Boeing 767-322
Service difficulty reports · 11,763
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 = '767322' 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 = '767322' 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 CALA2024090302360Shear Tie · corrodedB767-53-3-7058 AFT OF BULK CGO, STA 1562 S38L TO S38R SHEAR TIE FOUND CORROSION. AFT OF BULK CARGO STA 1562 BETWEEN STR 38L AND STR 38R SHEAR TIE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 ATTACHED FORM 44-0008 ITEM 1 TO ITEM 5 ACCOMPLISHSDR CALA2024090302358Structure · corrodedSUPPORT TASK - AFT OF BULK CARGO STA 1562 BTN S39L AND S39R FAIL SHORD CHORD CORROSION CRACK AT HOLE FND AFTER SHEAR TIE REMOVED. TRANSFER REFER NON-ROUTINE WO.3616838 AND ORIGINATOR V896820 AFT OF BULK CGO STA1562 BTW STR39L AND 39R FAIL SAFE CHORD WORK ACCOMSDR CALA2024090402380Plate · corrodedBULK CARGO STA 1564 RBL 2" DOME NUT AREA CORROSION FOUND. FUSELAGE STA 1564 TO STA 1582 BETWEEN STR 38L AND STR 38R NUT PLATE DOUBLER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.SDR CALA2024081902242Stiffener · crackedEA 5310-07143 REV E OP 001, LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BTW 159 TO 185 FOUND 1EA CRACK. NOSE WHEEL WELL STA 287 LBL 25" VERTICAL STIFFENER REPAIRED AS PER EA 5310-07143 REV E OP003 AND REFER TO CR.3595780 FOR WORK DETAILS.SDR CALA2024081902240Stiffener · crackedRH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BTW WL 159 TO 185 FOUND 1EA CRACKED. NOSE WHEEL WELL STA 287 RBL 25" VERTICAL STIFFENER REPAIRED AS PER EA 5310-07143 REV E OP004 AND REFER TO CR.3595782 FOR WORK DETAILS.SDR CALA2024081600440Wheel · damagedUPON PARKING..LEFT MAIN GEAR SHOWED SMOKE FROM POSSIBLE HYDRAU LIC FLUI D DRIPPING ON THE GEAR 4 PICS ADDED . . . SEE LOGPAGES 8918794 AND 8918788 FOR RECITIFICATION.REF LOGS 8916746 AND 8916737 REPLACE WHEEL 2 REPLACE BRAKE 2 INSPECT WHEEL AXLE 2 FOR HEATINSDR CALA2024081200403Connector · migrated37 38 39 FED EMERGENCY PATHWAY LIGHTS NOT WORKING BOTH SIDES - INVESTIGATE FOUND MIGRATED CONNECTOR AT SEAT 36E CABLE RUN AT SEAT LEG. RE-CONNECTED PLUG, RE-SECURED TRIM AROUND CABLE RUN AT SEAT LEG. ALL EMERGENCY LIGHTS CHKD NORMAL. WITH REF TO CMM 25-23-52 ASDR CALA2024081200402Control Panel · unserviceableSMOKE AND FUMES IN FD WHEN TAKING RWY. AIRCRAFT BACK TO STAND AS SMIKE IN THE COCKPIT NOTICED - FOUND C B N6 OVERHEAD PANEL POPPED, WITH STRONG ELECTRICAL SMELL IN THE COCKPIT.SMELL NOTICED COMING OUT THE L BOTTOM OVHD PANEL, NEAR L RUNWAY TURNOFF LIGHT CTL SWSDR CALA2024081202191Skin · corrodedWHILE WORKING HSTA WORK CARD, OBSERVED CORROSION/BULGING ON THE UPPER SKIN ON THE HORIZONTAL STABILIZER CENTER MAIN STRUCTURE. TRANSCRIBED FROM HAECO GSO NRC 9286005. 