# N708DH: 1964 Boeing 727-25, registration cancelled 2013-09-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 11, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-25](https://openairdocs.org/model/boeing-727-25) (registry code 1384006)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 18275
- Year built: 1964
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 20, 1964
- Certificate issued: November 16, 2004
- Last registry action: November 20, 2007
- Mode S code: A97299
- Owner when cancelled: [Air Trading International LLC](https://openairdocs.org/faa-owner/AIR%20TRADING%20INTERNATIONAL%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N708DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=708DH
- Page: https://openairdocs.org/deregistered/N708DH-2013-09-11

From the FAA registry file of October 31, 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 727-25: https://openairdocs.org/model/boeing-727-25.md

## Service difficulty reports (163, newest 50)

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

- [SDR DHL2002708009](https://openairdocs.org/sdr/DHL2002708009), Jul 12, 2002: BUTTON. BROKEN. SMOKE DETECTION SYSTEM NR 2 TEST BUTTON BROKE OFF DURING TEST. REPAIRED TEST BUTTON COVER IAW BMM 20-60-01.
- [SDR DHL2002708008](https://openairdocs.org/sdr/DHL2002708008), Jun 8, 2002: FIRE LOOP. OUT OF POSITION. NR 1 FIRE PROTECTION DETECTOR LIGHT ON. REPOSITIONED FIRE LOOP NR 1 ENG, OPS CHECKED GOOD IAW M/M 26-11-00.
- [SDR DHL2002708007](https://openairdocs.org/sdr/DHL2002708007), Jun 5, 2002: FIRE LOOP. OUT OF POSITION. ENG NR 1 FIRE DETECTION GROUND FAULT LIGHT FLASHES IN FLIGHT. REPOSITIONED ENG NR 1 FIRE LOOP AND REMOVED AND REPLACED NR 1 GROUND FAULT LENS COVER WITH NEW LEN
- [SDR DHL2002708006](https://openairdocs.org/sdr/DHL2002708006), May 14, 2002: WINDSHIELD WIPER. OUT OF ADJUST. CAPTAIN'S SIDE WINDSHIELD WIPER DOES NOT FUNCTION IN THE LOW POSITION THE WIPER DOES NOT HAVE ADEQUATE RANGE OF MOTION TO KEEP THE UPPER PORTION OF THE WINDSHIE
- [SDR DHL2002708005](https://openairdocs.org/sdr/DHL2002708005), Apr 15, 2002: POWER SUPPLY. NOT SEATED. APU FIRE DETECT SYS WILL NOT TEST. RESEATED APU FIRE WARNING POWER SUPPLY. OPS GOOD IAW MM 26-15-0.
- [SDR DHL2002708004](https://openairdocs.org/sdr/DHL2002708004), Mar 30, 2002: LIGHT. INOPERATIVE. COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE IN TEST. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CK NORMAL IAW B727 MM 33-50-1.
- [SDR DHL2002708003](https://openairdocs.org/sdr/DHL2002708003), Mar 26, 2002: TRANSMISSION. FAILED. CAPTAIN WINDSHIELD WIPER IS INOP. REMOVED AND REPLACED WINDSHIELD WIPER TRANSMISSION IAW B-M/M 30-42-11, OPS CHECK GOOD.
- [SDR DHL2002708002](https://openairdocs.org/sdr/DHL2002708002), Jan 28, 2002: LIGHT. INOPERATIVE. FWD ENTRY EMERGENCY EXIT LIGHT INOP IN TEST POSITION (ON POSITION). REMOVED AND REPLACED FWD ENTRY WAY EMERGENCY EXIT LIGHT ASSY IAW M/M 33-5-00. OPS CHECK SERV
- [SDR DHL2002708001](https://openairdocs.org/sdr/DHL2002708001), Jan 27, 2002: GLARE SHIELD. OUT OF POSITION. F/O'S SLIDING WINDOW IS BINDING AGAINST GLARE SHIELD WHEN TRYING TO OPEN WINDOW. REPOSITIONED GLARE SHIELD AT F/O'S SLIDING WINDOW. OPS CHECK SERVICEABLE PER B7
- [SDR DHL2001708016](https://openairdocs.org/sdr/DHL2001708016), Dec 18, 2001: WINDSHIELD WIPER. OUT OF ADJ. F/O WINDSHIELD WIPER DOES NOT WORK ON HALF SPEED. RUNS SLOW ON 3/4 SPEED.ADJUSTED WIPER TENSION PER 727 MM CHAPTER 30-42-01, OPS CK SATISFACTORY.
