Boeing 767-322
Service difficulty reports · 11,764
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 CALA2021061100828Skin · damagedAIRCRAFT SUSTAINED FUSELAGE DAMAGE FROM GROUND EQUIPMENT AT STA 460 STR 36, 37L. REPAIRED REF ECRA 5330-06835 AND ENR # 000284628SDR CALA2021060900824Bracket · brokenREF AIR RETURN FOR PRESSURIZATION: FOUND GROUND CONDITIONED AIR DUCT SEPARATED AT CLAMP WHERE GROUND AIR ATTACHES TO MAIN DISTRIBUTION DUCT. REF IPC 21-51-01-01 ITEM 335, 345. LABOR UPDATE ALSO FOUND CONDITIONED AIR CONNECTION BRACKET BROKEN, NGS DUCT 47-15-01SDR CALA2021060700810Controller · failedCABIN AUTO ONE PRESSURA TION CONTROLLER FAILURE RESULTING IN CAB IN HIGH ALT WARNING AUTO PRESSURE CONTROL 2 STATUS MESSAGE. CONTROLER FAILS BIT TEST. REMOVED AND REPLACED CABIN AUTO PRESS CONTROLER PER TASK 21-31-02-004-001 AND TASK 21-31-02-404-005. STATUS MSDR CALA2021060200780Hose · damagedRH ENGINE PYLON STRUT HYD HOSE TEMPORARY INSTALLED PER GPM 01-13 -015.DUE TO NO AVAILABILITY OF SOLID LINE. PER GPM 01-13-003 INT ERIM REPAIR MUST BE REPLACED WITH PERMENAT IN 50 FLIGHT HOURS.TH E REPAIR MUST BE CHECKED FOR INTEGRITY AT EACH MAINTENACE OPPORT SDR CALA2021053100766Panel · missingPDA 3 DURING W/A FOUND SMALL WING PANEL MISSING, RT WING LEADING EDGE UNDER THE WING O/B OF #2 ENGINE. REFER TO ORIGINAL LOG PAGE 6343710. THIS LOG PAGE WAS CREATED TO INCLUDE PDA INFO. REPLACED PANEL 621CB REF IPC 57-41-10. TOMC HAS BEEN NOTIFIED.SDR CALA2021053100763Screw · missingPDA 3 FOUND 2 SMALL SCREWS MISSING FROM RIGHT ENG PYLON INBORD SIDE REPLACED 2 MISSING SCREWS AS REQ OK TO CONTINUESDR CALA2021053100757Warning Message · illuminatedRUDDER RATIO EICAS MESSAGE ON DURING CLIMB REPLACED RH RUDDER RATIO MODULE REF AMM 27-09-00, CLEARED EICAS MSG. APPLY PLA 02700 TO ECS MAINTENACE MESSAGE. MAINT MSG FOR RUDDER RATIO, PLA 02700 APPLIED IPC REFERENCE 27-09-01 APPLIED PLA TO ECS RUDDER RATIO MASDR CALA2021052600735Skin · crackedB767-53-3-7064 - LOWER HALF FUSELAGE STA 1438 BETWEEN S38R-S39R HAS CRACK REF NRC 9130394, SKIN DAMAGED AREA TRIMMED OFF PER SRM 53-00-01- 2R-29 REAPIR FIG 201. SKIN THICKNESS IS 0.056". HFEC CARRIED OUT PER B767 NTM PART6 51-00-19 REV 125, NO CRACK FOUND. REPSDR CALA2021051900698Sensor · faultedON APP ICAS LE SLAT ASSY MESSAGE ON ICAS COMPLIED WITH QRH AND L ANDED BIT THE FSEU AND FOUND THE FOLLOWING FAULT: LE OUTBD ASYM MSG NO. 27-81021. FDE LE ASYM LATCHED. PRIMARY A/S <90 A-A02 FR PSEU, IB SLAT +1.21V, OB SLAT +5.54V, LRV POS -2.33V. INTERROGATED SDR CALA2021051700667Fuse · intermittentON TAKEOFF WHEN THE GEAR HANDLE WAS THE GEAR DOORS EICAS AND GEAR DISAGREE DISPLAYED, THE RIGHT MLG DID NOT INDICATE RETRACTED. CREW RAN CHECKLIST PERFORMED PSEU BITE & FOUND FAULT 264 ''R LATCH LOCKED''. PERFORMED PROXIMITY SENSOR