# N465AT: 1978 Boeing 737-2L9, registration cancelled 2013-09-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 26, 2013 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 737-2L9](https://openairdocs.org/model/boeing-737-2l9) (registry code 1384497) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 21528 - Year built: 1978 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 11, 1995 - Certificate issued: October 18, 2007 - Last registry action: October 18, 2007 - Mode S code: A5AC40 - Owner when cancelled: [Sky King Inc](https://openairdocs.org/faa-owner/SKY%20KING%20INC) - Location: [Sacramento, CA](https://openairdocs.org/faa-place/CA/Sacramento) - Owner type: Corporation - Owner's area on the map: 38.5438° N, 121.3783° W: Placed by OpenAirDocs at the center of ZIP code 95826, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N465AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=465AT - Page: https://openairdocs.org/deregistered/N465AT-2013-09-26 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-2L9: https://openairdocs.org/model/boeing-737-2l9.md ## Service difficulty reports (101, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR KNNA465091110KMIA](https://openairdocs.org/sdr/KNNA465091110KMIA), Sep 11, 2010: WINDOW. CRACKED. F/O'S SIDE WINDOW CRACKED. F/O'S NR 4 (SHOULD READ AS NR 5) WINDOW BEGAN CRACKING, DECENDED TO 14,000 FT WHILE PERFORMING ABNORMAL PROCEEDURES CHECKLIST BROUGHT - [SDR KNNA20100003](https://openairdocs.org/sdr/KNNA20100003), Jan 25, 2010: LINE. RUPTURED. STARTING DECENT, CALLED FOR FLAPS ONE, WITHIN 1 MINUTE THE HYD MASTER CAUTION ILLUMINATED. BOTH "A" HYD PUMPS INDICATED LOW PRESSURE. "A" PRESSURE SHOWED ZERO, - [SDR 2010F00021](https://openairdocs.org/sdr/2010F00021), Jan 25, 2010: LINE. RUPTURED. STARTING DECENT, CALLED FOR FLAPS ONE, WITHIN ONE MINUTE THE HYD MASTER CAUTION ILLUMINATED. BOTH "A" HYD PUMPS INDICATED LOW PRESSURE. "A" PRESSURE SHOWED ZERO - [SDR KNNA200800107](https://openairdocs.org/sdr/KNNA200800107), Nov 19, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP WAS CRACKED AT STA 827, STRINGER 5L. - [SDR KNNA200800106](https://openairdocs.org/sdr/KNNA200800106), Nov 19, 2008: STRINGER CLIP. CRACKED. FOUND STRINGER CLIP CRACKED AT STA 787, STRINGER 4R. - [SDR KNNA200800105](https://openairdocs.org/sdr/KNNA200800105), Nov 19, 2008: STRINGER CLIP. CRACKED. FOUND STRINGER CLIP CRACKED AT STA 639, STRINGER 3L. - [SDR KNNA200800104](https://openairdocs.org/sdr/KNNA200800104), Nov 19, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP WAS CRACKED AT STA 639, STRINGER 1L. - [SDR KNNA200800103](https://openairdocs.org/sdr/KNNA200800103), Nov 19, 2008: STRINGER CLIP. CRACKED. FOUND STRINGER CLIP CRACKED AT STA 616, STRINGER 0. - [SDR KNNA200800102](https://openairdocs.org/sdr/KNNA200800102), Nov 19, 2008: STRINGER CLIP. CRACKED. FOUND STRINGER CLIP CRACKED AT STA 616, STRINGER 