- [SDR DHL2001708014](https://openairdocs.org/sdr/DHL2001708014), Nov 28, 2001: FIRE LOOP. OUT OF POSITION. NR 2 ENGINE GROUND DET LIGHT ON DIM. OPENED COWLING, CLEARED FIRE LOOP FROM COWLING, CLOSED COWLING AND OP TEST NORMAL PER MM 26-00.
- [SDR DHL2001708015](https://openairdocs.org/sdr/DHL2001708015), Nov 24, 2001: SKIN. CRACKED. LEFT WING INBOARD AILERON UPPER SURFACE HAS 2 CRACKS 5.5 INCHES APART. OUTBOARD CRACK APPROX 2.25 INCHES LONG, INBOARD APPROX 2 INCHES. REMOVED EXISTING I/B AIL
- [SDR DHL2001708013](https://openairdocs.org/sdr/DHL2001708013), Oct 4, 2001: FIRE LOOP. OUT OF POSITION. 1) NR 1 GROUND DETECTOR CIRCUIT ILLUMINATED IN FLIGHT.2) REPOSITIONED NR 1 ENGINE LOOP-NO FAULTS NOTED.OPS CK SATISFACTORILY PER MM 26-11-000.THIS CLEARS DMI 72
- [SDR DHL2001708012](https://openairdocs.org/sdr/DHL2001708012), Aug 30, 2001: CONTROL VALVE. FAILED. LT MAIN GEAR BRAKE DRAGGING ON TAXI OUT. TAXI BACK TO GATE PER PHONE PATCH. MX FLT CONT CVG LT MAIN BRAKE FIRE THERMAL DISCHARGED TIRE 1 TIRE 2 FIRE LAST OVER 4
- [SDR DHL2001708010](https://openairdocs.org/sdr/DHL2001708010), Jul 22, 2001: FIRE LOOP. GROUNDED. NR 1 FIRE PROTECTION DET CIRCUIT GRD LIGHT ILLUMINATED IN FLT. FOUND ON ENG NR 1 FIRE PROTECTION LOOP WAS GROUNDING ON ENGINE COWLING, REPOSITIONED LOOP IAW B72
- [SDR DHL2001708009](https://openairdocs.org/sdr/DHL2001708009), Jul 21, 2001: FIRE LOOP. OUT OF POSITION. ENGINE NR 1 DETECTOR CIRCUIT GRD WAS ILLUMINATED ON TAXI OUT FROM MCO. FOUND NR 1 ENG LOOP TOUCHING A BRACKET. REPOSITIONED LOOP. SYS NOW OPS CHECK NORMAL PER M
- [SDR DHL2001708008](https://openairdocs.org/sdr/DHL2001708008), Jul 7, 2001: ACTUATOR. IN WINGS LEVEL DESCENT @ 280 KNOTS IAS SPEED BRAKE DEPLOYMENT CAUSES AIRCRAFT TO ROLL TO THE RIGHT. STOWING SPEED BRAKE CAUSES AIRCRAFT TO ROLL ABRUPTLY LEFT 15
- [SDR DHL2001708007](https://openairdocs.org/sdr/DHL2001708007), Jul 6, 2001: CONTROLLER. MALFUNCTIONED. WHEN DEPLOYING FLIGHT SPOILERS AIRCRAFT ROLLS RT, WHEN STOWING FLIGHT SPOILERS AIRCRAFT ROLLS ABRUPTLY TO THE RT. INSPECTED ALL SPOILERS FOR DELAM, NONE NOTED. 
