# Boeing 767-33AER

- Type: Aircraft model (FAA registry)
- Registry code: 1385230
- Manufacturer (registry): BOEING
- Model: 767-33AER
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 330
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-767-33aer

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 (288, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2023F00350](https://openairdocs.org/sdr/2023F00350), Dec 14, 2023: FITTING. CRACKED. SUPPORT FITTING NACELLE STRUT ENG LH WITH 12MM CRACK (P/N 31172114-7). CORRECTIVE ACTION: REPLACED SUPPORT FITTING IN NACELLE STRUT.
- [SDR IXXA202308280001](https://openairdocs.org/sdr/IXXA202308280001), Aug 28, 2023: LONGERON CLIP. CRACKED. #1 PYLON HAS TWO CRACKED LONGERON CLIPS ON O/B AND I/B SIDE OF WEB LOCATED JUST AFT OF HYD BAY DOORS. REMOVED AND REPLACED LONGERON CLIPS IN #1 PYLON IAW B767 S
- [SDR IXXA20211018078](https://openairdocs.org/sdr/IXXA20211018078), Sep 27, 2021: STIFFENER. CRACKED. WEB ON STIFFENER AT STATION 971 LBL 90 HAS DAMAGED HOLE. REMOVED, FABRICATED AND REPLACED NEW STIFFNER AT STATION 971 LBL 90 IAW ENGINEERING ORDER 74783FAB01.
- [SDR IXXA20211018077](https://openairdocs.org/sdr/IXXA20211018077), Sep 24, 2021: FAILSAFE. CRACKED. RIGHT FAILSAFE STRAP AT STA 955 HAS A CRACK INDICATION ON ULTRASOUND NDT INSPECTION. REPAIRED FAILSAFE STRAP AT STATION 955 IAW AMES ENGINEERING ORDER 472070RD0
- [SDR IXXA20211018075](https://openairdocs.org/sdr/IXXA20211018075), Sep 24, 2021: FLAP. DELAMINATED. LEFT WING TRAILING EDGE INBOUND TRAILING EDGE PLAP HAS DELAM AREA ON INBOUND EDGE. LAYED UP AND CURED IAW B767 SRM 51-70-10.
- [SDR IXXA20211018074](https://openairdocs.org/sdr/IXXA20211018074), Sep 24, 2021: BEAM. CRACKED. INBOUND HYD BAY LATCH CHANNEL IS CRACKED AT #3 LATCH MOUNT AREA. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-02.
- [SDR IXXA20211018069](https://openairdocs.org/sdr/IXXA20211018069), Sep 24, 2021: SKIN. DELAMINATED. RIGHT SIDE VERTICAL BETWEEN THE AUX SPAR AND FRONT SPAR THE COMPOSITE SKIN PANEL IS DELAMINATED. REPAIRED RIGHT SIDE VERT STAB PANEL BETWEEN THE AUX SPAR AND FT
- [SDR IXXA20211018067](https://openairdocs.org/sdr/IXXA20211018067), Sep 23, 2021: WEB. CRACKED. FWD DOUBLER ON FAIRING SUPPORT WEB AT TA 1081 CRACKED, FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.
- [SDR IXXA20211017066](https://openairdocs.org/sdr/IXXA20211017066), Sep 23, 2021: DOUBLER. CRACKED. AFT DOUBLER ON FAIRING SUPPORT WEB AT STA 1081 CRACKED. FABRICATED AND REPLACED NEW DOUBLER IAW B767 SRM 51-10-02.
- [SDR 2021FA0000266](https://openairdocs.org/sdr/2021FA0000266), Sep 23, 2021: NONE. NONE. R GEN OFF AFTER ENGINE START. CORRECTIVE ACTION: DISPATCH IAW MEL 24-00-01-01 CAT "B". THE FINAL CORRECTIVE ACTION WAS GIVEN ON 09-24-2021: HAS BEEN PERFORMED F
- [SDR IXXA20211017068](https://openairdocs.org/sdr/IXXA20211017068), Sep 21, 2021: NONE. CRACKED. RIGHT STUB BEAM CRACKED AT STATION 903.5 RBL89.REPAIRED RIGHT CRACKED STUB BEAM AT STATION 903.5 RBL 89 IAW ENGINEERING ORDER 53-767-7702.
