# N141AW: Bradford Heinitz AW 95 - Status: Valid registration - Airframe: [Bradford Heinitz AW 95](https://openairdocs.org/model/bradford-heinitz-aw-95) (registry code 056311D, 1 seats) - Serial number: 100-1 - Type: Rotorcraft - Engine type: 2 cycle - Certificate issued: January 20, 2022 - Expires: January 31, 2029 - Mode S code: A0A67C - Registered owner: [Heinitz Bradford C](https://openairdocs.org/faa-owner/HEINITZ%20BRADFORD%20C) - Location: [Arlington, WA](https://openairdocs.org/faa-place/WA/Arlington) - Owner type: Individual - Owner's area on the map: 48.2171° N, 121.9535° W: Placed by OpenAirDocs at the center of ZIP code 98223, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=141AW - Page: https://openairdocs.org/aircraft/N141AW From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Bradford Heinitz AW 95) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N141AW. ## FAA accident and incident reports None matched to N141AW. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N141AW not matched to an aircraft (60, newest 50) They name N141AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AWXA200601286](https://openairdocs.org/sdr/AWXA200601286), Jul 19, 2006: WIRE HARNESS. DAMAGED. SAL - EEL - MAINTENANCE EMERGENCY EXIT LIGHT INOP SEAT ROW 9. EMERGENCY EXIT LIGHT INOP SEAT ROW 9 WAS CORRECTED. REMOVED AND REPLACED SEAT HARNESS, OPS GOOD. - [SDR AWXA9900477](https://openairdocs.org/sdr/AWXA9900477), Dec 16, 1999: BATTERY PACK. DISCHARGED. ROW 6-14 EMERGENCY EXIT LIGHTS DID NOT WORK DURING TEST. BATTERY CHARGED BY CONTRACT MAINTENANCE PREVIOUS FLIGHT. REPLACED AFT EMERGENCY LIGHT BATTERY PACK IN D - [SDR AWXA9900400](https://openairdocs.org/sdr/AWXA9900400), Nov 7, 1999: WIRE. BROKEN. EMERGENCY LIGHT INOP, ROW 4. REPAIRED BROKEN WIRE, OPS CK NML. - [SDR AWXA9900337](https://openairdocs.org/sdr/AWXA9900337), Jun 10, 1999: RIB. CRACKED. C-CHECK, 2 INCH CRACK ON I/B UPPER ANGLE ON LEADING EDGE INT OF I/B FRAME AT WS 185.5 RT WING OF PYLON. REMOVED, FABRICATED, HEAT TREATED TO T3 COND, ALODINED A - [SDR AWXA9900340](https://openairdocs.org/sdr/AWXA9900340), Jun 3, 1999: TIE CLIP. CRACKED. C-CHECK, STRINGER TIE CLIP CRACKED, 16L FS 727A. REMOVED STRINGER TIE CLIP IAW SRM 51-30-2, FAB'D NEW STRINGER TIE CLIP IAW 51-10-1. TREATED AND PRIMED NEW CLIP - [SDR AWXA9900341](https://openairdocs.org/sdr/AWXA9900341), Jun 2, 1999: ANGLE. CRACKED. C-CHECK, .75 INCH CRACK ON UPPER ANGLE OF LT WING L/E RIB I/B SIDE OF NR 1 ENG PYLON. FABRICATED AND INSTALLED REPAIR PART AT WING STA 185.5 IAW 51-30-00, MATER - [SDR AWXA9900339](https://openairdocs.org/sdr/AWXA9900339), Jun 2, 1999: SKIN. CRACKED. C-CHECK, APPROX 2.5 INCH CRACK ON FUSLAGE SKIN 3.5 FT BELOW L-2 DOOR. REMOVED EXISTING DOUBLER PER SRM 51-40-2, CUTOUT DAMAGE PER PT6 51-00-00 FIG 23. FABRICATE - [SDR AWXA9900338](https://openairdocs.org/sdr/AWXA9900338), Jun 2, 1999: SKIN. CRACKED. C-CHECK, LT FUSLAGE CRACK AT SR17L. ALSO, LT WTB BETWEEN 2ND AND 3RD REPAIR, 4 TO 5 INCHES LONG. BOTH PLACES FABRICATED NEW REPAIR FROM 2024T3 .090 R646704 IAW - [SDR AWXA9900047](https://openairdocs.org/sdr/AWXA9900047), Feb 19, 1999: SKIN. CRACKED. DURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK LEFT SIDE AT STRINGER 17, BS 727, BELOW TEMP REPAIR FWD OF BS 747. INSTALLED REPAIR USING BLIND FA - [SDR AWXA9900046](https://openairdocs.org/sdr/AWXA9900046), Feb 19, 