# Rolls-Royce AE-3007A1

- Type: Engine model (FAA registry)
- Registry code: 54165
- Manufacturer (registry): ROLLS-ROYC
- Model: AE 3007A1
- Engine type: Turbo-fan
- Power: 7,580 lb thrust
- Data sheet: [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Holder: Rolls-Royce Corporation
- Installed in: 4 registered aircraft
- Page: https://openairdocs.org/engine/rolls-royce-ae-3007a1

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

Historical (superseded or no longer in force):

- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

## Registered aircraft (4)

- [N138DE](https://openairdocs.org/aircraft/N138DE): [Champion Air LLC](https://openairdocs.org/faa-owner/CHAMPION%20AIR%20LLC), [Mooresville, NC](https://openairdocs.org/faa-place/NC/Mooresville), S/N 145129
- [N157MG](https://openairdocs.org/aircraft/N157MG): [Valiair Lc Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 2007, S/N 14500999
- [N500DE](https://openairdocs.org/aircraft/N500DE): [Champion Air LLC](https://openairdocs.org/faa-owner/CHAMPION%20AIR%20LLC), [Mooresville, NC](https://openairdocs.org/faa-place/NC/Mooresville), built 1998, S/N 145084
- [N825HK](https://openairdocs.org/aircraft/N825HK): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 145510

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA16LA100](https://openairdocs.org/ntsb/DCA16LA100), Feb 24, 2016: Embraer EMB145 (N856HK), St Louis, MO, substantial damage. Probable cause: the flight crews' failure to consider all available runways for landing to minimize the gusty crosswind component. Contributing to the accident was the captain's reduction of the engine thrust for…

## FAA accident and incident reports (4)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20150725011689I](https://openairdocs.org/incident/20150725011689I), Jul 25, 2015: Embraer EMB-145MP (N853HK), Dulles, VA, Minor damage. Trans states airlines flight 3342 reported a bird strike on a three mile final to runway 19C at 1200 feet. Damage reported to the right side of the nose cone.
- [Incident 20150305002749I](https://openairdocs.org/incident/20150305002749I), Mar 5, 2015: Embraer EMB-145MP (N856HK), St. Louis, MO, Minor damage. Lof 3412, EMB-145, during takeoff roll runway 29 blew both main tires on right side. Aborted takeoff and exited the runway at taxiway A5. The right hand…
- [Incident 20130613011219I](https://openairdocs.org/incident/20130613011219I), Jun 13, 2013: Embraer EMB-145MP (N854HK), No damage. On June 13, 2013 raia flight 3414 roa-ord N854HK diverted to ind due to #2 engine shutdown at 31000FT. The crew reported noticing that the itt on the number #2…
- [Incident 20090811048139I](https://openairdocs.org/incident/20090811048139I), Aug 11, 2009: Embraer EMB-145LR (N834HK), Chantilly, VA, Minor damage. On 08/11/2009 at 0038Z, pilot reported bird strike while on short final to runway 19L at 200 ft AGL. Additionally, reported that the nose gear was damaged and…