- [SDR IXXA20211018076](https://openairdocs.org/sdr/IXXA20211018076), Sep 20, 2021: FORMER. CRACKED. NOSE FORMER IS CRACKED BY #9 SLAT INBOUND AUX TRACK AT WING LEADING STATION 562. REMOVED AND REPLACED DAMAGE NOSE FORMER IAW B767 SRM 51-40-02.
- [SDR IXXA2021100018075](https://openairdocs.org/sdr/IXXA2021100018075), Sep 20, 2021: RIB. CRACKED. LEFT WING LEADING EDGE AT APPROXIMATELY LES 563.0 HAS CRACKED NOSE RIB. REMOVED AND REPLACED NOSE RIB ON LEFT WING LEADING EDGE AT WS STA 565.9 IAW B767 51-40-0
- [SDR IXXA20211018073](https://openairdocs.org/sdr/IXXA20211018073), Sep 18, 2021: NONE. CRACKED. #2 AFT STRUT FAIRING SMALL ANGLE ON BACK SIDE OF HYD COMPT OUTBOARD SIDE CRACKED. REMOVED AND REPLACED SMALL "C" ANGLE ON #2 AFT STRUT FAIRING FWD SIDE JUST AFT
- [SDR IXXA20211018071](https://openairdocs.org/sdr/IXXA20211018071), Sep 18, 2021: CHANNEL. CRACKED. #2 AFT STRUT FAIRING WEB OUTBOARD "U" CHANNEL CRACKED AT BOTTOM IN RADIUS. REMOVED CHANNEL AND MATCH DRILLED NEW "U" CHANNEL IAW B767 SRM 51-40-05 AND INSTALLED
- [SDR IXXA20211018072](https://openairdocs.org/sdr/IXXA20211018072), Sep 17, 2021: STIFFENER. CRACKED. #2 AFT STRUT FAIRING ANGLE ON INBOUND FORWARD SIDE OF AFT WEB RUNNING FORE AND AFT IS CRACKED. REMOVED AND REPLACED STRUT FAIRING ANGLE IAW B767 SRM 51-40-02.
- [SDR IXXA20211018070](https://openairdocs.org/sdr/IXXA20211018070), Sep 16, 2021: BULKHEAD. CRACKED. #1 PYLON PANEL 437DB V FRAME CRACKED. REMOVED DAMAGED V FRAME AND INBD CHANNEL MATCH DRILLED HOLES IAW B767 1-40-05 AND REINSTALLED CHANNELS AND V FRAME IAW B76
- [SDR 2020F00059](https://openairdocs.org/sdr/2020F00059), Nov 19, 2019: CONTROL PANEL. FAILED. AUTOFLIGHT: EICAS MESSAGE AUTOPILOT ON THE LEFT, CENTER AND RIGHT. UNNABLE ETOPS DUE TO AUTOPILOT FAILURE. QUICK RETURN FLIGHT TO DEPARTURE STATION (MAD)
- [SDR 2019FA0000303](https://openairdocs.org/sdr/2019FA0000303), Jun 20, 2019: SENSOR. FAILED. RIGHT ENGINE OIL TEMPERATUREREACHED AMBER BAND DURING CLIMB AND CRUISE. CORRECTIVE ACTION: WAS REPLACED OIL TEMP SENSOR IAW AMM 79-34-01/403 OIL TEMP SENSOR TES
- [SDR 2019FA0000293](https://openairdocs.org/sdr/2019FA0000293), Jun 20, 2019: SENSOR. FAILED. ENGINE OIL TEMPERATURE REACHED AMBER BAND DURING CLIMB AND CRUISE. CORRECTIVE ACTION: WAS REPLACED OIL TEMP SENSOR IAW 79-34-01/403 OIL TEMP SESNOR TEST NORMAL 
- [SDR 2019FA0000019](https://openairdocs.org/sdr/2019FA0000019), Jan 13, 2019: MODULE. FAILED. HYDRAULIC SYSTEM PRIMARY PUMPS C1 AND C2 PRESS LIGHT ILLUMINATED IN FLIGHT. HYDRAULIC SYSTEM DEMAND PUMP PVHT LIGHT ILLUMINATED IN FLIGHT. L YAW DAMPER INOP ILL
- [SDR HALA2018123100691](https://openairdocs.org/sdr/HALA2018123100691), Dec 28, 2018: LIGHT. INOPERATIVE. 4L EXTERIOR EMERGENCY LIGHT INOP ( EXTERIOR EMERGENCY LIGHTING SYSTEM ). RELAMPED 4L EXT EMERGENCY LIGHT. CHK OK.
