# N938HA: 1989 Boeing DHC-8-102, registration cancelled 2021-01-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 30, 2021
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing DHC-8-102](https://openairdocs.org/model/boeing-dhc-8-102) (registry code 1386002)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM) (OpenAirDocs)
- Serial number: 152
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, normal
- Airworthiness date: May 15, 1989
- Certificate issued: October 11, 2017
- Last registry action: June 15, 2018
- Mode S code: AD0411
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N938HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=938HA
- Page: https://openairdocs.org/deregistered/N938HA-2021-01-30

From the FAA registry file of November 4, 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 DHC-8-102: https://openairdocs.org/model/boeing-dhc-8-102.md

## Service difficulty reports (112, newest 50)

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

- [SDR HNAA2017041700122](https://openairdocs.org/sdr/HNAA2017041700122), Apr 15, 2017: BATTERY. DISCHARGED. FWD EMERGENCY LIGHT SIGN AND EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED ALL BATTERY ELECTRICAL CONNECTORS TO ISOLATE PROBLEM. NO SUCCESS. REMOVED AFT BATTERY 
- [SDR HNAA2017030600074](https://openairdocs.org/sdr/HNAA2017030600074), Mar 6, 2017: BULB. INOPERATIVE. THIRD AFT EMERGENCY AISLE LIGHT FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.
- [SDR HNAA2017021500052](https://openairdocs.org/sdr/HNAA2017021500052), Feb 11, 2017: CONTROL PANEL. MALFUNCTIONED. AFTER TAKEOFF, THE F/O SELECTED GEAR UP. THREE RED UNSAFE LIGHTS AND THREE GREEN ILLUMINATED ON THE MLG PANEL ALONG WITH BOTH HANDLE LIGHTS. CREW FOLLOWED CHECK
- [SDR HNAA2017020300039](https://openairdocs.org/sdr/HNAA2017020300039), Feb 3, 2017: BULB. INOPERATIVE. EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2017012300027](https://openairdocs.org/sdr/HNAA2017012300027), Jan 23, 2017: GENERATOR. FAILED. DURING TAKEOFF ROLL, THE NR 2 AC GENERATOR FAILED. WOULD NOT RESET. NO VOLTS OR LOADS. REMOVED AND REPLACED THE NR 2 AC GENERATOR AND GCU IAW WORKCARD 24-20-11R
- [SDR HNAA2016102800338](https://openairdocs.org/sdr/HNAA2016102800338), Oct 28, 2016: BULB. INOPERATIVE. THIRD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2016100500311](https://openairdocs.org/sdr/HNAA2016100500311), Oct 5, 2016: CIRCUIT BREAKER. TRIPPED. DURING CRUISE FLIGHT, THE PRIMARY INVERTER CAUTION LIGHT ILLUMINATED, ALONG WITH CAPTAIN'S FLIGHT INSTRUMENTS WENT DARK AND TRANSPONDER FAILED. FOLLOWED CHECK L
- [SDR HNAA2016091400278](https://openairdocs.org/sdr/HNAA2016091400278), Sep 12, 2016: BULB. DIM. EMERGENCY EXIT SIGN ABOVE PAX DOOR DIM. R & R THE BULBS.
- [SDR HNAA2016091200276](https://openairdocs.org/sdr/HNAA2016091200276), Sep 9, 2016: UNKNOWN. MALFUNCTIONED. AIRCRAFT IS TOO HOT FOR REVENUE SERVICE. FLIGHT DECK DUCT TEMP AND AIRFLOW IS GOOD. CABIN DUCT TEMP NORMAL WITH POOR AIRFLOW. STANDBY CONDITION, PERFORMED OPS C
- [SDR HNAA2016081500248](https://openairdocs.org/sdr/HNAA2016081500248), Aug 13, 2016: CONTROLLER. INOPERATIVE. UPON ROTATION YAW DAMPER AP SELECT AND HSI SELECT ON 801 PANEL BECAME INOPERATIVE. R&R AFCS CONTROLLER AS REQUIRED IAW AMM 22-10-01. OPS AND TEST ON GROUND GOOD
- [SDR HNAA2016061700186](https://openairdocs.org/sdr/HNAA2016061700186), Jun 16, 2016: TSCU. MALFUNCTIONED. DURING TAKEOFF ROLL AT 85 PERCENT TORQUE AUTO FX FAILED TO ARM, REJECTED T/O. LIGHT ILLUMINATED UPON REDUCED POWER. R & R NR 2 ENGINE TSCU IN REF TO 77-10-00 C/
- [SDR HNAA2016062000191](https://openairdocs.org/sdr/HNAA2016062000191), Jun 15, 2016: UNKNOWN. MALFUNCTIONED. DURING TAKEOFF ROLL, AUTO FX WOULD NOT ARM AUTOFEATHER SYSTEM. REPLACED RELAY 6121-K5 AS PRECAUTIONARY MEASURE, OPS CK GOOD AT THIS TIME, REF 61-26-00.
