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 CALA2022011200118Beam · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACSDR CALA2022011000084None · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR BEAM BOTTOM SIDE SEVERAL ANCHOR NUT AREA CORROSION FOUND AT STA1329 BTN RBL16"-RBL29" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF513877 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1329 BETWEEN LBL43 AND RBL43 FLOOR BESDR CALA2022011000083None · corrodedB767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF516482 AND ORIGINATED BY EMP V896820 FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACSDR CALA2022011000105None · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR SUPPORT BEAM BOTTOM SIDE 5EA ANCHOR NUT AREA CORROSION FOUND STA1153 BTN RBL9" TO LBL36" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF510485 AND ORIGINATED BY EMP V896820 AFT CARGO COMPT STA1153 FLOOR BEAM UPPER CHORD REPLACSDR CALA2022011000103Skin · noneSUPPORT TASK - BULK CARGO DOOR OUTER SKIN AFT EDGE PREVIOUS REPAIR DOUBLER HAS DENT. TRANSFER REF. NON - ROUTINE ZHF517134 AND ORIGINATED BY EMP V896888 RII INSPECTED BY HX169509 ADD EMP:V898550 BULK CARGO DOOR OUTER SKIN INTERIM REPAIRED AS PER ECRA 5236-0102SDR CALA2022010700067Shear Tie · corrodedB767-53-3-7056 BULK CARGO COMPT - BELOW FLOOR SHEAR TIE CORROSION FOUND AT STA1540 S37R-S38R AS MARKED TRANSFER REF. NON - ROUTINE ZHF512861 AND ORIGINATED BY EMP V896820 BULK CARGO COMPT STA1540 BETWEEN STR37R AND 38R SHEAR TIE REPLACED AS PER SRM51-10-02 ATTSDR CALA2022010700051Floorbeam · corrodedB767-53-3-7025 FWD CARGO COMPT - FLOOR BEAM UPPER SURFACE CORROSION CRACK AT STA632 BTN LBL30"-LBL32" AS MARKED. FWD CARGO COMPT STA 632 BETWEEN LBL 43 AND RBL 43 FLOOR BEAM UPPER CHORD REPLACED AS PER SRM 51-10-02.SDR CALA2022010700050Floorbeam · corrodedB767-53-3-7154 AFT CARGO COMPT - FLOOR BEAM BOTTOM SIDE SEVERAL ANCHOR NUT AREA CORROSION FOUND AT STA1329 BTN RBL16"-RBL29" AS MARKED. TRANSFER REF. NON - ROUTINE ZHF513877 AND AFT CARGO COMPT STA1329 BETWEEN LBL43 AND RBL43 FLOOR BEAM UPPER CHORD REPLACED ASSDR CALA2022010500035Autothrottle Sys · failedAUTO THROTTLES FAILED TO ENGAGE ON TAKEOFF THRUST MANAGEMENT SYS (INCLUDING A/T SYS) PLACED ON MEL. MEL STICKER AND C/B COLLARED F16 ON THE P11. DOWNGRADED A/C TO "AUTOLAND LIMIT-LAND 2". DISPATCH DESK: 82 NAME: JERRY DATE: 02-JAN-22- NOC SDR CALA2022010500027Transmitter · unserviceableL HYD QTY ZEROINFLT. PRESS NORMAL. INSPECTED LH PYLON AREA FOR ANY EVIDANCE OF LEAK AND EDP ALL DRY REMOVED AND REPLACED LEFT HYD QTY TRANSMITTER I.A.W. M/M NO LEAK NOTED ALSO FLIGHT CNT NO LEK NOTED VERIFIED RESERVOIR 29-33-02-004-001 AND 29-33-02-404-014 UP SDR CALA2022010300008Bracket · corrodedB767-53-3-7077 