# Service difficulty reports: N776AM, cancelled Apr 14, 2017

A list on [N776AM, cancelled Apr 14, 2017](https://openairdocs.org/deregistered/N776AM-2017-04-14.md).

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

- [SDR ASMF201611015](https://openairdocs.org/sdr/ASMF201611015.md): Carbon Seal · leaking · Sep 25, 2016 · N776AM · Boeing 7772Q8 · Engine Oil Cooler
  > CAPTAIN REPORTED THAT DURING APPROACH, THE LEFT ENGINE OIL QUANTITY DECREASED TO 3 QTS WITH ENGINE PARAMETERS NORMAL. THE AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE LEAK CHECK IAW AMM 71-00-00-700-823, AMM 79-00-00-200-800,
- [SDR ASMF20160620011](https://openairdocs.org/sdr/ASMF20160620011.md): Transceiver · failed · May 6, 2016 · N776AM · Boeing 7772Q8 · Weather Radar System
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MESSAGE WXR FAIL. MAINTENANCE PERFORMED THE AIR/GROUND INTERFACE TEST IAW AMM 34-43-02, DETECTING WXR FAIL FLAG AND WXR SYS STATUS; SO THE LT TRANSCEIVER WAS REPLACED AND SYSTEM TEST WAS PERFORMED IAW AMM
- [SDR ASMF201602009](https://openairdocs.org/sdr/ASMF201602009.md): Windshield · cracked · Feb 3, 2016 · N776AM · Boeing 7772Q8 · Flight Compartment Windows
  > AIRCRAFT RETURNED FROM FLIGHT DUE TO, DURING CLIMB THE RT WINDSHIELD GOT CRACKED. PERFORMED THE QRH 1.9 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO THE HANGAR & MX REPLACED THE LT L1 WINDSHIELD ASSEMBLY IAW MM 56-11-01 & WINDOW HEAT SYS TEST WAS PERF
- [SDR ASMF201511008](https://openairdocs.org/sdr/ASMF201511008.md): Actuator Valve · failed · Nov 11, 2015 · N776AM · Boeing 7772Q8 · Engine Fuel Distribution
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG FAIL LIGHT TURNED ON WITHOUT ABNORMAL INDICATIONS & DURING THE RT ENG SHUTDOWN, THE EGT EXCEEDANCE WAS SHOWN. PERFORMED FIM 73-11 TASK 815 & FIM 73-22 TASK 815 & 820 PROCEDURES & IDLE POWER OPERAT
- [SDR ASMF201510028](https://openairdocs.org/sdr/ASMF201510028.md): Tire · punctured · Oct 9, 2015 · N776AM · Boeing 7772Q8 · Tire
  > AIRCRAFT RETURNED TO PLATFORM DUE TO MSG IN EICAS & STATUS OF LOW PRESS IN TIRE NR 11. PERFORMED REVISION DETECTING THE TIRE NR 11 WITH PRESS DROPPED OFF TO 26 PSI DUE TO DRILLING. WHEEL NR 11 WAS REPLACED IAW AMM 32-45-00, ALL CORRECT.
- [SDR ASMF201507018](https://openairdocs.org/sdr/ASMF201507018.md): Wire · damaged · Jun 29, 2015 · N776AM · Boeing 7772Q8 · Engine Fuel System Wiring
  > AIRCRAFT RETURNED TO PLATFORM, DURING LT ENG START, THE FAILURE CODE 73 21 52 51 & 732 152 51 WERE SHOWED & LT ENG NOT STARTED BY TWO ATTEMPTS. PERFORMED REVISION TO LT ENG, DETECTING LT HIGH PRESS FUEL SOV POSITION IN DISAGREE WITH COMMAND POSITION. THE FIM
- [SDR ASMF201310005](https://openairdocs.org/sdr/ASMF201310005.md): Radome · deformed · Sep 19, 2013 · N776AM · Boeing 7772Q8 · Aerodynamic Fairings
  > DURING TRANSIT CHECK, FOUND RADOME DEFORMED. FOUND OUT OF LIMITS IAW SRM 57-12-00. RADOME REPLACED IAW AMM 57-12-02.
- [SDR ASMF201306003](https://openairdocs.org/sdr/ASMF201306003.md): Wedge · cracked · Jun 2, 2013 · N776AM · Boeing 7772Q8 · Trailing Edge Flaps
  > DURING TRANSIT CHECK, THE T/E WEDGE RT OTBD FLAP WAS DAMAGED PROMOTING A CRACK OF 6.00" LENGTH AND 5.75" WIDE AT BS 214, ON UPPER & LOWER RT OTBD FLAP. MX PERSONNEL ISSUED THE NON ROUTINE CARD A0205977. THE T/E WEDGE RT OTBD FLAP WAS REPAIRED IAW SRM 57-53-0
- [SDR ASMF201210009](https://openairdocs.org/sdr/ASMF201210009.md): Engine · intermittent · Sep 29, 2012 · N776AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)
  > ACFT REJECTED TAKE AT 70 KNOTS WITH A GROSS WEIGHT OF 268 000 KG DUE TO RIGHT ENGINE STRONG EXPLOSION WITHOUT ADVISE ON ENGINE PARAMETERS OR EXCEEDS IN CREW CABIN WAS LISTENING. MX PERFORMED FIM 71-05 TASK 807 PROCEDURE; A RT ENGINE STALL INSPECTION IAW MM 71
- [SDR ASMF201207009](https://openairdocs.org/sdr/ASMF201207009.md): Panel · punctured · Jul 31, 2012 · N776AM · Boeing 7772Q8 · Nacelle/Pylon, Main Frame
