# GE GE90-90B

- Type: Engine model (FAA registry)
- Registry code: 30036
- Manufacturer (registry): GE
- Model: GE90-90B
- Engine type: Turbo-fan
- Power: 94,000 lb thrust
- Data sheet: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (OpenAirDocs)
- Holder: General Electric Company GE Aviation
- Installed in: 23 registered aircraft
- Page: https://openairdocs.org/engine/ge-ge90-90b

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 2025-25-07](https://openairdocs.org/ad/2025-25-07): Turbine Section · General Electric Company GE GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 6, 2026
- [AD 2023-26-07](https://openairdocs.org/ad/2023-26-07): Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 27, 2024
- [AD 2023-05-17](https://openairdocs.org/ad/2023-05-17): Turbine Section · General Electric GE90-76B, GE90-85B, GE90-90B and 1 more. Effective May 10, 2023
- [AD 2022-23-09](https://openairdocs.org/ad/2022-23-09): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Jan 17, 2023
- [AD 2022-18-06](https://openairdocs.org/ad/2022-18-06): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 26, 2022
- [AD 2021-26-06](https://openairdocs.org/ad/2021-26-06): Turbine Engine Accessory Drive · General Electric GE90-76B, GE90-85B, GE90-90B and 3 more. Effective Feb 15, 2022
- [AD 2018-17-12](https://openairdocs.org/ad/2018-17-12): Turbine Engine Compressor Section · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Sep 24, 2018
- [AD 2017-08-06](https://openairdocs.org/ad/2017-08-06): Engine Oil Cooler · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective May 22, 2017
- [AD 2017-08-05](https://openairdocs.org/ad/2017-08-05): Engine Compressor Section · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective May 19, 2017
- [AD 2016-19-09](https://openairdocs.org/ad/2016-19-09): High-pressure compressor (HPC) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Nov 4, 2016
- [AD 2015-27-01](https://openairdocs.org/ad/2015-27-01): High-pressure compressor (HPC) stage 8-10 spool · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Jan 27, 2016
- [AD 2013-17-07](https://openairdocs.org/ad/2013-17-07): Stage 1 high-pressure turbine (HPT) stator shrouds · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 18, 2013
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-15-06](https://openairdocs.org/ad/2011-15-06): High-pressure compressor rotor (HPCR) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Aug 18, 2011
- [AD 2002-04-11](https://openairdocs.org/ad/2002-04-11): Life Limits Section of Instructions for Continued Airworthiness (ICA) · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Apr 8, 2002
- [AD 2002-01-12](https://openairdocs.org/ad/2002-01-12): High Pressure Turbine (HPT) Interstage Seal · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Feb 26, 2002
- [AD 2002-01-27](https://openairdocs.org/ad/2002-01-27): High Pressure Compressor Stage 2-6 Spool · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Feb 14, 2002
- [AD 2001-21-03](https://openairdocs.org/ad/2001-21-03): P3B and Ps3 Sense Lines · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Nov 26, 2001
- [AD 2000-03-02](https://openairdocs.org/ad/2000-03-02): General Electric GE90-76B, GE90-85B and GE90-90B. Effective Apr 7, 2000
- [AD 97-12-05](https://openairdocs.org/ad/97-12-05): (VSCF) Gearshaft Flange ball Bearing · General Electric GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Jun 27, 1997
- [AD 97-12-04](https://openairdocs.org/ad/97-12-04): Liberated CDP Manifold Material · General Electric Aircraft Engines GE90-92B, GE90-76B, GE90-77B and 2 more. Effective Jun 27, 1997

Historical (superseded or no longer in force):