CABIN - LH STA999 S-16L TO S-17L SHEAR TIE FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130759 AND ORIGINATED BY EMP V926653 CABIN BS999 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FSDR CALA2022010300007Bracket · corrodedB767-53-3-7077 CABIN - S16L - S17L JOINT BRACKET FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130782 AND ORIGINATED BY EMP V923418 CABIN BS977 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-00SDR CALA2021122902478Bracket · corrodedB767-53-3-7077 CABIN - S16L - S17L JOINT BRACKET FOUND CORRODED. TRANSFER REF. NON - ROUTINE LP9130782 AND ORIGINATED BY EMP V923418 CABIN BS977 BETWEEN STR16L AND STR17L SHEAR TIE REPLACED AS PER SRM51-10-02 AND INSTALLED AS PER SRM51-40-02, ATTACH FORM 44-00SDR CALA2021122902469Fitting · crackedAD 2012-15-12, EA 5710-02220 REV.D OP 003 LH UNDERWING LONGERON FITTING TENSION BOLT HOLE INSP FOUND 3EA CRACKS AT 1ST LAYER COUNT FROM AFT TRANSFER REF. NON-ROUTINE ZGY511880 & ORIGINATED BY EMP V924733 RII APPROVED LH UNDERWING LONGERON FITTING (BATHTUB FITTSDR CALA2021122902468Stringer · crackedSTA 1629-1654.5 STR 14AR FOUND 3 EA CRACKS WHILE ACCOMPLISHING EA 5380-01178 OPS 002. REF TABLE 202 REPAIR 7 AND FIG 202 REPAIR 7 DETAIL XIV FOR FLIGHT CYCLES FROM THE REPAIR INSTALLATION, WHICHEVER COME FIRST REINSPECT REQUIREMENTS. IQ THRESHOLD 37500 FLT CYCSDR CALA2021122902467Stringer · crackedAD 2012-15-12, SUPPORT TASK - EA 5710-02220 OP 01 - LH LONGERON FITTING FOUND 1EA CRACK RUNNING AFT APPROX 7/8" IN LENGTH TRANSFER REF. HX NON-ROUTINE LP 9130257 & ORIGINATED BY EMP V924 735 LH LONGERON FTG REPLACED PER EA 5710-02220 REV D OP3 AND OP7 ACCOMPLISDR CALA2021122902466Light · inoperativeB767-33-3-7000 FLT DECK EMER EXIT LT INOP TRANSFER REF. NON-ROUTINE ZGY512623 & ORIGINATED BY EMP V920570 FLT DECK EMER EXIT LT ASSY REPLACED AND CARRIED OUT INSTALLATION TEST RESULT NORMAL PER AMM 33-51-01 WORK ACCOMPLISHED BY MECHANIC V898127 INSPECTED BY V8SDR CALA2021122702455Connector · damaged*EMERGENCY DECLARED*TE FLAP DISAGREE ON APPROACH MOVING FLAPS FROM 5 TO 15 REF FIM 27-51 TREE 809, FSEU BITE FOUND FAULT 27-51104, TE FLAP UPDATE CLARIFICATION FAULT TREES 105, 809, 810 WERE COMPLETED, CORRECTION COMPLETED BITE TEST REF FIM 27-51 TREE 809 FIGSDR CALA2021122702445Battery · inoperativeB767-33-3-7002 SEAT 21 TO 23 DEF EMER LIGHT FOUND DIM TRANSFER REF. NON-ROUTINE ZGY512680 & ORIGINATED BY EMP V920574 SEAT 21 TO 23 LK EMER POWER SUPPLY (M1209) REPLACED AS PER AMM 33-51-07 AND TEST NORMAL AS PER AMM 33-51-07 WORK ACCOMPLISHED BY MECHANIC V934SDR CALA2021122702442Shear Tie · corrodedB767-53-3-7056 BULK CARGO COMPT - BELOW FLOOR SHEAR TIE CORROSION FOUND AT STA1540 S37R-S38R AS MARKED TRANSFER REF. NON - ROUTINE ZHF512861 AND