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 IXXA2024021901Skin · corrodedCORROSION ALC INNER SKIN F/S 1197+148 O/B OF STR 35LSDR DALA2024022102406Skin · punctured(LOG 5568453) DURING MTC A/C SKIN PUNCTURED NEAR OUTFLOW VALVE BY LOWER SAFETY RELIEF VALVE. ACCOMPLISHED REPAIR PER ERA 615865-14 REV A.SDR SWAA2024031453150Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN COMMON TO FASTENER LOCATIONS FROM STA 1016+2; TO STA 1016+23; BUTT LINE 8 TO 13; LEFT AND RIGHT.<[01] CERTIFIED APPLICABILITY OF SRM 53-00-01-1A-1;[02] ' AS PER EA 24-153-00521; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICESDR DALA2024022002345Skin · dented(LOG 0206268) FUESLAGE SKIN DENT LOCATED AT STA 981 S-27L TO S-27R AT A STATIC PORT. REPAIRED PER ERA 615865-14.SDR DALA2024022002317Skin · damagedSHIP 188 FOUND ON ARRIVAL SKIN DAMAGE AT AFT LAV VACUUM BLOWER EXHAUST/ TANK VENT CUTOUT LOWER PORTION OF CUTOUT. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767 SRM 53-60-01-2R-3. (5770733)SDR SWAA2024030752957Doubler · crackedREPLACE PREVIOUS REPAIR AT EXTERNAL POWER DOOR INNER DOUBLER CUTOUT SKIN AFT EDGE<[01] REMOVED PREVIOUS REPAIR (INNER DOUBLER CUTOUT SKIN AFT EDGE) AT EXTERNAL POWER DOOR AS PER SRM 51-40-02-0G-0 AND SRM 53-10-15-2R-4. INSTALLED INNER DOUBLER AND RUBBING BLOCKSDR GTIA2024022037924Skin Panel · damagedEVIDENCE OF LIGHTNING STRIKE AT FR.35.4 AND STR 28L REF-01 3337403-01 GENERATED -PERFORMED PERMANENT REPAIR FASTENER HOLE AT FRAME 35.4 STR 28H IAW EA #53-0043-24 REPAIR IS CAT ASDR GTIA2024022037922Skin · damagedREF AEROMAN W/O 2024-53/1 NR 2024-38968. DURING LIGHTENING STRIKE INSP. FOUND 4 BURNED FASTNERS ON FR 16 AND STR 13L, FR 18 AND STR 29L, FR 19 AND STR 29L, AND ON FR 22 AND 31L ON SKIN PANEL D5311407520201. RAF-01 3337401-01 GENERATED.-PERFORMED PERMANENT RESDR DALA2024021902307Skin · damagedSHIP 1605 FOUND RIVET NO IN GOOD CONDITION ON FUSELAGE SKIN REPAIR DOUBLE(ER/A 454087-14) STA 1767 AND S-26R AREA. CORRECTIVE ACTION: THE FASTENER REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 REV.124.00 08 JAN 24 AND ERA:454087-14. (0203824)SDR ABXA2024021900642Skin Panel · corrodedMAINTENANCE CHECK. DURING ACCOMPLISHMENT OF SB-767-53A0100, FIGURE 37 (SPOT-FACING OF CORRODED SKIN)(REFERENCE AMES DOCUMENT 47008ORD10) REPAIR• FUSELAGE SECTION 45 - SKIN PANEL SPOTFACE REPAIR AT STA 955 RBL 97.S WL WAS FOUND THE MINIMUM MATERIAL READING IS 0SDR ABXA2024021900641Bear Strap · gougedDURING C-24 MAINTENANCE CHECK AT HAECO AMERICAS, GOUGE DAMAGE WAS FOUND ON THE CARGO DOOR CUTOUT, LOWER FORWARD COMER, INNER SURFACE BEARSTRAP AT APPROXIMATELY STA 547. POST BLEND MEASUREMENTS HAVE THE MINIMUM REMAINING MATERIAL THICKNESS AT 0.006-INCH FROM ANSDR DALA2024021702305Skin · damagedAIRCRAFT 3031, DAMAGE TO FUSELAGE 9" FWD OF LAV SERVICE DOOR. CORRECTIVE ACTION: REMOVED EXISTING FASTENERS AND CUT OUT DAMAGE PER A321 SRM 53-41-11-300-018. PERFORMED HFEC OF DAMAGE CUTOUT IAW A321 NTM 51-10-08 AND BOLT HOLE A321 NTM 51-10-01. NO FURTHER DAMGSDR DALA2024021602270Doubler · corrodedCORROSION ON RH PREVIOUS REPAIR DOUBLERS STA Y=451-464 AND Y=479 (LOWER