- [AD 2016-13-05](https://openairdocs.org/ad/2016-13-05) (historical): High-pressure compressor (HPC) stage 8-10 spool · General Electric GE90-76B, GE90-77B, GE90-85B and 2 more. Effective Jul 29, 2016
- [AD 2000-08-10](https://openairdocs.org/ad/2000-08-10) (historical): Life-limited Rotating Engine Parts · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 1 more. Effective Oct 23, 2000
- [AD 99-27-15](https://openairdocs.org/ad/99-27-15) (historical): Full Authority Digital Engine Control · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 17 more. Effective Jan 11, 2000
- [AD 99-08-17](https://openairdocs.org/ad/99-08-17) (historical): General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 2 more. Effective May 13, 1999
- [AD 98-15-03](https://openairdocs.org/ad/98-15-03) (historical): High Pressure Compressor · General Electric Aircraft Engines GE90-76B, GE90-77B, GE90-85B and 17 more. Effective Jul 29, 1998

## Information bulletins (advisory) (1)

- [SAIB NE-12-26](https://openairdocs.org/saib/NE-12-26): Fan Blade  GE90 Updated Inspections. Issued Apr 16, 2012

## Registered aircraft (23)

- [N27015](https://openairdocs.org/aircraft/N27015): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2000, S/N 28678
- [N37018](https://openairdocs.org/aircraft/N37018): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2002, S/N 31680
- [N57016](https://openairdocs.org/aircraft/N57016): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2000, S/N 28679
- [N69020](https://openairdocs.org/aircraft/N69020): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2007, S/N 31687
- [N74007](https://openairdocs.org/aircraft/N74007): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29477
- [N76010](https://openairdocs.org/aircraft/N76010): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29480
- [N76021](https://openairdocs.org/aircraft/N76021): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2010, S/N 39776
- [N77012](https://openairdocs.org/aircraft/N77012): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29860
- [N77014](https://openairdocs.org/aircraft/N77014): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29862
- [N77019](https://openairdocs.org/aircraft/N77019): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2007, S/N 35547
- [N77022](https://openairdocs.org/aircraft/N77022): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2010, S/N 39777
- [N777AS](https://openairdocs.org/aircraft/N777AS): [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), built 2003, S/N 29271
- [N78001](https://openairdocs.org/aircraft/N78001): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 27577
- [N78002](https://openairdocs.org/aircraft/N78002): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 27578
- [N78003](https://openairdocs.org/aircraft/N78003): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 27579
- [N78004](https://openairdocs.org/aircraft/N78004): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 27580
- [N78005](https://openairdocs.org/aircraft/N78005): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 27581
- [N78008](https://openairdocs.org/aircraft/N78008): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29478
- [N78009](https://openairdocs.org/aircraft/N78009): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29479
- [N78013](https://openairdocs.org/aircraft/N78013): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29861
- [N78017](https://openairdocs.org/aircraft/N78017): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2002, S/N 31679
- [N79011](https://openairdocs.org/aircraft/N79011): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1999, S/N 29859
- [N892FD](https://openairdocs.org/aircraft/N892FD): [Federal Express Cor](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20COR), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2011, S/N 38707

## NTSB investigations (3)

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 DCA23LA213](https://openairdocs.org/ntsb/DCA23LA213), Mar 21, 2023: Boeing 777-224 (N79011), Sacramento, CA, no damage. Probable cause: An encounter with forecast convective turbulence during climb.
- [NTSB DCA16WA176](https://openairdocs.org/ntsb/DCA16WA176), Jun 5, 2016: Boeing 777 24Q (N777AS), Paris, France, incident, minor damage
- [NTSB NYC05FA054](https://openairdocs.org/ntsb/NYC05FA054), Mar 2, 2005: Boeing 777-200 (N78008), Newark, NJ, substantial damage. Probable cause: The captain's failure to follow company procedures, which resulted in a tail strike. Contributing were the gusty crosswind and tailwind conditions, and the manufacturer's failure to provide adequate…