- [SDR DHL2001708006](https://openairdocs.org/sdr/DHL2001708006), Jun 21, 2001: COMPUTER. FAULTY. DURING CRUISE FLT ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. ELEVATOR FEEL DIFF PRESSURE LIGHT STAYED ILLUMINATED. REPLACED EL
- [SDR DHL2001708005](https://openairdocs.org/sdr/DHL2001708005), Jun 21, 2001: RECEIVER. UNSERVICEABLE. RADAR PAINTS GROUND CLUTTER AT 6 DEG TILT UP, WHEN TURNING PAINTS GROUND.CORRECTIVE ACTION - R&R RADAR RT PER M/M 34-41-01 OPS CK NORMAL. STATUS-CLOSED.
- [SDR DHL2001708003](https://openairdocs.org/sdr/DHL2001708003), May 23, 2001: STUD. MISSING. PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL. SHUTDOWN WHEN OIL PRESSURE STARTED TO DECREASE. ENGINE OIL PRESS/TEMP GOOD UNTIL TOUCHDOWN. PERFORMED ABNORMAL
- [SDR DHL2001708004](https://openairdocs.org/sdr/DHL2001708004), May 18, 2001: ENGINE. UNSERVICEABLE. REMOVED AND REPLACED ENG FOR EXCESSIVE OIL CONSUMPTION. REF W/O 600003170. REMOVED NR 1 ENG AND REPLACED PER DHL 727 TASK MANUAL MANUAL 71-01-03 THRU 71-01-18.
- [SDR DHL2001708002](https://openairdocs.org/sdr/DHL2001708002), Mar 16, 2001: GEARBOX. LEAKING. NR 1 ENGINE LOST OIL QUANTITY AND PRESSURE IN FLIGHT. COMMENCED ENGINE SHUTDOWN AT INDICATION OF LOW OIL PRESSURE. T/S SYSTEM. REMOVED AND REPLACED N2 GEARBOX I
- [SDR DHL2001708001](https://openairdocs.org/sdr/DHL2001708001), Jan 11, 2001: ALTIMETER. UNSERVICEABLE. ALTIMETER SPLIT BETWEEN CAPT AND F/O'S POSITION BY 70 FEET.INSTALLED SERVO-PNUMATIC ALTIMITER IN CAPTS POSITION PER M/M 34-11-0,OPS CHK GOOD.
- [SDR DHL2000708027](https://openairdocs.org/sdr/DHL2000708027), Dec 21, 2000: SENSOR. DAMAGED. AFTER T/O NR 3 ENG STRUT OVERHEAT LIGHT ILLUMINATED,ABNORMAL PROCEDURES COMPLIED WITH. PLACED NR 3 ENGINE MODULATING VALVE ON DEFERRAL PER DHL MEL 36-11, DMI 36
- [SDR DHL200070806C](https://openairdocs.org/sdr/DHL200070806C), Sep 20, 2000: PANEL. CRACKED. VERT STAB RT LWR SLIDING SEAL TRACK AREA LWR FIX PANEL HAS 2 CRACKS. REMOVED AND REPLACED PANEL PER SRM 55-30-2. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070812C](https://openairdocs.org/sdr/DHL200070812C), Sep 14, 2000: PANEL. CRACKED. PANEL NR 3429 I/B LARGE PANEL RADIOUS CORNER CRACK PROGRESSIVE BEYOND STOP DRILL HOLE. CUT OUT DAMAGED AREA AT PANEL PER SRM 51-40-1. INSTALLED DOUBLER REPAIR P
- [SDR DHL2000708020](https://openairdocs.org/sdr/DHL2000708020), Sep 14, 2000: PANEL. CRACKED. PANEL 5512 MOUNT HOLE CRACK. REPLACED PANEL 12 X 25 INCH PER SRM 51-30-2.
