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 UIEA2026013000024Junction Box · corrodedJUNCTION BOX COVER FOR RIGHT HAND BODY GEAR HAS CORROSION ON LOWER EDGE.(<P>REPAIRED AREA OF CORROSION ON RH BODY GEAR LOWER EDGE OF JUNCTION BOX PER SRM 51-70-13-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026013000025Junction Box · corrodedJUNCTION BOX COVER J15, FOR LT BODY GEAR HAS CORROSION ON LOWER EDGE. REPAIRED CORROSION OF THE J15 JUNCTION BOX OF THE LT BODY GEAR IAW SRM 51-70-13-2R-1. NO FURTHER DFECTS NOTED.SDR FDEA202602050133Floor Panel · dentedMIAN DECK CARGO COMPARTMENT, FLOOR PANEL 251LFF DENTED. JM40 FABRICATED NEW FLOOR PANEL 251LFF, MPN: 146T5869-127, LBL 11- RBL 11, STA 1208-1351 IN REF. TO BOEING DWG 146T5869-127, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR.SDR JJBA20260220069Rivet · brokenBAGGAGE DOOR STRUCTURE UNDERNEATH LIFTING ROD ATTACHMENT POINT IS DISTORTED AND CRACKED, AT LEAST 1 RIVET BROKEN. REPAIRED BAGGAGE DOOR STRUCTURE UNDERNEATH LIFTING ROD ATTACH POINT.SDR DALA2026012600550Not Reported · not reportedPERFORM ER/A 586145-14AD REV D FOR REPLACEMENT OF FR16 LT IN PASSENGER CABIN. ER/A 586145-14AD REV D, APPROVED DATE: 23/JAN/26 WAS VERIFIED AGAINST ER/A 586145-14AD REV D PRI REV 0 AND WERE FOUND INCOMPLIANCE WITH THE SCOPE OF THE WORK ACCOMPLISHED, STEP RELASDR AALA202601260827Unknown · vibrationAIRCRAFT WAS GROUNDED: AIRPLANE HAS VIBRATIONS DURING CLIMB OUT. SEEMED TO STOP AROUND FL23,000 AND SPEED 330. NOT ACTIVE DURING CRUISE OR DESCENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTTED** (OPEN)SDR DALA2026012200495Unknown · vibrationDIVERTED TO SYR DUE TO AIRFRAME VIBRATIONS IN FLIGHT. PERFORMED AIRFRAME VIBRATION INSPECTION PER AMM. PERFORMED IDLE ENGINE RUN WITH BOTH VIBRATION INDICATIONS WITHIN LIMITS. OPS CHECKS NORMAL.(7787876)SDR 2026FA0000046Frame · crackedDURING MAINTENANCE INSPECTIONS AT IAI FACILITIES, SHOP FOUND A CRACK IN ENGINE #1 INLET COWL AFT BULKHEAD OUTER FRAME FLANGE, BETWEEN 11 O'CLOCK AND 12 O'CLOCK. WORK PERFORMED IAW REA NO: MF03036R0235.SDR AALA202601127496Unknown · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAX DUE TO THE FLIGHT CREW REPORTING THAT INFLIGHT VIBRATIONS FELT FROM ABOUT 13,000 THROUGH CLIMB OUT 30,000 FEET APPROX SPEED 340. VIBRATION WAS FELT ON LEFT SIDE ON BOTH RUDDER PESDR CALA2026010612705Protector · damagedFOUND DAMAGE TO AFT EDGE PROTECTOR. REF ECRA 5308-01193. PERFORMED INTERIM REPAIR PER STEP 1. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR CALA2026010512652Structure · contaminatedDUE TO THE AMOUNT OF STANDING WATER AND ICE, INSPECTION OF THE FORWARD BILGE ARE IS NEEDED PER TRM ECRA 2011-01000. PARTICULARY BETWEEN BS 600 & 900. WITH WATER LEAK ORIGINATING BEHIND RT CARGO WALL LINER AT BS 800. SUPPLIED HOT CONDITIONED AIR WITH APU TO THESDR YENA2025123001310Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN HOLE C LOCATED IN DOUBLE JOGGLE AREA FR16 LH SIDE. CRACK DIRECTION IS 3 OCLOCK LOOKING OUTBOARD. CRACK DEPTH IS 0. 