Boeing 767-33A
Service difficulty reports · 1,978
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 = '76733A' 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 = '76733A' 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 HALA2010031400104Warning Light · false activationETOPS SIGNIFICANT SYSTEM, APU BATTERY CHARGER DISPLAYED ON STATUS PAGE. PERFORMED FIM 24-31-00-101 FIG 104. OPER CHECK OK NO FAULTS NOTED.SDR HALA2010031300108Indicator · stuckETOPS SIGNIFICANT SYSTEM - LT SIDE FLAP IND POINTER GOT STUCK AT 15 DEG, WHEN FLAPS GOING DOWN. TROUBLESHOT PER FIM 27-58-00/101 FIG 103. NO FAULTS FOUND. ALL OPERATIONS AND INDICATIONS NORMAL, THE SYSTEM CHECKS OK PER THE FIM.SDR HALA2010031300106Oil System · lowETOPS SIGNIFICANT SYSTEM - EICAS MX LEVEL MSG 'IDG OUT TEMP' AFTER 2+45 IN CRUISE IDG OUT L-63 R-89 IDG RISE L-7 R-11. BITE BPCU. NO FAULTS NOTED. RESERVICED IDG OIL. ACCOMPLISHED FIM 24-20-00/101 FIG 103. MESSAGE CLEARED, OK FOR SERVICE.SDR HALA2010030900097Warning Light · illuminatedOPEN - ETOPS SIGNIFICANT SYSTEM. ATO, ON TAKE OFF ROLL RT EICAS HPSOV INDICATION ILLUM. OK TO CONTINUE PER 36-11-2.SDR HALA2010030800093Adc · malfunctionedETOPS SIGNIFICANT SYSTEM - FRM 34129100 RECEIVED "ALT DISAGREE" MESSAGE F/O'S ALTIMETER OUT OF TOLERANCE W/CAPTS' ALTIMETER. REPLACED RT ADC PER AMM34-12-01, OPS CK OK.SDR HALA2010030800092Inverter · malfunctionedETOPS SIGNIFICANT SYSTEM - STATUS MSG "STBY INVERTER". REPLACED STANDBY INVERTER PER AMM 24-33-03. OPS CHECK OK. MESSAGE CLEARED.SDR HALA2010030700090Circuit Card · malfunctionedETOPS SIGNIFICANT SYSTEM - WARN ELEX STATUS MSG DISPLAYED. T/S PER FIM 31-51-00/101 FIG 105. REMOVED AND INSTALLED STALL WARNING CARDS IAW AMM 31-51-04-004-113. TESTED NEW CARD MODULE IAW AMM 31-51-04-724-154, MSG CLEARED DID NOT RETURN.SDR HALA2010030700088Inverter · malfunctionedETOPS SIGNIFICANT SYSTEM - PRIOR TO DEPARTURE RECIEVED STATUS MSG. "STBY INVERTER". ACCOMPLISHED FIM 24-33-00 FIG 106. CHECK OKAY.SDR HALA2010030600098Indicator · malfunctionedETOPS SIGNIFICANT SYSTEM, F/O ALTIMETER READS 160' LOW WHEN LEVEL AT 36000'. F/O AIRSPEED ALSO LOW C AND F/O SYS PER AMM 34-11-00. OPS CK OK. BOTH SYS ARE WITHIN LIMITS.SDR HALA2010030600089Altimeter · reads lowETOPS SIGNIFICANT SYSTEM - F/O ALTIMETER READS 160' LOW WHEN LEVEL AT 36000'. F/O AIRSPEED ALSO LOW COMPARED TO CAPT AS .810 VS .802 IAW 269 VS 267. PERF PITOT SYS TEST ON CAPT AND F/O SYS PER AMM 34-11-00. OPS CK OK. BOTH SYSTEMS ARE WITHIN