# Service difficulty reports: N788XA

A list on [N788XA](https://openairdocs.org/aircraft/N788XA.md).

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

- [SDR ASMF202011241011](https://openairdocs.org/sdr/ASMF202011241011.md): Acoustic Panel · damaged · Sep 29, 2020 · N788XA · Boeing 737752 · Nacelle/Pylon, Main Frame
  > DURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL DENTS AND NICKS ON BOTH ENGINES INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.001" DEPTH AND 0.187" WIDTH; A DENT OF 0.002" DEPTH AND
- [SDR ASMF202011001](https://openairdocs.org/sdr/ASMF202011001.md): Pump · leaking · Sep 10, 2020 · N788XA · Boeing 737752 · Hydraulic Pump (Electric/Engine), Main
  > DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED ON RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT EDP PUMP OUT OF LIMITS, SO THE RIGHT ENGINE EDP PUMP WAS REPLACED, IAW AMM 29-11-11 AND AMM TASK 29-00-00-870-801. OPERA
- [SDR ASMF2019061307](https://openairdocs.org/sdr/ASMF2019061307.md): Bulkhead Web · damaged · Apr 13, 2019 · N788XA · Boeing 737732 · Fuselage Main, Bulkhead
  > DURING OVERNIGHT CHECK, IT WAS DETECTED PRESSURIZATION LEAK IN THE NETWORK AREA OF REAR SPAR VERTICAL PRESSURE STA 663 LBL35 AND RBL35 ON DRAIN VALVE HOUSING BOTH SIDES; MAINTENANCE PERSSONNEL ISSUED THE WO 5367805 TO PERFORM WORKS; THE VALVE HOUSING BOTH SIDE
- [SDR ASMF2019042302](https://openairdocs.org/sdr/ASMF2019042302.md): Motor · failed · Jan 18, 2019 · N788XA · Boeing 737752 · Stabilizer Position Indicating
  > DURING TRANSIT CHECK, IT WAS DETECTED THE STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE STAB TRIM MOTOR DAMAGED; SO THE STAB TRIM MOTOR WAS REPLACED IAW AMM 27-41-71 AND THE FIM 22-11 TASK 801 PROCEDURE WAS PERFORMED,
- [SDR ASMF20190109007](https://openairdocs.org/sdr/ASMF20190109007.md): Extinguisher · activated · Nov 9, 2018 · N788XA · Boeing 737752 · Fire Bottle, Fixed
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING PUSH BACK, CAPTAIN REPORTED BELL SOUNDS OF FIRE IN FWD CARGO COMPARTMENT; SO THE FLIGHT CREW PERFORMED THE QRH 8.15 AND 8.16 PROCEDURES; AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED REVISION AT
- [SDR ASMF20180918009](https://openairdocs.org/sdr/ASMF20180918009.md): Windshield · scratched · Aug 1, 2018 · N788XA · Boeing 737752 · Flight Compartment Windows
  > DURING TRANSIT CHECK, THE LEFT WINDOW NUMBER 1 WAS DETECTED WITH SCRATCHES AND VISION DECREASED. AIRCRAFT WAS SENT TO THE HANGAR, MAINTENANCE PERSONNEL REPLACED THE LEFT WINDOW NUMBER 1 IAW AMM 56-11-11, TESTED CORRECT.
- [SDR ASMF20180918008](https://openairdocs.org/sdr/ASMF20180918008.md): Shutoff Valve · malfunctioned · Jul 30, 2018 · N788XA · Boeing 737752 · Fuel Selector/Shut-Off Valve
  > DURING FUELING, A FUEL SPILLAGE IN THE RIGHT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN AND MAINTENANCE PERSONNEL. CLEANED THE SELECTOR AND THE SHUTOFF VALVE WAS RESEATED AND TESTED SEVERAL TIMES IAW MM 28-21-00,
- [SDR ASMF20180828010](https://openairdocs.org/sdr/ASMF20180828010.md): Antenna · damaged · Jun 30, 2018 · N788XA · Boeing 737752 · Air Collision Avoidance System
  > CAPTAIN REPORTED THE TCAS FAIL FLAG ON THE NAVIGATION DISPLAY, FRM 344 370 00. MAINTENANCE PERFORMED A FAULT ISOLATION PROCEDURE IAW FIM 34-45, TASK 821 AND TCAS TOP ANTENNA WAS REPLACED IAW AMM 34-45-02, TESTED CORRECT.