## FAA accident and incident reports (10)

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 20260715008939I](https://openairdocs.org/incident/20260715008939I), Jul 15, 2026: Boeing 777-224 (N78003), Newark, Minor damage. The right backup generator (bug) failed during climb. Upon inspection by maintenance, it was discovered that the shaft sheared.
- [Incident 20260429003309I](https://openairdocs.org/incident/20260429003309I), Apr 29, 2026: Boeing 777-224 (N27015), Minor damage. On walk around found huge birds strike on r/h wing. The only damage found was on the landing light panel, and damage was found on the right-wing root area…
- [Incident 20251213021069I](https://openairdocs.org/incident/20251213021069I), Dec 13, 2025: Boeing 777-224 (N78004), Dulles, VA, Minor damage. Just after take-off, on climb out aircraft experienced a compressor stall. Crew heard a loud bang followed by N1 rollback to 12%. EGT went up 1000 degrees for…
- [Incident 20251201017469I](https://openairdocs.org/incident/20251201017469I), Dec 1, 2025: Boeing 777-224 (N77019), Chantilly, VA, Minor damage. Bird strike occurred on the right downwind RWY01R. The pilot believed the bird was a Vulture or an eagle. The pilot called pct and reported damage to the #3…
- [Incident 20140116000729I](https://openairdocs.org/incident/20140116000729I), Jan 16, 2014: Boeing 777-224 (N78017), Newark, NJ, No damage. United flight 89 departed Newark, NJ (ewr) for beijing, china (pek). The captain's paperwork indicated turbulence due to a strong jet stream. The dispatcher's…
- [Incident 20051020029749I](https://openairdocs.org/incident/20051020029749I), Oct 20, 2005: Boeing 777224 (N57016), Houston, TX, Minor damage. (-23) Continental 34, B777, Houston/bush airport, October 20, 2005, while taxiing for departure struck tail end of American 1383, MD80, with the wing tip.…
- [Accident 20050302019029A](https://openairdocs.org/incident/20050302019029A), Mar 2, 2005: Boeing 777224 (N78008), Newark, NJ, Substantial damage. (-23) On 03/02/2005 at 1551E Continental airlines flight 99 at take-off reported striking the tail on runway 4L during rotation. The aircraft air returned into…
- [Incident 20030710019649I](https://openairdocs.org/incident/20030710019649I), Jul 10, 2003: Boeing 777224 (N78002), Springfield, IL. (-23) [privacy data omitted] while taxiing out for departure the pilot in command was turning the aircraft onto taxiway bravo at the bravo four intersection…
- [Incident 20011227034219I](https://openairdocs.org/incident/20011227034219I), Dec 27, 2001: Boeing 777224 (N78005), Newark, NJ. (-23) On Thursday December 27, 2001 at 1142 local, ewr ATCT reported to Continental airlines, B777, N78005 that fuel was coming from the left wing during take…
- [Incident 19990825030889I](https://openairdocs.org/incident/19990825030889I), Aug 25, 1999: Boeing 777224 (N78003), Newark, NJ. (-23) Flt 56 departed ewr with the right main gear pin installed, gear would not retract and pilot dumped 55,000 lbs. Of fuel and returned to ewr without…

