# N747DH: 1980 Boeing 727-224, registration cancelled 2017-10-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 31, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-224](https://openairdocs.org/model/boeing-727-224) (registry code 1384076)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22253
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 6, 2001
- Certificate issued: July 13, 2011
- Last registry action: April 16, 2012
- Mode S code: AA0CDE
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N747DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=747DH
- Page: https://openairdocs.org/deregistered/N747DH-2017-10-31

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 727-224: https://openairdocs.org/model/boeing-727-224.md

## Service difficulty reports (124, newest 50)

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

- [SDR DHLA200800036](https://openairdocs.org/sdr/DHLA200800036), Mar 25, 2008: WIRE. DAMAGED. ON GROUND BURNING ELECTRICAL SMELL IN COCKPIT AFT OF CAPTS SEAT (L-2 WINDOW WIRING) L-2 HEAT INOP. TRANSFERRED TO DEFER LOG NR 32178 IAW MEL 30-15-1 CAT C PLACA
- [SDR 2008747001](https://openairdocs.org/sdr/2008747001), Mar 21, 2008: WEDGE. DELAMINATED. UPON INSPECTION TO THE EXTERIOR OF THE AIRCRAFT, FOUND THE LEFT INBOARD TRAILING EDGE MIDFLAP WEDGE DELAMINATED AT WBL 203.0 4 1/2 BY 2 1/2 AREA OF DELAMINATION
- [SDR DHL2007747001](https://openairdocs.org/sdr/DHL2007747001), Jan 5, 2007: SKIN. GOUGED. RT INBD FORE FLAP O/B LEADING EDGE HAS GOUGE ON REPAIR DOUBLER. REMOVED AND REPLACED DAMAGED REPAIR FROM RT INBD FORE FLAP O/B LEADING EDGE IAW B727 SRM 57-50-4
- [SDR DHL2006747003](https://openairdocs.org/sdr/DHL2006747003), Sep 19, 2006: BATTERY. NO TEST. COCKPIT EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED LIGHT ASSY. BATTERIES, OPS CK. NORMAL IAW BMM REF 33-50-01. P/N 37067-001.
- [SDR DHL2006747002](https://openairdocs.org/sdr/DHL2006747002), Mar 13, 2006: FAIRING. DAMAGED. MX RELEASE FOR DROP IN VISIT FOR DAMAGE TO LT AFT BODY FAIRING AND FAIRING SUPPORT. MX RELEASE DONE ON 3-13-06 UNDER WORK ORDER 5001328.
- [SDR DHL2006747001](https://openairdocs.org/sdr/DHL2006747001), Mar 1, 2006: PIN. INSTALLED. NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD NOSE GEAR PIN FOUND INSTALLED ON POST FLIGHT. DURING POST FLT FOUND ONE MAIN GEAR PIN MISSING. REMOVED NOSE GEAR 
- [SDR DHL2005747003](https://openairdocs.org/sdr/DHL2005747003), Dec 16, 2005: CONNECTOR. LOOSE. AFTER FLAPS WERE RETRACTED TO 0 THE AMBER LE FLAPS LIGHT ILLUMINATED ON FWD PANEL SO PANEL READ NR5 LE FLAP IN TRANSIT ABNORMAL PROCEDURE COMPLETE PROBLEM REMAI
- [SDR DHL2005747001](https://openairdocs.org/sdr/DHL2005747001), Nov 8, 2005: WIRE. CHAFED. NR 1 GEN FAILED ON T/O ROLL DISCONECTED CSD RTO INFO OAT 16 C PA 4300 SPEED 45 KNOTS MODERATE BREAKING A/C WEIGHT 131,400 REV. THRUST MODERATE. DEFERRED IAW MEL
- [SDR DHL2005747002](https://openairdocs.org/sdr/DHL2005747002), Nov 8, 2005: SMOKE. DETECTED. COCKPIT FILLED WITH SMOKE, EVACUATED A/C. WITH ENGINE PNEUMATICS RAN BOTH A/C PACKS AND INSPECTED FOR SMOKE SOURCE, NO DEFECTS A/C OK FOR SERVICE IAW MM JRH 6.3
- [SDR DHL2005747511](https://openairdocs.org/sdr/DHL2005747511), Aug 14, 2005: BEAR STRAP. CORRODED. CORROSION FOUND AFT PIT INTERNAL SKIN STA 990 STR 28R AFT OF BEAR STRAP DOUBLER. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER 20.25 X 15.5 INCH FROM 2024
- [SDR DHL2005747510](https://openairdocs.org/sdr/DHL2005747510), Aug 14, 2005: STRINGER. CORRODED. CORROSION FOUND ON STR 28R, STA 950F TO 970 AT SKIN ATTACHMENTS. REMOVED STR 28R FROM 950F TO 1010, FRAME STA 987 RT CLIPS AND ANGLE SUPPORT STA 950F, 985, 990.
