# N703DH: 1967 Boeing 727-30C, registration cancelled 2013-06-11

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 11, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-30C](https://openairdocs.org/model/boeing-727-30c) (registry code 1384009)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 19010
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 6, 1984
- Certificate issued: September 7, 2004
- Last registry action: September 18, 2007
- Mode S code: A96006
- 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/N703DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=703DH
- Page: https://openairdocs.org/deregistered/N703DH-2013-06-11

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 727-30C: https://openairdocs.org/model/boeing-727-30c.md

## Service difficulty reports (110, newest 50)

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

- [SDR DHL2001703003](https://openairdocs.org/sdr/DHL2001703003), May 26, 2001: SWITCH. FAULTY. UPON FIRST GEAR EXTENSION INTO CVG NOSE GEAR GREEN LIGHT WAS INTERMITTENT. RECYCLED LANDING GEAR AND ALL INDICATIONS NORMAL. REMOVED AND REPLACED NOSE POSITION 
- [SDR DHL2001703002](https://openairdocs.org/sdr/DHL2001703002), Mar 23, 2001: INDICATOR. INOPERATIVE. A-SYSTEM HYDRAULIC QUANTITY INDICATOR INOP. PLACED ON DEFERRAL PER DMI 4858. MEL REF 29-14 CAT C.
- [SDR DHL2001703001](https://openairdocs.org/sdr/DHL2001703001), Feb 20, 2001: SKIN. CORRODED. STRINGER 19 RIGHT AT FS 369 TO FS 400 LAP SEAM HAS BULGING SKIN AROUND SEVERAL FASTENERS. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER 12.55 X 7.05 INCH D
- [SDR DHL2000703007](https://openairdocs.org/sdr/DHL2000703007), Dec 19, 2000: RESERVOIR. LOW. DURING TAXI WITH FLAPS EXTENDED "A" HYD SYS QUANTITY DECREASED TO 1.9 GALLONS, ON RETURN TAXI QUANTITY INCREASED TO 2.4 GALS WITH FLAPS RETRACTED. C/W A VISUAL 
- [SDR DHL2000703006](https://openairdocs.org/sdr/DHL2000703006), Oct 31, 2000: TIRE. FAILED. O/B LEFT MAIN TIRE BLOWN. REPLACED LEFT MAIN O/B AND I/B TIRES PER M/M 32-40.
- [SDR DHL2000703005](https://openairdocs.org/sdr/DHL2000703005), Oct 6, 2000: ADC. INTERMITTENT. INTERMITTENT GYRO FLAG ON CAPTAINS ADI AND FLIGHT DIRECTOR FLAGS ON BOTH CAPTAINS AND F/OS. REMOVED AND REPLACED FLIGHT DIRECTOR COMPUTER.
- [SDR DHL2000703004](https://openairdocs.org/sdr/DHL2000703004), Oct 6, 2000: GYRO. FAILED. INTERMITTENT GYRO FLAG AND FLIGHT DIRECTOR FLAG. REMOVED AND REPLACED VERTICAL GYRO AND FLIGHT INSTRUMENT AMPLIFIER.
- [SDR DHL2000703003](https://openairdocs.org/sdr/DHL2000703003), Sep 29, 2000: BRAKE. MALFUNCTIONED. AFTER ROTATION PRIOR TO GEAR RETRACTION THE LEFT I/B AND RIGHT O/B ANTI SKID RELEASE LIGHTS ILLUMINATED. PLACED ANTI SKID SYS ON DMI 2456 PER MEL 32-5. TROUBLES