08-AUG-2026. PER ECRA 5512-01030 PART 1 INTERIM REPAIR ITEM 2 CREATE LOG PAGE TO PERFORM INSPSDR CALA2024080100345Door · missingPDA 1 #1 ENG NACELLE STRUT PRESSURE RELIEF DOOR MISSING. PICTURE UPDATE TOMC NOTIFIED. NO VISUAL DAMAGE.SDR CALA2024080702177Skin · damagedDURING ACCOMPLISHMENT NR 2114213 WAS FOUND A DAMAGE ON FUSELAGE SKIN LH SIDE BETWEEN STA 1702 AND 1746.125 , STRINGER 24L AND 26L. ITS NECESSARY TAKE ACTION TO PERFORM A REPAIR IAW SRM. TO PERFORM INSPECTION IAW SRM 53-00-01-2R-12 TABLE 202 & DELIVERY, REPEATSDR CALA2024072900299Bearing · failedPOWER IDLE SMELL FROM INOP RECIRC FAN INCREASE ON FLIGHT DECK/CA BIN CABIN ODOR FORM PHOTOS BONDING RESISTANCE CHECK MEASURES .00297 OHMS, WITHIN LIMITS. REF AMM TASK 21-25-01-404-019. PERFORMED INSPECTION FOR ODOR IN FLIGHT DECK/CABIN IN ACCORDANCE AMM 5-51-5SDR CALA2024072502099Escape Hatch · obstructedDURING REMOVAL OF LH OVERWING ESCAPE HATCH REF LOGPAGE 8707327, ESCAPE HATCH DOOR HITS LH CABIN CLASS DIVIDER FRAME PREVENTING CORRECT OPERATION OF EMERGENCY EXIT DOOR. CABIN CLASS DIVIDER ADJUSTED FORWARD ON SERATED PLATE AND CONFIRMATION OF ECAPE HATCH DOOR SDR CALA2024072400275Trans Rectifier · faulted767 FUEL FEED SYSTEM HEALTH CHECK - LH FWD BOOST PUMP - VOLTAGE INBALANCE OF FWD LH FUEL PUMP OUT OF TOLERANCE. LH TRANSFORMER RECTIFIER UNIT REPLACED AS PER AMM 24-32-01-004-001 AND 24-32-01-404-005. LH TRU OP-CHECK TEST OK, FWD LH FUEL PUMP VOLTAGE INBALANCESDR CALA2024072300271Pump · faultedR COMPRESSOR STALLGOT COMPRESSOR STALL AT 2500 FEET SPEED 200KT ON FINAL APPROACH INTO IAD. USE FIM 71-05 TASK 803 FOR TROUBLESHOOTING. WORKED FIM 71-05 THROUGH TO BLOCK 7 WITH NO DAMAGE NOTED.N1 ROTOR SPINS FREELY IN BOTH DIRECTIONS. NO DAMAGE TO FAN CASE RUBSDR CALA2024071800243Access Panel · missingPDA 2 ON AIRCRAFT ARRIVAL, LEFT ENGINE INBOARD PYLON PANEL 436AR MISSING. REPORTING SDR FOR PDA 2.SDR CALA2024071800244Pump · unknownR ELEC HYD DEMAND PUMP AUTO INOP THE PUMP RH DEMAND OPS NORMAL IN ON POSITION. REQUEST DEFERRAL MEL 2911K APPROVED FOR MEL 2911K PLACED RH ELEC HYD DEMAND PUMP ON MEL 2911K AS REQUESTED. DDP FOLLOWED. THIS IS NOT A SDR REPORTABLE EVENT PER THE GMM. ATTEMPTINGSDR CALA2024071700225Screw · missingPOP SCREW UNDER RIGHT WING ROOT MISSING PLEASE SEE PICTURES SCREW UNDER RIGHT WING ROOT INSTALLED IAM AMM 20-00-00 SATIS SCREW REPLACEDSDR CALA2024071700224Screw · missingSCREW MISSING LEFT WING GEARBAY TOP. PICTURE IN ATTACHED PICTURE FROM UPPER WING LH SIDE A/C RELEASED IAW EC/RA#5751-01513 INITIATE A DIP TO PERFORM PART 2 AFT EVERY CYCLE AND PART 3 PERMANENT REPAIR WITHIN 2 FLT CYCLES APPROVED FOR 2 CYCLE DIP WITH TAPE INSPESDR CALA2024071802061Trim