# N147AW: 1982 Boeing 737-297, registration cancelled 2014-10-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 17, 2014 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 737-297](https://openairdocs.org/model/boeing-737-297) (registry code 1384480) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22630 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 26, 1982 - Certificate issued: March 28, 2007 - Last registry action: November 19, 2010 - Mode S code: A0BCC6 - Owner when cancelled: [Decatur Properties LLC](https://openairdocs.org/faa-owner/DECATUR%20PROPERTIES%20LLC) - Location: [Margate, NJ](https://openairdocs.org/faa-place/NJ/Margate) - Owner type: Corporation - Owner's area on the map: 39.3264° N, 74.5045° W: Placed by OpenAirDocs at the center of ZIP code 08402, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N147AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=147AW - Page: https://openairdocs.org/deregistered/N147AW-2014-10-17 From the FAA registry file of October 29, 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 737-297: https://openairdocs.org/model/boeing-737-297.md ## Service difficulty reports (54, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR KNNA147071110KACY](https://openairdocs.org/sdr/KNNA147071110KACY), Jul 11, 2010: HYDRAULIC LINE. LEAKING. THE "A" SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT TO KACY (ATLANTIC CITY IAP, NJ). COMPLETED CHECKLIST 6.77 OF THE AFM. - [SDR KNNA20090001](https://openairdocs.org/sdr/KNNA20090001), Apr 3, 2009: SEAL. FAILED. NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO DURING FLIGHT FOLLOWED BY DROP IN OIL PRESSURE LEADING TO ENGINE SHUT DOWN AND DECLARATION OF AN EMERGENCY. IT WAS DISC - [SDR PIDR07001](https://openairdocs.org/sdr/PIDR07001), Aug 24, 2007: SKIN. CRACKED. CRACK IN THE FUSELAGE SKIN AT BS 727B+4 AT STR 17 RT WAS REPAIRED BY REPLACING THE DAMAGED SECTION OF SKIN FROM BS 727 TO BS 757 FROM STR 14 RT TO STR 20 RT DUE - [SDR PIDR07002](https://openairdocs.org/sdr/PIDR07002), Aug 24, 2007: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AT BS 727A+14.5 AT STR 17 LT WAS REPAIRED BY REPLACING SECTION OF SKIN FROM BS 727A +8 TO BS 767 FROM STR 16 LT TO STR 18 LT DUE TO PROXI - [SDR PIDR07003](https://openairdocs.org/sdr/PIDR07003), Aug 24, 2007: STRINGER. DAMAGED. STRINGER 16 RT AT BS 727B HAS A DAMAGED FASTENER HOLE. REPAIRED IN ACCORDANCE WITH SRM 53-10-3 FIGURE 2. - [SDR KNNA200700011](https://openairdocs.org/sdr/KNNA200700011), Feb 5, 2007: FRAME. MISDRILLED. FOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FASTENER HOLE BS 178 W/L 212. - [SDR KNNA200700018](https://openairdocs.org/sdr/KNNA200700018), Jan 25, 2007: FRAME. CRACKED. FOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212. - [SDR KNNA200700017](https://openairdocs.org/sdr/KNNA200700017), Jan 25, 2007: VERTICAL BEAM. CRACKED. FOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178. - [SDR KNNA200700015](https://openairdocs.org/sdr/KNNA200700015), Jan 25, 2007: BULKHEAD. CRACKED. FOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12. - [SDR KNNA200700014](https://openairdocs.org/sdr/KNNA200700014), Jan 25, 2007: FRAME. CRACKED. FOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE (RIGHT SIDE) SIDE CHORD AT WL 212. - [SDR