# Service difficulty reports: N342AM, cancelled Jul 18, 2023

A list on [N342AM, cancelled Jul 18, 2023](https://openairdocs.org/deregistered/N342AM-2023-07-18.md).

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

- [SDR ASMF2021120700315](https://openairdocs.org/sdr/ASMF2021120700315.md): Transmitter · failed · Oct 13, 2021 · N342AM · Boeing 7378Z9 · Aileron Control System
  > AILERONS FLIGHT CONTROL TEST WITH RIGHT MOVEMENT SLOWER. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING AILERONS FLIGHT CONTROL TEST WITH RIGHT MOVEMENT SLOWER. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING BITE TO PSEU IAW FIM 27-11 TASK 8081 PROCEDURE, NO
- [SDR ASMF20211026025](https://openairdocs.org/sdr/ASMF20211026025.md): Transmitter · failed · Oct 13, 2021 · N342AM · Boeing 7378Z9 · Aileron Control System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING AILERONS FLIGHT CONTROL TEST WITH RIGHT MOVEMENT SLOWER. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING BITE TO PSEU IAW FIM 27-11 TASK 8081 PROCEDURE, NO CONFIRMING FAILURE; AS A PRECAUTIONARY ACTION; THE FLAPS
- [SDR ASMF202106015](https://openairdocs.org/sdr/ASMF202106015.md): Control Cable · out of adjust · May 25, 2021 · N342AM · Boeing 7378Z9 · Aileron Control System
  > DURING TRANSIT CHECK, IT WAS DETECTED THE FLIGHT CONTROL TEST WITH SLOW RESPONSE OF AILERON MOVING RIGHT TO NEUTRAL. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING SLOW AILERON RESPONSE; SO THE SLOW AILERON RESPONSE TO CONTROL WHEEL INPUT WITH HYDRAULIC P
- [SDR 2021F00162](https://openairdocs.org/sdr/2021F00162.md): Aileron Sys · lack of lube · May 25, 2021 · N342AM · Boeing 7378Z9 · Aileron Control System
  > 26.05.2021 18:43 DURING TRANSIT CHECK THE FLIGHT CONTROL TEST SLOW DURING TRANSIT CHECK, IT WAS DETECTED THE FLIGHT CONTROL TEST WITH SLOW RESPONSE OF AILERON MOVING RIGHT TO NEUTRAL. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING SLOW AILERON RESPONSE; S
- [SDR ASMF202101021](https://openairdocs.org/sdr/ASMF202101021.md): Structure · cracked · Jan 16, 2021 · N342AM · Boeing 7378Z9 · Engine Thrust Reverser
  > DURING 8A-P CHECK IN TASK CARD J3770-818-02-01 (21) AT MEX STATION, IT WAS DETECTED SEVERAL CRACKS AT RIGHT ENGINE INNER THRUST REVERSER. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A CRACK ON UPPER FIREWALL STA 247.40 AND WL 100; A CRACK ON UPPER F
- [SDR ASMF202011013](https://openairdocs.org/sdr/ASMF202011013.md): Acoustic Panel · dented · Sep 30, 2020 · N342AM · Boeing 7378Z9 · Nacelle/Pylon, Main Frame
  > DURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL DENTS AND A NICK ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A SEVERAL DENTS WITH 2.875" AND 1.500"OF SEPARATION; A DENT OF 0.500
- [SDR ASMF202011007](https://openairdocs.org/sdr/ASMF202011007.md): Switch · failed · Sep 23, 2020 · N342AM · Boeing 7378Z9 · Drag Control System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXIING, WHEN PRESS TOGA FOR TAKEOFF SOUNDS THE ALARM OF TAKEOFF CONFIGURE WITH FLAPS 1 AND STAB TRIM 6.1. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU, IAW FIM 32-09 TASK 801 PROCEDURE AND FIM 27-62 TASK 808 PROCED
- [SDR ASMF202011005](https://openairdocs.org/sdr/ASMF202011005.md): Packing · damaged · Sep 21, 2020 · N342AM · Boeing 7378Z9 · Hydraulic System, Main
  > DURING TRANSIT CHECK, A HYDRAULIC LEAKAGE WAS DETECTED ON FLAP CONTROL VALVE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING PACKING´S OF HYDRAULIC LINES OF FLAP CONTROL VALVE WITH LEAKAGE. SO THE PACKING´S OF HYDRAULIC LINES P/N NAS1612-8A, MANUFACTURE
- [SDR ASMF20200603022](https://openairdocs.org/sdr/ASMF20200603022.md): Skin · damaged · Mar 23, 2020 · N342AM · Boeing 7378Z9 · Trailing Edge Flaps
