JASC 5300
Service difficulty reports · 8,204
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 HNAA2025080500532Seat Track · corrodedCORROSION ON CABIN RH INBD #4 SEAT TRACK. BLENDED CORROSION ON RH INBD #4 SEAT TRACK AND FOUND THE CORROSION TO BE DEEP AND BEYOND ALLOWABLE LIMITS, REMOVED AND REPLACED RH INBD #4 SEAT TRACK IAW EMB 145 SRM 51-10-03, SRM 53-00-11 AD,FIG 101, AND AMM 53-01-06SDR SWIA2025081800060Structure · corroded1 AREA OF CORROSION BEYOND ALLOWABLE LIMITS AS PER GREO 601R-53-41-666 REV -C DATED 2012-11-06 JUST FWD OF FS 559.00 AT LBL 42.5 APPROXIMATELY (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-41-3325 REV- DATED 2025-06-21 REPAIR TO PRESSURE FLOOR SILL BETWEESDR SWIA2025081800611Structure · corroded4 AREAS OF CORROSION BEYOND ALLOWABLE LIMITS AS PER GREO 601R-53-41-666 REV -C DATED 2012-11-06 BETWEEN FS449.85 AND FS529.00 AT APPROXIMATLY RBL 43.0 (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-41-3322 REV "--" DATED 2025-07-04 FOR 4 AREAS OF CORROSIOSDR DALA2025060904369Structure · not reportedSHIP 3417 PERFORM DVI OF THE CARGO CEILING. CORRECTIVE ACTION: COMPLIED WITH ERA 626805-14 REV ORIG. (1012655)SDR CALA2025053005125Window Frame · crackedREQUESTING ENGINEERING SUPPORT FOR EA5310-08195 REVISION B OP 003 LH SIDE NUMBER 3 WINDOW FRAME POST - PERMANENT REPAIR, FASTENER HOLE NUMBER 3 (BOTTOM TO TOP) HAS A CRACK SIGNAL NOTED AT 9 O?CLOCK POSITION. FASTENER HOLE CURRENTLY IS 0.297 INCHES OF DIAMETER,SDR CALA2025052604946Unknown · vibrationAIR RETURN FOR VIBRATIONS IN FLIGHT CONTROLS CREW DEBRIEF STATED AT 10,000 FT FELT VIBRATION IN THE CAPTS AND FOS YOKE IN CLIMB TO CRUISE AT SPEEDS OF 250,280 TO 320 THE INTENSITY RAMPED UP AND STAYED THERE IN ALL PHASES OF FLIGHT. DURING TURNS, ASCENDING ANDSDR IXXA20250521001Structure · cracked4 TOTAL LFEC INDICATIONS FOUND WHILE PERFORMING BS 1809.5 LEFT SIDE FORWARD OUTER CHORD. THE 2 AFT FASTENERS IN AREA 1, THE AFT UPPER FASTENER IN AREA 2, AND THE OUTBOARD UPPER INSDR SWIA2025090900515Structure · gougedLEFT HAND ICED DETECTOR PROBE CUT OUT LOWER CORNER GOUGED (C-CHECK RO 09/07/2025)REMOVED GOUGE ON LEFT HAND ICED DETECTOR PROBE CUT OUT LOWER CORNER, PER REF.CRJ/700 SRM.51-12-00-001-001-A01 AND COMPLIED WITH REO 670-53-11-2152 REV -- DATE 2025-06-19 COMPLIEDSDR QXEA2025052200224Rib · crackedLH SIDE OF RIB 52 CRACKED AT UPPER SIDE (MARKED). REPAIRED LH SIDE OF RIBS 2 IAW SRM 53-22-04-02-04 04P.SDR AALA202505097582Unknown · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CLIMBING THROUGH FL180 AN ABRUPT VIBRATION WAS FELT IN THE FLOOR OF THE COCKPIT AND THROUGHOUT THE AIRCRAFT WITH AN ASSOCIATED VIBRATORY NOISE. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SMF. SDR AALA202505087582Unknown · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CLIMBING THROUGH FL180 AN ABRUPT VIBRATION WAS FELT IN THE FLOOR OF THE COCKPIT AND THROUGHOUT THE AIRCRAFT WITH AN ASSOCIATED VIBRATORY NOISE. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SMF. SDR SWAA2025060966999Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2025-297785<[01] REPLACED ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7505 SHET 5 REV B. SEE INDIVIDUAL SIGSDR CALA2025042904317Repair · not reported(B757-53-3-0478) VERIFIED APPLICABILITY, STR-AFT CARGO COMPT. ST A 1320 BTWN STRG 24/26 HAS FRAME REPAIR VERY CLOSE TO FACTORY SPLICE, REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR IN AFT PIT STA 1320 STR 24/26R IAW 757 SRM 53-00-07-2R-5 DETAIL III. MAJORSDR CALA2025041803983Unknown · vibrationAIRFRAME VIBRATION ABOVE COST INDEX ZERO. HIGHER THE INDEX GREATER THE VIBRATION. FLIGHT ATTSDR AALA202508042508Fitting · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR RETRACT ACTUATOR UPPER FORWARD FITTING WORN ALLOWING THE BUSHING TO MIGRATE BETWEEN FR 42 AND FR 43 AT KEEL BEAM RIB W10. REPLACED FITTING PER EA 365943.SDR 9WGA2025041454612Shroud · crackedDURING HEAVY MAINTENANCE CHECK COPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK. ACCOMPLISHED REPAIR AT COPILOTS SLIDING WINDOW AFT SHROUD COVER IAW MD-11 SRM 51-43-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WG2025F00000Shroud · crackedCOPILOTS SLIDING WINDOW AFT SHROUD COVER HAS A CRACK.SDR CALA2025041703931Vent · bird ingestionBIRD CAUGHT IN PAC AIR VENT UNDER AIRCRFT. FOUND BIRD WHOLE AND INTACT IN LOUVER PANEL, ACCESSED THRU RIGHT WHEEL WELL MLDG DOOR FOR RETRIEVAL, NO ABNORMAL SMELLS OR INDICATIONS NOTED IN CABIN OR FLIGHT DECK, PERFORMED BIRD STRIKE INSPECTION REF AMM 05-51-SDR 2025FA0000259Nut Plate · corrodedCORROSION AROUND AFT AND FWD NUTPLATES ON PANEL 316DBC AND 316CBC MOUNTING FLANGESSDR NACA2025040700006Structure · damagedPERFORMED REPAIR AT STA 294.5 RBL51. TRIMED OUT DAMAGED AREA. MADE REPAIR PARTS AND INSTALLED. PER B737-300 SRM 53-10-51 REPAIR 5 FIG 201.SDR 2025FA0000249Skin · not reportedREPAIR - SECTION 46 - FUSELAGE SKIN AFT CARGO DOOR BETWEEN STA 1355 AND STA 1346 AND STR-28R & STR-33R.SDR 2025FA0000244Skin · corrodedREPAIR CENTER WING SKIN- UPPER SKI PANEL - RBL 54.81 / RBL 74.81 AT REAR SPAR AREA CORROSION.SDR IXXA2025040300012Beam · corrodedCORROSION F/S 1856 - 1862 RBL 14 - LBL 18 SEVERAL AREAS ON SHELF UPPER SURFACE LOCATED BELOW HORZ STAB CTR BOXSDR HNAA2025042800233Partition · corroded53-2259 CORRODED LH LATERAL DOUBLER PARTITION AT FR61. REPAIRED IAW ETD2025-145-905579 AND EO 1-53-25-0136SDR CALA2025032803291Structure · corrodedR2 DOOR CUTOUT LOWER CHORD UPPER SURFACE IS CORRODED, FROM STA 947-992 RBL 48.SDR IXXA20250327001Shim · corrodedFOUND CORROSION ON SHIM TO BE OUT OF LIMITSSDR UIEA2025031900359Longeron · crackedDURING HFEC INSPECTION, FOUND CRACK AT LONGERON EXTENSION FITTING STA 1480 LHS & RHS APPROX CRACK LENGTH = 0.6" RHS AND 0.4" LHS AS MARKED.