- [SDR DHL200070809C](https://openairdocs.org/sdr/DHL200070809C), Sep 13, 2000: FLANGE. CRACKED. NR 9 L/E SLAT I/B TRACK O/B MOUNT AFT FLANGE IS CRACKED. ROUTED OUT CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-3. TREATED AND PRIMED PER SRM 
- [SDR DHL2000708012](https://openairdocs.org/sdr/DHL2000708012), Sep 13, 2000: STRUCTURE. DAMAGED. OUTBOARD FLAP T/E HONEYCOMB DETERIORATING. REPAIRED PER SRM 51-40-1. SIZE OF REPAIR 10 X 3 INCH.
- [SDR DHL2000708005](https://openairdocs.org/sdr/DHL2000708005), Sep 13, 2000: RIB. CRACKED. LEFT WING LEADING EDGE SLAT RIB AFT FLANGE IS CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-50-3. SIZE OF REPAIR 8 X 2 INCH.
- [SDR DHL200070802C](https://openairdocs.org/sdr/DHL200070802C), Sep 12, 2000: STRINGER. CORRODED. EVIDENCE OF CORROSION AT S 23R BETWEEN BS 480 AND 500. REMOVED FASTENERS AND CUT OUT SECTION OF STR 23RT BETWEEN STA 480 AND 500 PER SRM 53-10-3. INSTALLED STR 
- [SDR DHL200070808C](https://openairdocs.org/sdr/DHL200070808C), Sep 11, 2000: RIB. CRACKED. RT WING NR 4 6 L/E SLAT O/B TRACK I/B MOUNT RIB AFT FLANGE IS CRACKED AT HORIZ NUT PLATE STRAP UPPER ANGLE. REMOVED FASTENERS AT NR 6 SLAT O/B TRACK I/B RIB PER
- [SDR DHL200070807C](https://openairdocs.org/sdr/DHL200070807C), Sep 11, 2000: FITTING. DAMAGED. FWD CARGO COMPT RT SIDE BS 480 STATIC PORT FITTINGS PROTECTOR PANEL HAS BROKEN LUG AND MISSING FASTENER. INSTALLED NEW COVER PROTECTOR PER SRM 53-10-2. ALODINED
- [SDR DHL200070805C](https://openairdocs.org/sdr/DHL200070805C), Sep 11, 2000: STRINGER CLIP. CORRODED. FWD BAGGAGE COMPT S-20L AT BS 500 WHERE CLIP ATTACHED TO STRINGER HAS A PIN HOLE AND SUSPECTED CORROSION. CUT OUT DAMAGED AREA PER SRM 53-10-3. TREATED AND PRIM
- [SDR DHL2000708024](https://openairdocs.org/sdr/DHL2000708024), Sep 11, 2000: LATCH. CRACKED. FWD CARGO DOOR UP LOCK LATCH BRACKET LATCH CRACK. REPLACED LATCH PER SRM 51-10-2. MATERIAL USED 10 X 20 INCH.
- [SDR DHL2000708021](https://openairdocs.org/sdr/DHL2000708021), Sep 11, 2000: ANGLE. SHEARED. SKIN BULGING, FASTENERS SHEARED ANGLE CORRODED AT TAIL SKID RIGHT SIDE STATION 1203. REPAIR PER B727 SRM 51-40-3, 51-30-2, 53-30-2. SIZE OF REPAIR 20 X 10 INCH.
- [SDR DHL2000708006](https://openairdocs.org/sdr/DHL2000708006), Sep 11, 2000: WEB. CRACKED. STA 294.5 STR 15L HORIZONTAL WEB HAS CRACK GOING BEYOND STOP DRILL. REPLACED HORIZONTAL WEB PER SRM 53-10-1.
- [SDR DHL2000708019](https://openairdocs.org/sdr/DHL2000708019), Sep 9, 2000: PRESSURE PANEL. CRACKED. NOSE WHEEL WELL CEILING WEB PANEL SHOW CRACKS RUNNING FROM BS 268.5 AND LBL 20. INSTALLED 13 X 19 INCH DOUBLER PER B727 SRM 51-30-2.
