Boeing 767-3P6
Service difficulty reports · 1,440
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 = '7673P6' 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 = '7673P6' 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 IXXA20240510029Flap System · faultedON APPROACH TO KRFD CREW REPORTED EXECUTING GO-AROUND DUE TO WIND SHEAR/UNSTABLE APP. ON FLAP RETRACTION EICAS LE SLAT SYM. EXTRA CONTROL FORCES RIGHT YOKE TO REMAIN LEVEL. ATI QUICK REFERENCE HANDBOOK PROCEDURES COMPLIED WITH. LANDING WAS WITHOUT INCIDENT ANSDR ABXA2024050489Skin · crackedDURING ROUTINE LINE OPERATIONS IN MIA, MAINTENANCE DISCOVERED TWO CRACKS AT THE RH EMPENNAGE SECTION AT STA. 1654.5. AT APPROXIMATELY STRINGER 15R. BOTH CRACKS MEASURE APPROXIMATELY 2¿¿ IN LENGTH. MIA INDICATED THAT THERE WAS NO DENT ASSOCIATED WITH THE CRACK.SDR ABXA2024041680Engine · unknownON TAXI OUT RT ENGINE DID NOT STABILIZE AFTER START ON 1ST ATTEMPT .AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . MAINTENANCE PERFORMED RH ENG RUN PER AMM 71-00-00. AFTER 5 MIN RH ENG VALUES STABLE ( N1& N2 ). RH ENG OPERATES NORMAL. A/C REMAINS NO ETOPS. SDR ABXA2024032868Hose · brokenON TAXI OUT GOT EICAS MESAGE L HYD QTY FOLLOWINED BY CAUTION BEEPER EICAS MESSAGE L HYD SYSTEM PRESS. STATUS PAGE SHOWED L HYD QTY 0.17 RF. FOUND BROKEN / DAMAGED HOSE FROM RUDDER RATIO CHANGER (REF LEAK CODE 320-6-3 LEFT TO PCA HOSE ASSY). REPLACED PER AMM 20SDR ABXA2024032060Display · inoperativeTMSP IS INOP (N1 DISPLAY BOTH ENGINES). PERFORMED AUTO FL AND TMC C/B'S RESET AND MCDP GND 05 IAW 22-03-00/201. THE SYSTEM OK. TMSP WORKS NORMAL. DEFERRED. RALM STATUS DOWNGRADED TO CAT I PENDING 30/40 TEST.SDR ABXA2024031054Priority Valve · unserviceableAFTER ENGINE START RT ENG BLEED WILL NOT TURN ON AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC. AND DEFERRED RH ENGINE BLEED FOR DEPARTURE IAW MEL ABX-36-11-1-2A-1. RETURNED AC TO SERVICE AND AC DEPARTED .RE ACT PRSOV AND FAN AIR VALVE SWAPPED LEFT AND RIGHTSDR ABXA202402270647Pitot Head · malfunctionedDURING TAXI F/O PITOT FAILED AFTER ENGINE START . AC RETURNED TO GATE AND MAINTENACE GROUNDED AC . TROUBLE SHOT AND REMOVED AND REPLACED F/O PITOT-STATIC PROBE(THIRD) IAW B767 AMM 34-11-01, OPS CHECK GOOD. HIGH RANGE LEAK GOOD IAW 34-11-00. MAINTENANCE RETUSDR ABXA20240227645Target · out of toleranceAFTER TAKEOFF ; FLAP HANDLE UP,FLAP INDICATION BETWEEN UP AND 1 ;LE SLAT ASYM CAUTION ON EICAS .AC RETURENED TO FIELD AND MAINTENANCE GROUNDED AC. MAINTENANCE VERIFIED RESISTANCE AND INDUCTANCE OF ALL LEADING EDGE SENSORS.VISUALLY INSPECTED ALL SENSORS ,FOUND"SDR ABXA20240227444Module · malfunctionedDURING CLIMB LE SLAT ASYM EICAS MSG APPEARED AC RETURNED TO FIELD AND MAINTENANCE GROUNDED AC .AND FLIGHT WAS SWAPPED MAINTENANCE CONTINUED TO WORK . REMOVED AND REPLACED C FSPM PER AMM 27-58-01 OPS