## Service difficulty reports (61, newest 50)

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

- [SDR CALA2026070117512](https://openairdocs.org/sdr/CALA2026070117512), Jun 21, 2026: COMPRESSOR. STALLED. RIGHT ENG COMPRESSOR STALL AND EGT EXCEEDANCE AT V1 REVIEWED AHM DATA, FOUND EGT DATA PEAKED AT 138.5 FOR 6 SECS. REF AMM 71-00-00-200-814-G00 7.C.(2)(B) TAKEOF
- [SDR CALA2026062417313](https://openairdocs.org/sdr/CALA2026062417313), Jun 19, 2026: HMU. FAULTED. RIGHT ENGINE COMPRESSOR STALLED ON ROTATION NO EXCEEDENCES. PERFORMED FAULT ISOLATION NR 2 ENG IAW FIM 71-05, TASK 807, STEPS A - E, NO DEFECTS NOTED. NR 2 ENGI
- [SDR CALA2026051816333](https://openairdocs.org/sdr/CALA2026051816333), May 17, 2026: EXHAUST CONE. DAMAGED. UPON ARRIVAL, DURING WALKAROUND ON ENGINE #1 A DENT WAS FOUND IN THE TURBINE NOZZLE EXHAUST AT 6 O CLOCK POSITION. PICS ATTACHED 17 INCH LONG INNER CRACK, 0,02 
- [SDR CALA2026022614102](https://openairdocs.org/sdr/CALA2026022614102), Feb 23, 2026: ENGINE. VIBRATION. NR 1 ENG VIBRATION INDICATION. VIBRATION HIT 5.5. VIBRATION NOTED THROUGH AIRFRAME BY AIRCREW, SUGGESTS NOT AN INDICATION ISSUE. PERFORMED TEST NR 12A, LOW PRES
- [SDR CALA2026011512975](https://openairdocs.org/sdr/CALA2026011512975), Jan 10, 2026: OIL SYSTEM. LOW. RIGHT ENG OIL QTY 0 QTS, OIL PRESS HOVERING AROUND 20 PSI. NR 1 ENGINE IS THE DISCREPANT ENGINE. INITIAL OIL SVC ACCOMPLISHED. ADDED NR 1 ENG 26QTS, AND NR 2 EN
- [SDR CALA2026010912852](https://openairdocs.org/sdr/CALA2026010912852), Jan 6, 2026: ANTI-ICE VALVE. FAILED. ANTI ICE ENG L EICAS, LT ENG ANTI ICE VALVE DEACTIVATED IN OPEN POSITION WITH KIT WAITING FOR DEFERRAL. APPROVES MEL 3021T LT EAI VALVE DEACTIVATED OPEN WITH KI
- [SDR CALA2025091508880](https://openairdocs.org/sdr/CALA2025091508880), Sep 9, 2025: INDICATION SYS. INTERMITTENT. NR 2 ENGINE IS INDICATING INTERMITTENT OIL QUANTITY READINGS. NO FAULTS FOUND UNDER EXISTING FAULTS OR FAULT HISTORY RELATED TO RT ENG OIL QUANTITY INDICATION, 
- [SDR CALA2025080507289](https://openairdocs.org/sdr/CALA2025080507289), Aug 1, 2025: CARBON SEAL. LEAKING. NR 1 ENGINE HAS BEEN TRENDING STABLE AT A HIGH OIL CONSUMPTION (0.65-0.75QPH). ACCOMPLISHED SNIFF CHECK FOR FUEL IN OIL SYSTEM AND BAGGED DRAIN LINES COMING FRO
- [SDR CALA2025080107206](https://openairdocs.org/sdr/CALA2025080107206), Jul 31, 2025: HMU. FAULTED. OBSERVER ON GND REPORTED STREAM FROM LT WING. FUEL -3. 5 LT SIDE ON LDG. AT ARRIVAL FOUND ENGINE ONE FUEL LEAK OUT OF LIMITS ON THE VSV DRAIN. SUSPECTED HYDRO M
- [SDR CALA2025062505876](https://openairdocs.org/sdr/CALA2025062505876), Jun 22, 2025: FUEL SYS. UNKNOWN. ENG 2 SHUTDOWN PER FUEL LEAK CHECKLIST. OIL PRESS ABV 10PSI. WINDMILL 45MIN. RAN ENGINE 2 TO PERFORM 5 MIN LEAK CHECK WITH NO SIGNS OF FUEL LEAKAGE FLAGGING SDR
