# N707DH: 1965 Boeing 727-22, registration cancelled 2015-05-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 21, 2015 - Status when cancelled: Sale reported, canceled - Airframe: [Boeing 727-22](https://openairdocs.org/model/boeing-727-22) (registry code 1384002) - 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: 18321 - Year built: 1965 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 25, 1965 - Last registry action: December 10, 2013 - Mode S code: A96EE2 - Location: [Burnsville, MN](https://openairdocs.org/faa-place/MN/Burnsville) - Owner type: Individual - Owner's area on the map: 44.7785° N, 93.2723° W: Placed by OpenAirDocs at the center of ZIP code 55337, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N707DH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=707DH - Page: https://openairdocs.org/deregistered/N707DH-2015-05-21 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 727-22: https://openairdocs.org/model/boeing-727-22.md ## Service difficulty reports (121, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DHL2002707003](https://openairdocs.org/sdr/DHL2002707003), Apr 30, 2002: ACCESSORY UNIT. MALFUNCTIONED. AFTER GEAR RETRACTION MOVED GEAR HANDLE TO OFF, GEAR DOOR LIGHT FORWARD PANEL AND RIGHT MAIN GEAR DOOR LIGHT S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO UP, LIG - [SDR DHL2002707002](https://openairdocs.org/sdr/DHL2002707002), Jan 30, 2002: SWITCH. INOPERATIVE. FIRE ALARM BELL DOES NOT WORK FOR ANY ALARM FUNCTION. REMOVED AND REPLACED THE S41 CUTOFF SWITCH WITH SERVICEABLE SWITCH, OPS CHECK GOOD IAW BOEING WM 26-11-01. - [SDR DHL2002707001](https://openairdocs.org/sdr/DHL2002707001), Jan 22, 2002: SENSOR. FAILED. APU FIRE TEST INOP. REMOVED AND REPLACED FIRE DETECTOR SENSOR IAW DHL 727 MM 26-15-002. SYSTEM OPS CHECKED GOOD. - [SDR DHL2001707015](https://openairdocs.org/sdr/DHL2001707015), Dec 14, 2001: AUTOPILOT SYS. MALFUNCTIONED. WHILE ON FINAL APPROACH COURSE WITH BOTH LOCALIZERS AND GLIDESLOPE INITIALLY CAPTURED ON AUTOPILOT, THE AUTOPILOT WAS NOT CAPABLE OF FLYING THE GLIDESLOPE. AIRC - [SDR DHL2001707014](https://openairdocs.org/sdr/DHL2001707014), Dec 14, 2001: WINDSHIELD WIPER. OUT OF ADJ. RANGE OF MOTION ON WINDSHIELD WIPERS, BOTH CAPT AND F/O ARE INADEQUATE FOR NORMAL FIELD OF VISION (DO NOT COME UP HIGH ENOUGH). WINDSHIELD WIPERS NEED REPLACING - [SDR DHL2001707013](https://openairdocs.org/sdr/DHL2001707013), Sep 19, 2001: SWITCH. INOPERATIVE. NOSE GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION, LIGHT TEST OK. REMOVED NLG POSITION SWITCH AND LINKAGE PER M/M 32-61-71. INSTALL - [SDR DHL2001707012](https://openairdocs.org/sdr/DHL2001707012), Sep 15, 2001: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-71. - [SDR DHL2001707011](https://openairdocs.org/sdr/DHL2001707011), Sep 1, 2001: BULKHEAD. CRACKED. ON