# N372AA: 1987 Sikorsky EH-60A

- Status: Valid registration
- Airframe: [Sikorsky EH-60A](https://openairdocs.org/model/sikorsky-eh-60a) (registry code 8141900, 4 seats)
- Engine: [GE T700 series](https://openairdocs.org/engine/ge-t700-series) (registry code 30029)
- Serial number: 87-24672
- Year built: 1987
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Restricted, agriculture and pest control, forest, other
- Airworthiness date: February 22, 2022
- Certificate issued: May 3, 2021
- Expires: May 31, 2028
- Mode S code: A43B3A
- Registered owner: [Hawk Aviation LLC](https://openairdocs.org/faa-owner/HAWK%20AVIATION%20LLC)
- Location: [Broomfield, CO](https://openairdocs.org/faa-place/CO/Broomfield)
- Owner type: LLC
- Owner's area on the map: 39.8907° N, 105.1137° W: Placed by OpenAirDocs at the center of ZIP code 80021, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=372AA
- Page: https://openairdocs.org/aircraft/N372AA

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. The registry lists only the engine series, so ADs for every GE T700 model are included.

## ADs that may apply (OpenAirDocs): 1 in force

### Matched by airframe (Sikorsky EH-60A)

- [AD 2020-22-19](https://openairdocs.org/ad/2020-22-19): Main Rotor Head--Main Rotor Spindle Cuff · ACE Aeronautics UH-60A, BHI H60 (UH-60A), UH-60A and 17 more. Effective Dec 3, 2020

### Matched by engine (GE T700 series)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N372AA.

## FAA accident and incident reports

None matched to N372AA.

## Reports on N372AA not matched to an aircraft (2)

They name N372AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19951004039599I](https://openairdocs.org/incident/19951004039599I), Oct 4, 1995: Boeing 767 (N372AA), Chicago, IL. Narrative: flt. 136 from lax to london, england encountered lt. to mod. Turbulence over rock-springs, WY. F/a was injured with possible concusion. No…
- [Incident 19930627020529I](https://openairdocs.org/incident/19930627020529I), Jun 27, 1993: Boeing 767323 (N372AA), Raleigh-Durham, NC, Minor damage. Flew through moderate turbulance. Four flight attendants injuried. Diverted to Raleigh. Landed safely.