- [SDR CALA2025051304651](https://openairdocs.org/sdr/CALA2025051304651), May 11, 2025: ENGINE. OIL CONSUMPTION. E1 ESN 900511 HAS EXPERIENCED AN INCREASE IN OIL CONSUMPTION. PL EASE ACCOMPLISH A SNIFF CHECK OF THE OIL FOR FUEL SMELL IN THE O IL SYSTEM, REF. AMM 12-13-01-2
- [SDR 2025FA0000184](https://openairdocs.org/sdr/2025FA0000184), Mar 3, 2025: CASE. DAMAGED. DURING ROOT CAUSE ANALYSIS WHILE PROCESSING OF A CUSTOMER COMPLAINT (202502-1029217) MTU MAINTENANCE CHECKED PREVIOUSLY REPAIRED GE90 FAN STATOR MODULES INCLUDI
- [SDR CQ5Y2025FA0000184](https://openairdocs.org/sdr/CQ5Y2025FA0000184), Mar 3, 2025: CASE. DAMAGED. DURING ROOT CAUSE ANALYSIS WHILE PROCESSING OF A CUSTOMER COMPLAINT (202502-1029217) MTU MAINTENANCE HANNOVER GMBH CHECKED PREVIOUSLY REPAIRED GE90 FAN STATOR M
- [SDR CALA2024111301119](https://openairdocs.org/sdr/CALA2024111301119), Nov 10, 2024: ENGINE. OIL CONSUMPTION. E2 ESN 900229 HAS EXPERIENCED AN INCREASE IN OIL CONSUMPTION. PLEASE ACCOMPLISH A SNIFF CHECK OF THE OIL FOR FUEL SMELL IN THE OIL SYSTEM, REF. AMM 12-13-01-200
- [SDR CALA2022042101048](https://openairdocs.org/sdr/CALA2022042101048), Apr 21, 2022: SHROUD. DAMAGED. RIGHT ENGINE ABRADABLE SHROUD AT 9 O''CLOCK POSITION: MATERIAL MISSING, DIMENSION IS 0.75 INCH X 1 INCH X 0.14 INCH DEEP. PERFORMED ABRADABLE SHROUD INSPECTION 
- [SDR CALA2019041900588](https://openairdocs.org/sdr/CALA2019041900588), Apr 9, 2019: TUBE. LEAKING. L ENG INFLIGHT SHUTDOWN AND AIR RETURNED BACK TO DEPARTURE DUE TO OIL PRESSURE INDICATION (ENGINE) AMBER LEFT ENGINE DUE TO TRF BALANCE TUBE FOUND BROKEN AND DA
- [SDR CALA2019041900589](https://openairdocs.org/sdr/CALA2019041900589), Apr 9, 2019: TUBE. BROKEN. L ENG INFLIGHT SHUTDOWN AND AIR RETURN BACK TO PVG DUE TO OIL PRESSURE INDICATION (ENGINE) AMBER LEFT ENGINE DUE TO TRF BALANCE TUBE FOUND BROKEN AND DAMAGE TO 
- [SDR CALA2019041900590](https://openairdocs.org/sdr/CALA2019041900590), Apr 9, 2019: TUBE. BROKEN. L ENG INFLIGHT SHUTDOWN AND AIR RETURN BACK TO PVG DUE TO OIL PRESSURE INDICATION (ENGINE) AMBER LEFT ENGINE DUE TO TRF BALANCE TUBE FOUND BROKEN AND DAMAGE TO 
- [SDR CALA2017051201355](https://openairdocs.org/sdr/CALA2017051201355), May 12, 2017: ENGINE. MAKING METAL. GEAR CONFIG T/O WARNING ON TAKEOFF DUE TO SLOW LEFT ENG SPOOL U P T/S AND FOUND METAL IN THE TAILPIPE. REQUIRES ENGINE CHANGE. REMOVED #1 ENGINE DUE TO DAMAGE R
- [SDR CALA2016092700700](https://openairdocs.org/sdr/CALA2016092700700), Sep 27, 2016: WIRE HARNESS. DAMAGED. RT ENGINE HAS 3 FAULTS AND IS SURGING N1 AND N2 89-96%. EEC WILL NOT REVERT TO ALT. ENG IGN RT ENG C1 RT ENG CTL RT THERE IS NO PROCEDURE FOR THE PILOT TO MANUA
