Boeing 767-323
Service difficulty reports · 8,544
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '767323' 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 aircraft_model_key = '767323' 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 MK1Y20212804009Skin · dentedDURING MAINTENENCE INSPECTION FOUND THREE (3) DENTS ON EXTERNAL FUSELAGE SKIN BETWEEN DOOR STA 111 AND DOOR STA 129, BETWEEN STR 7L AND 9L.SDR MK1Y20212804008Skin · scratchedDURING MAINTENENCE INSPECTION FOUND SEVERAL SCRATCHES ON EXTERNAL FUSELAGE SKIN COMMON TO FASTENERS ZONE AND LARGE CARGO DOOR CUTOUT.SDR MK1Y20212804007Keelbeam · damagedDURING MAINTENENCE INSPECTION FOUND DAMAGED HOLE ON KEEL BEAM, STA 720, RBL 9.5SDR MK1Y20212804006Skin · damagedDURING MAINTENENCE INSPECTION FOUND GOUGES, NICKS AND SCRATCHES ON FWD EDGE OF BULK CARGO DOOR CUTOUT, SEC 46, BETWEEN STA 1395 AND STA 1471, STR 26L TO STR 31L.SDR MK1Y20212804005Skin · damagedDURING MAINTENENCE INSPECTION FOUND A SCRATCH EXTERNAL FUSELAGE SKIN, STA 1395, STR 26R.SDR MK1Y20212804004Skin · damagedDURING MAINTENENCE INSPECTION FOUND GOUGES AND SCRATCHES AT TREE (3) LOCATION UNDER THE LH PASSENGER AFT ENTRY DOOR CUTOUT, DOOR STA 889 - 991, STR 20L -22L.SDR MK1Y20212804003Keelbeam · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION ON KEEL BEAM SPLICE FITTING IN FOUR (4) PLACES.SDR MK1Y20212804002Frame · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION IN MAIN DECK FRAME OUTBD CHORD FREE FLANGE AT STA 1285, STR 17R.SDR MK1Y20212804001Frame · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION IN MAIN DECK FRAME OUTBD CHORD FREE FLANGE AT STA 1373, STR 17RSDR IXXA20210418015Flashlight · not reportedDEFERRAL MAINTENANCE ITEM #21961 INITIATED. AIRCRAFT RELEASED TO SERVICE.REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT IAW B767 AMM 25-60-00. THIS CLEARS DEFERRAL MAINTENANCE ITEM 21961. NO FURTHER MAINTENANCE ACTION REQUIRED. AIRCRAFT RELEASED TO SERVSDR NACA2021041600004Pump · leakingMAINTENANCE DISCOVERED #2 ENGINE FUEL PUMP LEAKING DURING WALK AROUND. REPLACED FUEL PUMP IAW AMM 73-11-01 . ETOP'S SS, ETOP'S GROUND VERIFICATION CHECKED GOOD.SDR NACA2021041600003Shaft · shearedDURING ENGINE RUN OPERATIONAL CHECK FOR IDG REPLACEMENT, NO GENERATOR OUTPUT. REPLACED IDG DUE TO SHEARED SHAFT IAW AMM 24-11-01, OP AND LEAK CHECK IAW 71-00-00, NO LEAK NOTED AND OP CHECK GOOD. ETOP SS'SSDR NACA2021041600002Idg · leaking#2 ENGINE IDG HAS EVIDENCE OF LEAKAGE. REMOVED AND REPLACED INTEGRATIVE DRIVE UNIT IAW AMM 24-1104, OPS AND LEAK CHECK GOOD. ETOPS SS'S.SDR NACA2021041600001Relay · failedHYDRAULIC