# N375FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2024
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas MD-10-10F](https://openairdocs.org/model/mcdonnell-douglas-md-10-10f) (registry code 3022112)
- Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46613
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 4, 2005
- Certificate issued: April 16, 1998
- Last registry action: October 20, 2023
- Mode S code: A446E0
- Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N375FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=375FE
- Page: https://openairdocs.org/deregistered/N375FE-2024-03-02

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 Mcdonnell Douglas MD-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (127, newest 50)

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

- [SDR FDEA2023012312917](https://openairdocs.org/sdr/FDEA2023012312917), Nov 10, 2019: CABLE. FRAYED. REISSUED PREVIOUS MEL, REF 52-10-9523. L1 DOOR CABLE. MEL 10NOV19 18:20 MEM U RELEASED FOR SERVICE PER MEL : 52-10-02-01 CATEGORY : C EXPIRATION : 20NOV19 "MEL 
- [SDR FDEA201908091822](https://openairdocs.org/sdr/FDEA201908091822), Aug 9, 2019: WIRE HARNESS. FAILED. PASSING 12000 AT 302 KTS WITH CLIMB POWER SELECTED. NR 2 ENGINE EGT ROSE QUICKLY TO 1077 DEGREE, THEN FLUCTUATED FOR 2 SECONDS. PULLED THROTTLE TO IDLE AND EGT 
- [SDR FDEA2019080211783](https://openairdocs.org/sdr/FDEA2019080211783), Aug 1, 2019: COALESCER BAG. ODOR. ELECTRICAL SMELLING SMOKE IMMNATED FROM CAPTAIN SIDE OF COCKPIT @ CRUISE LEVEL 360. SMOKE LASTED APPROX 2-3 MINUTES AND THEN DISIPATED. PERFORMED DUCT CLEANING 
- [SDR FDEA2019041640792](https://openairdocs.org/sdr/FDEA2019041640792), Apr 14, 2019: BATTERY. INOPERATIVE. DURING PRE FLIGHT LEFT SIDE RAFT LIGHT DID NOT TEST. REPLACED THE BATTERIES.
- [SDR FDEA201902150420](https://openairdocs.org/sdr/FDEA201902150420), Feb 15, 2019: CYLINDER. FAILED. AFTER T/O, RECEIVED LT LG MAIN GEAR UNSAFE INDICATION ON PRIMARY AND SECONDARY GEAR RETRACTION GEAR INDICATION. RAN QRH, GEAR PRIMARY OR SECONDARY LIGHTS ILLUMI
- [SDR FDEA201902070265](https://openairdocs.org/sdr/FDEA201902070265), Feb 7, 2019: SENSOR. OUT OF ALIGNMENT. PDIS 375 32-60 8663 06FEB19 LAX FACT U LOGPAGES:3071618 AFTER T/O, L MAIN GEAR UNSAFE UP. RAN QRH. STILL UNSAFE. SHGN 06FEB19 21:39 LAX U SWUNG GEAR 20 TIMES, U
- [SDR FDEA201808172070](https://openairdocs.org/sdr/FDEA201808172070), Aug 17, 2018: SKIN. GOUGED. FUSELAGE SKIN GOUGED, COVERED BY THE RR BODY FAIRING, AT THE MID SECTION. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIG 6, VOL 1, 53-00-01, FIG.1A, HFEC IAW NTSPM
- [SDR FDEA2018081412010](https://openairdocs.org/sdr/FDEA2018081412010), Aug 11, 2018: HINGE. WORN. CENTER CARGO DOOR FWD HINGE LOBE DIAMETER, FUSELAGE SIDE, EXCEEDED ITS WEAR LIMITS. REMOVED AND REPLACED CENTER CARGO DOOR FWD HINGE IAW AMM 52-32-04-2, AND SRM
- [SDR FDEA201804070927](https://openairdocs.org/sdr/FDEA201804070927), Apr 7, 2018: SWITCH. FAILED. DURING PREFLIGHT OF PUSH TO TEST SWITCH FOR THE R1 DOOR, THE SWITCH BROKE INTO PIECES.
