Boeing 767-306
Service difficulty reports · 2,510
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 = '767306' 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 = '767306' 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 UIEA2023011900012Seal · damagedSEVERAL ACCESS FUEL PANELS FROM RH WING WITH DAMAGED RUBBER SEALS. DAMAGED RUBBER SEALS WERE REPLACED PER AMM 28-11-01-404-005 REQUIREMENTS.SDR UIEA2023011900011Window · crackedFOUND A CRACK ON THE WINDOW OF AFT ENTRY DOOR. REPLACED THE WINDOW OF AFT ENTRY DOOR. AMM 56-31-01-004-001.SDR UIEA2023011910010Relief Valve · faultedSURGE TANK PRESSURE RELIEF VALVE FOR THE LT SIDE WAS FOUND OUT OF LIMITS PER TASK A-28-004-00-01. SURGE TANK PRESSURE RELIEF VALVE FOR THE LT SIDE WAS REPLACED PER AMM REQUIREMENTS. AMM 28-13-04-002-002.SDR UIEA2022111701191First Aid Kit · openFIRST AID KIT SEAL BROKEN.(<P>REMOVED AND REPLACED FIRST AID KIT IAW B767 AMM 25-64-03.SDR UIEA2022092601046None · noneFOUND LEFT AND RIAGHT OVERHEAD EMERGENCY LIGHTS IN COCKPIT INOP.(<P><SPAN>RELAMPED LIGHTS , OPS CHECKS NORMAL IAW AMM 33-51-11.</SPAN></P>)SDR UIEA2022082900923Light · inoperativeFOUND FLIGHT DECK CEILING LEFT EMERGENCY LIGHT INOP(<P>RELAMPED, OPS CHECK NORMAL I/A/W AMM 33-51-00 </P>)SDR P5CA2022081600167Elt · damagedELT BROKEN SEAL(<P>R/R ELT IAW AMM 25-63-03. OPS CHECK GOOD. MDDR 169983 CLOSED.</P>)SDR UIEA2022081300857Slat · delaminated#1 SLTAT HAS DISBONDED METAL ON THE OUTBD END TOP SIDE(<P>THE PART HAS BEEN INSPECTED AND REPAIRED IAW APPROVED TECHNICAL DATA, WITH DUAL RELEASE CERTIFICATE, FAA8130-3 AND EASA AND TECHNICAL DATA SRM 51-70-10-2R-1 REPAIR 1 REV 120 DATE 15AUG22</P>)SDR UIEA2022081300858Door · corrodedFWD LWR CARGO FWD RH BALL MAT FWD LATERAL LOCK HOUSING CORRODED(<P>REMOVED AND REPLACED FWD LATERAL LOCK HOUSING IAW SRM 51-40-05 & SRM 51-40-02</P>)SDR UIEA2022080800827Light · inoperativeFOUND EMERGENCY LIGHT AT L I DOOR INOP.(<P><SPAN>RELAMPED LIGHT AT L I DOOR , OPS CHECK NORMAL IAW AMM 33-51-03.</SPAN></P>)SDR UIEA2022070100704Fuel Tank · leakingWING CENTER TANK, RH SIDE, FROM L-11 TO L-1C AND BBL 97.42, FUEL LEAK ON JOINS (AUXILIAR CENTER TANK, RH SIDE, ROOT OF FUEL LEAK AT RBBL 97.42 AND STGR L-6 WAS REPAIRED IAW AMM 28-11-00</P>)SDR UIEA2022070100706Hydraulic Line · leakingAREA AFT OF PRESS BULK HEAD TO BS 1725.5, ELEVATOR FEEL COMPUTER, EVIDENCE OF LEAK ON LOWER HYD TUBES. (BTW STA 1702.2 AND 1725.5, LH SIDE).