# Service difficulty reports: N967AM

A list on [N967AM](https://openairdocs.org/aircraft/N967AM.md).

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

- [SDR M17F20230808104](https://openairdocs.org/sdr/M17F20230808104.md): Actuator · failed · Jul 16, 2023 · N967AM · Boeing 7878 · Drag Control Actuator
  > - FLAPS DRIVE - ROLL/YAW ASYMETRY - GND PROX SYS - GPWS FLAP OVRD - SPOILER- NO AUTO LAND - HYD SPOILERS SYS - ELEC SPOILERS SYS
- [SDR 2023F00045](https://openairdocs.org/sdr/2023F00045.md): Module · unserviceable · Jan 30, 2023 · N967AM · Boeing 7878 · Hydraulic Power System
  > MAINTENACE MSG OF FLIGHT CONTROL SYS (RUDDER, AILERON, ELEVATOR FLAP) AND HYD PRESS
- [SDR 2023F00095](https://openairdocs.org/sdr/2023F00095.md): Unknown · unknown · Jan 23, 2023 · N967AM · Boeing 7878 · Fuel Boost Pump
  > DURING STARTING THE MESSAGE "ENG FUEL SPAR VALVEL" APPEARS, THE ENGINE STARTS NORMAL
- [SDR 2022F00220](https://openairdocs.org/sdr/2022F00220.md): None · none · Mar 10, 2022 · N967AM · Boeing 737 · Landing Gear Brake System
  > ACTUADOR DE FRENOS 8 EN ESTATUS, FRM 324 143 08
- [SDR 2022F00215](https://openairdocs.org/sdr/2022F00215.md): None · none · Mar 10, 2022 · N967AM · Boeing 737 · Landing Gear Brake System
  > ACTUADOR DE FRENOS 8 EN ESTATUS FRM 324 143 08,
- [SDR 2022FA0000060](https://openairdocs.org/sdr/2022FA0000060.md): Slat · damaged · Jan 31, 2022 · N967AM · Boeing 7878 · Wing, Attach Fittings
  > DURING TRANSIT CHECK, IT WAS DETECTED THREE DENTS ON SLAT NUMBER 1 SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING 3 DENTS ON SLAT 1 WITH MULTIPLE DAMAGES ON LE FRONTAL AREA LOCALIZED BETWEEN STA 1151.75 AND STA 1160; A DENT AT STA 1152.75 WITH 1.7
- [SDR ASMF2021120800324](https://openairdocs.org/sdr/ASMF2021120800324.md): Skin · damaged · Nov 2, 2021 · N967AM · Boeing 7878 · Leading Edge Devices
  > THREE DENTS ON SLAT NUMBER 1 SKIN. DURING TRANSIT CHECK, IT WAS DETECTED THREE DENTS ON SLAT NUMBER 1 SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING 3 DENTS ON SLAT 1 WITH MULTIPLE DAMAGES ON LE FRONTAL AREA LOCALIZED BETWEEN STA 1151.75 AND STA 1
- [SDR ASMF202106007](https://openairdocs.org/sdr/ASMF202106007.md): Depressor · damaged · Mar 17, 2021 · N967AM · Boeing 7878 · Engine Thrust Reverser
  > DURING OVERNIGHT AND APPLICATION OF TASK CARD J8778-025-02-01(13) AT MEX, IT WAS DETECTED WORN WELDMENT ASSY ON BOTH SIDES OF RIGHT DEPRESSOR PYLON ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING WORN WELDMENT ASSY ON BOTH SIDES OF RIGHT DEPRESSO
- [SDR ASMF202101016](https://openairdocs.org/sdr/ASMF202101016.md): Acoustic Panel · dented · Dec 29, 2020 · N967AM · Boeing 7878 · Nacelle/Pylon, Plate/Skin
  > DURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED DENT ON LEFT T/R IFS INNER WALL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 1.125" DIAMETER, 0.021" DEPTH ON LEFT T/R IFS INNER WALL ACOUSTIC PANEL, AT LOWER BIFURCATIO
- [SDR ASMF20200603020](https://openairdocs.org/sdr/ASMF20200603020.md): Door · nicked · Mar 25, 2020 · N967AM · Boeing 7878 · Electrical/Electronic Compartment Doors
