# Service difficulty reports: N396AN, cancelled Mar 23, 2022

A list on [N396AN, cancelled Mar 23, 2022](https://openairdocs.org/deregistered/N396AN-2022-03-23.md).

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

Page 1 of 3 · 137 reports

- [SDR MK1Y202201025](https://openairdocs.org/sdr/MK1Y202201025.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > THE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE RIGHT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR. RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTI
- [SDR MK1Y202201024](https://openairdocs.org/sdr/MK1Y202201024.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > THE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE LEFT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR. RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIF
- [SDR MK1Y202201023](https://openairdocs.org/sdr/MK1Y202201023.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Wing Structure
  > DENT DAMAGE AND AN EXISTING BLEND-OUT WAS FOUND ON THE LOWER WING SKIN PANEL (P/N 112T4702-1) COMMON TO THE OUTBOARD STRINGER L-9.5 (P/N 767-3421-7) BETWEEN WS 990.2 AND WS 1006. AN EXISTING FREEZEPLUG AND THE OUTBOARD STRINGER L-9.5 HAD BEEN INSTALLED PER SER
- [SDR MK1Y202201022](https://openairdocs.org/sdr/MK1Y202201022.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Engine Thrust Reverser
  > PROBLEM DESCRIPTION: ENGINE #2, THRUST REVERSER TRANSLATING COWL, INNER SKIN, P/N CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI A CRACKED DENT WAS FOUND IN THE INNER SKIN OF INBD THRUST REVERSE IN CLOSE PROXIMITY TO AN EXISTING REPAIR OF EN
- [SDR MK1Y202201021](https://openairdocs.org/sdr/MK1Y202201021.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuel Boost Pump
  > R/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.
- [SDR MK1Y202201020](https://openairdocs.org/sdr/MK1Y202201020.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuel Boost Pump
  > L/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.
- [SDR MK1Y202201019](https://openairdocs.org/sdr/MK1Y202201019.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Wing Structure
  > PROBLEM DESCRIPTION: SLAT NO. 4, OSS 579.05: SHOP FOUND A DENT ADJACENT TO A BULGE IN UPPER LE SKIN OF SLAT NO. 4. THE DAMAGED AREA LOCATED ON A RIB AND STIFFENER. SLAT: P/N 114T4104-203G; S/N 000010.
- [SDR MK1Y202201018](https://openairdocs.org/sdr/MK1Y202201018.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > FUSELAGE SKIN (SEC 45), STA 999 AND STA 1043, STR-2L AND STR-2R: DURING CONVERSION PROCESS, AIRCRAFT MAINTENANCE WAS REQUIRED TO DEACTIVATE AND REMOVE THE HIGH GAIN SATCOM SYSTEM PER CUSTOMER REQUEST THAT WAS INSTALLED BY THE PREVIOUS OPERATOR. THE LARGE EXTER
- [SDR MK1Y202201017](https://openairdocs.org/sdr/MK1Y202201017.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Wing Structure
  > PROBLEM DESCRIPTION: SLAT NO 5 AT OSS 389.71: SHOP FOUND DENT AMONG FASTENERS AT THE EDGE OF SLAT LE SKIN ATTACHMENT COMMON TO A RIB. THE REPORTED DAMAGE WAS FOUND SMOOTH WITHOUT SHARP EDGES OR LOOSE FASTENERS.
- [SDR MK1Y202201016](https://openairdocs.org/sdr/MK1Y202201016.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Empennage Structure
  > HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U3 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THE
- [SDR MK1Y202201015](https://openairdocs.org/sdr/MK1Y202201015.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Empennage Structure
  > HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT LBL10.83 STR U3 TO U2 AND LBL 11.83 STR U2 TO U1: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS W
- [SDR MK1Y202201013](https://openairdocs.org/sdr/MK1Y202201013.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Engine Thrust Reverser
  > PROBLEM DESCRIPTION: #2 ENGINE OUTBOARD THRUST REVERSER DAGMAR FAIRING DAMAGE, ASSY IDENT: 683L136613, MODEL NO. TR-CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ELONGATED HOLES SUNK RIVETS AND GOUGES ACROSS THE FAST
- [SDR MK1Y202201012](https://openairdocs.org/sdr/MK1Y202201012.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Powerplant System
