# British Aerospace Reg Acft AVRO-146RJ100 - Type: Aircraft model (FAA registry) - Registry code: 1500089 - Manufacturer (registry): BRITISH AEROSPACE REG ACFT LTD - Model: AVRO-146RJ100 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Turbo-fan - Seats: 100 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/british-aerospace-reg-acft-avro-146rj100 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 (33) As reported by operators and repair stations, by the model named in the report. - [SDR CA190604027](https://openairdocs.org/sdr/CA190604027), Jul 18, 2018: HMU. MALFUNCTIONED. (CAN) #4 ENGINE FADEC FAULT OCCURRED, LITTLE ENGINE CONTROL WITH SWITCH OFF. HMA REPLACED WITH SERVICEABLE UNIT. LEAK AND FUNCTION RUNS C/O IAW 73-20-01, 72-00- - [SDR CA180529015](https://openairdocs.org/sdr/CA180529015), May 29, 2018: BRACKET. CORRODED. (CAN) DURING THE INSPECTION OF CPCP CARD NR C57-530-02-01 (48 MONTH) LEVEL 3 CORROSION. EXFOLIATION WAS FOUND ON THE LOWER CORNER BRACKET OF THE RT AILERON 1/B - [SDR CA160211004](https://openairdocs.org/sdr/CA160211004), Aug 5, 2015: EXTINGUISHER. UNWANTED DEPLOY. (CAN) CARGO FIRE EXTINGUISHER BOTTLE AUTO DEPLOYED, NOT ENTIRELY SURE OF CAUSE- SUSPECT ACFT BATTERY WAS LT ON THUS POWER DRAINED DOWN TO AN ALMOST DEAD CAPACIT - [SDR MALA000573](https://openairdocs.org/sdr/MALA000573), Oct 9, 2000: DISPLAY. MALFUNCTIONED. JUST AFTER TAKEOFF, NR 4 ENGINE EGT DROP TO ABOUT 50 DEGREES, THEN WOULD NOT READ STABLE FOR ABOUT 10 MINUTES. ENGINE INDICATED 50 DEGREE WARMER AND ON SHUTDOWN - [SDR 20000913SH026](https://openairdocs.org/sdr/20000913SH026), Aug 29, 2000: PUMP. MISMANUFACTURED. ACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEAL - [SDR 20000913SH025](https://openairdocs.org/sdr/20000913SH025), Aug 29, 2000: PUMP. MISMANUFACTURED. ACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEAL - [SDR 20000913SH024](https://openairdocs.org/sdr/20000913SH024), Aug 29, 2000: PUMP. MISMANUFACTURED. ACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEAL - [SDR 20000913SH023](https://openairdocs.org/sdr/20000913SH023), Aug 29, 2000: PUMP. MISMANUFACTURED. ACFT WAS UNDERGOING WING REPAIRS FOLLOWING FUEL TANK CONTAMINATION. POST-FUEL SYSTEM CHECKS CARRIED OUT AND 3 FUEL PUMP CANNISTERS WERE FOUND TO HAVE BLOWN SEAL - [SDR AU000772](https://openairdocs.org/sdr/AU000772), Aug 26, 2000: TRANSCEIVER. FAULTY. (AUS) HF TRANSCEIVER CAUSES FIRE BELL TO RING WHEN TRANSMITTER KEYED. TRANSCEIVER HAD BEEN FITTED FOLLOWING REPAIR. - [SDR 99ZZZX62](https://openairdocs.org/sdr/99ZZZX62), Nov 9, 1998: FUEL TANK. LEAKING. DURING A C-3 CHECK PERFORMED 11-9-98, FUEL LEAK WAS FOUND IN THE CENTRAL FUEL TANK. SUBMITTER STATED THE POSSIBLE CAUSE FOR THIS DEFECT IS FATIGUE OF THE JOINT - [SDR SADF9807](https://openairdocs.org/sdr/SADF9807), Jul 25, 1998: TRIM TAB. LOOSE. CLO/ADZ - FLT 176 - DURING CRUISE AT