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 ASAA2025020856678Skin · corrodedBELOW THE VERTICAL AT STR 4R AND BETWEEN STA 985.5 AND STA 947 CORROSION ON SKIN SEVERAL PLACES SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON FUSELAGE SKIN P/N 147A3110-20 AT STR 4R BETWEEEN STA 947 AND 1006 IAW EA#800-53EA-2883 REV 00 SRSDR AALA202502172499Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK RADIATING OUT FROM FASTENER HOLE. MAINTENANCE ADDED DOUBLE REPAIRE IAW EA 361924.SDR SWAA2025031794115Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AT LEVEL STR 17R BTW BS 291.5 TO 294.5 AT PASSENGER CABIN 2025-112898 <[01]. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT LEVEL STR 17R BTW BS 291.5 TO 294.5 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8310SDR IPXA2025021825288Skin · gougedFAULT-MXP-ZL-300-01-1-300JIC - STRS ZONE 180. TAIL JACK POINT HAS DAMAGE ON THE DOUBLER AND SKIN AFT OF THE DOUBLER. ACCOMPLISH THE PERMANENT REPAIR PER SRM 53-10-12-201 PARAGRAPH 13 FIGURE 210 (REV. 41). REVIEWEDSDR DALA2025021101079Skin · ground damageSHIP 1811 AN IMPACT CAUSED BY A GSE EQUIPMENT IN THE A/C STRUCTURE DAMAGED THE FUSELAGE SKIN BETWEEN STA325 AND S36L. CORRECTIVE ACTION: ACCOMPLISHED SECTION II: PERMANENT REPAIR PER ERA 624166-14 REV A. (6953366)SDR DALA2025021101066Doubler · inadequateSHIP 5654 CUSTOMER REQUEST: PERFORM ER/A 546994-14 REV D. PRI REV 0 " FUSELAGE / SKIN AT FWD ATG4 ANTENNA / FS 508-520 BETWEEN S-28R & S-28L / EXTENSION OF DOUBLER" CORRECTIVE ACTION: SUMMARY OF NRC 00182. AREA ON FUSELAGE SKIN AT FWD ATG4 ANTENA FS 508-520 BESDR DALA2025020700971Skin · corrodedSHIP 3361 WASTE TANK FWD VACCUM VENT HOLE EXTERNAL SKIN CORROSION. CORRECTIVE ACTION: CLEANED AND TREATED CORROSION PER A330 SRM 53-41-11-283-018. OK FOR SERVICE. (0799519)SDR DALA2025020700970Skin · corrodedSHIP 3361 WASTE TANK AFT VACCUM VENT HOLE EXTERNAL SKIN CORROSION. CORRECTIVE ACTION: CLEANED AND TREATED CORROSION PER A330 SRM 53-41-11-205-037. OK FOR SERVICE. (0799515)SDR HNAA2025031100153Skin · dented53-2038 DENT ON LH LWR SKIN BTW FR80-81, BTW STR14-15L. REPAIRED IAW ETD 2025-145-901511 AND EO 1-53-25-0073.SDR ASAA2025020655775Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN BELOW R2 DOOR STATIC PORT FWD OF STA 986 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR ON FUSELAGE SKIN BELOW R2 DOOR STATIC POR STA 967-986 STGR 20R-21R IAW EA# 800-53EA-28220 REV 00 SRXR430X.SDR SWIA2025021006Skin · dentedEVALUATED DAMAGE AND FOUND TO BE DENT ON FR11 BETWEEN STGR 18L AND STGR 19L WITH CREASE ON BOTH SIDES OF FRAME. (FILED CLOSED) UPON INSPECTION FOUND DENT WITH A CREASE AT FR11 BETWEEN STGR 18L AND 19L TO BE OUT OF LIMITS. PERFORMED RECTANGULAR REPAIR SDR DALA2025021001032Skin · gouged(LOG 0798723) DURING INSPECTION OF THE VIASAT RADOME SUPPORT FITTINGS AND DOUBLERS INSTALLED BY AA 4430-01009, MAINTENANCE FOUND A GOUGE ON THE INNER SURFACE OF THE SKIN UNDER THE DOUBLER FOR THE #5 RADOME