# N705DH: 1967 Boeing 727-22C, registration cancelled 2015-05-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 14, 2015
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 19191
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 13, 1981
- Last registry action: December 10, 2013
- Mode S code: A96774
- 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/N705DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=705DH
- Page: https://openairdocs.org/deregistered/N705DH-2015-05-14

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 727-22C: https://openairdocs.org/model/boeing-727-22c.md

## Service difficulty reports (179, newest 50)

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

- [SDR DHL2002705012](https://openairdocs.org/sdr/DHL2002705012), Oct 21, 2002: LIGHT. 1) MAIN ENTRANCE DOOR EMERGENCY LIGHT WILL NOT CHARGE.2) REPLACED EMERGENCY LIGHT ASSEMBLY PER M/M 33-50-00. OPS CHECKED GOOD.
- [SDR DHL2002705011](https://openairdocs.org/sdr/DHL2002705011), Aug 16, 2002: FIRE LOOP. 1) #1 ENGINE FIRE LOOP WILL NOT TEST. 2) R&R #1 ENG FIRE LOOP PER M/M 26-11-00.
- [SDR DHL2002705010](https://openairdocs.org/sdr/DHL2002705010), Jul 19, 2002: OXYGEN MASK. 1) F/O'S O2 MASK BREATHER VALVE STUCK OPEN, MASK WILL NOT PULL TO FACE UPON INHALE.2) R + R F/O'S O2 MASK IAW B727 M/M 35-11-00, OP AND LEAK CHECK GOOD.
- [SDR DHL2002705009](https://openairdocs.org/sdr/DHL2002705009), Jul 18, 2002: FIRE WARNING. MALFUNCTIONED. FIRE BELL DID NOT SOUND DURING ENGINE, APU, OR LOWER CARGO FIRE TEST. PERFORMED AURAL WARN FIRE DETECTION TEST ON ENGINES, APU, W/W AND LOWER CARGO SMOKE IAW 31
- [SDR DHL2002705008](https://openairdocs.org/sdr/DHL2002705008), Jul 13, 2002: SMOKE DETECTOR. 1) LOWER CARGO FIRE DETECTOR SHOWS A FALSE ALARM & A4291 CODE WHEN MX TEST. 2) R&R SMOKE DETECTOR ON AFT CARGO PIT, OPS CK GOOD IAW SMM 26-16-01.
- [SDR DHL2002705007](https://openairdocs.org/sdr/DHL2002705007), Jul 11, 2002: SMOKE DETECTOR. FAULTY. LWR CARGO SMOKE DETECTOR TEST ALARM FAULT ILLUMINATED WITH CODE F6929. REMOVED AND REPLACED FWD LWR CARGO SMOKE DET TESTED CHECK OK AS PER DHL B727-200 ADV MM S
- [SDR DHL2002705002](https://openairdocs.org/sdr/DHL2002705002), Apr 26, 2002: LAMP. INOPERATIVE. UPPER LEFT CABIN SMOKE DETECTOR LAMP, INOPERATIVE. REMOVED AND REPLACED BOTH UPPER CABIN SMOKE DETECTOR BULBS IAW MM 26- 17-00, 401. OPS CHECK GOOD.