## 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 N372AA not matched to an aircraft (101, newest 50)

They name N372AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MK1Y20171129001](https://openairdocs.org/sdr/MK1Y20171129001), Nov 29, 2017: SKIN. DENTED. DENT ON EXTERNAL FUSELAGE STA 1241 TO 1285 AND BETWEEN STR 33L TO 34L.
- [SDR ABXR2017063000006](https://openairdocs.org/sdr/ABXR2017063000006), Jun 30, 2017: SKIN. BENT. CREASE IN SKIN
- [SDR ABXR2017063000005](https://openairdocs.org/sdr/ABXR2017063000005), Jun 30, 2017: SKIN. CORRODED. CORROSION ON UPPER EXTERIOR SURFACE.
- [SDR ABXR2017063000004](https://openairdocs.org/sdr/ABXR2017063000004), Jun 30, 2017: SKIN. CRACKED. FUSELAGE SKIN CRACK
- [SDR ABXR017063000003](https://openairdocs.org/sdr/ABXR017063000003), Jun 30, 2017: SKIN. DENTED. BULK CARGO DOOR FORWARD LOWER CORNER DENTED.
- [SDR AALA20150607003](https://openairdocs.org/sdr/AALA20150607003), Jun 7, 2015: UNKNOWN. MALFUNCTIONED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CRUISE, LAVATORIES FS3, M2, A5 WOULD NOT FLUSH. ACCOMPLISHED FIM PROCEDURE 38-30-00-8
- [SDR AALA20150515002](https://openairdocs.org/sdr/AALA20150515002), May 15, 2015: TRANSCEIVER. FAULTY. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CREW REPORTED WEATHER RADAR INOPERATIVE. R & R WEATHER RADAR TRANSCEIVER IAW AM
- [SDR AALA20150324017](https://openairdocs.org/sdr/AALA20150324017), Mar 24, 2015: SMOKE DETECTOR. DEFECTIVE. F1 LAVATORY SMOKE DETECTOR SOUNDING INTERMITTENTLY. MX ACTION ACCOMPLISHED IAW FIM TASK 26-13-815-806. R & R SMOKE DETECTOR IAW AMMA 26-13-01. PERFORMED OPERATI
- [SDR AALA20150215006](https://openairdocs.org/sdr/AALA20150215006), Feb 12, 2015: FRAME. CRACKED. RIGHT PYLON OTBD VERTICAL FRAME FOUND WITH A CRACK DURING THE ACCOMPLISHMENT OF WORK CARD 6986. R & R VERTICAL STIFFENER IAW FEA 18082.
- [SDR AALA20141224012](https://openairdocs.org/sdr/AALA20141224012), Dec 23, 2014: WARNING SYSTEM. FALSE ACTIVATION. AIR INTERRUPT, NO EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. LT ENG ANTI-ICE DISPLAYED ON EICAS. LT VLV LIGHT ON ENG ANTI-ICE WHEN SELECTED, U
- [SDR AALA20140904007](https://openairdocs.org/sdr/AALA20140904007), Sep 4, 2014: SIGN. BROKEN. LEFT NR 2 DOOR EXIT LIGHT ASSEMBLY BROKEN. REPLACED LT NR 2 DOOR EXIT SIGN ASSEMBLY. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140904006](https://openairdocs.org/sdr/AALA20140904006), Sep 4, 2014: LIGHT. INOPERATIVE. RIGHT NR 1 DOOR EXTERIOR FUSELAGE EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR EXTERIOR FUSELAGE EMER LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140826008](https://openairdocs.org/sdr/AALA20140826008), Aug 24, 2014: LIGHT. MISSING. SEAT MOUNTED EMER LIGHT AT ROW 29AB MISSING LAMP. REPLACED LAMP FOR SEAT MOUNTED EMER LIGHT. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140824007](https://openairdocs.org/sdr/AALA20140824007), Aug 24, 2014: LENS. MISSING. SEAT MOUNTED EMER LIGHT AT ROW 29AB MISSING CLEAR LENS. REPLACED LENS FOR SEAT MOUNTED EMER LIGHT AT ROW 29AB. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140817003](https://openairdocs.org/sdr/AALA20140817003), Aug 16, 2014: BOTTLE. DEFECTIVE. CREW O2 PRESS DROPPING. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. REPLACED CREW O2 BOTTLE & LEAK CHECKED. SYS GND CHECKED NORMAL OPERATION CLOSED
- [SDR AALA20140611009](https://openairdocs.org/sdr/AALA20140611009), Jun 11, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 13H. OPERATIONS CHECKED NORMAL. RELAMPED LIGHT ASSEMBLY IAW MM 33-51-10. OPERATION
- [SDR AALA20140611007](https://openairdocs.org/sdr/AALA20140611007), Jun 11, 2014: LIGHT. INOPERATIVE. FS3 LAVATORY LOWER EMER LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR FS3 LAVATORY LOWER EMER LIGHT SIGN. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140611006](https://openairdocs.org/sdr/AALA20140611006), Jun 11, 2014: LIGHT. INOPERATIVE. LEFT NR 4 DOOR, UPPER AFT EMER LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR, UPPER AFT EMER LIGHT SIGN. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140611005](https://openairdocs.org/sdr/AALA20140611005), Jun 11, 2014: LIGHT. INOPERATIVE. LEFT AFT OVERWING INTERIOR LOWER EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT AFT OVERWING INTERIOR LOWER EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140611003](https://openairdocs.org/sdr/AALA20140611003), Jun 11, 2014: LIGHT. INOPERATIVE. RIGHT NR 1 DOOR, LOWER EMER LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR LOWER EMER LIGHT SIGN. OPERATIONS CHECKED NORMAL.