LIMITS. COMPLSDR HALA2010030500087Warning Message · illuminatedETOPS SIGNIFICANT SYS - PRIOR TO PUSHBACK STBY INVERTER MESSAGE ON EICAS. PERFORMED FIM IAW 24-23-00. STBY INVERTER EICAS EXTINGUISHED. OK TO CONTINUE.SDR HALA2010030200084Seal · leakingETOPS SIGNIFICANT SYS - DURING REMOVE NR 2 ENG STARTER FOM FOUND START DRIVE PAD SEAL LEAKING. R & R NR 2 ENG STARTER DRIVE PAD SEAL IAW AMM 72-61-03-5755. OPS & LEAK CHECK OK. OK FOR SERVICE.SDR HALA2010030100082Skin · damagedFOUND DAMAGE TO RT WING OTBD AILERON PANEL NR 661NB (3) CORNER SCREWS PULLED THRU DUE TO HAMMER FOUND INSIDE PANEL AREA (DAILY INSP REQ). OK TO CONTINUE IAW M105 NR 589041. CORNER SCREWS PULLED THRU DUE TO HAMMER FOUND INSIDE PNL AREA (DAILY INSP REQ). PICKSDR HALA2010022500079Engine · surgesETOPS SIGNIFICANT SYS - ENG 1 GAS PATH ADVISORY REPORT: SURGE, VIA ACARS. IAW FIM 71-05-00/101 FIG 103 SH1. NO CREW REPORT OR OBSERVATIONS OF NO 1 ENG. IAW FIM NO CORRECTIVE ACTION NECESSARY. NOTE:(INSPECTED ENG INLET AND EXHAUST NO DEFECTS FOUND).SDR HALA2010022400075Generator · trippedETOPS SIGNIFICANT SYSTEM - APU GEN FAILED TO COME ON LINE WHEN ENGINES SHUT DOWN FIELD RELAY WAS TRIPPED ON SIDE CONSOLE. REMOVED AND REPLACED APU GEN PER AMM 24-21-01-024-001 AND 24-21-01-424-002 CHECK GOOD PER AMM 24-21-00-715-001.SDR HALA2010022300076Controller · faultedETOPS SIGNIFICANT SYSTEM - EICAS MAINT MSSG LT PACK BITE. LT PACK CONTROLLER FAULTED LOW LIMIT VALVE, T/S IAW FIM 21-51-00 FIG 103 VERIFY INDICATED NO FAULTS CLEARED MEMORY.SDR HALA2010022300074Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, ATTEMPTED AUTO LAND IN PDX ILS 10R AFTER GS INTERCEPT AIRCRAFT STARTED PITCHING SMALL AT FIRST THEN LARGER AMBER LINE APPEARED THROUGH GLIDE SLOP WINDOW ON THE FMA AUTOPILOT DISCONNECTED. T/S PER FIM 22-00-02-1 FAULT ISOLATION LAST FSDR HALA2010022300073A/C Pack · unknownETOPS SIGNIFICANT SYSTEM - LEFT PACK SHUT DOWN IN FLIGHT FOLLOWED BY A L PAC TEMP EICAS SELECTED STANDBY - N WAITED 5 MINUTES THEN RESET PAC. PAC OPERATED NORMAL IN STBY- N. PERFORMED BITE OF L PACK CONTROLLER PER FIM 21 51 00/101, NO FAULTS ON CONTROLLER OPSDR HALA2010022100072Warning Light · false activationETOPS SIGNIFICANT SYSTEM - L PACK OFF LIGHT ILLUMINATED. EICAS MESSAGE "PACK OFF LIGHT" DISPLAYED, OPERATED NORMAL AFTER STBY SELECTED. T/S AS PER FIM 21-51-00/101 FIG 103 BLOCK 1 CHECKS OK ALL THE WAY THROUGH FIM 21-51-00/101 FIG 103 SHEET 5 BLOCK 8 OPS NORSDR HALA2010021100062Autopilot Sys · unknownETOPS