- [SDR DHL2000708007](https://openairdocs.org/sdr/DHL2000708007), Sep 9, 2000: ANGLE. CRACKED. FUSELAGE LOWER EXTERIOR BS 610 RT SIDE FAIRING PANEL ANGLE SUPPORT SHOWS CRACKS. INSTALL ANGLE SUPPORT. SIZE OF REPAIR 35 X 1 X 4 INCH.
- [SDR DHL200070813C](https://openairdocs.org/sdr/DHL200070813C), Sep 8, 2000: WEB. CRACKED. MCD INTERNAL UPPER ROW OF LIGHTENING HOLES LOWER ROW NR 11 HOLE HAS A CRACK. TRIMMED OUT CRACK PER SRM 51-40-2. INSTALLED DOUBLER PER SRM 51-40-2. ALODINED AND 
- [SDR DHL200070810C](https://openairdocs.org/sdr/DHL200070810C), Sep 8, 2000: ANGLE. CRACKED. MAIN CARGO DOOR FWD EDGE LWR SECTION, SMALL SECTION OF LINING CRACKED. INSTALLED NEW ATTCH ANGLE AT MCD FWD EDGE LWR SECTION PER SRM 51-10-1. TREATED AND PRIMED
- [SDR DHL200070803C](https://openairdocs.org/sdr/DHL200070803C), Sep 8, 2000: FRAME. CRACKED. CARGO CABIN CIRCUMFERENTIAL FRAME BS 480 CRACKED WHERE ATTACH TO FUS STR 16/17L CRACK ABOUT 6 INCHES LONG. REMOVED FASTENERS AT CIRC FRAME STA 480 PER SRM 51-30
- [SDR DHL200070801C](https://openairdocs.org/sdr/DHL200070801C), Sep 8, 2000: DUCT. CRACKED. EVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REMOVED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCT PER SRM 51-30-2. TREAT
- [SDR DHL2000708026](https://openairdocs.org/sdr/DHL2000708026), Sep 8, 2000: STRAP. CRACKED. EVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REPAIRED PER B727 SRM 51-10-2, 51-30-2. MATERIAL USED 12 X 20 INCH.
- [SDR DHL2000708014](https://openairdocs.org/sdr/DHL2000708014), Sep 8, 2000: SEAT TRACK. CORRODED. CORRODED CABIN SEAT TRACK AT LBL 25 BS 400. INSTALLED 40 INCHES OF NEW SEAT TRACK PER SRM 53-10-5.
- [SDR DHL2000708011](https://openairdocs.org/sdr/DHL2000708011), Sep 8, 2000: FLOORBEAM. CORRODED. LAVATORY AREA FLOORBEAM BS 328 AND BBL 54 AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER SRM 51-40-4. SIZE OF REPAIR 35 X 9 INCH.
- [SDR DHL2000708010](https://openairdocs.org/sdr/DHL2000708010), Sep 8, 2000: FLOORBEAM. CORRODED. LAVATORY AREA FLOORBEAM BS 328 AND BBL 48 RIGHT AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER 51-40-4. SIZE OF REPAIR 35 X 9 INCH.
- [SDR DHL2000708009](https://openairdocs.org/sdr/DHL2000708009), Sep 8, 2000: FLOORBEAM. CORRODED. LAVATORY AREA FLOORBEAM BS 328 AND BBL 36 RIGHT AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER B727 SRM 51-40-4. SIZE OF REPAIR 35 X 9 INCH.
- [SDR DHL2000708008](https://openairdocs.org/sdr/DHL2000708008), Sep 8, 2000: WEB. CRACKED. WEB BENT AND CRACKED AT SEVERAL PLACES BETWEEN BS 1148 AND 1166 AT S-21R. INSTALL NEW INTERCOSTAL WEB PER SRM 53-10-1. SIZE OF REPAIR 16 X 4 INCH.

All 163: https://openairdocs.org/deregistered/N708DH-2013-09-11/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 19920831041329I](https://openairdocs.org/incident/19920831041329I), Aug 31, 1992: Boeing 72725 (N708DH), Houston, TX, Minor damage. Right main NR3 and NR4 and left main NR1 tires blew on rollout. Brakes locked up. Replaced brake antiskid unit.

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