ORIGINATED BY EMP V896820SDR CALA2021122702441Battery · failedB767-33-3-7002 - EMERGENCY BATTERY PACK M9047 SELF TEST FAIL TRANSFER REF. NON-ROUTINE ZGY512672 & ORIGINATED BY EMP V897802 EMERGENCY POWER SUPPLY CHARGER REPLACED AND INSTALLATION TEST NORMAL IAW AMM 33-51-07 WORK ACCOMPLISHED BY MECHANIC V920595 INSPECTED BSDR CALA2021122302433Charger · inoperativeTRANSFER REF. NON-ROUTINE ZGY502632 & ORIGINATED BY EMP V897815 B767-33-3-7000 CABIN OFF-WING SECTION EMER EXIT SIGN NOT ILLUMIN ATED BATTERY CHARGER M1209 REPLACED AND TEST FOUND NORMAL IAW AMM 33- 51-07SDR CALA2021122202426Angle · crackedAD 2005-11-02 - SUPPORT TASK EA 5300-01600 REV.A OP 01, LH 1809 BHD 1EA HOLE FOUND CRACK ON FWD OUTER CHORD LAYER TRANSFER REF. HX NON-ROUTINE LP 9130608 & ORIGINATED BY EMP V913 608 LH STA1809 BHD FWD OUTER CHORD REPAIRED AS PER EA5300-01600 REV A OP2(SEQ 161SDR CALA2021122202420Panel · crackedAD 2005-11-02 - SUPPORT TASK EA 5300-01600 REV.A OP 01, LH 1809 BHD 1EA HOLE FOUND CRACK ON FWD OUTER CHORD LAYER TRANSFER REF. HX NON-ROUTINE LP 9130608 & ORIGINATED BY EMP V913 608 LH STA1809 BHD FWD OUTER CHORD REPAIRED AS PER EA5300-01600 REV A OP2(SEQ 161SDR CALA2021121402365None · crackedEA5300-01606 REV A OP 001 NOSE WHEEL WELL BULKHEAD LH VERTICAL CHORD ABOVE WL159 FOUND 1EA CRACK AS MARKED TRANSFER REF. NON - ROUTINE LP9130522 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 INSPECTED BY V896888 ANSDR CALA2021121402359None · crackedEA5300-01606 REV A OP 001 NOSE WHEEL WELL BULKHEAD LH VERTICAL CHORD ABOVE WL159 FOUND 1EA CRACK AS MARKED TRANSFER REF. NON - ROUTINE LP9130522 AND ORIGINATED BY EMP V914372 LH NOSE WHEEL WELL VERTICAL STIFFENER ON STA287 BETWEEN WL159 INSPECTED BY V896888 ANSDR CALA2021120802302Skin · crackedSUPPORT TASK- EA5725-01003 OP005 AD2018-11-14, 1EA CODE ''A'' FASTENER HOLE FOUND CRACKED AT LHW STR L-6.5 TRANSFER REF. NR LP 9131047 ORIGINATED BY EMP V924732 INTERVALS NOT TO EXCEED 12,000 CYCLES OR 32,000 FH''S (WHICHEVER COMES FIRST) THERE AFTER. DIP REQUSDR CALA2021120802285Skin · noneSUPPORT TASK - BULK CGO DOOR EXTERIOR SKIN FOUND PREVIOUS REINFORCING REPAIR FROM BS 1450 TO 1460 S26L TO 28L TRANSFER REF NON-ROUTINE LP9130969 AND ORIGINATED BY EMP V898549 REPAIRED DOOR REACHES 30,000 TOTAL DOOR FLIGHT CYCLES. PERFORM EQUIVALENT TO ACFT HOUSDR CALA2021120802284Skin · crackedSUPPORT TASK RH PYLON ACCESS DOOR 442AL CUTOUT SKIN FOUND CRACKED TRANSFER REF NON-ROUTINE LP9132040 AND ORIGINATED BY EMP V896826 NO.2 PYLON INBOARD SKIN AT 442AL ACCESS DOOR CUTOUT PERMANENT REPAIRED AS PER ECRA5450-02695 REV A WORK ACCOMPLISHED BY MECHANIC SDR CALA2021120802283Skin · noneSUPPORT TASK- UAL QC PICK UP SHEET- DURING THE AAI RECORD REVIEW NO RECORD OF REPAIR AND NO RECORD TO ACCOUNT FOR