1999: SKIN. CRACKED. DURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK BELOW STRINGER 16 RT SIDE, AFT OF WING TO BODY FAIRING FROM STATION 747 TO 767. REPAIRED PER ER 2- - [SDR AWXA9900045](https://openairdocs.org/sdr/AWXA9900045), Feb 19, 1999: SKIN. CRACKED. DURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK AT STRINGER 19 RT SIDE AT BS 727 TO 747. REPAIRED PER ER 2-53-34-08 STEP 8, NEED TO REPLACE SKIN O - [SDR AWXA9900012](https://openairdocs.org/sdr/AWXA9900012), Jan 7, 1999: BATTERY PACK. DISCHARGED. RT EMERGENCY EXIT LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK, OPS CK GOOD. - [SDR AWXA9800078](https://openairdocs.org/sdr/AWXA9800078), Mar 14, 1998: POWER SUPPLY. INOPERATIVE. EMERG EXIT LIGHT CENTER AISLE OVERWING WON'T LIGHT WITH OTHER EXIT LIGHTS. REMOVED AND REPLACED BATTERY PWR SUPPLY UNIT, OPS CKD NORMAL. STC NR SA3432NM. - [SDR AWXA9700391](https://openairdocs.org/sdr/AWXA9700391), Jul 9, 1997: LIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLASHLIGHT INOP AT L-2 DOOR. REMOVED ANDANDREPLACED L-2 DOOR EMERGENCY FLASHLIGHT & HOLDER. - [SDR AWXA9700338](https://openairdocs.org/sdr/AWXA9700338), Jun 11, 1997: BATTERY PACK. DISCHARGED. DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. STC - SA3432NM. - [SDR AWXA9700329](https://openairdocs.org/sdr/AWXA9700329), Jun 6, 1997: CONNECTOR. INOPERATIVE. DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT ROW 1 TO 5 EMERGENCY LIGHTS WILL NOT EXTINGUISH WITH EMERGENCY LIGHT SWITCH OFF AND SHIP'S POWER OFF. INSTALLED NEW - [SDR AWXA9700302](https://openairdocs.org/sdr/AWXA9700302), May 26, 1997: BATTERY PACK. DISCHARGED. DURING ROUTINE MAINTENANCE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS COME ON WHEN BATTERY TURNED OFF. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOO - [SDR AWXA9700233](https://openairdocs.org/sdr/AWXA9700233), Apr 17, 1997: POSITION IND. INOPERATIVE. UNSCHEDULED LANDING IN LAS. TRAILING EDGE FLAPS SPLIT, 1 AND 5 POSITIONS. REMOVED AND REPLACED FLAP T/E POSITION INDICATOR. CYCLED FLAPS SEVERAL TIMES, OPS CHEC - [SDR AWXA9700244](https://openairdocs.org/sdr/AWXA9700244), Apr 7, 1997: FLOORBEAM. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 312, WL 208, LBL 11 TO RBL 11. REMOVED UPPER CHORD OF FLOORBEAM AT BS 312 FROM - [SDR AWXA9700243](https://openairdocs.org/sdr/AWXA9700243), Apr 7, 1997: FLOORBEAM. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM BS 328, RBL 11 TO 20, WL 208. REMOVED UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED PER SRM - [SDR AWXA9700225](https://openairdocs.org/sdr/AWXA9700225), Mar 25, 1997: BATTERY PACK. DISCHARGED. DURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING CEILING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERWING CEILING EMERGENCY LIGHT BATTERY PACK, OPS CHE - [SDR AWXA9700191](https://openairdocs.org/sdr/AWXA9700191), Mar 20, 1997: RUDDER PCU. MALFUNCTION. RUDDER AND AIRCRAFT SHUDDERED EXCESSIVELY DURING DEFLECTION OF RIGHT RUDDER. LEFT RUDDER DEFLECTION NORMAL. REMOVED AND REPLACED RUDDER PCU AND C/W ADJUSTMENT T - [SDR AWXA9700190](https://openairdocs.org/sdr/AWXA9700190), Mar 18, 1997: BOLTS. LOOSE. VIBRATION NOTED BY INBOUND CREW AT FLAPS 2, RT INBOARD FLAP AREA. FOUND LT AND RT INBOARD FOREFLAP TOGGLE BOLTS LOOSE. TIGHTENED AND RE-SAFETIED BOLTS. ALSO, TI - [SDR AWXA9700175](https://openairdocs.org/sdr/AWXA9700175), Mar 