(THE ELEVATOR FEEL COMPUTER WAS INSTALLED CORRECTLY AS PER AMM 27-31-19-424-015, REV 136</P>)SDR UIEA2022070100707Actuator · leakingRH WING, INBOARD AILERON, ACTUATORS, LEAK EVIDENCE (LEAK CHECK HAS BEEN PERFORMED ON THE RH INBOARD AILERON ACTUATORS AND NO LEAKS WERE FOUND. TEST PERFORMED IN ACCORDANCE WITH AMM 29-11-00-796-053, REV 135</P>)SDR UIEA2022070100708Bearing · cokedENG 2, CORE SECTION BEARING NO.6 PRESSURE AND RETURN PIPES WITH OIL LEAK EVIDENCE (OIL COKE BUILD UP WAS REMOVED AND THE NUTS WERE RE-TORQUED PER AMM 72-50-00-216-032 AND 72-53-04-434-020, REV. 135</P>)SDR UIEA2022070100709Access Panel · contaminatedLEFT WING, IN ACCESS PANELS 551TB AND 551UB WITH EWIS CONTAMINATED OF HYDRAULIC(EWIS WAS CLEANED PER SWPM 20-10-04, REV 80</P>)SDR UIEA2022070700741Ecs · inoperativeDURING RUN TEST, ONE INDICATION OF AIR TEMPERATURE OF ECS IN EICAS, IS MISSING. PACK OUTLET TEMPERATURE BULB AND COMPRESOR OUTLET SENSOR WAS INSTALLED AS PER AMM 21-51-06-404-011 AND AMM 21-52-06-404-010, REV 136</P>)SDR UIEA2022070700743Pca · leakingDURING THE DEVELOPMENT OF THE TASK CARD HYDRAULIC POWER LEAK CHECK, RH WING, WAS FOUND WITH INTERNAL LEAK EVIDENCE AT THE O/B AILERON PCA(LEAK TEST WAS PERFORMED ON RH OUTBOARD AILERON PCA´S, NO LEAKS WERE FOUN. TEST PEFORMED IAW AMM 29-11-00-796-053, REV 135SDR UIEA2022070700744Lcca · leakingLEFT WING, WELL WHEEL ZONE LEFT TOP LCCA WITH LEAK EVIDENCE. LEAK TEST WAS PERFORMED ON LEFT TOP LCCA AND NO LEAK FOUND. REF. AMM 29-11-00-796-053, REV. 135</P>)SDR UIEA2022070700745Lcca · leakingLEFT WING, WELL WHEEL ZONE LEFT BOTTOM LCCA WITH LEAK EVIDENCE. LEAK TEST WAS PERFORMED ON THE LH BOTTOM LCCA, NO LEAKS FOUND. REF. 29-11-00-796-053</P>)SDR UIEA2022070700746Lockout · leakingDURING THE DEVELOPMENT OF THE TASK CARD HYDRAULIC POWER LEAK CHECK, RH WING, WAS FOUND LEAK EVIDENCE AT THE O/B AILERON LOCKOUT MECHANISM. LEAK TEST WAS PERFORMED ON O/B RH AILERON LOCKOUT MECHANISM AND NO LEAKS FOUND. TEST PERFORMED IAW 29-11-00-796-053, REVSDR UIEA2022070700747Spoiler · leakingDURING DEVELOPMENT OF TASK CARD HYDRAULIC POWER LEAK CHECK, RH WING, WAS FOUND LEAK EVIDENCE AT THE SPOILER NO. 9. LEAK TEST WAS PERFORMED ON THE RH WINGS, SPOILER ACTUATOR #9 AND NO EVIDENCE OF LEAKS FOUND. TEST REFERENCE AMM 29-11-00-786-053 REV 135</P>)SDR UIEA2022070700749Acoustic Panel · damagedLH INLET COWL INNER BARREL ACOUSTIC PANEL (LATERAL AND LOWER SEGMENT)(ENGINE # INLET COWL, INNER BARREL, AND ACOUSTIC PANELS WERE REPAIRED IAW SRM 54-15-01, REPAIR 3 & TRE6754160</P>)SDR UIEA2022070800759Actuator · leakingRH WING, INBOARD FLAP, OUTBOARD ACTUATOR, LEAK EVIDENCE(<P>LEAK TEST WAS PERFORMED ON RH INBOARD FLAP AND NO LEAKS FOUND. TEST PERFORMED IAW AMM 29-11-00-796-053 REV 125</P>)SDR UIEA2022071200761Acoustic Panel · damagedLH INLET COWL INNER BARREL ACOUSTIC PANEL (LATERAL AND LOWER SEGMENT)(ENGINE # INLET COWL, INNER BARREL, AND ACOUSTIC PANELS WERE REPAIRED IAW SRM 54-15-01, REPAIR 3 & TRE6754160</P>)SDR UIEA2022070100705Actuator · leakingNLG LOCK ACTUATOR WITH LEAK .