CENTER VALVE STATUS MESSAGE. REPLACED K858 L AC BUS OFF SENSE RELAY PER SWPM 20-81-14 WDM 24-25-11. OP CHECK NORMAL.SDR IXXA20210402999Tension Tie · not reportedCOMPLY WITH FVCI #21011-5 FABRICATION TENSION FITTING REAR SPAR BULKHEAD 100T1432-3. FABRICATED CENTER WING TENSION FITTING PN-100T1432-3 PER FA BAS 21019 REV 1R, FVCI EO 21011-5 REV B AND 8110-3 DATED 8 MARCH 2021.SDR MK1Y20210324012Skin · dented: LOWER SURFACE SKIN – R/H HORIZONTAL STABILIZER BETWEEN AUX SPAR AND FRONT SPAR MAINTENANCE HAS DISCOVERED TWO DENTS ON LOWER SURFACE OF R/H HORIZONTAL STABILIZER BETWEEN AUX SPAR AND FRONT SPAR. LOCATION AND A/Y RATIO OF THE DENTS: DENT 1: 5" FROM AUX SPAR SDR MK1Y20210324011Skin · damagedHORIZONTAL STABILIZER, L/H INB ELEVATOR HSBL 113.30: DURING THE MAINTENANCE WORK AT IAI, DAMAGE WAS CAUSED TO THE SKINS OF L/H INBD ELEVATOR (P/N 183T2001-33, S/N 00070) AT HSBL 113.30. THE DAMAGE OF APPROX. 10.0”X4.0” IS LOCATED IN CRITICAL AREA AS PER SRM 55SDR MK1Y20210324010Skin · dentedDURING MAINTANENCE INSPECTIONS AT IAI, FOUNDED LARGE DENT WITH GOUGE ON EXTERNAL FUSELAGE SKIN AT STA 1197+101 AND 2" BELOW STRINGER 9L.DAMAGED AREA CUT OUT 5.5"X3". THE CUT OUT IS 10" FROM LAP JOINT SKIN THICKNESS AT CUT OUT IS 0.056".SDR MK1Y20210324007Skin · corrodedSATCOM – FUSELAGE SKIN, SEC 45, STA 977 TO STA 1043, STR 2L TO 2R:
AS PER CUSTOMER REQUEST, SATCOM ANTENNA WAS DEACTIVATED AND DISMANTLED FROM A/C. EXISTIN COAX CABLE CUTOUT AND TWO BLEND OUT AREA SHOULD BE REPAIRED. SRM DOESN'T ALLOW SKIN REPAIR DOUBLER TO ESDR MK1Y20210324006Skin · corroded: CORROSION DAMAGE WAS FOUND TO THE R/H WING UPPER INNER SPAR SKIN PANEL NO.1 OVER WING FILL PORT ADAPTER AT WS 785.2, S-15 TO S-16 LOCATION.
AFTER CORROSION REMOVAL AT EACH OVERWING FILL PORT UPPER SKIN, THE AREA WAS INSPECTED:
1. NO CORROSION OR CRACKS WERSDR MK1Y20210324005Skin · corrodedDURING MAINTENANCE INSPECTIONS AT IAI, THE CORROSION DAMAGE WAS FOUND ON THE UPPER AFT SKIN (111T3017-1) OF CENTER WING WHEN EXCEEDS UNDER THE TENSION FITTING (100T1432-3). THE CORROSION ON THE UPPER SURFACE OF THE SKIN WAS BLENDED OUT PER SRM 51-10-02. THE MASDR MK1Y20210324004Skin · damagedDURING CONVERSION PROCESS, THE GLOBAL COMMUNICATION SUITE (G.C.S) ANTENNA WAS REQUESTED TO BE DEACTIVATED AND REMOVED FROM THE AIRCRAFT PER CUSTOMER REQUEST – PRODUCTION ORDER #13.
THE SKIN UNDERNEATH ANTENNA REQUIRES REPAIR DUE TO COAX PIERCE POINTS.SDR MK1Y20210324003Skin · damagedPROBLEM DESCRIPTION: REPAIR – FUSELAGE SKIN STA 474.5, STA 476, STA 615.5, STA 1346 AND STA 1373, STR 26R/36R (SECTION 43 & 46), SKIN PANEL P/N 143T3521-5, P/N 146T3531-3.
