JASC 5300
Service difficulty reports · 8,206
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 DALA2022063004557None · noneSHIP 664 DENT ON FRAME STA 1380 S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00260: DENT ON FRAME STA 1380 S-26L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2296451)SDR SWIA202265972None · smokeD:WHILE SITTING AT THE GATE,SMOKE STARTED ENTERING THE COCKPIT ON THE RIGHT SIDE. THE SMOKE HAD AN ELECTRICAL SMELL . CREW EVACUATED THE PLANE.IMMEDIATELY AND AND AIRCRAFT WAS SHUTDOWN / C:ON ARRIVAL TO A/C CREW NOTED SMOKE WAS COMING FROM F/O'S SIDE WALL VENTSDR CALA2022062801597Floor Support · corrodedSUPPORT TASK: MAIN CABIN STA 300 RBL 18-34 INTERCOSTAL HAS CORROSION ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NRC 9282557 REMOVED AND INSTALLED NEW SUPPORT IAW BAC DWG 141N5160 AND SRM 5 1-40-02, SRM 51-40-05. CREATED SDR #1028928. HAECO GSO MECH V9 014SDR EVCA062722None · crackedTHERE IS AN APPROX. 4.5 INCH CRACK ON THE HORIZONTAL STABILZER UPPER INBOARD RH SIDE.SDR CALA2022062701590Flange · crackedMAIN CABIN FWD WET AREA FUS FRAME FLANGE CRACKED ABOVE L-1 DOOR CUTOUT AT STA 312.INSTALLED REPAIR AT MAIN CABIN FUS FRAME FLANGE ABOVE L-1 DOOR CUTOUT STA312 STR 5L. REQUIRE RE-INSPECTION THRESHOLD 50,000 TOTAL F/C OR 12,000 F/C AFTER REPAIR INSTALLATION WHICSDR GTIA2022062736496None · noneELECTRICAL SMOKE OTHER FWD GALLEY ON APPROACH -PERFORMED INSPECTION OF FWD GALLEY IAW TSM 05-50-00-810-831-A. NO DEFECTS NOTED AT THIS TIME A/C OK FOR SVCSDR FDEA202206251701Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 17 , Y 450 REMOVED DAMAGE PARTS & NEW TRACK INSTALLED WORK INSTRUCTION IAW A600-600 SRM 51- 40-21-001 PARA.6 , PAGE.7B-23 & SRM 51-76-20-201 PARA.4E , PAGE.210~211 , FIG.204.SDR FDEA202206251549None · noneAGING AIRCRAFT - EXISTING DOUBLER FOUND AT UPPER TORQUE BOX WEB STATION 2020 BETWEEN X = - 6.950 TO X = - 15.250.SDR FDEA202206241581None · noneREPAIR ASSESSMENT: R/H FUSELAGE STATION 1160-1329, L46R-L48R, HAS EXISTING REPAIR FOR LIGHTNING STRIKE DAMAGE. REF. DOT #56. LIGHTENING STRIKE REPAIRED PER LUFTANSA ENG. EI-53-0241, AND SRM 53-00-01-2R-6.SDR FDEA202206241702Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 15C , Y 950 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE.2 & 51-40-21- 001 PARA.6 , PAGE7B-23.SDR FDEA202206241700Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 12A 2" , Y 700 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE.2 & 51-40-21- 001 PARA.6 , PAGE.7B~23 .SDR JJBA20220624031None · noneAT REAR FUSE II EXT, SUSPECTED CRACKS (9X) FOUND ON RIGHT SIDE SKIN BTW FR 77 - FR 78 AND BTW STR 3R - 9R. REPAIR DOUBLER ON RH REAR FUSE 2 SKIN, ON FR 78 BTW STR 5R-7R. EXTERNAL DETAILED VISUAL INSPECTION, AT REPAIR, INTERVAL OF 30000 FCSDR Y2PA2022062422036Angle · corrodedDISCREPANCY: WHILE AT C-CHECK AT COMMERCIAL JET IN KDHN A FLOOR BEAM UPPER ANGLE WAS FOUND CORRODED IN MULTIPLE PLACES IN THE AFT
