Boeing 767-316
Service difficulty reports · 453
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 = '767316' 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 = '767316' 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 ABXA20260202044Flap System · stuckDURING TAXI OUT RIGHT FLAPS STUCK AT FLAPS 1 WHEN SELECTED TO FLAPS 5 .AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED AC .MTX T/S AS PER FIM 27-58 FT 803, CYCLE FLAPS UP AND TO 5 DETENT NO ISSUES, NEEDLE REMAIN MOVING TOGETHER CYCLE FLAPS AT EACH DETENT 6 TISDR ABXA2026020301046Fire Loop · false indicationPILOT REPORTED CARGO FIRE LOOP 2 YELLOW ILLUMINATED. MAINTENANCE PERFORMED AFOLTS TEST AS PER REF IAI SUPPLEMENT MAIN MANUAL 26-14-00, TEST NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR ABXA202601198019Warning Light · false activationMAIN CARGO DOOR LIGHT ILLMINATED ON PUSHBACK NEVER DISCONNECTED FROM TUG (BTB). MTX ENTERED ACFT AND OPENED MCD DOOR AND CHECKED OPERATION .CLOSED CARGO DOOR AND LOOKED. ADVISORY LIGHT ADVISORY LIGHT WENT OUT. OPS CHECK NORMAL AND IAW AMM 52-32-00, ACFT DEPASDR ABXA20251219350Warning Message · illuminatedDURING TAXI OUT ALTN ANTISKID AND NORM ANTISKID STATUS MESSAGE ON GROUND ANTI-SKID EICAS MESSAGE APPEARED A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C MTX THEN DEFERRED ANTI SKID IAW MEL ABX-32-42-1-1A AND RETURNED ACFT TO SERVICE.SDR ABXA20251212332A/C Pack · inoperativeAFTER START CHECKLIST WAS COMPLETED, AND LEFT PACK OFF EICAS MESSAGE ILLUMINATED A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C . MTX DEFERRED THE LEFT PACK IAW MEL ABX-21-51-1-1. AND RETURNED TO SERVICE.SDR ABXA202512054318Valve · faultedDURING TAXI OUT, AFT CABIN TEMP MESSAGE APPEARED BEFORE ENG START. AIRCRAFT RETURNED TO GATE (BTB). MAINTENANCE DEFERRED AFT ZONE TEMP MOD TRIM VALVE IAW ABX B767 MEL 21-61-1-2. AIRCRAFT RETURNED TO SERVICE.SDR IPXA2025081828045Battery Pack · inoperativeEMERGENCY DOOR LIGHTS AND R/H DOME EMERGENCY LIGHT INOP. REPLACED M735 EMERGENCY BATTERY PACK AND TESTED LIGHT SATIS IAW AMM 33-51-07-401 REV 145.SDR IPXA2025072131163Power Supply · inoperativeEXTERIOR EMERGENCY LIGHT AND L9801 DOME EMERGENCY LIGHT INOP T/S ACCOMPLISHED IAW IAI WDM 33-51-13 AND FOUND M736 PWR SUPPLY INOP. R & R M736 IAW AMM 33-51-07-401 REV 145.SDR UIEA2025032300377Retainer · corrodedCORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BL, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DESDR UIEA2025032300378Retainer · corrodedCORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BR, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BR WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEFSDR UIEA2025032300379Skin · gougedGOUGE AT INTERIOR SKIN OF FWD CARGO DOOR LWR FWD FRAME, STA 494.(<P>REWORKED AND INSPECTED PER TRE6752058 (BOEING MESSAGE CMA-TLS-25-0024). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025032700392Computer · leakingELEVATOR FEEL COMPUTER, WITH HYDRAULIC LEAK.