  > DURING TRANSIT CHECK, IT WAS DETECTED NICKS AT RT SIDE FWD ELECTRONICS EQUIPMENT ACCESS DOOR. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING FIVE NICKS, THREE NICKS WITH DIMENSIONS APPROXIMATELY OF 0.312" LENGTH AND 0.250" WIDE BETWEEN STA 305 & 307 AND TW
- [SDR ASMF2019061304](https://openairdocs.org/sdr/ASMF2019061304.md): Fan · failed · Apr 6, 2019 · N967AM · Boeing 7878 · Air Distribution Fan
  > DURING TRANSIT CHECK, IT WAS DETECTED EICAS MESSAGE LIQUID COOLING 21-81013. MAINTENANCE PERSONNEL PERFORMED A REVIEW TO COOLING SYSTEM, DETECTING THE LEFT POWER ELECTRONICS COOLING (PECS) FAILED; SO THE LEFT POWER ELECTRONICS COOLING WAS REPLACED IAW AMM DMC
- [SDR ASMF201901090006](https://openairdocs.org/sdr/ASMF201901090006.md): Warning Message · false activation · Oct 31, 2018 · N967AM · Boeing 7878 · Drag Control System
  > AIRCRAFT RETURNS TO PLATFORM DUE TO SPOILER LIGHT IN EICAS AND STATUS FLAP GROUND INHIBIT MESSAGE. MAINTENANCES PERSONNEL PERFORMED REVIEW, DETECTING FAILURE CODES 27-12303 AND 27-17752; SO THE FIM DMC-B787-A-27-60-F1-DMA-421A-A PROCEDURE WAS PERFORMED, NO CON
- [SDR ASMF2019010900003](https://openairdocs.org/sdr/ASMF2019010900003.md): Autothrottle Sys · malfunctioned · Oct 27, 2018 · N967AM · Boeing 7878 · Auto Throttle System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO AUTOTHROTTLES DID NOT ENGAGE. MAINTENANCE PERSONNEL PERFORMED AUTOTHROTTLE SYSTEM OPERATIONAL TEST IAW FIM DMC-B787-A-31-90-F8-01A-421B-A PROCEDURE, SHOWING FAILURE CODES 22-20060 AND 22-20050; SO THE FIM DMC-B787-A-31-90-F
- [SDR ASMF201809021](https://openairdocs.org/sdr/ASMF201809021.md): Not Reported · malfunctioned · Sep 19, 2018 · N967AM · Boeing 7878 · Trailing Flap Position Indicating System
  > AIRCRAFT RETURNED TO PLATFORM, DUE TO AFTER STARTS ENGINES THE FLAP/SLAT PRIMARY SYSTEM INDICATION WAS SHOWN WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED FLAP/SLAT PRIMARY SYSTEM TEST WAS IAW DMC-B787-A-27-51-00-01B-300B-A, TESTED SATISFACTORY.
- [SDR ASMF20180902718](https://openairdocs.org/sdr/ASMF20180902718.md): Battery Pack · failed · Sep 9, 2018 · N967AM · Boeing 7878 · Emergency Lighting
  > DURING TRANSIT CHECK, THE CENTER EMERGENCY LIGHTS ROWS 29 TO 33 TURNED OFF. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE BATTERY PACK FAILED; SO THE BATTERY PACK WAS REPLACED IAW AMM DMC-B787-A-33-51-07-02B-520A-A / 720A-A AND EMERGENCY LIGHT TEST WA
- [SDR ASMF20170202001](https://openairdocs.org/sdr/ASMF20170202001.md): Actuator · damaged · Jan 19, 2017 · N967AM · Boeing 7878 · Leading Edge Slat Actuator
  > CAPTAIN REPORTED THAT DURING APPROACH, THE MESSAGE IN EICAS AND STATUS SLAT DRIVE. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERFORMED THE FIM PROCEDURE IAW DMC-B787-A-27-80-F1-33A-421A-A, DETECTING GEAR ROTATORY ACTUATORS ON SLAT 11, LANYARD SKEW AND BL
- [SDR ASMF20161216004](https://openairdocs.org/sdr/ASMF20161216004.md): Seal · leaking · Oct 26, 2016 · N967AM · Boeing 7878 · Accessory Gearboxes