- [SDR AALA20140318001](https://openairdocs.org/sdr/AALA20140318001), Mar 17, 2014: DUCT. RUPTURED. HNL CREW REPORTED LT ENG OVERHEAT CAUTION CAME ON UPPER EICAS & PEDESTAL ANNUNCIATOR LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT IN
- [SDR AALA20140210004](https://openairdocs.org/sdr/AALA20140210004), Feb 10, 2014: SUPPORT BEAM. CRACKED. AFT CARGO FWD ROLLOUT STOP SUPPORT BEAM AT STATION 1300 CRACKED. REPLACED BEAM IAW SRM 51-10 -02-0G.
- [SDR AALA20140209007](https://openairdocs.org/sdr/AALA20140209007), Feb 9, 2014: LIGHT. NOT SEATED. EXTERNAL EMERGENCY EXIT LIGHT AT AFT LT DOOR INOPERATIVE. FOUND LAMP NOT FULLY SECURED IN FIXTURE. PROPERLY RESEATED LAMP IN FIXTURE, OPERATIONS CHECKED NORMAL.
- [SDR AALA20140201006](https://openairdocs.org/sdr/AALA20140201006), Feb 1, 2014: LIGHT. INOPERATIVE. EXTERNAL EMERGENCY EXIT LIGHT AT AFT LT DOOR IS INOPERATIVE. REPLACED LIGHT FOR EXTERNAL EMERGENCY EXIT LIGHT AT AFT LT DOOR. OPERATIONS CHECKED NORMAL.
- [SDR AALA20130731004](https://openairdocs.org/sdr/AALA20130731004), Jul 31, 2013: BYPASS SWITCH. INOPERATIVE. OPO INFLIGHT MAD-MIA CREW REPORTED RT ENGINE FILTER BYPASS EICAS MESSAGE. CREW SHUT ENGINE DOWN, SINGLE ENGINE TIME 60 MINUTES. EMERGENCY DECLARED FLIGHT DIVERT
- [SDR AALA20120831015](https://openairdocs.org/sdr/AALA20120831015), Aug 31, 2012: INTERCOSTAL. CRACKED. INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 742 TO 764 AT LEFT BUTTLINE 40 HAS 2 CRACKS AT NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-2
- [SDR AALA20120831006](https://openairdocs.org/sdr/AALA20120831006), Aug 31, 2012: STRINGER. CORRODED. STRINGER 34 RIGHT FROM STATIONS 742 TO 764 CORRODED. ACCOMPLISHED STRINGER SPLICE REPAIR SRM 53-00-03-2R2.
- [SDR AALA20120803010](https://openairdocs.org/sdr/AALA20120803010), Aug 3, 2012: BATTERY PACK. DISCHARGED. LEFT AND RIGHT NUMBER 2 DOORS THRESHOLD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.
- [SDR AALA20120208AFW06](https://openairdocs.org/sdr/AALA20120208AFW06), Feb 1, 2012: STRINGER. CORRODED. CORROSION TO STRINGER 22 LEFT AT STATION 960. REMOVED CORROSION AND ACCOMPLISHED REPAIR PER EA B767-53-021621.
- [SDR AALA20120208AFW08](https://openairdocs.org/sdr/AALA20120208AFW08), Feb 1, 2012: FITTING. CRACKED. LEFT WING AFT PITCH LOAD FITTING OUTBOARD TENSION BOLT HOLE CRACKED. INSTALLED AFT PITCH LOAD FITTING PER EA B767-57-021103.
- [SDR AALA20120208AFW07](https://openairdocs.org/sdr/AALA20120208AFW07), Feb 1, 2012: FITTING. CRACKED. RIGHT WING AFT PITCH LOAD FITTING OUTBOARD TENSION BOLT HOLE CRACKED. INSTALLED AFT PITCH LOAD FITTING PER EA B767-57-021245.
- [SDR AALA201202080009](https://openairdocs.org/sdr/AALA201202080009), Jan 31, 2012: SKIN. CORRODED. LEFT SKIN PANEL STATION 960 CORRODED. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT AND REMOVED CORROSION PER EA B767-53-021212.
- [SDR AALA201202080010](https://openairdocs.org/sdr/AALA201202080010), Jan 27, 2012: SKIN. CORRODED. CENTER WING UPPER SKIN FORWARD OF STATION 955, RIGHT AND LEFT BUTTLINE 82 CORRODED. REMOVED CORROSION AND ROTO PEENED AREA PER EA B767-57-021172.
- [SDR AALA20120208AFW05](https://openairdocs.org/sdr/AALA20120208AFW05), Dec 4, 2011: STRAP. CRACKED. LEFT BODY STATION 955 FAILSAFE STRAP CRACKED. ACCOMPLISHED REPAIR PER ECO C3039AE.
- [SDR AALA20110712TUL01](https://openairdocs.org/sdr/AALA20110712TUL01), Jul 11, 2011: MODULE. FAULTY. MIA - INFLIGHT STI-JFK. CREW REPORTED AILERON AND AUTO-PILOT FAULTS. EMERGENCY DECLARED FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVI
- [SDR AALA20110508CNF01](https://openairdocs.org/sdr/AALA20110508CNF01), May 8, 2011: MODULE. DEFECTIVE. EMERGENCY EVACUATION SYSTEM ALARM CAME ON UNCOMMANDED ON GROUND. FOUND M885 COMMAND SWITCH DEFECTIVE. REPLACED MODULE AT RIGHT NUMBER 4 DOOR CONTROL PANEL. OPS 
- [SDR AALA20110321AFW02](https://openairdocs.org/sdr/AALA20110321AFW02), Mar 18, 2011: PYLON. CRACKED. CRACK WAS FOUND FROM THE FORWARD INBOARD RADII OF THE POWER FEEDER CABLE PASS THROUGH HOLE JUST AFT OF RIGHT PYLON STATION 221.25. ACCOMPLISHED DOUBLER REPAIR P
- [SDR AALA20110321AFW01](https://openairdocs.org/sdr/AALA20110321AFW01), Mar 18, 2011: PYLON. CRACKED. CRACK WAS FOUND FROM THE FORWARD INBOARD RADII OF THE POWER FEEDER CABLE PASS THROUGH HOLE JUST AFT OF LEFT PYLON STATION 221.25. ACCOMPLISHED DOUBLER REPAIR PE
- [SDR AALA20110315AFW01](https://openairdocs.org/sdr/AALA20110315AFW01), Mar 15, 2011: SKIN. DAMAGED. BLEND WAS FOUND ON STRINGER 8 RIGHT LAP SKIN JOINT AT STATION 724. ACCOMPLISHED AN OPEN HOLE AND SURFACE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPLACED FASTEN
- [SDR AALA20110318AFW01](https://openairdocs.org/sdr/AALA20110318AFW01), Mar 15, 2011: SPAR. CRACKED. CRACK WAS FOUND ON THE RIGHT PYLON FORWARD UPPER SPAR WEB COMMON TO THE IDG POWER FEEDER CABLE PASS THROUGH. INSTALLED DOUBLER REPAIR PER EA B767-54-015643.
- [SDR AALA20110314AFW01](https://openairdocs.org/sdr/AALA20110314AFW01), Mar 14, 2011: WEB. CRACKED. CRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-015644.
- [SDR AALA20100915JFK01](https://openairdocs.org/sdr/AALA20100915JFK01), Sep 15, 2010: START VALVE. INOPERATIVE. JFK - INFLIGHT MIA-CDG. CREW REPORTED NUMBER TWO ENGINE START VALVE MESSAGE ILLUMINATED. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERV
- [SDR AALA20100710JFK01](https://openairdocs.org/sdr/AALA20100710JFK01), Jul 10, 2010: TRANSCEIVER. MALFUNCTIONED. JFK - CREW REPORTED WEATHER RADAR FAILED SHORTLY AFTER TAKEOFF. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER. SYS
- [SDR AALA20100618MIA01](https://openairdocs.org/sdr/AALA20100618MIA01), Jun 17, 2010: UNKNOWN. MALFUNCTIONED. MIA - TRAILING EDGE FLAP DISAGREE LIGHT ON FINAL WHEN SELECTING 25 DEGREE FLAPS. FLAP INDICATOR STUCK AT 20 DEGREE FLAPS. ACCOMPLISHED QUICK REFERENCE HANDBOOK 
- [SDR AALA20100227ORD01](https://openairdocs.org/sdr/AALA20100227ORD01), Feb 27, 2010: TRANSMITTER. FAULTY. ORD - DURING APPROACH HAD A TRAILING EDGE FLAP ASSYMETRY. RAN THE QRH AND LANDED WITH FLAPS 20. ALSO HAD TRAILING EDGE FLAPS SHUTDOWN STATUS MESSAGE. FLIGHT LAN
- [SDR AALA20100208LGW01](https://openairdocs.org/sdr/AALA20100208LGW01), Feb 8, 2010: PIN. BURNED. POWERPORTS 5AB CAUSED AC ADAPTOR TO SMOKE. REPLACED BURNT PIN ON POWER PORT HARNESS. OPS CHECKS NORMAL.
- [SDR AALA20090901TUL01](https://openairdocs.org/sdr/AALA20090901TUL01), Aug 31, 2009: WARNING SYSTEM. MALFUNCTIONED. PAP - AIRCRAFT HAD TRAILING EDGE FLAP DISAGREE INDICATION DURING ARRIVAL TO PAP. EMERGENCY DECLARED, LANDED AT PAP WITHOUT INCIDENT. ACCOMPLISHED FAULT ISOLATIO
- [SDR AALA2009051400003](https://openairdocs.org/sdr/AALA2009051400003), May 14, 2009: VALVE. INOPERATIVE. RIGHT ENGINE BLEED OVERHEAT INDICATION. EMERGENCY DECLARED RETURNED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENGINE HP VALVE AND CONTROL
- [SDR AALA2009032600003](https://openairdocs.org/sdr/AALA2009032600003), Mar 26, 2009: INDICATOR. INOPERATIVE. BOS - INFLIGHT JFK-CDG. CAPTAIN REPORTED STANDBY ATTITUDE INDICATOR GYRO FLAG WAS IN VIEW. LANDED BOS WITHOUT INCIDENT. REMOVED AND REPLACED STANDBY ATTITUDE IN
- [SDR AALA200802278](https://openairdocs.org/sdr/AALA200802278), Aug 29, 2008: BATTERY PACK. INOPERATIVE. MIA EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H AND 21H INOPERATIVE. REPLACED BATTERY PACK AT RT HAND OVERWING DOOR FOR EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H AND 21

All 101: https://openairdocs.org/aircraft/N372AA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Sikorsky EH-60A aircraft: https://openairdocs.org/model/sikorsky-eh-60a/aircraft.md
- The GE T700 series engine: https://openairdocs.org/engine/ge-t700-series.md

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