- [SDR FDEA201803220759](https://openairdocs.org/sdr/FDEA201803220759), Mar 22, 2018: COALESCER BAG. DIRTY. DURING DESCENT THRU 13000 FT, FUMES FROM PACKS WERE EXCESSIVE. FOLLOWED QRH, NR 1 & 2 PACKS WERE ON. FIRST OFFICER DETECTED A MUSTY ODOR. REMOVED AND REPLACED D
- [SDR FDEA201710243035](https://openairdocs.org/sdr/FDEA201710243035), Oct 24, 2017: PUMP. MALFUNCTIONED. NR 2 ENGINE WOULD NOT ACHIEVE CLIMB POWER. THE THROTTLE WAS FIRE WALLED DURING CLIMB, ALL INDICATIONS CONSISTANTLY LESS THAN 1 & 3. REMOVED AND REPLACED THE NR 
- [SDR FDEA201708012091](https://openairdocs.org/sdr/FDEA201708012091), Aug 1, 2017: SLIDE. FAILED. WHILE TRYING TO PUT NEW ARD ON ACFT, FOUND L1 DOOR ARMED WENT THRU L2 DOOR AND AFTER TRYING TO RESET L1 DOOR BOTTLE BLEW AND SLIDE FELL OUT OF RETAINER CASE. RE
- [SDR FDEA201705061362](https://openairdocs.org/sdr/FDEA201705061362), May 6, 2017: BOTTLE. LOW PRESSURE. R1 DOOR PNEUMATIC ASSIST BOTTLE HAS NO PRESSUE. REMOVED AND REPLACED THE DOOR ASSIST BOTTLE IAW MM 52-11-07-2. OPS CHECKED GOOD IAW AMM 52-10-01-2.
- [SDR FDEA201606172036](https://openairdocs.org/sdr/FDEA201606172036), Jun 17, 2016: SKIN. CRACKED. LEFT WING, AT THE INBD SLAT AREA, L/E OF WING, THE NR 1 SLAT TRACK CUTOUT IS CRACKED AT THE LOWER INBD CORNER, THE CRACK IS APPROXIMATELY 1" LONG THE CRACK IS N
- [SDR FDEA201606152016](https://openairdocs.org/sdr/FDEA201606152016), Jun 15, 2016: FLOOR PANEL. PUNCTURED. MAIN DECK FLOORBOARD BETWEEN STA 600-670 AND FROM LBL 75.5-LBL102 HAS PUNCTURE ABOARD, SEVERAL INSERTS DAMAGED. FABRICATED FLOOR PANEL ON T16/1211640. REMOVAL A
- [SDR FDEA201507102190](https://openairdocs.org/sdr/FDEA201507102190), Jul 10, 2015: COWLING. ABNORMAL. AIRCRAFT ARRIVED WITH NR 2 ENG LT FAN COWL MISSING. PERFORMED GVI OF FAN COWL ATTACH POINTS, APPEARS THAT FAN COWL HINGES SEPARATED FROM PYLON STRUCTURE WITH CO
- [SDR FDEA201507082172](https://openairdocs.org/sdr/FDEA201507082172), Jul 8, 2015: COWL DOOR. MISSING. AIRCRAFT ARRIVED WITH NR 2 ENG LT FAN COWL MISSING. PERFORMED GVI OF FAN COWL ATTACH POINTS, APPEARS THAT FAN COWL HINGES SEPARATED FROM PYLON STRUCTURE WITH CO
- [SDR FDEA201505101459](https://openairdocs.org/sdr/FDEA201505101459), May 10, 2015: CYLINDER. LEAKING. AFTER TAKEOFF LEVEL 2 ALERT HYD 1 FAIL FLUID GONE IAW AMM 32-52-01-2-0. UPON ARRIVAL INTO GATE FOUND LT NOSE WHEEL STEERING CYLINDER LEAKING HYD FLUID. R & R LT
- [SDR FDEA201504021136](https://openairdocs.org/sdr/FDEA201504021136), Apr 2, 2015: LIGHT. INOPERATIVE. LIGHT INDICATING L1 ENTRY DOOR IS DISARMED & DOES NOT ILLUMINATE WHEN THE DOOR IS DISARMED. RELAMPED L1 ENTRY DOOR, DISARMED LIGHT ASSEMBLY. LIGHT OPERATIONS CH
- [SDR FDEA201411173720](https://openairdocs.org/sdr/FDEA201411173720), Nov 17, 2014: PRESSURE SWITCH. FAILED. WING ANTI-ICE DISAGREE AFTER TAKEOFF, FOLLOWED BY AIR SYS 1 OFF. AFTER CONSULTING MOC & GOC RETURNED. TROUBLESHOOTING IAW FIM 30-11 TASK 801. AIR SYS 1 OFF ALER
- [SDR FDEA201409262804](https://openairdocs.org/sdr/FDEA201409262804), Sep 26, 2014: SWITCH. INOPERATIVE. R1 DOOR ESCAPE SLIDE LOW PRESS INDICATOR PRESS TO TEST LIGHT INOPERATIVE. R & R R1 DOOR PRESS TO TEST SWITCH IAW SWPS. OPERATIONS NOW NORMAL. ACFT OK FOR SERVIC
- [SDR FDEA201408022036](https://openairdocs.org/sdr/FDEA201408022036), Aug 2, 2014: BULB. FAILED. R1 DOOR SLIDE REMOTE PRESSURE, PRESS TO TEST LIGHT NOT ILLUMINATING WHEN PUSHED. REMOVED AND REPLACED BULBS. CHECKED OK IAW AMM 25-61-03-5.