CHECK NORMAL. ALSO PERFORMED -63 FSEU READOUT OF SENSORS/RVSDR IXXA20240212004Unknown · odorDURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED WITH LEFT AND RIGHT PACKS IN OPERATION EXHAUST SMELLS IN THE THE FLIGHT DECK WERE NOTED. SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER B767 AMM 05-51-56 SATISFACTORY. NO SIGNS OF OIL CONTAMINATION. WISDR ABXA2024020820Circuit Card · malfunctionedAMENDED:.AFTER BOTH ENG'S STARTED ADP PRESS LGT ILLUMINATED PRESS LGT STAYS ILUMINATED WITH SELECTOR SWITCH IN ON POSTION .AC RETURNED TO THE GATE , MAINTENACE GROUNDED AC DEFERRED ADP FOR DEPARTURE IAW MEL ABX-29-11-3. RETURENED AC TO SERVICE AND DEPARTED. SDR ABXA20240209820Warning Light · illuminatedAFTER BOTH ENG'S STARTED ADP PRESS LGT ILLUMINATED PRESS LGT STAYS ILUMINATED WITH SELECTOR SWITCH IN ON POSTION .AC RETURNED TO THE GATE , MAINTENACE GROUNDED AC DEFERRED ADP FOR DEPARTURE IAW MEL ABX-29-11-3. RETURENED AC TO SERVICE AND DEPARTED. WILL AMENSDR IXXA20240209003Battery · inoperativeDURING SCHEDULED INSPECTIONS LINE MAINTENANCE REPORTED, LEFT EMERGENCY LIGHTS INOPERATIVE. FORWARD EMERGENCY LIGHT BATTERY REMOVED AND REPLACED. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.SDR IXXA20231128084Unknown · unknownDURING SERVICE CHECK INSPECTIONS LINE MAINTENANCE IDENTIFIED EMERGENCY LIGHTS SWITCH GUARD NOT PULLING SWITCH TO ARMED POSITION. OVERHEAD PANEL SWITCH GUARD REMOVED AND REPLACED PER B767 AIRCRAFT MAINTENANCE MANUAL 33-13-00. OPERATIONAL CHECK GOOD. NO ADDITIONSDR IXXA20231118001Failsafe · corrodedCORROSION ON FAILSAFE STRAP IN FLC DOOR CUTOUTSDR IXXA2023111701Skin · crackedFUSELAGE SKIN AND BEAR STRAP AT THE LOWER TWO HOLES OF THE R1 DOOR LOWER CORNER ARE CRACKED.SDR IXXA2023110303Skin · crackedFUSELAGE SKIN AND BEAR STRAP IS CRACKED AT THE L1 DOOR LOWER CORNER.SDR IXXA2023110301Skin Panel · delaminatedRH SIDE OF VERTICAL STAB SKIN IS DELAMINATED.SDR IXXA20231015070Unknown · unknownPOST FLIGHT CREW REPORTED, #6 INERTIAL REEL FELL OUT OF HOLDER. REMOVED INERTIAL REEL IAW B767 IAW SMM 25-61-03. SYSTEM FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM-45790 IAW MEL 25-61-01. REMOVED AND REPLACED #6 DESCENT DEVICE IAW IAI SMM 25-61-03. DEFERRASDR IXXA20230914062Unknown · unknownPOST FLIGHT, CREW REPORTED EMERGENCY LIGHTS SWITCH COVER WILL NOT STAY CLOSED. REMOVED AND REPLACED EMERGENCY LIGHTS SWITCH GUARD IAW B767 SWPM 20-83-11. OPERATIONAL CHECK GOOD. NO ADDITIONAL FAULTS NOTED.SDR ABXA20230912185Unknown · unknownAILERON LOCKOUT MESSAGE DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AILERON LOCKOUT SYSTEM PER MEL 27-11-2. AIRCRAFT RETURNED TO SERVICESDR 21GA20230911012Stringer · corrodedCORROSION FOUND ON SURFACE HFEC AT HORZ STAB UPPER STRINGER S-9L AND LBL 39 ON LOWER AFT FLANGE UPPER SURFACE.SDR 21GA20230911011Stringer · corrodedCORROSION