# N924TS: 1975 Boeing 727-227, registration cancelled 2013-09-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 16, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-227](https://openairdocs.org/model/boeing-727-227) (registry code 1384078)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21041
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 3, 1975
- Certificate issued: November 30, 2001
- Last registry action: April 4, 2008
- Mode S code: ACCEC0
- Owner when cancelled: [Northwest Air Leasing LLC](https://openairdocs.org/faa-owner/NORTHWEST%20AIR%20LEASING%20LLC)
- Location: [Bellevue, WA](https://openairdocs.org/faa-place/WA/Bellevue)
- Owner type: Corporation
- Owner's area on the map: 47.6183° N, 122.2053° W: Placed by OpenAirDocs at the center of ZIP code 98004, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N924TS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=924TS
- Page: https://openairdocs.org/deregistered/N924TS-2013-09-16

From the FAA registry file of November 3, 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 727-227: https://openairdocs.org/model/boeing-727-227.md

## Service difficulty reports (59, newest 50)

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

- [SDR USAA100001](https://openairdocs.org/sdr/USAA100001), Oct 3, 2000: SMOKE DETECTOR. FALSE INDICATION. FLT 8800 - LGA-BOS - RIGHT AFT LAV SMOKE DETECTOR SOUNDED IN FLIGHT. NO SMOKE OR FIRE. REPLACED RIGHT AFT LAV SMOKE DETECTOR. (M)
- [SDR USAA090007](https://openairdocs.org/sdr/USAA090007), Sep 29, 2000: SMOKE DETECTOR. MALFUNCTIONED. FLT 6850 - DCA-LGA - LEFT AFT LAVATORY SMOKE WENT OFF SEVERAL TIMES IN FLIGHT. CI NR M559489 ASSIGNED PER MEL SEQ 26-17. C1 CLEARED, REPLACED AFT LEFT LAV SMOKE
- [SDR USAA090006](https://openairdocs.org/sdr/USAA090006), Sep 26, 2000: SMOKE DETECTOR. INOPERATIVE. FLT 6865 - LGA-DCA - AFT LEFT LAVATORY SMOKE DETECTOR INOPERATIVE. REINSTALLED SMOKE DETECTOR. OPS CHECKS OK. (M)
- [SDR USAA090005](https://openairdocs.org/sdr/USAA090005), Sep 20, 2000: SMOKE DETECTOR. INOPERATIVE. BOS-LGA - FLT 8801 - LEFT AFT LAVATORY SMOKE DETECTOR ALARM ACTIVATED IN FLIGHT. NO SMELL OR VISIBLE EVIDENCE OF SMOKE IN LAVATORY. REPLACED AFT LEFT LAVATORY S
- [SDR USAA090003](https://openairdocs.org/sdr/USAA090003), Sep 19, 2000: SWITCH. INOPERATIVE. FLT 6808 - LGA-BOS - AT CRUISE ALTITUDE 16,000 START VALVE OPEN LIGHT ILLUMINATED. FOLLOWED ALL CHECKLISTS AND PROCEDURES. REPLACED NR 3 START VALVE AND PRESSUR
- [SDR USAA090002](https://openairdocs.org/sdr/USAA090002), Sep 19, 2000: SMOKE DETECTOR. INOPERATIVE. FLT 8801 - BOS-LGA - SMOKE DETECTOR RIGHT AFT LAV SOUNDED. REPLACED RIGHT AFT LAVATORY SMOKE DETECTOR. (M)
- [SDR USAA090004](https://openairdocs.org/sdr/USAA090004), Sep 19, 2000: SMOKE DETECTOR. INOPERATIVE. FLT 6806 - LGA-BOS - RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF, REPEAT ITEM. REPLACED RIGHT AFT LAV SMOKE DETECTOR. CHECKS OK. (M)
- [SDR USAA020005](https://openairdocs.org/sdr/USAA020005), Feb 26, 2000: ENGINE. FAILED. FLT 6317 - BOS-LGA - NR 2 ENGINE FAILURE ON TAKEOFF. VIBRATION, LOUD NOISE, EGT RED-LINE. ABORTED TAKEOFF. REPLACED NR 2 ENGINE IAW FORMS 01TS087, 01TS090, 01TS
- [SDR USAA04003](https://openairdocs.org/sdr/USAA04003), Feb 3, 2000: LIGHT. INOPERATIVE. FOUND L/S, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECKS OK. (M)
