# Boeing 767-3Z9 - Type: Aircraft model (FAA registry) - Registry code: 1385207 - Manufacturer (registry): BOEING - Model: 767-3Z9 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 330 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-767-3z9 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (24) As reported by operators and repair stations, by the model named in the report. - [SDR RYNA201205140024](https://openairdocs.org/sdr/RYNA201205140024), May 14, 2012: ACTUATOR. FAILED. LOUD BANG, POWER LOSS, FLAMES FROM RIGHT ENGINE ON CLIMBOUT. DID NOT PERFORM INFLIGHT SHUTDOWN. A/C IS AOG IN WORK. ACCOMPLISHED FIM 71-05-00 FAULT TREE 803 STE - [SDR RYNA201204300022](https://openairdocs.org/sdr/RYNA201204300022), Apr 30, 2012: SENSOR. OUT OF ADJUST. BLOCK TURNBACK L/E SLAT ASYMMETRY MESSAGE BEFORE TAKEOFF. FOUND NR 12 L/E SLAT SENSOR OUT OF ADJUSTMENT. CLEANED AND RE-SECURED SENSOR IAW MM OPS CHECKED PER MM - [SDR RYNA201204290021](https://openairdocs.org/sdr/RYNA201204290021), Apr 29, 2012: WARNING SYSTEM. FALSE ACTIVATION. RETURN TO BLOCK L/E SLAT ASYMMETRY AND EICAS MESSAGE. TROUBLESHOT IAW FIM 27-18-00 PG 134-135, BITE CHECKED PSEU 27-09-03-101, FSEU 27-51-00 FIG 101, NO DEFECTS - [SDR RYNA201202010008](https://openairdocs.org/sdr/RYNA201202010008), Feb 1, 2012: WARNING SYSTEM. FALSE ACTIVATION. RIGHT OVERWING SLIDE LIGHT COME ON IN FLIGHT. LIGHT WAS OFF ON ARRIVAL. THE SYSTEM WAS CHECKED OUT PER MM 25-65-00. NON DEFECTS WERE NOTED. BOTTLE PRESSURE WAS - [SDR RYNA2011102900022](https://openairdocs.org/sdr/RYNA2011102900022), Oct 29, 2011: WINDSHIELD. CRACKED. RIGHT (R1) FORWARD WINDSHIELD CRACKED IN FLIGHT FROM BZZ TO YYC. DIVERTED TO RFD FOR REPAIRS. REMOVED AND REPLACED R1 WINDOW PER AMM 56-11-01. REMOVED AND REPLA - [SDR RYNA2011091600019](https://openairdocs.org/sdr/RYNA2011091600019), Sep 16, 2011: BATTERY PACK. DISCHARGED. LEFT AND RIGHT EMERGENCY LIGHTS INOPERATIVE ABOVE OVERWING HATCHES. IN ADDITION THE AFT RIGHT DOOR AND EMERGENCY LIGHTS ON RIGHT SIDE OF FUSELAGE INOPERATIVE. R - [SDR RYNA2011073100017](https://openairdocs.org/sdr/RYNA2011073100017), Jul 31, 2011: POWER SUPPLY. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS INOPERATIVE, LEFT AND RIGHT SIDES. REMOVED AND REPLACED BATTERY POWER SUPPLY, POS M00731 AND M00735 REF AMM 33-51-07. SYSTEM OPERATION - [SDR RYNA2011031700010](https://openairdocs.org/sdr/RYNA2011031700010), Mar 17, 2011: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT L-4 DOOR EXTERNAL INOPERATIVE DURING TEST PER TASK CARD. RELAMPED EMERGENCY LIGHT ASSEMBLY. REF M/M 33-51-06. SYSTEM OPERATIONAL CHECKED NORM - [SDR RYNA2011022100007](https://openairdocs.org/sdr/RYNA2011022100007), Feb 21, 2011: LIGHT. INOPERATIVE. LEFT AFT PASSENGER DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LEFT AFT EXTERIOR EMERGENCY LIGHT PER AMM 33-51-06. OPERATIONAL CHECK NORMAL. - [SDR RYNA2011012700004](https://openairdocs.org/sdr/RYNA2011012700004), Jan 27, 2011: SWITCH. CORRODED. RIGHT OVERWING ESCAPE SLIDE DOOR AND INADVERTENTLY DEPLOYED DURING PERFORMANCE OF MAINTENANCE. LACES RIPPED ON SLIDE. REMOVED AND REPLACED BACKUP FIRE SWS2, BAC - [SDR 2010FA0001256](https://openairdocs.org/sdr/2010FA0001256), Dec 22, 2010: BATTERY PACK. DISCHARGED. FWD LT EMERGENCY LIGHT PACK INOP. FOUND BATTERY PACK DISCHARGED. - [SDR RYNA2010001020034](https://openairdocs.org/sdr/RYNA2010001020034), Oct 2, 2010: LIGHT. INOPERATIVE. L3 + R1 G-EXTERIOR EMERGENCY LIGHT INOP. RELAMPED L3 + R1 EXTERIOR EMERGENCY LIGHTS PER MM 33-51-01, OPS CHECKS GOOD. - [SDR RYNA2010009020032](https://openairdocs.org/sdr/RYNA2010009020032), Sep 22, 2010: ACTUATOR. MALFUNCTIONED. RIGHT WING SLIDE LIGHT ILLUMINATED IN UPPER EICAS IN FLIGHT. RIGHT WING SLIDE LIGHT DEFLECTED FLOOR ASSIST CARTRIDGES, REMOVED AND REPLACED DOOR ACTUATORS PER A - [SDR RYNA2010009002003](https://openairdocs.org/sdr/RYNA2010009002003), Sep 22, 2010: ACTUATOR. MALFUNCTIONED. RIGHT WING SLIDE LIGHT ILLUMINATED IN UPPER EICAS IN FLIGHT. RIGHT WING SLIDE LIGHT DEFLECTED FLOOR ASSIST CARTRIDGES, REMOVED AND REPLACED DOOR ACTUATORS PER A - [SDR RYNA2010009020031](https://openairdocs.org/sdr/RYNA2010009020031), Sep 22, 2010: WARNING SYSTEM. FALSE ACTIVATION. EMERGENCY DOOR LIGHT ON UPPER PANEL ILLUMINATED IN FLIGHT. PERFORMED OPERATIONAL TEST PER AMM 25-65-00, OPS CHECK GOOD. - [SDR RYNA2010007020020](https://openairdocs.org/sdr/RYNA2010007020020), Jul 7, 2010: LIGHT. INTERMITTENT. LEFT WING SLIDE AND EMERGENCY DOOR LIGHTS INTERMITTENT. TROUBLESHOT PER FIM 52-71-00. NO FAULTS NOTED ON PSEU. TEST CHECKS GOOD. OK FOR SERVICE. DOOR VISUALLY C - [SDR 2010F00158](https://openairdocs.org/sdr/2010F00158), Jul 7, 2010: LIGHT. INTERMITTENT. LT WING SLIDE AND EMERGENCY DOOR LIGHTS INTERMITTENT. TROUBLESHOT IAW FIM 52-71-00. NO FAULTS NOTED ON PSEU. TEST CHECK GOOD. OK FOR SERVICE. DOOR VISUALLY CHEC - [SDR RYNA2010000330000](https://openairdocs.org/sdr/RYNA2010000330000), Mar 28, 2010: FSEU. MALFUNCTIONED. DURING FLIGHT, AIR / GROUND DISAGREE STATUS MESSAGE. AFTER TAKEOFF ON FLAP RETRACTION FLAP LEVER O* - INDICATOR 1 * (BOTH L/R)- NO EICAS MESSAGE, NO WARNING LIG - [SDR RYNA200912180029](https://openairdocs.org/sdr/RYNA200912180029), Dec 7, 2009: STRUCTURE. DENTED. DURING INSPECTION OF AIRCRAFT FOUND DENT AT STA 1480 RTR 31L. REVIEW OF FINDINGS FOUND DAMAGE OUTSIDE NORMAL SRM LIMITS. PERFORMED PERMANENT REPAIRS PER DELTA E - [SDR RYNA200911020022](https://openairdocs.org/sdr/RYNA200911020022), Oct 30, 2009: CARRIAGE. DAMAGED. DURING WALK AROUND FOUND THE LT OUTBOARD FLAP O/B TRACK ROLLER CARRIAGE AND TRACK ASSEMBLY DAMAGED. ADDITIONALLY FLAP SKIN TO END CLOSER RIBS WERE DAMAGED, ALSO - [SDR RYNA200909300020](https://openairdocs.org/sdr/RYNA200909300020), Sep 29, 2009: GCU. MALFUNCTIONED. RIGHT GENERATOR OFF MESSAGE APPEARED ON THE EICAS DURING CLIMBOUT, CPM COMPLETED BUT RESET WAS UNSUCCESSFUL. REMOVED AND REPLACED THE RT GCU PER AMM 24-22-02. C - [SDR RYNA200908100012](https://openairdocs.org/sdr/RYNA200908100012), Aug 8, 2009: PROXIMITY SENSOR. OUT OF ADJUST. AT 120 KTS ABORTED TAKEOFF DUE TO FLAP TAKEOFF WARNING INDICATION CAUTION LIGHT ILLUMINATED ADDITIONALLY THE MASTER WARNING LED ASYMMETRY LIGHT BELOW 80KTS. PER - [SDR RYNA200907140009](https://openairdocs.org/sdr/RYNA200907140009), Jul 12, 2009: CONTROLLER. MALFUNCTIONED. DURING THE CLIMB PHASE OF FLIGHT THE STATUS MESSAGE CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 APPEARED ON THE EICAS. AIRCRAFT RETURNED TO DFW. MAINTENANCE PERFORMED - [SDR RYNA200906230008](https://openairdocs.org/sdr/RYNA200906230008), Jun 21, 2009: BATTERY PACK. DISCHARGED. DURING GROUND TEST OF EMERGENCY LIGHTING SYSTEM INSPECTION OF THE AIRCRAFT REVEALED THE RT EXTERIOR EMERGENCY LIGHTS ABOVE THE R-1, 2 AND 3 DOORS FAILED TO ILLU --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.