# N702DH: 1968 Boeing 727-30C, registration cancelled 2013-09-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 20, 2013 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 727-30C](https://openairdocs.org/model/boeing-727-30c) (registry code 1384009) - Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000) - Serial number: 19793 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: None - Airworthiness: Standard, transport - Airworthiness date: January 6, 1983 - Certificate issued: September 7, 2004 - Last registry action: September 18, 2007 - Mode S code: A95C4F - 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/N702DH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=702DH - Page: https://openairdocs.org/deregistered/N702DH-2013-09-20 From the FAA registry file of November 3, 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 (162, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DHL2001702014](https://openairdocs.org/sdr/DHL2001702014), Jul 17, 2001: CONNECTOR. CONTAMINATED. AUTOPILOT IS INOPERATIVE IN ALL ROLL MODES AIRCRAFT ROLLED HARD TO LEFT IN MANUAL MODE AND WAS UNRESPONSIVE TO INPUTS. CLEANED OXIDATION FROM ROLL SERVO CANNON - [SDR DHL2001702013](https://openairdocs.org/sdr/DHL2001702013), Jul 17, 2001: AUTOPILOT SYS. INTERMITTENT. AUTOPILOT ROLL CONTROL INTERMITTENT. WHEN MALFUNCTIONING AUTO PILOT ENGAGES AND ROLLS SHARPLY UNCOMMANDED. CANNOT DUPLICATE, NO HISTORY. FOUND OPS CHECK GOOD ON - [SDR DHL2001702012](https://openairdocs.org/sdr/DHL2001702012), May 18, 2001: SWITCH. DIRTY. UPON CLEARANCE FOR TAKEOFF, ADVANCED THRUST LEVER T/O CONFIG WARNING HORN SOUNDED (REF - SPEEDBRAKE WAS STOWED, TRIM SET FLAPS WERE 15 - 15 GREEN). CLEANED FLAP - [SDR DHL2001702011](https://openairdocs.org/sdr/DHL2001702011), May 12, 2001: WARNING SYSTEM. MALFUNCTIONED. REJECTED T/O IN ROC DUE TO T/O WARNING HORN. WE DEPART RUNWAY. RESET CONTROLS. ON NEXT ATTEMPT, NO FURTHER PROBLEMS. TESTED TAKEOFF WARNING SYSTEM PER MM 31-26- - [SDR DHL2001702010](https://openairdocs.org/sdr/DHL2001702010), Apr 24, 2001: SWITCH. STUCK. TAKEOFF WARNING HORN SOUNDED WHEN TAKEOFF THRUST WAS APPLIED WITH FLAPS AT 15, SPEED BRAKE STOWED, AND STAB TRIM AT 5.5. TAKEOFF WAS DISCONTINUED. FOUND TAKEOFF - [SDR DHL2001702009](https://openairdocs.org/sdr/DHL2001702009), Apr 11, 2001: SWITCH. OUT OF ADJ. TAKEOFF WARNING HORN SOUNDED DURING T/O ROLL 60 KTS. TAKEOFF REJECTED. VERIFIED T/O CONFIGURATION WAS CORRECTED. 