LATCH LOCKED SENSOR TEST. SDR CALA2021051000632Hydraulic Line · leakingDURING CHECK NO 2 SERVICE HMG BLOCK 8 OPRATIONAL CHECK FOUND HYDRAULIC LEAK THRU BODY OF HMG. PERFORMED INTERIM REPAIR PER ECRA 2420-01623 PART 1. HYD LINES PLUGGED ,UNIONS REMOVED NO LEAKS NOTED FROM HYDRAULIC LINES PRESSURIZED.INITIATE A DIP TO PERFORM PERMASDR CALA2021051000630Skin · debondedB767-06-3-7222 RHW I/B AFT FLAP UPPER AND BOTTOM SURFACE FOUND DISBOND - REFER NR LP 9130574. RHW I/B AFT FLAP DISBOND AREA PERFORMED REPAIR AS PER EC/RA 5752-01851 REV - REFER FORM 44-0008 ITEM 1-29 ACCOMPLISHED ADD EMP:V912779 RII INSPECTED OK BY HX198855 RSDR CALA2021051000622Rib · damagedRH HORIZONTAL STABILIZER TIP DAMAGED REMOVED DAMAGED TIP CAP (348AR) REPLACED TIP ASSY. REF AMM 55-11-01-404-005 THROUGH ITEM F 1E, WILL ALSO NEED EDGE SEAL. ACCOMPLISHED AMM55-11-01-404-005 PAGE 2OF2 ITEM F (1) (F)&(H) ACCOMPLISHED EDGE SEAL AND INSTALLATION SDR CALA2021050600618Hydraulic System · leakingIN REFERENCE LOG PAGE 625880 HMG INOP. IN REFERENCE LOG PAGE 6258880 HMG INOP DEFERRED PER MEL 2425A. ADD EMP:U288719,U235671 DISPATCH DESK: 76 HMG CAPPED DUE TO HYD LEAK PER ECRA 2420-01623 LOG PAGE 6258880 . NO LEAKS WITH LINES AND HMG CAPPED 64-2425-9-0001SDR CALA2021050300595Skin · chafedB767-53-3-7093 FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BL, 322AL , 323AL, 324AL, IS CHAFFED FROM THE PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. REF AMES NR 0446 AND UAL JOB CARD 63-5330-1-2602 ADD EMP:V92955SDR CALA2021050300594Skin · chafedREF AMES NR 0448 AND UAL JOB CARD 63-5330-1-2602. B767-53-3-7093 AFT FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BR, 322AR, 323AR, 3 24AR IS CHAGGED FROM PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. ADD EMP:V92955SDR CALA2021050300589Skin · corrodedB767-53-3-7058 - BULK CGO STA1540 TO 1545 CTR BOTTOM DRAIN VALVE AREA SKIN FOUND CORROSION.REF NR LP 9130687 BULK CGO STA1540 TO STA1545 BETWEEN S39L AND S39R FUSELAGE SKIN REPAIRED AS ECRA 5361-01084 REV- PART 1 INTERIM REPAIR AND ATTAC H FORM 44-0008 MAINTENSDR CALA2021043000587Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK INOP AT 44LK. REPLACED BATTERY PACK AS PER AMM 33-51-07-422-012. OPS CHECKED GOOD.SDR CALA2021043000586Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK INOP AT 43LK. REPLACED BATTERY PACK AS PER AMM 33-51-07-422-012. OPS. CHECKED GOOD.SDR CALA2021043000585Battery Pack · inoperativeEMERGENCY LIGHT BATTERY PACK INOP AT 38LK. REPLACED BATTERY PACK AS PER AMM 33-51-07-422-012. OPS. CHECKED GOOD.SDR CALA2021043000584Skin · corrodedCORROSION DAMAGE WAS FOUND ON FUSELAGE INTERNAL SKIN, PN 1146T3241-12, JUST AFT OF STA 1540 BETWEEN S39L & 39R IN THE AREA WHERE A DRAIN VALVE AND AN EXISTING REPAIR EXIST. AMOUNT OF MATERIAL REMOVED