- [SDR CALA2016042700260](https://openairdocs.org/sdr/CALA2016042700260), Apr 27, 2016: WARNING SYSTEM. FALSE ACTIVATION. EGT INDICATION, ENG, RED LT ENG, LT EGT RED ON TAKEOFF. COMPLIED WITH BORESCOPE INSPECTION OF STG 1 HPT BLADES IAW AMM 71-00-00-200-814-G00 & AMM 71-00-00-200-8
- [SDR CALA2015081400665](https://openairdocs.org/sdr/CALA2015081400665), Aug 14, 2015: COWLING. DAMAGED. FOUND NR 2 ENG OTBD THRUST REVERSER COWL DAMAGED. RT OTBD THRUST REVERSER C DUCT HAD BURN THROUGH HOLE DUE TO BORESCOPE PLUG DISLODGED. REPLACED NR 2 ENG OTBD T
- [SDR CALA2015041300279](https://openairdocs.org/sdr/CALA2015041300279), Apr 13, 2015: LENS. LOOSE. SMALL EXIT SIGN COVER NEAR DOOR 1R HANDLE IS LOOSE & WILL NOT STAY ATTACHED DURING TURBULENCE. ON LT SIDE OF BUSSELL. COVER SECURED, CHECKED OK. THIS ITEM IS SD
- [SDR CALA2015010900028](https://openairdocs.org/sdr/CALA2015010900028), Jan 8, 2015: COMPRESSOR. STALLED. RIGHT ENG COMP STALL & DISPLAYED ENG FAIL AT 80 KTS ON FULL POWER TO DUE STRONG LT CROSSWINDS & WIND SHEAR. COMPLIED WITH ENG STALL INSPECTION IAW MM 71-00-00-2
- [SDR CALA2014060500728](https://openairdocs.org/sdr/CALA2014060500728), Jun 5, 2014: UNKNOWN. MALFUNCTIONED. ON TAKEOFF EGT ON LT ENG REDLINED AT APPROXIMATELY 100 KIAS, DECISION WAS MADE TO REJECT. PERFORMED DETAIL VISUAL CHECK OF ENG INLET & EXHAUST, NO FAULT FOUND. 
- [SDR CALA2012091700607](https://openairdocs.org/sdr/CALA2012091700607), Sep 17, 2012: STRIKER. INOPERATIVE. COCKPIT DOOR FAILS TO UNLOCK. R & R SOLENOID ACTUATED DOOR STRIKER IAW AMM 52-52-01. OPS CHECK GOOD.
- [SDR CALA2012091700604](https://openairdocs.org/sdr/CALA2012091700604), Sep 15, 2012: WIRE. LOOSE. ELECTRIC ODOR ON DECENT, WENT AWAY, ELECTRIC ODOR AGAIN ON TAXI-IN THEN GOES AWAY, AFTER BLOCK IN F/O AND IROS DETECTED ELECTRICAL ODOR AGAIN OVER BY F/O SIDE O
- [SDR CALA2012082100525](https://openairdocs.org/sdr/CALA2012082100525), Aug 21, 2012: HMU. MALFUNCTIONED. RIGHT ENGINE FAILED AND EGT ROSE TO START LIMIT. ENGINE WAS SHUTDOWN. CHECKED MAT FOR CURRENT LEG FAULTS, FOUND 73-31802 AND 73-21002 . TROUBLESHOT IAW FIM 73-2
- [SDR CALA2012082100526](https://openairdocs.org/sdr/CALA2012082100526), Aug 21, 2012: CHILLER. INOPERATIVE. F/A CALLED SAID HEAVY HOT ELECTRIC SMELL IN REAR OF CABIN PERFORMED SMOKE/ODOR INSP IAW AMM 05-51-58-800-801C3. FOUND MID GALLEY SFT CHILLER OVERHEATING & AMP; 
- [SDR CALA2012081300500](https://openairdocs.org/sdr/CALA2012081300500), Aug 10, 2012: SKIN. DAMAGED. LIGHTINING STRIKE AT BS 1245 STR 6 LT. INSTALLED REPAIR DOUBLER AS REF TO SRM 53-00-01. REPAIR 6, FIG 203 AND ECRA 5340-01470.