- [SDR DHL2000703002](https://openairdocs.org/sdr/DHL2000703002), Sep 12, 2000: BULLET. CONTAMINATED. NR 3 ENGINE EPR READS HIGH N1 AND N2 LOW NR 3 THROTTLE 3 & 1/2 BEHIND NR 1 AND NR 2. BLEW DEBRIS FROM NR 3 BULLET. PERFORMED ENGINE RUN. OPS CHECK GOOD.
- [SDR DHLA200070301](https://openairdocs.org/sdr/DHLA200070301), Aug 18, 2000: STRINGER. CORRODED. FOUND LOCALIZED CORROSION AT STATION 650 STRINGER 18R IN LAP JOINT. INSTALLED FLUSH DOUBLER REPAIR ON LAP SEAM AT STR 18 RIGHT FROM BS 615 TO BS 621. REPAIR ACC
- [SDR DHL9970334C](https://openairdocs.org/sdr/DHL9970334C), Aug 6, 1999: TRACK. CRACKED. AT C CHECK, NR 3 FLAP TRACK MOVABLE FAIRING O/B TRACK CRACKED. REMOVED AND REPLACED TRACK PER SRM 51-30-2, N/R 5107.
- [SDR DHL9970342C](https://openairdocs.org/sdr/DHL9970342C), Jul 30, 1999: HINGE FITTING. CRACKED. AT C CHECK, RT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED RT TAIL SKID DOOR HINGE FITTING PER SRM 51-30-2, N/R 3198.
- [SDR DHL9970341C](https://openairdocs.org/sdr/DHL9970341C), Jul 30, 1999: HINGE FITTING. CRACKED. AT C-CHECK, LEFT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT TAIL SKID DOOR HINGE FITTING AS PER SRM 51-30-2, N/R 3197.
- [SDR DHL9970336C](https://openairdocs.org/sdr/DHL9970336C), Jul 30, 1999: BULKHEAD SKIN. CRACKED. AT C CHECK, CRACK AT BS 1183 BULKHEAD SKIN AFT CARGO COMPT WL 182 LBL 15. REMOVED FASTENERS AND STOP DRILLED CRACK PER SRM 51-30-2, AND 51-10-1 PG NR 7. PERFOMR
- [SDR DHL9970335C](https://openairdocs.org/sdr/DHL9970335C), Jul 30, 1999: BULKHEAD SKIN. CRACKED. C-CK, CRACK BS 1183 BULKHEAD SKIN, AFT BAG COMPT WL 182 RBL 15. OVERSIZED HOLE BY .015625 TO REMOVE INDAT WL190 RBL 15.5 AND ACCOMP PER SRM 51-10-1, VERIFIED CR
- [SDR DHL9970348C](https://openairdocs.org/sdr/DHL9970348C), Jul 29, 1999: BULKHEAD. DAMAGED. AT C CHECK, REPLACED TEMP REPAIR WITH PERMANENT REPAIR BS 870 BULKHEAD WEB. REF: AVITAS ENG LETTER 98 PMS 1.213D-1. REMOVED TEMPORARY REPAIR AT BS 870. REMOVED 
- [SDR DHL9970347C](https://openairdocs.org/sdr/DHL9970347C), Jul 29, 1999: SKIN. DAMAGED. AT C CHECK, LT INBD HORIZONTAL STABILIZER LEADING EDGE DAMAGED. REMOVED LEADING EDGE FOR APPROX STA 20 LE TO LE STA 147.32 PER SRM 51-30-2. REMOVED RIBS TO AID 
- [SDR DHL9970344C](https://openairdocs.org/sdr/DHL9970344C), Jul 29, 1999: ANGLE. CRACKED. C-CK, LT WING BS 930 LBL 64 VERT ANG CRACKED. R & R FITTING AT LT STA 930 LBL 64, ALOD & PRIM. INSTALL SPLICES STA 920 STR 15/16 RT. INSTALL REPAIR STR 14 & SUB
- [SDR DHL9970328C](https://openairdocs.org/sdr/DHL9970328C), Jul 27, 1999: BOLTS. CRACKED. AT C CHECK, 2 EA SLAT ROLLER BOLTS CRACKED AT LUBE HOLE AND 6 EA SLAT ROLLER BOLTS WORN. REPLACED PER MM 27-81-11, N/R 2074.
- [SDR DHL9970329C](https://openairdocs.org/sdr/DHL9970329C), Jul 23, 1999: SKIN. CRACKED. AT C CHECK, RT WING FIXED LEADING EDGE CUT OUT FOR THE NR 5 SLAT INBD TRACK IS CRACKED. REMOVED SEALS TO GAIN ACCESS TO BACKSIDE OF LEAD EDGE OF WING PER SRM 57