DURING MAINTENANCE INSPECTIONS AT IAI, EXISTING BLEND OUTS WERE FOUND ON THE R/H SIDE SDR MK1Y20210324002Skin · damagedMAINTEANCE REPORTED BLENDEOUT ON EXTERNAL FUSELAGE SKIN AT STA 1417-1429 STR 32L-34L.
THE BLENDOUT EXTENDS INTO FASTENERS AREAS. SRM 53-00-01 FIG 101 ALLOWABLE DAMAGE 1 DOESN'T PROVIDE DAMAGE LIMITS IN CLOSE PROXIMITY TO FASTENERS.SDR MK1Y20210324001Skin · damaged: MAINTEANCE REPORTED BLENDEOUT ON EXTERNAL FUSELAGE SKIN AT STA 1417 STR 29L-32L.
THE BLENDOUT EXTENDS INTO FASTENERS AREAS. SRM 53-00-01 FIG 101 ALLOWABLE DAMAGE 1 DOESN'T PROVIDE DAMAGE LIMITS IN CLOSE PROXIMITY TO FASTENERS.SDR 2DYA20210315000Relief Valve · failedDEPARTED FROM SPJC WITH A CREW OF TWO (PILOTS) AND NO PASSENGERS UNDER DAY TIME FLIGHT CONDITIONS. THE FLIGHT CREW REPORTED DURING CLIMB TO FL 380 THEY ENCOUNTERED AN EICAS STATUS MESSAGE CABIN ALT AUTO 2 MESSAGE. THE FLIGHT CREW SELECTED AUTO 1. THEY CONTINUESDR IXXA20210303013Battery Pack · inoperativePOST FLIGHT, FLASHLIGHT AFT OF P-61 PANEL INOPERATIVE. INITIATED DEFERRAL MAINTENANCE ITEM 21097 IAW MEL 25-63-04-01 CAT C NO FLY DATE 03/12/2021. REMOVED AND REPLACED BATTERY IN EMERGENCY FLASHLIGHT NEXT TO P-61 IAW AMM 25-60-00. OPERATIONAL CHCECK SATISFACTOSDR IXXA20210402333Skin · corrodedAFTER CLEANING INBOUND SIDE OF CENTER TANK AREA FOUND CORROSION ON UPPER SKIN AREA AT STA 952, BETWEEN 8 TO 12 INCH FROM FUSELAGE SKIN TO INBOUND SIDE. ACCOMPLISHED REPAIR ON CENTER WING SKIN AT STA 952 IAW FAS EA 21019 REV 1R, FVCI E0 21011-4 REV B AND 8110-3SDR IXXA20210225011Skin · crackedDURING ROUTINE OPERATIONS IN SMF. MAINTENANCE DISCOVERED A CRACK IN THE LEFT-HAND STA 952.65 UNDERWING FAIRING SKIN. THE SKIN IS MADE FROM 2024-T3 X 0.050” AND CLASSIFIED AS A PRIMARY STRUCTURE. A 22” DETAILED VISUAL INSPECTION (DVI) OF THE SURROUNDING STRUSDR MK1Y20210221039Skin · dentedDURING MAINTENANCE INSPECTIONS AT IAI, 2 EXISTING DENTS WERE FOUND ON UNDERSIDE OF THE RT WING OUTBOARD TRAILING FLAP. THE DENTS WERE MEASURED AS HAVING WIDTHS OF 1.8" AND 1.7" AS DEPTHS OF 0.027" AND 0.029" RESPECTIVELY. THE DAMAGES WERE FOUND ABOVE LIMITS SDR MK1Y20210221038Support Rib · crackedDURING MAINTENANCE INSPECTIONS AT IAI, A CRACK WAS FOUND NEAR THE RADIUS OF ACTUATOR SUPPORT RIB PN 114T2504-2. PENETRANT INSPECTION OF THE CRACK AREA WAS PERFORMED AND NO ADDITIONAL CRACKS WAS FOUND.SDR MK1Y20210221035Skin · dentedEXTERNAL FUSELAGE SKIN – 3 BULGES AND A DENT WERE FOUND ON EXTERNAL FUSELAGE SKIN BETWEEN STA 434-456 STR 26L-28L. THE DAMAGES ARE LOCATED WITHIN THE EXTRA CRITICAL AREA AROUND THE STATIC