KNNA200700012](https://openairdocs.org/sdr/KNNA200700012), Jan 25, 2007: BULKHEAD. CRACKED. FOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213 - [SDR KNNA200700010](https://openairdocs.org/sdr/KNNA200700010), Jan 25, 2007: BULKHEAD. CRACKED. FOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 . - [SDR KNNA200700013](https://openairdocs.org/sdr/KNNA200700013), Jan 19, 2007: SKIN. DAMAGED. E/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR . - [SDR KNNA200700016](https://openairdocs.org/sdr/KNNA200700016), Jan 12, 2007: STRINGER SPLICE. ACTIVE. FOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75. - [SDR KNNA200300001](https://openairdocs.org/sdr/KNNA200300001), Feb 24, 2003: SKIN. CRACKED. AIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON- - [SDR 2001F00633](https://openairdocs.org/sdr/2001F00633), Jan 26, 2001: TIRE. SEPARATED. LOSS OF A SYSTEM HYDRAULICS. LEFT INBOARD TIRE LOST TREAD DURING TAKEOFF ROLL. PIECES OF THE TIRE TREAD DAMAGED HYDRAULIC LINES AND CONTROL CABLES LOCATED IN TH - [SDR AWXA9900373](https://openairdocs.org/sdr/AWXA9900373), Oct 21, 1999: POWER SUPPLY. INOP. CONDITION: NON-ROUTINE-- EMER LTNG LOG 3203678DISCREPANCY: EMERGENCY LIGHTS ROW 6 THROUGH 14 INOPCORRECTIVE ACTION: REPLACED POWER SUPPLY AND BATTERYCURRENT HIS - [SDR AWXA9900137](https://openairdocs.org/sdr/AWXA9900137), Apr 14, 1999: ENGINE. FAILED. AIR TURNBACK, ENGINE SHUT DOWN. ON CLIMBOUT OIL TEMP ON NR 1 ENG WAS IN THE RED BAND. ENGINE WAS SHUTDOWN INFLIGHT PER QRH. DRAINED 1 GALLON ENGINE OIL FROM NR - [SDR AWXA9800237](https://openairdocs.org/sdr/AWXA9800237), Dec 17, 1998: PCU. LEAKS. INBOUND TO LAX, LOST 'B' SYSTEM HYDRAULIC FLUID. DECLARED EMERGENCY. REMOVED AND REPLACED RUDDER PCU FOR LEAKING. ADDITIONAL INFORMATION TO FOLLOW, TO INCLUDE T - [SDR AWXA9800229](https://openairdocs.org/sdr/AWXA9800229), Dec 1, 1998: ACTUATOR. MALFUNCTIONED. CABIN FLOORBEAM STA 696 LBL 63 FLOORBEAM WEB IS CRACKED, MARKED NR 38. RESEARCHED, NOT A REPAIR IN THE SRM MAPPED AREA AND SENT TO ENGINEERING REF LOG 5082720. - [SDR AWXA9800163](https://openairdocs.org/sdr/AWXA9800163), Jul 29, 1998: CONNECTOR. LOOSE. NR 2 FIRE WARNING LIGHT AND BELL WENT OFF ABOUT 50 MILES PRIOR TO LAND QRH PROCEDURES COMPLETE AND ENGINE SECURED. BOTH FIRE BOTTLES EXPENDED INTO NR 2 ENGINE. - [SDR AWXA9800146](https://openairdocs.org/sdr/AWXA9800146), Jun 18, 1998: SKIN. CRACKED. D-FUSELAGE CRACK AT STA 727 NEAR STRINGER 17 RT SIDE C-CONFIRMED BY HFEC AND REPAIRED PER SRM 53-30-03 FIG 1. - [SDR 99ZZZX1821](https://openairdocs.org/sdr/99ZZZX1821), May 4, 1998: VALVE. MISOVERHAULED. RED, TI-TEMP RTV HAS BEEN APPLIED IN THE THROAT OF THE HOUSING AROUND THE BUTTERFLY SEAL SEAT. THIS BUTTERFLY SEAL IS DESIGNED TO FLOAT IN THE HOUSING, BUT IN T - [SDR AWXA9800003](https://openairdocs.org/sdr/AWXA9800003), Jan 6, 1998: WIRE. LOOSE. SEAT 1L EMERGENCY LIGHT INOP. RECONNECTED WIRE HARNESS, OPS GOOD. STC NR SA3432NM - [SDR AWXA9700707](https://openairdocs.org/sdr/AWXA9700707), Dec 26, 1997: LIGHT. LOOSE. PST DECK EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, GRD OPS OK. STC NR SA3432NM - [SDR AWXA9700613](https://openairdocs.org/sdr/AWXA9700613), Oct 17, 1997: MEGAPHONE. INOPERATIVE. DURING ROUTINE MAINTENANCE CHECK, FOUND AFT EMERGENCY MEGAPHONE INOP. REMOVED AND REPLACED MEGAPHONE. - [SDR