## Service difficulty reports (321, newest 50)

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

- [SDR HNAA202608100646](https://openairdocs.org/sdr/HNAA202608100646), Aug 3, 2026: O-RING. LEAKING. EXHAUST FUME SMELL IN COCKPIT. APU BLEED SYSTEM. R&R APU BLEED VALVE O-RINGS IAW AMM 36-12-03. OPS CHECKED GOOD. LEAKS CHECK GOOD.NO OTHER OR FUMES IN COCKPIT O
- [SDR HNAA2026081400718](https://openairdocs.org/sdr/HNAA2026081400718), Jul 9, 2026: YOKE. CRACKED. R/H ENGINE LOWER FWD ENGINE YOKE FITTING HAS A CRACK. REMOVED AND REPLACED CRACKED RH ENGINE LOWER FWD ENGINE YOKE FITTING IAW PDT FCD1-54-21-0017D AND REMOVED 
- [SDR HNAA2026070600575](https://openairdocs.org/sdr/HNAA2026070600575), Jul 5, 2026: SENSOR. FAULTED. IN FLIGHT, ENGINE 2 OIL TEMP REACHED 143C. FOLLOWED QRH PROCEDURE AND SHUTDOWN ENGINE 2. R & R ENG 2 OIL TEMP PRESS SENSOR IAW MM 79-31-10, OPS CHKD AND LEAK CH
- [SDR HNAA2026062400553](https://openairdocs.org/sdr/HNAA2026062400553), Jun 23, 2026: RELAY. FAULTED. ICE CONDITION, ANTI ICE INOP, ENG REF ANTI ICE DISAG, ICE CONDITION DISPLAYED ON TAKEOFF AT 76KTS. R & R RELAYS K0264, K0532, K0531, K0323 IAW AMM 20-13-02. PER
- [SDR HNAA2026061600501](https://openairdocs.org/sdr/HNAA2026061600501), Jun 13, 2026: DAU. FAULTED. NR 2 BLEED VALVE CLOSED AFTER TAKEOFF, MSG CLEARED AFTER LANDING. R & R DAU NR 1 & 2 IAW AMM 31-41-01-04. INSPECTED FUEL QTY INDICATION HARNESS IAW AMM 28-41-00
- [SDR HNAA2026042000290](https://openairdocs.org/sdr/HNAA2026042000290), Apr 19, 2026: SWITCH. FAULTED. BLEED 2 VALVE FAIL ON T/O ROLL. RIGHT ENG BLEED INOP. R & R 200 HIGH STAGE PRESSURE SWITCH AND KO172, OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2026031700219](https://openairdocs.org/sdr/HNAA2026031700219), Mar 16, 2026: BUTTON. FAULTED. WITH E2 A/ICE MEL ENG 2 OPEN INSCRIPTION WENT OUT IN ICING CONDITIONS UNTIL DESCENT ALONG WITH ICE CONDITION A/I INOP MESSAGE. R & R E2 AIR INLET PUSHBUTTON IAW
- [SDR HNAA2026021000114](https://openairdocs.org/sdr/HNAA2026021000114), Feb 9, 2026: WARNING MESSAGE. FALSE ACTIVATION. ON TAKE OFF ROLL 75 KNOTS, NR 1 ENGINE FUEL LOW TEMP. PERFORMED CONTINUITY & RESISTANCE TESTS ON ENGINE HARNESS W9 IAW RMM 73-31-00-900-801. NO DEFECETS NOTED. 
- [SDR HNAA2026012000008](https://openairdocs.org/sdr/HNAA2026012000008), Jan 12, 2026: WARNING MESSAGE. FALSE ACTIVATION. BLEED 1-2 VALVE CLOSED MSG ON EICAS & WOULD NOT RESET. PERFORMED OPS CHECK OF ENGINE BLEED VALVES IAW AMM 36-11-01. OPS CHECK GOOD. AIRCRAFT IS GOOD FOR SERVICE