- [SDR DHL2002705006](https://openairdocs.org/sdr/DHL2002705006), Apr 19, 2002: BULKHEAD. CRACKED. PER CUSTOMER REQUEST, REPAIR CRACKS 2 EACH ON BS 870 BULKHEAD WL 200 AT RBL 45. CUT OUT DAMAGED SECTION OF BULKHEAD, FABRICATED AND INSTALLED DOUBLER AND FILLER
- [SDR DHL2002705005](https://openairdocs.org/sdr/DHL2002705005), Apr 19, 2002: BULKHEAD. CRACKED. WHILE PERFORMING INSPECTION FOUND BS 870 BULKHEAD WEB CRACKED APPROX 2 INCHES RBL 60, WL 200 AS VIEWED FROM RT MLG W/W ABOVE SPOILER MIXER. CUT OUT CORRODED ARE
- [SDR DHL2002705004](https://openairdocs.org/sdr/DHL2002705004), Apr 18, 2002: SUPPORT. CORRODED. DURING DROP IN CHECK STA 870 WL 186 RBL 42, SUPPORT ANGLE HAS CORROSION BEHIND SPOILER MIXER. CUT OUT CORROSION ON SUPPORT ANGLE. FABRICATED AND INSTALLED REPAI
- [SDR DHL2002705003](https://openairdocs.org/sdr/DHL2002705003), Apr 18, 2002: FITTING. CORRODED. DURING INSPECTION FOUND STA 880 WL 198 RBL 62 SMALL FRAME & ATTACH FITTING HAS CORROSION. REMOVED ATTACH ANGLE STA 880 WL 198 RBL 62 FROM FRAME. REMOVED CORROSI
- [SDR DHL2002705543](https://openairdocs.org/sdr/DHL2002705543), Mar 27, 2002: SUPPORT FITTING. UPON COMPLYING WITH VISUAL INSP OF LEFT WING, FOUND # 4 SPOILER ACTUATOR SUPPORT BRKT BOTTOM LEG CRACKED AND INBD AFT SPAR MOUNT ANGLE CRACKED AT LOWER END.
- [SDR DHL2002705001](https://openairdocs.org/sdr/DHL2002705001), Feb 2, 2002: LINE. LEAKING. A SYS FAILURE 0,PRESSURE 0, QUANITY. REPLACED ENGINE DRIVEN PUMP PRESSURE FLEX LINE ON NR 2 ENGINE. LEAK AND OPS CHECK GOOD.
- [SDR DHL2001705007](https://openairdocs.org/sdr/DHL2001705007), Dec 4, 2001: LIGHT. OUT OF POSITION. EMERGENCY EXIT LIGHT IN COCKPIT FELL OFF. REINSTALLED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD IAW MM 33-50-01.
- [SDR DHL2001705006](https://openairdocs.org/sdr/DHL2001705006), Sep 28, 2001: BATTERY. DISCHARGED. 1) EMERGENCY EXIT LIGHTS ABOVE DOORS INOP.2) REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-101 OPS CHECKED GOOD.STATUS: CLOSED
- [SDR DHL2001705004](https://openairdocs.org/sdr/DHL2001705004), Aug 9, 2001: POWER UNIT. FAILED. APU FIRE TEST INOP. REMOVED & REPLACED POWER UNIT IAW 26-15-0 OPS CHECK NORMAL.
- [SDR DHL2001705545](https://openairdocs.org/sdr/DHL2001705545), Jun 14, 2001: PLATE. CORRODED. ON LINE CHECK- BACK UP PLATE FOR INSPECTION HOLE AT STA 870 RBL 62 HAS CORROSION. REMOVED PRODUCTION DOUBLER AT STA 870 RBL 62 AND ACCESS PANEL. FABRICATED AND 
- [SDR DHL2001705544](https://openairdocs.org/sdr/DHL2001705544), Jun 13, 2001: FITTING. CORRODED. ON LINE CHECK- BS 870 FITTING TO HORIZ BEAM RT WHEEL WELL SPLICE TEE IS CORRODED AT APPROX W/L 175. REMOVED SPLICE TEE AT BS 870 FITTING TO HORIZ BEAM RT W/W AP
- [SDR DHL2001705003](https://openairdocs.org/sdr/DHL2001705003), Jun 2, 2001: TURBINE WHEEL. DAMAGED. EXCESSIVE VIBRATION AFTER TAKEOFF - DURING CLIMB NR 3 ENG VIBRATED AND LOST POWER. DECLARED EMERGENCY. RETURNED TO ROC. FOUND TURBINE WHEEL DAMAGED. REMOVED AND
- [SDR DHL2001705538](https://openairdocs.org/sdr/DHL2001705538), May 7, 2001: SKIN. CRACKED. C-CHECK- LT WING IB L/E EDGE O/B SIDE UPPER SURFACE HAS 2 INCH CRACK. REMOVED DAMAGE AREA AND INSTALLED REPAIR PER B-727 SRM 57-30-4 FIG.6
- [SDR DHL2001705540](https://openairdocs.org/sdr/DHL2001705540), May 5, 2001: BRACKET. CRACKED. C-CHECK, NR 12 SPOILER ACTUATOR MOUNT BRACKET IS CRACKED, OUTBOARD LWR LUG.REMOVED AND REPLACED NR 12 SPOILER ACTUATOR BRACKET.