- [SDR ASMF201801012](https://openairdocs.org/sdr/ASMF201801012.md): Starter · leaking · Dec 28, 2017 · N788XA · Boeing 737752 · Engine Starter
  > CAPTAIN REPORTED THAT DURING CRUISE, A LEFT ENGINE MECHANICAL MESSAGE WITH OIL INDICATION OF 1 QUART AND TEMPERATURE AND PRESSURE NORMAL. MAINTENANCE PERFORMED AN INSPECTION IN THE LEFT ENGINE IAW AMM 71-00-00. FOUND OIL LEAKING IN THE LEFT ENGINE STARTER A
- [SDR ASMF201702005](https://openairdocs.org/sdr/ASMF201702005.md): Pcu · failed · Jan 12, 2017 · N788XA · Boeing 737752 · Engine Thrust Reverser
  > AIRCRAFT RETURNED TO PLATFORM AFTER START OF ENGINES, THE THRUST REVERSER UNIT LIGHT TURNED ON. PERFORMED BITE TO SPCU MODULE IAW FIM 24-31 TASK 801 PROCEDURE, CONFIRMING THE FAILURE. THE SPCU MODULE WAS REPLACED IAW AMM 24-34-11, TESTED CORRECT.
- [SDR ASMF201612002](https://openairdocs.org/sdr/ASMF201612002.md): Warning Light · illuminated · Oct 19, 2016 · N788XA · Boeing 737752 · Cabin Temperature Control System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO HIGH PASSENGER CABIN TEMPERATURE WITHOUT LIGHT INDICATION. MAINTENANCE PERSONNEL PERFORMED THE FIM 21-61 TASK 801 PROCEDURE, NO CONFIRMING FAILURE.
- [SDR ASMF201610008](https://openairdocs.org/sdr/ASMF201610008.md): Pulley · stuck · Aug 14, 2016 · N788XA · Boeing 737752 · Drag Control Actuator
  > AIRCRAFT RETURNED TO PLATFORM DURING FLIGHT CONTROL CHECK, THE LEFT FLIGHT SPOILER WAS DEPLOYED PARTIALLY AFTER BOTH ENGINES START. MAINTENANCE PERSONNEL CHECKED LEFT SPOILER CONTROL SYSTEM, CABLE GUARDS, CONTROL CABLE PULLEYS AND BRACKETS IAW AMM 27-61-00/601
- [SDR ASMF201610006](https://openairdocs.org/sdr/ASMF201610006.md): Speed Brake · out of alignment · Aug 9, 2016 · N788XA · Boeing 737752 · Drag Control System
  > DURING TRANSIT CHECK, THE LEFT WING SPEED BRAKE DOOR NUMBERS 3, 4 AND 5 WERE OUT OF ALIGNMENT. MAINTENANCE PERSONNEL PERFORMED THE SPOILERS CONTROL SYSTEM CABLE LUBRICATING AND SPEED BRAKE CONTROL SYSTEM OPERATIONAL TEST IAW AMM 12-26-00 AND AMM 27-62-00, ALL
- [SDR ASMF2016072600011](https://openairdocs.org/sdr/ASMF2016072600011.md): Engine · leaking · May 29, 2016 · N788XA · Boeing 737752 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED THAT DURING LANDING, THE LEFT ENGINE OIL INDICATION LIGHT TURNED ON AND 9 QTS WAS SHOWN. MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE LEAK CHECK IAW AMM 71-71-00, NO DETECTING ANY EXTERIOR OIL LEAK; SO THE LEFT ENGINE WAS OIL SERVICED TO FULL A
- [SDR ASMF2016072600010](https://openairdocs.org/sdr/ASMF2016072600010.md): Gasket · leaking · May 28, 2016 · N788XA · Boeing 737752 · Turbine Section
  > CAPTAIN REPORTED THAT DURING DESCENT, THE LEFT ENGINE OIL INDICATION LIGHT TURNED ON AND 3 QTS WAS SHOWN. MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE LEAK CHECK IAW AMM 71-00-00-700-823, TESTS 3A AND 3B, DETECTING OIL LEAK IN INTERFACE TRF DISCHARGE TURBINE; S
- [SDR ASMF2016072600005](https://openairdocs.org/sdr/ASMF2016072600005.md): Gasket · leaking · May 18, 2016 · N788XA · Boeing 737752 · Engine (Turbine/Turboprop)
  > DURING TRANSIT CHECK, IT WAS DETECTED AN OIL LEAK IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED ENGINE LEAKING INSPECTION IAW AMM 71-00-00 DETECTING AN OIL LEAK ON AFT SUMP ROTATING SEAL, CCM ENGINE ENGINEER EVALUATED THE OIL LEAK AND FOUND IT WITHIN OPE