CABIN @ F.S. 1338 RBL 24- RBL 44
CORRECTIVE ACTION: COMMERCIAL JET IN KDHN REMOVED CORROSION FROM THE FLOOR BEAM UPPER ANGLE ATSDR Y2PA2022062422035Floor Panel · corrodedDISCREPANCY: WHILE AT C-CHECK AT COMMERCIAL JET IN KDHN, A FLOOR PAN WAS FOUND CORRODED AT DRAIN HOLE IN THE MAIN CABIN
AT F.S. 207 LBL-50
CORRECTIVE ACTION: COMMERCIAL JET IN KDHN REMOVED THE CORROSION AT MAIN CABIN F.S. 207 LBL-50 IAW MD80 SRM 51-10-3 ANDSDR GTIA2022062736494None · noneL1,L2,R1 AND R2 DOOR ASSIST REQUIRE NITROGEN SERVICE-SERVICED L1,L2,R1 AND R2 DOOR ASSIST BOTTLES PER AMM 52-10-00. LEAK CHECK GOODSDR SCNA20220705075SUFlange · corrodedSUPPLEMENTAL: CORROSION AT FLOOR SUPPORT UPPER CHORD FLANGE. CAUSE OF CORROSION: MOISTURE.SDR JJBA20220623032None · noneAT REAR FUSE II EXT, SUSPECTED CRACKS (14X) FOUND ON LH SIDE SKIN BTW FR 77-80 AND BTW STR 3R-9R. 7 BUSHING REPAIRS ON LH REAR FUSE 2 SKIN, AT FR 77-79 AND BTW STR 3L-9L. EXTERNAL GVI, AT REAPIR, INTERVAL OF 9000 FCSDR COEA2022090606921Fitting · damagedWO 240087 NR 8 HEAVY CHECK COE/MAJOR REPAIR: TWO FASTENER HOLES COMMON TO L/H NODE 3 SILL AND UPPER FITTINGS HAVE FLAW INDICATION. REPAIR PER SRAS ES_0163526_01...19446 ISSUE A, DATED 9/6/2022.SDR SWIA202266375None · corrodedCENTER FUSELAGE III SKIN CORRODED UNDER FRAME 82 SHEAR CLIP STRINGER 27R/28R. (C-CHECK RO 8/29/2022) / CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED CUTOUT, FILLER, INNER AND OUTER DOUBLER REPAIR REF SRM 53-23-01/REPAIR13P. SEE CONTINUATION CARD FOR WSDR SWIA202266374None · corrodedCOCKPIT RH FLOOR STRUCTURE DOUBLER CORRODED AT SEVERAL AREAS AS MARKED (C-CHECK RO 8/29/2022) / PERFORMED REPAIR OF COCKPIT RH FLOOR STRUCTURE DOUBLER REF ETD2022-170-021607. 102.4 GRAMS ADDED FROM REPAIR, NO CHANGE TO WEIGHT AND BLANCE REQUIREDSDR SWIA202266373None · corrodedCOCKPIT LH FLOOR STRUCTURE DOUBLER CORRODED AT SEVERAL FASTENERS AS MARKED (C-CHECK RO 8/29/2022) / REPAIRED COCKPIT LH FLOOR STRUCTURE DOUBLER BY SPLICING A NEW SECTION IN FROM FR 7 TO FR 12 AND RESTORED SURFACE PROTECTION REF ETD 2022-170-021533SDR SWIA202266309None · corroded*RH PRESSURE FLOOR SILL MEMBER FROM FS409.0+128-FS559 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 8/15/2022) REMOVED CORROSION ON RH PRESSURE FLOOR SILL MEMBER (15 LOCATIONS) FROM FS409+128 TO FS559 AND FOUND THEM WITHIN LIMITS REF. REO 601R-53SDR SWIA202266308None · corroded*LH PRESSURE FLOOR SILL MEMBER FROM FS409.0+128-FS559 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 8/15/2022) REMOVED CORROSION ON LH PRESSURE FLOOR SILL MEMBER FROM FS409+128 TO FS559 ON MULTIPLE AREAS OF CORROSION AND FOUND THEM WITHIN LIMITSSDR 2022FA0000306None · usedTHE DAVID CLARK DC PRO-X