DROP IN CHECK, FWD CARGO COMPT, WING CENTER SECTION FWD BULKHEAD WEB CRACKED (APPROX 1 INCH) RBL 29 APPROX 14 INCHES ABOVE PRESS SPAL BETWEEN VERTICAL ROW OF - [SDR DHL2001707010](https://openairdocs.org/sdr/DHL2001707010), Aug 4, 2001: SWITCH. MALFUNCTIONED. NR 2 ENGINE OIL PRESSURE LIGHT CAME ON DIM DURING FLIGHT. COULD EXTINGUISH LIGHT BY RETARDING THRUST TO IDLE INITIALLY. BUT EVENTUALLY CAME ON AT IDLE. OIL TEMP - [SDR DHL2001707009](https://openairdocs.org/sdr/DHL2001707009), Aug 4, 2001: BLEED VALVE. FAILED. T/O THRUST LEFT MANIFOLD DUCT PRESSURE ROSE TO 100PSI DEFERRED PER MAINT. CONTROL 36-11-1 MB. WHEN ATTEMPTING TO START ENGINES TO CHECK PRESSURIZATION, NR 1 ENG - [SDR DHL2001707008](https://openairdocs.org/sdr/DHL2001707008), Jun 21, 2001: BRAKE. MALFUNCTIONED. AT 38 DEGREES C IN SMF, ANTI-SKID REPEATEDLY RELEASED AS T/O THRUST WAS SET WITH BRAKES ON. FORWARD MOVEMENT OF ACFT WAS MINIMAL. DID NOT OBSERVE RELEASE LIGHTS - [SDR DHL2001707007](https://openairdocs.org/sdr/DHL2001707007), Jun 8, 2001: AUTOPILOT SYS. MALFUNCTIONED. WHEN OPERATING AUTOPILOT IN MANUAL MODE USING TURN MODE AUTOPILOT WILL NOT TURN RIGHT. ALL OTHER FUNCTIONS NORMAL. DEFFERED TO DMI 5936, PER MEL 22-1 CAT B, ITE - [SDR DHL2001707006](https://openairdocs.org/sdr/DHL2001707006), May 19, 2001: COMPUTER. MALFUNCTIONED. WITH AUTOPILOT IN AUTO G/S MODE, AND GLIDE SLOPE CAPTURED, THE AIRCRAFT PITCHES UP AND DOWN AND MAY OR MAY NOT RECOVER TO GLIDE PATH. REPLACED PITCH CHANNEL COM - [SDR DHL2001707005](https://openairdocs.org/sdr/DHL2001707005), Apr 10, 2001: LIGHT. DAMAGED. RIGHT TAIL NAV LIGHT ASSY DAMAGED BY BAGGAGE CART. REPLACED RT WING TIP ASSY IAW MM 57-20-0. STATUS: CLOSED. - [SDR DHL2001707003](https://openairdocs.org/sdr/DHL2001707003), Mar 30, 2001: PANEL. DEBONDED. UPON ROUTINE A-CHECK INSPECTION, FOUND THE 10 FLIGHT SPOILER PANEL LOWER SKIN SEPARATED FROM PANEL. THE OUTBOARD EDGE WAS COMPLETELY OPEN AND APPEARED THAT SKIN - [SDR DHL2001707002](https://openairdocs.org/sdr/DHL2001707002), Feb 12, 2001: FASTENER. LOOSE. DURING A/C RECEIVING INSPECTION FOUND LOOSE BLIND FASTENERS ON EXTERNAL SKIN REPAIR BS 218, STRINGER 25R. REMOVED EXTERNAL SKIN REPAIR AND BLIND FASTENERS. INST - [SDR DHL2001707001](https://openairdocs.org/sdr/DHL2001707001), Feb 7, 2001: MOTOR. INOPERATIVE. CAPTS WINDSHIELD WIPERS INOP IN ALL SPEEDS. REMOVED AND REPLACED CAPTS WIPER MOTOR IAW MM 30-42-11. - [SDR DHL2000707037](https://openairdocs.org/sdr/DHL2000707037), Sep 19, 2000: SKIN. DAMAGED. HOLE IN FUSELAGE, FWD RT SIDE OF NOSE, AFT OF RADOME. REPAIR SKIN USING PROCEDURES OUTLINED IN THE SRM 53-30-3 PG 74C -- 74F. THIS IS AN INTERM REPAIR. - [SDR DHL2000707031](https://openairdocs.org/sdr/DHL2000707031), Aug 31, 2000: TURBINE. FAILED. NR 3 ENGINE FAILED ON T/O, ENGINE SHUT DOWN (POWER LOSS). EMERGENCY DECLARED, RETURNED