1L. - [SDR KNNA200800100](https://openairdocs.org/sdr/KNNA200800100), Nov 19, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP WAS CRACKED AT STA 616, STRINGER 3R. - [SDR KNNA200800099](https://openairdocs.org/sdr/KNNA200800099), Nov 19, 2008: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP AT STA 685, STRINGER 8L. - [SDR KNNA200800098](https://openairdocs.org/sdr/KNNA200800098), Nov 19, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT STA 685, STRINGER 3R. - [SDR KNNA200800097](https://openairdocs.org/sdr/KNNA200800097), Nov 19, 2008: STRINGER CLIP. CRACKED. FOUND STRINGER CLIP CRACKED AT STA 706, STR 9L. - [SDR KNNA200800096](https://openairdocs.org/sdr/KNNA200800096), Nov 19, 2008: STRINGER CLIP. CRACKED. FOUND STRINGER CLIP CRACKED AT STA 706, STR 0. - [SDR KNNA200800095](https://openairdocs.org/sdr/KNNA200800095), Nov 19, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP WAS CRACKED AT STA 727B, STR 3L. - [SDR KNNA200800094](https://openairdocs.org/sdr/KNNA200800094), Nov 19, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP WAS CRACKED AT STA 767, STR 4R. - [SDR KNNA2000800093](https://openairdocs.org/sdr/KNNA2000800093), Nov 19, 2008: DOUBLER. DELAMINATED. FOUND BONDED DOUBLER WITH DELAM BETWEEN STA 727-727A AND STR 15R TO 17R. DELAM WAS REPAIRED IAW SRM 53-30-3 FIG 17. - [SDR KNNA20080092](https://openairdocs.org/sdr/KNNA20080092), Nov 10, 2008: FRAME. CRACKED. DURING C-CHECK FOUND FRAME CRACKED AT STA 639 BETWEEN STR 14R AND 15R. REPAIRED FRAME IAW SKY KING ACO-085357. - [SDR KNNA20080009](https://openairdocs.org/sdr/KNNA20080009), Apr 17, 2008: SKIN. DELAMINATED. DELAMINATION OF LEFT WING INBOARD AFT FLAP TRAILING EDGE WAS ORIGINALLY FOUND TO BE WITHIN LIMITS SO SPEED TAPE WAS APPLIED AS A TEMPORARY REPAIR AND THEN PLACE - [SDR KNNA200700064](https://openairdocs.org/sdr/KNNA200700064), Nov 22, 2007: BALL JOINT. LEAKING. WHILE EN ROUTE, THE CREW WAS ALERTED BY A NR 1 ENGINE FIRE WARNING ALARM BELL/LIGHTS. DECLARING AN IN-FLIGHT EMERGENCY, AND SHUTTING DOWN NR 1 ENGINE, AND A SIN - [SDR 02072007](https://openairdocs.org/sdr/02072007), Feb 4, 2007: LIGHT. FAILED. WHILE LANDING AT KLAX, DID NOT GET A GREEN LIGHT AFTER EXTENDING THE GEAR. THE MARKS ON THE LEFT MAIN GEAR. THE MARKS SEEN THROUGH THE VIEW PORT DUE TO THE MIRR - [SDR KNNA200600001](https://openairdocs.org/sdr/KNNA200600001), Nov 28, 2006: BULKHEAD. CRACKED. COMPRESSION FRAME CRACKED ON BULKHEAD BS 727 AT BL 0 FWD WALL OF AFT CARGO COMPARTMENT. CO 0653105 PROVIDE REPAIR INSTRUCTIONS ON REPAIR OF CRACKED WEB ANGLE IN - [SDR KNNA200600004](https://openairdocs.org/sdr/KNNA200600004), Nov 28, 2006: FLOORBEAM. CORRODED. FOUND CORROSION AT FLOORBEAM STA 344 LBL 62.50 TO RBL 24.75. - [SDR 46504](https://openairdocs.org/sdr/46504), Nov 28, 2006: FLOORBEAM. CORRODED. FOUND CORROSION AT FLOORBEAM STA 344 LBL 62.50 TO RBL 24.75. - [SDR 