- [SDR DHL2001705515](https://openairdocs.org/sdr/DHL2001705515), Apr 30, 2001: WEB. CRACKED. C-CHECK WEB CRACKED AT NLG WW RT SIDE AT STA 257 W/L 180 IN BETWEEN PANELS 3123 AND3125 AT 3 EA LOCATION. INSTALLED FILLER & DOUBLER REPAIR AT NLG WW RT SIDE AT
- [SDR DHL2001705531](https://openairdocs.org/sdr/DHL2001705531), Apr 23, 2001: RIB. CRACKED. FOUND WING O/B RIB CRACKED USING HFEC INSP.
- [SDR DHL2001705509](https://openairdocs.org/sdr/DHL2001705509), Apr 21, 2001: FRAME. CORRODED. AT C-CHECK-NOSE W/W RT SIDE WALL, SIDE FRAME CORRODED AT INNER AREA OF FUSE TUNNEL STA 257 WL 180 AND IN BETWEEN ACCESS PANEL 3123. REMOVED FASTENER AND CUTOUT 
- [SDR DHL2001705511](https://openairdocs.org/sdr/DHL2001705511), Apr 20, 2001: STIFFENER. CORRODED. AT C-CHECK- WING CENTER SECTION STA 870 WEB VERTICAL STIFFENER AT BL 0 HAS CORROSION. REMOVED WEB VERTICAL STIFFENER AT WING CENTER SECTION FOR REPLACEMENT AS P
- [SDR DHL2001705500](https://openairdocs.org/sdr/DHL2001705500), Apr 20, 2001: CHANNEL. CORRODED. AT C-CHECK, FUSELAGE CORROSION AT HAT CHANNEL ATTACHED TO FLOORBEAM, STA 344 RBL 39. REMOVED HAT CHANNEL FOR REPLACEMENT AS PER SRM 51-30-22. FABRICATED AND INS
- [SDR DHL2001705530](https://openairdocs.org/sdr/DHL2001705530), Apr 19, 2001: SUPPORT FITTING. CRACKED. AT C-CHECK - LEFT MAIN BEAM WHEEL WELL SUPPORT FITTING BS 930 SHOW'S CRACK AT L-18L, AS MKD LOWER FWD SIDE. CRACK VERIFY BY NDT AS PER 51-000 FIG 1 RUNNING BETW
- [SDR DHL2001705518](https://openairdocs.org/sdr/DHL2001705518), Apr 19, 2001: PANEL. DAMAGED. C-CHECK- LT WING FIXED LEADING EDGE. CORNER OF L/E PANEL IS BROKEN OFF. LOCATED DIRECTLY BELOW GHE I/B WING ROOT LANDING LIGHT ASSY. INSTALLED DOUBLER & FILLER.
- [SDR DHL2001705502](https://openairdocs.org/sdr/DHL2001705502), Apr 19, 2001: FLOOR PANEL. CORRODED. AT C-CHECK, FWD LAVATORY FWD FLOOR PANEL AT FS 303 HAS SEVERAL SPOTS OF CORROSION. REMOVED FWD LAV FLOOR PANEL AT STA 303 FOR REPLACEMENT AS PER B727 SRM 51-30-
- [SDR DHL2001705525](https://openairdocs.org/sdr/DHL2001705525), Apr 19, 2001: ANGLE. CORRODED. C-CHECK, FWD LAVATORY HAS CORROSION UNDER CENTER ANGLE AT FS 340 RBL 40.REMOVED DAMAGED SECTION AND INSTALLED REPAIR.