- [SDR ASMF201605002](https://openairdocs.org/sdr/ASMF201605002.md): Skin · damaged · Feb 27, 2016 · N788XA · Boeing 737752 · Elevator, Plate/Skin
  > PERFORMED A LIGHTNING STRIKE INSPECTION IAW AMM 05-51-19, DETECTING A LIGHTNING STRIKE WITH DELAMINATION OF 3.5” LONG & 1.5” WIDE IN THE RT ELEVATOR TE. LIGHTNING STRIKE ON 3 FASTENERS IN THE RT ELEVATOR TE, ON RT ENG EXTERIOR THRUST REVERSER TE & ON 2 RT WIN
- [SDR ASMF201511005](https://openairdocs.org/sdr/ASMF201511005.md): Unknown · vibration · Nov 3, 2015 · N788XA · Boeing 737752 · Engine Ignition Analyzer
  > CAPTAIN REPORTED THAT DURING CLIMB, THE LT ENG VIBRATION REACHED 4.2 UNITS. PERFORMED FIM 71-05 TASK 808 PROCEDURE, NO DAMAGES WERE FOUND, TESTED CORRECT. AS PRECAUTIONARY ACTION, REPLACED THE VIBRATION MONITOR IAW AMM 77-31-03-401 & TRIM BALANCE WAS PERFORM
- [SDR ASMF201509010](https://openairdocs.org/sdr/ASMF201509010.md): Receiver · damaged · Aug 1, 2015 · N788XA · Boeing 737752 · Audio Integrating System
  > DURING TRANSIT CHECK, IT WAS DETECTED A LIGHTNING STRIKE IN THE VOR ANTENNA NR 1. PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19, DETECTING THE REMOTE ELEC UNIT NR 1 DAMAGED, REPLACED IAW AMM 23-51-01, TESTED CORRECT.
- [SDR ASMF201506002](https://openairdocs.org/sdr/ASMF201506002.md): Gcu · failed · Apr 20, 2015 · N788XA · Boeing 737752 · AC Regulator
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO SOURCE OFF, GEN OFF & BUS ON LIGHTS TURNED ON. THE FLIGHT CREW ACCOMPLISHED THE QRH 6.4 PROCEDURE & APU WAS NOT STARTED, CONFIRMING THE FAILURE. PERSONNEL REVISION DETECTING LT IDG FAILED, SO THE LT IDG WAS DE
- [SDR ASMF201503001](https://openairdocs.org/sdr/ASMF201503001.md): Blade · damaged · Jan 7, 2015 · N788XA · Boeing 737752 · Turbine Engine Compressor Section
  > DURING OVERNIGHT CHECK, IT WAS DETECTED IN THE RT ENG A MISSING MATERIAL AT FAN BLADE ABRADABLE SHROUD & DISTORTION AT FAN BLADE LE. PERFORMED REVISION DETECTING A MISSING MATERIAL AT RT ENG FAN BLADE OF 1.0 INCH LENGTH, 0.200 INCH DEPTH, 0.500 INCH WIDE, SO
- [SDR ASMF201501005](https://openairdocs.org/sdr/ASMF201501005.md): Shutoff Valve · failed · Oct 10, 2014 · N788XA · Boeing 737752 · Pneumatic Distribution System
  > AIRCRAFT REJECTED TAKE OFF AT 50 KNOTS, DUE TO BLEED TRIP OFF LIGHT TURNED ON. DEFERRED THE LT ENG PRSOV IAW MEL 36-5-2 CAT C. THE LT ENG PRSOV WAS REPLACED IAW AMM 36-11-04 & HIGH STAGE VLV OF THE LT ENG WAS REPLACED IAW AMM 36-11-06. TESTED CORRECT & THE
- [SDR ASMF2014061706003](https://openairdocs.org/sdr/ASMF2014061706003.md): Blade · lack of lube · Apr 11, 2014 · N788XA · Boeing 737752 · Turbine Engine Compressor Section
  > CAPTAIN REPORTED THAT DURING CRUISE, BOTH ENGS VIBRATION REACHED 3.2 & 3.6 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED LUBRICATION OF THE FAN ROTOR BLADE OF THE RT ENG IAW AMM 72-21-00 & FAN TRIM BALANCE TEST 14B IAW AMM 71-00-00, BEING WITHIN LIMITS.
- [SDR ASMF201403017](https://openairdocs.org/sdr/ASMF201403017.md): Starter · damaged · Mar 14, 2014 · N788XA · Boeing 737752 · Engine Starter
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START SMOKE WAS DETECTED IN THE RT ENG. PERFORMED RT ENGINE LEAKING INSPECTION IAW MM 72-00-00 DETECTING THE STARTER DAMAGED, SO THE RT STARTER WAS REPLACED IAW MM 80-11-01, TESTED CORRECT.