- [SDR USAA119919](https://openairdocs.org/sdr/USAA119919), Nov 29, 1999: BRACKET. CHAFFED. RIGHT WING AFT SPAR AREA SPOILER BRACKET, FOUND AILERON CABLE CHAFFING INTO BRACKET JUST FORWARD OF INBOARD AILERON AT WING STATION 410. ACCOMPLISHED REWORK OF 
- [SDR USAA119918](https://openairdocs.org/sdr/USAA119918), Nov 29, 1999: FLOORBEAM. CORRODED. FOUND CORROSION AT STATION 1130 FLOORBEAM LOWER CHORD FROM AT RBL 48 TO BL 0. INSTALLED REPAIR AT STATION 1130 FLOORBEAM LOWER CHORD, FROM RBL 20 TO RBL 52. MAT
- [SDR USAA119917](https://openairdocs.org/sdr/USAA119917), Nov 29, 1999: SKIN. DENTED. FOUND DURING C-CHECK, EXTERIOR SKIN STATION AT 203 ACROSS STRINGER 19R LAP SEAM HAS ELONGATED DENT. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR AT BS 203, STRINGER 
- [SDR USAA119916](https://openairdocs.org/sdr/USAA119916), Nov 29, 1999: STIFFENER. CRACKED. AFT CARGO COMPARTMENT AFT BULKHEAD STATION 1183, VERTICAL STIFFENER CRACKED AT LOWR END, LBL 8 AND RBL 8. INSTALLED KIT REPAIR AT BS 1183, LBL 8 AND RBL 8, VERT
- [SDR USAA119915](https://openairdocs.org/sdr/USAA119915), Nov 29, 1999: STIFFENER. CORRODED. VERTICAL BEAM AT AFT PRESSURE BULKHEAD STATION 1183 LBL 18, HAS SPOT OF CORROSION AT TOP END. ACCOMPLISHED BS 1183 BULKHEAD, LBL 17.8 VERTICAL BEAM CORROSION BL
- [SDR USAA119914](https://openairdocs.org/sdr/USAA119914), Nov 29, 1999: BULKHEAD. CRACKED. FOUND DURING C-CHECK, RIGHT MAIN WHEEL WELL STATION 870, PRESSUER WEB HAS 3 INCH CRACK JUST OUTBOARD OF KEEL BEAM. INSTALLED WEB REPAIR AT RIGHT MAIN WHEEL WELL
- [SDR USAA119913](https://openairdocs.org/sdr/USAA119913), Nov 29, 1999: SKIN. CRACKED. FOUND DURING C-CHECK, RIGHT WING OUTBOARD FLAP, FORE FLAP DOUBLER, ON FORE FLAP HAS LOOSE RIVETS AND CRACKED AREA OUTBOARD FLAP TOGGLE CARRIAGE. INSTALLED DOUBL
- [SDR USAA119912](https://openairdocs.org/sdr/USAA119912), Nov 29, 1999: STIFFENER. CRACKED. FOUND DURING C-CHECK, AFT CARGO COMPARTMENT STATION 1183 BULKHEAD CRACK INDICATION AT WEB VERTICAL STIFFENER LOWER END LBL 8 INCHES WL 181. INSTALLED REPAIR KIT
- [SDR USAA119911](https://openairdocs.org/sdr/USAA119911), Nov 29, 1999: SKIN. GOUGED. SKIN EXTERIOR BETWEEN STRINGER 5L AND 7L STATION 345 TO 380 HAS DENTS AND GOUGES. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR FROM BS 345 TO BS 380, STRINGER 5 TO S
- [SDR USAA119920](https://openairdocs.org/sdr/USAA119920), Nov 27, 1999: BEAM. CRACKED. FOUND DURING C-CHECK, AFT PRESSURE BULKHEAD, FORWARD FLANGE CRACK, BLR 17.8, WL 278 IN FLAGE RADIUS. ACCOMPLISHED REPAIR AT AFT PRESSURE BULKHEAD RBL 17.8 WL 27
- [SDR USAA099904](https://openairdocs.org/sdr/USAA099904), Sep 29, 1999: VOLTAGE REGULATO. FAILED. FLT 6071 - BOS-LGA - ABORTED TAKEOFF DUE TO NR 2 GENERATOR DIFFERENTIAL FAULT, OVERVOLTAGE LIGHT ILLUMINATED. REPLACED NR 2 ENGINE VOLTAGE REGULATOR. OPERATIONA
- [SDR USAA089903](https://openairdocs.org/sdr/USAA089903), Aug 18, 1999: HOSE. LEAKING. HYDRAULIC SYSTEM B ELECTRIC PUMP NR 2 LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. B SYSTEM HYDRAULIC QUANTITY INDICATED ZERO. EXECUTED APPROPRIATE ABNORMAL PROCED
- [SDR USAA089901](https://openairdocs.org/sdr/USAA089901), Aug 11, 1999: CHARGER. FAILED. RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED CHARGER AND BATTERY PACK. (M)
