# N715DH: 1967 Boeing 727-155C, registration cancelled 2017-07-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 7, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-155C](https://openairdocs.org/model/boeing-727-155c) (registry code 138404Z)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 19618
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 26, 1967
- Certificate issued: September 7, 2004
- Last registry action: September 18, 2007
- Mode S code: A98EF3
- 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/N715DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=715DH
- Page: https://openairdocs.org/deregistered/N715DH-2017-07-07

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 727-155C: https://openairdocs.org/model/boeing-727-155c.md

## Service difficulty reports (153, newest 50)

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

- [SDR DHL2002715010](https://openairdocs.org/sdr/DHL2002715010), Oct 22, 2002: WARNING SYSTEM. MALFUNCTIONED. RTO AT CVG MAXIMUM ATTAINED AIRSPEED 5 KIAS. UPON INITIATION OF TO THRUST, THE TO WARNING HORN SOUNDED. AFTER TAXIING CLEAR OF THE RUNWAY, NOTIFIED FLIGHT CONTR
- [SDR DHL2002715009](https://openairdocs.org/sdr/DHL2002715009), Jun 19, 2002: SWITCH. DIRTY. T/O WARNING HORN SOUNDED ON T/O ROLL. CLEANED CONTACTS ON AIRBRAKE POSITION SWITCH IN FWD NOSE BAY. OPS CHECK GOOD IAW 31-26-00.
- [SDR DHL2002715008](https://openairdocs.org/sdr/DHL2002715008), May 29, 2002: WARNING SYSTEM. MALFUNCTIONED. WHILE BRINGING POWER UP FOR TAKEOFF WITH AIRCRAFT CONFIGURED, GOT CONFIGURATION HORN AND SYSTEM THEN TESTED BAD ON TAXIWAY. ABORTED TAKEOFF. CYCLED FLAPS, TAKEO
- [SDR DHL2002715007](https://openairdocs.org/sdr/DHL2002715007), May 3, 2002: POWER UNIT. FAILED. APU FIRE WARNING BELL IN COCKPIT INOP, HORN IN NOSE WHEEL WELL WORKS NORMALLY. REMOVED APU FIRE DETECTION POWER UNIT AND CLEANED CONTACTS. REINSTALLED POWER UNI
- [SDR DHL2002715006](https://openairdocs.org/sdr/DHL2002715006), Apr 23, 2002: WARNING SYSTEM. ACTIVATED. TAKEOFF REJECTED FOR AURAL WARNING HORN. CYCLED FLAPS AND SPEED BRAKE, VERIFIED MOVEMENT OF FLT CONTROL SURFACES. PERFORMED AURAL OPERATIONAL CHECKOUT IAW 31-26
- [SDR DHL2002715005](https://openairdocs.org/sdr/DHL2002715005), Apr 13, 2002: WARNING HORN. FAILED. DURING APU FIRE WARNING TEST, FIRE BELL AND FIRE WARNING HORN FAIL SOUND. REMOVED AND REPLACED FIRE WARNING HORN IN NOSE WHEEL WELL IAW MM 26-11-00. OPS CHECK G
- [SDR DHL2002715004](https://openairdocs.org/sdr/DHL2002715004), Apr 10, 2002: FITTING. CRACKED. REPLACE MAIN CARGO DOOR LATCH FITTING. GAINED ACCESS TO MCD LATCH SUPPORT FITTING AT B.S. 580 THROUGH FWD. CARGO PIT LT SIDEWALL/ CEILING AND MAIN CABIN. REMOVE
- [SDR DHL2002715003](https://openairdocs.org/sdr/DHL2002715003), Apr 8, 2002: ANGLE. CRACKED. On weekly visit "discrepancy" Frame at door latch fitting is cracked in radius at BS 500, 4l 200, below S-17L.1) Upon further evaluation found attach angle "T" 
- [SDR DHL2002715002](https://openairdocs.org/sdr/DHL2002715002), Feb 2, 2002: POWER SUPPLY. INOPERATIVE. APU FIRE DETECTION SYSTEM WILL NOT TEST. TROUBLESHOT SYSTEM, REMOVED AND REPLACED APU FIRE DETECT OPERATING POWER SUPPLY. OPERATIONAL CHECK OF SYSTEM GOOD MM RE
- [SDR DHL2002715001](https://openairdocs.org/sdr/DHL2002715001), Jan 29, 2002: POWER UNIT. INOPERATIVE. APU FIRE TEST WILL NOT TEST. REPLACED APU FIRE DETECTION POWER UNIT IAW B727 M/M 26-15-00, OP CHECK GOOD.