46501](https://openairdocs.org/sdr/46501), Nov 28, 2006: STRUCTURE. CRACKED. COMPRESSION CHORD CRACKED ON BULKHEAD B-STA727 AT BL-0 FWD WALL OF AFT CARGO COMPARTMENT. - [SDR 465C7](https://openairdocs.org/sdr/465C7), Nov 28, 2006: STRUCTURE. CRACKED. COMPRESSION CHORD CRACKED ON BULKHEAD B-STA727 AT BL-0 FWD WALL OF AFT CARGO COMPARTMENT. - [SDR KNNA200600003](https://openairdocs.org/sdr/KNNA200600003), Nov 16, 2006: FLOORBEAM. CORRODED. FOUND CORROSION AT FLOORBEAM STA 328 BL-0 TO RBL 62.50. - [SDR 46503](https://openairdocs.org/sdr/46503), Nov 16, 2006: FLOORBEAM. CORRODED. FOUND CORROSION AT FLOORBEAM STA 328 BL-0 TO RBL 62.50 - [SDR KNNA200600005](https://openairdocs.org/sdr/KNNA200600005), Nov 11, 2006: SKIN. DAMAGED. FOUND LIGHTNING STRIKE AT STA 216R BELOW RT EMERGENCY EXIT HANDLE. PROVIDE INSTRUCTIONS ON REPAIR OF LIGHTNING STRIKE AT FUSELAGE DRAIN HOLE STA 218, UNDER WIND - [SDR KNNA20060001A](https://openairdocs.org/sdr/KNNA20060001A), Nov 8, 2006: ANGLE. CORRODED. COMPRESSION CHORD CRACKED ON BULKHEAD OF BS 727, BL 0 (TOP) FWD WALL OF THE AFT CARGO COMPARTMENT. PROVIDE REPAIR INSTRUCTIONS ON REPAIR OF CRACKED WEB ANGLE IN - [SDR 2003F00545](https://openairdocs.org/sdr/2003F00545), Jun 28, 2003: SKIN. DELAMINATED. MSY-BNA - DURING POST REPOSITIONING FLIGHT INSPECTION, FLIGHT CREW OBSERVED UPPER SKIN DELAMINATION OF THE TRAILING EDGE NR 2 L/E SLAT, P/N 65-46422-267. A FOUR - [SDR AT0000446](https://openairdocs.org/sdr/AT0000446), Sep 25, 2000: SPAR. CORRODED. DURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON RIGHT WING FORWARD SPAR WEB AND SPAR CAP AT BS 414 AND BS 426. INSTALLED FILLER AND R - [SDR AT0000298](https://openairdocs.org/sdr/AT0000298), May 25, 2000: BATTERY PACK. DISCHARGED. FOUND EMERGENCY PATH LIGHTS BETWEEN SEAT ROW 12 AND 17 DID NOT ILLUMINATE DURING, TEST. REMOVED AND REPLACED THE BATTERY PACK AND ONE FUSE. PERFORMED OPERATIONA - [SDR AT0000275](https://openairdocs.org/sdr/AT0000275), Apr 19, 2000: SKIN. DENTED. FOUND DENT IN FUSELAGE TO BE OUT OF LIMITS AT BS 916 STRINGER 21L. PERFORMED EXTERNAL REPAIR IAW 737 SRM 53-30-3 FIGURE 6. - [SDR AT0000274](https://openairdocs.org/sdr/AT0000274), Apr 3, 2000: SKIN. DENTED. FOUND DENT IN FUSELAGE AT BS 1013 BETWEEN STRINGER 21 - 22R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED PLATE IAW 737 SRM 53-30-3. - [SDR AT0000273](https://openairdocs.org/sdr/AT0000273), Apr 3, 2000: SKIN. DENTED. FOUND DENT IN FUSELAGE TO BE OUT OF LIMITS AT BS 1018 BETWEEN STRINGER 15 - 16L. CUT OUT DAMAGED AREA AND REPAIRED DAMAGE IAW 737 SRM 53-30-3. - [SDR AT0000272](https://openairdocs.org/sdr/AT0000272), Apr 3, 2000: SKIN. DENTED. FOUND FUSELAGE DENT AT BS 905 STRINGER 23R, OUT OF LIMITS. REPAIRED IAW 737 SRM 53-30-3 FIGURE 28. - [SDR AT0000271](https://openairdocs.org/sdr/AT0000271), Apr 2, 2000: FLOORBEAM. CORRODED. FOUND CABIN BS 967 RBL 48-46 FLOORBEAM TOP CAP CORRODED IN SEVERAL