SURFACE) X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00524: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER STA Y=451-464 AND Y=479 (LOWER SURFACE) X=- 60 AT PASSENGER CABIN WAS REPLACED PER B717-SDR VNAA202403230015Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1348REV --SDR SWAA2024031452452Skin · debondedPANEL 194CL OUTER SKIN HAS 2 TIGHTLY GROUPED DISBONDS NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED PANEL 194CL OUTER SKIN HAS BEEN REPAIRED IASDR DALA2024022602645Skin · damagedSHIP 3426 DAMAGE FOUND BETWEEN STGR 39 AND 40. CORRECTIVE ACTION: BLENDED AND SMOOTHED AREA PER A330 SRM 51-11-11. (5432771)SDR DALA2024022302555Skin · mechanic errorSHIP 5635 WHILE PERFORMING INSPECTIONS PER WC 2330-01322-03I, ET-GPS ANTENNA, B757-200 INSPECT, SECTION 03I, NINE (9) PLUG LOCATIONS COMMON TO THE SKIN ONLY WERE FOUND BETWEEN STA 620 640 AND STRINGERS 2R 2L. THESE LOCATIONS ARE ADJACENT TO THE FASTENERSSDR DALA2024022302551Doubler · corrodedSHIP 6807 DTA - ERA 615826-14 THE EXTERNAL GOGO DOUBLER WAS PREVIOUSLY FOUND WITH CORROSION DAMAGE ON THE GOGO KU STC EXTERNAL DOUBLER. THE CORROSION WAS BLENDED PER ER/A 594639-14. THE BLANKING PLATES USED TO COVER THE FUSELAGE ARE COMMON TO THE CORROSION BLESDR DALA2024021602292Skin · ground damageSHIP 672 WHILE TAXIING A BAGGAGE CART DROVE ACROSS AND WE COLLIDED. CORRECTIVE ACTION: C/W REPAIR AT STA 395-409 + STR 527R 28R PER ERA 615664-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. REF LOG 0201269. REPAIRS GOOD PER ERA LOG 615664-14AD REV ORG. ALL RIISDR DALA2024021602280Skin · nickedSHIP 3417 FWD CARGO DOOR CUT-OUT, AFT/LOWER CORNER, SEVERAL NICKS ON EDGE OF FUSELAGE SKIN. CORRECTIVE ACTION: COMPLIED WITH ERA 615787-14 REV 0, REV 1 AND ERA 615787-14 REV ORIGINAL. (0202550)SDR QXEA2024021500034Skin · mechanic errorMISDRILLED HOLE AT STR 2L 19.5" AFT OF FR 20 AND 13.2" FWD OF FR23. REPAIRED THE STRINGER AS PER SRM 51-10-07, CASE 2 BY INSTALLING A CYLINDRICAL BUSHING TO THE STRINGER AND A COUNTERSUNK BUSHING TO THE DAMAGED SKIN. INSTALLED FASTENER ONCE BUSHING IS INSTALLESDR DU4R2024021500005Skin · damagedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND A PIN HOLE IN R/H FUSELAGE EXTERIOR SKIN BETWEEN FR61 – 62, STR. 40R AT THE 7TH FASTENER HOLE FWD OF FR62, OR 14TH FASTENER HOLE AFT OF FR61. S/O 634004 N/R 26894SDR ASAA2024021451240Skin · dentedRAMP REPORTS SMALL DENT FWD OF POTABLE WATER SERVICE DOOR GROUNDED - YES. ACCOMPLISHED MAJOR REPAIR IAW AIRBUS TD/81405756/032/2024#A AND ALASKA AIRLINES EA A320-53EA-02190 REV 00. PER AIRBUS RDAF 81405756/003/2024#A DATED 09/07/2024, THE PERFORMED REPAIR IS CSDR SWIA20240214Skin · dentedPROTRUDING DENT NOTED ON L/H EXTERNAL SKIN 3"-6" BELOW L/H WINDSHIELD SIDE POST AT APPROX. FS235.00 (MARKED) (C-CHECK RO 4/3/2024) CUT AWAY FS 235.0 FRAME UPPER FLANGE AND DRESSED BACK DENT ON FUSELAGE SKIN AT FS 235.0 BETWEEN STR 11L-12L TO ORIGINAL CONTOSDR VNAA202403230024Skin · damagedPERM REPAIR BEFORE 20,337.49 FH - LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS501.00 - FS661+16 & STR26L - STR23R THIS TEMPORARY DISPOSITION IS VALID FOR 600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV - - . PERM REPAIR BEFORE 