- [SDR DHL2001715011](https://openairdocs.org/sdr/DHL2001715011), Dec 1, 2001: COMPUTER. FAULTY. WITH AUTO PILOT ENGAGED RAPID DEFLECTION OF CONTROL WHEEL OCCURS BOTH LEFT AND RIGHT OF ABOUT 10 DEGREES. DEFERRED AUTO PILOT SYSTEM AND MX CONTROL WAS NOTIFIED
- [SDR DHL2001715010](https://openairdocs.org/sdr/DHL2001715010), Aug 10, 2001: SKIN. DAMAGED. BELOW RIGHT CORNER OF MAIN CARGO DOOR (APPROX 3 FEET) A 4 INCH BY 1/4 GASH IN SKIN APPROX 1/4 DEEP. AREA IS ALSO DENTED, ALSO 2 AREAS ADJACENT TO GASH ARE DOWN 
- [SDR DHL2001715009](https://openairdocs.org/sdr/DHL2001715009), Aug 8, 2001: WARNING SYSTEM. MALFUNCTIONED. TAKEOFF WARNING CAME ON AT THE TAKEOFF ROLL, TAXIED CLEAR OF THE RUNWAY AND CYCLED THE FLAPS,TRIM AND SPEED BRAKE SYSTEM WENT BACK TO NORMAL. PERFORMED TAKEOFF 
- [SDR DHL2001715008](https://openairdocs.org/sdr/DHL2001715008), Jun 30, 2001: DOWNLOCK SWITCH. DURING GEAR EXTENSION @ CVG LT. MAIN GEAR LIGHT DID NOT ILLUMINATE. RED LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, PROBLEM WAS NOT
- [SDR DHL2001715007](https://openairdocs.org/sdr/DHL2001715007), Jun 29, 2001: COMPUTER. FAULTY. WITH AUTOPILOT A SERVO SELECTED, A/C PITCHES UP AND DOWN. OK WITH SERVO B SELECTED. DEFFERED AUTO PILOT A-MODE PER MEL 22-1-11A, CAT C, DMI 6211. PLACARDS INSTA
- [SDR DHL2001715006](https://openairdocs.org/sdr/DHL2001715006), May 26, 2001: COMPUTER. MALFUNCTIONED. ON CLIMBOUT IN A-MODE AUTOPILOT PORPOISED. REPLACED PITCH CHANNEL PER MM 22-11-101. OPS CKS GOOD. THIS CLEARS DMI 5771.
- [SDR DHL2001715005](https://openairdocs.org/sdr/DHL2001715005), May 26, 2001: RECEIVER. UNSERVICEABLE. AUTOPILOT WILL NOT TRACK VOR IN NAV/LOC MODE. REPLACED NR 1 NAV RCVR PER MM 34-31-21, OPS CKS GOOD. THIS CLEARS DMI 5772.
- [SDR DHL2001715004](https://openairdocs.org/sdr/DHL2001715004), Apr 10, 2001: SILL. CRACKED. FAA INSPECTION FOUND LWR BELLY DOOR FWD THRESHOLD SILL-PLATE CRACKED.REMOVED OLD SILL-PLATE AND INSTALLED SERVICABLE PLATE IAW M/M 53-13-0. STATUS-CLOSED.