- [SDR DHL9970330C](https://openairdocs.org/sdr/DHL9970330C), Jul 22, 1999: HINGE. CRACKED. AT C CHECK, LW NR 7 SPOILER PANEL CENTER HINGE CASTING OUTBOARD LEG CRACKED AT AFT HOLE. CUT OUT CRACK FROM HINGE CASTING 2 LONG PER SRM 51-10-1, DYE PENETRANT 
- [SDR DHL9970317C](https://openairdocs.org/sdr/DHL9970317C), Jul 22, 1999: TAIL CONE. DELAMINATED. AT C CHECK, TAIL CONE HAS DELAMINATION AT LEFT TOP AREA. REMOVED VERTICAL STABILIZER TAILCONE PER SRM 51-30-2. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40
- [SDR DHL9970345C](https://openairdocs.org/sdr/DHL9970345C), Jul 21, 1999: DOOR. CORRODED. AT C CHECK, GALLEY DOOR UPPER FLAP HINGE HAS CORROSION. REMOVED GALLEY DOOR UPPPER FLAP PER MM 20-10-1. INSTALLED GALLEY DOOR UPPER FLAP (GATE ASSY) PER MM 52-1
- [SDR DHL9970332C](https://openairdocs.org/sdr/DHL9970332C), Jul 21, 1999: BULKHEAD PANEL. CRUSHED. AT C CHECK, RT BS 1183 BULKHEAD PANEL IS CRUSHED AT LOWER END. REPLACED RT STA 1183 BLKHD PANEL PER 53-20-11 MATERIAL USED P/N AE4155-81162, APPROXIMATELY 7X4N/
- [SDR DHL9970331C](https://openairdocs.org/sdr/DHL9970331C), Jul 21, 1999: MOUNT. CRACKED. AT C CHECK, ENGINE NR 1 GEARBOX FWD MOUNT CRACKED. REMOVED G/B PER MM-72-00, INSTALLED O/H G/B PER MM-72-0. INSTALLED FUEL LINE FROM FUEL OIL COOLER PER MM 28-4
- [SDR DHL9970325C](https://openairdocs.org/sdr/DHL9970325C), Jul 21, 1999: LONGERON. CRACKED. AT C CHECK, NR 1 LOWER COWL OUTBOARD LONGERON IS CRACKED UNDER RUB PLATE BY NR 3 LATCH V-BOLT CUTOUT. ALSO, SKIN IS BENT AND CRACKED AROUND CUTOUT. REWORKED SKI
- [SDR DHL9970320C](https://openairdocs.org/sdr/DHL9970320C), Jul 21, 1999: SKIN. CORRODED. AT CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG ROW OF FASTENERS JUST FWD OF THE NR 8 SPOILER PANEL. REMOVED PANEL FOR REAIR, CLEANED MATING SURFACE ON WING, 
- [SDR DHL9970319C](https://openairdocs.org/sdr/DHL9970319C), Jul 21, 1999: BRACKET. CRACKED. AT C CHECK, FWD CARGO DOOR UPLOCK SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR UP LOCK SUPPORT BRACKET PER SRM 51-30-2. REPLACED FWD CARGO DOOR UPLOCK SUP
- [SDR DHL9970318C](https://openairdocs.org/sdr/DHL9970318C), Jul 21, 1999: STRUCTURE. CRACKED. AT C CHECK, FWD ENTRY DOOR INTERIOR FWD UPPER CORNER IS CRACKED. REMOVED INTERIOR FWD ENTRY DOOR PER SRM 51-30-2, FABRICATED NEW LINER SUPPORT FWD CORNER PER SR
- [SDR DHL9970316C](https://openairdocs.org/sdr/DHL9970316C), Jul 21, 1999: FAIRING. DELAMINATED. AT C CHECK, V STABILIZER HAS FAIRING DELAMINATED ON BOTH SIDES BELOW TAIL CONE. INSTALLED BONDING REPAIR AT VERTICAL STABILIZER FAIRINGS BELOW TAIL CONE PER SRM