- [SDR USAA040002](https://openairdocs.org/sdr/USAA040002), Aug 4, 1999: CHARGER. INOPERATIVE. FOUND ON L/S CHECK, RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK. (M)
- [SDR USAA069946](https://openairdocs.org/sdr/USAA069946), Jun 16, 1999: VALVE. FAILED. NR 3 ENGINE OIL TEMP HIGH. PERFORMED ABNORMAL HIGH OIL TEMP PROCEDURE. CYCLED FUEL HEAT SWITCH, NO HELP. SHUT DOWN NR 3 ENGINE BEFORE 15 MINUTES MAXIMUM OIL TEM
- [SDR USAA059907](https://openairdocs.org/sdr/USAA059907), May 24, 1999: SMOKE DETECTOR. FAILED. FLT 6181 - BOS-LGA - FOUND ON L/S, FORWARD LAVATORY SMOKE DETECTOR WILL NOT TEST. REPLACED FORWARD LAVATORY SMOKE DETECTOR. (M)
- [SDR USAA049908](https://openairdocs.org/sdr/USAA049908), Apr 28, 1999: BATTERY CHARGER. FAILED. FLT 6151 - BOS-LGA - FOUND ON L/S, EPL LIGHTS OUT FROM ROW 8 TO ROW 15. FOUND FUSE BLOW IN FORWARD EPL BATTERY CHARGER. FUSE PIGTAIL BROKEN IN F3 FUSE HOLDER. R
- [SDR USAA039915](https://openairdocs.org/sdr/USAA039915), Mar 20, 1999: COVER. BENT. FLT 6400 - DCA-LGA - EXTREMELY LOUD NOISE (AIR FLOW) AROUND L-1 DOOR IMMEDIATELY AFTER TAKEOFF. RETURNED TO BASE. PRESSURIZATION INDICATION NORMAL OPERATION. FO
- [SDR USAA039911](https://openairdocs.org/sdr/USAA039911), Mar 15, 1999: SKIN. CRACKED. FUSELAGE STATION 385, DENT AND GOUGE FOUND ABOVE STRINGER 1R. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 1. (M)
- [SDR USAA039910](https://openairdocs.org/sdr/USAA039910), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 720 THROUGH 720A HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M)
- [SDR USAA039909](https://openairdocs.org/sdr/USAA039909), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 500 THROUGH 555 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M)
- [SDR USAA039908](https://openairdocs.org/sdr/USAA039908), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 630 THORUGH 645 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M)
- [SDR USAA039907](https://openairdocs.org/sdr/USAA039907), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 560 THROUGH 580 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M)
- [SDR USAA039906](https://openairdocs.org/sdr/USAA039906), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 700 THROUGH 720 HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 15A. (M
- [SDR USAA039905](https://openairdocs.org/sdr/USAA039905), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 725C THROUGH 730C HAS CRACK INDICATIONS FOUND DURING EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M
- [SDR USAA039904](https://openairdocs.org/sdr/USAA039904), Mar 15, 1999: SKIN. CRACKED. FUSELAGE LAP SEAM 4R, STATION 720B THROUGH 725B HAS CRACK INDICATIONS FOUND DURING CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW 727 SRM 53-30-3 FIGURE 5. (M)
- [SDR USAA039901](https://openairdocs.org/sdr/USAA039901), Mar 3, 1999: BATTERY PACK. DISCHARGED. FLT 6160 - LGA-BOS - OVERHEAD AISLE EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 17. REPLACED BATTERY PACK, CHECKS OK. (M)
- [SDR USAA029909](https://openairdocs.org/sdr/USAA029909), Feb 17, 1999: LIGHT. INOPERATIVE. FLT 6141 - BOS-LGA - FOUND ON POST FLIGHT INSPECTION, COCKPIT EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH WHEN EMERGENCY EXIT LIGHTS DISARMED. RESEATED LIGHT ASSEM
- [SDR USAA129809](https://openairdocs.org/sdr/USAA129809), Dec 28, 1998: BATTERY PACK. DISCHARGED. FLT 6141 - BOS-LGA - FOUND ON L/S CHECK, CEILING EMERGENCY EXIT LIGHT AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK OK. (M)