- [SDR ASMF201403014](https://openairdocs.org/sdr/ASMF201403014.md): Unknown · leaking · Mar 10, 2014 · N788XA · Boeing 737752 · Engine Fuel and Control
  > DURING RT ENGINE START, A FUEL LEAK WAS DETECTED & THE RT ENGINE CONTROL LIGHT TURNED ON WITH INDICATION OF EGT LOW. AIRCRAFT RETURNED TO PLATFORM. PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE DRAIN PORT. THE RT ENGINE WAS MOTORING, A
- [SDR ASMF201402008](https://openairdocs.org/sdr/ASMF201402008.md): Door · open · Jan 13, 2014 · N788XA · Boeing 737752 · Potable Water System
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MID DUE TO DURING CRUISE THERE WAS NO POTABLE WATER IN GALLEY OR LAVATORIES & THE INSTRUMENT INDICATED 3 /4 FULL. DURING MX REVISION, THE WATER TANK ACCESS DOOR PANEL NR 146ARY WAS DETECTED OPENED. SO THE PANEL WA
- [SDR ASMF201309002](https://openairdocs.org/sdr/ASMF201309002.md): Pump · leaking · Aug 14, 2013 · N788XA · Boeing 737752 · Engine Fuel Pump
  > DURING OVERNIGHT CHECK, MX PERSONNEL ATTENDED THE NRC A0732762 TO CORRECT FUEL LEAK IN RT ENGINE OF 40 DROPS IAW MINUTE THROUGH THE FUEL PUMP PAD DRAIN DURING IDLE POWER OPERATION. RT ENGINE FUEL PUMP WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT.
- [SDR ASMF201308013](https://openairdocs.org/sdr/ASMF201308013.md): Lubrication Unit · leaking · Jul 18, 2013 · N788XA · Boeing 737752 · Engine Oil Cooler
  > DURING TRANSIT CHECK, AN OIL LEAK DETECTED ON RT ENGINE. MX PERSONNEL PERFORMED ENGINE LEAKING INSPECTION IAW MM 73-21-00 OIL LEAK ON THE LUBRICATION UNIT. REPLACED IAW MM 79-21-01 AND RT ENGINE WAS RAN IAW MM 71-00-00, TEST 3A, ALL CORRECT.
- [SDR ASMF201308009](https://openairdocs.org/sdr/ASMF201308009.md): Rudder Pedal · out of adjust · Jul 14, 2013 · N788XA · Boeing 737752 · Rudder Tab Control System
  > DURING TRANSIT CHECK, CAPTAIN REPORTED THE RUDDER PEDALS OUT OF SERVICE. DURING MX REVISION, THE MECHANISM AND OPERATION WAS FOUND WITHIN LIMIT OF HIS SCROLL AND JOINED. MECHANISM WAS ADJUSTED AND DETACHED IAW MM 27-21-41, TESTED CORRECT.
- [SDR ASMF20130523003](https://openairdocs.org/sdr/ASMF20130523003.md): O-Ring · leaking · Apr 24, 2013 · N788XA · Boeing 737752 · Turbine Engine Oil System
  > DURING TRANSIT CHECK, DETECTED AN OIL LEAK IN THE RT ENGINE. MX PERSONNEL PERFORMED ENGINE LEAKING INSPECTION IAW AMM 73-21-00, DETECTING OIL LEAK IN THE DIFFERENTIAL PRESSURE SWITCH, SO THE O-RINGS WERE REPLACED IAW AMM 79-21-07, TESTED CORRECT.
- [SDR ASMF201301005](https://openairdocs.org/sdr/ASMF201301005.md): Line · damaged · Jan 6, 2013 · N788XA · Boeing 737752 · Hydraulic System, Main
  > DURING TRANSIT CHECK, DETECTED A HYD LEAK IN THE RT MLG. MX PERSONNEL PERFORMED REVISION DETECTING THE HYD LINE DAMAGED; SO THE HYD LINE WAS REPLACED IAW MM 29-00-00, TESTED CORRECT.
- [SDR ASMF201212015](https://openairdocs.org/sdr/ASMF201212015.md): Seal · leaking · Dec 30, 2012 · N788XA · Boeing 737752 · Nose/Tail Landing Gear Strut/Axle
  > CAPTAIN REPORTED THAT DURING LANDING, A STRONG NOISE IN CREW CABIN, WAS LISTENING WHEN LOWERED THE LANDING GEAR. MX REPLACED THE ACTIVE SEALS AND PERFORMED SERVICE, A NLG SHOCK STRUT IAW MM 12-15-41 AND MM 32-21-11, TESTED CORRECT.