SIGNIFICANT SYSTEM - TUNED AND IDENTIFIED APPROACH ARMED, AUTOPILOT AND FLIGHT DIRECTOR WOULD NOT CAPTURE LOCALIZER OR GLIDESLOPE, NO GLIDESLOPE INDICATION ON ADI. PERFORMED LOCALIZER, GLIDESLOPE AND ILS TEST WITH CURRENT CALIBRATED RAM TEST SET T-300 BSDR HALA2010020900055Idg · malfunctionedETOPS SIGNIFICANT SYSTEM - ATB - RT GEN DRIVE LT AND RT GEN LT. REMOVED AND REPLACED RT IDG PER TASK CARD 767-3-405001. RUN AND LEAK CHECK OK. OK FOR SERVICE.SDR HALA2010020800053Controller · malfunctionedETOPS SIGNIFICANT SYSTEM -CABIN PRESSURIZATION UNABLE TO MAINTAIN SCHEDULE ALTITUDE AT FL 380 W/ENG ANTI ICE ON. DUCT PRESS 15 PSI, OUTFLOW VALVE FULLY CLOSED, CABIN CLIMB AT 300 FPM REACHED 8500' (SCHED IS 6500') COND SAME IN AUTO1 OR AUTO2 W/ENG ANTI-ICE OFSDR HALA2010012100038Starter · making metalETOPS SIGNIFICANT SYSTEM, DURING RT ENG STARTER MAGNETIC CHIP DETECTOR INSP. FOUND UNWANTED METAL MATERIAL. REMOVED AND REPLACED RT ENGINE STARTER PER AMM80-11-01-004-001-N00 AND AMM80-11-01-404-014 N00.SDR HALA2010012000037Wire · damagedETOPS SIGNIFICANT SYSTEM - "L ENG FIRE LP2" EICAS MSG ON STATUS PAGE. RETERMINATED WIRE AT NR 1 ENG LP2 LWR AFT DETECTOR ELEMENT, OPS CK OK PER AMM 26-71-00.SDR HALA2010011800036Controller · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MESSAGE FWD CABIN TEMP. TEST CABIN TEMP CONTROL IAW BFIM 21 61 00 FIG 404, SYSTEM OK.SDR HALA2010011800034Engine · fluctuatesETOPS SIGNIFICANT SYSTEM - LEFT PRIM ENG EPR FLUCTUATES +/- 0.02 N1 FLUXES +/-0.01 FUEL FLOW FLUXES +/- 0.1. TROUBLESHOT PER FIM 77-11-00-1 FIG 103. NO FAULTS NOTED OPERATED ENGINE MULTIPLE TIMES NO FLUCTUATIONS NOTED ON GROUND. ALL PARAMETERS NORMAL. NO 9SDR HALA2010011700035Indicator · failedETOPS SIGNIFICANT SYSTEM, TCAS FAILED DURING DESCENT. TROUBLESHOT TCAS PER FIM 34-45-00-1. NO FAULTS PER FIM. TCAS SYSTEM TEST OK. SYSTEM OK PER FIM.SDR HALA2010011600032Display · inoperativeETOPS SIGNIFICANT SYSTEM - NR 1 MCDU, NO DISPLAY. REPLACED NR 1 MCDU. OPS CHECK OK PER M/M 34-61-00.SDR HALA2010011500033Anti-Ice Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, LEFT ENG ANTI ICE STICKS IN THE ON POSITION. EXERCISED VALVE MANUALLY FOR LEFT ENG ANTI ICE VALVE. REMOVED, INSPECTED, CLEANED AND REINSTALLED C/P FOR ANTI ICE VALVE. ALL INDICATIONS NOW NORMAL. OK FOR FURTHER SERVICE.SDR HALA2010011400023Fan · inoperativeETOPS SIGNIFICANT SYSTEM - FOUND OVERNIGHT CHECK AFT VENT FAN AFT CARGO CENTER NR 1 INOP. REMOVED AND REPLACED VENTILATION FAN NR 1 WITH A