- [SDR DHL9970314C](https://openairdocs.org/sdr/DHL9970314C), Jul 21, 1999: COWL. CHAFF. AT C CHECK, NR 1 TOP COWL OUTBOARD LONGERON HAS DEEP CHAFED SPOTS AT 46 AND 54 INCHES FROM AFT EDGE. REPLACED COLGERON SECTION PER SRM 51-40-2 AND 54-10-2 ON NR
- [SDR DHL9970313C](https://openairdocs.org/sdr/DHL9970313C), Jul 21, 1999: SKIN. CHAFED. AT C CHECK, ENGINE NR 2 FWD RT COWL LOWER FWD INSIDE CORNER DOUBLER CHAFFED THROUGH. REMOVED FASTENER AND DAMAGED DOUBLER PER SRM 51-30-2, CLEANED AND PRIMED AR
- [SDR DHL9970310C](https://openairdocs.org/sdr/DHL9970310C), Jul 21, 1999: DEPRESSOR. DAMAGED. AT C CHECK, SEAL DEPRESSOR AT MCD AFT OF NR 6 LATCH HAS A SQUARE .25 OF MATERIAL MISSING REQUIRES REPAIR. SMOOTHED DAMAGED SECTION PER SRM 51-40-1. ALODINED AND
- [SDR DHL9970308C](https://openairdocs.org/sdr/DHL9970308C), Jul 21, 1999: PANEL. CRACKED. AT C CHECK, V STAB ACCESS PANEL NR 9774 HAS REPAIRS CRACKING UP L/S. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1 USING RESIN 1304, 6 INCH BY 4 INC
- [SDR DHL9970305C](https://openairdocs.org/sdr/DHL9970305C), Jul 21, 1999: FAIRING. CORRODED. AT C CHECK, LEFT WING NR 1 MOVABLE FAIRING SKIN CORRODED AT FWD I/B SIDE AT FAIRING ATTACH POINT. REMOVED PAINT FROM SKIN CORRODED AREA PER MM 51-20-0, CUT 6 IN
- [SDR DHL9970340C](https://openairdocs.org/sdr/DHL9970340C), Jul 20, 1999: CARRIAGE. LOOSE. LS NR 4 FLAP CARRIAGE HAS THRUST NUT LOOSE, IT HAS EXCESS CLEARANCE BETWEEN SHIMS AND FLAP FITTING. REMOVED LEFT INBOARD FLAP ASSY PER MM 27-51-3. FOUND LEFT IN
- [SDR DHL9970339C](https://openairdocs.org/sdr/DHL9970339C), Jul 20, 1999: ANGLE. CRACKED. AT C-CHECK, LEFT WING LEADING EDGE CAVITY AREA FSS 115.0 VERTICAL ANGLE CRACKED LOSER SECTION. CUTOUT DAMAGED SECTION 3 BY 2 PER SRM 51-40-3. FABRICATED NEW VER
- [SDR DHL9970327C](https://openairdocs.org/sdr/DHL9970327C), Jul 20, 1999: SKIN. DAMAGED. AT C CHECK, LW TOP SKIN PANEL HAS FIBERGLASS REPAIR NOT FINISHED BETWEEN WING AND FUSELAGE. REMOVED LW TOP SKIN PANEL LOCATED BETWEEN WING AND FUSELAGE PER SRM 
- [SDR DHL9970326C](https://openairdocs.org/sdr/DHL9970326C), Jul 20, 1999: STIFFENER. CRACKED. AT C CHECK, LW VERT STIFFENER IS CRACKED AT LOWER END AT FALSE SPAR BELOW NR 5 SPOILER O/B SIDE. STOP DRILLED 1 CRACK PER SRM 57-50-6. REMOVED APPROX 6 OF FASTE
- [SDR DHL9970323C](https://openairdocs.org/sdr/DHL9970323C), Jul 20, 1999: BOLT. SHEARED. AT C CHECK, LT WING NR 3 LE SLAT ACTUATOR TIE DOWN BOLT IB LOWER BOLT SHEARED. REPLACE THE IB LOWER BOLT ON NR 3 LE SLAT ACTUATOR PER MM 20-80-1, N/R 1199.
- [SDR DHL9970322C](https://openairdocs.org/sdr/DHL9970322C), Jul 20, 1999: SKIN. CORRODED. AT C CHECK, RT WING INBOARD FORE FLAP HAS SURFACE CORROSION ON LOWER SKIN APPROXIMATELY 12 FROM OUTBD END. REMOVED CORROSION AT RT WING PER SRM 51-10-6, OUT OF 