  > ENGINE #1 OUTBD CORE COWL HAT FRAME NAC STA 303.75, LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, CRACK WAS FOUND AT DATUM LOCATION WITH 1.5 INCH LENGTH.
- [SDR MK1Y202201011](https://openairdocs.org/sdr/MK1Y202201011.md): Tear Strap · corroded · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Main, Plate/Skin
  > TEAR STRAP, INNER SKIN, STA 544, S-1R AND S-4R, DOOR SURROUND ZONE: SHOP DISCOVERED DEEP CORROSION ON TEAR STRAP EDGE COMMON TO S-2R (LAP SPLICE). THE DAMAGED AREA IS LOCATED IN CONVERSION INSTALLATION ZONE.
- [SDR MK1Y202201010](https://openairdocs.org/sdr/MK1Y202201010.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Wing Structure
  > PROBLEM DESCRIPTION: R/H WING LOWER SKIN SURFACE BETWEEN WS.994.7 AND WS.1001.7: SHOP FOUND TOOL MARK AMONG FASTENERS, PAINT STRIPPED AND PERFORMED NDT THICKNESS INSPECTION WAS PERFORMED.
- [SDR MK1Y202201009](https://openairdocs.org/sdr/MK1Y202201009.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Powerplant System
  > WORN CORE COWL ALUMINUM HAT FRAME – ENGINE# 1, R/H CORE COWL, HAT FRAME, NAC STA 303.75, UPPER AREA DURING THE MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ON #1 ENGINE, R/H CORE COWL HAT CHANNEL FRAME NAC STA 303.75 UPPER SECTION WITH WORN, DAMA
- [SDR MK1Y202201008](https://openairdocs.org/sdr/MK1Y202201008.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > . DURING A/C SURVEY AT TLV, MAINTENANCE DISCOVERED EXISTING BLENDOUT AT THE EDGE OF AN EXISTING FLUSH REPAIR CUTOUT LOCATED ON THE FUSELAGE SKIN AT STA 616 BETWEEN S38L AND S39L. THE EXISTING FLUSH REPAIR WAS FOUND TO BE INSTALLED BY THE PRIOR OPERATOR, AMERI
- [SDR MK1Y202201007](https://openairdocs.org/sdr/MK1Y202201007.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Engine Cowling System
  > ENGINE # 2, LH CORE COWL, HAT FRAME, NAC STA 303.75, MID LOWER AREA: DURING MAINTENANCE INSOECTION AT IAI, MAINTENANCE DISCOVERED ON #2 ENGINE, LH CORE COWL HAT CHANNEL FRAME NAC STA 303.75 MID LOWER SECTION WITH CRACK AND GOUGE. PLEASE REFER TO FIGURE 2 FOR T
- [SDR MK1Y202201006](https://openairdocs.org/sdr/MK1Y202201006.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > NLG SUPPORT STRUCTURE, AFT VERTICAL STIFFENERS, UPPER EDGES, STA 287, L/RBL 13.10 DURING THE MAINTENANCE INSPECTION AT IAI, TWO CRACKS WERE FOUND AT DATUM LOCATIONS WITH 0.6 INCH LENGTH EACH ONE. THERE IS NO APPLICABLE DAMAGE EXISTING. VERTICAL STIFFENERS PI
- [SDR MK1Y202201005](https://openairdocs.org/sdr/MK1Y202201005.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > EXTERNAL FUSELAGE SKIN, STA 1487, STR-21L & STA 1460, STR-29L-STR-30L: DURING THE MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUTS EXCEED\ THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFE
- [SDR MK1Y202201004](https://openairdocs.org/sdr/MK1Y202201004.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > EXTERNAL FUSELAGE SKIN, STA 308, STR-33L: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.
- [SDR MK1Y202201003](https://openairdocs.org/sdr/MK1Y202201003.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > EXTERNAL FUSELAGE SKIN, STA 588, STR-33R: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.
- [SDR MK1Y202201002](https://openairdocs.org/sdr/MK1Y202201002.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Nacelle/Pylon Structure
  > FAN COWL SUPPORT BEAM LINK, #2 PYLON, P/N 31112522-1 DURING THE MAINTENANCE INSPECTION AT IAI, THE BORES IN THE #2 PYLON FAN COWL SUPPORT BEAM LINK PIN 311T2522-1 WERE FOUND TO BE WORN. THE BORE DIAMETERS WERE FOUND TO BE Ø.8770". THE NOMINAL DIAMETER OF THE
- [SDR MK1Y202201001](https://openairdocs.org/sdr/MK1Y202201001.md): None · none · Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)
  > PROBLEM DESCRIPTION: DURING THE MAINTENANCE INSPECTION FOUND SCRATCHES ON EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. - SHOP CLEANED DAMAGED AREA IAW SRM 51-10-02. SHOP REMOVED
- [SDR AALA2020022089025](https://openairdocs.org/sdr/AALA2020022089025.md): Clutch · sticking · Feb 17, 2020 · N396AN · Boeing 767323 · Auto Throttle System