System · unknownAFTER TAKEOFF NEEDED ALMOST 8 DEGREES RIGHT RUDDER. TRIED TO ALS O USE AILERON TRIM. NO HELP DEBRIEFIED CREW, BOTH ENGINE EPR WAS SAME PASSED. TRIM TEMPERATURE COMPENSATING LINKAGE. NO DEFECTS FOUND. NO SIGNIFICANT FINDINGS AT THIS TIME. FIM: 27-09 TASK 814,SDR CALA2024071600201Roller · damagedR-2 SERVICE DOOR (AFT. GALLEY) REQUIRES R.I.R. / D.V.I. OF AFT. ROLLER TRACK ASSY. EVERY 15 DAYS PER. EC/RA # 5211-01872 REV. [A]. PART # 2 (INSPECTIONS PROCEDURE) AND PART # 3 (PERMANENT REPAIR PROCEDURE) WITHIN 60 CALENDAR DAYS. [ACFT. # 6458]. REQUEST DIP ASDR CALA2024071102012Frame · corrodedB767-53-3-7036 CAB - STA977 BELOW FLOOR RH S/W O/B FRAME CHORD LWR EDGE (NEAR PRESSURE DECK AREA) FOUND CORROSION . CABIN RH STA977 FRAME OUTER CHORD AT WL186 INTERIM REPAIRED AS PER ECRA5311-03241 REV - PART 1 - INTERIM REPAIR WORK DETAIL ATTACHED FORM 44.000SDR CALA2024071102009Skin · crackedEA 5315-01152 OP001 - 1EA FASTENER HOLE FOUND CRACK ON L1 DOOR CUTOUT AFT CORNER AREA , DETAILS REFER TO ATTACHED REPORT TRANSFER REF HXWO 3270748. L1 DOOR CUTOUT AFT LOWER CORNER LH FUSELAGE SKIN INTERIM REPAIRED AS PER ECRA 5310-08353 REV - PART 1 INTERIM RSDR CALA2024071102007Stringer · corrodedFOUND CORROSION IN STRINGER 28L, BS 368 TO 390.SDR CALA2024070800163Monitor · faultyDURING TAKEOFF ROLL GOT R HYD QTY EICAS. RT HYD QTY INDICATED .4 0. REJECTED T/O CHECKED AND APPROVED FOR DEFERRAL I.A.W. B763MEL 2933E. M PROCEDURE CARRIED OUT AND PLACARD INSTALLED. TOMC APPROVED REF MEL 2933E DEFERRAL 2933E APPROVED. PLACARD INSTALLED *DM* SDR CALA2024081202193Floorbeam · corrodedIT WAS FOUND CORROSION UPPER SURFACE PLATE FLOOR BEAM STRUCTURE STATION 303 LBL 20 TO 54. ( ORIGINATING DOCUMENT NR 2080547)SDR CALA2024070901978Transmitter · faultedLOSS OF L HYD QTY WDM 29-33-11-2. RECONNECTED D38 AND REINSTALLED HYD MON UNIT. INSPECTED LT HYD QTY TRANSMITTER, SUSPECT TRANSMITTER AT FAULT. LT HYD QTY SHOWS 1.00 AT GATE. PERFORMED WIRE HARNESS SHAKEDOWN IAW WDM 29-33-11-2. ALL MEG CHECKED AND CONTINUITSDR CALA2024071102010Skin · crackedEA 5315-01152 OP.002 - 2EA FASTENERS HOLES FOUND CRACK ON R1 DOOR CUTOUT AFT CORNER AREA , DETAIL REF TO ATTACHED REPORT , R1 DOOR CUTOUT AFT LOWER CORNER RH FUSELAGE SKIN INTERIM REPAIRED AS PER ECRA 5310-08354 REV - PART 1 INTERIM REPAIR ATTACHED FORM 44.0SDR CALA2024071001999Skin · crackedB767-54-3-0008 #1 PYL PNL 436BL CUTOUT SKIN FOUND CRACKED. TRANSFER REF. NON-ROUTINE WO.3277610 NR 1 PYLON LH SKIN NO.436BL ACCESS PANEL CUTOUT PERMANENT REPAIRED AS PER EC/RA 5450-02947 REV.