- [SDR DHL2001715003](https://openairdocs.org/sdr/DHL2001715003), Mar 27, 2001: BEARING. SEPARATED. VIBRATION DURING TAXI AND A/C REQUIRES HIGHER THAN NORMAL THRUST TO TAXI. NR 1 MAIN TIRE NUT AND BEARING SEPERATED. REPLACED LT MLG LOWER CYLINDER ASSY. FOUND N
- [SDR DHL2001715001](https://openairdocs.org/sdr/DHL2001715001), Jan 3, 2001: BULB. BURNED OUT. UPPER MAIN CARGO SMOKE DETECTORS NOT VISIBLE. RELAMPED UPPER SMOKE DETECTOR. OPS CHECK GOOD I.A.W 26-17-01
- [SDR DHL2000715026](https://openairdocs.org/sdr/DHL2000715026), Dec 13, 2000: HINGE. BENT. LOUD WHISTLE HEARD DURING CLIMBOUT, STARTED AT 2 PSI THEN GEAR WARNING HORN SOUNDED. WHISTLE STOPPED AT 6 PSI DURING DECENT. FOUND L-1 ENTRY DOOR SEAL PULLED OU
- [SDR DHL2000715003](https://openairdocs.org/sdr/DHL2000715003), Oct 27, 2000: DOUBLER. DAMAGED. PANEL NUMBER 9216 HAS INTERNAL REPAIR CRACKED. REPLACED DOUBLER. SIZE OF REPAIR 6 X 4.5 INCHES.
- [SDR DHL2000715006](https://openairdocs.org/sdr/DHL2000715006), Oct 23, 2000: ANGLE. CORRODED. FAIRING SUPPORT ANGLE HAS CORROSION ON UPPER SURFACE BS 660 UNDER STRINGER 27R. INSTALL REPAIR PER B727 SRM 51-40-3, 51-10-2. MATERIAL SIZE 30 X 2 INCHES.
- [SDR DHL2000715025](https://openairdocs.org/sdr/DHL2000715025), Oct 21, 2000: PANEL. CORRODED. CORROSION AT FAIRING PANEL 3430 FWD FLANGE LOCATED AT BS 660. INSTALL REPAIR PER B727 SRM 53-10-01, 51-40-3. SIZE OF MATERIAL USED 30 X 2 INCHES.
- [SDR DHL2000715024](https://openairdocs.org/sdr/DHL2000715024), Oct 12, 2000: ANGLE. BENT. MCD TOP CUTOUT HAS A ANGLE WITH DENT AND BENT AT BS 600. REPLACED ANGLE PER B727 SRM 51-10-1 & 2. SIZE OF MATERIAL 12.5 X 6 INCHES.
- [SDR DHL2000715023](https://openairdocs.org/sdr/DHL2000715023), Oct 12, 2000: STRUCTURE. DAMAGED. MCD HAS ALUMINUM SHEET WITH EXCESS HOLES BS 620 (VERTICAL). REPAIRED PER B727 SRM 51-10-1 & 2, 51-30-2. SIZE OF MATERIAL USED 21 X 3.5 INCHES.
- [SDR DHL2000715022](https://openairdocs.org/sdr/DHL2000715022), Oct 12, 2000: ANGLE. CRACKED. M.C.D. HAS ALUMINUM SEAL PROTECTOR CHAFED AND CRACKED AT LOWER END. REMOVED AND REPLACED SEAL PROTECTOR PER B727 SRM 51-30-2, 51-40-3.
- [SDR DHL2000715012](https://openairdocs.org/sdr/DHL2000715012), Oct 12, 2000: STRUCTURE. CHAFED. MAIN CARGO DOOR FWD CUTOUT HAS VERTICAL STRIP CHAFED BS 480 S-6L. FABRICATED AND INSTALLED NEW FRAME PER B727 SRM 51-40-3. SIZE OF REPAIR 8 X 28 INCHES.
- [SDR DHL2000715010](https://openairdocs.org/sdr/DHL2000715010), Oct 12, 2000: DOOR FRAME. BENT. MAIN CARGO DOOR UPPER AFT FRAME FOUND BENT. FABRICATED AND INSTALLED NEW UPPER AFT FRAME PER B727 SRM 51-30-2 AND 51-10-3. SIZE OF REPAIR 8 X 28 INCHES.