6, 1997: LINE. BLOWN. AIR TURNBACK, LOSS OF SYSTEM-A HYDRAULICS. SHORTLY AFTER TAKEOFF, NR 2 A-HYDRAULIC LOW PRESSURE LIGHT FOLLOWED BY A-SYSTEM QUANTITY TO ZERO. REMOVED AND REPLACE - [SDR AWXA960605](https://openairdocs.org/sdr/AWXA960605), Oct 19, 1996: POWER SUPPLY. INOPERATIVE. PHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GO - [SDR 96ZZZM1484](https://openairdocs.org/sdr/96ZZZM1484), Oct 19, 1996: POWER SUPPLY. INOPERATIVE. PHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GO - [SDR AWXA960592](https://openairdocs.org/sdr/AWXA960592), Oct 14, 1996: POWER SUPPLY. INOPERATIVE. PHX - FLT 2592 - DURING ROUTINE MAINTENANCE CEHCK, FOUND RIGHT OVERWING EXIT INTERIOR EXIT SIGN ON DOOR FRAME INOP. REPLACED BATTERY POWER CHARGER WITH SERVICEA - [SDR AWXA960591](https://openairdocs.org/sdr/AWXA960591), Oct 14, 1996: BATTERY. DISCHARGED. PHX - FLT 2550 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT L1 AND R1 DOORS. REMOVED AND REPLACED BATTERY PACK, OPS NORMAL AT THIS TI - [SDR AWXA960533](https://openairdocs.org/sdr/AWXA960533), Sep 27, 1996: BATTERY PACK. DISCHARGED. PHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR LIGHT SIGNS AT R1, L1 AND RIGHT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK M1050. - [SDR AWXA960521](https://openairdocs.org/sdr/AWXA960521), Sep 21, 1996: CONNECTOR. SHORTED. PHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT EMERGENCY EXIT AFT VERTICAL EXIT LIGHT INOP. FOUND POWER CONNECTOR SHORTING ON A/C FRAME. REPLACE - [SDR AWXA960513](https://openairdocs.org/sdr/AWXA960513), Sep 18, 1996: POWER SUPPLY. INOP. PHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID RIGHT EMERGENCY LIGHT POWER SUPPLY. OPERA - [SDR AWXA960375](https://openairdocs.org/sdr/AWXA960375), Sep 9, 1996: TURBINE BLADE. FAILED. LAS - FLT 2976 - AIR TURN BACK, AT CLIMB POWER FL 200 NR 1 ENGINE COMMENCED SEVERE VIBRATIONS. ALL ENGINE INDICATIONS NORMAL. RETARDED THRUST LEVER. VIBRATIONS - [SDR AWXA960350](https://openairdocs.org/sdr/AWXA960350), Jul 24, 1996: SEAT. NOT SECURED. PHX - FLT 2890 - AIR TURNBACK, SEAT ROW 6 A, B, C, NOT SECURED. SECURED SEAT ROW 6 A, B, C IN SEAT TRACK AS NEEDED. (M) - [SDR AWXA960331](https://openairdocs.org/sdr/AWXA960331), Jul 8, 1996: ENGINE. BIRD STRIKE. LAS - FLT 0981 - ABORTED TAKEOFF. BIRD STRIKE ON TAKEOFF ROLL. LEFT HAND FORWARD PART OF A/C. C/W AWA FORM 382 FOD INSPECTION PARAGRAPH A, SECTIONS 1 AND 2. FOD - [SDR AWXA960320](https://openairdocs.org/sdr/AWXA960320), Jul 5, 1996: ENGINE. OVERTEMP. PHX/ONT - FLT 2622 - AIR TURNBACK. NR 1 ENGINE OIL TEMPERATURE CLIMBED TO 118 DEGREES AT CRUISE, 123 CELSIUS ON DESCENT, 140 CELSIUS FOR 10 MINUTES AT 110 FEET. - [SDR AWXA960255](https://openairdocs.org/sdr/AWXA960255), May 18, 1996: SKIN. DENTED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SMALL DENT AFT OF L-2 DOOR (CENTER OF DOOR, 2 INCH AFT). REFERENCE FORM 106 NR 23581. REP - [SDR SWXA960252](https://openairdocs.org/sdr/SWXA960252), May 15, 1996: SEAT TRACK. CORRODED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 947-967, LBL 25, WL 208. REMOVED AND INSTALLED FABRICATED SEAT - [SDR AWXA960256](https://openairdocs.org/sdr/AWXA960256), May 15, 1996: SKIN. DENTED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SKIN DENTED STATION 1047-1063, STRINGER 18 RT, WL 206. REMOVED DAMAGED SKIN, FABRICATED R - [SDR