- ATTACHED FORM 44-0008 ITEM 1 TO ITEM 33.SDR CALA2024071002000Pressure Deck · deformedB767-53-3-7036 - CABIN STA955 TO 960 RBL35 TO 38 WHEEL WELL PRESSURE DECK WEB UPPER SURFACE FOUND DEFORMED. CABIN STA955 PRESSURE DECK WEB RBL35" DENT AREA INTERIM CREATED LP 8489125 AND 8489205 AND CARRIED REPAIRED AS PER ECRA 5350-02544 REV - ATTACHED FORMSDR CALA2024070500138Trim Switch · faultedSTAB TRIM EICAS CAME ON ON INIT CLIMBOUT PERFORMED TROUBLESHOOTING PROCEDURE FOR STAB TRIM REF FIM 27-48 TASK 809, FAULTING LEFT HYDRAULIC BRAKE PRESSURE SWITCH STAB TRIM MESSAGE NO LONGER ACTIVE REFERENCE LOG PAGE 8475892 FOR ACTION TAKEN. LEFT HYDRAULIC BRAKSDR CALA2024070501964Access Panel · missingPDA 2 DURING WALKAROUND INSPECTION AFTER LANDING, LH PYLON STRUT ACCESS PANEL 436BR MISSING INSTALLED NEW PANEL 436BR REF AMM 12-30-00/201 AND AMM TASK 54-53-01-404-007. GOOD FOR SERVICE.SDR CALA2024070101936Shutoff Valve · faultedJUST AFTER TAKEOFF GOT STARTER CUTOUT CAUTION MESSAGE ON RIGHT S IDE ALSO CHECK ENG START SWITCH YAY ON THE ENGINE IGNITION AND CONT ROL MODULE, M49. REPORT FINDINGS. WHQLM-EMC ARSHAD. 29JUN24. ENG2 SN. 727968, REVIEW HIT L/P8403387-ORD-25JUN, (R ENG SPEED C TSDR CALA2024070201951Access Door · missingENG 1 OUTBOARD NACELLE STRUT ACCESS DOOR 436BL MISSING ON ARRIVAL. PLESE REFER TO LOG 8447087 FOR ACTION.SDR CALA2024070101933Idg · warning lightDEBRIEFED FLIGHT CREW, CREW STATES L GEN DRIVE LIGHT ILLUMINATED ON OVERHEAD IN FLIGHT. PILOTS SELECTED L IDG DISCONNECT SW TO DISCONNECT IDG R BEING 11. 24-20 TASK 804, NO FAILURES/FAULTS DISCOVERED. FOUND SIGNIFICANT OIL LEAKS INSIDE LH ENGINE COWLINGS AND OSDR CALA2024062400071Seal · leakingLOUD HIGH PITCH NOISE IN AFT GALLEY. SOURCE SEEMS TO BE AFT OF G ALLY BEHIND OVEN 711 AREA. CREW TRIED SHUTTING DOWN CHILLERS & OVENS, NO HELP. CREW STATED THE NOISE APPEARED TO BE COMING FROM AFT OF OVENS. INSPECTED GALLEY EQUIP & AREA ABOVE IN OPERATION & SDR CALA2024062400070Bottle · faultedOFF-WING SLIDE INFLATION CYLINDER REGULATOR CHECK - LT OVERWING SLIDE CYLINDER REGULATOR CABLE BALL SUSPECT NOT BEHIND RETAINING SPRING. REGULATOR CABLE BALL FOUND TO BE ON INCORRECT SIDE OF RETAINING SPRING. LT OVERWING ESCAPE SLIDE CYLINDER TO BE REPLACED.SDR CALA2024062400069Chip Detector · missing#2 ENGINE MAGNETIC CHIP DETECTORS (MCD) INSPECTION {B767-72-3-7011} - COMPT NO.4 MCD FOUND MISSING ON INSP SDR AND MATERIAL UPDATE MCD INSTALLED IAW AMM: 79-21-10-424-008-N0.SDR CALA2024062000030Control Unit · unknownALL REAR GALLEY OVEN CIRCUIT BREAKERS POPPED DURING CLIMBOUT SETTING SDR FLAG. INSPECTED BEHIND CB PANEL NO SIGN OF ARCING OR ANY FAULTS T/S PER SSM 25-31-02-102, NO FAULTS FOUND, REMOVED AND REPLACED BOTH RIGHT ELCU S AS PRECAUTIONARY, REF AMM 25-31-03-404-0SDR CALA2024062000035Lamp · blownEMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - RH AISLE