- [SDR DHL2005747509](https://openairdocs.org/sdr/DHL2005747509), Aug 14, 2005: SHEAR WEB. CORRODED. CORRODED AFT CARGO INTERCOSTAL FROM STA 950F TO 970 STR 28R. REMOVED FLOOR SUPPORT CLIPS, REMOVED SHEAR WEB. FABRICATED AND INSTALLED NEW SHEAR WEB 19.5 X 7 INC
- [SDR DHL2005747508](https://openairdocs.org/sdr/DHL2005747508), Aug 14, 2005: STRINGER SPLICE. CORRODED. CORRODED STRINGER SPLICE 28R IN AFT CARGO COMPT BS 1010. REMOVED CORRODED SPLICE. FABRICATED AND INSTALLED REPAIR STRINGER SPLICE 12.5 INCHES FROM BAC1498-131 I
- [SDR DHL2005747507](https://openairdocs.org/sdr/DHL2005747507), Aug 14, 2005: ATTACH ANGLE. CORRODED. CORROSION ON SKIN ATTACH ANGLE FS 990 FROM STR 27R TO STR 29R. REMOVED CORROSION OFF SKIN ATTACH ANGLE FS 990 STR 27R TO 29R. PERFORMED ULT INSP ON BLENDED AREA
- [SDR DHL2005747506](https://openairdocs.org/sdr/DHL2005747506), Aug 14, 2005: SHEAR TIE. CORRODED. CORROSION ON AFT PIT FRAME AT BS 970 STR 28R - 29R. REMOVED FLOOR SUPPORT AND VERTICAL STIFFENER BS 930 - 990. ANGLE SHEAR TIE FOUND 100 PERCENT MATERIAL LOSS. 
- [SDR DHL2005747502](https://openairdocs.org/sdr/DHL2005747502), Jul 27, 2005: WEDGE. DELAMINATED. LEFT WING INBD MID FLAP T/E WEDGE APPROX 61" FROM INBD END HAS AREA OF DELAMINATION ON BOTTOM SKIN. REPAIRED LEFT INBD MID FLAP T/E INNER BOTTOM SKIN AT APPROX 
- [SDR DHL2005747513](https://openairdocs.org/sdr/DHL2005747513), Jul 17, 2005: WEB. CORRODED. CORROSION ON WEB AT STR 27L STA 950 TO STA 950A. REMOVED CORROSION ON WEB AT STA. 950 TO 950A LONGERON 27L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 AND 51-10-6
- [SDR DHL2005747512](https://openairdocs.org/sdr/DHL2005747512), Jul 17, 2005: SKIN. GOUGED. LT WING INBOARD TRAILING EDGE FORE FLAP OUTBOARD LOWER LEADING EDGE REPAIR DOUBLER IS GOUGED THRU. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW 
- [SDR DHL2005747503](https://openairdocs.org/sdr/DHL2005747503), Jul 12, 2005: SKIN. DELAMINATED. LT WING INBD MID-FLAP T/E APPROX 61" FROM INBD END HAVE DELAMINATION. REPAIRED LT INBD MID FLAP T/E AT APPROX 61" FROM INBD END IAW B-727 SRM 51-40-20 PAR 20-22
- [SDR DHL2005747500](https://openairdocs.org/sdr/DHL2005747500), Jul 12, 2005: WEB. CORRODED. CORROSION ON WEB AFT CARGO BIN FS 950 TO FS 950A AT STR 27R. REMOVED CORROSION ON WEB IN AFT CARGO BIN FS 950 TO 950A AT STR 27R. FOUND OUT OF LIMITS. OPEN PANE
- [SDR DHL2005747505](https://openairdocs.org/sdr/DHL2005747505), Jul 10, 2005: SKIN. DEBONDED. RT WING INBD MID FLAP T/E APPROX 1/2" FROM INBD END IS DISBONDED. CUT OUT DELAM AREA, FAB FILLER AN DOUBLERS ON TRAVELER NR T-828368. CLEANED UP AN PREP REPAIR 