AWXA960254](https://openairdocs.org/sdr/AWXA960254), May 15, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 947, LBL 0-4, WL 208. REMOVED STRAP AND REPAIRED PER ER 2-53-1 - [SDR AWXA960253](https://openairdocs.org/sdr/AWXA960253), May 15, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 967, LBL 21-19, WL 208. REMOVED DAMAGED AREA AT BS 967, LBL 21 - [SDR AWXA960251](https://openairdocs.org/sdr/AWXA960251), May 15, 1996: SPLICE. CORRODED. FLT 7812 - PAE - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 27, RIGHT SPLICE BS 905. REMOVED STRINGER SPLICE AT BS 905 AND STRI - [SDR AWXA960250](https://openairdocs.org/sdr/AWXA960250), May 14, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 1006, LBL 11, WL 208. REMOVED CORROSION BS 1006, LBL 11, WL 20 - [SDR AWXA960249](https://openairdocs.org/sdr/AWXA960249), May 14, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 986.5, RBL 41, RBL 50, WL 208. REMOVED CORROSION BS 986.5, RBL - [SDR AWXA960158](https://openairdocs.org/sdr/AWXA960158), Mar 25, 1996: ACTUATOR. BROKEN. TUS-PHX - FLT NR 604 - GATE RETURN, A SYSTEM HYDRAULIC FAILURE DURING TAXI. NR 8 SPOILER ACTUATOR BROKEN AT CASTING. REPLACED NR 8 SPOILER ACTUATOR PER CARD R3M - [SDR AWXA960155](https://openairdocs.org/sdr/AWXA960155), Mar 21, 1996: STATIC INVERTER. FAILED. LAS - FLT NR 1931 - AIR TURN BACK, AFTER TAKEOFF LOST NAVIGATION AND COMMUNICATION ON CAPTAINS SIDE. REMOVED AND REPLACED STATIC INVERTER AND R-36 RELAY IN P-6. - [SDR AWXA960132](https://openairdocs.org/sdr/AWXA960132), Mar 12, 1996: SEALANT. FAILED. FLT NR 510 - PHX-OMA - AIR TURN BACK, WINDOW NR 1 REPAIR TAPE AND SEALANT BLEW OUT PASSING THROUGH 230K. PRESSURIZATION OK, BUT WINDOW SCREEN WIND NOISE OUITE B - [SDR AWXA960031](https://openairdocs.org/sdr/AWXA960031), Jan 24, 1996: STRUT. LOW PRESSURE. DEN/PHX - FLT 0491 - ABORTED TAKEOFF. ON TAKEOFF ROLL, FELT LIKE AIRCRAFT HAD FLAT TIRE AND AIRCRAFT NEEDED LEFT RUDDER TO STAY STRAIGHT. CONTRACT MAINTENANCE C - [SDR AWXA9500766](https://openairdocs.org/sdr/AWXA9500766), Nov 16, 1995: SKIN. CRACKED. LAS - FLT NR 067 - ON WALK AROUND INSPECTION, FOUND A 2.375 INCH CRACK IN FUSELAGE SKIN, AT STATION 947 STRINGER 18L. REPAIRED IAW SRM 53-30-03, FIGURE 6. (M) - [SDR AWXA9500751](https://openairdocs.org/sdr/AWXA9500751), Nov 11, 1995: BATTERY. DISCHARGED. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR AND R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AT L1 DOOR, OPS CHECK - [SDR AWXA9500576](https://openairdocs.org/sdr/AWXA9500576), Aug 23, 1995: EEL ASSY. INOPERATIVE. PHX - DURING ROUTINE MAINTENANCE CEHCK, FOUND EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE AT L2 DOOR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHEC All 60: https://openairdocs.org/aircraft/N141AW/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N141AW The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N141AW before. - [Cancelled 2008-06-05](https://openairdocs.org/deregistered/N141AW-2008-06-05): Agusta AW139, S/N 41011. Exported to United Arab Emirates. Owner: [Agusta Aerospace Corp](https://openairdocs.org/faa-owner/AGUSTA%20AEROSPACE%20CORP), [Philadelphia, PA](https://openairdocs.org/faa-place/PA/Philadelphia) ## Related - Other Bradford Heinitz AW 95 aircraft: https://openairdocs.org/model/bradford-heinitz-aw-95/aircraft.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.