(<P>ELEVATOR FEEL COMPUTER HYDRAULIC LINES WERE RE-TORQUED IAW AMM 27-31-19-424-015 REV. 144 22DEC24. TORQUE APPLIED 270 IN/LB AND 170 IN/LB, TORQUES WRENCH DATA S/N: 0422127314 D/D: 17SEP25 AND S/N: 1123126519 D/D: SDR UIEA2025040100423Skin · crackedLH SIDE, FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER, WAS FOUND CRACK INDICATION, ON OPEN HOLE # 4 POSITION 5 O'CLOCK AT SKIN AND 10 O'CLOCK POSITION BEAR STRAP.(<P>LH SIDE, FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER, ON OPEN HOLE # 4 POSITION 5 O'CLOCK AT SKINSDR UIEA2025040100424Skin · crackedRH SIDE, FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER, WAS FOUND CRACK INDICATION, ON OPEN HOLE # 4 POSITION 1 O'CLOCK AT SKIN APPROX.(<P>RH SIDE, FORWARD SERVICE DO OR CUTOUT AFT LOWER CORNER, ,ON OPEN HOLE # 4 POSITION 1 O'CLOCK AT SKIN CRACK WAS REPAIRED IASDR UIEA2025040100425Torsion Box · corrodedCORROSION ON TORSION BOX TOP SKIN BTW RBL 13.83 AND RBL 41.50, STGR 3 AT HORIZONTAL STABILIZER CENTER SECTION.(<P>ON TORSION BOX TOP SKIN BTW RBL 13.83 AND RBL 41.50, STGR 3 AT HORIZONTAL STABILIZER CENTER SECTION, CORROSION LEVEL 2 WAS REPAIRED IAW TRE6755083SDR UIEA2025040100426Fuel Cell · leakingFUEL LEAK AT LOWER SIDE AREA OF LT WING LWR REAR SPAR SPLICE FITTING.<BR>(<P>LOWER SIDE AREA OF LT WING LWR REAR SPAR SPLICE FUEL LEAK WAS REPAIRED AND TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013 REV 144 22/DEC/24. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040300428Blocker Door · crackedENG. 1, RIGHT T/R BLOCKER DOOR NO. 9 WITH A CRACK.(<P>ENG. 1, RIGHT T/R BLOCKER DOOR NO. 9 WAS REPLACED IAW AMM TASK 78-31-14-404-008-H00. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040300429Apu · inoperativeAPU INOP (AUXILIARY POWER UNIT) ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60).(<P>APU INOP (AUXILIARY POWER UNIT) ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60) WAS REPLACED WITH TASK CARD 8027 A-49-999-00-01. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040300430Seal · brokenWING RH, BROKEN SEAL ON ACCESS PANELS 661 LB AND 661 CB.(<P>WING RH SEAL WAS REPLACED ON ACCESS PANEL 661LB, WING RH SEAL WAS REPLACED ON ACCESS PANEL 661CB IAW SRM 51-10-02-0G-0 PAR 9. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025040300431Metering Valve · leakingLH WHEEL WELL AREA FWD BULKHEAD LH BRAKE METERING VALVE ASSY WITH HYDRAULIC LEAK.(<P>LH BRAKE METERING VALVE ASSY WAS INSTALLED IAW 32-41-02-424-002-003. STEP D1 STEP D10 TORQUE APPLIED S/N 0422127314 DUE DATE 17SEP25, TORQUE APPLIED 85 IN LBS, 140 IN LB, 200 SDR UIEA2025040300432Pca · leakingRH WING, REAR SPAR, INBOARD AILERON, BOTH PCA´S WITH HYDRAULIC LEAK.(<P>AILERON PCAS (2 EAS) WERE REPLACED (SN: 1133 PN: 282800-1009 & SN: 1196 PN: 282800-1009). CHECKED FOR LEAKS & NO LEAK FOUND. ADJUSTMENT AND TESTS WERE SATISFACTORY. ALL WORKS IAW AMM 27-11SDR UIEA2025040400433Union · brokenRIGHT ENGINE STRUT 2 AFT NACELLE STRUT FAIRINGS IN ACCESS PANEL 447BL INTERNAL PART IN HYDRAULIC SHUT OFF VALVE WITH BROKEN CONNECTOR.(<P>CONNECTOR OF HYDRAULIC SHUTOFF VALVE AND BACKSHELL WERE REPLACED (PN: BACC63BW14SC5S & PN: BACC10HV14) INSTALLATION TEST WSDR UIEA2025040400434Pbe · leakingWING LH, INBOARD AILERON, BOTH PCA'S WITH LEAK.