- [SDR CALA2012081300501](https://openairdocs.org/sdr/CALA2012081300501), Aug 10, 2012: SKIN. DAMAGED. LIGHTINING STRIKE AT BS 1245, STRINGER 6 LT. INSTALLED REPAIR DOUBLER AS REF TO SRM 53-00-01. REPAIR 6, FIG 203 AND ECRA 5340-01470.
- [SDR CALA2012080600497](https://openairdocs.org/sdr/CALA2012080600497), Aug 6, 2012: CHILLER. INOPERATIVE. STRONG ELECTRICAL ODOR AT AFT GALLEY. GALLEY POWER SWITCH TURNED OFF AND CIRCUIT BREAKERS PULLED. ODOR DISSAPATED, FOUND AFT GALLEY CHILLER B CIRCUIT BREAKER TR
- [SDR CALA2011111100728](https://openairdocs.org/sdr/CALA2011111100728), Nov 11, 2011: PLUG. OUT OF POSITION. UPON OPENING NR 2 ENGINE COWLING FOUND HPC STAGE 4 BORESCOPE PLUG "F" LAYING IN T/R HALF. REF L/P 8977608 AND L/P 8977609 FOR INSTALLATION OF BORESCOPE PLUG AND
- [SDR CALA2011102400684](https://openairdocs.org/sdr/CALA2011102400684), Oct 24, 2011: PLUG. MISSING. WHILE PERFORMING T/S ON NR 1 ENG, FOUND DAMAGE ON LEFT T/R FIRE BLANKET ALSO FOUND HIGH PRESS COMPRESSOR BOROSCOPE PLUG MISSING ON LEFT SIDE (8TH STAGE VANE H.P
- [SDR ASMF201012009](https://openairdocs.org/sdr/ASMF201012009), Dec 17, 2010: TIRE. DAMAGED. DURING TOWING TO PLATFORM, THE TOW TRACTOR DRIVER WAS EXCEEDING THE MAXIMUM NLG TOWING ANGLE TO LT SIDE AND TOW BAR WAS BROKEN. MX PERFORMED THE MAXIMUM NLG TOW
- [SDR ASMF201009001](https://openairdocs.org/sdr/ASMF201009001), Sep 1, 2010: SKIN. DAMAGED. CAPTAIN REPORTED A LIGHTNING STRIKE IN THE LT SIDE LOWER FUSELAGE SKIN. MX PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, NO DAMAGES WERE DETECTED.
- [SDR ASMF201008004](https://openairdocs.org/sdr/ASMF201008004), Jul 3, 2010: SKIN. DAMAGED. DURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN. MX PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTING RIVETS WITH HEAD BURNE
- [SDR ASMF201006004](https://openairdocs.org/sdr/ASMF201006004), Jun 27, 2010: FLAP SYSTEM. MALFUNCTIONED. ACFT REJECTED TAKEOFF AT 65 KNOTS, DURING TAKEOFF ACCELERATION A FLAP CONFIGURATION ALARM WITH RED ANNOUNCEMENT TURNED ON. MX PERSONNEL VERIFIED FOR FAILURE DET
- [SDR 2010FA0000693](https://openairdocs.org/sdr/2010FA0000693), Jun 7, 2010: SEAL. CRACKED. (QEMY) DURING O/H OF THE HPT FORWARD SEAL, 2OF CRACKS NOTED ON WEBB SECTION. BOTH CRACKS RUN IN A RADIAL DIRECTION. THE LONGEST OF THE TWO CRACKS IS 0.350" LONG
- [SDR 2010FA0000694](https://openairdocs.org/sdr/2010FA0000694), Jun 7, 2010: SEAL. UNSERVICEABLE. (QEMY) DURING DISASSEMBLY OF THE HP TURBINE MODULE, THE HPT FORWARD ROTATING SEAL WAS FOUND WITH LONG CRACK RUNNING RADIALLY ACROSS FRONT FACE OF SEAL. CRACK AP