TO BWI. INITIAL INSPECTION INDICATES TURBINE FAILURE. - [SDR DHL2000707032](https://openairdocs.org/sdr/DHL2000707032), Aug 31, 2000: ENGINE. FAILED. NR 3 ENG FAILED ON L/O. ENGINE SHUT DOWN, EMERGENCY WAS DECLARED AND RETURN TO BWI. A/C WAS FERRIED TO CVG FOR ENG CHANGE. REMOVED AND REPLACED NR 3 ENGINE. - [SDR DHL2000707030](https://openairdocs.org/sdr/DHL2000707030), Jul 7, 2000: INDICATOR. FAILED. REJECTED TAKE OFF, NO AIRSPEED INDICATION ON CAPTAIN SIDE.VERIFIED NO OBSTRUCTION IN CAPT PITOT.REMOVED AND REPLACED MACH AIR SPEED INDR.AND OPS CHKD IAW MM 34- - [SDR DHL2000707029](https://openairdocs.org/sdr/DHL2000707029), Jul 7, 2000: WARNING LIGHT. ILLUMINATED. ON TACK OFF ROLL THE RIGHT INBD MAIN LANDING GEAR ANTI-SKID LIGHT ILLUMINATED AT 60 KTS,REJECTED TAKE OFF. PLACED ON D M I PER MEL 32-05. - [SDR DHL200070729C](https://openairdocs.org/sdr/DHL200070729C), Jun 8, 2000: PANEL. CHIPPED. AT C CK; RT VERTICAL STAB PANEL 9604-HONEYCOMB SHOWING THRU AND CHIPPED SURFACE. INSTALLED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG. 1. PAINTED - [SDR DHL200070728C](https://openairdocs.org/sdr/DHL200070728C), Jun 8, 2000: SKIN. DELAMINATED. AT C CK; AFT CARGO DOOR MOVABLE FAIRING EXTERNAL SKIN HAS DELAMINATION ON DIFFERENT PLACES. INSTALLED FIBERGLASS OVERLAY REPAIR AFT CARGO DOOR FAIRING EXTERNAL - [SDR DHL200070726C](https://openairdocs.org/sdr/DHL200070726C), Jun 1, 2000: SUPPORT BRACKET. CRACKED. FWD CARGO BAY, LT SIDE WALL SUPPORT, CRACKED STA 540 ABOVE STR 26 LT. REMOVED DAMAGED SECTION OF SIDE WALL LINER SUPPORT FROM STA 480 TO STA 530 ABOVE STR 26 LT - [SDR DHL200070733C](https://openairdocs.org/sdr/DHL200070733C), May 26, 2000: TAB. DELAMINATED. AT C CK; LWR RUDDER TAB LWR LT & RT SURFACE DELAMINATED. ACCOMPLISHED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG 1. REF: N/R 4545. - [SDR DHL200070730C](https://openairdocs.org/sdr/DHL200070730C), May 26, 2000: COWLING. WORN. AT C CK; NR 2 ENGINE RT/AFT COWLING WORN AT LOWER SIDE OF NR 7 RIB. CUTOUT WORN AREA AT NR 2 ENGINE RT AFT COWLING AT RIB NR 7, 6 INCH X 1&1/8 INCH PER B727 SRM - [SDR DHL200070704C](https://openairdocs.org/sdr/DHL200070704C), May 24, 2000: FITTING. CRACKED. FS 870 RT TERMINAL FITTING AT SPLICE FWD BETWEEN STR 9 & 10 SHOWS CRACK. REMOVED FASTENERS FWD OF SPLICE STA 870 RT STR 9 & 10. REMOVED FWD SPLICE FOR INSP SRM - [SDR DHL200070725C](https://openairdocs.org/sdr/DHL200070725C), May 23, 2000: LAP JOINT. DAMAGED. 1080 LAP JOINT HAS + 10 PERCENT INDICATION OF CORROSION BELOW S-2 LT, FROM LBL 13 TO 14 AFT OF AFT FASTNER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF AF - [SDR DHL200070711C](https://openairdocs.org/sdr/DHL200070711C), May 23, 2000: ANGLE. BROKEN. NR 2 ENGINE FWD MOUNTS REAR AREA BS 1400 APROX METAL ANGLE STRIP BROKEN. REMOVED AND REPLACED ANGLE STRIP PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-2. - [SDR DHL200070708C](https://openairdocs.org/sdr/DHL200070708C), May 23, 2000: SKIN. CORRODED. 