EMERGENCY LIGHT ABOVE SEAT 32LK INOPERATVIE. AISLE EMERGENCY LAMP REPLACED AS PER AMM 33-51-05-002-039. NOW OPERATIONAL.PARTS USED: 00-0596-3-2874,QTY :1 PARTS USED: 00-0596-3-2874,QTY :1SDR CALA2024062000034Floorbeam · corrodedPERFORMED PERMANENT REPAIR OF THE FLOOR BEAM UPPER CHORD AT STA 325 AND LBL 54.75 CORROSION AS PER ECRA#5310-08344.SDR CALA2024062000033Stringer · corrodedREPLACED STRINGER 36 LH AS PER SRM 51-40-02-0G-0. SRM REFERENCE 53-8--03-0I-1 ITEM 1 FIG1 SECTION 48 - SHEET 3. MATERIAL BAC1498-144 (CLAD 7075-T6) - PO#9284221.FOR PARTS AND DETAILS SEE ESFR#1036499.SDR CALA2024062000032Stringer · corrodedREPLACED STRINGER 36RH AS PER SRM 51-40-02-0G-0.PARTS REPAIR AND DETAILS AS PER ESFR#1036501.ITEM OK TO SERVICE.SDR CALA2024062000029Stringer · corrodedFOR IDENTIFICATION REFERENCE SEE SRM 53-80-03-0I-1 FIGURE 1, ITEM 7 (MATERIAL BAC1498-143).REMOVED STRINGER AS PER SRM 51-40-02-0G-0 PARAGRAPH 4 AND 7.INSTALLED THE NEW STRINGER AS PER SRM 51-40-02-0G-0 PARAGRAPH #04, #07, #09 AND SRM 51-10-02-0G-0 PARAGRAPH 0SDR CALA2024062101878Frame · corrodedDURING C-CK IN ILN (WILMINGTON, OH) AMES MAINTENANCE FOUND THE L WR CHORD CORRODED LOCATED AT STA 1809.5 BULKHEAD FRAME INSTALLATION(P/N-148T1150-1). CORROSION WAS COMMON TO THE VERTICAL & HORIZONTAL FLANGE AS SHOWN IN FIGURES. DAMAGE WAS RE MOVED BY BLENDING SDR CALA2024062601902Skin · crackedDURING INSPECTION WAS FOUND INDICATION CRACK AT FWD PASSENGER DOOR (LH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21L. THE LATEST REVISION OF ECRA# 5330-07278 ON OR BEFORE THE AC REACHES 37,500 TOTAL FC. ACCOMPLISH REPEAT INSPECTION AT INTERVALSDR CALA2024062601901Bear Strap · crackedDURING INSPECTION WAS FOUND INDICATION CRACK AT FWD SERVICE DOOR (LH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21L. THE CORRECT LOCATION OF THE CRACK IS AT FWD SERVICE DOOR (RH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21R. ISSDR CALA2024061801853Floorbeam · corrodedDURING REMOVAL FLOOR MAT COVERING WAS FOUND A CORROSION AT FLOOR BEAM UPPER CHORD AT STA 325 AND LBL 54.75.(NR002042977).SDR CALA2024061901873Fitting · wornDURING C-CHECK, AMES MAINT DISCOVER ED 2 FASTENER HOLES ON NR 2 PYLON BULKHEAD FITTING WAS WORN & ELONGATED. BOTH INBD & OTBD FASTENER HOLES MEASURED 0.3125" DIA WITH DISTANCE BETWEEN HOLES MEASURING NG 0.250". ATTACHING ANGLE WAS CRACKED & REPLACED. AS TSDR CALA2024061701827Access Door · corrodedAFT FLIGHT CONTROLS BAY ACCESS DOOR 313AL IS CORRODED. REMOVED ALL CORRODED PARTS DEEMED OUT OF LIMITS AND INSTALLED NE W PARTS IAW B767 SRM 51-40-02 ALONG WITH BOEING DWG 148T6602. SE E NON-ROUTINE 170098-0300-0005 FOR DETAILS
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