- [SDR HALA2018102300534](https://openairdocs.org/sdr/HALA2018102300534), Oct 21, 2018: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM - WXR SYS STATUS MSG. CLEARED "WXR SYS" STATUS MSG PER FIM 34-43 TASK 801. OPS CHECK OF BOTH L/R WX RADAR SYSTEMS IN COCKPIT OK PER AMM
- [SDR HALA2018102300533](https://openairdocs.org/sdr/HALA2018102300533), Oct 21, 2018: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - LEFT PACK OFF LIGHT ON DURING DESCENT. DUCT PRESSURE 40 PSI. PERFORMED BITE TEST OF LT PACK TEMP CONTROLLER PER FIM 21-51 F/T 803. NO
- [SDR HALA2018101500497](https://openairdocs.org/sdr/HALA2018101500497), Oct 14, 2018: SHUTOFF VALVE. FAULTY. ETOPS SIGNIFICANT SYSTEM - APU FUEL VLV EICAS MESSAGE DURING APU SHUTDOWN AFTER PUSH BACK. REMOVED AND REPLACED APU SHUTOFF VALVE ACTUATOR PER AMM 28-25-02. OPS
- [SDR HALA2018100900484](https://openairdocs.org/sdr/HALA2018100900484), Oct 8, 2018: OVEN. MALFUNCTIONED. MID GALLEY OVEN SMELLED LIKE BURNING AND WOULD NOT COOL DOWN. UTILITY BUSES WERE RESET AND GALLEY OVEN COOLED DOWN AND DIDN'T SMELL LIKE BURNING. RAN OVENS AT H
- [SDR HALA2018100500470](https://openairdocs.org/sdr/HALA2018100500470), Oct 4, 2018: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYSTEM - UNABLE TO CONTROL FWD CABIN COMPARTMENT TEMPERATURE. TEMP IN FWD CABIN FLUCTUATED BETWEEN 69F AND 80F WITH KNOB IN 11 O'CLOCK POSITIO
- [SDR HALA2018100500469](https://openairdocs.org/sdr/HALA2018100500469), Oct 3, 2018: UNKNOWN. ODOR. OVEN F105 FWD GALLEY HAD BURNING ODOR. LIKE THE WIRE INSULATION. TURNED OVEN OFF. RAN OVEN F105 FWD GALLEY. NO ODOR NOTED. OK TO CONTINUE.
- [SDR HALA2018100200463](https://openairdocs.org/sdr/HALA2018100200463), Oct 1, 2018: DISPLAY. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - ON 10 MILE FINAL BOTH F/O EFIS SCREENS BLANKED. SWITCHED EFI TO ALT. ON F/O SIDE AND LANDED IN ALT. F/O'S EFIS SCREENS OPS CHECK OK P
- [SDR 2018FA0000338](https://openairdocs.org/sdr/2018FA0000338), Aug 16, 2018: ENGINE. VIBRATION. RIGHT ENGINE MAXIMUM VIBRATION 4.1.