2ND T/O NORMAL. FOUND SPEED BRAKE TAKEOFF WARNI - [SDR DHL2001702007](https://openairdocs.org/sdr/DHL2001702007), Mar 30, 2001: WINDSHIELD. FAILED. L-2 WINDSHIELD CRACKED DURING CRUISE FLIGHT. CORRECTIVE ACTION: REPLACED L-2 WINDOW IAW B727 MM 56-12-11. OPS CK SERVICABLE PRESSURIZED A/C ON GROUND. NO LEAKS - [SDR DHL2001702008](https://openairdocs.org/sdr/DHL2001702008), Mar 29, 2001: GEARBOX. LEAKING. IN CRUISE FLIGHT LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-40 PSI. PERFORMED OIL PRESS BELOW 40 PSI ABNORMAL CHECKLIST AND DISCOVERED - [SDR DHL2001702006](https://openairdocs.org/sdr/DHL2001702006), Mar 23, 2001: BOLT. SHEARED. MAIN CARGO DOOR WILL NOT CLOSE.CORRECTIVE ACTION: REPLACED SHEARED BOLTS AT FWD CAM LATCH PER MM 52-34-21. OPS CHECK GOOD. STATUS CLOSED. - [SDR DHL2001702003](https://openairdocs.org/sdr/DHL2001702003), Mar 2, 2001: PUMP. FAILED. NR 2 ENGINE FAILURE ON TAKEOFF ROLL AT 90 KTS. REMOVED AND REPLACED FUEL PUMP. FUEL CONTROL UNIT CHECKS GOOD PER M/M 73-11-1 & 72-00. - [SDR DHL2001702004](https://openairdocs.org/sdr/DHL2001702004), Feb 17, 2001: FLOORBEAM. CORRODED. AT FS 1050 LBL 3 ON BOTTOM OF FLOORBEAM WL 200 CORROSION ON FLOORBEAM AND GILLINER ATTACH ANGLE. REMOVED AND REPLACED LOWER SUPPORT TEE. - [SDR DHL2001702005](https://openairdocs.org/sdr/DHL2001702005), Feb 17, 2001: SEAT TRACK. DAMAGED. SIDE BASH BAR NR 3 AND 4 MUSHROOM OUT OF FLOOR TRACK. REMOVED AND REPLACED FLOOR TRACK FROM STA 480 TO 560 PER SRM 53-10-2 AND 53-10-5. - [SDR DHL2001702002](https://openairdocs.org/sdr/DHL2001702002), Jan 30, 2001: WARNING SYSTEM. FALSE ACTIVATION. DISCONTINUED TAKEOFF DUE TO TAKEOFF WARNING HORN. FLAPS, SPEEDBRAKE AND TRIM ALL PROPERLY SET. PERFORMED T/O WARN TEST PER MM 31-26-0 PARA 6, TEST OK. - [SDR DHL2001702001](https://openairdocs.org/sdr/DHL2001702001), Jan 6, 2001: WARNING SYSTEM. ACTIVATED. RTO BECAUSE OF FALSE T/O WARNING HORN-RECYCLED FLAPS, WARNING DID NOT SOUND WHEN T/L ADVANCED. PREFORMED T/O WARNING TEST,FOUND NORMAL OPS PER M/M 34-00 AND 31- - [SDR DHL2000702003](https://openairdocs.org/sdr/DHL2000702003), Oct 19, 2000: TRANSMITTER. STUCK. NR 3 ENGINE OIL PRESSURE INDICATION STUCK AT 10 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER IAW M/M 79-32-1. - [SDR DHL2000702002](https://openairdocs.org/sdr/DHL2000702002), Feb 18, 2000: CAM. CRACKED. MAIN CARGO DOOR SUPPORT CENTERING CAM CRACKED. INSTALLED CAM PER 53-30-0. - [SDR DHL2000701001](https://openairdocs.org/sdr/DHL2000701001), Feb 18, 2000: CAM. CRACKED. MAIN CARGO DOOR SUPPORT CENTERING CAM CRACKED. INSTALLED CAM PER 53-30-0. - [SDR DHL20007020](https://openairdocs.org/sdr/DHL20007020), Feb 4, 2000: PIN. INSTALLED. AFTER TAKEOFF, GEAR WOULD NOT RETRACT. RETURNED FOR LANDING AND FOUND GEAR PINS INSTALLED - [SDR DHL2000702001](https://openairdocs.org/sdr/DHL2000702001), Feb 4, 2000: PIN. INSTALLED. AFTER TAKEOFF, GEAR WOULD NOT RETRACT. RETURNED FOR LANDING AND FOUND