- [SDR FDEA201405130991](https://openairdocs.org/sdr/FDEA201405130991), May 13, 2014: WARNING SYSTEM. FALSE ACTIVATION. ON FINAL GOT NO GEAR DOWN & LOCKED INDICATIONS ON HANDLE OR EAD SYNOPTIC, LIGHTS ALL RED, WENT AROUND, RAN QRH GEAR LIGHTS ALL GREEN AFTER QRH. SUSPECT SWITCH I
- [SDR FDEA201404290888](https://openairdocs.org/sdr/FDEA201404290888), Apr 29, 2014: BUSHING. MISSING. LT MLG UNSAFE AFTER TO. FLASHED ON & OFF DURING QRH CHECKLIST. REVIEWED PSEU CURRENT FAULTS, NONE REPORTED IN FAULT REVIEW. REPORTS OF LT GEAR UP & LATCHED, AB 
- [SDR FDEA201404290887](https://openairdocs.org/sdr/FDEA201404290887), Apr 29, 2014: WARNING SYSTEM. FALSE ACTIVATION. LEFT MAIN GEAR RED LIGHT STAYED ON AFTER RETRACTION. COMPLIED WITH QRH & LIGHT WENT OUT ON SECOND TRY. TROUBLE SHOT IAW FIM 32-30-01. INSPECTED LT MLG HYD COMPO
- [SDR FDEA201402080288](https://openairdocs.org/sdr/FDEA201402080288), Feb 8, 2014: AIU. FAILED. RECEIVED A LEVEL ON, AIR SYS 2 OFF ALERT, FOLLOWED BY A LEVEL 3 AIR MANIFOLD 2 FAIL ALERT IN FLIGHT. RED MANIFOLD LIGHT FOR BLEED AIR 2. IAW QRH, THROTTLE IDLE,
- [SDR FDEA201312183002](https://openairdocs.org/sdr/FDEA201312183002), Dec 18, 2013: UNKNOWN. MALFUNCTIONED. REJECTED TAKEOFF DUE TO CAWS, STABILIZER MOTION, ALERT AT ABOUT 100KTS NOTICED STAB TRIM WAS 0.2 UNITS, GREATER THAN BEFORE TAKEOFF SETTING. ON SUBSEQUENT TAKEO
- [SDR FDEA201311162796](https://openairdocs.org/sdr/FDEA201311162796), Nov 16, 2013: TARGET. CONTAMINATED. LEFT MAIN GEAR UNSAFE ON RETRACTION. BOTH PRIMARY AND SEC. INDICATIONS UNSAFE WITH GEAR HANDLE UP, CYCLED GEAR IAW QRH. 3 SAFE INDICATIONS BOTH PRI AND SEC. ACC
- [SDR FDEA201210013518](https://openairdocs.org/sdr/FDEA201210013518), Oct 1, 2012: PROXIMITY SENSOR. DIRTY. AFTER TAKE OFF, RAISED GEAR. LT MAIN HAD PRIMARY AND SECONDARY UNSAFE INDICATION. COMPLIED WITH QRH PROCEDURE AND CYCLED GEAR. NOW PRIMARY AND SECONDARY INDICAT
- [SDR FDEA201206042073](https://openairdocs.org/sdr/FDEA201206042073), Jun 4, 2012: BLADE. DAMAGED. ON POST FLIGHT, FOUND FOD DAMAGE TO NR 3 ENGINE FAN BLADE WITH BIRD REMAINS VISIBLE. PERFORMED FOD BOROSCOPE INSPECTION IAW MD10 AMM 72-00-00-6-1, FIG 609, ITEM
- [SDR FDEA201205161815](https://openairdocs.org/sdr/FDEA201205161815), May 16, 2012: SHEAR TIE. DAMAGED. AFT LOWER FUSELAGE AT STA 1801 L-51L HAS RIVET HEAD SHEARED. REMOVED FASTENERS AND DAMAGED SHEAR TIE IAW SRM 51-31-01. FABRICATED SHEAR TIE. TREATED, PRIMED AND
- [SDR FDEA201205111798](https://openairdocs.org/sdr/FDEA201205111798), May 11, 2012: SKIN. GOUGED. GOUGES IN RT OTBD FLAP LOWER SKIN WS 500 CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01, L=1.0" X W=.50" X D=.085". FABRICATED DOUBLER IAW SRM 57
- [SDR FDEA201205101786](https://openairdocs.org/sdr/FDEA201205101786), May 10, 2012: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK STA 1381, LBL 75 FOUND TO HAVE BROKEN EARS. REMOVED DAMAGED SEAT TRACK SECTION BS 1371 TO 1409. FABRICATED AND INSTALLED NEW SECTION IAW SR
- [SDR FDEA201104171508](https://openairdocs.org/sdr/FDEA201104171508), Apr 17, 2011: LAMP. INOPERATIVE. BOTH EMERGENCY POWER "OFF" AND "ON" LIGHTS INOPERATIVE REGARDLESS OFF BATTERY SWITCH POSITION. RELAMPED AFFECTED SWITCH LIGHTS IAW AMM 33-11-17-2-0. ALL OPS CHE