SERVICEABLE UNIT IAW AMM 21-26-01. OPS CK GOOD.SDR HALA2010011400022A/C Pack · shutdownETOPS SIGNIFICANT SYSTEM - LEFT PACK OFF AND LEFT ENG BLEED SHUT OFF AFTER REDUCING POWER AT DESCENT RESET BLEED AND PACK AND OPERATIONS RETURNED TO NORMAL. PERFORMED FIM 21-51-00. BITE PACK TEMP CONTROLLER, NO FAULTS NOTED. OPS CHECK GOOD ON GROUND. OK TOSDR HALA2010011400021Shutoff Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - "R"-DUCT PRESS-(PNEUMATIC) GAGE INDICATED LOW - (ON CLIMB OUT AND CRUISE) 13 PSI (LEFT SIDE=32PSI). REMOVED AND REPLACED RT PRSOV PER AMM 36-11-09. LEAK CHECK OPS CHECK OK. OK FOR SERVICE.SDR HALA2010011300020A/C Pack · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT PACK OFF AND LEFT ENGINE BLEED SHUT OFF AFTER REDUCING POWER AT DESCENT. RESET BLEED AND PACK, OPERATIONS NORMAL. PERFORMED FIM 21-51-00. BITE PACK TEMP CONTROLLER, NO FAULTS NOTED. OPS CHECK GOOD ON GROUND. OK TO CONTINUE.SDR HALA2010011300018Controller · malfunctionedETOPS SIGNIFICANT SYSTEM - FWD CABIN TEMP INOP LIGHT DISPLAYED ON EICAS AND OVERHEAD. RESET ZONE TRIM CONTROLLER AND OPS NORMAL.SDR HALA2010011200017Engine · malfunctionedETOPS SIGNIFICANT SYS - WITH ENG EPR MATCHED RT ENG PARAMETERS HIGH N2 LOW IN CLIMB/ CRUISE. ALL PARAMETERS WITHIN AMM LIMITS REF 71-00-00-802-063-N100. NOTIFIED ENGINEERING AND MOC OK FOR SVC.SDR HALA2010011200016Starter · failedETOPS SIGNIFICANT SYS - APU FAILED TO START ON GROUND. T/S IAW FIM 49-11-00 FIG 105 REPLACED STARTER MOTOR IAW AMM 49-41-01, OP TEST GOOD. NO FAULTS, OK FOR SERVICE.SDR HALA2010011200014Fire Loop · false activationETOPS SIGNIFICANT SYS - EICAS MSG L ENG FIRE LP 2 DISPLAYED. T/S IAW FIM 26-11-00/101 INSPECTED FIRE LOOPS ON ENG NO TROUBLE FOUND- MSG CLEARED AND DID NOT RETURN SYS CHECKS OK.SDR HALA2010010900015Display · malfunctionedETOPS SIGNIFICANT SYS - STATUS PG DISPLAYS EICAS MSG "WXR SYS" W/L SYS SELECTED. RECYCLED NR 1 WXR C/B. OPS CK OK IAW MM 34-53-00."WXR SYS" MESSAGE CLEARED.SDR HALA2010010400004Generator · failedETOPS SIGNIFICANT SYS - ON ENG START RT GEN FAILED. RESET RT GEN SYS. SYS OK IAW AMM 24-20-00-001 FIG 101. PERFORMED ENGINE RUN OF 5 MIN. SYS CHECK OK IAW AMM 24-16-00-825-012, AND AMM 24-11-00-175-006.SDR HALA2009123100611Engine · malfunctionedETOPS SIGNIFICANT SYS - AFTER LANDING APU FAILED TO START AFTER 2 ATTEMPTS. CHECKED APU COND, SECURITY, OIL NO LEAKS NOTED. BITE CHECK APU ECU NO FAULTS NOTED PERFORMED NORMAL START APU OIL QTY CHECK REF 49-11-00, GOOD.SDR HALA2009122800607Warning Light · false activationETOPS SIGNIFICANT SYS - C IRS FAULT LIGHT ILLUMINATED ON TOUCHDOWN NOTE