ATTACH FITTING. REPAIRED DAMAGE PER ERA 623785-14AD.SDR DALA2025021000999Doubler · corrodedSHIP 5654 CORROSION ON INTERNAL DOUBLER OF WASTE PANEL BTW STA 700 AND STA 720 AND BTW S-20R AND S-22R AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00257: INTERNAL DOUBLER OF WASTE PANEL BTW STA 700 AND STA 720 AND BTW S-20R AND S-22R AT FWD CARSDR ASAA2025020655769Skin · corrodedPOSSIBLE CORROSION AT FUSELAGE SKIN LOCATION STA 927 STGR 4L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 147A3110-1 STA 907-927 STGR 4L IAW EA 800-53EA-28239 REV 00 SRXR430X.SDR ASAA2025020655757Skin · corrodedPOSSIBLE CORROSION AT FUSELAGE SKIN AFT DRAIN MAST AFT OF STA 986 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 147A3400-4 AT AFT DRAIN MAST BETWEEN STA 986.5 AND STA 1016 STGR 24L -25L IAW EA# 800-53EA-28213 REV 00 SRXR43SDR ASAA2025020655756Skin · corrodedPOSSIBLE CORROSION STA 1088 BETWEEN STGR 15R-17R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN 148A3321-13 AT STA 1088 STGR 16R TO STGR 18R IAW EA# 800-53EA-28233 REV 00.SDR SWIA202507210205Skin · scratchedFORWARD DRAIN MAST EXTERIOR SKIN PENETRATION FORWARD INBOARD FASTENER HOLE HAS MULTIPLE SCRATCHES AFT OF FS333.00 BETWEEN STGR25R - STGR24R (C-CHECK RO 07/18/2025)COMPLIED WITH REO 670-53-21-2588 REV -- DATED 2025-03-12 REPAIR FORWARD DRAIN MAST EXTERIOR SKSDR AALA202504143075Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON AFT LOWER FASTENER HOLE AT FR 35 AND STR 30L . CRACK DIRECTION 5 OCLOCK VIEW FROM OUB. CRACK D= 0.185 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC. ON AFT LOWER FASTENER HOLE AT FR 35 AND STR 30L SDR HNAA2025031100161Skin · damaged53-2033 CRACK AROUND RIVET AT FR78 BTW STR5-6R. REPAIRED IAW SRM 52-32-01 AND EO 1-53-25-0071SDR R61A2025022600105Doubler · crackedCORROSION FOUND ON ANTENNA INTERNAL DOUBLER AT FWD FUSELAGE FWD CARGO BETWEEN FR19-20,STR26L-27L. ANTENNA INTERNAL DOUBLER AT FUSELAGE FWD CARGO BETWEEN FR19-20, STR26L-27L, REMOVED AND REPLACED IAW SRM 51-41-02SDR JJBA20250225039Skin · crackedCRACK FOUND AROUND RIVET ON LH REAR FUSE II SKIN AT FR 79 STR 7L-8L. CRACK AROUND RIVET AT SKIN FR79 BTW STR 7L-8L REPAIREDSDR DALA2025021001004Skin · damagedSHIP 694 FUSELAGE SKIN DAMAGED LEFT SIDE BETWEEN STA. 600" & STA. 620" AT STR. 16L. CORRECTIVE ACTION: INSTALLED REPAIR PARTS REF: B757-200 SRM 53-00-01-2R REPAIR 28. (0796791)SDR DALA2025021001000Skin · damagedSHIP 694 FUSELAGE SKIN DAMAGED LEFT SIDE BETWEEN STA. 600" & STA. 620" AT STR. 16L. CORRECTIVE ACTION: INSTALLED REPAIR PARTS REF: B757-200 SRM 53-00-01-2R REPAIR 28. (0796691)SDR A6WA202502058858Skin · dentedRH AFT FUSELAGE HAS DENTS. AIRCRAFT REMOVED FROM SERVICE. PERFORMED REPAIR ON RH FUSELAGE SKIN BETWEEN FS 625.30 TO FS672.20 STR 20-23R IAW MHIRJ REO 601R-53-61-8276 REV -- DATED 2025-02-04.SDR GTIA2025020638729Skin Panel · damagedPERMANENT SKIN REPAIR BETWEEN 5-7, Y330-Y520 EA 5311-2456-2 GENERATED-PERFORMED PERMANENT REPAIR OF THE FUSELAGE