- [SDR DHL2000715021](https://openairdocs.org/sdr/DHL2000715021), Oct 11, 2000: FLOOR SUPPORT. CRACKED. LOWER AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 1090 AND BBL 27. INSTALL NEW ANGLE SUPPORT PER B727 SRM 51-30-2, 53-10-1 AND -2. SIZE OF MATERIAL USED 1
- [SDR DHL2000715020](https://openairdocs.org/sdr/DHL2000715020), Oct 11, 2000: FLOOR SUPPORT. CRACKED. LOWER AFT CARGO COMP FLOOR SUPPORT ANGLE CRACKED AT BS 1070 AND RBL 27. INSTALLED NEW SUPPORT ANGLES PER B727 SRM 51-30-2, 51-10-1 AND -2. SIZE OF MATERIAL USED
- [SDR DHL2000715005](https://openairdocs.org/sdr/DHL2000715005), Oct 11, 2000: FITTING. CRACKED. MAIN CARGO DOOR LATCH FITTING STA 580 UPPER FLANGE CRACK. INSTALLED ANGLE REPAIR PER BOEING TELEX DHL-MIA-00-00033H. SIZE OF REPAIR 7 X 2 X 3 INCHES.
- [SDR DHL2000715019](https://openairdocs.org/sdr/DHL2000715019), Oct 10, 2000: SKIN. CORRODED. NR 2 CARGO DOOR HAS EXTERNAL SKIN WITH CUTOUT AT AFT EDGE BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER B727 SRM 52-00-2 AND 52-00-3. SIZE OF DOUBLER 15 X 4 INCHE
- [SDR DHL2000715011](https://openairdocs.org/sdr/DHL2000715011), Oct 10, 2000: PANEL. DAMAGED. NR 3 ENGINE PYLON FIXED COWL PANEL DAMAGED UPPER SIDE AFT OF 2ND VERTICAL LATCH CUTOUT. REPAIR PER SRM 51-10-1. SIZE OF REPAIR 23 X 4 INCHES.
- [SDR DHL2000715018](https://openairdocs.org/sdr/DHL2000715018), Oct 9, 2000: BULKHEAD. CRACKED. FWD PRESSURE BULKHEAD BS 178 IS CRACK AT RBL 02 AND WL 196. INSTALLED DOUBLER REPAIR PER SB-727-53-0213. SIZE OF MATERIAL 9.6 X 132 INCHES.
- [SDR DHL2000715017](https://openairdocs.org/sdr/DHL2000715017), Oct 9, 2000: BULKHEAD. CRACKED. FWD PRESSURE BULKHEAD BS 178 IS CRACK AT RBL 10 AND WL 300. INSTALLED DOUBLER REPAIR PER SB-727-53-146. SIZE OF DOUBLER 6 X 7 INCHES.
- [SDR DHL2000715014](https://openairdocs.org/sdr/DHL2000715014), Oct 9, 2000: FITTING. CRACKED. LEFT WING I/B MID FLAP ROLLER SUPPORT FITTING HAS CRACK. FABRICATE AND INSTALL DOUBLER REPAIR PER B727 SRM 51-30-2, 57-50-4. SIZE OF MATERIAL USED 6 X 3 INCHES.
- [SDR DHL2000715013](https://openairdocs.org/sdr/DHL2000715013), Oct 9, 2000: TORQUE TUBE. CRACKED. FWD ENTRANCE FRONT CUTOUT ACCESS FOR VERTICAL TORQUE TUBE HAS TWO CRACKS. REMOVED AND REPLACED DAMAGED SECTION PER B727 SRM 51-30-2. SIZE OF MATERIAL USED 10 X 
- [SDR DHL2000715007](https://openairdocs.org/sdr/DHL2000715007), Oct 9, 2000: BULKHEAD. CRACKED. FWD PRESSURE BULKHEAD BS 178 IS CRACKED RBL 02 WL 196. CRACK IS 1.5 INCH LONG. INSTALLED DOUBLER PER B727 SRM 53-10-9 AND SB 727-53-043. SIZE OF REPAIR 7 X 9 IN
- [SDR DHL2000715002](https://openairdocs.org/sdr/DHL2000715002), Oct 9, 2000: WEB. CRACKED. FWD ENTRY DOOR HAS TOP HORIZONTAL WEB CRACKED AFT TOP CORNER, SEE THROUGH INSPECTION HOLE. INSTALLED REPAIR AT UPPER AFT CORNER AS PER B727 SB 52-115 FIG 4 AND 
- [SDR DHL2000715004](https://openairdocs.org/sdr/DHL2000715004), Oct 8, 2000: SKIN. CORRODED. NOSE SECTION LT SIDE EXTERIOR BS 243.7 AND STR 26L SKIN BULGING, RIVETS PULLING THROUGH. INSTALLED DOUBLER REPAIR PER SRM 51-10-1 AND 51-30-2 AND 53-30-3 AND MM
- [SDR DHL2000715009](https://openairdocs.org/sdr/DHL2000715009), Oct 6, 2000: PRESSURE PANEL. CRACKED. NOSE WHEEL WELL RIGHT SIDE PANEL LOWER BS 240.7 WL 150 CRACKED. INSTALL DOUBLER REPAIR PER B727 SRM 51-10-1. SIZE OF REPAIR 7.5 X 3.5 INCHES.