GEAR PINS INSTALLED. - [SDR DHL99702001](https://openairdocs.org/sdr/DHL99702001), Aug 31, 1999: BOLT. LOOSE. WHEN SELECTING FLAP 2 DEGREE UPON FLAP RETRACTION, AMBER L/E LIGHT FAILED TO EXTINGUSH. NO AMBER L/E LIGHTS ON S/O AUX PANEL WERE ILLUMINATED. FOUND AND SECURED - [SDR DHL9970203C](https://openairdocs.org/sdr/DHL9970203C), Jun 30, 1999: FRAME. CRACKED. C CHECK, NR 1 ENGINE UPPER COWLING NR 14 FRAME HS EVIDENCE OF HEAVY CHAFING UNDER IMPROPER STRAP REPAIR AT 1/B FLANGE, AT O/B AFT CORNER OF COWL. REMOVED REPAIR - [SDR DHL9970244C](https://openairdocs.org/sdr/DHL9970244C), Jun 26, 1999: SEAT TRACK. CRACKED. C CHECK, LWR AFT CARGO COMPARTMENT RT SEAT TRACK CRACK AT BOTH FWD AFT ENDS. REPLACED DAMAGE SECTION OF SEAT TRACK FROM STA 950 TO STA 1030; INSTALLED REPAIR AT - [SDR DHL9970214C](https://openairdocs.org/sdr/DHL9970214C), Jun 25, 1999: SKIN. CRACKED. C-CHECK, CRACK INDICATION AT FASTENER ONE INCH RIGHT OF (BLO) STA 480. CUT-OUT DAMAGED AREA OF SKIN AT FWD SIDE STA 480 PRODUCTION BREAK BETWEEN BLO AND STR 28R - [SDR DHL9970211C](https://openairdocs.org/sdr/DHL9970211C), Jun 25, 1999: SKIN. CORRODED. C CHECK, PLUS 10 PERCENT MATERIAL LOSS AT STA 259 CIRCUIT BUTT SEAM APPRX S-9L LOCTION. INSTALLED DOUBLER REPAIR AT BS 259 STR 9L PER B727 S/B 727-53-0084 ALODI - [SDR DHL9970235C](https://openairdocs.org/sdr/DHL9970235C), Jun 24, 1999: SKIN. CRACKED. C CHECK, RT WING O/B AILERON, I/B UPPER SKIN CRACKED AT I/B TAB BOND WIRE ATTACHMENT FASTENER. REMOVED AILERON TAB, CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPA - [SDR DHL9970221C](https://openairdocs.org/sdr/DHL9970221C), Jun 24, 1999: FITTING. CRACKED. C CHECK NR 6 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED AT TOP FLANGE. CUT OUT DAMAGED AREAS I/B AND O/B SIDE OF NR 6 SPOILER ACT FITTING IAW AVITAS ENG. REPAI - [SDR DHL9970216C](https://openairdocs.org/sdr/DHL9970216C), Jun 24, 1999: ANGE. CRACKED. C CHECK, NR 2 ENG PYLON, ANGLE CRACKED AT AFT OF ENG-MOUNT. REMOVED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT IAW B727 SRM 51-30-2. REPLACED ANGLE AT NR 2 ENG - [SDR DHL9970245C](https://openairdocs.org/sdr/DHL9970245C), Jun 23, 1999: WEB. CORRODED. C-CHECK, MAIN CABIN SHEAR WEB PLATE HAS CORROSION BELOW THE PLATE BS 1176 LBL 26. REMOVED FASTENERS ON HAT CHANNEL ANGLE AT BS 1176 LBL26 AS PER SRM 51-30-2. CU - [SDR DHL9970242C](https://openairdocs.org/sdr/DHL9970242C), Jun 23, 1999: BRACKET. CRACKED. C-CHECK, RT WING T/E COVE PNL SUPPORT BRACKET CRACK AT FASTENER HOLE, I/B END OF NR 11 SPOILER PNL AND BELOW. REPLACED BRACKET AT I/B END OR NR 11 SPOILER PNL A - [SDR DHL9970234C](https://openairdocs.org/sdr/DHL9970234C), Jun 23, 1999: PANEL. CRACKED. C