  > AIRCRAFT WAS NOT GROUNDED: LEFT THROTTLE STICKING AUTO AND MANUAL OPERATION DOES NOT KEEP UP WITH RIGHT THROTTLE IN AUTO MODE. REPLACED AUTO THROTTLE CLUTCH PACK PER AMM 22-32-05.
- [SDR 2019FA0000383](https://openairdocs.org/sdr/2019FA0000383.md): Light · inoperative · Nov 23, 2019 · N396AN · Boeing 767323 · Emergency Lighting
  > 7A SEAT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD.
- [SDR AALA201910039007](https://openairdocs.org/sdr/AALA201910039007.md): Access Panel · damaged · Oct 2, 2019 · N396AN · Boeing 767323 · Fuselage Floor Panel
  > AIRCRAFT WAS GROUNDED: CABIN FLOOR ACCESS PANEL FOR E&E COMPARTMENT BOARD SOFT. REPLACED ACCESS PANEL PER AMM 52-48-05.
- [SDR AALA201906189013](https://openairdocs.org/sdr/AALA201906189013.md): Slide · low pressure · Jun 16, 2019 · N396AN · Boeing 767323 · Escape Slide
  > AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L1 DOOR SLIDE DOES NOT SHOW NEEDLE SHADOW IN GREEN BAND AND IS OUT OF LIMITS FOR PRESSURE GAUGE ON LOW SIDE. REMOVED AND REPLACED SLIDE ASSY IAW AMM 25-66-01. ALL CHECKS NORMAL.
- [SDR AALA20190512004](https://openairdocs.org/sdr/AALA20190512004.md): Support Fitting · corroded · May 12, 2019 · N396AN · Boeing 767323 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SUPPORT FITTING AT BS 1570 ON THE LAVATORY DUMP CRANK TOWER. REPLACED SUPPORT FITTING PER SRM 51-40-02.
- [SDR AALA20190512002](https://openairdocs.org/sdr/AALA20190512002.md): Shear Tie · corroded · May 12, 2019 · N396AN · Boeing 767323 · Fuselage Internal Mounting Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHEAR TIE AT BS 1562 AND BL 0. REPLACED SHEAR TIE PER SRM 51-10-02-0G
- [SDR AALA201902264001](https://openairdocs.org/sdr/AALA201902264001.md): Fuel Filter · dirty · Feb 23, 2019 · N396AN · Boeing 767323 · Fuel Controlling System
  > DURING CLIMB, THE RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATED. REFERRED TO THE QRH, ADVISED TO LAND AS SOON AS POSSIBLE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACCOMPLISHED MCM 4918. RT FUEL FILTER ELEMENTS REMOVED A
- [SDR AALA2018102979001](https://openairdocs.org/sdr/AALA2018102979001.md): Flashlight · no test · Oct 25, 2018 · N396AN · Boeing 767323 · Emergency Equipment
  > EMERGENCY FLASHLIGHTS AT THE FLIGHT ATTENDANTS JUMPSEAT, DID NOT TEST. REPLACED THE FLASHLIGHT AND TESTED GOOD IAW FIM 25-60-05.
- [SDR AALA2018101529023](https://openairdocs.org/sdr/AALA2018101529023.md): Battery Pack · inoperative · Oct 10, 2018 · N396AN · Boeing 767323 · Emergency Equipment
  > MID CABIN, LEFT SIDE,AFT FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLASHLIGHT BATTERY IAW GPM 05-01-07. OPS CHECKED GOOD.
- [SDR AALA2018091879012](https://openairdocs.org/sdr/AALA2018091879012.md): Antenna · faulted · Sep 16, 2018 · N396AN · Boeing 767323 · Weather Radar System
  > WEATHER RADAR FAILED DURING FLIGHT. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND WEATHER RADAR PANEL AND ANTENNA AT FAULT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED IA
- [SDR AALA2018091879004](https://openairdocs.org/sdr/AALA2018091879004.md): Control Panel · failed · Sep 16, 2018 · N396AN · Boeing 767323 · Weather Radar System
  > WEATHER RADAR FAILED DURING FLIGHT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND THE WEATHER RADAR PANEL AND ANTENNA AT FAULT. REPLACED IAW MM 3
- [SDR AALA201807129024](https://openairdocs.org/sdr/AALA201807129024.md): Battery · inoperative · Jul 10, 2018 · N396AN · Boeing 767323 · Emergency Equipment
  > MID GALLEY LEFT SIDE LOWER ACCESS DOOR DETACHABLE FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY. CHECKED NPRMAL.
- [SDR AALA20180327007](https://openairdocs.org/sdr/AALA20180327007.md): Light · inoperative · Mar 26, 2018 · N396AN · Boeing 767323 · Emergency Lighting
  > SEAT 3J MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED 3J SEAT MOUNTED EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECKED NORMAL. AIRCRAFT WAS GROUNDED.
- [SDR AALA201801199005](https://openairdocs.org/sdr/AALA201801199005.md): Battery · no test · Jan 16, 2018 · N396AN · Boeing 767323 · Emergency Equipment