- [SDR DHL2005747504](https://openairdocs.org/sdr/DHL2005747504), Jul 10, 2005: SKIN. CRACKED. CRACK IN T/E FLAP LWR SKIN AT NR 3 ATTACH CUT OUT I/B SIDE LT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER IAW B727 SRM
- [SDR DHL2005747501](https://openairdocs.org/sdr/DHL2005747501), Jul 10, 2005: SKIN. CRACKED. CRACK IN T/E FLAP SHIM AT NR 2 ATTACH CUT OUT I/B SIDE LOWER SIDE LEFT WING. FABRICATED REPAIR DOUBLER, CHEM TREATED AN PRIMED AN INSTALLED REPAIR DOUBLER IAW B
- [SDR DHL2004747011](https://openairdocs.org/sdr/DHL2004747011), Dec 18, 2004: SWITCH. DIRTY. LEFT MAIN GEAR DOOR LIGHT ILLUM DURING TAKEOFF ROLL EXTINGUISHED DURING CLIMBOUT (RED LIGHT ON F/O PANEL). FOUND LEFT MAIN GEAR DOOR SWITCH CONTAMINATED. CLEANE
- [SDR DHL2004747010](https://openairdocs.org/sdr/DHL2004747010), Dec 1, 2004: WARNING LIGHT. ILLUMINATED. AFTER T/O FROM IAH, GEAR HANDLE PLACED TO OFF THE RED DOORS LIGHT AND RT DOOR LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES LIGHTS WENT OUT. WHEN GEAR HAN
- [SDR DHL2004747009](https://openairdocs.org/sdr/DHL2004747009), Nov 30, 2004: ACTUATOR. INOPERATIVE. "A" SYSTEM FAILED DURING LDG GEAR EXTENSION. PERFORMED ABNORMAL PROCEDURE AND LANDED. A/C TOWED IN. REMOVED AND REPLACED NR 1 SLAT ACTUATOR IAW M/M 27-81-31, NO
- [SDR DHL2004747008](https://openairdocs.org/sdr/DHL2004747008), Nov 10, 2004: LIGHT. DISLODGED. EMERGENCY EXIT LIGHT FELL OFF MOUNT DURING FLIGHT. SECURED LIGHT ASSEMBLY, OPS CHECK GOOD IAW 727 MM CH 33-50.
- [SDR DHL2004747007](https://openairdocs.org/sdr/DHL2004747007), Nov 10, 2004: CONTROL LEVER. OUT OF ADJUST. DURING TAKEOFF ROLL AT MIO LEFT MAIN GEAR UNSAFE LIGHT FLICKERED OFF AND ON. OPS CHECKED LANDING GEAR CONTROL LEVER POS SWITCH IAW ASTAR MM 32-61-11 PG 401. IND
- [SDR DHL2004747006](https://openairdocs.org/sdr/DHL2004747006), Sep 29, 2004: LINE. LEAKING. BEFORE LANDING CVG B HYD SYSTEM QUANTITY WENT TO ZERO QUANTITY HYD SYSTEM B FAILED ABNORMAL PROCEDURE C/W. INSTALLED FLEX LINE BETWEEN B HYD SYSTEM AND FILTER P
- [SDR DHL2004747005](https://openairdocs.org/sdr/DHL2004747005), Aug 4, 2004: CONTROL UNIT. INOPERATIVE. MAIN GEAR ANTI- SKID OB INOPERATIVE, (LIGHT REMAINED ILLUMINATED AND IB INOPERATIVE LIGHT WOULD NOT TEST. TO ADD , OB ANTI SKID ILLUMINATED WHILE ON APPROACH. R
- [SDR DHL2004747004](https://openairdocs.org/sdr/DHL2004747004), Mar 16, 2004: WIRE. FRAYED. CAPTAIN'S ADJUST LAMP CORD IS FRAYED AND IS ARCING. INSTALLED CLAMP AND TIGHTEN HARDWARE HOLDING GROUND WIRE PER M/M 20-80-1, OPS CHECKED NORMAL PER M/M 33-10-0
- [SDR DHL2004747003](https://openairdocs.org/sdr/DHL2004747003), Feb 11, 2004: DOOR. OUT OF ADJUST. MAIN ENTRY DOOR DIFFICULT TO CLOSE. ADJUSTED MAIN ENTRY DOOR IAW M/M 52-11-01. OPS CHECKED GOOD.