- [SDR DHL9970321C](https://openairdocs.org/sdr/DHL9970321C), Jul 20, 1999: SKIN. DELAMINATED. AT C CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG PANEL 10 FORWARD OF NR 9 AND NR 10 SPOILER PANEL. REMOVED FASTENERS AT RT WING PANEL PER SRM 51-30-2. FOUND 
- [SDR DHL9970315C](https://openairdocs.org/sdr/DHL9970315C), Jul 20, 1999: PLATE. CRACKED. AT C CHECK, MAIN CARGO DOOR INTERIOR LOWER PLATE COVER FWD TO AFT SECTION HAS SEVERAL CRACKS AND DENTS ON SURFACE. REMOVED PLATE AT MAIN CARGO DOOR INTERIOR LOW
- [SDR DHL9970312C](https://openairdocs.org/sdr/DHL9970312C), Jul 20, 1999: LONGITUDINAL. CRACKED. AT C CHECK, E3 ELECTRONIC RACK UPPER RT LONGITUDINAL IS CRACKED 2 PLACES. STOP DRILLED CRACKS PER SRM 51-10-1 2 PLACES. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1 
- [SDR DHL9970309C](https://openairdocs.org/sdr/DHL9970309C), Jul 20, 1999: FLOOR. CRACKED. AT C CHECK, NOSE W/W PRESS FLOW HAS CRACK AT BS 284.5. REMOVED FLOOR PANEL AT FWD PER SRM 51-30-2. REMOVED 2 EACH OLD DOUBLERS PER SRM 51-30-2. CUT OUT DAMAGED 
- [SDR DHL9970307C](https://openairdocs.org/sdr/DHL9970307C), Jul 20, 1999: ANGLE. CRACKED. AT C CHECK, RT WING TRAILING EDGE COVER PANEL INBOARD SUPPORT ANGLE IS CRACKED AT WS 447.90 JUST INBOARD OF NR 11 SPOILER ACTUATOR. REMOVED AND REPLACED SUPPORT
- [SDR DHL9970302C](https://openairdocs.org/sdr/DHL9970302C), Jul 20, 1999: ANGLE. CRACKED. AT C CHECK, RT WING TRAILING EDGE COVE PANEL OUTBOARD SUPPORT ANGLE IS CRACKED AT WS 498.08 INBOARD OF THE NR 12 SPOILER ACTUATOR. REPLACED COVER PANEL OUTBRD S
- [SDR DHL9970301C](https://openairdocs.org/sdr/DHL9970301C), Jul 20, 1999: CIRCUMFERENTIAL. CRACKED. AT C CHECK, FWD CARGO COMPT, CRACK AT CIRCUMFERENTIAL STA 640 STRINGER 26L. REMOVED OLD REPAIR, STOP DRILLED CRACK, HFEC. INSTALLED REPAIR PARTS PER SRM 53-10-4
- [SDR DHL9970338C](https://openairdocs.org/sdr/DHL9970338C), Jul 19, 1999: BULKHEAD. CRACKED. AT C-CHECK, CRACK AT 1183 BULKHEAD SKIN AFT CARGO COMPT WL 172 RBL 8. REMOVED FASTENERS AND STOP DRILL CRACK AT 1183 BLKD WL 172 RBL 8. PERFORMED HFEC INSPECTIO
- [SDR DHL9970311C](https://openairdocs.org/sdr/DHL9970311C), Jul 19, 1999: RECEPTACLE. CRACKED. AT C CHECK, BARRIER NET ATTACH RECEPTACLE AT BS 364 BETWEEN STRINGERS 5L AND 6L UPPER MOUNT BRACKET MISSING ATTACH RIVET AND CRACKED. REMOVED BRACKET SUPPORT PE

All 110: https://openairdocs.org/deregistered/N703DH-2013-06-11/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 20001128037839I](https://openairdocs.org/incident/20001128037839I), Nov 28, 2000: Boeing 72730C (N703DH), Rochester, NY. (-23) On Tuesday, November 28, 2000, a dhl airways, inc B727, N703DH, landed on runway 22 at Rochester international airport (roc) and blew #1 tire. The…

## Other aircraft with N703DH

- [Registered now](https://openairdocs.org/aircraft/N703DH): Airbus S A S A321-271NX, S/N 13353

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