080 INCHES APROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED OSDR YENA2025123001309Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN HOLE B LOCATED ON DOUBLE JOGGLE AREA FR16 LH SIDE. CRACK DIRECTION IS 3 OCLOCK LOOKING OUTBOARD. CRACK DEPTH IS 0. 120 INCHES APROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED OSDR YENA2025123001308Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 R H SIDE. CRACK DIRECTION IS 3 OCLOCK LOOKING OUTBOARD. CRACK DEPTH IS 0 .130 INCHES APROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVEDSDR CALA2025123012546Unknown · vibrationACFT DIVERTED TO EWR FOR VIBRATION IN MID GALLEY 3. CREW STATED VIBRATION FELT BETWEEN DOORS 2L & R. VIBRATION BEGAN AT CRUISE & CREW REPORTED IT INCREASED & DECREASED WITH AIRSPEED. VIBRATION STOPPED AFTER LANDING WHEN THRUST LEVERS RETURNED TO IDLE. HAS HSDR FDEA202512262291Structure · damagedWHILE UNDERGOING EXTENSIVE STRUCTURES REPAIR FOR IMPACT DAMAGE TO BS 368 - 478, S35 - 38L ACFT SUSTAINED MAJOR FIRE DAMAGE DURING REPAIR WITH ROOT CAUSE CURRENTLY BEING INVESTIGATED. MAJOR REPAIR. COMPLIED WITH EA H-5310-T0383765. MAJOR REPAIR AFTER FWD CASDR DALA2025122209322Repair · not reportedIN REFERENCE TO AMDS 5311-01227-02B STEP 2 , EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1360 STR 26RH. CORRECTIVE ACTION: SUMMARY OF NRC 00054: REPAIR WAS ACCOMPLISHED ACCORDANCE ER/A 538373-14 AD . REV A. SECTION I. (1360222)SDR DALA2025122209321Repair · not reportedIN REFERENCE TO AMDS 5311-01227-02B STEP 2 , EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT BS 1300 AT S26R. REPAIR WAS ACCOMPLISHED IAW ER/A 538382-14.AD, REV A .SECTION I. (1360209)SDR YENA2025122201246Unknown · vibrationFLT#147, EWR-SJU. "DURING CRUISE #1 FA CALLED STATING LOUD HUMMING NOISE AND VIBRATION IN CABIN FLOOR NEAR ROW 13. CA INVESTIGATED AS WELL. NO OTHER INDICATIONS ON SYSTEMS. PAGE POSSIBLE LOOSE PANEL OR FAIRING SEAL" (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR MASA20260116002Seat Track · corrodedDURING THE C-CHECK, IDENTIFIED CORROSION ON THE FWD FUSELAGE FLOOR STRUCTURE INBOARD SEAT TRACK FRAME13 TO 20. CORRODED SEAT TRACK AT FWD FUSELAGE RT INBD SIDE, FR 13 - 20, REMOVED AND REPLACED IAW SRM 51-41-01, 51-43-03, AND 51-43-04.SDR CALA2025121512082Structure · corroded"CORROSION" AT FWD WET AREA STA328 RBL50 INNER CHORD DOT EV11 REF AAR N/R 99978986 INSTALLED NEW INNER CHORD AT FWD WET AREA STA328 RBL50 IAW B737-800 SRM 51-40-02-0G-0 AND DWG# 141A8310. REMOVED AND REPLACED INNER CHORD AT FWD WET AREA STA328 RBL50 IAW B73SDR VNAA202512020050Washer · corrodedF.S 280 LH LOWER BULKHEAD @ LBL 9 HAS SEVERE INTERGRANULAR CORROSION CAUSING LOWER WEB CLOSE OUT ANGLE TO BE PUSHED OUT. 670-53-11-594-1 WEBSDR VNAA202512020049Washer · damagedRFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00557371, SO# 400382749 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7 WASHERSDR VNAA202512020048Washer · damagedPER CUSTOMER