THE REINSPECTION OF THE FUSELAGE DOUBLER REPAIR AT FUSELAGE STATION 1809 STR.38L TRANSFER REF NON-ROUTINE LP9132202 AND ORIGINATED BY EMP V913166 SDR CALA2021120802282Skin · noneSUPPORT TASK- UAL QC PICK UP SHEET- DURING THE AAI RECORD REVIEW NO RECORD OF REPAIR AND NO RECORD TO ACCOUNT FOR THE REINSPECTION OF THE FUSELAGE DOUBLER REPAIR AT FUSELAGE STATION 440 STR.32R. FWD OF FWD CARGO DOOR FRAME TRANSFER REF NON-ROUTINE LP9132198 ANSDR CALA2021120602258Skin · noneSUPPORT TASK- UAL QC PICK UP SHEET- DURING THE AAI RECORD REVIEW NO RECORD OF REPAIR AND NO RECORD TO ACCOUNT FOR THE REINSPECTION OF THE FUSELAGE DOUBLER REPAIR AT FUSELAGE STATION 654+110 STR.31R AND STR.33R TRANSFER REF NON-ROUTINE LP9132197 AND ORIGINATED SDR CALA2021120602257Skin · noneSUPPORT TASK- UAL QC PICK UP SHEET- DURING THE AAI RECORD REVIEW , NO RECORD OF REPAIR AND NO RECORD TO ACCOUNT FOR THE REINSPECTION OF THE FUSELAGE DOUBLER REPAIR AT FUSELAGE STATION 654+121 STR.39L AND STR.39R TRANSFER REF NON-ROUTINE LP9132196 AND ORIGINATESDR CALA2021120602256Brake · failedNUMBER 6 BRAKE LEAKING FLUID AND CAUSING SMOKE REMOVED AND REPLACED #6 BRAKE REF AMM 32-41-08,OPS AND LEAK CHEAK OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1368206 SN OFF 0661 IDT CW ON MLG #6 BREAK ROD ,OK TO CONTINUE BRAKE, MLG, CAR OFF 76-3243-9-0002 0SDR CALA2021120602246Skin · noneSUPPORT TASK, DURING AAI RECORD REVIEW, NO RECORD OF REPAIR AND NO RECORD TO ACCOUNT FOR THE REINSPECTION OF THE FUSELAGE DOUBLER REPAIR AT FUSELAGE STATION 1582 TO 1605 AND S-38R TO S-39L.. HAECO LOG 9132200, V913166 ON OR BEFORE THE ACFT ACCUMULATING 37500 TSDR CALA2021120602243Shear Tie · corrodedB767-53-3-7010 - BULK CARGO STA1562 FRAME TO SKIN SHEAR TIE BETWEEN S38L-S39L FOUND CORROSION TRANSFER REF NON-ROUTINE LP9132035 AND ORIGINATED BY EMP V896798 BULK CARGO STA1562 S38L-S39L SHEAR TIE REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM SDR CALA2021112502173Fmc · failedR FMC FAIL ITEM LOCKED BY TOMC ON OTHER FMC INPUT BUS. TMC FINDS NO DATA ON FMC DATA BUS, MCDP P-11, FAULT CLEARED AND UNABLE TO DUPLICATE AGAIN. ....WITH RIGHT FMC. AND REPLACED LEFT FMC WITH NEW PART. S/N NO INFC L-R FMC DATA. CROSS CHANNEL ACTIVITY MONITOR SDR CALA2021112202157Landing Gear · nonePER CREW VERBAL, AFTER TAKE OFF AND GEAR RET. WE HAD MASTER CAUTION WITH GEAR DISAGREE AND GEAR DOORS EICAS. AT SAME TIME AMBER DOORS AND AMBER GEAR ANOUNCIATOR LIGHTS ILLUMINATED. RAN QRH CHECKLIST AND SUBSEQUENTLY LOWERED GEAR WICH PRODUCED NORMAL INDICATIONSDR CALA2021111702123Skin · corrodedREFER NRC L/P 9131558 FUSELAGE STA 1205 STR 36L STRINGER SECTION CUTOFF FOUND ATTACH SKIN CORROSION. TRANSFER REF NR LP 9131765 AND ORIGINATED BY V896890. AFTER REF NDT PART 6, 53-00-06 REPAIR INSP