TO CLEAN THE DAMAGE EXCEEDS LIMIT 0.15T IAW 767-300 SRM 53-0SDR CALA2021042800562Skin · corrodedB767-53-3-7058 - BULK CGO STA1540 TO 1545 CTR BOTTOM DRAIN VALVE AREA SKIN FOUND CORROSION.REF NR LP 9130687 BULK CGO STA1540 TO STA1545 BETWEEN S39L AND S39R FUSELAGE SKIN REPAIRED AS ECRA 5361-01084 REV- PART 1 INTERIM REPAIR AND ATTAC H FORM 44-0008 MAINTENSDR CALA2021042800556Frame · damagedB767-06-3-7007 BULK CGO DOOR INTERNAL LOWEST FRAME FOUND CHIPPED REF NR LP 9130524 BULK CGO DOOR INTERNAL LOWEST FRAME REPLACED AND INSTALLED AS PER SRM 51-10-02 AND SRM 51-40-02 AND ATTACH FORM 44-0008 MAINTENANCE WORKSHEET ITEM 1 TO 24 ACCOMPLISHED ADD EMP:VSDR CALA2021042600550Seal · missingPAX INFORMED US WHEN FLAPS WERE LOWERED ON FINAL A PIECE OF RUBBER CAME OFF LT WING INSPECTED LEFT WING FOR MISSING SEALS. FOUND UPPER SEAL LOCATED NEXT TO OUTBOARD SIDE OF THE INBOARD AILERON MISSING, LOCATED AT APPROX WING STATION 534. REF L/P 6194234 FOR MISDR CALA2021041600468Lock · inoperativeCOCKPIT DOOR ENTRY LOCK SYSTEM INOP CB T4 OUT FLIGHT DECK DOOR LOCK LATCH HAS BURNING ODUR. ATTEMPTED TO RESET C/B BUT C/B TRIPS AFTER 2 SECONDS. BACK OF C/B INSPECTED FOR SIGNS OF OVERHEATING NONE FOUND. FLIGHT DECK DOOR ACCESS SYSTEM MEASURE.DOOR DEADBOLT VESDR CALA2021040600428Indicator · fluctuatesLOST ALL HYD FLUID RIGHT SIDE QTY SHOWING 0.00 REQUEST DEFERRAL. REQUIRES CHECK IAW AMM 29-33-99-601 APPROVED MEL 2933F VERFIED QTY ON ARRIVAL OK. NO PRESS WAS LOST DURIND QTY FLUX. SERVED TO FULL.SDR CALA2021040500420Tat Probe · faultedTAT PROBE MESSAGE ON LIFTOFF FOUND CB P63 GRID L 18 "L TAT" PROBE HEAT OPEN. CLOSED CB AND PERFORMED OPS CK REF AMM 34-12-02-404-008. CB REMAINED CLOSED THROUGH OUT TEST. AS PRECAUTION REPLACED K411 LEFT TAT PROBE CURRENT SENSING RELAY IN P33 PANEL. ALSO PERFOSDR CALA2021033000384Skin · corrodedBULK CGO COMPT AT STA 1540 BILGE AREA S-39L DRAIN HOLE AREA FOUND CORROSION REFER NR LP 9131172 BULK CGO COMPT STA 1540 BTW S39L TO S39R WATER DRAIN VALVE AREA SKIN INTERIM REPAIRED AS PER ECRA 5361-01082 REV - ADD EMP:V897545 RII BY HX 102369SDR CALA2021033000383Shear Angle · corrodedBULK CARGO STA 1540 BETWEEN S39L TO S39R SHEAR TIE FOUND CORROSION REF NR LP 9131299 BULK CARGO STA 1540 BTW S39L TO S39R SHEAR TIE REPLACED AS PER SRM 51-10-02 AND NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02 ADD EMP:V906027 RII OK BY HX 102369SDR CALA2021033000382Shear Angle · corrodedBULK CARGO STA 1540 BETWEEN S38L TO S39L SHEAR TIE FOUND CORROSION CRK REF NR LP 9131280 BULK CARGO STA 1540 BTW S38L TO S39L SHEAR TIE REPLACED AS PER SRM 51-10-02 AND NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02 ADD EMP:V906027 RII OK BY HX 102369SDR CALA2021032600374Stringer · corrodedBULK CGO COMPT BILGE AREA AT STA 1540 TO 1546 S39L STRINGER