- [SDR USAA129804](https://openairdocs.org/sdr/USAA129804), Dec 7, 1998: FUEL PUMP. FAILED. FLT 6170 - LGA-BOS - ON TAKEOFF AFTER 1.4 EPR CHECK, WHEN POWER APPLIED FOR TAKEOFF NR 1 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 1 ENGINE DRIVEN FUEL PUMP PE
- [SDR TAOA089807](https://openairdocs.org/sdr/TAOA089807), Aug 23, 1998: BATTERY PACK. DISCHARGED. FLT 6492, FOUND L/S CHECK, EMERGENCY EXIT SIGN AT R-2 DOOR DOES NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK AT R-2 DOOR LOCATION. OPERATIONAL CHECK NORMAL
- [SDR TAOA039806](https://openairdocs.org/sdr/TAOA039806), Mar 26, 1998: APU. OVERHEATING. LGA-BOS - FLT 6080 - SMOKE IN CABIN WITH BOTH PACKS AND GASPER FAN ON. PACKS WERE NOT OVERHEATED, BEFORE DEPARTURE LGA AIRCRAFT SWAP. REPLACED AUXILIARY POWER U
- [SDR TAOA039804](https://openairdocs.org/sdr/TAOA039804), Mar 16, 1998: BATTERY PACK. DISCHARGED. FLT 6141 - BOS-LGA - RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK AND BASE ASSEMBLY, OPERATIONAL CHECK NORMAL. (M)
- [SDR TAOA129707](https://openairdocs.org/sdr/TAOA129707), Dec 25, 1997: CHAIN. FAILED. FLT 6140 - LGA-BOS - THE STABILIZER TRIM FAILED. A LOUD BANG WAS HEARD WHEN THE TRIM WAS ELECTRICALLY OPERATED. BICYCLE CHAIN THAT RUNS FROM THE MANUAL CONTROL 
- [SDR TAOA079707](https://openairdocs.org/sdr/TAOA079707), Jul 12, 1997: SMOKE DETECTOR. FAILED. FLT 6141 - AFT LEFT HAND LAVATORY SMOKE DETECTOR INOPERATIVE, NO TEST. REPLACED LEFT HAND LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. (X)
- [SDR TAOA079706](https://openairdocs.org/sdr/TAOA079706), Jul 12, 1997: SMOKE DETECTOR. FAILED. FLT 6080 - AFT LAVATORY SMOKE DETECTOR WARNING SOUNDED FOR NO APPARENT REASON AND THEN SILENCED ITSELF. REPLACED LEFT HAND LAVATORY SMOKE DETECTOR, OPERATIONAL 
- [SDR TAOA079705](https://openairdocs.org/sdr/TAOA079705), Jul 12, 1997: SMOKE DETECTOR. FAILED. FLT 6101 - AFT LAVATORY SMOKE DETECTOR SOUNDED INTERMITTENTLY. REPLACED AFT LEFT HAND LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK NORMAL. (X)
- [SDR TAOA079704](https://openairdocs.org/sdr/TAOA079704), Jul 8, 1997: BATTERY PACK. DISCHARGED. FLT 6100 - BOS - AFT SECTION OF EMERGENCY PATH LIGHTING FOUND INOPERATIVE ON A-3 CHECK. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. (M)
- [SDR TAOA079703](https://openairdocs.org/sdr/TAOA079703), Jul 6, 1997: SMOKE DETECTOR. FAILED. INFLIGHT THE RIGHT AFT LAV SMOKE DETECTOR SOUND, NO EVIDENCE OF SMOKE. REPLACED AFT RIGHT LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL IAW MM 26-10-0. (M)
- [SDR TAOA069706](https://openairdocs.org/sdr/TAOA069706), Jun 20, 1997: SMOKE DETECTOR. MALFUNCTIONED. AFT LAVATORY SMOKE DETECTOR GOES OFF INTERMITTENTLY. FOUND SMOKE DETECTOR TOO SENSITIVE. REPLACED SMOKE DETECTOR PER MM 26-10-00. (X)
- [SDR TAOA129604](https://openairdocs.org/sdr/TAOA129604), Dec 8, 1996: BATTERY PACK. DISCHARGED. FORWARD ENTRY AISLE EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPERATION CHECK NORMAL. (M)

All 59: https://openairdocs.org/deregistered/N924TS-2013-09-16/reports.md

## Other aircraft with N924TS

- [Registered now](https://openairdocs.org/aircraft/N924TS): Beechcraft B200GT, S/N BY-186, built 2013

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