- [SDR HNAA2016052700154](https://openairdocs.org/sdr/HNAA2016052700154), May 21, 2016: FLAP TRACK. CRACKED. RIGHT WING NR 5 FLAPTRACK SHOWS INDICATIONS WHILE PERFORMING EDDY CURRENT INSPECTION AROUND SEVERAL FASTENER HEADS ON OTBD SIDE OF TRACK.
- [SDR HNAA2016052700153](https://openairdocs.org/sdr/HNAA2016052700153), May 21, 2016: FLAP TRACK. CRACKED. RIGHT WING NR 4 FLAP TRACK SHOWS INDICATIONS WHILE PERFORMING EDDY CURRENT INSPECTION AROUND SEVERAL FASTENER HEADS ON OTBD SIDE OF FLAPTRACK.
- [SDR HNAA2016051100143](https://openairdocs.org/sdr/HNAA2016051100143), May 10, 2016: PRESSURE SWITCH. MALFUNCTIONED. NR 2 ENGINE OIL PRESSURE WARING LIGHT ILLUMINATED INFLIGHT. OIL PRESSURE SHOWS IN GREEN ARC ON GAUGE. ALL OTHER ENGINE PARAMETERS ARE NORMAL. INSPECTED NO LEAKS
- [SDR HNAA2016022200048](https://openairdocs.org/sdr/HNAA2016022200048), Feb 22, 2016: SKIN. DAMAGED. MULTIPLE RIVETS PULLING THROUGH SKIN AT BS 252, BETWEEN STR 29-31. R & R RIVETS AT BS 252, BETWEEN STR 29-31 IAW EO8-53-16-0098.
- [SDR HNAA2016022200047](https://openairdocs.org/sdr/HNAA2016022200047), Feb 22, 2016: SKIN. CORRODED. FOUND CORROSION AT BS 253.40, BETWEEN STR 28 AND 30. R & R RIVETS, STRAP AND EXISTING PATCH AT BS 240-5. COMPLIED WITH STEPS 1 THRU 6B OF EA15-2016-024. REPAIRE
- [SDR HNAA2016012200016](https://openairdocs.org/sdr/HNAA2016012200016), Jan 22, 2016: WIRE. BROKEN. AUTOFEATHER WILL NOT ARM. FOUND BROKEN WIRE AT NR 1 ENGINE POWER LEVER MICROSWITCH TERMINAL. RESOLDERED WIRE TERMINAL, PERFORMED OPS CHECKED. OPS CHECK GOOD. CO
- [SDR HNAA2015110400323](https://openairdocs.org/sdr/HNAA2015110400323), Nov 4, 2015: WARNING LIGHT. FALSE ACTIVATION. AFTER GEAR RETRACTION, ALL LIGHTS WENT OUT, THEN NOSE GEAR RED UNSAFE LIGHT FLICKERED ALONG WITH GEAR HANDLE LIGHTS, THEN EXTINGUISHED. NOSE GEAR UNSAFE LIGHT A
- [SDR HNAA2015072900245](https://openairdocs.org/sdr/HNAA2015072900245), Jul 29, 2015: LIGHT. INOPERATIVE. EMERGENCY FLOOR PATH LIGHT IS INOPERATIVE. R & R EMERGENCY FLOOR PATH LIGHT.
- [SDR HNAA2015062900210](https://openairdocs.org/sdr/HNAA2015062900210), Jun 29, 2015: GENERATOR. NOT REPORTED. R & R NR 1 AC GENERATOR IAW WORK CARD 24-20-11R. R & R NR 1 AC GCU AND SECURED WITH RETAINED HARDWARE. OPS AND LEAKED CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2015052700171](https://openairdocs.org/sdr/HNAA2015052700171), May 27, 2015: BULB. INOPERATIVE. ONE RED EMERGENCY EXIT FLOOR LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2015051500161](https://openairdocs.org/sdr/HNAA2015051500161), May 15, 2015: BULB. INOPERATIVE. THIRD FROM AFT EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2015012600026](https://openairdocs.org/sdr/HNAA2015012600026), Jan 26, 2015: BULB. INOPERATIVE. EMERGENCY LIGHT IS INOPERATIVE AT ROW 1. R & R THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2014120300344](https://openairdocs.org/sdr/HNAA2014120300344), Dec 3, 2014: BULB. INOPERATIVE. CEILING EMERGENCY LIGHT AT ROW 5 IS INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2014062400188](https://openairdocs.org/sdr/HNAA2014062400188), Jun 20, 2014: PROPELLER. VIBRATION. SEVERE PROPELLER VIBRATION. SHIMED NR 100 AND 200 PROPELLER BLADES IAW MM 61-10-00. . OPS CHECKED GOOD DURING ENGINE RUNS.