(<P>BOTH PCA'S, WERE REPLACED, ADJUSTED AND TESTED. (SN: 0683 PN: 282800-1011 & SN: 280 PN: 282800-1007) TEST WAS SATISFACTORY AND NO LEAK FOUND. ALL WORK IAW AMM: 27-11-48-022-003, AMM 27-11-48-422-040 AND 27-11-SDR UIEA2025040400436Fuse · leakingHYDRAULIC LEAK AT RH ANTISKID MODULE FUSE.(<P>IN RH ANTISKID MODULE FUSE WAS REPLACED IAW AMM 32-42-02-404-014, CHECK FOR LEAK, NO LEAK FOUND, OPERATION OF BRAKES WAS SATISFACTORY, IAW AMM 32-42-03-404-033.</P>)SDR UIEA2025040400437Seal · brokenLH WING ACCESS PANEL 561BB WITH BOTH BULB SEAL BROKEN.(<P>BROKEN SEAL REPLACED AND CORRECTLY INSTALLED PER SRM 51-10-02-0G-0 PARA 9 REV 51. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040400439Pad · brokenLEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD BROKEN.(<P>LEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD WAS REPLACED IAW AMM 57-54-06-914-002 REV 144 DATE 22DEC24. NO FURTHER DEFECT NOTED.</P>)SDR UIEA2025040400440Proximity Sensor · damagedBROKEN TAG WASHER SUPPORT ON INBOARD AUX TRACK AT SLAT NO. 9.(<P>LEADING EDGE SENSOR SWITCH ON INBOARD AUX TRACK AT SLAT NO. 9 WAS REPLACED IAW AMM 27-88-01-902-001 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040400441Cover · dentedDURING RAM AIR TURBINE DEPLOYMENT TEST BY TASK CARD 8017-0101, FOUND A DENT ON RAM AIR TURBINE COVER SURFACE; IT WAS EVALUATED AND FOUND OUT OF LIMITS. L= 2.400 IN, W= 1.100 IN, D= 0.075 IN.(<P>N/R 00278 THE COVER WAS REMOVED FROM THE RAM AIR TURBINE IAW CMM 2SDR UIEA2025040400442Skin · dentedVERTICAL STABILIZER LH PANEL ASSEMBLY OUTER SKIN WITH DENT.(<P>DENT ON VERTICAL STABILIZER, LH PANEL ASSEMBLY, OUTER SKIN, WAS EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W. SRM 55-30-01-1A-1 AD.1 FIG. 101, DETAIL III. REV. 52 15APR25. DENT DOT 9025SDR UIEA2025040400443Skin · debondedLH VERTICAL STABILIZER SKIN PANEL BTW FSS 270.784 TO FSS 118.75 PANEL WITH DISBONDED.(<P>LH VERTICAL STABILIZER SKIN PANEL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52 15-APR-25. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025040400444Pump · faultedLH WING THE FUEL BOOST PUMP LH FWD, TEST OPERATIONAL NOT SATISFACTORY. LT FWD BOOST PUMP LIGHT IN PANEL "P5" WAS INSTALLED CORRECTLY. IAW SWPM 20-84, REV 88, DATE 15-FEB-2025. TEST RESULT SATISFACTORY.SDR IPXA2025031292106Knob · out of adjustCREW REPORTS THAT THE TILT KNOB POSITION DID NOT MATCH WITH THE INDICATION ON THE NAV DISPLAY. TILT KNOB ADJUSTED IAW AMM 34-43-02 PB401 REV.144. AND TESTED IAW AMM 34-43-00 PB501 REV.144. FOUND SATIS.SDR UIEA2025011000027Control Unit · damagedPERFORMED TURNBACK TO IAH, DUE TO ELECTRICAL FUMES SMELL.(<P>FOUND M00897 ELECTRICAL LOAD CONTROL UNIT WITH LOOSE HARDWARE AND BURNT PLASTIC COVERING. REMOVED AND REPLACED ELCU IAW B767 AMM 29-11-14, OPS CHECK GOOD. SMELL IS NOW FAINT AND GOING AWAY. IPC 29-11SDR UIEA2024123001192Escape Reel · missingEMERGENCY DESCENT DEVICES MISSING ONE.(<P>INSTALLED ONE EMERGENCY DESCENT DEVICE PER AMM 25-61-03. NO DEFECTS NOTED. PART EFFECTIVITY VERIFIED PER IPC 25-61-03-02.