- [SDR CALA2010060100237](https://openairdocs.org/sdr/CALA2010060100237), May 30, 2010: INDICATION SYS. MALFUNCTIONED. CLIMBING THRU 16.000 RECEIVED A CLEAR O2 LOW EICAS MSG. PRESSURE READ 50 PSI BUT 1400 PSI DURING PRE FLIGHT. PLACED INDICATION ON DEFERRAL INOP CONFIRMED BOTTLE
- [SDR CALA2010041200134](https://openairdocs.org/sdr/CALA2010041200134), Apr 11, 2010: EEC. MALFUNCTIONED. AS PER MAINTENANCE CONTROL REQUEST, REMOVE & REPLACE RIGHT ENGINE EEC IN REFERENCE TO L/P 8478370 ENG R1 AND R2 IGNITION FAULTS. R&R''D NR 2 ENG EEC AS 
- [SDR 2009FA0001077](https://openairdocs.org/sdr/2009FA0001077), Dec 22, 2009: COMPRESSOR. MISMANUFACTURED. NOTIFICATION REGARDING A CONFIGURATION ISSUE WITH HP COMPRESSOR. SN UMO22124- FITTED TO ESN 900223 HAS A 3D CONFIG RUDDER ( 350-007-530-0) FITTED INSTEAD OF A 2
- [SDR 2009FA0001078](https://openairdocs.org/sdr/2009FA0001078), Dec 22, 2009: COMPRESSOR. MISMANUFACTURED. RECEIVED NOTIFICATION REGARDING A CONFIGURATION ISSUE WITH HP COMPRESSOR. SN WM022163 - FITTED TO ESN 900149 HAS ONE SET OF 3D STG 1 SHROUDS FITTED (350-385-202
- [SDR 2009FA0000056](https://openairdocs.org/sdr/2009FA0000056), Jan 15, 2009: SEAL. UNSERVICEABLE. DURING DISSASSEMBLY OF THE HPT ROTOR, IT WAS NOTED THAT THE INTERSTAGE SEAL HAD ROTATED BEYOND ITS LOCKING MECHANISM RESULTING IN DAMAGE TO IST ID BAYONET FEATU
- [SDR ASMF200711004](https://openairdocs.org/sdr/ASMF200711004), Nov 25, 2007: ENGINE. DAMAGED. CAPTAIN REPORTED THAT AT 39,000 FEET, LEFT ENGINE STALLED, DESCENDING TO 27,000 FEET WITH OSCILLATIONS IN N1 AND N2 WITH ENG CONTROL L AND ENG EEC C1 L MESSAGES
- [SDR ASMF200710004](https://openairdocs.org/sdr/ASMF200710004), Oct 18, 2007: ENGINE. OVERTEMP. AIRCRAFT REJECTED TAKEOFF AT 101 KNOTS DUE TO HIGH TEMPERATURE INDICATION ON THE LT ENGINE, REACHING 1035 CELSIUS DEGREES MOMENTARY AND 1015 DURING 11 SECONDS. 
- [SDR 2007FA0000350](https://openairdocs.org/sdr/2007FA0000350), Apr 1, 2007: SHAFT. UNSERVICEABLE. AIRCRAFT TAKEOFF WAS ABORTED, A 147 KNOTS AFTER ENGINE LOST POWER. AC WAS STOPPED SAFELY AND ALL PASSENGERS AND CREW DEPLANED SAFELY. UPON INSPECTION OF THE ENG
- [SDR CALA0700137](https://openairdocs.org/sdr/CALA0700137), Mar 20, 2007: SHAFT. FAILED. TAKEOFF WAS ABORTED AT 160 KNOTS DUE TO NR 2 ENGINE FAILURE. N1 WENT FROM 104 PERCENT TO 34 PERCENT. INITIAL EXAMINATION OF THE NR 2 ENGINE REVEALED METAL IN TH
- [SDR 2005FA0001289](https://openairdocs.org/sdr/2005FA0001289), Jun 21, 2005: SEAL. FAILED. DURING ENGINE O/H UPON EXPOSURE OF THE HPT ROTOR, EVIDENCE OF HEAT DISTRESS WAS NOTED AT THE AFT SEAL LOCATION. THE HPTR AFT SEAL SUMP SEAL TEETH AND OIL SLING 

All 61: https://openairdocs.org/engine/ge-ge90-90b/reports.md

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