AWXA9700557](https://openairdocs.org/sdr/AWXA9700557), Sep 13, 1997: LIGHT. COVER MISSING. DURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OPS TEST GOOD. STC - SA - [SDR AWXA9700556](https://openairdocs.org/sdr/AWXA9700556), Sep 12, 1997: SOLENOID. FAILED. L/G HANDLE WOULD NOT MOVE PAST OFF ON TAKEOFF. CYCLED HANDLE DOWN AND BACK TO NO AVAIL. USED RED TRIGGER TO RETRACT GEAR. REMOVED AND REPLACED LANDING GEAR LEVE - [SDR AWXA9600769](https://openairdocs.org/sdr/AWXA9600769), Dec 20, 1996: WIRE. BROKEN. DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 13 INOPERATIVE. REPAIRED SEAT WIRING. OPS GOOD. STC - SA3432NM. - [SDR 97ZZZX111](https://openairdocs.org/sdr/97ZZZX111), Dec 19, 1996: DRAG BRACE. DAMAGED. DRAG BRACE SENT TO BFG FOR REPAIR. FOUND BEARING MIGRATED FROM LOCATION CAUSING DAMAGE TO BRACE DURING GEAR ACTUATION. BEARING INSTALLATION RECORDS NOT AVAILABL - [SDR AWXA960608](https://openairdocs.org/sdr/AWXA960608), Nov 12, 1996: FUEL HEAT VLV. LOOSE WIRING. TUS - FLT 2062 - PILOT SHUT DOWN NR 1 ENGINE DUE TO HIGH OIL TEMP. PILOT CYCLED FUEL HEAT VALVE SUSPECTING IT MAY BE PARTIALLY OPEN, VALVE APPARENTLY FAILED TO - [SDR AWXA9600667](https://openairdocs.org/sdr/AWXA9600667), Nov 11, 1996: LIGHT. INOP. PHX - FLT 2455 - DURING ROUTINE MAINTENANCE INSPECTION, FOUND L-1 DOOR EMERGENCY EXIT LIGHT (OUTER DOOR) DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXI - [SDR AWXA960598](https://openairdocs.org/sdr/AWXA960598), Oct 17, 1996: CONNECTOR. LOOSE. PHX - FLT 2245 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT OVERWING WINDOW EXIT INOP. RECONNECTED CONNECTOR ON BATTERY PACK. OPS CHECK GOOD. - [SDR AWXA960422](https://openairdocs.org/sdr/AWXA960422), Aug 7, 1996: WIRE. BROKEN. PHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 11 EMERGENCY LIGHT INOP. REPAIRED WIRE. OPS CHECK OK. (M) - [SDR AWXA960014](https://openairdocs.org/sdr/AWXA960014), Jan 11, 1996: DUCT ASSY. CRACKED. PHX/SJC - FLT 0870 - DURING CLIMB-OUT, NR 1 ENGINE FIRE LIGHT CAME ON. (NR 1 OVHT DET CURRENTLY ON MEL 26-02.) THE FIRE DET SYSTEM WOULD NOT TEST IN EITHER NORM - [SDR AWXA9500790](https://openairdocs.org/sdr/AWXA9500790), Nov 29, 1995: TRACK. WORN. PHX - FLT NR 417 - PHX/COS - AIR TURN BACK - AIRCRAFT ROLLED TO THE LEFT AND REQUIRED 15 TO 20 DEGREE RIGHT AILERON TO CORRECT. SITUATION CORRECTED AFTER FLAPS - [SDR AWXA9500773](https://openairdocs.org/sdr/AWXA9500773), Nov 19, 1995: WIRE. BROKEN. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 1L. REPAIRED WIRES, OPS CHECK GOOD. (M) - [SDR AWXA9500730](https://openairdocs.org/sdr/AWXA9500730), Nov 1, 1995: PITOT TUBE. HEAT INOP. PHX/DEN - FLT NR 499 - AIR TURNBACK DUE TO LEFT ELEVATOR PITOT HEAT LIGHT ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDEN - [SDR AWXA9500668](https://openairdocs.org/sdr/AWXA9500668), Sep 30, 1995: EEL BATTERY PACK. DISCHARGED. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT EMERGENCY EXIT LIGHT IDENTIFIER INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD BATTERY PACK, SYSTEM OPS CHECK - [SDR AWXA9500663](https://openairdocs.org/sdr/AWXA9500663), Sep 21, 1995: SKIN. CRACKED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT L2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. FABRICATED AND INSTALLED DOUBLER - [SDR AWXA9500661](https://openairdocs.org/sdr/AWXA9500661), Sep 21, 1995: PANEL. CRACKED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND A .75 INCH CRACK IN LEFT SIDE OF KEEL BEAM SKIN AT STATION 685 BL 0. FABRICATED AND INSTALLED REPLACEMENT PANEL PER - [SDR AWXA9500660](https://openairdocs.org/sdr/AWXA9500660), Sep 21, 1995: SHEAR TIE. CORRODED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON SHEAR TIE AT STATION 930, OUTBOARD OF STRINGER 28L IN AFT CARGO PIT. FABRICATED AND INST - [SDR AWXA9500659](https://openairdocs.org/sdr/AWXA9500659), Sep 21, 1995: STRINGER. CORRODED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON STRINGER 28L BS 910 IN AFT CARGO PIT. FABRICATED AND INSTALLED NEW STRINGER PER SRM 53-1 - [SDR AWXA9500658](https://openairdocs.org/sdr/AWXA9500658), Sep 21, 1995: FLOOR BEAM. CORRODED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND AFT CABIN FLOOR BEAM AT STATION 947 RBL 5 TO RBL 6 CORRODED BEYOND LIMITS. REPAIRED BEAM PER SRM 53-10-9. (M) - [SDR AWXA9500657](https://openairdocs.org/sdr/AWXA9500657), Sep 21, 1995: ANGLE. CRACKED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN LT SIDE OF ZERO FLOOR SUPPORT ANGLE AT STATION 540 BL 0. INSTALLED NEW SUPPORT ANGLE PER SRM 51-10-1 AND S - [SDR AWXA9500656](https://openairdocs.org/sdr/AWXA9500656), Sep 21, 1995: HINGE CUTOUT. CRACKED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND A CRACK IN L1 DOOR SKIN AT UPPER HINGE CUTOUT UPPER CORNER. ROUTED OUT CRACK PER SRM 52-00-2, PAGE 34. (M) - [SDR AWXA9500655](https://openairdocs.org/sdr/AWXA9500655), Sep 21, 1995: SKIN. CRACKED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND TWO CRACKS IN RT SIDE OF KEEL BEAM SKIN. A 2 INCH CRACK FOUND AT STATION 685 BL ZERO AND A 1.5 INCH CRACK FOUND AT - [SDR AWXA9500654](https://openairdocs.org/sdr/AWXA9500654), Sep 21, 1995: STRINGER. CORRODED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND STRINGER 28L AT BS 910 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED STRINGER PER SRM 53-10-3. (M) - [SDR AWXA9500653](https://openairdocs.org/sdr/AWXA9500653), Sep 21, 1995: STRINGER. CRACKED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN FUSELAGE FRAME AT BS 360 BETWEEN STRINGER 20L AND STRINGER 21L. STOP DRILLED CRACK AND REPAIRED PER EO 53- - [SDR AWXA9500652](https://openairdocs.org/sdr/AWXA9500652), Sep 21, 1995: FLOOR BEAM. CORRODED. PHX - DURING SCHEDULED C13 INSPECTION, FOUND AFT GALLEY FLOOR BEAM TOP CAP AT STATION 986.5 RBL 17 CORRODED BEYOND LIMITS. REMOVED AND REPLACED T-CAP PER SRM 53 All 54: https://openairdocs.org/deregistered/N147AW-2014-10-17/reports.md ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19910720037999I](https://openairdocs.org/incident/19910720037999I), Jul 20, 1991: Boeing 737297 (N147AW), Wichita, KS. Passenger complained of shortness off breath. Medical service alerted and met aircraft on arrival. - [Incident 19900527025869I](https://openairdocs.org/incident/19900527025869I), May 27, 1990: Boeing 737297 (N147AW), Fresno, CA. Aft lavatory smoke alarm came on. Odor of burning wire. Diverted for landing. Light ballast had failed. ## Other aircraft with N147AW - [Registered now](https://openairdocs.org/aircraft/N147AW): Scoda Aeronautica Ltda SUPER PETREL LS, S/N S0377, built 2020 --- 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.