- [SDR 2017F00022](https://openairdocs.org/sdr/2017F00022), Jan 31, 2017: OIL COOLER. NOT REPORTED. QRF TO VVI FOR HIGH OIL TEMP 158C ON LEFT ENGINE. CONT ITEM M-066
- [SDR UIEA2017012900116](https://openairdocs.org/sdr/UIEA2017012900116), Jan 29, 2017: ELT. DAMAGED. COCKPIT ELT DAMAGED. REMOVED AND REPLACED THE ELT IAW AMM 25-03-00.
- [SDR UIEA2017011200018](https://openairdocs.org/sdr/UIEA2017011200018), Jan 12, 2017: RELAY. FAILED. LEFT ENGINE IGNITOR 1 STATUS MESSAGE. REPLACED RELAYS K158 AND K159 IAW WDM 74-31-01. OPS CHECKED NORMAL.
- [SDR UIEA2017011200019](https://openairdocs.org/sdr/UIEA2017011200019), Jan 12, 2017: IGNITER. INOPERATIVE. LEFT ENGINE DID NOT START ON 2 ATTEMPTS, LT ENGINE IGNITOR 2/1 STATUS MESSAGE. REPLACED TWO. IGNITORS IAW AMM 74-21-02, OPS CHECKED NORMAL.
- [SDR UIEA2017011000014](https://openairdocs.org/sdr/UIEA2017011000014), Jan 10, 2017: IGNITION SYS. MALFUNCTIONED. LEFT ENGINE DID NOT START, ATTEMPTED TWICE. STATUS MESSAGE DISPLAYED LEFT ENGINE IGNITION SYS 2 AND 1. RESET IGNITION CIRCUIT BREAKER, OPS CHECK NORMAL IAW AMM 
- [SDR UIEA2017010500008](https://openairdocs.org/sdr/UIEA2017010500008), Jan 5, 2017: WARNING MESSAGE. FALSE ACTIVATION. LEFT ENGINE EXPERIENCED HUNG START STATUS MESSAGE L ENGINE IGNITOR 2 COMPLIED WITH QRH PROCEDURE , NORMAL START CLEARED STATUS MESSAGE, NO MESSAGES PRESENT AFTE
- [SDR UIEA2016122801060](https://openairdocs.org/sdr/UIEA2016122801060), Dec 26, 2016: WARNING LIGHT. FALSE ACTIVATION. RIGHT PACK OFF EICAS AFTER SELECTING APPROACH MODE AND PASSING 1500'AGL. PERFORMED BITE TEST ON PACK CONT, NO FAULTS PRESSENT MCDP SHOWS NO FAULTS, TEST 30-40 C
- [SDR UIEA2016122701056](https://openairdocs.org/sdr/UIEA2016122701056), Dec 26, 2016: WARNING MESSAGE. FALSE ACTIVATION. RT PACK OFF EICAS AFTER SELECTING APP MODE. PERFORMED RT PACK TEMP CONTROL BITE TEST IAW AMM 21-51-14, ALL SYSTEM GO, OPS NML.
- [SDR UIEA2016121901045](https://openairdocs.org/sdr/UIEA2016121901045), Dec 17, 2016: WARNING SYSTEM. ACTIVATED. DURING APPROACH AT 3000FT, WHEN APP MODE SELECTED, A PWR TRANSFER,LOAD SHED EVENT OCCURS. EICAS RT PACK OFF, AUDIBLE ALARM HEARD, BEEPING FOR A COUPLE SECONDS. 
- [SDR UIEA2016120100949](https://openairdocs.org/sdr/UIEA2016120100949), Dec 1, 2016: WARNING MESSAGE. FALSE ACTIVATION. STATUS MESSAGE FOR CABIN ALT AUTO 1. PERFORMED FIM PROCEDURE 21-31 FAULT TREE 809 RESET FAULT OPS CHECK OK.