(<P>WORK ACCOMPLISHED IAW EN# 1018-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025031900362Rub Strip · obstructedDURING PERFORMING LH AND RH RUB STRIP INSTALLATION PER SB 747-53A2721R3/ AD 2013-26-12, FOUND AFT RUB STRIPS INTERFERING WITH EXISTING PROTUDING HEAD FASTENERS ON FUSELAGE SKIN AT BS2517 TO 2628 LH AND RH(<P>WORK ACCOMPLISHED IAW EN# 1019-25 REV 0. NO FURTHER SDR 2025FA0000200Skin Panel · corrodedCORROSION FOUND AT FS 779 THAT WAS CLASSIFIED AS LEVEL 2 AND A REPAIR WAS REQUIRED.SDR DALA2025032402168Not Reported · out of adjust(LOG 0870275) GAP MEASURED ON WORK CARD 5311-01251-01B (FORECAST CARD 38-0553-8-0152) PAGE 9 STEP 11 MEASURES GREATER THAN 0.006. REPAIRED PER WORK CARD 5311-01251-02B (FORECAST CARD 38-0553-8-0156).SDR DALA2025032402182Not Reported · out of adjust(LOG 0870286) GAP MEASURED ON WORK CARD 5311-01251-01A (FORECAST CARD 38-0553-8-0149) PAGE 9 STEP 11 MEASURES GREATER THAN 0.006. REPAIRED PER WORK CARD 5311-01251-02A (FORECAST CARD 38-0553-8-0154)SDR FDEA202503190456Floorboard · damagedMAIN CARGO COMPARTMENT FLOOR PANEL 241XFF HAS 3 DAMAGE INSERTS. REPLACED 3 DAMAGED INSERTS ON FLOORBOARD PNL# 241XFF MPN: 145T5876-103 AT STA: 975- 1114.82 AND LBL 11 THROUGH LBL 33.IN REF TO B767 SRM 53-00-50-2R FIG 201 SHEET 8 REPAIR 1. THIS IS A MJOR REPSDR AALA202503190171Vapor Barrier · looseAIRCRAFT IN BASE MAINTENANCE: VAPOR BARRIER UNDER CAPTAINS SUITCASE STORAGE AREA IS LOOSE. SECURED VAPOR BARRIER TO FORWARD EDGE OF A LAVATORY WITH TAPE.SDR KCSA202503151032Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN APPROX. STA 738 LS-17SDR NACA2025041400007Not Reported · corrodedCORROSION - DURING PERFORM EO 767-27-0012-02 FOUND THE CORROSION AT STA 1725.5 BETWEEN S-33L ~ S-33R.SDR SWAA2025040804261Fastener · unsecureFLOOR BEAM TO L/H MOP SEAL HARDWARE IN FWD WET AREA NOT SECURE - BS 344; LBL 62; WL 208<[01] FLOOR BEAM AT BS 344; WL 208; LBL 62 ESCAPE SLIDE TIE DOWN ATTACH FASTENER RETIGHTENED PER IPC 53-42-00-20 AND AMM 20-50-11-910-801. <BR>TORQUE ID: 2556<BR>CAL DUE 11/SDR DALA2025031501992Structure · damagedSHIP 3148 DISC: DTE, ER/A 620540-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A319 / 3148 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME & SKIN / OVZ HOLE. C/A: ER/A 620540-14AD REV A REQUIRES STAGE 3 DTA APPROVAL ON OR BEFOR E 60,000 FC FROM SECTION I REPAISDR 2025FA0000177Not Reported · not reportedFABRICATION SUPPORT FWD CARGO COMPARTMENT BETWEEN STA 588-610 AT LBL 31 AND STA 588-610 AT RBL 31.SDR IPXA2025031071222Skin · crackedSKIN CRACK - L/H AFT FUSELAGE UPPER AREA AT STA 1659~STA 1665 S-13AL.REPAIRED DAMAGED AREA I.A.W SRM 53-80-01-2R-7 REV.91 AND EGAT WORK SHEET NO. 50153.ACCOMPLISHED THE REPAIR PER 767-300F SRM (REV. 91) 53-80-01-2R-7.SDR DALA2025022401422Repair · noneSHIP 6705 A.A. IN REF AMDS 5311-01227-01A STEP 2: EXISTING REPAIR WAS FOUND IN INSPECTION AREA AT STA 1460, S-26L AT AFT CARGO COMPARMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00167: AREA AT STA 1460, S-26L AT AFT CARGO COMPARMENT WAS REPAIRED PER ERA 623706-14ADSDR CALA2025022402447Unknown · noiseLOUD BANGING NOISE FROM UNDERNEATH FLOOR OF FORWARD GALLEY DURING CLIMB OUT. CREW ALSO REPORTED THE NOISE WAS PERSISTENT DURING CLIMB AND STOPPED ONCE LEVELED OUT. DID NOT RETURN AGAIN DURING DESCENT. REMOVED FWD PIT CREW O2 BOTTLE ACCESS PANEL & FWD LAV TOILESDR CALA2025021802361Door · contaminatedAPU OIL SMELL IN CABINPACKS RUNNING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INVESTIGATE AND CONTACT AIRCRAFT MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003129638 AND PRTR ACCOMPLISHED ENGINE RUN AT GATE WITH FLIGHT CREW AND WISDR 2025FA0000102Grease Fitting · defectiveGREASE FITTING ON MAIN ROTOR PITCH LINK UNIVERSAL BEARING WOULD NOT ACCEPT GREASE BUT WOULD PURGE GREASE. UPON FURTHER INVESTIGATION, THE FITTING APPEARS TO HAVE BEEN ASSEMBLED INCORRECTLY WITH THE STOPPER BALL ON THE INSIDE OF FITTING WITH THE SPRING PRESSINSDR YENA2025021100149Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 1 LOC FR16RH DOUBLE JOGGLE AREA. C RACK DIRECTION 2 OCLOCK AND CRACK LENGTH 0.100 INCH; (RESOLVED ON W/O: 1353223 TASKCARD: NR-00006) REF AEROMAN WO 2025 25/1 NR 2025-76442 PERFORMED PERMANENT REPAISDR IPXA2025021463465Not Reported · corrodedCORROSION - MAIN DECK STA 500 LBL 95. (REPLACE). FABRICATE P/N:69B62123-4 PER BOEING DWG NO.69B62123 SH1 REV."C", PL REV."-" AND EGAT WORK SHEET NO.50081 AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH9.08 REV.10 REQUIREMENT.SDR A6WA202501228854Stiffener · meltedREQUEST INSPECTION FOR SHORTED GROUND POWER RECEPTACLE. AC GROUND POWER AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FND A/C RECEPT AND SHIELD MELTED, RECEPT SUPPORT MEMBER & INTERCOSTAL HAS HEAT DAMAGE AND MELTED AREAS. FWD PRESS BULHEAD HAS APPROX 2"X 1SDR FDEA202501200239Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO: E6- 5230-E0378588 B P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24, LONGN1~3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:981, TITLE: DOORS-CARGO DOOR/HSDR DXTA2025011501953Unknown · vibrationINFLIGHT VIBRATION (EXCEPT ENGINE): DURING DESCENT WITH AUTOPILOT ON WHILE PASSING THROUGH 25000FT AND 310KIAS, WE OBSERVED A NOTICEABLE VIBRATION THROUGH BOTH YOKES. THIS VIBRATION CONTINUED THROUGHOUT THE REST OF THE DESCENT AND WAS MOST PRONOUNCED ABOVE 25SDR SWIA202501160011Seal · damagedTRANSFER FROM EAML 1506706 : TRANSFERRED FROM CAMP 29417867. REF AML# 1498041: DUE TO BIRDSTRIKE DAMAGE, RH INTERCOSTAL AT BL6.10 P/N: 600-33011-68, REF , AL ALY ALCD 2024-T42, 0.032€? NOM. THK., REF IS DAMAGED. DAMAGE IS A DENT: 1.00€? L X 0.250€? W X 0SDR IPXA2025011345538Screw · missingPANEL SURROUND FOR EMERGENCY ESCAPE DESCENT DEVICE HAS MISSING SCREWS. INSTALLED FASTENERS PER AMM 20-51-01
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