20,33SDR 2024FA0000177Stiffener · crackedAFT FUSELAGE LOWER SKIN STIFFENER FOUND CRACKED. REPLACED WITH NEW STIFFENER.SDR DALA2024021502259Skin · mechanic errorSHIP 696 SECONDARY NRC: IN REF. NRC 00246: DURING FASTENER INSTALLATION VERIFICATION 02 FASTENERS WERE FOUND THAT DO NOT HAVE THE MINIMUM DISTANCE REQUIRED BTW STA 660-680 AND STRINGER 26R AT EXTERNAL SKIN (C1). CORRECTIVE ACTION: SUMMARY OF NRC 00714: FUSELAGSDR DALA2024021502256Skin · mechanic errorSHIP 672 FIVE MARKED HOLES HAVE TOOLING DAMAGE. CORRECTIVE ACTION: OVERSIZED 5EA HOLES, 4 AT .308, 1 AT .402. C/W BHEC ON 5 OVERSIZED HOLES PER PRI 615664-14AD REV.O. NO INDICATIONS NOTED. 5EA HOLES REPAIRED IAW ERA 615664-14AD REV ORIG.SDR QXEA2024021500035Skin · mechanic errorFORWARD FUSELAGE-FR22 STRINGER 2L MISDRILLED HOLE PERMANENT REPAIR. COMPLIED WITH EC ETD2024-170-003979 FORWARD FUSELAGE-FR22 STRINGER 2L MISDRILLED HOLE PERMANENT REPAIR.SDR DALA2024021502250Doubler · misinstalledDURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON T HE FUSELAGE EXTERIOR, LEFTHAND SIDE FR23L AT STR22L TWO (2) FASTENERS ARE LOCATED IN THE RADIUS OF THE CHEM-MIL AREA. THE REPAIR DOUBLER WAS INSTALLED AS PER ER/A 560683-14 REV B ON 27 JUL 201. C/A: PERSDR DALA2024021502249Doubler · misinstalledDURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON THE FUSELAGE EXTERIOR, LOCATED ON THE RIGHTHAND SIDE FR69 - FR70 BETWEEN STR 31R AND STR 32R (LAV VENT EXHAUST) REF ER/A 589202-14AD. REV A: T WO (2) FASTENERS ARE LOCATED IN THE REPAIR DOUBLER ARE IMPROPSDR CALA2024021500427Skin · dentedFUSELAGE STA 500C+11 INCHES BELOW STR 18R HAS DENT. REF. ACCOMPLISHED REPAIR AT FUSELAGE SKIN STA 500C - 500D STRINGER 18R AS PER SRM 53-00-01-2R-1. ACCOMPLISHED REPETITIVE INSPECTION AS PER TABLE 205 AND TABLE 207.SDR CALA2024021500426Skin · dentedFUSELAGE STA 500E+10 INCHES AND 4 INCHES BELOW STRG 18R HAS DENT REF. AAR N/R:9219112. ACCOMPLISHED REPAIR AT FUSELAGE SKIN STA 500E TO 500F STRINGER 18R- STRG 19R AS PER SRM 53-00-01-2R-3, ACCOMPLISHED REPETITIVE INSPECTIONS AS PER TABLE 205 AND TABLE 204SDR DALA2024021402189Skin · handler errorAIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. AFT FUSELAGE HAS 2 LARGE HOLES AFT OF DOOR 4L. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE DAMAGED SKIN PER SRM 51-27-11 TO REMOVE ALL PUNCTURES, CRACKS, ANSDR DALA2024041004270Skin · ground damageAIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. THE FUSELAGE SKIN SUSTAINED A PUNCTURE BETWEEN FR 69-70 AND STR 34L 32L. THE FUSELAGE SKIN IS P/N D5348002324200. REMOVE ALL FASTENERS IN THE DAMAGE AREA. TSDR SWAA2024031551938Angle · crackedCRACK ANGLE - CLIP BS 500C AT LEVEL STRINGER 26L FWD CARGO COMPARTMENT 2024-123933<[01] REPLACED ANGLE - CLIP BS 500C AT LEVEL STRINGER 26L FWD CARGO COMPARTMENT IAW B737 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9 ; DRAWING 143A7505 REV - .SEE INDIVIDUAL SISDR SWI2024F00181Skin · damagedDAMAGE TO FUSELAGE SKIN AND INTERCOSTAL LOCATED AT STR12A BETWEEN FS220.0 - FS235.0, LHS. THE DENT DIMENSIONS ARE: 6€? (L) X 4.5€? (W) X 0.032€? DEEP. SEE EAML 1296554 (FLIGHT 4827 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27816391 