REQUEST, SUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00557370, SO# 400382748 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7). CC670-10635-7 WASHERSDR CALA2025113011585Unknown · smokeSMOKE REPORTED FROM WHEEL WELL AREA BY AIRCRAFT BEHIND AND OPS INSPCT ALL LANDING GEARS AND CACS INLETS OUTLETS AND SURROUNDING AREA. NO SIGNS OF OVERHEAT OR FIRE. NO INDICATIONS OF OVERHEAT IN CABIN. NO FLUCUTATIONA OF PACKS APU OR ANY OTHER SYSTEMS. COULD NOSDR CALA2025112811568Unknown · unknownLOUD NOISE SOUNDED LIKE TIRE BLOWN AFTER TAKE OFF. ALTITUDE 600 FEET LANDING GEAR UP FLAPS 1 PERFORMED WAK AROUND , NO BIRD STRIKE , NO TAIL STRIKE , NO MISSING PANELS , WHEELWELL AREAS NORMAL , HYD SYSTEMS NORMAL , NO FLAT TIRES , NO BAD TIRES , FLT CONTROL OSDR DALA2025113008739Structure · damagedINSPECTION ERA 630590-14AD REV ORIGINAL. REPAIR PART AND HORIZONTAL FLANGES FILLET RADII REQUIRE FOLLOW ON INSPECTIONS PRIOR TO 60,130 TFC AND EVERY 16,200 FC, THEREAFTER. ACCOMPLISH FOLLOW ON INSPECTIONS PER ERA 630590-14AD SECTION II PRIOR TO 60,130 TFC AND SDR FDEA202511182189Structure · no discrepancyWE HEARD A LOUD BANG IN FLIGHT AT THE TOP OF DESCENT. THE SAME NOISE OCCURRED SEVERAL MORE TIMES AT THE BEGINNING OF EACH DESCENT. UPON INSPECTION AFTER LANDING, THE DEMI CAN IN POSITION 7D WAS NOT PROPERLY SECURED AND IT WAS SLIDING BACK AND FORTH DURINGSDR QXEA2025112000346Structure · damagedFLIGHT 2431. ON DESCENT NEAR 10,000' MSL LIGHT TO MODERATE TURBULENCE AND PRECIPITATION. ONE MAJOR BANG (NOISE) HAPPENED WITH A FLASH, FOLLOWED BY 2-3 SUBSEQUENT FLASHES WITH NO BANG OR NOISE, AND A BURNED ODOR LASTED ABOUT 5 SECONDS ONLY IN COCKPIT, BUT CABINSDR QMLA2025111020113Structure · damagedBIRD STRIKE WITH POSSIBLE MULTIPLE BIRDS RESULTING IN DAMAGE TO SEVERAL AREAS ON THE AIRCRAFTSDR DALA2025111108261Panel · inflt separationUPON LANDING, PANEL 149 BL DEPARTED AIRCRAFT. TEMP REPAIR PER ERA 630421 REV. ORIG (7972140)SDR QXEA2025103100336None · no discrepancyFLIGHT 2134. BIRD IMPACTED AIRCRAFT JUST ABOVE FO (RIGHT) WINDSHIELD. LOUD BANG/ SOLID IMPACT. OCCURRED AT APPROX 800 FT AGL ON TAKEOFF. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REMOVED FROM SERVICE. CLEANED AREA OF IMPACT AND PERFORMED INSPECTSDR IXXA20251026004Structure · crackedINNER CHORD STA 859.5 RBL 89 WL 200 CRACKEDSDR QXEA2025102700333Structure · no discrepancyFLIGHT 2264. BIRD STRIKE ON TAKEOFF ROLL, LARGE BIRD ABOVE WINDSHIELD. APPROXIMATELY 100 KTS. REJECTED TAKEOFF. REMOVED FROM SERVICE. INSPECTED FUSELAGE ABOVE WINDSHIELDS AND DID NOT SEE ANY EVIDENCE OF A BIRDSTRIKE. NO SNARGE OR DENTS NOTED. ALL OTHER ARESDR DALA2025102207710Not Reported · crackedA CRACK WAS FOUND AT HOLE 263 RH. REPAIRED PER ERA 629510-14. (1264152)SDR DALA2025102207709Not Reported · crackedCRACK WAS FOUND AT HOLE 260 RT. REPAIRED PER ERA 629510-14. (1264149)SDR DALA2025102107678Not Reported · corrodedBULK CARGO SECTION LONGITUDINAL CORROSION AT Y480 FR68-FR69. REPLACED PER A330 SRM 51-72-11-911-001. (1263316)SDR DALA2025102107677Not