- [SDR ASMF201202001](https://openairdocs.org/sdr/ASMF201202001.md): Skin · damaged · Jan 28, 2012 · N788XA · Boeing 737752 · Fuselage Main, Plate/Skin
  > DURING TRANSIT CHECK, FOUND A 2 INCH CRACK AND A.750 INCH HOLE ON FUSELAGE SKIN AT BS 308, AND STRINGER 22R WITH DEFORMATION. SKIN AND STRINGER REPAIRED IAW AMX-AMX-12-0033-3B, SRM 53-00-01 AND NDT INSPECTION WERE PERFORMED, NO CRACKS WERE FOUND IAW NDTM PA
- [SDR ASMF201112005](https://openairdocs.org/sdr/ASMF201112005.md): Skin · damaged · Dec 9, 2011 · N788XA · Boeing 737752 · Leading Edge Devices
  > DURING TRANSIT CHECK, MX DETECTED A ONE INCH HOLE IN FLEX SKIN OF SLAT NR 8, IT WAS CONFIRMED THAT HOLE WAS WITHIN LIMITS IAW SRM 57-42-01, AND WAS TEMPORARY COVERED WITH ALUMINUM FOIL TAPE IAW SRM 57-42-01 PAGES 103 AND 110. SLAT NR 8 WAS REPLACED IAW MM 27-
- [SDR ASMF201105005](https://openairdocs.org/sdr/ASMF201105005.md): Structure · dented · May 7, 2011 · N788XA · Boeing 737752 · Horizontal Stabilizer Structure
  > DURING TRANSIT CHECK A BIRD STRIKE WAS ON THE RT WINDSHIELD AND RT HORIZONTAL STABILIZER L/E. MX PERSONNEL PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING A DENT OF 20.0 X 6.0 INCHES, WITH 1.125 INCH BETWEEN STA 81.5 TO 101.5; IT WAS CONFIRMED THAT DENT W
- [SDR ASMF201101001](https://openairdocs.org/sdr/ASMF201101001.md): Control Cable · out of adjust · Dec 26, 2010 · N788XA · Boeing 737752 · Rudder Control System
  > CAPTAIN REPORTED THAT DURING CRUISE, ACFT REQUIRED 10 UNITS OF RT OF RUDDER AND AILERON COMPENSATOR TO MAINTAIN STRAIGHT AND LEVELED FLIGHT. ACFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK MX ADJUSTED THE RUDDER AND AILERON CONTROL CABLES IAW MM 27-21-
- [SDR ASMF201012006](https://openairdocs.org/sdr/ASMF201012006.md): Filter · obstructed · Dec 4, 2010 · N788XA · Boeing 737705 · Turbine Engine Oil System
  > ACFT RETURNED TO PLATFORM DUE TO AFTER ENGINES WERE STARTED, THE RT ENGINE "OIL FILTER BY PASS" LIGHT TURNED ON. MX PERSONNEL PERFORMED THE FIM 73-05, TASK 801CONFIRMING THE FAILURE; SO RT ENGINE FILTER AND ALARM WERE REPLACED THE IAW MM 73-11-02 AND MM 73-34
- [SDR ASMF20101002](https://openairdocs.org/sdr/ASMF20101002.md): Access Panel · cracked · Oct 2, 2010 · N788XA · Boeing 737752 · Elevator Control System
  > DURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN RT WING MAIN TANK DUE TO A CRACK AT DRIP STICK NR 4 OF THE FUEL TANK ACCESS DOOR PANEL NR 632FB. MX PERFORMED FUEL LEAK INSP DETECTING FUEL LEAK IN LIMITS IAW MM 28-11-00 PAGE 604. AT MEX, THE FUEL TANK ACCES
- [SDR ASMF201005001](https://openairdocs.org/sdr/ASMF201005001.md): Shroud · grooved · May 14, 2010 · N788XA · Boeing 737705 · Turbine Engine Compressor Section
  > DURING THE MX INSP, AFTER THE LAST FLIGHT OF THE DAY, IT WAS DETECTED IN THE LT ENGINE, THE FAN BLADES WITH PLASTIC BAG REMAIN. MX PERFORMED A FOD INSP IAW MM TASK 71-00-00-800-802-F00, DETECTING A GROOVE 1.125 INCHES WIDE ON 360 DEGREES OF ABRADABLE SHROUD. T

## 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 = 'N788XA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N788XA/reports

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