FL 240 IN ICING CONDITIONS USING ENGINE WING AND TAIL ANTI-ICE ALONG WITH CONT IGN, AND SPEED REDUCED TO M 0,60, THE AIRPLA - [SDR 99ZZZX623](https://openairdocs.org/sdr/99ZZZX623), Jul 4, 1998: TAB. MALFUNCTIONED. CLO/ADZ - FLT 176 - FLIGHT DIVERSION TO PTY. AT 22,000 FT ASL WITH 86,000 POUNDS GW, THE AIRCRAFT PRESENTED PITCH OSCILLATION WITH ALL AIRFRAME PROTECTION SELEC - [SDR 98ZZZX2560](https://openairdocs.org/sdr/98ZZZX2560), Jun 29, 1998: SELECTOR SWITCH. MALFUNCTIONED. FLT 596 - AIR TURN BACK. WHEN THE LANDING GEAR LEVER IS SELECTED UP, THE LEVER STICKS AND A STRIKE OF THE GEAR. WHEN SELECTED UP, STILL CONTINUED AND GOT WORSE. - [SDR 98ZZZX2558](https://openairdocs.org/sdr/98ZZZX2558), Jun 15, 1998: FLIGHT CONTROL. OSCILLATION. CLO/ADZ - FLT 1176 - STRONG PITCH OSCILLATION WAS FELT DURING FLIGHT. LEVELLED AT FL 240, SPEED 260 KNOTS, ENGINE ANTIICE ON. OUTER WING AND TAIL ANTI-ICE ON. C - [SDR SADF9803](https://openairdocs.org/sdr/SADF9803), Jun 7, 1998: ENGINE. VIBRATION. BOG/VUP - FLT 594 - REJECTED TAKEOFF DUE TO HIGH VIBRATION (MAX TRUST 1.0 INCHREASING DURING RUNNING TO 1.2) ENGINE NR 1 REJECTED WAS DONE AT 65 KNOTS. IT WAS C - [SDR SADF9802](https://openairdocs.org/sdr/SADF9802), May 23, 1998: R/T UNIT. FAILED. BOB/BOB - FLT 184 - WEATHER RADAR IS INOPERATIVE DURING INITIAL CLIMB. THE WEATHER RADAR RECEIVER TRANSMITTER WAS CHANGED ACCORDING AMM 34-41-00. (X) - [SDR SADF9801](https://openairdocs.org/sdr/SADF9801), Jan 21, 1998: ENGINE. BIRD STRIKE. FLT 166 AIR TURN TO BAQ - FOD (BIRD) DURING TAKEOFF ENGINE NR 4. ENGINE WAS SHUT DOWN ACCORDING TO CHECK LIST. EXTINGUISHER NR 1 WAS DISCHARGED DUE TO POSSIBLE - [SDR SADF9707](https://openairdocs.org/sdr/SADF9707), Dec 11, 1997: DETECTOR LOOP. GROUNDED. CTG/CTG - FLT 1169 - AIR TURN-BACK. DURING TAXI, FADEC FAULTY NR 2 LIGHT CAME ON, FADEC FAULTY PROCEDURES FOR TAKEOFF WERE DONE. AFTER TAKEOFF AT 500 FEET, ENGI - [SDR SADF9706](https://openairdocs.org/sdr/SADF9706), Nov 3, 1997: VALVE ACTUATOR. FAILED. AFTER DEPARTURE, LANDING GEAR DID NOT GO UP. IT REMAINED DOWN. FLT 396 AIR TURN-BACK TO BOGOTA. LANDING GEAR ELECTRIC ACTUATOR OF SELECTOR VALVE WAS REPLACED IA - [SDR SADF9700002](https://openairdocs.org/sdr/SADF9700002), Apr 2, 1997: SERVICE DOOR. OUT OF PLACE. ADZ/BOG - FLT 503 - DURING FLIGHT FROM ADZ/BOG, PILOTS EXPERIENCED PRESSURIZATION PROBLEMS WITH FLUCTUATIONS AND CABIN ALTITUDE CONTROL PROBLEMS. FLIGHT DIVERTE - [SDR 96ZZZX6130](https://openairdocs.org/sdr/96ZZZX6130), Nov 17, 1996: ENGINE. VIBRATION. DURING TAKEOFF ROLL, ENGINE VIBRATION WARNING LIGHT CAME ON. ENGINE NR 2 REACHED 2.2. TAKEOFF WAS REJECTED. ENGINE NR 2 WAS CHANGED. TEST WAS PERFORMED ACCORDIN - [SDR 96ZZZX6129](https://openairdocs.org/sdr/96ZZZX6129), Nov 16, 1996: LANDING GEAR. LACK OF LUBE. AFTER TAKEOFF, LANDING GEAR LEVER DIDN'T COME UP AND SPOILER LIGHT ON MWS CAME ON. RETURNED