  > DURING OVERNIGHT CHECK AND THE EO 8772004 ISSUED TO REPLACE THE TRANSFER GEARBOX (TGB) ON BOTH ENGINES, MAINTENANCE PERSONNEL DETECTED OIL LEAK IN RIGHT TGB SLEEVE; SO THE RIGHT TGB SLEEVE SEALS WERE REPLACED IAW AMM DMC-B787-A-G72-01-00A-520A-A AND TEST 4 PAR
- [SDR ASMF20161216003](https://openairdocs.org/sdr/ASMF20161216003.md): Warning Light · illuminated · Oct 22, 2016 · N967AM · Boeing 7878 · Central Warning
  > AIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGINES, THE RIGHT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO CMCF IAW FIM DMC-B787-A-G13-20-F1-52A-421A-A, SHOWING FAILURE CODE 73-11152 AND DURING CHANGE OF THE CONFIGURATION TYPE
- [SDR ASMF201611002](https://openairdocs.org/sdr/ASMF201611002.md): Actuator · leaking · Aug 21, 2016 · N967AM · Boeing 7878 · Landing Gear Door Actuator
  > DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. FOUND TO BE OUT OF LIMITS IAW A-A-29-11-00-00C-364-A. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RIGHT MAIN LANDING GEAR RETRACT AC
- [SDR ASMF201610011](https://openairdocs.org/sdr/ASMF201610011.md): Actuator · leaking · Aug 21, 2016 · N967AM · Boeing 7878 · Hydraulic System, Main
  > DURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR OUT OF LIMIT IAW DMC B787A-A-29-11-00-00C-364-A. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RIGHT MAIN LANDING GEAR RETRACT ACTUA
- [SDR ASMF201510012](https://openairdocs.org/sdr/ASMF201510012.md): Actuator · failed · Aug 27, 2015 · N967AM · Boeing 7878 · Stabilizer Position Indicating
  > DURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE HORIZONTAL STABILIZER TRIM ACTUATOR. ACFT WAS SENT TO THE HANGAR. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR IAW DMC-B787-A-27-41-07-00B-520A-A, TESTED CORRECT.
- [SDR ASMF201510007](https://openairdocs.org/sdr/ASMF201510007.md): Heat Exchanger · failed · Aug 21, 2015 · N967AM · Boeing 7878 · Cabin Cooling System
  > DURING TRANSIT CHECK, IT WAS DETECTED A FLUID LEAK IN THE AFT GALLEY. THE AFT GALLEY WAS CLEANED. PERFORMED REVISION & CLEANING IAW AMM DMC-B7878-A-12-25-01-02A-258A-A, NO CONFIRMING FLUID LEAK. AS PRECAUTIONARY ACTION, THE AFT GALLEY WAS DEFERRED IAW MEL 2
- [SDR ASMF201408001](https://openairdocs.org/sdr/ASMF201408001.md): Ram Air Turb · deployed · Jul 18, 2014 · N967AM · Boeing 7878 · Hydraulic System, Auxiliary
  > AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE EICAS MESSAGE RAT EXTEND & RAT UNLOCKED LIGHT TURNED ON, WITH THE LANDING GEAR LEVER IN UP POSITION. DURING MAINTENANCE REVISION, THE RAM AIR TURBINE WAS FOUND EXTENDED. ACFT WAS SENT TO THE HANGAR & THE N
- [SDR ASMF201407002](https://openairdocs.org/sdr/ASMF201407002.md): Warning System · false activation · Jun 8, 2014 · N967AM · Boeing 7878 · Central Warning
  > CAPTAIN REPORTED THAT DURING APPROACH, THE AHM EICAS MSG OF OVERSPEED WAS REACHED WITH MORE 15 KNOTS. PERFORMED FLAP & SLAT DOWN OVERSPEED OR ABOVE 20,000 FEET CONDITION INSPECTION IAW AMM DMC-B787-A-05-51-08-00B-280B-A, PHASE I, NO DAMAGES WERE FOUND.

## 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 = 'N967AM' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N967AM/reports

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