- [SDR FDEA201104011277](https://openairdocs.org/sdr/FDEA201104011277), Apr 1, 2011: HANDLE. OUT OF SEQUENCE. DURING PREFLIGHT COULD NOT OPERATE DOOR R1, FOUND THE EMERGENCY BOTTLE HANDLE OUT OF SEQUENCE MEL 01APR11, 03:10 IAD R RELEASED FOR SERVICE IAW MEL: 52-10-03 CA
- [SDR FDEA201103030834](https://openairdocs.org/sdr/FDEA201103030834), Mar 3, 2011: WEB. CRACKED. CTR WHEEL RT SIDE WALL, BETWEEN THE SECOND AND THIRD STATIONS AFT OF THE FWD BULKHEAD APPROX STA 1381 TO 1401. THERE ARE 9 CRACKS IN A DOUBLER. REMOVED AND REPL
- [SDR FDEA201103030832](https://openairdocs.org/sdr/FDEA201103030832), Mar 3, 2011: BULKHEAD. CRACKED. CTR WHEEL WELL, RT SIDE WALL, BETWEEN STA 1381 AND 1401 LIGHTNING HOLE NEAR TOP HAS A CRACK COMING OUT OF IT. VERIFIED BY HFEC REPAIRED CTR WHEEL WELL RT SIDE W
- [SDR FDEA201007272681](https://openairdocs.org/sdr/FDEA201007272681), Jul 27, 2010: SKIN. MISREPAIRED. EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 1979 TO STA 2007 BETWEEN LONGERON 48R AND LONGERON 47L. EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 1979 TO STA 2007 B
- [SDR FDEA201007272680](https://openairdocs.org/sdr/FDEA201007272680), Jul 27, 2010: BULKHEAD. MISREPAIRED. EXISTING REPAIR AT FWD CARGO PRESSURE BULKHEAD STA 595 BETWEEN LONGERON 42R AND LONGERON 43R. EXISTING REPAIR AT FWD CARGO PRESSURE BULKHEAD STA 595 BETWEEN LON
- [SDR FDEA201007272674](https://openairdocs.org/sdr/FDEA201007272674), Jul 27, 2010: SKIN. MISREPAIRED. EXISTING REPAIR AT FUSELAGE LOWER SKIN STA 2007 TO STA 2014 LONGERON 50R. EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. SKIN REPLACEMENT CARRIED OUT IAW DW
- [SDR FDEA201007272679](https://openairdocs.org/sdr/FDEA201007272679), Jul 27, 2010: SKIN. DENTED. FUSELAGE STA 495, BETWEEN LONGERON 25R TO LONGERON 27R, SKIN FOUND WITH DENT AND AN ELONGATED HOLE AFTER EXISTING TEMPORARY REPAIR DOUBLERS REMOVED. FUSELAGE ST
- [SDR FDEA201007262669](https://openairdocs.org/sdr/FDEA201007262669), Jul 26, 2010: SKIN. MISREPAIRED. EXISTING FLUSH REPAIR AT RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE SKIN XFS 289. EVALUATED AND FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. REPAIR CA
- [SDR FDEA201007262672](https://openairdocs.org/sdr/FDEA201007262672), Jul 26, 2010: SKIN. MISREPAIRED. EXISTING REPAIR AT LOWER FUSELAGE SKIN INTERNAL DOUBLER STA 859 L-31R. EXISTING REPAIR AT LOWER FUSELAGE SKIN INTERNAL DOUBLER STA 859 L31R EVALUATED AND FOUND 
- [SDR FDEA201007262668](https://openairdocs.org/sdr/FDEA201007262668), Jul 26, 2010: FLOORBEAM. MISREPAIRED. EXISTING REPAIR AT FORWARD CARGO FLOORBEAM STATION 979. EXISTING REPAIR AT FORWARD CARGO FLOORBEAM STATION 979 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT I
- [SDR FDEA201007262667](https://openairdocs.org/sdr/FDEA201007262667), Jul 26, 2010: FRAME. MISREPAIRED. EXISTING REPAIR AT WASTE TANK COMPARTMENT FRAME STATION 1986 L-50L TO L-50R. PRVIOUSLY ACCOMPLISHED NOT IAN ACCORDANCE WITH SRM REPAIR SCHEME. EXISTING REPAIR R