SKIN PANEL AT FR.5-7 BETWEEN Y330-Y520 IAW AE EA #53-0004-25 AND EC 5311-2514SDR DALA2025020600947Skin · damagedSHIP 3426 DAMAGE AT FWD CARGO DOOR SURROUNDING AFT LOWER SIDE. CORRECTIVE ACTION: REWORKED AREA PER SRM 53-21-11. OK FOR SERVICE. (6761142)SDR N6WA2025020504Strap · corrodedCIRCUMFERAL STRAP AT FS280 AT AT STR27 TO STR26R IS CORRODED. REPAIRED CIRCUMFERALSTRAP AT FS280 AT STR27 TO STG26R IAW STS EA 109-2025-005 AND GOJET EO C550-53MR -051-0.SDR GTIA2025050938908Skin · damagedPENETRATION DAMAGE FOUND ON CROWN SKIN AT FRAME 49-50 STRINGERS 5L-5R. RAF-01 3072220-01 CREATED. --SDR AALA202504211839Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION EXTERNAL SKIN UNDER ACCESS PANEL 321AL ON UPPER FUSELAGE, MEASURE CORROSION ARE L=1.264 INCH W=1.135 INCH D=0.008 INCH.SDR CALA2025021100340Skin · dentedREF L/P 3744746 & AVO 14096 - VISUAL INSP - FOUND STR-19L AT BS 1650 - UPPER RADIUS DEFORMED (DENTED) APPROX 3 " LENGTH, WIDTH = 1.65 X 0.080 DEPTH. A/Y= 20.625, OUT OF SRM 53-00-03-1A-1 LIMITS. TEST PER AVO14096 REV B STEP 12 AND 13, VERIFIED SUCCESSFUL REWSDR DALA2025021001040Doubler · corrodedAFT RIGHT CORNER OF WASTE BOX DOUBLER IS CORRODED. REPAIRED PER ER/A 623783-14 PRI REV O, ER/A 623783-14 PRI REV 1, ER/A 623783-14 PRI REV 2, ER/A 623783-14 PRI REV 3, AND FINAL ER/A 623783-14 SECTION I REV ORIGINAL. (LP# 0796032)SDR UIEA2025020300117Skin · gougedFUSELAGE SKIN FOUND GOUGE AT L1 DOOR AFT LOWER MID AREA(<P>GOUGE EVALUATED AND MEASURED LENGTH: 9", (A) WIDTH: 2.2", (Y) DEPTH: 0.135", A/Y = 16.29 FOUND OUT OF LIMIT AS PER B747-400F SRM 53-00-01-1A-1 ALLOWABLE DAMAGE DETAIL III REV 102. WORK ACCOMPLISHED AS SDR ASAA2025020455755Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN AT AFT JACK POINT STA 1088 STGR 24R- 25R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON AFT FUSELAGE SKIN AT AFT JACK POINT P/N 148A3321 AT STA 1088 STGR 24R-25R IAW EA#800-53EA-28214 REV 01 SRXR430X.SDR ASAA2025020455728Skin · corrodedPOSSIBLE CORROSION APPROXIMATE LOCATION STA 360 STGR 24L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 143A3212-20/143A3232-28 AT LAP SEAM STGR 24L BETWEEN STA 360 -380 IAW EA 800-53EA-28215 REV 00 SRXR430X.SDR SWI2025F01006Skin · corrodedCORROSION ON SKIN BETWEEN FS295.0 AND FS310. STGR27 AND STGR26R AS MARKED (C-CHECK RO 07/18/2025)REPAIRED CORROSION ON SKIN BETWEEN FS295.0 AND FS310. STGR27 AND STGR26R IAW REO 670-53-21-2585 REV -- DATED 2025-03-18. COMPLIED WITH ALL STEPS OF REO 670-53-2SDR LR7A2025020303707Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND LH FORWARD FUSELAGE SKIN CRACKED AT FS156, LBL56, WL240.75. / REPAIRED IAW LAC MEA 382-53-25-008. NR# 1001231852SDR LR7A2025020303706Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND RH FORWARD FUSELAGE SKIN CRACKED AT FS162, RBL56, WL240.75. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001231851SDR HNAA2025030500129Skin · dentedF025768 FUSELAGE SKIN HAS MULTIPLE PROTRUSIONS BETWEEN FRAME 12A AND FRAME 13 AND STRINGERS 06L - 08L. REPAIRED THE PROTRUSIONS BETWEEN FR12A/13 STRINGERS 06L - 08L IAW EMBRAER ETD2025-145-901668SDR R61A2025022100099Skin · corrodedCENTER FUSELAGE 3 EXTERIOR SKIN INSIDE LAV WASTE CUTOUT INTERIOR SKIN DOUBLER CORRODED, REMOVED AND REPLACED LAV WASTE DOUBLER REF SRM 51-40-08.SDR CALA2025021100341Skin · damagedMOVE TEAM FOUND DAMAGE BELOW L4 DOOR. DAMAGE FOUND APPROXIMATELY 8.5X6.75 INCHES. UPDATING WITH DAMAGE IS AT APPROX. STA. 1650 LH SIDE BETWEEN S19 & S20. PERFORMED STEPS 1 & 2 OF AVO14096. RII INSP C/W OF AVO 14096 REV A STEP 6 - INSURANCE CUT. PERFORMED STESDR N6WA2025020302Skin · mechanic errorMISDRILLED HOLE IN LOWER SKIN AT FS295.00 STR27. REPAIRED IAW STS EA 129-2025-005 AND GOJET EO C550-53MR-46SDR SWIA20250303201Doubler · corrodedWASTE SERVICE DOOR CUTOUT ON FUSELAGE INTERNAL DOUBLER CORRODED INBOARD OF HINGE POINT (C-CHECK RO 3/1/2025) REMOVED AND REPLACED WASTE SERVICE DOOR CUTOUT ON FUSELAGE INTERNAL DOUBLE REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART NO CHANGE TO WEIGHT SDR SWAA2025020491976Skin · crackedAFT FUSELAGE SKIN HAS 1/2' LONG CRACK ON AFT SIDE OF VACUUM WASTE EXHAUST PORT. FUSELAGE STATION 918 AND 3.5 INCHES ABOVE STRINGER 22L. COMPLIED WITH TASK CARD. COMPLIED WITH EA 25-153-00283.SDR SIMA20250201001Skin · damagedINTERNAL SKIN WITH TOOLING MARK, LOCATED AT FR 78+14.5" BTW S-1L AND S-2L. REPAIR REQUIRED TO DAMAGED AREA. (MAJOR REPAIR) BLENDED DAMAGE AREA IN SKIN IML AT INTERNAL CROW SKIN BETWEEN STRINGER 1L AND 2L AND BETWEEN FR78 AND FR79 IAW E175 SRM 51-10-03 AND EA98SDR SWI2025F01037Skin · gougedFORWARD CARGO DOOR SURROUND STRUCTURE -FORWARD EDGE OF THE DOOR OPENING THE SKIN IS GOUGED BELOW THE TWO FORWARD GUIDE FITTINGS APPX FS535.00. (MARKED) (C-CHECK RO 07/18/2025)ORIGINAL MATERIAL THICKNESS IS 0.160", MINIMUM REMAINING THICKNESS IS 0.139" FOR ASDR VNAA20250329023Skin · corrodedCORROSION ON CUT OUT INNER FACE AT E/E DOOR SETTLEMENT AREA. CORROSION ON CUT OUT INNER FACE AT E/E DOOR SETTLEMENT AREA WAS REPAIRED PER REO 690-53-21-032 REV - -SDR REXA2025022500221Skin · chafedFOUND CHAFE ON BELLY OF AIRCRAFT AT FS 913 LBL 27. COMPLIED WITH BOMBARDIER GREO 670-53-00-290 REV F DATED 2019/04/26 SOLUTION 2. THIS REPAIR HAS SDIR/ REINSPECT REQUIREMENTS.SDR U2RA2025013100011Skin · deformedDURNING C CHECK IN HAECO SECTION 41 FUSELAGE SKIN, BETWEEN STA 488 AND STA 520 AND BETWEEN 22L AND STR -257 WAS FOUND WITH BLENDOUT DENT DAMAGESDR DALA2025020400866Skin · corroded(LOG 6976703) CORROSION FOUND AT STA 1016 STR 21L & 22L. PERFORMED CUTOUT OF DAMAGED AREA, LOCATED AND DRILLED FABRICATED REPAIR PART. ALL PARTS ALODINED AND PRIMER APPLIED IAW 737 SRM 53-70-01.(2422056) C/W HFEC & LFEC IAW B737SRM 53-70-01-2R PROCEDURE 4. INSSDR CALA2025020200251Skin · crackedIT WAS FOUND A CRACK INDICATION AT FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AFTER NDT INSPECION PART 6 51-00-16 REV 139. (ORIGINATING DOCUMENT NR2396712)
Back to JASC 5330