1080 CIR JOINT HAS + 10 PERCENT CORROSION LOSS IND FROM LBL 7 AFT OF FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF AFT SKIN BS 1080 FROM STR 4L - [SDR DHL200070732C](https://openairdocs.org/sdr/DHL200070732C), May 20, 2000: SKIN. CRACKED. AT C CK; CABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE AREA. STOP DRILLED CRACK PER B727 SRM 51-10-1, PERFORMED HFEC PER NDT M/M 51-00-00 PART 6 - [SDR DHL200070720C](https://openairdocs.org/sdr/DHL200070720C), May 20, 2000: DOUBLER. CRACKED. CORRUGATED DOUBLER CRACKED AT T/E AREA L/W SPAR LOWER SECTION APPROX WS 546.5 (I/B SECTION OF STATION). STOP DRILLED CRACK AT CORRUGATED STRAP AT FT WING REAR S - [SDR DHL200070715C](https://openairdocs.org/sdr/DHL200070715C), May 19, 2000: SKIN. CRACKED. CABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE PANEL. STOP DRILLED CRACK AT CABIN SERVICE DOOR ON UPPER HINGE AREA PER SRM 51-10-1.PERFORMED HFEC - [SDR DHL200070724C](https://openairdocs.org/sdr/DHL200070724C), May 18, 2000: PLATE. CRACKED. MAIN CARGO DOOR CUT OUT SCUFF PLATE AND ADJACENT COVER WORN AND CRACKED AT FWD LOWER CORNER. SMOOTHED OUT SCUFF PLATE AT CARGO DOOR, FWD LOWER CUT OUT AS PER SR - [SDR DHL200070723C](https://openairdocs.org/sdr/DHL200070723C), May 18, 2000: SKIN. CRACKED. LT HORIZ STAB L/E SKIN HAS A CRACK AT RIVET HEAD STA 47.3. PERFORMED HFEC INSP AND CONFIRMED CRACK PER NDT MAN 51-00-00 PART 6 FIG 4. CUT OUT DAMAGED AREA 2.5 X - [SDR DHL200070707C](https://openairdocs.org/sdr/DHL200070707C), May 18, 2000: FRAME. CRACKED. RT MAIN LANDING GEAR WING DOOR LOWER END FRAME IS CRACKED ON O/B BEND RADIUS AT FWD END. REMOVED CRACKED END FRAME AT RT MLG WING DOOR LWR END AS PER SRM 51-30- - [SDR DHL200070706C](https://openairdocs.org/sdr/DHL200070706C), May 18, 2000: SKIN. CORRODED. 1808 CR JOINT HAS +10 PERCENT IND OF CORROSION BELOW S 2L FROM LBL 13 TO 14 AFT OF AFT FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF SKIN BS 10 - [SDR DHL200070703C](https://openairdocs.org/sdr/DHL200070703C), May 18, 2000: SKIN. CORRODED. 1080 CIR JOINT HAS 2090 CORR LOSS FROM S-8R TO S10R AFT OF AFT FASTENER ROW. REMOVED FASTNERS AND CUT OUT DAMAGED SECTION OF AFT SKIN 13S 1080 FROM STR 10R TO S - [SDR DHL200070719C](https://openairdocs.org/sdr/DHL200070719C), May 17, 2000: PANEL. CRACKED. NR 6 L/E SLAT ANTI-ICE TELOSCOPIC DUCT FAIRING PANEL CRACKED. REMOVED AND REPLACED ANTI ICE DUCT PANEL ON NR 6 L/E SLAT PER SRM 51-30-2. ALODINED AND PRIMED PER - [SDR DHL200070718C](https://openairdocs.org/sdr/DHL200070718C), May 17, 2000: SKIN. SCRATCHED. RT WING UPPER SKIN HAS DEEP SCRATCH AT WS 546.5 APPROX. CUT OUT DAMAGED AREA AT L/E RT WING UPPER SKIN AS PER 727 SRM 57-30-4 FIG 2, CUT DIMENSIONS 4 X 2 