- [SDR DHL2000715008](https://openairdocs.org/sdr/DHL2000715008), Oct 6, 2000: FRAME. CRACKED. NOSE L/G WHEEL WELL LT SIDE PANEL TO LWR CHORD BS 248 WL 150 SHOWS CRACK RUNNING FROM RIVET IS ABOUT 1.5 INCH LONG. INSTALLED DOUBLER REPAIR PER B727 SRM 51-10-
- [SDR DHL2000715016](https://openairdocs.org/sdr/DHL2000715016), Oct 5, 2000: PRESSURE PANEL. CRACKED. NOSE WHEEL WELL RIGHT SIDE LATERAL WEB PANEL AT BS 285.5 SHOW CRACK RUNNING BETWEEN RIVETS. FABRICATED AND INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2, AND 51
- [SDR DHL2000715015](https://openairdocs.org/sdr/DHL2000715015), Oct 5, 2000: SKIN. DAMAGED. FUSELAGE SKIN CREASED AT ATA 1342 JUST ABOVE STR 20L. FABRICATED AND INSTALLED REPAIR PER B727 SRM 51-30-2, 51-10-1, 53-30-1 AND 53-30-3.
- [SDR DHL2000715001](https://openairdocs.org/sdr/DHL2000715001), Sep 7, 2000: OUTFLOW VALVE. FAILED. WHILE OPERATING ON RT PACK, A/C CABIN ALTITUDE REACHED 9800 FT AND CONTINUED TO CLIMB UNTIL DECENDED TO 10,000 FT. AT 10,000 FT CABIN STABILIZED AT 1.0 PSI/8000
- [SDR DHL99715001](https://openairdocs.org/sdr/DHL99715001), Oct 15, 1999: HINGE. DAMAGED. MAIN CARGO DOOR HINGE ACTUATORS ATTACH POINT HOLES ELONGATED. FABRICATED AND REPAIRED HOLES AND PARTS PER TIMCO EO W00001 REV C AND BOEING SRM 51-10-7.
- [SDR DHL9871520C](https://openairdocs.org/sdr/DHL9871520C), Oct 29, 1998: ANGLE. CRACKED. AT C-CHECK, LEFT WING NR 2 SLAT ACTUATOR COVER DOOR BOTH ATTACH ANGLE I/B AND O/B ARE CRACKED AT FWD END. REMOVED AND REPLACED ATTACH ANGLES PER SRM 51-40-4, 11
- [SDR DHL98715004](https://openairdocs.org/sdr/DHL98715004), Oct 29, 1998: DUCT. BROKEN. NR 7 SLAT DID NOT RETRACT WITH FLAPS SELECTED TO UP. ABNORMAL ROLL INDICATION. FOUND WING ANTI-ICING TELESCOPING DUCT ON NR 7 SLAT BROKEN AND HANGING OUT. REMOV
- [SDR DHL9871528C](https://openairdocs.org/sdr/DHL9871528C), Oct 19, 1998: WEB. CRACKED. AT C-CHECK, VERTICAL WEB CRACKED AT BOTTOM LIGHTENING HOLES AT BS 1263 RT SIDE OF AFT AIRSTAIRS AREA. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 51-40

All 153: https://openairdocs.org/deregistered/N715DH-2017-07-07/reports.md

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