TO AIRPORT. LUBRICATED LANDING GEAR LEVER MECHANISM. CHECKED SPOILER - [SDR 96ZZZX6132](https://openairdocs.org/sdr/96ZZZX6132), Nov 14, 1996: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF ROLL, THE LOWER DOOR NOT SHUT LIGHT CAME ON. TAKEOFF WAS REJECTED. ALL LOWER DOORS HYDRAULIC, ELECTRICAL AND CARGO WERE CHECKED AND FOUND OK. RES - [SDR 96ZZZX6131](https://openairdocs.org/sdr/96ZZZX6131), Nov 10, 1996: ENGINE. BIRD STRIKE. PERFORMING WALK-AROUND IN SAN JOSE, A BIRD WAS FOUND INGESTED IN ENG NR 3. ACCOMPLISHED ENGINE BORESCOPIC INSPECTION DUE TO BIRD STRIKE, NO DAMAGE FOUND ON THE - [SDR 96ZZZX6128](https://openairdocs.org/sdr/96ZZZX6128), Oct 30, 1996: CONNECTOR. DIRTY. 45 MIN AFTER T/O FROM SKBO AT FL 280. VIBRATION FOR ENG NR 3 SHOWED 2.0 WITH MWS CALL OUT. SOON AFTER ENG 1 SHOWED 1.3 VIBR, ENG 2 AND 4 SHOWED 1.4. ALSO, ALL E - [SDR 96ZZZX4630](https://openairdocs.org/sdr/96ZZZX4630), Aug 9, 1996: LAMP HOLDER. BURN DAMAGE. FOUND LAMP HOLDER WITH BURN DAMAGE. APPARENTLY EXTERNAL HEAT SOURCE. - [SDR 96ZZZX4041](https://openairdocs.org/sdr/96ZZZX4041), Mar 5, 1996: ENGINE. FLAME OUT. ADZ - FLT 169 - DURING SHORT FINAL TO RWY 06 IN ADZ, ENGINE NR 1 FLAMED OUT. JUST MEMORY ITEMS PROCEDURE. ONLY OBSERVED N2 WENT TO ZERO. PERCENT RPM AND OIL PRE - [SDR 96ZZZX3974](https://openairdocs.org/sdr/96ZZZX3974), Jan 31, 1996: COMPRESSOR. STALLED. GUA - FLT 503 - AFTER PASSING 1,000 FEET AGL, A COMPRESSOR STALL WAS HEARD, ENG NR 3 PARAMETERS BEGAN TO FLUCTUATE. EGT EXCEEDED THE TAKEOFF LIMIT THROTTLE, NR - [SDR 96ZZZX3970](https://openairdocs.org/sdr/96ZZZX3970), Jan 21, 1996: COMPUTER. MALFUNCTIONED. BOG - FLT 506 - TAKEOFF WAS ABORTED DUE TO THRUST RATING PANEL (TRP) AND FLIGHT GUIDANCE COMPUTER (FGC) DISCONNECTING. FAULT RESET. FAILURE COULD NOT BE DUPLICA - [SDR 96ZZZX3975](https://openairdocs.org/sdr/96ZZZX3975), Jan 18, 1996: CONNECTOR. DIRTY. SMR/RNG - FLT 161 - IN-FLIGHT, ENGINE NR 4 SHUT DOWN. ACCOMPLISHED DUE OIL LOW PRESSURE. ENGINE NR 4 WAS CHECKED PER LEAK EVIDENCES AND IT IS OK. OIL PRESSURE T - [SDR 96ZZZX3972](https://openairdocs.org/sdr/96ZZZX3972), Jan 1, 1996: HMA. MALFUNCTIONED. BOG - FLT 502 - DURING TAKEOFF RUN LIMITED TO MAX POWER DUE TO MAX WEIGHT, THE ENGINE NR 4 FOR 96 N1 REQUIRED, DID NOT REACH 96. IT SHOWS 94 PERCENT AND DESECND - [SDR 96ZZZX3971](https://openairdocs.org/sdr/96ZZZX3971), Dec 30, 1995: ENGINE. MALFUNCTIONED. RNG - FLT 160 - ABORTED TAKEOFF DUE TO N1 ENGINE NR 4 FALL 3 PERCENT OF N1 TARGET 96.8 OAT REPORTED 12 OC. ENGINE NR 4 WAS CHECKED AND PERFORMED SEQUENCE OF MAI - [SDR 96ZZZX3973](https://openairdocs.org/sdr/96ZZZX3973), Dec 22, 1995: ENGINE. FAILED. FLT 180 - EXCESSIVE ENGINE VIBRATION. ENGINE NR 3 (3.0 OF VIBRATION). ENGINE SHUT DOWN IN-FLIGHT. ENGINE NR 3 WAS REPLACED. RUN-UP TEST NORMAL. PERFORMED FUNCTI --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.