- [SDR FDEA201007242662](https://openairdocs.org/sdr/FDEA201007242662), Jul 24, 2010: SKIN. UNKNOWN. EXISTING REPAIR AT FUSELAGE UPPER SKIN STA 1771 BETWEEN LONGERON 4R TO LONGERON 5R. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED IAW SRM 53-20-00, FIG 6,
- [SDR FDEA201007242661](https://openairdocs.org/sdr/FDEA201007242661), Jul 24, 2010: SKIN. UNKNOWN. EXISTING REPAIR AT FUSELAGE SKIN LOWER STA 795 BETWEEN LONGERON 49L AND LONGERON 50L. EXISTING REPAIR REMOVED AND REPLACED AS PER SRM 53-20-00 FIG 6 VOL 1 REV 9
- [SDR FDEA201007242660](https://openairdocs.org/sdr/FDEA201007242660), Jul 24, 2010: SKIN. MISREPAIRED. EXISTING REPAIR AT FUSELAGE ABOVE FWD LOWER CARGO DOOR CONTROL PANEL STA 859. FOUND NOT IN ACCORDANCE WITH ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED AND CA
- [SDR FDEA201007242659](https://openairdocs.org/sdr/FDEA201007242659), Jul 24, 2010: SKIN. MISREPAIRED. EXISTING REPAIR AT FUSELAGE SKIN BELLY STA 919, 6 O'CLOCK POSITION. EVALUATED PREVIOUSLY ACCOMPLISHED NOT IAN ACCORDANCE WITH SRM REPAIR SCHEME. EXISTING REPAIR
- [SDR FDEA201007222643](https://openairdocs.org/sdr/FDEA201007222643), Jul 22, 2010: LONGERON. UNKNOWN. EXISTING REPAIR AT FORWARD CARGO STATION 879 TO STATION 899 LONGERON 50R. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED AS PER SRM 53-00-00 FIG 2 VOL I RE

All 127: https://openairdocs.org/deregistered/N375FE-2024-03-02/reports.md

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DEN04IA012](https://openairdocs.org/ntsb/DEN04IA012), Oct 12, 2003: McDonnell Douglas DC-10-10 (N375FE), Denver, CO, incident, minor damage. Probable cause: the manufacturer's improper installation of the inboard slat drive mechanism's lower left hand anti-torque strut, which resulted in the axial migration of the rod-end bearing, the binding of the…
- [NTSB IAD01IA034](https://openairdocs.org/ntsb/IAD01IA034), Mar 6, 2001: McDonnell Douglas DC-10 (N375FE), Boston, MA, incident, minor damage. Probable cause: The inadequate de-ice and preflight inspection procedure of the #2 engine inlet and bellmouth area by company maintenance personnel that resulted in ice ingestion and foreign object damage of the #2…

## FAA accident and incident reports (3)

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 20031012026399I](https://openairdocs.org/incident/20031012026399I), Oct 12, 2003: Doug DC1010 (N375FE), Denver, CO, Minor damage. (-23) During takeoff acceleration, the crew received a take-off warning horn and initiated a rejected take-off. During deceleration, the tower reported via…
- [Incident 20021226034699I](https://openairdocs.org/incident/20021226034699I), Dec 26, 2002: Doug DC1010 (N375FE), Kansas City, MO. (-23) On December 26, 2002 federal express flight 3606 a DC-10 advised a.t.c. that the number one engine was out, an emergency was declared and the aircraft…
- [Incident 20010303003559I](https://openairdocs.org/incident/20010303003559I), Mar 3, 2001: Doug DC1010 (N375FE), Boston, MA, Substantial damage. (-23)Weather: snow and ice ref NE incidnet 2001-444, night IFR

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