# N750DH: Hesterman Donald C ZENITH CH750 - Status: Valid registration - Airframe: [Hesterman Donald C ZENITH CH750](https://openairdocs.org/model/hesterman-donald-c-zenith-ch750) (registry code 056315D, 2 seats) - Serial number: 75-8455 - Type: Fixed wing single engine - Engine type: Reciprocating - Kit: Zenith Aircraft Co STOL CH 750 - Certificate issued: August 7, 2012 - Expires: August 31, 2028 - Mode S code: AA1A5C - Registered owner: [Hesterman Donald C](https://openairdocs.org/faa-owner/HESTERMAN%20DONALD%20C) - Location: [Rudolph, WI](https://openairdocs.org/faa-place/WI/Rudolph) - Owner type: Individual - Owner's area on the map: 44.4846° N, 89.7931° W: Placed by OpenAirDocs at the center of ZIP code 54475, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=750DH - Page: https://openairdocs.org/aircraft/N750DH From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Hesterman Donald C ZENITH CH750) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N750DH. ## FAA accident and incident reports None matched to N750DH. ## Reports on N750DH not matched to an aircraft (3) They name N750DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20041209034419I](https://openairdocs.org/incident/20041209034419I), Dec 9, 2004: Boeing 7272M7 (N750DH), Atlanta, GA, Minor damage. (-23) December 9, 2004 dhl flight 495 departed from cincinnati, Ohio enroute to Atlanta Hartsfield airport. When the airplane landed at the Atlanta Hartsfield… - [Incident 20040921022759I](https://openairdocs.org/incident/20040921022759I), Sep 21, 2004: Boeing 7272M7 (N750DH), Covington/Cinci, KY, Substantial damage. (-23) Aircraft N750DH operating as flight ER108 (phx-cvg) was being marshalled into spot 54 on the dhl ramp. Aircraft N752DH was parked (stationary) in… - [Incident 20030816024099I](https://openairdocs.org/incident/20030816024099I), Aug 16, 2003: Boeing 7272M7 (N750DH), Guadalajara, Mexico, Minor damage. (-23) Crew encountered tail strike during landing. Post flight indicated that the tail skid was heavily damaged, #2 engine reversers were damaged. Wx does not… ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N750DH not matched to an aircraft (121, newest 50) They name N750DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DHLA200800120](https://openairdocs.org/sdr/DHLA200800120), Nov 1, 2008: LIGHT. LOOSE. PILOT REPORT, EMERGENCY EXIT LIGHTS ILLUMINATE PERIODICALLY WITH SWITCH IN THE ARMED POSITION. RESOLUTION, CONFIRMED. RESEATED COCKPIT EMERGENCY EXIT LIGHT. OPS - [SDR DHL2008F00031](https://openairdocs.org/sdr/DHL2008F00031), Aug 26, 2008: LIGHT. INOPERATIVE. L1 DOOR EMER EXIT LIGHT INOP. R&R EMER EXIT LIGHT ASSY OPS CHECK GOOD IAW MM 33-50-71. ACFT WAS GROUNDED. FLIGHT NR 820. - [SDR DHL2008F00029](https://openairdocs.org/sdr/DHL2008F00029), Jul 8, 2008: SKIN. CRACKED. L1 DOOR FRAME 303 9 CRACK ON INBOARD FASTENER HOLE INSIDE UPPER HINGE CUTOUT. REPAIRED L-1 DOOR FRAME BS 303.95 UPPER HINGE CUTOUT IAW EVA B253-00089 REV IR DAT - [SDR DHL2008F00023](https://openairdocs.org/sdr/DHL2008F00023), Jul 6, 2008: SKIN. CORRODED. LT WHEEL WELL BS 931.5 ABOVE STRINGER 18A CORROSION SPOT SKIN BLOWN WBL 70.5. INSTALLED REPAIR PARTS AT LT WHEEL WELL BS 931 5 ABOVE STRINGER 18A AREA WBL 70 5 - [SDR DHL2008F00028](https://openairdocs.org/sdr/DHL2008F00028), Jul 3, 2008: SKIN. GOUGED. FUSELAGE INNER SKIN BELOW UPPER HINGE IS GOUGED BS 303 STRINGER 12L TO 306.65 LT HAND. FABRICATED REPAIR AND INSTALLED IAW EVA B253-00086 REV 03 DATED 2 JULY 08 - [SDR