  > DURING TRANSIT CHECK, IT WAS DETECTED A DISBONDED AND ERODED OF LT OUTBOARD AFTER FLAP. MAINTENANCE PERSONNEL PERFORMED REVISION TO DISBONDED AND ERODED 2 AT UPPER AND LOWER SKIN ON TRAILING EDGE INBOARD CORNER OF LT OUTBOARD AFTER FLAP, FROM OTEF STA 88.2 TO
- [SDR ASMF20190712004](https://openairdocs.org/sdr/ASMF20190712004.md): Window · cracked · Jul 3, 2019 · N342AM · Boeing 7378Z9 · Flight Compartment Windows
  > AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF THE RT WINDOW NR 2 WAS CRACKED FRM 56102042; SO MAINTENANCE PERSONNEL REPLACED THE RT WINDOW P/N: 141A4810-39, S/N: 01269H9011 NR 2 IAW AMM56-12-11-400-801; IT WAS PERFORMED CABIN PRESSURE LEAK TEST IAW AMM 05-51
- [SDR ASMF2019042320](https://openairdocs.org/sdr/ASMF2019042320.md): Idg · failed · Mar 16, 2019 · N342AM · Boeing 737800* · AC Generator-Alternator
  > AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MID DUE TO DURING CRUISE, THE APU SHUTDOWN AND RIGHT IDG WAS PREVIOUS DEFERRED. MAINTENANCE PERSONNEL PERFORMED REVIEW TO SYSTEM, DETECTING APU LOW OIL PRESSURE LIGHT TURNED ON WITH LIGHTEN AND APU WAS HAD PROTECTIV
- [SDR ASMF2019042318](https://openairdocs.org/sdr/ASMF2019042318.md): Line · leaking · Mar 8, 2019 · N342AM · Boeing 737800* · Hydraulic System, Main
  > DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT HYDRAULIC SYSTEM B IN PLUG OF RETURN FILTER MODULE; SO THE RETURN FILTER MODULE PLUG P
- [SDR ASMF20190109010](https://openairdocs.org/sdr/ASMF20190109010.md): Mount · failed · Nov 20, 2018 · N342AM · Boeing 737800* · Weather Radar System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE EICAS MESSAGE WXR FAIL WAS SHOWN; MAINTENANCE PERSONNEL PERFORMED INSPECTION DETECTING MBA 4A MOUNTING TRAY FAILED IAW AMM 34-42; SO THE WEATHER RADAR R/T MOUNT WAS REPLACED P/N: 2041213-0413 S/N: MBA4A-0
- [SDR ASMF20190109005](https://openairdocs.org/sdr/ASMF20190109005.md): Warning System · false activation · Oct 29, 2018 · N342AM · Boeing 737800* · Central Warning
  > AIRCRAFT RETURN TO PLATFORM DUE TO BEFORE TO TAKEOFF, THE TAKEOFF CONFIGURATION ALARM AND LIGHT, PSEU LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO PSEU IAW AMM 31-51-00, SHOWING MESSAGES AND FAILURE CODES STAB TRM NOT GRN, STAB TRM GREEN AND TAKEOF
- [SDR ASMF20180902717](https://openairdocs.org/sdr/ASMF20180902717.md): Seal · leaking · Sep 7, 2018 · N342AM · Boeing 737800* · Turbine Engine Oil System
  > DURING OVERNIGHT CHECK, IT WAS DETECTED AN OIL LEAK IN THE LH ENGINE. MAINTENANCE PERSONNEL PERFORMED ENGINE 3A IDLE-POWER LEAKING TEST, DETECTING AN OIL LEAK ON N2 PAD DRAIN SEAL OF 60 DROPS PER MINUTE, BEING OUT OF LIMITS IAW AMM 71-71-00; SO THE MAGNETIC SE
- [SDR ASMF201803002](https://openairdocs.org/sdr/ASMF201803002.md): Shutoff Valve · leaking · Mar 8, 2018 · N342AM · Boeing 737800* · Pneumatic Distribution System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DUCT PRESSURE LOW INDICATION IN THE RIGHT ENGINE, SHOWING 18 PSI. MAINTENANCE PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE RIGHT ENGINE PRSOV. THE RIGHT ENGINE PRSOV AND THE RIGHT ENGINE BLEED AIR REG
- [SDR ASMF201704010](https://openairdocs.org/sdr/ASMF201704010.md): Connector · loose · Apr 12, 2017 · N342AM · Boeing 737800* · Flight Control System Wiring
  > DURING TRANSIT CHECK, IT WAS DETECTED THE STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE CONNECTOR D381 LOOSE, THEREFORE THE CONNECTOR WAS TIGHTENED IAW AMM 27-41-00,TESTED CORRECT. AS A PRECAUTIONARY ACTION, THE STAB
- [SDR ASMF201700301003](https://openairdocs.org/sdr/ASMF201700301003.md): Slide · out of limits · Feb 4, 2017 · N342AM · Boeing 737800* · Escape Slide
  > DURING THE TRANSIT CHECK, THE ESCAPE SLIDE PACK FROM FWD ENTRY DOOR WAS FOUND OUT OF RANGE OF PRESSURE. MAINTENANCE PERSONNEL REPLACED THE ESCAPE SLIDE PACK IAW AMM 25-65-01, TESTED CORRECT.