PORT AS NOTED IN SRM 51-10-01 GENERAL FIG 3 (SHEET 3 OF 4) DETAIL IV EXSDR MK1Y20210221034Skin · damagedENGINE NR 1-INLET COWL LEADING EDGE OUTER LIP-BETWEEN 7 AND 8 O'CLOCK POSITION. SHOP FOUND AN EXISTING UNDOCUMENTED REPAIR DOUBLER AT THE DATUM LOCATION, ACCORDING TO SRM 54-15-01 REPAIR 2, THERE IS NO APPLICABILITY FOR SUCH REPAIR THEREFORE THIS REA IS MAJORSDR MK1Y20210221033Skin · corrodedHORIZONTAL STABILIZER CENTER SECTION UPPER SKIN, BETWEEN STR 8/11 AND RBL 13/32; MAINTENANCE FOUND CORROSION ON PREVIOUSLY BLENDED SKIN AREA LOCATED BETWEEN STR 9-10 AND ON PREVIOUSLY INSTALLED DOUBLER LOCATED BETWEEN STR 10-11 PER BOEING SR 1-1906538101 AND 1SDR MK1Y20210221032Skin · damagedREPAIR – FUSELAGE SKIN STA 1263 – 1270, STR-32R-33R & 27R-29R, SECTION 46; PN 146T3510. SHOP FOUND EXISTING BLEND OUT AREAS NAMED M0054 AND M0055 AT FUSELAGE SKIN IN THE NOTED LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLSDR MK1Y20210221031Skin · corrodedCORROSION DAMAGE WAS FOUND TO THE RT WING UPPER INNER SPAR SKIN PANEL NR .1 OVER WING FILL PORT ADAPTER AT WS 785.2, S-15 TO S-16 LOCATION. SEE FIGURE 4 FOR EXISTING REPAIR DAMAGE DETAILS. AFTER CORROSION REMOVAL AT EACH OVER WING FILL PORT UPPER SKIN, THE ASDR MK1Y20210221030Skin · corrodedCORROSION DAMAGE WAS FOUND TO THE LT WING UPPER INNER SPAR SKIN PANEL NR 1 OVER WING FILL PORT ADAPTER AT WS 785.2, S-15 TO S-16 LOCATION. AFTER CORROSION REMOVAL AT EACH OVER WING FILL PORT UPPER SKIN, THE AREA WAS INSPECTED:
1. NO CORROSION OR CRACKS WERESDR MK1Y20210221029Skin · damagedREPAIR EXTERNAL FUSELAGE SKIN BETWEEN STA 287 – STA 406, STR - 1R/4R, AND STA 266 – STA 348, STR 5R-7R, (SECTION 41). MULTIPLE BLEND OUTS AND LIGHTNING STRIKES WERE FOUND ON EXTERNAL FUSELAGE SKIN BETWEEN STA 287-406 STR 1R-4R AND STA 266 – STA 348, STR 5R-7RSDR MK1Y20210221028Skin · damagedINNER FUSELAGE SKIN PANEL STA 1193 BETWEEN STR-28L AND 29L, PN 146T3252-1: AN EXISTING DEEP GOUGE WAS FOUND AND WAS BLENDED OUT AS PER SRM B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. AFTER THE BLEND AND DRILL OUT (0.250"), THE MEASURED MINIMUM FUSELAGE SKIN THSDR MK1Y20210221027Skin · damagedEXTERNAL FUSELAGE SKIN AT STA 1417, BETWEEN STR-31L/33L, SECTION 46. SHOP FOUND 9 BLEND OUTS IN FASTENERS ZONE IN FUSELAGE SKIN AT THE DATUM LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENERS AREA.SDR MK1Y20210221026Skin · damagedFUSELAGE SKIN EXTERNAL FUSELAGE SKIN AT STA 632, STR-26R SECTION 43. SHOP FOUND BLEND OUT IN FASTENERS ZONE IN UPPER SKIN OF LAP JOINT IN FUSELAGE SKIN AT THE DATUM LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENSDR MK1Y20210221025Skin · dentedELEC/ELEX ACCESS DOOR INNER SKIN. DURING CONVERSION AT IAI FACILITIES, MAINTENANCE HAS FOUND AT SERVICE DOOR ELEC/ELEX 2 DENTS ON INNER SKIN AND GOUGED WEB. THE DENTS WERE FOUND WITH CREASE AND ARE OUT OF ALLOWABLE DAMAGE PER SRM 52-40-01 AD5. THE INNER SKISDR MK1Y20210221024Skin · corrodedREPAIR – FUSELAGE SKIN (SECTION 45), BETWEEN STA 999 AND STA 1043, BETWEEN STR 2L AND STR 2R AS PER COSTUMER REQUEST SATCOM ANTENNA WAS DEACTIVATED AND DISMANTLED FROM THE AIRCRAFT. THE ANTENNA WAS MOUNTED TO AN ADAPTER PLATE AT DATUM LOCATION. UNDER ANTENNASDR MK1Y20210221023Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 1347 AND STA 1387, BETWEEN STR-28R AND STR 33R, SECTION 46. SHOP FOUND FIVE (5) EXISTING BLENDOUTS AREAS NAMED NRC: M0062, M0065, M0066, M0069 AND M0151 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERSDR MK1Y20210221022Skin · dentedPRIMARY EXHAUST NOZZLE OUTER SLEEVE SKIN, NR 1 ENGINE, AT 3 O'CLOCK. DURING CONVERSION AT IAI FACILITIES, MAINTENANCE HAS FOUND TWO (2) DENTS ON THE NR 1 ENGINE EXHAUST'S AFT EDGE AT 3 O'CLOCK. THE DENTS ARE OUT OF TOLERANCE DUE TO THEIR AY/Y RATIO AND ALSO SDR MK1Y20210221021Skin · damagedEXTERNAL FUSELAGE SKIN, STA 1535, STR 20L – 22L P/N 146T3340. SHOP FOUND AN EXISTING BLENDOUT AREA NAMED M0153 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUT FALL ON ASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLESDR MK1Y20210221020Skin · damagedEXTERNAL FUSELAGE SKIN AT STA 1417 STR 36L AND STA 1567, STR-37L, (2EA REPAIR LOCATIONS) SECTION 46. SHOP FOUND EXISTING BLENDOUTS AREAS NAMED NRC: M0086 AND M0099 AT FUSELAGE SKIN IN THE NOTED LOCATION. BLENDOUT M0086 IS LOCATED 1.1 INCHES FROM SPLICE JOUNT.SDR MK1Y20210221019Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 343 AND STA 350, STR-22R, SECTION 41. SHOP FOUND FORE (4) EXISTING BLENDOUTS AREAS NAMED NRC : M0048 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1SDR MK1Y20210221018Skin · damagedEXTERNAL FUSELAGE SKIN BETWEEN STA 450.5 AND STA 478, STR-26R/32R, (3EA REPAIR LOCATIONS), SECTION 43. SHOP FOUND THREE (3) EXISTING BLENDOUTS AREAS NAMED NRC : M0032, M0038 AND M00040 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZOSDR MK1Y20210221017Skin · damaged: EXTERNAL FUSELAGE SKIN BETWEEN STA 1351 AND STA 1373, STR-22R/25R, (3EA REPAIR LOCATIONS), SECTION 46. SHOP FOUND THREE (3) EXISTING BLENDOUTS AREAS NAMED NRC :M0078, M0075 AND M00076 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS Z
Back to Boeing 767-323