- [SDR HNAA2014031000081](https://openairdocs.org/sdr/HNAA2014031000081), Mar 10, 2014: PUMP. MALFUNCTIONED. WHEN STANDBY HYD PUMPS WERE SELECTED ON, NR 1 AC GENERATOR DROPS OFF LINE, BUT WILL RESET. R & R NR 2 STANDBY AD NR 2 CASE DRAIN FILLER ELEMENT IAW AMM 29-11-17
- [SDR HNAA2014010300653](https://openairdocs.org/sdr/HNAA2014010300653), Jan 3, 2014: BRAKE ASSY. OVERHEATED. SMOKE COMING FROM LT BRAKE WHICH APPEARS TO BE HOT. R & R NR 2 BRAKE ASSY.
- [SDR HNAA2013123000643](https://openairdocs.org/sdr/HNAA2013123000643), Dec 28, 2013: RELAY. FAILED. ON TAKE OFF ROLL, AUTO FX DID NOT ARM. RTO SYS TESTS OK AFTERWARDS. R & R RELAY 6121-K5. GROUND-RAN AIRCRAFT IAW -8 RUNUP MANUAL. OK FOR SERVICE.
- [SDR HNAA2013123000641](https://openairdocs.org/sdr/HNAA2013123000641), Dec 26, 2013: AUTOFEATHER SYS. MALFUNCTIONED. AUTOFEATHER E/N ARM ON TAKE OFF ROLL WITH TAKE OFF POWER SET. REJECTED TAKE OFF. COMPLIED WITH SELF TEST OF SYSTEM AND CHECKED GOOD.
- [SDR HNAA2013111500575](https://openairdocs.org/sdr/HNAA2013111500575), Nov 15, 2013: ACTUATOR. LEAKING. NLG UNSAFE LIGHT FLASHING INTERMITTENTLY WITH GEAR HANDLE, ACCOMPANIED BY NLG ATTEMPTING TO CYCLE. PERFORMED ALTERNATE EXTENSION AND RECEIVED THREE GREEN LIGHTS
- [SDR HNAA2013092300510](https://openairdocs.org/sdr/HNAA2013092300510), Sep 23, 2013: BULB. FAILED. SIDEWALL EMERGENCY LIGHT IS DIM AT ROW 4DF. R & R BULB AT SIDEWALL EMERGENCY LIGHT IN ROW 4DF. OPS CHECKED GOOD.
- [SDR HNAA2013092300508](https://openairdocs.org/sdr/HNAA2013092300508), Sep 23, 2013: BULB. FAILED. FWD FUSELAGE RT EMERGENCY LIGHT IS DIM. R & R BULB AT RT FWD EMERGENCY LIGHT FUSELAGE. OPS CHECKED GOOD.
- [SDR HNAA2013090300487](https://openairdocs.org/sdr/HNAA2013090300487), Sep 3, 2013: SENSOR. OUT OF ADJUST. FLAP DRIVE CAUTION LIGHT FLICKERED ON AND OFF IN FLIGHT AND ON GROUND. R & R FLAP DRIVE TORQUE SENSOR IAW MM 27-52-51. ADJUSTED SENSOR IAW WC 27-50-11Q. INSPECT
- [SDR HNAA2013083000482](https://openairdocs.org/sdr/HNAA2013083000482), Aug 30, 2013: BULB. MALFUNCTIONED. LT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2013080700453](https://openairdocs.org/sdr/HNAA2013080700453), Aug 7, 2013: POWER SUPPLY. FAILED. THIRD AND FOURTH FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. R & R POWER SUPPLY PS2 IAW MM 33-53-01. OPS CHECKED GOOD.
- [SDR HNAA2013062600361](https://openairdocs.org/sdr/HNAA2013062600361), Jun 26, 2013: ACTUATOR. INOPERATIVE. TAXIING ON BOTH ENGINES, FLIGHT/TAXI SWITCH SELECTED TO FLIGHT, ROLL SPOILER INBD CAUTION LIGHT ILLUMINATED, FOLLOWED BY NR 1 ISOLATION VALVE CAUTION LIGHT ILLU
- [SDR HNAA2013060500324](https://openairdocs.org/sdr/HNAA2013060500324), Jun 5, 2013: CONNECTOR. FAILED. RADAR FAILED ON CLIMBOUT IN A TURN FROM DEPARTURE. CLEANED AND REMOVED CORROSION FROM RADAR RT CONNECTOR PLUG. R & R RADAR RT OPS CHECKED GOOD IAW MM 34-41-04.