IN. IN - [SDR DHL200070716C](https://openairdocs.org/sdr/DHL200070716C), May 17, 2000: ANGLE. CHAFED. AFT CARGO COMPT FLOORBEAM SUPPORT ANGLE IS WORN (CHAFED) ON TOP BS 111073 ABOVE STR 29R. CUT OUT DAMAGED AREA AT CARGO SUPPORT ANGLE AT AFT CARGO COMPT SUPPORT - [SDR DHL200070710C](https://openairdocs.org/sdr/DHL200070710C), May 17, 2000: RIB. CRACKED. TAIL CONE INTERIOR RIB CROSS SUPPORT ANGLE CRACKED. REMOVED FIBERGLASS RIB CROSS SUPPORT ANGLE AT TAIL CONE PER SRM 51-30-2. APPLIED FIBERGLASS CLOTH OVERLAY RE - [SDR DHL200070702C](https://openairdocs.org/sdr/DHL200070702C), May 17, 2000: RIVET. LOOSE. NR 1 ENG, LWR COWLING SHOWS 8 WORKING RIVETS AT LOWER MID AREA. CUT OUT DAMAGED AREA 13.5 IN X 2.5 IN PER SRM 54-10-3 FIG 5. CLEANED, ALODINED AND PRIMED PER SR - [SDR DHL200070721C](https://openairdocs.org/sdr/DHL200070721C), May 16, 2000: SLAT TRACK. CRACKED. THE NR 2 SLAT O/B TRACK TO SLAT ATTACH CLIP IS CRACKED ON THE I/B RADIUS. REPLACED ATTACH CLIP AT NR 2 SLAT O/B TRACK TO SLAT PER SRM 51-30-2. - [SDR DHL200070709C](https://openairdocs.org/sdr/DHL200070709C), May 16, 2000: ANGLE. CRACKED. LEFT W/W, VERT ANGLE BETWEEN BULKHEAD 870 AND KEEL BEAM HAS CRACK, FWD SIDE OF APU. VERIFIED CRACK PER NDT M/M PART 6-51-00 FIG 4. REMOVED VERT ANGLE PER SRM 51 - [SDR DHL200070727C](https://openairdocs.org/sdr/DHL200070727C), May 15, 2000: SKIN. DELAMINATED. LT HORIZONTAL STAB, ELEVATOR UPPER SURFACE, HAS SEVERAL AREAS DELAMINATED. OPENED ACCESS PANEL FOR EVALUATION. REMOVED LT HORIZONTAL STAB ELEVATER UPPER SKIN FR - [SDR DHL200070713C](https://openairdocs.org/sdr/DHL200070713C), May 15, 2000: SEAT TRACK. WORN. SEAT TRACK LBL 24 HAS LOCK LUG WORN STA 850. REMOVED SEAT TRACK PER SRM 51-30-2. INSTALLED NEW SEAT TRACK FROM STA 850 TO 870 PER SRM 53-10-5. ALODINED AND PRIM - [SDR DHL200070712C](https://openairdocs.org/sdr/DHL200070712C), May 15, 2000: SEAT TRACK. WORN. SEAT TRACK AT LBL 45 HAS LOCK LUG WORN AT STA 860. REMOVED SEAT TRACK AT BS 860 LBL 45 PER SRM 51-30-2. INSTALLED SEAT TRACK SECTION PER M/M 53-4-0 AND SRM 5103 - [SDR DHL200070722C](https://openairdocs.org/sdr/DHL200070722C), May 13, 2000: FAIRING. TORN. NR 7 FLAP JACKSCREW FAIRING TORN AT I/B EDGE, UPPER SURFACE. CUT OUT DAMAGED AREA AT NR 7 JACKSCREW FAIRING I/B EDGE PER SRM 51-40-2. MATRL LOSS .5 INCH. INSTAL All 121: https://openairdocs.org/deregistered/N707DH-2015-05-21/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 19910618028369I](https://openairdocs.org/incident/19910618028369I), Jun 18, 1991: Boeing 72722 (N707DH), San Antonio, TX. NR2 engine compressor stall when power retarded. Stalls continued on climb. Returned. Faulty fuel control. ## Other aircraft with N707DH - [Registered now](https://openairdocs.org/aircraft/N707DH): Learjet 45, S/N 010, built 1998 --- 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.