- [SDR DHL2001705522](https://openairdocs.org/sdr/DHL2001705522), Apr 19, 2001: FLOOR SUPPORT. CRACKED. C-CHECK- CORROSION & CRACKED FLOOR SUPPORT AFT BAGGAGE COMPART LBL22 STA 1012-1027. REMOVED AND REPLACED FLOOR SUPPORT RUNNER FROM STA 960 TO STA 1027 LBL22 IAW
- [SDR DHL2001705520](https://openairdocs.org/sdr/DHL2001705520), Apr 19, 2001: FLOOR SUPPORT. CORRODED. C-CHECK- CORROSION, FLOOR SUPPORT AFT BAGGAGE COMPART STA 1160 STR 26 WL 156 LBL 24 UNDER SIDE. REMOVED AND INSTALLED NEW FLOOR SUPPORT AT AFT CARGO COMPT BS 11
- [SDR DHL2001705508](https://openairdocs.org/sdr/DHL2001705508), Apr 18, 2001: RETAINER. CRACKED. AT C-CHECK, FUSELAGE BS 870 REAR UPPER CHORD CENTER TANK RBL 46 TO OUT. HEAVY CORROSION AND PRESSURE SEAL RETAINER IS ALSO CRACKED. FOUND SEAL RETAINER ATTACH A
- [SDR DHL2001705506](https://openairdocs.org/sdr/DHL2001705506), Apr 18, 2001: DOUBLER. DAMAGED. AT C-CHECK, NR 3 ENG, LWR COWL INTERNAL SURFACE, RIGHT AFTER 2ND U-BOLT, STRINGER PREVIOUS DOUBLER REPAIR SHOWS BIG HOLE (8 O''CLOCK POS APPROX). REMOVED DAMAGE
- [SDR DHL2001705504](https://openairdocs.org/sdr/DHL2001705504), Apr 18, 2001: SEAT TRACK. DAMAGED. AT C-CHECK, SEAT TRACK NR 6 SHOWS PREVIOUS HEAVY BLEND-OUT REWORK AT BS 680 - BS 695 RBL 45. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA 680 TO STA 695 
- [SDR DHL2001705514](https://openairdocs.org/sdr/DHL2001705514), Apr 17, 2001: ANTENNA. DELAMINATED. AT C-CHECK- NR 2 ATC ANTENNA DELAMINATED AND GASKET DETERIORATED. REMOVED NR 2 ATC ANTENNA AND ROUTED TO STOCK IAW B727 MM 34-43-41. INSTALLED NR 2 ATC ANTENNA 
- [SDR DHL2001705507](https://openairdocs.org/sdr/DHL2001705507), Apr 17, 2001: SPOILER. DELAMINATED. C-CHECK, NR 9 SPOILER IS DELAMINATED AT FWD UPPER RT CORNER. REMOVED AND REPLACED NR 9 SPOILER PANEL PER B727 MM 27-62-1 P 401. ADJUST AND TEST. ACCOMPLISH OPER
- [SDR DHL2001705503](https://openairdocs.org/sdr/DHL2001705503), Apr 17, 2001: ANGLE. CRACKED. AT C-CHECK, NR 2 ENG LT AFT COWL HAS LOWER FWD COENER WITH CRACK ANGLE. REMOVED AND REPLACED NR 2 LT AFT CORNER ANGLE. MATERIAL USED 2024T3 .050 MATERIAL SIZE 1
- [SDR DHL2001705501](https://openairdocs.org/sdr/DHL2001705501), Apr 17, 2001: ATTACH ANGLE. CRACKED. AT C-CHECK, MAIN CARGO DOOR CUTOUT, UPPER AFT CORNER AREA, GILL LINER ATTACH ANGLE SHOWS CRACK DAMAGE. REMOVED CRACKED GIL LINER ATTACH ANGLE AT MAIN CARGO DOOR
- [SDR DHL2001705529](https://openairdocs.org/sdr/DHL2001705529), Apr 17, 2001: RIB. CRACKED. C-CHECK- C/W DHL J/C MPRGAA1A57005 INSP. REPLACE WING OUTBOARD RIB WS 686.5. PERFORMED HFEC INSP OF RT WING RIB STA 686.5 RIB TO STRINGER ATTACH POINTS. CRACK F
- [SDR DHL2001705537](https://openairdocs.org/sdr/DHL2001705537), Apr 17, 2001: RIB. CRACKED. C-CHECK C/W DHL J/C MPRGAA1AS7005 INSP, REPLACE WING OUTBOARD RIB WS 738.5 RTPERFORMED HFEC INSP. OF RT. WING RIB STA 738.5 RIB, CRACK FOUND AT LOWER RIB STR 8.