- [SDR HNAA2026012100036](https://openairdocs.org/sdr/HNAA2026012100036), Dec 21, 2025: INLET. CORRODED. RIGHT ENGINE INLET HAS CORROSION ON THE INTERNAL LWR SIDE WHERE THE GENERATOR INLETS ARE LOCATED. RAR RH ENGINE INLET IAW EMB 145 AMM 71-60-01,
- [SDR HNAA2025120100727](https://openairdocs.org/sdr/HNAA2025120100727), Nov 26, 2025: BLEED VALVE. FAULTED. BLD 2 VLV FAIL DURING T/O ROLL. R & R #2 BLEED VALVE IRW AMM 36-11-05. OPS CHECK GOOD. NO LEAKS NOTED. A/C OK FOR SERVICE4 AT THIS TIME
- [SDR HNAA2025120100827](https://openairdocs.org/sdr/HNAA2025120100827), Nov 26, 2025: BLEED VALVE. FAILED. BLEED 2 VALVE FAIL DURING T/O ROLL R & R NR 2 BLEED VALVE IAW AMM 36-11-05. OPS CHECK GOOD. NO LEAKS NOTED. A/C OK FOR SERVICE AT THIS TIME.
- [SDR HNAA2025101800707](https://openairdocs.org/sdr/HNAA2025101800707), Oct 17, 2025: BLEED VALVE. FAULTED. HSV 1 FAIL ON EICAS DURING T/O ROLL. R & R ENGINE BLEED VALVE 1 IAW AMM 36-11-05. OPS CHECK GOOD,. ACFT IS OK FOR SERVICE
- [SDR JJBA20251006015](https://openairdocs.org/sdr/JJBA20251006015), Oct 5, 2025: ENGINE. NO DISCREPANCY. POSSIBLE BIRD INGESTION, #2 ENGINE. PERFORMED BORESCOPE OF LAST STAGE COMPRESSORS FROM BOTTOM IGNITER PLUG. NO DEFECTS NOTED. PERFORMED BORESCOPE INSPECTION OF 
- [SDR HNAA2025092900652](https://openairdocs.org/sdr/HNAA2025092900652), Sep 27, 2025: ANTI-ICE VALVE. FAILED. ENG 1 ANTI-ICE VALVE FAILED DURING TAKE OFF ROLL. R & R NR 100 ENGINE ANTI-ICE VALVE IRT AMM 30-21-01. OPS CHECKED GOOD. A/C OK FOR SERVICE.
- [SDR HNAA2025092300638](https://openairdocs.org/sdr/HNAA2025092300638), Sep 22, 2025: BLEED VALVE. FAILED. BLEED 1 VALVE FAILED MESSAGE ON TO ROLL. R & R THE BLEED VALVE IAW AMM 36-11-05. OPS CHECKED GOOD IRT AMM 36-00-00-700-803-A. GROUND RAN AIRCRAFT. NO LEAKS NOTE
- [SDR JJBA20251006010](https://openairdocs.org/sdr/JJBA20251006010), Sep 8, 2025: PRECOOLER. NO TEST. LH ENG BLEED AIR PRECOOLER FAILED PRESSURE TEST. LH PRECOOLER REMOVED AND REPLACED.
- [SDR HNAA2025071000466](https://openairdocs.org/sdr/HNAA2025071000466), Jul 10, 2025: ENGINE. SMOKE. AFTER E-2 SHUTDOWN THERE WAS SMOKE OUT THE EXHAUST WITH A SMOKEY SMELL IN THE CABIN. COULD NOT DUPLICATE E2 SMOKE, SEE SEQ #2 FOR DMT. FOUND APU LEAKING OIL, SE
- [SDR HNAA2025061700455](https://openairdocs.org/sdr/HNAA2025061700455), Jun 16, 2025: WIRE HARNESS. DAMAGED. DURING TAKE OFF CLIMB ENG 2 OIL TEMP TEMP REACHED 133 DEG C. FOLLOWED QRH AND ENG WAS SHUT DOWN. FACT 18JUN25 16:21 CLT R+R'D #2 ENG INDICATING HARNESS IAW RRMM
- [SDR HNAA2025022000090](https://openairdocs.org/sdr/HNAA2025022000090), Feb 19, 2025: ENGINE. MAKING METAL. E-2 ENGINE SHUT DOWN DURING CLIMB OUT AT ABOUT 5300' EICAS E-2 OUT DISPLAYED. (CAPT SAID OIL QTY STILL FULL AND NO ABNORMAL NOISES HEARD.) FACT 24FEB25 15:08 RD