- [SDR HNAA2013050100245](https://openairdocs.org/sdr/HNAA2013050100245), May 1, 2013: HOSE. DISCONNECTED. BOTH LT AND RT DEICE BOOTS WILL NOT INFLATE IN NR 5 POSITION. FOUND DEICE HOSE DISCONNECTED AT TAIL RT INBD BOOT. RESECURED HOSE AS REQUIRED. OPS CHECKED GOOD.
- [SDR HNAA2013040300200](https://openairdocs.org/sdr/HNAA2013040300200), Apr 3, 2013: BULB. FAILED. ROW 4AC AND 4DF EMERGENCY SIDEWALL LIGHTS ARE INOP. REMOVED LENS, REMOVED AND REPLACED BULBS. REINSTALLED LENS. OPS CHECKED GOOD.
- [SDR HNAA2013021900082](https://openairdocs.org/sdr/HNAA2013021900082), Feb 19, 2013: BULB. FAILED. SECOND EMERGENCY FLOOR LIGHT IS INOPERATIVE. R & R EMERGENCY FLOOR LIGHT. OPS CHECKED GOOD. RESECURED LENS.
- [SDR HNAA2013013000029](https://openairdocs.org/sdr/HNAA2013013000029), Jan 30, 2013: BULB. FAILED. EMERGENCY EXIT SIGN OVER AIRSTAIR DOOR HAS BULB INOPERATIVE. REMOVED LENS, REMOVED AND REPLACED BULBS. REINSTALLED LENS. OPS CHECKED GOOD.
- [SDR HNAA2013010701152](https://openairdocs.org/sdr/HNAA2013010701152), Jan 7, 2013: BULB. FAILED. FLOOR EMERGENCY LIGHT IS INOPERATIVE, 7TH FROM FRONT. R & R BULB. OPS CHECKED GOOD. REINSTALLED FLOOR LENS COVER.
- [SDR HNAA2012112901080](https://openairdocs.org/sdr/HNAA2012112901080), Nov 29, 2012: BULB. FAILED. RT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT IS DIM. R & R BULB, OPS CHECKED GOOD.
- [SDR HNAA2012112601072](https://openairdocs.org/sdr/HNAA2012112601072), Nov 26, 2012: SENSOR. FAILED. STRONG ODOR IN AFT CABIN WITH ENGINE BLEEDS ON. RETURN TO GATE FOUND AUTO TEMP TO BE INOPERATIVE. MANUAL CONTROL OPS NORMAL. R & R CABIN ZONE TEMP SENSOR IAW MM
- [SDR HNAA2012091400953](https://openairdocs.org/sdr/HNAA2012091400953), Sep 14, 2012: BULB. INOPERATIVE. FOURTH RED FLOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED PLASTIC COVER, REMOVED BULB, INSTALLED NEW BULB. REINSTALLED LIGHT LENS COVER. OPS CHECKED GOOD.
- [SDR HNAA2012081300915](https://openairdocs.org/sdr/HNAA2012081300915), Aug 10, 2012: DOOR. OPEN. GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINT INSPECTED AND FOUND OVERHEAD BYPASS DOOR OPEN. MAINT CLOSED DOOR AS REQUIRED.
- [SDR HNAA2012080200891](https://openairdocs.org/sdr/HNAA2012080200891), Aug 2, 2012: WARNING LIGHT. FALSE ACTIVATION. NOSE GEAR RED UNSAFE LIGHT ILLUMINATED INTERMITTENTLY WITH GEAR DOWN AND LOCKED. COULD NOT DUPLICATE. R & R PSEU IAW -8MM 32-61-50 FOR MX CONVIENCE. OPS CHECKED
- [SDR HNAA2012071800868](https://openairdocs.org/sdr/HNAA2012071800868), Jul 18, 2012: OIL SYSTEM. LOW. NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED ON TAKEOFF. CREW DEPARTED RUNWAY. OIL PRESSURE NORMAL. INSPECTED ENGINE, FOUND 3 QUARTS LOW. SERVICED AS REQUIRED. GR
- [SDR HNAA2012051000769](https://openairdocs.org/sdr/HNAA2012051000769), May 10, 2012: BATTERY PACK. FAILED. FORWARD FUSELAGE RT EMERGENCY LIGHT IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PS2 IN COAT CLOSET IAW AMM 33-51-00.

All 112: https://openairdocs.org/deregistered/N938HA-2021-01-30/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 20100314029179I](https://openairdocs.org/incident/20100314029179I), Mar 14, 2010: Dehavilland DHC-8-102 (N938HA), Harrisburg, PA, Minor damage. Aircraft returned to gate due to dragging right brake. Right inboard brake caught fire and was immediately extinguished by mechanic.
- [Incident 19930422012899I](https://openairdocs.org/incident/19930422012899I), Apr 22, 1993: Dhav DHC8102 (N938HA), Tampa, FL. Left engine surged on climb out. Secured engine and returned. Fire light on. Discharged fire bottles. No fire.

---
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.