STATUS LIGHT ALSO. PERFORMED FIM 34-21-00 C IRS OPS CHECK GOOD.SDR HALA2009122600608Engine · malfunctionedETOPS SIGNIFICANT SYS - AFTER 3 ATTEMPTS APU WOULD NOT START AFTER LANDING. APU FAULT LIGHT ILLUMINATED. PERFORMED BITE CHECK ON ECU NO FAULTS NOTED. INSPECTED AROUND APU AREA NO LEAKS NOTED. SERVICED APU. OPERATED APU. HAD NORMAL START. ACFT OK FOR SERVICESDR HALA2009122100592Idg · warning lightETOPS SIGNIFICANT SYS - MX LEVEL EICAS MSG LT IDG TEMP ENS DISPLAYED/ LT IDG RISE TEMP O DEG L IDG OUT 87RT OUT 82 L IDG RISE 0 R RISE 10. MX NOTED FOUND L IDG OVERSERVICED. SERVICED L IDG IAW HAL M261-767 OVERNIGHT CHECK INTERROGATED MX LEVEL EICAS MSGS- FOUSDR HALA2009121700589Indicator · inoperativeETOPS SIGNIFICANT SYS - ON TAKEOFF V1 INOP (AMBER) ON ADI SPEEDTAPE, NO SPEEDS FOR VR OR V2. INPUT V1 SPEED IAW FIM 34-63-22-1. V1 OP CKS NORMAL. OK FOR SERVICE.SDR HALA2009121500587Valve · faultedETOPS SIGNIFICANT SYS - MID CABIN TRIM AIR INOP LIGHT AND EICAS MSG
ILLUMINATED WHILE ON THE GROUND. INTERROGATED ZONE TEMP CTL FOUND MID CABIN VALVE FAULT. REPLACED TRIM AIR VALVE IAW AMM 21-61-07 AND OPS LEAKED CK GOOD.SDR HALA2009121300578Starter · failedETOPS SIGNIFICANT SYS - BTB - ENGINE LT NR N2 ROTATION WITH START VALVE OPEN PRESSURE NORMAL. REMOVED AND REPLACED LT ENG STARTER, IAW 80-11-01 LEAK CHECK GOOD, STARTING NORMAL. OK FOR SERVICE.SDR HALA2009120500569Radar · no testETOPS SIGNIFICANT SYS - RT SIDE RADAR TEST FAIL. CYCLED R WXR C/B. OPS CK OK IAW MM 34-43-00.SDR HALA2009120400572Engine · inoperativeETOPS SIGNIFICANT SYS - APU FAULT. APU WOULD NOT START AFTER LANDING PRIOR TO THE GATE (2 ATTEMPTS). BITE APU ECU IAW FIM49-11-00. NO FAULTS, NO FLAGS, ONLY ABORTED START MSG ON ECU WHICH CAPT. INITIATED. NO LRU FAULTS. OIL QTY FULL. INSPECT APU COND AND SESDR HALA2009120300561Apu · malfunctionedETOPS SIGNIFICANT SYS - APU FAULT EICAS MSG. AFTER LANDING. PERFORMED APU ECU BITE PROCEDURE. ECU FAULTS REVERSE FLOW. FAULT NOT ASSOCIATED WITH START. FOUND APU COLD SOAKED. APU START NORMAL ON FIRST ATTEMPT. APU BITE C/W IAW FIM 49-11-00.SDR HALA2009120300560Wire · brokenEICAS MESSAGE "ANTI SKID" ON STATUS PAGE "NORM ANTISKID AND ALT ANTI-SKID ON. FOUND BROKEN WIRE TO NR 8 WHEEL TRANSDUCER. REPLACED WIRE WDM 32-42-11 SECURITY CHECK OK IAW 32-42-00-405 NO FAULTS NOTED.
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