FOUN DURING SURFACE HFEC AT HORZ STAB UPPER STRINGER S-5L AND LBL 39 ON LOWER AFT FLANGE UPPER SURFACE. REPAIRED PER KALITTA DWG 55102302-1 OR.SDR 21GA20230911010Stringer · corrodedFOUND SURFACE CORROSION ON HORIZONTAL STABILIZER UPPER STRINGER S-10R AND RBL 39 ON LOWER FLANGE. REPAIRED PER KALITTA DWG 55102304-1.SDR 21GA20230911009Frame · corrodedCORROSION FOUND ON AFT LOWER SIDE OF PRESSURE DECK FRAME AT STA 977, RBL 97. REPAIRED PER KALITTA DWG 53502301.1-ORSDR 21GA20230911008Stiffener · crackedDURING ACCOMPLISHMENT OF AD 2005-02-02. CRACK INDICATION WAS FOUND EXTENDING BELOW WL 160. REPAIR WAS ACCOMPLISHED PER BOEING.SDR ABXA20230905183Unknown · unknownDURING PUSH BACK MAINTENANCE NOTED TOILET DOOR SERVICE SNAPPED. REALLIGHNMENT HINGE SPRINGS AND SECURED DOOR CLOSED IAW AMM 52-49-07SDR ABXA20230815175Module · faultedGEAR DISAGREE TAILSKID AND MASTER CAUTION ILLUNINATED ON TURN TO FINAL. RAN QRH 14.17 WHICH CLEARED GEAR DISAGREE AND TAILSKID GEAR DOORS ILLUMINATED. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. AIRCRAFT WAS GRPONDED BY MAINTENANCE. SDR 21GA20230803007Lamp · blownFLIGHT DECK EMERGENCY LIGHT INOPERATIVE.SDR IXXA2023070701Seat Track · crackedFIRST OFFICER INBOARD SEAT TRACK CRACKED.SDR ABXA20230705142Starter · failed#2 ENGINE DID NOT ROTATE WHEN SELECTED TO START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RH STARTER, REF AMM 80-11-01 OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20230703140Computer · malfunctionedAFTER ENGINE START, WE HAD AN ELEV FEEL STATUS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED ELEVATOR FEEL COMPUTER PER B767 AMM 27-31-00. LEAK CHECK GOOD. OPS CHECK GOOD PER B767 AMM 27-31-00. AIRCRAFT RETURNED TO SERVICE.SDR IXXA2023071003Skin · damagedLMLG WHEEL WELL FUSELAGE FORWARD OF BODY DOOR IS DAMAGED AT AND AROUND DOUBLER REPAIRSDR IXXA202306280001Skin · damagedLW LEADING EDGED HAS COMPOSITE DAMAGE.SDR IXXA2023071002Skin · crackedR1 DOOR CUTOUT AFT LOWER CORNER CRACKEDSDR IXXA2023071001Skin · crackedL1 DOOR CUTOUT AFT LOWER CORNER CRACKEDSDR 21GA20230614006Unknown · unknownAFTER TAKEOFF, TCAS FAILED AND CB POPPED. RESET CB. ONE HOUR INTO FLIGHT GOT MESSAGE FWD EQUIP COOLING AND SMELLED SMOKE. PULLED TCAS CB AND SMELL SLOWLY DISSIPATED.SDR ABXA20230608115Unknown · unknownRUDDER TRIM INDICATOR INOPERATIVE ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE . MAINTENANCE DEFERRED IAW MEL 27-21-3. AIRCRAFT RETURNED TO SERVICESDR ABXA20230605114Unknown · unknownLT HYDRAULIC QUANTITY DROPPING DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE INSPECTED AIRCRAFT FOR HYDRAULIC LEAKS. NO EXTERNAL LEAKS NOTED. SUMPED FUEL FROM LH MAIN DUE TO RECENT MX. NO HYD FLUID NOTICED IN SAMPLE. RESERVICED SDR ABXA2023051297Unknown · unknownTE FLAP DISAGREE EICAS MESSAGE ILLUMINATED AFTER FLAPS 5 WERE SELECTED & INDICATED 5. MISSED THE APPROACH AND PERFORMED TROUBLESHOOTING & QRH PROCEDURES. DUE TO THE COMBINATION OF MAINTENANCE ISSUES, AN EMERGENCY WAS DECLARED DUE TO LANDING DISTANCE & STOPPINGSDR MK1Y20230503023Unknown · unknownSTA 139 - ATA 180.5, BELOW WINDOWS R1 AND R1: DURING MAINTANACE INSPECTION AT IAI, SHOP FOUND TWO (2) DOCUMENTED REPAIRS AT THE NOTED LOCATION. FWD REPAIR: LIGHTNING STRIKE REPAIR AT STA 139, BELOW WINDOW R1. AFT REPAIR: A DOUBLER REPAIR ON THE EXTERNAL FUS SKSDR MK1Y20230503022Unknown · unknownSTRUT #2, AFT FAIRNG - TRAILING EDGE, RH AND LH, NAC STA 410 TO 413: DURING MAINTENANCE INSPECTION AT IAI FACILITES, SHOP DISCOVERED UNDOCUMENTED DOBULER REPAIR IN STRUT #2, SKIN PANELS, ON BOTH SIDES.SDR MK1Y20230503021Unknown · unknownEXTERNAL FUSELAGE SKIN, STA 661, STR-30R-STR-31R: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE BULGE ON FUSELAGE SKIN LOCATED AT STA 661, 2-INCH BELOW THE STR 30R. INITIAL DIMENSION OF BULGE IS A=0.57”, Y=0.0278” (A/Y=20). BULGE IS OUT OF LIMITS PER SRSDR MK1Y20230503020Unknown · unknownSEC 46 FUSELAGE SKIN, STA 1564.3, 5” ABOVE STR 16L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 1264.3, 5” ABOVE STR 16L. INITIAL DIMENSION OF DENTED AREA A=0.720”, Y=0.032” (A/Y=22). DENT IS OUT OF LIMITS PER SRM SDR MK1Y20230503019Unknown · unknownSECTION 41 – FUSELAGE SKIN – STA 422 BETWEEN STR 31L AND STR 32L: A BULGE OUT OF LIMITS ON THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8SDR MK1Y20230503018Unknown · unknownSECTION 43 FUSELAGE SKIN STA 669.3 BETWEEN STR 35L AND STR 36L: AN EXISTING BULGE OUT OF LIMITS ON FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8.SDR MK1Y20230503017Unknown · unknownSEC 43 FUSELAGE SKIN, STA 600.8 BTWN STR 32L-33L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 600.8 BETWEEN STR 32L AND STR 33L. INITIAL DIMENSION OF DENTED AREA A=0.680”, Y=0.027” (A/Y=25). DENT IS OUT OF LIMITS PSDR MK1Y202305173016Unknown · unknownR/H MLG DOOR: MAINTENANCE DISCOVERED A PUNCTURE AT THE INNER SKIN OF R/H MLG DOOR IN A CRITICAL AREA (LESS THAN 10 INCHES FROM THE CENTER HINGE). SHOP REPORTED SEVERAL DAMAGES NEAR THE NOTED PUNCTURE. ALL OTHER DAMAGES WERE REPAIRED PER SRM 52-80 REQUIREMENTS.SDR MK1Y202305173015Unknown · unknownDURING CONVERSION OF S/N 25354, MAINTENANCE WAS REQUIRED TO REPLACE ENGINE #2 INLET COWL. THE REPLACEMENT INLET COWL P/N 224-2101-563, S/N 0634RV860 PROVIDED BY COSTUMER. THE NOTED INLET COWL WAS INSTALLED ON A/C AND POLISHED. MAINTENANCE REPORTED CORROSION/PISDR MK1Y20230503014Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND EXISTING LATCH REPAIR DOUBLER ON THE OUTBD CORE COWL ENG #2 B/T NAC STA 267 TO 274.5 AT 6 O’CLOCK, CENTER LATCH. DURING DISASSEMBLE THE EXISTING DOUBLER, SHOP FOUND TWO (2) ELONGATED HOLES, 1 HOLE IN DIA 0.328” AND THE
Back to Boeing 767-3P6