- [SDR DHL2004747002](https://openairdocs.org/sdr/DHL2004747002), Jan 23, 2004: CONNECTOR. FAILED. NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLIED. (TOGW 144900, IAS 20 KTS, OAT -16 C, 500 FT PA, AND BRAKE ENERGY ZONE NORMAL). TRANSFERRED TO DMI LOG 15488
- [SDR DHL2004747001](https://openairdocs.org/sdr/DHL2004747001), Jan 16, 2004: INDICATOR. INOPERATIVE. NR 3 EPR INDICATOR INOPERATIVE. WEIGHT: 156000, AIRSPEED: 40 KNOTS, AND OAT -22 C. DEFERRED NR 3 EPR PER MEL 77-1-1 CAT-A DMI 15408.
- [SDR DHL2003747015](https://openairdocs.org/sdr/DHL2003747015), Dec 30, 2003: DOOR FRAME. CRACKED. MAIN CARGO DOOR FRAME AFT ACT AREA HAS CRACK. REPAIRED IAW AERONAUTICAL SOLUTIONS REPORT 03-011 IR DTD 12/30/03. MATERIAL USED 2024-T3 .090 PO 21582, FASTENERS 
- [SDR DHL2003747014](https://openairdocs.org/sdr/DHL2003747014), Dec 19, 2003: DOOR. UNSECURE. CAPTAIN'S SIDE ESCAPE ROPE DOOR WON'T CLOSE. RE-SECURED DOOR AS REQUIRED; OPS CHECKED NORMAL.
- [SDR DHL2003747012](https://openairdocs.org/sdr/DHL2003747012), Nov 21, 2003: POWER SUPPLY. MALFUNCTIONED. IN CRUISE FLIGHT ALL THREE FUEL FLOW GAUGES WENT TO ZERO, S/O ADVISED THAT 28 VDC AND 115 AC FUEL FLOW CIRCUIT BREAKERS HAD POPPED. REMOVED AND REPLACED FUEL FL
- [SDR DHL2003747013](https://openairdocs.org/sdr/DHL2003747013), Nov 4, 2003: SLEEVE. DAMAGED. OUTSIDE MAIN ENTRY DOOR HANDLE WOULD NOT ENGAGE. SPRING ACTION FINE. REMOVED AND REPLACED MAIN ENTRY DOOR HANDLE MECHANICAL SLEEVE PER B-727 M/M 52-11-01. OPS C
- [SDR DHL2003747011](https://openairdocs.org/sdr/DHL2003747011), Oct 11, 2003: LIGHT. INOPERATIVE. ENTRY EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00. OPS CHECKED GOOD.
- [SDR DHL2003747010](https://openairdocs.org/sdr/DHL2003747010), Aug 27, 2003: LIGHT. MALFUNCTIONED. EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR ILLUMINATED. EMERGENCY EXIT LIGHT NOT ILLUMINATED PER 33-50-01 PAGE 7. THE 2-28V BULBS ILLUMINATED WITH NO SMOKING SWI
- [SDR DHL2003747009](https://openairdocs.org/sdr/DHL2003747009), Jul 30, 2003: SNUBBER. OUT OF ADJUST. ON TOUCHDOWN FORWARD ENTRY DOOR HANDLE POPPED OPEN. ADJUSTED ENTRY DOOR SNUBBERS, OPS CHECKED GOOD IAW 52-11-0.