- [SDR HNAA2024122301234](https://openairdocs.org/sdr/HNAA2024122301234), Dec 22, 2024: ENGINE. FAULTED. LOUD BANG ENG 1 OUT MESSAGE. NO N2 ROTATION. R & R #100 ENG IAW W/C 71-00-0. OPS CHECK GOOD.
- [SDR HNAA2024102901034](https://openairdocs.org/sdr/HNAA2024102901034), Oct 28, 2024: ENGINE. MAKING METAL. ENGINE 2 SHUTDOWN IN FLIGHT, WITH NO N2 ROTATION DFRL 28OCT24 21:14 PHL MX FOUND FOD IN CORE AND EXHAUST. RAR #2 ENGINE IAW WC 710000 AND OPS CHECKED IAW WC 727
- [SDR OZCA2024007241](https://openairdocs.org/sdr/OZCA2024007241), Oct 9, 2024: FMS. FAILED. ENROUTE FROM KMIA TO WMCR FOR HURRICANE EVACUATION, OVER CUBAN AIRSPACE, THE FMS DISPLAY AS WELL AS ROUTE INFORMATION ON THE MFD WERE LOST, AFTER THIS A SMELL O
- [SDR HNAA2024100700935](https://openairdocs.org/sdr/HNAA2024100700935), Oct 4, 2024: BLEED VALVE. FAILED. HS VLV 2 FAIL ON T/O ROLL MEL 04OCT24 18:37 EWN C27818 36-1-3 RIGHT ENG BLEED INOP DFRL 04OCT24 22:55 EWN C/W MEL PROCEDURE. E2 BLD VLV SECURED CLOSED.
- [SDR HNAA20240903211](https://openairdocs.org/sdr/HNAA20240903211), Sep 3, 2024: ENGINE. BIRD INGESTION. DURING APPROACH #1 ENGINE FLAMED OUT AFTER BIRD STRIKE. CREW SAID SHORTLY AFTER PASSING 2200 FT.
- [SDR HNAA20240903212](https://openairdocs.org/sdr/HNAA20240903212), Sep 2, 2024: PUMP. MALFUNCTIONED. DURING GEAR RETRACTION HYD QTY 1 DROPPED THAN DROPPED AGAIN DURING LEVEL CRUISE. R & R NR 1 EDP IRT AMM 29-10-03. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.
- [SDR HNAA2024090300711](https://openairdocs.org/sdr/HNAA2024090300711), Aug 31, 2024: ENGINE. BIRD INGESTION. DURING APPROACH #1 ENGINE FLAMED OUT AFTER BIRD STRIKE. #1 ENGINE R+R IAW W/C 71-00-00. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR HNAA202408270205](https://openairdocs.org/sdr/HNAA202408270205), Aug 25, 2024: WARNING MESSAGE. ACTIVATED. DURING CLIMB, RUD SYSTEM 1/2 INOP EICAS MESSAGE, FOLLOW QRH AND SELECTED #2 OFF AND #1 SYSTEM RETURNED.
- [SDR HNAA202408270206](https://openairdocs.org/sdr/HNAA202408270206), Aug 25, 2024: RUDDER. FAILED. RUDDER SYSTEM 1/2 INOP, YAW DAMPER FAIL AND AUTOPILOT FAIL EICAS MESSAGE DISPLYED. RAN QRH RUDDER 1-2 INOP MESSAGE PERSISTED.
- [SDR HNAA2024082700656](https://openairdocs.org/sdr/HNAA2024082700656), Aug 23, 2024: LIGHT. MALFUNCTIONED. FLIGHT DECK AND F/A EMERGENCY LIGHT CAME ON COMMANDED DURING PUSHBACK WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION.
- [SDR HNAA2024052400473](https://openairdocs.org/sdr/HNAA2024052400473), May 23, 2024: ENGINE. POWER LOSS. ENGINE #2 ROLLED BACK WITH LOUD BANG ON TAKEOFF ROLL. ( CAPTAIN SAID HE REJECTED TAKEOFF AND REQUESTED MAINTENANCE TO TOW THE PLANE BACK, AFTER WHICH HE SHUT DO