CHECK, LW PANEL ON TOP WING HAS I/B SIDE WITH CRACK AND WORN, O/B SIDE OF NR 5 SPOILER. REMOVED CRACKED METAL STRIP ON L/W PANEL O/B OF NR 5 SPOILER PER B727 - [SDR DHL9970229C](https://openairdocs.org/sdr/DHL9970229C), Jun 23, 1999: SUPPORT. CRACKED. C CHECK, RT WING L/E STRUCTURE, CEILING CROSS SUPPORT CRACKED AT O/B END, L/E STA 130.7. REMOVED UNSERVICEABLE CROSS SUPPORT AND REPLACED WITH NEW EXTRUSION ANG - [SDR DHL9970224C](https://openairdocs.org/sdr/DHL9970224C), Jun 23, 1999: FITTING. CORRODED. C-CHECK RT WING L/E FLAP NR 6, MIDDLE HINGE UPPER FITTING SUPPORT (MAGNESIUM) HAS SEVERAL AREAS OF CORROSION OR EROISION (MRKD). REMOVED UPPER HINGE FITTING AND - [SDR DHL9970223C](https://openairdocs.org/sdr/DHL9970223C), Jun 23, 1999: DOOR. MISREPAIRED. C CHECK, FWD CARGO COMPARTMENT DOOR, IMPROPER REPAIR DOUBLER INSUFFICIENT AMOUNT OF FASTENERS AND IMPROPERLY COVERING AREA OF DAMAGE. FS 550 AFT BOTTOM SEEN THR - [SDR DHL9970222C](https://openairdocs.org/sdr/DHL9970222C), Jun 23, 1999: SUPPORT. CRACKED. C CHECK, RT WING L/E STRUCTURE WBL 92.8 VERT SUPPORT CRACKED AT BOTTOM WITH SEVERAL STOP DRILLED HOLES. CUT OUT DAMAGED SECTON, INSTALLED ANGLE REPAIR 1 BY 1.5 - [SDR DHL9970210C](https://openairdocs.org/sdr/DHL9970210C), Jun 23, 1999: DOUBLER. CRACKED. C CHECK, FWD CARGO COMPARTMENT DOOR HAS A CRACKED DOUBLER AT THE AFT BOTTOM INTERIOR OF DOOR. THIS CAN BE SEEN WITH THE DOOR CLOSED AND INSIDE THE CARGO COMPART - [SDR DHL9970207C](https://openairdocs.org/sdr/DHL9970207C), Jun 23, 1999: SKIN. CORRODED. C CHECK, LW L/B AFT FLAP HAS CORROSION AND DELAMINATION AT I/B SIDE TOP SKIN. CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REP - [SDR DHL9970206C](https://openairdocs.org/sdr/DHL9970206C), Jun 23, 1999: SKIN. CORRODED. C CHECK, LW NR 2 FLAP (1/B) HAS MID FLAP WITH CORROSION AND DELAMINATION ON TOP SKIN ON TOP OF SECOND TRACK FOR AFT FLAP. CUT-OUT SMALL CORROSION AND DELAMINATI - [SDR DHL9970205C](https://openairdocs.org/sdr/DHL9970205C), Jun 23, 1999: FRAME. CRACKED. C CHECK, NR 2 ENG R4 FWD COWLING FRAME IS CRACKED AT NR 1 GUIDE AREA. CUT OUT DAMAGED SECTION, INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 13 BY 5, N/R 6041. - [SDR DHL9970201C](https://openairdocs.org/sdr/DHL9970201C), Jun 23, 1999: CASTING. CRACKED. C-CHECK, GALLEY DOOR CUTOUT LOWER AFT CORNER CASTING HAS CRACK AND GOUGE. REPLACED CASTING AT DOOR CUT OUT LOWER AFT CORNER IAW B77 SRM 51-30-2, N/R 3121. - [SDR DHL9970243C](https://openairdocs.org/sdr/DHL9970243C), Jun 22, 1999: SKIN. CRACKED. C-CHECK, NR 1 ENG INLET COWL CRACKED OUTER SKIN IN POSITION CRACK CONFIRMED BY NDT PART 6-51-00-00 HFEC JRT NDTI58. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL 1 - [SDR DHL9970238C](https://openairdocs.org/sdr/DHL9970238C), Jun 22, 1999: ANGLE. CRACKED. C-CHECK, NLG W/W AFT, SUPPORT ANGLE IS CRACKED AT STA 3441, ABOVE LOCK DOWN MECHANISM. REMOVED ANGLE, FOUND WEB CRACKED. CUT OUT DAMAGED AREA OF WEB, HFEC OF AR - [SDR DHL9970237C](https://openairdocs.org/sdr/DHL9970237C), Jun 22, 1999: SKIN. DAMAGED. C-CHECK, AFT UPPER AIRSTAIRS WELL TOP TORQUE BOX SKIN IS OIL CAN BS 1285. CUT OUT DAMAGED AREA AT AFT UPPER AIRSTAIRS WELL, TOP TORQUE BOX SKIN. MAT CUT OUT 18 - [SDR DHL9970236C](https://openairdocs.org/sdr/DHL9970236C), Jun 22, 1999: SKIN. DAMAGED. C-CHECK, RT UPPER AIRSTAIRS AREA, TOP TORQUE BOX SKIN IS OIL CAN BS 1263 TO 1243. CUT OUT DAMAGED AREA AT RT UPPER AIRSTAIR AREA TOP TORQUE BOX SKIN MAT CUT OUT - [SDR DHL9970233C](https://openairdocs.org/sdr/DHL9970233C), Jun 22, 1999: FLOOR. CRACKED. C CHECK, AFT CARGO COMPARTMENT AFT BULKHEAD AREA BOTTOM OF CABIN FLOOR HAS AREA OF CORROSION AND A CRACK LEFT SIDE. REMOVED FASTENERS AFT CARGO AFT BULKHEAD BOT - [SDR DHL9970232C](https://openairdocs.org/sdr/DHL9970232C), Jun 22, 1999: SEAT TRACK. CORRODED. C-CHECK, AFT CARGO COMPT STA 1166 RT SEAT TRACK CRACKED. CUT OUT DAMAGED SECTION FROM STA 1166 TO 1130 AS PER B727 SRM 53-10-5 FIG 8. INSTALLED NEW SECTION OF S - [SDR DHL9970231C](https://openairdocs.org/sdr/DHL9970231C), Jun 22, 1999: SEAT TRACK. CORRODED. C CHECK, AFT CARGO BIN SEAT TRACK CRACKED STA 970 RT SIDE. CUT AND TRIMMED NEW SECTION OF FLOOR TRACK, MADE SPLICE STRIPS, PICKED UP EXISTING FASTENER HOLES AND - [SDR DHL9970227C](https://openairdocs.org/sdr/DHL9970227C), Jun 22, 1999: PANEL. DELAMINATED. C-CHECK, RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E DELAMINATED (MRK). REMOVED PANEL NR 8505 RT WING LOWER SURFACE FOR FIBERGLASS REPAIR IAW B727-200 12-30- - [SDR DHL9970220C](https://openairdocs.org/sdr/DHL9970220C), Jun 22, 1999: FRAME. CRACKED. C CHECK, RIGHT SERVICE DOOR, THE DOOR FRAME HAS .5 INCH CRACK AREA OF FORWARD NR 2 STOP FROM THE BOTTOM. REMOVED RT SERVICE DOOR IAW B727 MM 52-40-0. INSTALLED - [SDR DHL9970213C](https://openairdocs.org/sdr/DHL9970213C), Jun 22, 1999: SKIN. CRACKED. C CHECK, LT/W O/B UPPER T/E PANEL O/B OF NR 1 SPOILER, I/B EDGE OLD REPAIR HAS CRACK AT FASTENER HOLE WS620. REPLACED O/D REPAIR STRAP PR B727 SRM 57-30-4 FIG 1 - [SDR DHL9970209C](https://openairdocs.org/sdr/DHL9970209C), Jun 22, 1999: SUPPORT. DAMAGED. C CHECK, FAIRING SUPPORTS AT B5 600 AND 610 ARE BENT AND CRACKED AT LEFT SIDE STRINGER 281. CUT OUT DAMAGED RIB WEB INSTALLED REPAIR PER B727 SRM 51-40-2 AT BS All 162: https://openairdocs.org/deregistered/N702DH-2013-09-20/reports.md --- 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.