  > FLASHLIGHT AT THE JUMPSEAT REAR LEFT FLIGHT COMPARTMENT BATTERY WILL NOT TEST. REPLACED THE BATTERY IAW AMM 25-64-00.
- [SDR AALA201712279032](https://openairdocs.org/sdr/AALA201712279032.md): Threshold · loose · Dec 25, 2017 · N396AN · Boeing 767323 · Fuselage Miscellaneous Structure
  > FIRST CLASS FORWARD LAVATORY DOOR STICKING AT THRESHOLD BASE. TIGHTENED THRESHOLD SCREWS. CHECKED NORMAL.
- [SDR AALA20171205003](https://openairdocs.org/sdr/AALA20171205003.md): Stiffener · cracked · Dec 5, 2017 · N396AN · Boeing 767323 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER ON FORWARD SIDE OF FRAME 246 AT LBL26. INSTALLED ANGLE STIFFENER PER SRM 53-10-51-2R3.
- [SDR AALA20171204002](https://openairdocs.org/sdr/AALA20171204002.md): Stiffener · cracked · Dec 4, 2017 · N396AN · Boeing 767323 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6. REPLACED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6 PER SRM 53-10-51-2R3.
- [SDR AALA20171204001](https://openairdocs.org/sdr/AALA20171204001.md): Stiffener · cracked · Dec 4, 2017 · N396AN · Boeing 767323 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4. REPLACED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4 PER SRM 53-10-51-2R3.
- [SDR AALA201709059036](https://openairdocs.org/sdr/AALA201709059036.md): Smoke Detector · no test · Sep 1, 2017 · N396AN · Boeing 767323 · Smoke Detection
  > THE AIRCRAFT WAS NOT GROUNDED. PASSENGER SMOKING IN LAV A5. SMOKE DETECTION SYSTEM DID NOT INDICATE ANY SMOKE. LAV A5 SMOKE DETECTOR OPS CHECK PERF IAW AMM 26-13-00-715-090, TEST OK. THERMAL STICKER IN WASTE BIN CHECKED FOR SIGNS OF HEAT, NIL EVIDENT. A/C OK
- [SDR AALA201707249032](https://openairdocs.org/sdr/AALA201707249032.md): Pump · failed · Jul 21, 2017 · N396AN · Boeing 767323 · Fuel Boost Pump
  > DURING FLIGHT LEFT FWD BOOST PUMP WOULD NOT WORK AFTER BALANCING FUEL. CIRCUIT BREAKER DISCOVERED TRIPPED. REMOVED AND REPLACED LEFT FWD BOOST PUMP IAW AMM 28-22-03. OPS CHECKED AND LEAK CHECKED GOOD.
- [SDR AALA201706279041](https://openairdocs.org/sdr/AALA201706279041.md): Lens · detached · Jun 26, 2017 · N396AN · Boeing 767323 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE L1 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-03. OPERATIONAL CHECK GOOD.
- [SDR AALA20170622006](https://openairdocs.org/sdr/AALA20170622006.md): Lens · missing · Jun 22, 2017 · N396AN · Boeing 767323 · Emergency Lighting
  > EMERGENCY EXIT CEILING LIGHT NEAR SEATS 26G AND 25H HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR AALA201706019034](https://openairdocs.org/sdr/AALA201706019034.md): Attach Angle · corroded · May 30, 2017 · N396AN · Boeing 767323 · Nacelle/Pylon, Main Frame
  > LEFT ENGINE FAN CASE NOSE COWL ATTACH ANGLE HAS EVIDENCE OF CORROSION AT THE 4 O'CLOCK AND 5'OCLOCK POSITIONS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT ENGINE IAW MCM 71-93-01, 71-95-22, 71-94-45, 71-94-03, AND 71-94-43. OPERATIONAL CHECK GOOD.
- [SDR AALA201704259001](https://openairdocs.org/sdr/AALA201704259001.md): Battery Pack · no test · Apr 21, 2017 · N396AN · Boeing 767323 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TEST. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
- [SDR AALA201704249031](https://openairdocs.org/sdr/AALA201704249031.md): Charger · no test · Apr 21, 2017 · N396AN · Boeing 767323 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TO TEST. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
- [SDR AALA20170413002](https://openairdocs.org/sdr/AALA20170413002.md): Connector · broken · Apr 13, 2017 · N396AN · Boeing 767323 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 39H HAS A BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR IAW SWPM 20-64-17. OPERATIONAL CHECK IAW AMM 33-51-00 GOOD.

Next page: https://openairdocs.org/deregistered/N396AN-2022-03-23/reports.md?page=2

## 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 = 'N396AN' AND deregistration_id = 'N396AN-2022-03-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N396AN-2022-03-23/reports

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