- [SDR DHL2001705528](https://openairdocs.org/sdr/DHL2001705528), Apr 17, 2001: RIB. CRACKED. C-CHECK C/W DHL J/C MPRGAA1A57005INSP, REPLACE WING OUTBOARD RIB WS 656.5. PERFORMED HFEC INSP OF RT WING RIB STA 656.5, RIB TO STRINGER ATTACH POINTS CRACK FOU
- [SDR DHL2001705534](https://openairdocs.org/sdr/DHL2001705534), Apr 17, 2001: BEAM. CRACKED. ON C-CHECK, FWD SIDE BS 1183 VERTICAL BEAM LBL 26.83 WL 268 HAS A VISUAL CRACK TOP SIDE OF THE LIGHTENING HOLE (MARKED) REP MPRGAA1A53001 S/B 727-53AO173. AD 85
- [SDR DHL2001705527](https://openairdocs.org/sdr/DHL2001705527), Apr 17, 2001: RIB. CRACKED. AT C CHECK C/W DHL J/C MPRGAA1A57005 INSP, REPLACE WING OUTBOARD RIB WS 546.5 RT. HFEC INDICATED RIB IS CRACKED.
- [SDR DHL2001705526](https://openairdocs.org/sdr/DHL2001705526), Apr 17, 2001: SKIN. DENTED. C-CHECK- LOWER FWD CARGO DOOR EXT SKIN HAS MANY DENTS. REPAIRED CARGO DOOR SKIN.
- [SDR DHL2001705519](https://openairdocs.org/sdr/DHL2001705519), Apr 17, 2001: ATTACH ANGLE. DAMAGED. C-CHECK- MAIN CARGO DOOR CUT-OUT AT BS 510 GILLLINER ATTACHING ANGLE DAMAGED. REMOVED & REPLACED GILL LINER ATTACH ANGLE.
- [SDR DHL2001705516](https://openairdocs.org/sdr/DHL2001705516), Apr 16, 2001: ANGLE. CRACKED. AT C-CHECK-T/E LWR PANEL SUPPORT ANGLE IS CRACKED AT STA 545. REPLACED T/E LWR PANEL SUPPORT ANGLE AT R/W STA 545 PER B727 SRM 51-30-2.
- [SDR DHL2001705505](https://openairdocs.org/sdr/DHL2001705505), Apr 16, 2001: ANGLE. BENT. AT C-CHECK, NR 1 ENG, LWR COWL O/B FWD AREA , INT ANGLE WORN AND BENT. REFERENCE: FWD OF 2ND U-BOLT, UPPER OF OIL SERVICE DOOR. REMOVED AND REPLACED INTERNAL AN
- [SDR DHL2001705521](https://openairdocs.org/sdr/DHL2001705521), Apr 16, 2001: ANGLE. CORRODED. C-CHECK LT RAM AIR DUCT SUPPORT STRUCTURE HAS CORROSION BULGE BS 660 AT LT RAM AIR DOOR INBD HINGE. REMOVED AND REPLACED RAM AIR DUCT SUPPORT ANGLE AS PER B727 
- [SDR DHL2001705541](https://openairdocs.org/sdr/DHL2001705541), Apr 15, 2001: PRESSURE PANEL. CRACKED. AT C-CHECK, NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158 CRACK RUNNING ALONG FASTENERS ROWS, 2 PLACES. ACCOMPLISHED HFEC INSP OF NOSE WHEEL

All 179: https://openairdocs.org/deregistered/N705DH-2015-05-14/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 20010602014079I](https://openairdocs.org/incident/20010602014079I), Jun 2, 2001: Boeing 72722C (N705DH), Rochester, NY. (-23) On Saturday, June 2, 2001, just after take-off from the Rochester international airport (roc), the number three engine of a dhl airlines, inc. aircraft,…

---
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.