# Service difficulty reports: N745AM, cancelled Apr 6, 2018

A list on [N745AM, cancelled Apr 6, 2018](https://openairdocs.org/deregistered/N745AM-2018-04-06.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ASMF20170531005](https://openairdocs.org/sdr/ASMF20170531005.md): Monitor · damaged · May 27, 2017 · N745AM · Boeing 7772Q8 · Flight Control System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAKE OFF, CONFIGURATION STABILIZER ALARM WAS ACTIVED. MAINTENANCE PERSONNEL PERFORMED INSPECTION IAW FIM 31-43 TASK 867, CONFIRMING FAILURE IN IOM 003 RH OF INVALID DATA, THEREFORE THE IOM M003 RIGHT WAS REPLACED IAW
- [SDR ASMF201705002](https://openairdocs.org/sdr/ASMF201705002.md): Pump · failed · May 16, 2017 · N745AM · Boeing 7772Q8 · Aircraft Fuel Distribution System
  > CAPTAIN REPORTED THAT DURING CRUISE, THE FUEL QUANTITY INDICATION WAS WRONG, FUEL QUANTITY WAS VERIFIED USING FUEL DIPSTICK. OPS TESTED FOR THE SYSTEM FUEL QUANTITY INDICATOR PERFORMED IAW AMM 28-24-00, FUEL TRANSFER WHEN NOT COMMANDED WAS PERFORMED IAW FIM 2
- [SDR ASMF201602007](https://openairdocs.org/sdr/ASMF201602007.md): Hydraulic Line · leaking · Jan 24, 2016 · N745AM · Boeing 7772Q8 · Hydraulic System, Main
  > CAPTAIN REPORTED THAT DURING APPROACH, THE HYD CENTRAL SYS QTY DECREASED TO 0.14 GAL & THE MSG IN EICAS & STATUS OF AUTO BRAKE SOL VLV WAS SHOWN. PERFORMED ACFT TURN AROUND, DETECTING HYD LEAK IN LT MLG HOSE. THE HOSE WAS REPLACED IAW AMM 20-10-14 & AMM 32-3
- [SDR ASMF201503012](https://openairdocs.org/sdr/ASMF201503012.md): Valve · loose · Feb 6, 2015 · N745AM · Boeing 7772Q8 · Landing Gear Brake System
  > DURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE WHEEL NR 4. DURING MX REVISION, THE WHEEL NR 4 WAS DETECTED LEAKING WITHIN LIMITS. THE BRAKES BLEED PORT OF THE WHEEL NR 4 WAS TIGHTENED & CLEANED IAW AMM 32-45-00, TESTED CORRECT.
- [SDR ASMF201407008](https://openairdocs.org/sdr/ASMF201407008.md): Bracket · broken · Jul 1, 2014 · N745AM · Boeing 7772Q8 · Main Landing Gear Strut/Axle/Truck
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO URGENT ATTENTION OF A SICK PAX. PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW MM 05-51-35 PHASE 1, DETECTING A RT MLG HYD TRUCK BRACKET BROKEN. EVALUATED THE DAMAGE & FOUND IT WITHIN LIMITS IAW AMM 32-10-01.
- [SDR ASMF2014061706010](https://openairdocs.org/sdr/ASMF2014061706010.md): Slide Raft · out of position · Apr 27, 2014 · N745AM · Boeing 7772Q8 · Escape Slide
  > DURING TRANSIT CHECK, THE LT DOOR SLIDE RAFT NR 2 WAS FOUND OUT OF POSITION ON THE ACFT FLOOR & WITH METAL SEAMS LOOSEN. ACFT WAS SENT TO THE HANGAR & SENT THE LT DOOR SLIDE RAFT TO SURVIVAL SHOP FOR ASSEMBLY CORRECTLY IAW CMM 25-61-52. INSTALLED THE RT DOOR
- [SDR ASMF201308008](https://openairdocs.org/sdr/ASMF201308008.md): Fairing · damaged · Jul 12, 2013 · N745AM · Boeing 7772Q8 · Wing Structure
  > DURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN RT ENGINE. BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING 6 FAIRING DAMAGES AND 2 PANELS WITH 4 IMPACT, BEING WITHIN LIMITS OF OPERATION IAW AMM 71-00-00. PANELS WERE REPAIRED I
- [SDR ASMF201211007](https://openairdocs.org/sdr/ASMF201211007.md): Probe · malfunctioned · Nov 18, 2012 · N745AM · Boeing 7772Q8 · Engine EGT/TIT Indicating System
  > ACFT RETURNED TO PLATFORM DUE TO AFTER RT ENGINE START, IT WAS HAD OSCILLATIONS BETWEEN 540 AND 580 CELSIUS DEGREES OF EGT. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE LOWER AND UPPER EGT PROBES AND HARNESS T-49 IAW MM 77-21-01 AND 77-21-05, TES
- [SDR ASMF201106001](https://openairdocs.org/sdr/ASMF201106001.md): Sensor · damaged · Jun 1, 2011 · N745AM · Boeing 7772Q8 · Cabin Cooling System
  > AIRCRAFT RETURNED DURING CLIMB, THE EICAS MESSAGE LT PACK WAS SHOWN AND IT WAS NOT AIR ON LT DUCT. DURING MX REVISION, THE MESSAGES 21-23041 WAS SHOWN, THE FIM 21-51 TASK 803 PROCEDURE WAS PERFORMED; SO THE LT PACK SENSOR WAS REPLACED IAW MM 21-51-03, TESTED C
- [SDR ASMF201010007](https://openairdocs.org/sdr/ASMF201010007.md): Sensor · damaged · Oct 20, 2010 · N745AM · Boeing 777222 · Turbine Engine Oil System
  > ACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DURING CLIMB THE ENG OIL FILTER SENSOR AND ENG OIL FILTER LIGHTS TURNED ON AND DURING CRUISE THE EICAS MESSAGE ENG OIL FILTER WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH 7.20 PROCEDURE, CONFIRMING THE FAILURE. DUR
- [SDR ASMF201008001](https://openairdocs.org/sdr/ASMF201008001.md): Tire · detached · Aug 19, 2010 · N745AM · Boeing 7772Q8 · Tire
  > DURING TAKEOFF RUN; A STRONG NOISE WAS HEARD, IECAS MESSAGE OF TIRE PRESS WAS SHOWN AND TIRE PRESS LIGHT TURNED ON, THE TIRE NR 1 WAS DEFLATED AND THE FLIGHT CONTINUED TO MAD IAW FCT 777 (TM) 8.18 (32-40-72-00 PROCEDURE). MX DETECTED MAIN TIRE NR 1 FLOOR DETA
- [SDR ASMF201004002](https://openairdocs.org/sdr/ASMF201004002.md): Blades · damaged · Mar 21, 2010 · N745AM · Boeing 7772Q8 · Turbine Engine Compressor Section
  > DURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENGINE WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGI
- [SDR ASMF20100321001](https://openairdocs.org/sdr/ASMF20100321001.md): Blade · damaged · Mar 21, 2010 · N745AM · Boeing 7772Q8 · Turbine Engine Compressor Section
  > DURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENG WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGINE
- [SDR ASMF200911001](https://openairdocs.org/sdr/ASMF200911001.md): Brake Assy · leaking · Nov 11, 2009 · N745AM · Boeing 7772Q8 · Landing Gear Brake System
  > DURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON THE RT MLG BRAKE NR 8. MX REPLACED THE BRAKE ASSY NR 8 IAW MM 32-45-07, TESTED CORRECT.
- [SDR MAS2008F00062](https://openairdocs.org/sdr/MAS2008F00062.md): Thrust Reverser · damaged · Aug 21, 2008 · N745AM · Boeing 7772Q8 · Engine Thrust Reverser
  > DURING TRANSIT CHECK WAS DETECTED THE OUTBOARD REVERSER OF THE RT ENGINE WITH EXTENDED DAMAGE ON FAN DUCT INNER WALL WITH MATERIAL MISSING OF 70 X 60 INCH BY IMPACT OF THE BOROSCOPE L PLUG, THE ACFT WAS SENT TO HANGAR FOR REVERSER REPLACEMENT WHICH WILL BE SEN
- [SDR 2008FA0000472](https://openairdocs.org/sdr/2008FA0000472.md): Engine · failed · Jun 6, 2008 · N745AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)
  > DURING TRANSIT CHECK, THE RT ENGINE WAS DETECTED WITH DAMAGES. MAINT PERFORMED BOROSCOPIC INSPECTION, DETECTING DAMAGES OUT OF LIMITS, SO RT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-00, ALL CORRECT. (K)
- [SDR 2008FA0000471](https://openairdocs.org/sdr/2008FA0000471.md): Sensor · failed · Jun 1, 2008 · N745AM · Boeing 7772Q8 · Engine Indicating System
  > AC RETURNED TO DEPARTURE DUT TO RT ENGINE STALLED. MAINT PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES. NO DAMAGES WERE DETECTED IAW MM 71-00-00. RT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED CORRECT. THE OVERWEIGHT
- [SDR ASMF200806001](https://openairdocs.org/sdr/ASMF200806001.md): Sensor · failed · Jun 1, 2008 · N745AM · Boeing 7772Q8 · Fuel Controlling System
  > AIRCRAFT RETURNED OF FLIGHT DUE TO RIGHT ENGINE STALLED. MAINTENANCE PERSONNEL PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES, NO DAMAGES WERE DETECTED IAW MM 71-00-00. RIGHT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED
- [SDR ASMF200710004](https://openairdocs.org/sdr/ASMF200710004.md): Engine · overtemp · Oct 18, 2007 · N745AM · Boeing 777* · Engine (Turbine/Turboprop)
  > 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. MAINTENANCE PERSONNEL PERFORMED FIM PROCEDURE 73-22 TASK 819 FOUND ALL CORRECT, ADDITIONALLY HIGH EN
- [SDR ASMF200607003](https://openairdocs.org/sdr/ASMF200607003.md): Scuff Plate · ground damage · Jul 2, 2006 · N745AM · Boeing 777* · Standard Practices/Structures
  > DURING TRANSIT CHECK, AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR PROMOTING A DENT OF 3 INCHES LONG, 1 INCH WIDE AND.2500 INCH DEPTH IN THE SCUFF PLATE OF THE ACCESS BULK CARGO, SO IT WAS REPAIRED IAW SRM 51-10-01. DURING OVERNIGHT CHECK SCUFF PLATE WAS REMOVED TO

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N745AM' AND deregistration_id = 'N745AM-2018-04-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N745AM-2018-04-06/reports

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