HEADSET IS CLAIMED TO BE FAIL-SAFE IN THAT COMMUNICATION IS NOT INTERRUPTED WHEN THE NOISE CANCELLING FEATURE LOSES POWER, FOR EXAMPLE WHEN THE BATTERIES ARE DEPLETED. I DISCOVERED THAT MY HEADSET ONLY PASSES AUDIO AT AN EXTREMELY LOW SDR 2022F00271None · noneCO-PILOT HEARD A POP UNDER SEAT AND A PLUME OF SMOKE AROUND HIS LEFT KNEE BY THE DASH.SDR CALA2022062201552Door Sill · corrodedR2 DOOR SILL AND FWD FR68 AROUND GIRT BAR FITTING HAVE 2 AREAS W ITH CORROSION RED MARKED GEN BY V061682 NR9291027/27027 RMVD AND RPLD R2 DOOR SILL FR68 IAW SRM 51-72-12 BY MECH V061742 INSP BY V061334SDR HNAA2022071800238None · noneE920543 - CORROSION ON DIAMOND GUSSET AT FRAME 22 GALLEY AREA .... REMOVED AND REPLACED DIAMOND GUSSET AT FRAME 22 GALLEY AREA IAW EMB 145 SRM 51-40-02SDR FDEA202206201615None · noneTHE LOWER FUSELAGE SKIN WAS FOUND CHAFFING AT FR66 STR 51-52R LOWER AREA WITH MARK. CUT OUT THE DAMAGE AND INSTALLED THE FILLER AND REPAIR DOUBLER, THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 53-10-12-201 PARA.6 PAGE.357-360 FIG.225 (SHEET.3), SRI:53-10-12- SDR JJBA20220620028None · noneFR 25 CRACKED SIDE BEHIND RH SILL BTW STR 15R-16R. EXTENDED SPLICE REPAIR ON RH CENTER FUSE 2 FRAME 25, BTW STR 14R-16R. INTERNAL DETAILED VISUAL INSPECTION, AT REPAIR, INTERVAL OF 10000 FCSDR JJBA20220620027None · noneSHEAR CLIP FOUND CRACKED AT RH FR 68 BTW STR 6-10. SHEAR CLIP AT FR 68 RH BTW STR 6-10 REPLACED WITH MADE REPAIR PART AND MASTER PARTSDR JJBA20220620017None · noneCENTER FLOOR SUPPORT GUSSET CORRODED BTW FRA 59 & 61. REPAIR DOUBLER ON CENTER FUSE 4, ON CENTER OMEGA BEAM BTW FR 60-61SDR CALA2022062201546Skin · damagedABM CLEANING TRUCK HIT FUSELAGE AT 3 FEET BELOW DOOR 4 LEFT, PUTTING A HOLE IN THE FUSELAGE. DAMAGE IS 2 AND 1/4 INCH HORIZONTAL BY 1 INCH VIRTICAL. SHOULD READ PUNCTURE IN FUSELAGE. PUNCTURE IS LOCATED IN SECTION 47, STATION 1768, STRINGER 29L. BEHIND DAMAGE SDR JJBA20220620008None · noneSHEAR CLIP FOUND CRACKED AT FR 71 LH BTW STR 6-10. SHEAR CLIP AT FR71 LH BTW STR 6-10 REPALCED WITH MADE REPAIR PART.SDR 2022FA0000304Propeller · departedON 6/19/2022 ONE OF THE BLADES FROM A 2 BLADED CONSTANT SPEED MT PROPELLER ON WACO CLASSIC AIRCRAFT CORP GREAT LAKES S/N 1207 DEPARTED THE AIRCRAFT IN-FLIGHT. THE AIRCRAFT MADE A SAFE EMERGENCY LANDING WITH NO INJURIES. THE AIRCRAFT IS LOCATED IN STELLAR, AZ.SDR 2022F00266Pressure Switch · unserviceableFUEL FILTER CAUTION LIGHT ILLUMNATED ON TAKEOFF.SDR 2022F00265None · noneDURING RT ENG START, NO N2; NO START VALVE; NO ROTATION VERIFIED ON GRIND. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE RE-SECURED CANNON PLUG ON START VALVE IAW B767 AMM 20-60-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR V0XD20220620002None · noneBL 0 FRAME GUSSET HAS SIGNS OF CORROSION AROUND NUTPLATE HOLES FROM FR 60- FR 62. CORRECTIVE ACTION : REMOVED DAMAGED GUSSET AND INSTALLED NEW GUSSET ( P/N: 145-22226-003) AT BL 0 IAW EMB 135/145 SRM 51-40-02.SDR SWIA202266304None · dented*EVALUATE DENTS ON EXTERNAL SKIN BETWEEN FS 589.00 - 605.00, STGR 23L - 24L (C-CHECK RO 8/15/2022) / EVALUATED DENTS ON EXTERNAL SKIN BETWEEN FS 589.00 - 605.00, STGR 23L - 24L. FOUND TO BE OUT OF LIMIT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED RSDR FDEA202206181632Floor Panel · dentedAT THE TIME OF AGING AIRCRAFT INSPRCEION,FOUND FLOOR PANEL 162HF HAS SEVERAL IMPACT DAMAGES IN THE BULK COMPARTMENT. MEASURED THE SEVERAL DAMAGES WITHIN REPAIRABLE LIMITS AND FILLED WITH FILLER I.A.W A300-600 S.R.M 53-10-20-201 PARA .10A , PAGE. 212-213 , SDR JJBA20220617007None · noneLH FLOOR GUSSET FR 24-38 LBL 18 HAS CORROSION SEVERAL AREAS BETWEEN AND AROUND TRACKS. REPLACED FLOOR GUSSET FR 24-29, FR 36-39SDR CALA2022062001532Door Sill · corrodedL-2 DOOR SILL I/B FR 68 AREA HAS EVIDENCE OF CORROSION. GENERATE D BY V052040 ON HAECO LCQ NR 9290696/26696 REMOVED AND REPLACED L-2 DOOR SILL FR 66-68 IAW A320 SRM 51-72-1 1 ACMP BY MECH V080280 INSP BY V061682SDR 2022FA0000297Fitting · shearedINSTRUMENT PANEL DROP DOWN FITTING SHEAREDSDR JJBA20220616005None · noneCO-PILOT SEAT TRACKS HAS SIGNS OF CORROSION ON GUSSET. REMOVED DAMAGED DOUBLER SHEET FLOOR AND INSTALLED NEW DOUBLER SHEET FLOOR AT CO-PILOT FLOOR O/B GUSSETSDR CALA2022061701521Floorbeam · corrodedB767-53-3-7002 CABIN STA303 LBL24 TO 54 FLOORBEAM FOUND CORROSION TRANSFER REF HXWO 822811 AND ORIGINATED BY EMP V897790 CABIN STA303 LBL46" TO LBL54" FLOOR EAM CORROSION BLEND OUT REPAIR 1 FIG.201 ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO ITEM33 AREA REMAIN 0.0SDR 2022FA0000294None · shearedINSTRUMENT PANEL DROP DOWN FITTING SHEARED.SDR K11A2022072900152Doubler · dentedEXTERNAL FUSELAGE DOUBLER DENTED AT STA 344-360 BETWEEN STR 16R AND 18RSDR JJBA20220615006None · noneSIGNS OF CORROSION AT FR58 STR 20R STRINGER HAS SIGNS OF CORROSION. REMOVED AND REPLACED STRINGER AT FR58-60, STR 20R. NO DEFECTS NOTED AT THIS TIME.SDR FDEA202206141635Floor Panel · dentedAT THE TIME OF AGING AIRCRAFT INSPRCEION,FOUND FLOOR PANEL 161GF HAS SEVERAL IMPACT DAMAGES IN THE BULK COMPARTMENT. MEASURED THE SEVERAL DAMAGES WITHIN REPAIRABLE LIMITS AND FILLED WITH ADHESIVE I.A.W A300-600 S.R.M 53-10-20-201 PARA.10A , PAGE.212-213 , SDR CALA2022061501506Skin · chafedB767-53-3-0197 - EMP FUSELAGE STA 1815 RH HORI. STAB BLADE SEAL FAIRING UNDER SKIN FOUND CHAFING - TRANSFER REFER NON-ROUTINE WO.779908 - AND ORIGINATED BY EMP V896810 FX - RH HORI STAB BLADE SEAL FAIRING UNDER SKIN STA 1809 - STA 1822 WL 235 PERMANENT REPAIRESDR 2022FA0000296Fitting · shearedINSTRUMENT PANEL DROP DOWN FITTING SHEARED
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