- [SDR HNAA2024050900345](https://openairdocs.org/sdr/HNAA2024050900345), May 8, 2024: ANTI-ICE VALVE. FAULTED. ON T/O ROLL AT 60 KNTS ICE COND-A/I INOP, NO T/O CONFIG AND E2 A/ICE FAIL DISPLAYED. E2 A/ICE FAIL REMAINS DISPLAYED. FACT 08MAY24 19:00 TRI PERFORMED A/ICE VAL
- [SDR HNAA2024050800333](https://openairdocs.org/sdr/HNAA2024050800333), May 6, 2024: BLEED VALVE. FAULTED. BLEED 2 VALVE FAIL MSG ON TAKE OFF ROLL. FACT 06MAY24 16:07 ROA R&R'D #2 ENG HIGH STAGE PRESS SWITCH IAW AMM 30-11-07 PERFORMED EBV OPS CHECK IAW AMM 36-11-05 H
- [SDR HNAA2024031500192](https://openairdocs.org/sdr/HNAA2024031500192), Mar 14, 2024: BLEED VALVE. WARNING MESSAGE. BLEED 1 VLV CLOSED EICAS MESSAGE DISPLAYED FOR APROX 20 MINS. SELF CLEARED AND DID NOT REAPPEAR. R&R E1 BLEED VALVE. NO FIX. DONE IAW AMM 36-11-05. R&R BLEED 1 
- [SDR HNAA2024031100190](https://openairdocs.org/sdr/HNAA2024031100190), Mar 8, 2024: BLEED VALVE. FAILED. AT 27K FT ENCOUNTERED ICING OBSERVED BLEED VALVE 2 FAIL, OBSERVED 3K FT PER MINUTE IN RATE OF CLIMB. WING ANTI ICE MESSAGE ICE CONDITION ANTI ICE WARNING. RAN Q
- [SDR K4DA202308230001](https://openairdocs.org/sdr/K4DA202308230001), Aug 23, 2023: UNKNOWN. UNKNOWN. DURING CLIMB OUT (3 - 6 MINUTES) CAS MESSAGE DISPLAYED "FAN DAMAGE R" FOLLOWED SHORTLY BY THE RIGHT ENGINE SHUTTING DOWN. AIRCRAFT RETURNED TO THE DEPARTING AIR
- [SDR HNAA2022103100297](https://openairdocs.org/sdr/HNAA2022103100297), Oct 27, 2022: ENGINE. UNKNOWN. DURING CLIMB ENG 2 OUT EICAS MESSAGE WITH NOTABLE POP SOUND. R&R #2 ENGINE IAW W/C 71-00-00
- [SDR HNAA2022090700256](https://openairdocs.org/sdr/HNAA2022090700256), Sep 6, 2022: ENGINE. HUNG START. ENGINE 2 HUNG START, AFTER START WAS ABORTED FUMES WERE NOTED IN CABIN AND FLIGHT DECK. INSPECTED #2 ENGINE FOR POSSIBLE FUEL LEAK. NONE FOUND. PERFORMED #2 ENG
- [SDR HNAA2022090700257](https://openairdocs.org/sdr/HNAA2022090700257), Sep 6, 2022: FADEC. FAULTED. HUNG START OF #2 ENG FOLLOWED BY EXHAUST FUMES. OIL NOTED DRIPPING FROM #2 LOWER COWLING. RAN E2 OFF FADEC A WITH NO DEFECTS NOTED. RAN E2 OFF FADEC B WITH HUNG
- [SDR SIMA2021090183001](https://openairdocs.org/sdr/SIMA2021090183001), Aug 31, 2021: ROLLER. SEIZED. NO 1 ENGINE THRUST LEVER WILL NOT ADVANCE TO MAX THRUST DECLARED EMERGENCY. CLEANED AND FREED UP ROLLER ON RH POWER LEVER AND SLIDING ROD ASSEMBLY IN THE RH POW
- [SDR HNAA2021071500323](https://openairdocs.org/sdr/HNAA2021071500323), Jul 13, 2021: ENGINE. SMOKE. SMOKE AND SMELL COMING FROM #1 ENG AFTER SHUTDOWN FROM INLET AND EXHAUST. USED BORESCOPE TO INVESTIGATE POSSIBLE OIL LEAK FOUND OIL COATING ON OIL SUPPLY LINE T