- [SDR DHL2003747008](https://openairdocs.org/sdr/DHL2003747008), Jun 26, 2003: DOWNLOCK SENSOR. FAULTY. WHEN LANDING GEAR LOWERED, RIGHT GEAR RED LIGHT ILLUMINATED WITH RIGHT GEAR GREEN LIGHT OUT. SECONDARY MAIN GEAR POSITION INDICATOR GREEN LIGHTS BOTH ON. COMPLE
- [SDR DHL2003747006](https://openairdocs.org/sdr/DHL2003747006), Jun 10, 2003: ENGINE. MALFUNCTIONED. IN-FLIGHT ENGINE NR 1 OIL FILTER BYPASS LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURES, SHUT DOWN ENGINE AS PER ABNORMAL PROCEDURES. DIVERTED TO KMCI. ON SHOR
- [SDR DHL2003747509](https://openairdocs.org/sdr/DHL2003747509), May 14, 2003: SUPPORT. CRACKED. DURING C CHECK, UPON REMOVAL OF NR 7 SLAT ACTUATOR SUPPORT STRUCTURE FOUND O/B MOUNT CRACKED AND I/B MOUNT CHAFED. REMOVED FUEL TANK ACCESS PANEL 7615 AND 7618 
- [SDR DHL2003747517](https://openairdocs.org/sdr/DHL2003747517), May 13, 2003: INTAKE DUCT. CRACKED. DURING C-CHECK, N/R 53639 EMP STA 1303 WEB ABOVE NR 2 ENGINE INTAKE DUCT IS CRACKED, LOWER RT CORNER. REMOVED FASTENERS FOR ACCESS PER B-727 SRM 51-30-2. STOP D
- [SDR DHL2003747516](https://openairdocs.org/sdr/DHL2003747516), May 13, 2003: STRINGER. CORRODED. DURING C-CHECK, N/R 53605 IN AFT CARGO STR 27L HAS CORROSION FROM BS 950 A TO BS 1070. CUT-OUT DAMAGED SECTION OF STR 27 L FROM STA 950A PLUS 10 TO 1080 IAW B-7
- [SDR DHL2003747515](https://openairdocs.org/sdr/DHL2003747515), May 13, 2003: SKIN. DENTED. DURING C-CHECK, N/R 53604 IN AFT CARGO FRAME BS 1050 HAS A DENT INTO THE RADIUS BELOW STR 26 L. CUT OUT DAMAGED AREA DIM 1 INCH X 1 INCH AND FABRICATED ONE DOUB
- [SDR DHL2003747512](https://openairdocs.org/sdr/DHL2003747512), May 13, 2003: SKIN. DENTED. DURING "C" CHECK, N/R 53655, CABIN INTERIOR AT BS 560 DENT AND CRACK BTW. ST. 16R-17R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREAS
- [SDR DHL2003747510](https://openairdocs.org/sdr/DHL2003747510), May 13, 2003: STIFFENER. CRACKED. DURING "C" CHECK N/R 53650 LT WING LE CAVITY LE STA. 1307 VERTICAL STIFFENER IS CRACKED AT BOTTOM END (FRONT SPAR WBL 92.8. REMOVED L/H WING ACCESS PANEL 6303 T
- [SDR DHL2003747506](https://openairdocs.org/sdr/DHL2003747506), May 13, 2003: FRAME. DENTED. DURING "C" CHECK IN AFT. CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS BELOW STR 26L. CUT-OUT DAMAGE AREA APROX 1 INCH FRAME 1030 STR 26 L IAW B-727 S.R.M. 51-

All 124: https://openairdocs.org/deregistered/N747DH-2017-10-31/reports.md

## FAA accident and incident reports (1)

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 20061104026259I](https://openairdocs.org/incident/20061104026259I), Nov 4, 2006: Boeing 727224 (N747DH), Atlanta, GA. (-23) While at FL330, fo [privacy data omitted] became ill. Capt [privacy data omitted] declared an emergency and diverted into katl. Approach, landing and…

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