PLACES. FABRICATED AND INSTALLED PARTS, IAW DWG NR 65C37472, 65C37528, AND 65C37522. - [SDR AT0000111](https://openairdocs.org/sdr/AT0000111), Feb 25, 2000: BULB. FAILED. FOUND MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE AND INTERMITTENT. SECURED EMERGENCY LIGHT AND REPLACED BULBS IAW 737 MM. - [SDR AT0000110](https://openairdocs.org/sdr/AT0000110), Feb 25, 2000: LIGHT. INOPERATIVE. FOUND EMERGENCY EXIT LIGHT ABOVE R-1 DIM AND INTERMITTENT. REMOVED AND REPLACED LIGHT ASSEMBLY IAW 737 MM. - [SDR AT0000082](https://openairdocs.org/sdr/AT0000082), Feb 9, 2000: BULB. FAILED. FOUND FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. RELAMPED BULBS IAW B737 MM 33-50. - [SDR AT0000009](https://openairdocs.org/sdr/AT0000009), Jan 2, 2000: O-RING. DEFECTIVE. DURING TAKEOFF, THE HYDRAULIC INDICATOR WENT TO ZERO AND EMERGENCY GEAR HANDLE WOULD NOT RAISE TO UP POSITION. REPLACED O-RING ON RIGHT MAIN LANDING GEAR BRAKE - [SDR AT9900910](https://openairdocs.org/sdr/AT9900910), Dec 16, 1999: PCU. MALFUNCTIONED. DURING CRUISE, EXPERIENCED RUDDER HARDOVER. AIRPLANE ROLLED LEFT THEN RIGHT APPROX 30 DEGREE BANK WITH AUTOPILOT ON. REMOVED AND REPLACED FLIGHT DATA RECORDER, - [SDR AT9900758](https://openairdocs.org/sdr/AT9900758), Oct 18, 1999: POWER SUPPLY. INOP. FOUND FORWARD AND AFT EMERGENCY EXIT AISLE SIGNS INOPERATIVE. REPLACED POWER SUPPLY IN EACH FORWARD AND AFT EMERGENCY EXIT SIGNS. - [SDR AT9900672](https://openairdocs.org/sdr/AT9900672), Sep 23, 1999: LIGHT. INOP. DURING INSPECTION FOUND L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. - [SDR AT9900447](https://openairdocs.org/sdr/AT9900447), Jun 16, 1999: FUSE. BLOWN. DURING LAY OVER CHECK, FOUND THE FORWARD SECTION OF EMERGENCY PATH LIGHTING NOT WORKING. REPLACED BAD FUSE IN BATTERY CHARGER IAW MM 33-21-27 PAGE 35. - [SDR AT9900037](https://openairdocs.org/sdr/AT9900037), Jan 23, 1999: LIGHT. INOPERATIVE. CABIN EMERGENCY LIGHT ABOVE R-1 DOOR DID NOT ILLUMINATE DURING LAYOVER CHECK. SECURED FIXTURE PROPERLY INTO CONNECTOR ASSEMBLY, OPS CHECKED GOOD PER MM 33-50. ( - [SDR AT9900036](https://openairdocs.org/sdr/AT9900036), Jan 21, 1999: LAMP. FAILED. LEFT FUSELAGE EMERGENCY LIGHT AFT OF WING DOES NOT ILLUMUNATE. RELAMPED LEFT AFT FUSELAGE EMERGENCY LIGHT IAW MM 33-51-61, OPS CHECKED GOOD. - [SDR AT9900014](https://openairdocs.org/sdr/AT9900014), Jan 11, 1999: WIRE. BROKEN. LOWER L-1 DOOR EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE BEHIND LIGHT. SPLICED WIRE PER STANDARD PRACTICES CHAPTER 20. OPS CHECKED GOOD. (X) - [SDR AT9900013](https://openairdocs.org/sdr/AT9900013), Jan 11, 1999: BULB. FAILED. EMERGENCY LIGHT ON RIGHT HAND LOWER AFT WING TO BODY FAIRING IS INOPERATIVE (NEXT TO AFT PIT DOOR). RE-LAMPED RIGHT HAND AFT LOWER WING TO BODY EMERGENCY LIGHT All 101: https://openairdocs.org/deregistered/N465AT-2013-09-26/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.