(REMOVED& AND REPLACED NLG&UPLOCK ACTUATOR PER AMM 32-34-02.)SDR MK1Y20220629008Frame · crackedDURING MAINTENENCE INSPECTION FOUND CRACK ON THE FRAME INNER CHORD AT STA 632, STR 13R TO STR 14RSDR MK1Y20220629007Frame · dentedDURING MAINTENENCE INSPECTION FOUND DENT ON LARGE CARGO DOOR SURROUND STRUCTURE, AFT FRAME WEB, STA 618 BETWEEN STR 29R AND STR 30R.SDR MK1Y20220629006Flange · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION ON INBD SURFACE OF THE FLANGE AT STA 999, STR 18RSDR MK1Y20220629005Flange · corrodedDURING MAINTENENCE INSPECTION FOUND FOUND SEVERE CORROSION ON THE INNER CHORD FREE FLANGE AT STA 1439, STR 17L.SDR MK1Y20220629004Longeron · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION ON LONGERON CHORD AT STA 1087 BETWEEN STR 23L AND STR 24LSDR MK1Y20220629003Frame · corrodedDURING MAINTENENCE INSPECTION FOUND SEVERE CORROSION ON FRAME INNER CHORD AT STA 933, STR 18L TO STR 19LSDR MK1Y20220629002Failsafe · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION ON FAIL SAFE STRAP AND INNER CHORD AT SEVERAL LOCATION ON FRAME 478 BETWEEN STR 17R AND STR 19RSDR MK1Y20220629001Skin · damagedDURING MAINTENENCE INSPECTION FOUND IMPACT DAMAGE THAT CAUSE TORN SKIN ON FUSELAGE AT STA 1926, BL 0 TO RBL 5.SDR UIEA2022061900611Seal · damagedR/W I/B AFT FLAP HAS DAMAGED SEAL AT O/B SIDE. REMOVED AND REPLACED DAMAGED SEAL AT RIGHT WING I/B AFT FLAP O/B SIDE AS PER 767-300 AMM 20-10-23-964-001</P>)SDR UIEA2022061900612Bonding Jumper · broken#2 ENG R/H SIDE HAS 1EA BROKEN BONDING WIRE ( LOCATED ABOVE FUEL FILTER ) REMOVED & REPLACED #2 ENG R/H SIDE BONDING JUMPER TO THE HPSOV IAW B767 AMM 36-11-07</P>)SDR UIEA2022061900613Bolt · brokenBOLT IS BROKEN FOR CLAMP LOCATED ON #2 ENG R/H SIDE AFT OF HEAT EXCHANGER. INSTALLED BOLT AS PER B767-300 AMM 70-50-00. OPS CHECK GOOD</P>)SDR UIEA2022061900614Fastener · missing#2 ENG AFT STRUT FAIRING MISSING 2EA FASTENERS ON R/H SIDE INSTALLED MISSING FASTENERS AT #2 ENGINE AFT STRUT FAIRING ON RH SIDE AS PER 767-300 SRM 51-40-02-0G-0</P>)SDR UIEA2022061900615Rub Strip · worn#1 ENGINE EXHAUST DUCT RUB PADS (ALL) LOOSE/WORN. REMOVED AND REPLACED WORN WEAR PADS AND SECURED LOOSE PADS AS PER 767-300 SRM 51-40-02-0G-0</P>)SDR UIEA2022061900616Door Track · lack of lubeFWD ENTRY DOOR (L1) TRACK REQUIRES CLEANING & LUBRICATION. CLEANED & LUBRICATED FWD ENTRY DOOR (L1) TRACKS PER; B767-300 AMM 12-21-108. OPS CHECK GOOD</P>)SDR UIEA2022061900617Hose · frayedCOCKPIT CAPT OXYGEN MASK HOSE FRAYED. REMOVED & REPLACED CAPT O2 MASK PER B767-300 AMM 35-11-51. OPS CHECK GOOD NO LEAKS</P>)SDR UIEA2022061900618Evas Unit · looseCOCKPIT CAPT EVAS TOP COVER LOOSE READJUSTED CAPT EVAS COVER PER B767-300 AMM 25-60-99SDR UIEA2022061900619Fastener · missing# 2 ENGINE INLET CASE CHAFING STRIP MISSING PLASTIC FASTENERS AT 5 AND 9 O'CLOCK POSITIONS. INSTALLED MISSING PLASTIC FASTENERS AT ENGINE INLET CASE CHAFING STRIP AS PER 767-300 SRM 51-40-02-0G-0SDR UIEA2022051100454Band · brokenFLASH BAND ON ENTRY DOOR FLASHLIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED PLASTIC BAND ON ENTRY DOOR FLASHLIGHT ASSEMBLY AMM 25-64-00</P>)SDR UIEA2022032800243Tab · missingCA O2 MASK LEFT DOOR RETENTION TAB BROKEN AND MISSING.(<P>REMOVED AND REPLACED BOX ASSY, EQIP IAW AMM 35-11-51. OPS GOOD, LEAK CHECK GOOD.</P>)SDR P5CA2022032100091Escape Reel · noneFLIGHT DECK, ONE INERTIAL REEL ACCIDENTALLY DEPOYED, 6 REMAIN OPERATIONAL(REMOVED FROM THE A/C).(<P>TRANSFER TO MDDR 162932, PER MEL 25-61-01-01, CAT "C", DUE DATE: 31MAR22. DISP: JA @ 1601Z.</P> / <P>CVG MX-21MAR: LP 1543129, ITEM M4: INSTALLED #1 DESCENT DEVSDR P5CA2022032100092Escape Reel · noneFOUND #4 DESCENT DEVICE UNREELED.(<P>REMOVED AND REPLACED #4 DESCENT DEVICE IAW AMM 25-61-05.</P>)SDR UIEA2022021600137Mask · noneFOUND L/H SUPERNUMERARY PARTIAL FACE OXYGEN MASK LEAKING.(<P>REMOVED AND REPLACED L/H SUPERNUMERARY PARTIAL FACE OXYGEN MASK ASSY IAW AMM 35-11-51. OPS CHECK GOOD.</P>)SDR UIEA2022020200083None · noneCRACK ON FWD UPPER CHORD AT STA 1809.5 BULKHEAD, STRINGER S-7LH.(<P ><SPAN>REPAIR WAS INSTALLED ON FWD UPPER CHORD AT STA 1809.5 AND STRINGERS S-6LH TO S-8LH PER 767 SRM 53-80-08 REPAIR 9</SPAN></P> / <P> </P>)SDR UIEA2022020200084None · noneCORROSION ON THE UPPER SURFACE OF U-17 STRINGER OF RH WING SKIN PANEL 1 & 2 AND RIB 1 AND RIB 3(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>AFFECTED U-17 STRINGER SEGMENT WAS TRIMMED TO REMOVE ALL CORROSION.</SPAN></P> / <P STYLE="MARGIN: 0IN 0IN 0.0SDR UIEA2022020200085None · noneCRACK ON LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 BETWEEN NAC STA 221.25 / NAC STA 237.5 (CUTOUT FOR ACCESS PANEL 432AL)(<P ><SPAN>LH STRUT OUTBD SKIN PANEL P/N 311T2450-23 WAS REPAIRED PER BOEING SR 4-5340563504</SPAN></P> / <P> </P>)
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