Reported · corrodedBULK CARGO SECTION LONGITUDINAL CORROSION AT Y0 FR69. REPLACED PER A330 SRM 51-72-11-911-001. (1263309)SDR CALA2025102110354Structure · no discrepancyBIRD STRIKE ON ROTATION IN KMKE. ABOVE FLIGHT DECK. CLEANED BIRDSTRIKE IN REFERENCE TO AMM 12-40-04. PERFORMED BIRD STRIKE INSPECTION IN REFERENCE TO AMM 05-51-18. ONLY SINGLE IMPACT OCCURED APPROXIMATELY 2 FEET ABOVE CAPTAINS WINDOW. NO OTHER IMPACTS FOUND ONSDR IPXA2025100926914Panel · crackedPANEL 831AZ CRACKED (2 LOCATIONS).CLEANED AND PREPARED PANEL FOR ALLOWABLE REPAIRS. IAW SRM A300-600 51-77-11 PARA 3 A.1.REPAIRED PANEL WITH 08-090, BATCH 4354723. IAW SRM A300-600 51-77-11 PARA 3.A.2-7. REVIEWEDSDR ABXA202509176229Unknown · vibrationAFTER ENGINE START, UNUSUAL AIRFRAME VIBRATION. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED FLT CONTROL CHECK IAW AMM 27-00-00, NO DEFECTS FOUND. ADDED MORE FUEL TO AIRCRAFT AND PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00 OPS GOOD, NO VIBRATION NOTED. AFSDR FDEA202509111685Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251HFF GOUGED. JM26 REPAIRED MAIN CARGO COMPT. DAMAGED AREAS AT STA.1197 22-1260 LBL 33-54.75 PNL# 251HFF MPN: 146T5869-143 TOPSKIN OF FLOORBOARD. IN REF. TO 767 SRM 53-00-50-2R FIG. 201 SHEET.2 REPAIR#: 1. SEE JPF SDR ASAA2025091061086Landing · gougedPANEL 193B RT SIDE OTBD, PANEL LANDING GOUGED. GROUNDED - YES. REMOVED & REPLACED PANEL 193 RT SIDE OTBD PANEL LANDING IAW SRM 51-40-02-0G-0.SDR IPXA2025091500931Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.93. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.93 AND B0EING DWG NO 146T5650 SHEET 5 REV C.SDR CALA2025091208820Cover · missingFLT INPH JACK IN THE NOSE WHEEL WELL IS MISSING THE COVER. COVER HAS DEPARTED THE A/C.SDR FDEA202509091675Seat Track · corrodedCABIN SEAT TRACK AT B.S 770 RBL 58.22 WITH CORROSION. TRIMMED, LOCATED AND DRILLED NEW SEAT TRACK MAIN CABIN STA 660-880 RBL 58.22 IAW B757 SRM 51-40-05-0G, 51-40-08-0G BOEING DWG # 657N3332 REV A. INSTALLED MAIN CABIN NEW SEAT TRACK FROM STA 660-880 RBL SDR IPXA2025092267597Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-17L PERFORM EO-95208-REQ1 REV.1 AND EI NO.F2025A53M-2194 AND EGAT WORK SHEET NO. 50699. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS.SDR DALA2025090906647Access Panel · puncturedPUNCTURE ON ACCESS PANEL 192KB AT LOWER FUSELAGE. COMPLIED WITH ER/A 524189-14. (1188635).SDR UIEA2025090401155Rivet · damagedSTA 200 STR 31AL L/H 1 EA RIVET FOUND LIGHTNING STRIKE. STA 200 STR 31AL L/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS REPAIR IS CATEGORY C REPAIR. NO FURTHER DEFECTS NOTED.SDR UIEA2025090401156Rivet · damagedFX - STA 200 STR 23-24A R/H 1EA RIVET FOUND LIGHTNING STRIKE. STA 200 STR 23-24A R/H 1EA RIVET HEAD LIGHTNING STRIKE REPAIRED IAW SRM 53-00-01-2R-9 REPAIR 9 SECTION II STEP 4, BLIND FASTENER REPAIR. THIS REPAIR IS CATEGORY C REPAIR. NO FURTHER DEFECTS NOTED.
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