  > DURING TRANSIT CHECK, DAMAGE WAS DETECTED IN THE NOSE COWLING SKIN ACOUSTIC PANEL OF THE LT ENGINE, A PUNCTURE 1 X 0.75 INCH BEING OUT OF LIMITS IAW SRM 54-11-01. THE DAMAGE WAS REPAIRED IAW AMX-12-0324-02B, TESTED CORRECT.
- [SDR ASMF201110002](https://openairdocs.org/sdr/ASMF201110002.md): Unknown · smoke · Oct 6, 2011 · N776AM · Boeing 7772Q8 · Air Distribution System
  > DURING CLIMB, SMOKE IN THE PASSENGER CABIN ON THE PREMIER CLASS AND THE FIRST 20 ROWS WAS VISIBLE ALONG THE CEILING; SO FLIGHT CREW ACCOMPLISHED THE QRH 8.5 PROCEDURE. ACFT RETURNED, MX PERSONNEL PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM
- [SDR ASMF201104002](https://openairdocs.org/sdr/ASMF201104002.md): Pump · leaking · Apr 4, 2011 · N776AM · Boeing 7772Q8 · Hydraulic Pump (Electric/Engine), Main
  > CAPTAIN REPORTED THAT DURING CRUISE, THE HYD QTY LOW LT AND HYD PRESS PRI LT LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 13.3 AND 13.22 PROCEDURES, CONFIRMING THE FAILURE AND CONTINUING TO DESTINATION. MX PERSONNEL, A REVISION, DETECTING HYD LEAK IN TH
- [SDR ASMF201007006](https://openairdocs.org/sdr/ASMF201007006.md): Wheel · damaged · Jul 23, 2010 · N776AM · Boeing 7772Q8 · Wheel/Ski/Float
  > DURING PUSH BACK THE TOW FITTING WAS BROKEN. MX PERFORMED GENERAL VISUAL INSP TO THE NLG IAW MM 05-51-01 DETECTING DAMAGE OUT OF LIMIT IN THE RT NOSE LANDING WHEEL. TECH REPLACED BOTH NOSE LANDING WHEELS IAW MM 32-45-02, TESTED CORRECT.
- [SDR ASMF201007003](https://openairdocs.org/sdr/ASMF201007003.md): Access Door · damaged · Jul 7, 2010 · N776AM · Boeing 777222 · Wing, Plate/Skin
  > DURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED BETWEEN SLAT NR 9 AND 10. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DAMAGES IN ANTI ICE RELEASE ACCESS DOORS SLAT. THE RT WING SLAT LEADING EDGE NR 9 WAS REPLACED IAW DWG NR 114W4565 AND INSTALLED FA
- [SDR ASMF201004001](https://openairdocs.org/sdr/ASMF201004001.md): Blades · damaged · Apr 12, 2010 · N776AM · Boeing 777222 · Turbine Engine Compressor Section
  > DURING A BORESCOPE INSP OF THE HPC 1, 4 AND 9 STAGES BLADES OF THE RT ENGINE WAS DETECTED. 1 BLADE OF THE HPC 1ST STAGE WITH L/E TIP CURLED 90 DEGREES OUT OF LIMITS IAW 72-00-00, PARA 5H (L) (7), PAGE 625; WITH DIMENSIONS OF 3.5 INCHES LENGTH AND 1.25 INCHES W
- [SDR ASMF20090402](https://openairdocs.org/sdr/ASMF20090402.md): Skin · damaged · Apr 14, 2009 · N776AM · Boeing 777 · Fuselage Main, Plate/Skin
  > DURING TRANSIT CHECK, MX FOUND 3 SCRATCHES OF.5 INCHES ON THE FUSELAGE SKIN, AT THE COVER RECEPTACLE EXTERNAL POWER. A SCRATCH AT STA 342 WITH THICKNESS FOUND 0.020 INCHES, AT STA 348 WITH THICKNESS FOUND 0.089 INCHES, AND AT STA 351 WITH THICKNESS FOUND 0.06
- [SDR ASMF 20081201](https://openairdocs.org/sdr/ASMF%2020081201.md): Tire · separated · Dec 1, 2008 · N776AM · Boeing 7772Q8 · Tire
  > DURING TAKE OFF, CAPTAIN REPORTED STRONG VIBRATION IN MLG. MX PERSONNEL DETECTED TREAD LOSS IN THE WHEEL POSITION NR 1 IN THE LT MLG, CRACK IN THE LT FLAP LOWER SKIN AT STA 261 AND A DENT OF 8 IN LONG X 4 IN WIDTH 0.200” DEPTH IN THE LOWER ACCESS PANEL 511JB
- [SDR ASM2008F00005](https://openairdocs.org/sdr/ASM2008F00005.md): Hose · damaged · Sep 13, 2008 · N776AM · Boeing 7772Q8 · Hydraulic System, Main
  > DURING TRANSIT CHECK, MAINT DETECTED DAMAGE AND HYDRAULIC LEAK ON SUPPLY HOSE ASSEMBLY TO RT ENGINE EDP. THE HOSE ASSY, PN AE70970110 WAS REMOVED AND REPLACED AND PERFORMED LEAK CHECK IAW AMM 29-11-05, NO LEAKS WERE FOUND. (K)
- [SDR ASM2008F00001](https://openairdocs.org/sdr/ASM2008F00001.md): Blade · bent · Aug 3, 2008 · N776AM · Boeing 7772Q8 · Turbine Engine Compressor Section
  > DURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIRST STAGE OF HIGH PRESSURE COMPRESSOR ROTABLE SECTION AND A IGV SCRATCHED IN THE RT ENG, OUT OF LIMITS IAW MM 72-00-00. THE RT ENG WAS REPLA

## 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 = 'N776AM' AND deregistration_id = 'N776AM-2017-04-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N776AM-2017-04-14/reports

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