- [SDR HNAA2021062100268](https://openairdocs.org/sdr/HNAA2021062100268), Jun 20, 2021: LINE. CRACKED. DURING FLIGHT. E2 A/I FAIL MESSAGE APPEARED. FOLLOWED QRH AND MESSAGE REMAINED. T/S IN REF TO FIM 30-11-00-810-801-A. INSPECTED ENG BLEED DUCTS ON #2 ENGINE. FO
- [SDR HNAA2021062100267](https://openairdocs.org/sdr/HNAA2021062100267), Jun 18, 2021: LINE. CRACKED. DURING FLIGHT WING A/I FAIL MESSAGE APPEARED. FOLLOWED QRH AND MESSAGE REMAINED. HA300 FACTED OUT AS - T/S IN REF TO FIM 30-11-00-810-801-A. INSPECTED ENG BLEED
- [SDR SIMA20210609004](https://openairdocs.org/sdr/SIMA20210609004), Jun 9, 2021: COMPRESSOR. DAMAGED. ENG 1 FAILURE ON CLIMBOUT, AFTER T/O CHECK COMPLETE, PASSING 5,500 FT LOUD BANG ENG 1 FAIL MESSAGE ON EICAS E1 FAILURE / DECLARED EMERGENCY / EQP SWAP FLT CONT.
- [SDR HNAA2021042200158](https://openairdocs.org/sdr/HNAA2021042200158), Apr 21, 2021: RELAY. FAILED. NR BLEED VALVE FAILED AT 60-65 KNOTS. REMOVED AND REPLACED RELAY K0172 IN REF TO AMM TASK 20-13-02-000-400-801-A. OPS CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT OK 
- [SDR SIMA20210404002](https://openairdocs.org/sdr/SIMA20210404002), Apr 4, 2021: LINKAGE. CRACKED. LEFT ENGINE FORWARD LOWER YOKE-PYLON FORWARD LINKAGE IS CRACKED.-C/A-COMPLETE: REPAIRED LH ENGINE FORWARD LOWER YOKE PYLON LINKAGE FITTING IAW ERS- EM-54MR-698 
- [SDR HNAA2021032900104](https://openairdocs.org/sdr/HNAA2021032900104), Mar 26, 2021: BLEED VALVE. FAILED. BLEED 2 VALVE FAILED AT 40 KNOTS ON TAKEOFF, FAILED FOR THE SECOND TIME. R & R BLEED VALVE ON #2 ENGINE PER FIM 36-11-00,AND AMM 36-11-05. NO FIX, LEAK CHECK GO
- [SDR SIMA20210212001](https://openairdocs.org/sdr/SIMA20210212001), Feb 12, 2021: FUEL/OIL COOLER. MALFUNCTIONED. ABORTED TAKE OFF 80KTS ACCT MECHANICAL E1 FUEL LOW TEMP MSG ON E1 OIL TEMP 26C, OIL PRESSURE 70-80 PSI. AMBIENT TEMP -29C FLIGHT CANCELED-C/A-TROUBLESHOT IAW RR
- [SDR JJBA20210211011](https://openairdocs.org/sdr/JJBA20210211011), Feb 11, 2021: ANTI-ICE VALVE. CRACKED. ENG A/I FAIL, NO ICE ON, AND BLEED 1 LOW TEMP MESSAGES IN FLIGHT (E2 E/I FAIL WITH NO ICE A/I ON MESSAGES ON CLIMB FROM FL220 TO FL270. BLEED 1 LOW TEMP CAME ON
- [SDR YV3R2021020300429](https://openairdocs.org/sdr/YV3R2021020300429), Jan 29, 2021: DUAL TACHOMETER. DEFECTIVE. CUSTOMER REPORTED DUAL TACHOMETER ASSEMBLY P/N: F792-1 ROTOR RPM NEEDLE WAS ERRATIC.

All 321: https://openairdocs.org/engine/rolls-royce-ae-3007a1/reports.md

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