #48 BETWEEN FRAMES 93-94 AND STRINGERS 03R-04R LENGTH 2.125", WIDTH 1.875", DEPTH 0.07". W/H = 27 (C-CHECK RO 3/4/2025) INSTALLED PERMANENT DOUBLER REPAIR ON RH FUSELAGE SKINSDR SWIA202503050212Skin · dentedRA91428-RA91428-ETD2024-170-015605 REV: E EVALUATE AND IMPROVE APPEARANCE DENT #47 FRAMES 92-93 AND STRINGERS 04R-05R LENGTH 2.190", WIDTH 2.130", DEPTH 0.138". W/H = 15 (C-CHECK RO 3/4/2025) INSTALLED PERMANENT DOUBLER REPAIR ON RH FUSELAGE SKIN FR92-9SDR JJBA20250225033Skin · dentedEXTERNAL CENTER FUSELAGE, SKIN DENTED BTW FRAME 19-20 AND BTW STR 11L-12L. EXTERNAL CENTER FUSE, BTW FR 19-20 AT STR 11L. EXISTING RIVET REMOVED FOR REPAIR DOUBLER. EXTERNAL CENTER FUSELAGE I, SKIN BTW FR19-20 AND BTW 11L-12L DENT REPAIRED.SDR AALA202502176251Skin Panel · dentedAIRCRAFT IN BASE MAINTENANCE: DENT LOC. ON EXTERNAL SKIN AT LEVEL STRG 19RH BTW FR85 AND FR86 ON TAILCONE. DENT MEASURE ARE L=6.013 INCH W=3.453 INCH D=0.007 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR (DOUBLER) CATEGORY (A) ON EXTERNAL SKIN AT LEVEL STRG 19RSDR DALA2025021401157Skin · dentedSHIP 5814 DENT ON EXTERNAL LOWER SKIN BTW STA 570-580 8.5" FROM LOWER EDGE FWD CARGO DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00040 REPAIR CATEGORY "B" ON DENT OUT OF LIMITS AT EXTERNAL LOWER SKIN BTW STA 570-580 8.5" FROM LOWER EDGE FWD CARGO DOOR WAS PERFORMESDR DALA2025021301132Skin · dentedSHIP 5814 DENT ON EXTERNAL LOWER SKIN BTW STA 570-580 8.5" FROM LOWER EDGE FWD CARGO DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00040 REPAIR CATEGORY "B" ON DENT OUT OF LIMITS AT EXTERNAL LOWER SKIN BTW STA 570-580 8.5" FROM LOWER EDGE FWD CARGO DOOR WAS PERFORMESDR SWIA202503050211Skin · dentedADM #8860 EVALUATE AND IMPROVE APPEARANCE FOR DAMAGE AT (9 DENTS TOTAL)DENT #2 RH FWD FUSELAGE BELOW STRG15R FWD OF FR08DENT #3 RH FWD FUSELAGE ABOVE STRG 13 AFT OF FR 08DENT #4 RH FWD FUSELAGE BETWEEN STRG 15R AND 13R AFT OF FR 08DENT #5 RH FWD FUSELAGE BETWESDR AALA202502240420Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: DURING CPCP 57-030-00 TASK FOUND LEFT HAND RAM AIR INLET MODULE LOCATED BETWEEN BS 500G TO 500H AND STR 22L TO 24L HAS CORROSION. REMOVED CORROSION UPON EVALUATION FOUND TO BE WITH ALLOWABLE LIMITS, PER B737NG SRM 51-10-02 SRM 53-SDR SWIA20250214001Skin · damagedLIGHTNING STRIKE DAMAGE FOUND TO FUSELAGE SKIN BETWEEN FS625.30 AND FS654.50 AND BETWEEN STGR3R AND STGR5R. THIS REPAIR WILL BE CONSIDERED A MAJOR REPAIR PER GMM 3-26 (FILED CLOSED) COMPLIED WITH PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN FS625.30 AND FSSDR DALA2025021401156Skin · dented(LOG 6922490) DENT FOUND BELOW L1 DOOR, AT STATION 363 BETWEEN STRINGERS 17 & 18. C/W B737 SRM 53-00-01-1A, PARA 4, STEP A3.SDR DALA2025021301131Skin · dentedSHIP 658 DTE, ERA 624103-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN AT STA 888 AND S-14L FOR DENT. CORRECTIVE ACTION: REF ERA 624103-14. (0806047)SDR DALA2025021301130Bear Strap · crackedSHIP 6705 INITIAL / A.D. / A.A. / DURING NDT INSPECTION TWO CRACKS WERE FOUND IN THE BEAR STRAP EDGE BTW STA 340 AND STA 350, ON THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT, IN REF CARD 5331-01232- 02A JOB # 081-0001, STEP 7. CORRECTIVE ACTION: SUMMARY OF NRC 0SDR DALA2025021301129Skin · dentedSHIP 658 INITIAL INSPECTION DENT BTW STA 879-900 AND STGR-14L AT FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00088: FUSELAGE SKIN BTW BSTA 879-900 AT S14L WAS REPAIRED PER PRI 624103-14 REV. 2 AND PER ER/A 624103-14 REV. ORIGINAL SECTION I: REPAIR INSTRICTIONSSDR CALA2025021202295Skin · scratchedEXTERNAL WALK AROUND - SERVICE CHECK PROCEDURE - SCRATCH FOUND ON FUSELAGE UNDER DOOR 1L. ATTACHED SDR. GOUGE FOUND DURING WALK AROUND ON SERVICE CHECK. NO OTHER INFORMATION AVAILABLE. REMOVED PAINT AND DIRT IN AREA TO EVALUATE DAMAGE. FOUND DAMAGE TO FUSELAGESDR DALA2025021101076Skin · damagedLEFT SIDE OF FUSELAGE HAS A SMALL DENT/NICK BETWEEN STR23. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0557:2090-2107/002 00406 REPAIRED GOUGE PER ER/A 623625-14 PRI REV 0,REV 1,REV 2, AND ER/A 623625- 14 REV ORIGISDR VNAA202502110021Skin · corrodedCORROSION ON INNER SKIN SURFACE BTW FS 364.00 TO FS394.00, BTW STGR 25LH TO 25RH AT THE MAIN AVIONICS BAY DOOR CUTOUT. REPAIRED PER REO
690-53-21-032 REV. - -SDR VNAA202502110030Skin · dentedINITIAL INSPECTION: SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF RH VENTRAL FIN FAIRING. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1498 REV - -SDR AALA202504017686Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN PANEL BETWEEN FR 69 AND FR 70, BETWEEN S31R AND S32R. REPAIRED SKIN PANEL PER SRM 53-41-11-300-004.SDR AALA202502175586Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK AT FASTNER/ FRAME 14 RHS. MAINTENANCE ADDED DOUBLER TO SKIN AT FR12 TO FR14 IAW EA 361937.
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