WITH THESDR SWIA202402160013Skin · scratchedDEEP SCRATCHES ON THE LEFT SIDE OF FUSELAGE ABOUT 8€™ FROM THE MAIN CABIN DOOR. (FLIGHT 3270 FILED CLOSED)DAMAGE HAS BEEN EVALUATED AND DETERMINED TO BE OUT OF LIMITS. SEE EAML 1296863 FOR DAMAGE.SDR DALA2024021502258Skin · mechanic errorSHIP 696 DTE / FUSELAGE / EXTERNAL SKIN / BTW STA 660 & STA 680 / BTW S- 26R & S-27R / EXTRA HOLE. CORRECTIVE ACTION: REF ERA 615644-14.SDR SWIA2024021500003Skin · dentedDENT INFRONT OF PORT SIDE STANDBY PITOT PROBE BELOW LH WINDSHIELD. (FLIGHT 4827 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27816382 WITH THE FOLLOWING CORRECTIVE ACTION: "PLEASE SEE ML 27816384 FOR CORRECTIVE ACTIONS "SDR SWIA202402140003Skin · dentedDENT INFRONT OF PORT SIDE STANDBY PITOT PROBE BELOW LH WINDSHIELD. (FLIGHT 4827 FILED OPEN)DAMAGE FOUND TO BE OUT OF LIMITS, SEE EAML 1296795 FOR DAMAGE DESCRIPTION.SDR IXXA2024021301Skin · crackedAFT LOWER CORNER OF FUSELAGE SKIN AND BEAR STRAP OF THE FWD SERVICE DOOR CUTOUT CRACK INDICATIONS WERE NOTEDSDR ASAA2024021248095Doubler · corrodedLOWER FUSELAGE STA727 CENTER DRAIN DOUBLER HAS CORROSION AROUND FASTNERS GROUNDED - YES. REMOVED AND REPLACED CENTER DRAIN DOUBLER AT LOWER FUSELAGE STA 727 IAW B737-900ER SRM 51-40-02 AND DWG NO. 146A0070 REV A. DWG 146A3239 REV -, BOEING CONTROL # 270917615SDR DALA2024021302116Skin · damagedSHIP 672 DTE, ER/A 615664-14AD RH LOWER SKIN PANEL CONSISTING OF DENT WITH GOUGES. CORRECTIVE ACTION: REF ERA 615664-14AD FOR REPAIR. (0198442)SDR DALA2024021302115Skin · noneSHIP 698 AD, AA, IN REFERENCE AMDS 5331-01282-03: STEP 2 PREVIOUS REPAIR WAS FOUND FROM BSTA 640 TO BSTA 660 BTW S-14L TO S-19L AT FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00009. AREA WAS PREVIOUSLY REPAIRED PER ER/A 542509-14 REV B SECTION I: PERMANENSDR FDEA202402100152Skin · cracked#3 PACK DOOR CUT OUT UPPER AFT CORNER SKIN LOOKS TO BE CRACKED APPROX 1 3/8 FROM RIVET TO EDGE. REPAIRED AIR CONDITIONING AND EXHAUST VALVE DOOR JAM UPPER AFT CORNER REF SRM 53-20-15-2R REPAIR 3 FIG 201 SHEET 3 PG 16. REF NR 04 FOR DOOR INSTALLATION "MAJSDR UATA202403183483Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.5" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, THE SITUATION REPORTED, AND A REPAIR SCHEME WAS PROVSDR SWAA2024030850539Skin · corrodedREJECT: CORROSION AT FUSELAGE SKIN AROUND RADIO ALTIMETER ANTENNA STA-450 BTW STR-27L TO STR-28L<[01] REMOVED CORROSION AND REWORKED AREA AROUND RADIO ALTIMETER ANTENNA STA-450 BTW STR-27L TO STR-28L IAW EA 24-153-00438.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1SDR SWAA2024030850538Skin · corrodedREJECT: CORROSION AT FUSELAGE SKIN AROUND RADIO ALTIMETER ANTENNA STA-410 BTW STR-27L TO STR-28L<[01] VERIFIED STEP 3 COMPLETED;[02] 'REFER TO FAULT TTG8Q00RFUS3 FOR REPAIR RESOLUTION'.;[03] VERIFIED CORRECTIVE ACTION ENTRY 2.SDR SWIA20240304209Skin · dentedRIGHT WING INBOARD FLAP LOWER SKIN, AFT OF INTERCOSTAL SPAR, FLS104.4-112.3, DENT, HN00138175 (C-CHECK RO 3/2/2024) PERFORMED CUTOUT AND APPLIED REPAIR DOUBLER TO RH WING INBD FLAP LOWER SKIN REF CRJ-900 SRM 57-52-01-201-001-A01. COMPLIED WITH TASK CAR
Back to JASC 5330