- [SDR ASMF201612015](https://openairdocs.org/sdr/ASMF201612015.md): B-Nut · loose · Dec 4, 2016 · N342AM · Boeing 737800* · Hydraulic System, Main
  > DURING TRANSIT CHECK, DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR WW. MAINTENANCE PERFORMED FOUND THE HYDRAULIC LEAK IN THE HYDRAULIC SYSTEM B OF THE ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE NUT. THE HYDRAULIC PRESSURE LINE WAS TIGHTENED IAW A
- [SDR ASMF201612011](https://openairdocs.org/sdr/ASMF201612011.md): Shutoff Valve · malfunctioned · Nov 16, 2016 · N342AM · Boeing 737800* · Fuel Storage
  > DURING FUELING, A FUEL SPILLAGE IN THE LEFT TANK WAS DETECTED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN AND MAINTENANCE PERSONNEL CLOSED THE VALVE MANUALLY AND THE REFUELING SHUTOFF VALVE WAS DEFERRED BY MEL 28-10-2 CAT C. AT
- [SDR ASMF201611005](https://openairdocs.org/sdr/ASMF201611005.md): Pump · failed · Aug 27, 2016 · N342AM · Boeing 737800* · Engine Fuel Pump
  > AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAF
- [SDR ASMF201610014](https://openairdocs.org/sdr/ASMF201610014.md): Pump · failed · Aug 27, 2016 · N342AM · Boeing 737800* · Engine Fuel Pump
  > AIRCRAFT RETURNED DURING CLIMB AT FL 170´, THE LEFT ENGINE EXPERIENCED THRUST DETERIORATION AT A SHOW RATE, THE LEFT ENGINE THRUST LEVER WAS ADVANCED TO THE FULL THRUST POSITION WITHIN INDICATION OF THRUST INCREASING AT ALL PARAMETERS. AIRCRAFT WAS SENT TO TH
- [SDR ASMF2016072600014](https://openairdocs.org/sdr/ASMF2016072600014.md): Actuator · failed · Jun 5, 2016 · N342AM · Boeing 737800* · Engine Fuel Distribution
  > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINES START, THE LEFT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO LEFT EEC IAW FIM 73-10 TASK 801 PROCEDURE, SHOWING THE MESSAGES L REVERSER SLEEVE POSITION SIGNAL OUT OF RANGE; SO THE L
- [SDR ASMF2015030400001](https://openairdocs.org/sdr/ASMF2015030400001.md): Relay · failed · Feb 1, 2015 · N342AM · Boeing 737800* · Emergency Exits
  > AIRCRAFT REJECTED TAKE OFF AT 80 KNOTS DUE TO MASTER CAUTION & RT AFT OVERWING DOOR LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED REMOVAL & INSTALLATION OF THE RT EMER EXIT DOOR IAW AMM 52-22-00 & IT PER
- [SDR ASMF201503008](https://openairdocs.org/sdr/ASMF201503008.md): Warning System · false activation · Jan 30, 2015 · N342AM · Boeing 737800* · Central Computers
  > AIRCRAFT REJECTED TAKE OFF AT 60 KNOTS DUE TO MASTER CAUTION & RT AFT OVERWING DOOR LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 1.8 PROCEDURE, CONFIRMING THE FAILURE. PERFORMED BITE TO PSEU & THE CB`S WERE RESEATED IAW FIM 32-09 TASK 801 PROCEDURE, N
- [SDR ASMF201501028](https://openairdocs.org/sdr/ASMF201501028.md): Battery Pack · damaged · Jan 5, 2015 · N342AM · Boeing 737800* · Emergency Lighting
  > AIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CLIMB, ALL EMER LIGHTS TURNED ON & BURNED ODOR WITH NO EVIDENCE OF SMOKE WAS DETECTED. PERFORMED REVISION DETECTING IN THE M1671 BATTERY PACK THE CB P18-3 B-10 POPPED. O THE BATTERY PACK NR M1671 WAS DEFERRED IAW M
- [SDR ASMF201501022](https://openairdocs.org/sdr/ASMF201501022.md): Solenoid · malfunctioned · Dec 28, 2014 · N342AM · Boeing 737800* · Emergency Exits
  > AIRCRAFT REJECTED TAKE OFF AT 60 KNOTS, DUE TO RT AFT OVERWING LIGHT TURNED ON. PERFORMED A REVISION AT THE AFT OVERWING DOOR IAW AMM 52-20-00 & BITE TO PSEU IAW FIM 52-20 TASK 801 PROCEDURE, SHOWING FAILURE MSG. R FL SW FAULT, & DETECTING FAILURE OF FLIGHT L
- [SDR ASMF201501012](https://openairdocs.org/sdr/ASMF201501012.md): Wire Harness · damaged · Nov 10, 2014 · N342AM · Boeing 737890 · Pneumatic System Wiring
  > CAPTAIN REPORTED THAT DURING CRUISE, THE BLEED TRIP OFF LIGHT TURNED ON. ACCOMPLISHED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE & CONTINUING TO DESTINATION. PERFORMED THE FIM 36-10 TASK 801 DETECTING WIRING HARNESS DAMAGE. MW0311 LT ENG WIRING HARNESS W
- [SDR ASMF2015010500002](https://openairdocs.org/sdr/ASMF2015010500002.md): Brake Assy · damaged · Oct 4, 2014 · N342AM · Boeing 737800* · Landing Gear Brake System
  > AIRCRAFT REJECTED TAKEOFF AT 120 KNOTS, DUE TO AN ABNORMAL VIBRATION IN THE LT MLG. PERFORMED HIGH ENERGY STOP INSPECTION & AIRFRAME VIBRATION CONDITION INSPECTION IAW AMM 05-51-07 & AMM 05-51-67, DETECTED LT MLG BRAKES & WHEELS NRS 1 & 2 DAMAGED, LT MLG AXLE
- [SDR ASMF201310002](https://openairdocs.org/sdr/ASMF201310002.md): Oven · contaminated · Sep 15, 2013 · N342AM · Boeing 737832 · Buffet/Galleys
  > ACFT RETURNED TO PLATFORM, F/A REPORTED THAT A WIRE BURNED ODOR AFTER AFT GALLEY OVENS TURNED ON. MAINTENANCE PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56, DETECTING PAPER BURNED PROPERTY OF CATERING; THE PAPER WAS REMOVED AND AFT
- [SDR ASMF201309009](https://openairdocs.org/sdr/ASMF201309009.md): Unknown · unknown · Sep 4, 2013 · N342AM · Boeing 737832 · Standard Practices/Structures
  > CAPTAIN REPORTED THAT DURING DESCENT, A STRONG NOISE IN COCKPIT FWD COMPARTMENT WAS HEARD. MX PERFORMED A PRESSURIZATION VALVE AND OUTFLOW VALVE EXTERIOR VISUAL INSPECTION AND BITE TO CONTROLLER NR 2 IAW AMM 21-31-00, ALL CORRECT.
- [SDR ASMF20130531013](https://openairdocs.org/sdr/ASMF20130531013.md): Skin · damaged · May 19, 2013 · N342AM · Boeing 737800* · Fuselage Main, Plate/Skin
  > CAPTAIN REPORTED A LIGHTNING STRIKE DURING APPROACH IN THE FUSELAGE SKIN. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING A PERFORATION OUT OF LIMITS OF.1250" DIAMETER AT BS 480. FUSELAGE SKIN AT BS 480 WAS REPAIRED IAW SRM 53

## 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 = 'N342AM' AND deregistration_id = 'N342AM-2023-07-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N342AM-2023-07-18/reports

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