</P>)SDR IPXA2024120432892Idg · failedATB L GEN OFF DURING TAKEOFF ROLL. RAN CHECKLIST, RESULTED IN MOMENTARY GEN OPERATION BEFORE FAILING AGAIN. ATB REPLACED JAW AMM 24-22-02 PB 401 SATISSDR IPXA2024112569479Smoke Detector · false activationMAIN DECK SMOKE DETECTOR LED A2 REMAINED AMBER (ILLUMINATED) ONCE AIRBORNE WITHOUT EICAS OR STATUS MESSAGE. NO FAULTS AFTER POWER RESET. MAIN DECK SMOKE DETECTOR SYSTEM TEST C/O IAW AMM 26-16-00-715-001 REV. 143. TEST SATIS.SDR UIEA2024111701095Warning Light · abnormalLOW-SPEED RTO DUE TO CONFIG WARN FLASPS M/S SET WITH FLAPS RESET SYS OPS NORMAL(<P>PERFORMED FLAPS SYS TEST PER 767 AMM 27-51-00, OPS CKS NORMAL, NO FAULTS NOTED </P>)SDR 2024FA0000829Idg · oil consumptionON OCTOBER 26TH, 2024 DURING THE TAKE-OFF ROLL IT WAS NECESSARY TO PERFORM MANEUVERS OF REJECTED TAKEOFF AT 80 KNOTS DUE TO INTEGRATED DRIVE GENERATOR (IDG) FAILURES; THE AIRCRAFT RETURN TO THE RAMP AND THE MAINTENANCE COMPLETED AND INSPECTION OF THE IDG; IT WSDR IPXA2024082938616None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDRSDR IPXA2024081938616Drain · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPENSDR IPXA2024082516569Floor Panel · damagedMAJOR REPAIR, DAMAGE FOUND M/D FLOOR PNL DAMAGE P/N:371-53-13-C4218-103 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-13-C4218-103SDR IPXA2024082516559Floor Panel · damagedMAJOR REPAIR, DAMAGE - FOUND M/D FLOOR PNL DAMAGE P/N:371-53-15-C6405-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-15-C6405-101.SDR IPXA2024082516575Floor Panel · damagedMAJOR REPAIR, DAMAGE , FOUND M/D FLOOR PNL DAMAGE P/N: 368-53-00-95626-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-00-95626-101SDR IPXA2024082996283Pump · cracked*** SUPPLEMENTAL SDR *** FAULT - CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV 143 REPLACE THE R/H WING AUX FUEL PUMP PNLNO.631AB. 2.CONDITION CHECK NORMAL. 3.IPC VERIFIED AND SERVICEABLE TASDR IPXA2024082993754Handle · brokenFOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE 1. I.A.W AIPC 52-11-25-13-144 REV.28 TO REMOVE FWD ENTRY DOOR HANDLE. 2. I.A.W AIPC 52-11-25-13-144 REV.28 TO INSTALL NEW FWD ENTRY DOOR HANDLE. 3. I.A.W AMM TASK 52-11-00-715-128 REV.143 TO DO OPERATIONAL TESTSDR IPXA2024081693754Bearing · brokenFOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE OK TO WORKSDR IPXA2024081696283Access Panel · crackedCRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE)SDR IPXA2024090674434Skin · dentedSKIN DENTED, RT FUSELAGE TAIL SECTION BS 1915.1 - 1923.5. MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.4" DEPTH(Y)=0.006" AND A/Y = 66 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126SDR IPXA2024090674300Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-36R (EVALUATE) MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.6" DEPTH(Y)=0.007" AND A/Y = 85 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126SDR IPXA2024082977067Skin · cracked*** SUPPLEMENTAL SDR *** FAULT - CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR) INSTALLED L/H WING LEADING EDGE UPPER FIX PANEL I.A.W SRM 51-40-02-0G REV.126 AND BOEING DWG 114T2230 SH1 REV.D AND 114T2510 SH1 REV.E AND 114T21
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