REQUIREMENTS ARE AS FOLLOWS PER SRM 53-00-01-2R-31 RPR 31 TABLSDR CALA2021111702115Stringer · crackedAFT CARGO COMPT STA 1205 S-36L AREA FOUND CORROSION CRACK. TRANSFER REF NR LP 9131558 AND ORIGINATED BY V897013. AFT CARGO COMPT STRINGER 36L BETWEEN STA 1197+120VAND STA 1219 REPAIRED AS PER SRM 53-00-03 REPAIR 2 FIG 201. WORK ACCOMPLISHED BY MECHANIC V897532SDR CALA2021111702109Aileron Sys · malfunctionedON APP W/FLAPS 15 - RT AIL DROOPED FULL AND L AIL AT HALF. TE DISAGREE EICAS. FOR THE RIGHT INBD AILERON IS BYPASSING OR A PROBLEM WITH INBD AILERON DROOP MECHANISM. ITEM LOCKED FOR FURTHER CHECKS. UNLOCKED FOR L/P UPDATE LOGPAGE LOOCKED AS REQ''D. RIGHT INBSDR CALA2021111502105None · corrodedAFT CGO COMPT STA 1285 LBL 24" FLOOR BEAM UPPER CHORD FOUND CORROSION CRACK. TRANSFER REF. HX NON-ROUTINE LP 9131773 AND ORIGINATED BY EMP NO. V896921 AFT CARGO COMPT STA 1285 LBL 20.5 - LBL 25.5 WL 123 FRAME INNER CHORD J SECTION REPAIRED AS PER EC/RA 5360-01SDR CALA2021111102091None · noneCREW REPORT, L MAIN FUEL TANK AND TOTAL QTY INDICATION READING BLANK LEFT FLIGHT DECK FUEL QTY INDICATOR DEFERRED PER B767-300 MEL LEFT FLIGHT DECK FUEL QTY INDICATOR DEFERRED PER B767-300 MEL 2841R.M PROCEDURE COMPLIED WITH. REF LOG PAGE 7401962 FOR 2841R. M SDR CALA2021110802057Wire · damagedDOOR 1L UPPER EMERGENCY LIGHT WIRE BROKEN SECURED TERMINAL END EMERGENCY LIGHTS SYS OPS CHECKS NORMAL REF SWPM 20-10-13SDR CALA2021110502041Beam · elongatedB767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 SDR CALA2021110302031None · noneB767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 SDR CALA2021110302021Beam · noneB767-53-3-0166 CABIN - BS1500 RBL10 FLOOR SUPPORT HOLE ELONGATED AS MARK. TRANSFER REF. NON-ROUTINE LP 9131246 AND ORIGINATED BY EMP V896926. CABIN BS 1500 FLOOR BEAM UPPER CHORD RBL 10 REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201. ATTACHED FORM 44-0008 ITEMSDR CALA2021110102015None · noneAUTO THOTTLES WILL NOT ENGAGE. CREW DEBRIEFED, STATED NO FMA ON EADI. TRIED IN MULTIPLE MODES LOCKED FOR T/S. PER LP 7341532 R IDG STATUS MESSAGE. FURTHER DETAILS AWAITEDSDR CALA2021102001939Idg · lowR GEN DRIVE LT AND EICAS INTEROGATED GCU, FOUND "LOW OIL" MSG. RESET GCU. INSPECTED ENG2 TOPPED OFF 1 & 2IDG''S AFTER ENGINE RUN. IDG, DELTA ''P'' NORMAL, NO BURNT SMELL, SERVICED #2 IDG FOUND LOW PULLED RESET RING ON IDG. RESET FIELD SWITCH, SAFTIED DISCONNESDR CALA2021101801904Spar · crackedB767-06-3-7110 - NO.2 PYLON STA175 RH UPPER SPAR WEB FOUND CRACKED AT HYD TUBE CUTOUT POSITION TRANSFER REF NR LP9131205 AND ORIGINATED BY EMP V896810 RII INSPECTED BY HX126723 ADD EMP:V896826 NO.2 PYLON NAC STA175 RH UPPER SPAR WEB CASE DRAIN TUBE CUTOUT INTE
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