FOUND CORROSION AS MARKED REFER NR LP 9131240 BULK CGO COMPT STA 1540-1546 S39L STRINGER PERMANENT REPAIRED AS PER ECRA 5360-01594 REV - ADD EMP:V897545 RII BY HX 102369SDR CALA2021032600373Stringer · corrodedBULK CGO COMPT BILGE AREA AT STA 1540 - 1546 S39R STRINGER AREA FOUND CORROSION AS MARKED REFER NR LP 9131241 BULK CGO COMPT STA 1540-1546 S39R STRINGER PERMANENT REPAIRED AS PER ECRA 5360-01594 REV - ADD EMP:V897545 RII BY HX 102369SDR CALA2021032200353Floor Support · corrodedREF AMES NR 0869. DURING PANEL INSTALL FOUND CORROSION ON FLOOR PANEL SUPPORT FRAME AT STA 1197+88 FLOOR PANEL SUPPORT FRAME BLENDED TO REMOVE CORROSION AT STA 119 7+88 ORIGINAL THICKNESS .063" MATERIAL REMOVED .030" REMAINING T HICKNESS .033". FOUND TO BE OUTSDR CALA2021031900344Actuator · failedCABIN AUTO INOP EICAS B THERE IS A FAILURE OF THE NO. 1 AND 2 AUTOMATIC PRESSURIZATION C ONTROLLERS OR THE PILOT CHANGED TO MANUAL PRESSURIZATION CONTROL . 0 UPDATE TO INDICATE FLT 0252 DELAY. CONTROLERS SHOW AC MOTOR FAILURE. REPLACED OUTFLOW ACTUATOR PER AMMSDR CALA2021031900343Floorbeam · corrodedREF AMES NR 0869. DURING PANEL INSTALL FOUND CORROSION ON FLOOR PANEL SUPPORT FRAME AT STA 1197+88 FLOOR PANEL SUPPORT FRAME BLENDED TO REMOVE CORROSION AT STA 119 7+88 ORIGINAL THICKNESS .063" MATERIAL REMOVED .030" REMAINING T HICKNESS .033". FOUND TO BE OUTSDR CALA2021031900342Skin · crackedREF AMES NR 0428. EA 5380-01178 REV A OP 2 R/H AFT EXTERIOR FUSE LAGE SKIN STA 1680 STRINGER 12R IS CRACKED (VERIFIED WITH HFEC S URFACE SCAN) REPAIRED FUSELAGE SKIN CRACK R/H STA 1680 STRINGER 12R IAW AMES REA DOC 47453REA02. SEE PARTIAL WORK ACCOMPLISHED ON SDR CALA2021031900337Floorbeam · corrodedREF AMES NR 0867. DURING PANEL INSTALL FOUND CORROSION ON STATIO N 1197 FLOOR PANEL SUPPORT FRAME REMOVED CORROSION STA 1197+110 ORIGINAL THICKNESS .063" REMOVED .050" FOUND TO BE OUT OF LIMITS REPLACED INNER CHORD IAW B767 SR M 53-00-07 AND BOEING DWG 146T106SDR CALA2021031900336Skin · crackedREF AMES NR 0460. THE FUSELAGE SKIN IS WORE THROUGH AND CRACKED AT THE FWD LWR EDGE OF THE CUTOUT FOR THE HOR STAB ON THE RIGHT SIDE REPAIRED FUSELAGE SKIN ON THE FWD LOWER EDGE OF CUTOUT FOR HORZ STAB IAW B767 SRM 53-60-01 REPAIR 3. SEE BACK AND PARTIAL WORKSSDR CALA2021031000291Wire · shortedUPON ARRIVAL TO ACP BITE 24-20-00-810-801. AND RECORD YOUR FINDING. NEED TO CONNECT DRIVE AND INSPECT TERMINAL CONNECTIONS TO RIGHT IDG. RUN ENGINE AND CHECK FOR VOLTS AND FREQS. ALSO, CHECK FOR ADDITIONAL EICAS MSG. CARRIED BY ELB LOCKED LP . CONTACT TOMC WITSDR CALA2021030800274Skin · crackedCRACK FOUND APPROX 1.125" LONG AT STR13AL BETWEEN BS1654-1674 WHILE ACCOMPLISHING EA 5380-01178 OPS 001 SKIN INSPECTION. FUSELAGE SKIN CRACK REPAIRED BETWEEN STA1654-1674 STR 13AL IAW SRM 53-80-01 