- [SDR UIEA2016113000911](https://openairdocs.org/sdr/UIEA2016113000911), Nov 30, 2016: CIRCUIT BREAKER. MALFUNCTIONED. NO APU PNEUMATIC AIR OUTPUT. CYCLED THE CIRCUIT BREAKER AND PERFORMED BITE TEST OPS CHECK NORMAL IAW 49-11-00 FAULT TREE 958, NO FAULTS NOTED.
- [SDR UIEA2016090600735](https://openairdocs.org/sdr/UIEA2016090600735), Sep 5, 2016: BLOWER. DEFECTIVE. AFT CARGO FAN EICAS MESSAGE MAINTENANCE. R & R AFT CARGO NR 1 BLOWER, M718, IAW AMM 26-16-02. OPS CK NORMAL.
- [SDR UIEA2016082400699](https://openairdocs.org/sdr/UIEA2016082400699), Aug 24, 2016: VALVE. MALFUNCTIONED. WITH PACKS ON APU SURGES. R & R APU SURGE VALVE IAW AMM 49-53-01. OPS CHECK NORMAL.
- [SDR UIEA2016081600684](https://openairdocs.org/sdr/UIEA2016081600684), Aug 15, 2016: FIRE DETECTOR. MALFUNCTIONED. STATUS MESSAGE LT ENGINE FIRE LOOP 2. REMOVED AND REPLACED THE FIRE DETECTOR IAW AMM 26-11-02, PERFORMED ENGINE FIRE & OVER HEAT TEST IAW AMM 26-11-00. TEST PAS
- [SDR UIEA2016081000677](https://openairdocs.org/sdr/UIEA2016081000677), Aug 8, 2016: MODULE. INOPERATIVE. INTERMITTENT , NO DUCT PRESSURE FROM APU. REPLACED FLOW SENSING MODULE IAW AMM 49-53-08. OPS CHECKED NORMAL.
- [SDR HALA2016062900259](https://openairdocs.org/sdr/HALA2016062900259), Jun 29, 2016: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYS. WEATHER SYS STATUS MESSAGE ON EICAS. PERFORMED FIM 34-43 FAULT TREE 805. MESSAGE EXTINGUISHED, NO FAULTS NOTED. OK FOR SERVICE.
- [SDR UIEA2016063000554](https://openairdocs.org/sdr/UIEA2016063000554), Jun 27, 2016: TRIM SYSTEM. OUT OF ADJUST. AILERON TRIM, MAX TRIM TO THE LT EXCEEDED LIMIT 6.1, OK TO THE RT: 5.3, MAX LIMIT 5.9. ADJUSTED AILERON TRIM CONTROL TO RT WING DOWN 30 DEGREES, 5.6 UNIT YOLK, 
- [SDR UIEA2016063000556](https://openairdocs.org/sdr/UIEA2016063000556), Jun 27, 2016: TRIM SYSTEM. OUT OF ADJUST. AILERON TRIM-MAX TRIM TO THE LT EXCEED LIMIT 6.2, OK TO THE RT: 5.3. MAX LIMIT 5.9. DUE TO TEST TRIM ON RT WING DOWN POSITION, FOUND THE CONTROL WHEEL TURNS TO 
- [SDR UIEA2016063000553](https://openairdocs.org/sdr/UIEA2016063000553), Jun 27, 2016: HYDRAULIC SYSTEM. UNKNOWN. HYDRAULIC QTY-1.37 WITH OVERFILL APPEARED DURING CLIMB, WENT DOWN TO -1.15 AFTER CENTER HYD PUMPS WERE SWITCHED OFF. CENTER HYD SYS SERVICED PROPERLY IAW MM 12-
- [SDR UIEA2016063000552](https://openairdocs.org/sdr/UIEA2016063000552), Jun 27, 2016: FILTER. DEFECTIVE. C HYD PUMPS OVERHEAT, ALL C HYD PUMPS GOT OVERHEATED, THEN ELECT 1, ELEC 2 AFTER THAT, C HYD PRESSURE STARTED TO SURGE AND DROPPED TO "0". ADP FILTER MODULE REP

All 288: https://openairdocs.org/model/boeing-767-33aer/reports.md

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