REPAIR 7 FIG 201 DETAIL VII CAT B REPAIR. REF TABLE 202 FOR IQ SDR CALA2021030800273Stringer Splice · crackedB767-53-3-7154 AFT CGO STA 1300-1307 S-38R SPLICE FOUND CORRODED AND CRACKED REF NR LP 9131244 AFT CARGO STA 1300 TO STA 1307 S38R STRINGER SPLICE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 AND ATTACH FORM 44.0008 ITEM 1-6 ACCOMPLISHED.SDR CALA2021030500259Floorbeam · corrodedB767-53-3-7062 CABIN STA 325 LBL 53 FLOOR BEAM FOUND CORRODED AS MARKED REF NR LP 9131170 CABIN STA 325 LBL 30" TO LBL 60" FLOOR BEAM REPLACED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND ATTACH FORM 44.0008 MAINTENANCE WORKSHEET ITEM 1-30.SDR CALA2021030100247Skin · cracked63-5530-1-2500 L/H EXTERIOR FUSELAGE SKIN STA 1654.5 BETWEEN STR INGER 3L-4L IS CRACHED VERIFIED WITH HFEC REPAIRED CRACKS AT STA 1654.5 BETWEEN S3-4LT IAW 767 SRM 53-80-0 1REPAIR 4 AND REA 47451REA 05 AND ECRA 5380-01277.SDR CALA2021030100246Skin · crackedRH EXTERIOR FUSELAGE SKIN AT STA 1660 STRINGER 13R SKIN IS CRACK ED REPAIRED CRACK AT STA 1660 AND 13R IAW 767 SRM 53-80-01 REPAIR 7 .SDR CALA2021030100245Skin · crackedSUPPORT TASK AFT EXTEROR R/H FUSELAGE SKIN STA 1654.5 BETWEEN STRIGNER 3R-4R IS CRACKED.(VERIFIED WITH HFEC SURFACE SCAN) AFT EXTERIOR RH FUSELAGE SKIN STA 1654.5 TO STRINGER 3R-4R ID 0717075T6 PO# 0167028 TAG# 2760222 FILLER MAT''L ID .032 707ST6 IAW B767 SRSDR CALA2021022200211Skin · crackedRIGHT EXTERIOR FUSELAGE SKIN AT STA 1660 STRINGER 13R SKIN IS CRACKED. REPAIRED CRACK AT STA 1660 AND 13R IAW 767 SRM 53-80-01 REPAIR 7. SEE PARTIAL WORK ACCOMPLISHED FOR WORK PERFORMED. LOG PAGE OPEN. MORE DETAILS AWAITED.SDR CALA2021021900187Skin · corrodedBULK CARGO - STA 1542 STR 39 BL0 WATER DRAIN VALVE SURROUNDING SKIN FOUND CORR REFER NR LP 9131165 BULK CARGO STA 1542 STR 39 BLD WATER DRAIN VALVE SKIN AREA. REPLACED AS PER ECRA 5360-01578 REV - PART 1 INTERIM REPAIR ADD.SDR CALA2021021700185Skin · dentedB767-53-3-7006 BULK CGO - CGO DOOR EXTERIOR AREA STA 1461 EXISTING PATCH FOUND DENT AS MARKED REF NR LP 9130916 ACCOMPLISH INITIAL INSPECTIONS AS DEFINED IN LATEST REVISION EC5236-01021 PART 2 ON OR BEFORE THE BULK CARGO DOOR REACHES 30,000 FLT CYCLES. PERFORMSDR CALA2021021700184Shear Tie · corrodedB767-53-3-7058 BULK CARGO - STA 1540 STR 38R-39R INTERNAL SHEAR TIE FOUND CORR REF NR LP 9131254 BULK CARGO STA 1540 STR 38R-39R SHEAR TIE REPLACED AS PER SRM 51 -10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.SDR CALA2021021700183Shear Tie · corrodedB767-53-3-7154 AFT CGO - STA 1219 BILGE AREA S36R - S38R SHEAR TIE FOUND CORRODED AS MARKED REF NR LP 9131157 AFT CARGO STA 1219 S36R-S38R 2EA SHEAR TIE REPLACED AS PER SRM 5 1-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02
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