DHL2008F00015](https://openairdocs.org/sdr/DHL2008F00015), Jun 26, 2008: ANGLE. CORRODED. L-2 DOOR TAP INTERIOR ANGLE SUPPORT AND WEB ARE CORRODED (EXFOLIATION) BS 1040/1065. REMOVED AND REPLACED L-2 DOOR UPPER ANGLE SUPPORT WEB BEAM IAW B727 SRM 51- - [SDR DHL2008F00018](https://openairdocs.org/sdr/DHL2008F00018), Jun 25, 2008: WEB. CRACKED. L-1 DOOR LOWER FORWARD CORNER OF WEB HAS CRACK. CUT OUT DAMAGE L-1 DOOR LOWER FORWARD CORNER WEB IAW B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER REPAIR AND INSTA - [SDR DHL2008F00010](https://openairdocs.org/sdr/DHL2008F00010), Jun 23, 2008: WEB. CRACKED. L-1 DOOR LOWER FORWARD BOTTOM OF DOOR HAS CRACKED WEB. INSTALLED NEW LOWER WEB FROM L-1 DOOR WITH MATERIAL 7075-T6 .075 SIZE 37 5 X 8 AND PO 9007406 IAW B727 SR - [SDR DHL2008F00014](https://openairdocs.org/sdr/DHL2008F00014), Jun 22, 2008: KEELBEAM. CORRODED. SURFACE CORROSION FRONT LOWER CHORD CENTER OF KEEL BEAM BS 740. REMOVED AND REPLACED BS 740 LOWER CHORD T ANGLE P/N 69-4711Y2, PO 8180132 IAW B727 SRM 51-30-2. - [SDR DHL2008F00021](https://openairdocs.org/sdr/DHL2008F00021), Jun 19, 2008: BEAM. MISINSTALLED. HORIZONTAL WALKWAY BEAM LOWER CHORD LT SIDE, HAS SEVERAL FASTENERS BUCK TAIL FLAT, ALSO IMPROPER SIZE FASTENERS BETWEEN BS 312 AND BS 328. REMOVED AND REPLACED - [SDR DHL2008F00011](https://openairdocs.org/sdr/DHL2008F00011), Jun 19, 2008: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT HORIZONTAL WALKWAY BEAM AREA BS 328 STRINGER 26L. REPAIRED SHEAR TIE AT HORIZONTAL WALKWAY BEAM BS 328 STRINGER 26L IAW B727 SRM 53-10-4 FI - [SDR DHL2008F00009](https://openairdocs.org/sdr/DHL2008F00009), Jun 16, 2008: SKIN. BULGED. BULGE AT BS 660 AND STRINGER 27R EXTERIOR SKIN. REMOVED FASTENERS AND SHEAR TIE, TEE AT BS 660 AND STRINGER 27R IAW B727 SRM 51-30-2. FOUND SHEAR TIE OUT OF LIM - [SDR DHL2008F00026](https://openairdocs.org/sdr/DHL2008F00026), Jun 13, 2008: CHANNEL. CORRODED. CORROSION, NOSE GEAR TRUNNION WELL LT FORWARD C-CHANNEL BS 303. REMOVED CORROSION ON LT FORWARD C-CHANNEL BS 303 IAW B727 SRM 51-10-6. EVALUATED OUT OF LIMITS I - [SDR DHL2008F00027](https://openairdocs.org/sdr/DHL2008F00027), Jun 12, 2008: STRINGER. CORRODED. EXFOLIATED CORROSION ON STRINGER 28L CHANNEL BETWEEN BS 620 AND BS 640. REPAIRED STRINGER BS 620-640 STRINGER 28L IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. (A) - [SDR DHL2008F00022](https://openairdocs.org/sdr/DHL2008F00022), Jun 12, 2008: STRINGER. CRACKED. STRINGER 15R IS CRACKED AT BS 720B + 5 INCHES. CUT OUT DAMAGE AREA DIMENSION .625 AT STRINGER 15R 720B IAW SRM 53-10-3 FIG 5. FABRICATED CHANNEL USING 7075-T6 0 - [SDR DHL2008F00012](https://openairdocs.org/sdr/DHL2008F00012), Jun 11, 2008: SEAT TRACK. CORRODED. CABIN SEAT TRACK BS 1166 TO 848 LBL 24-25 LIGHT CORROSION IN SEVERAL AREA AND MISSING PRIMER. REMOVED CORROSION ON SEAT TRACK BETWEEN BS 1050 TO 848 LBL 24.25 I - [SDR DHL2008F00008](https://openairdocs.org/sdr/DHL2008F00008), Jun 10, 2008: SKIN. CRACKED. LT WING UPPER LEADING EDGE WS 507 AFT CORNER OF HOOK CUT OUT IS CRACKED. REMOVED HOOK SEAL IAW B727 SRM 51-30-2. STOP DRILLED CRACK DIMENSION .250 IAW B727 SRM - [SDR DHL2008F00020](https://openairdocs.org/sdr/DHL2008F00020), Jun 7, 2008: SEAT TRACK. CORRODED. PITTING CORROSION ON SEAT TRACK UPPERMOST SURFACE AT BS 1029 AND RBL 24. BLEND OUT AREA AT SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3. FABRICATED NEW - [SDR DHL2008F00025](https://openairdocs.org/sdr/DHL2008F00025), Jun 6, 2008: HINGE. CRACKED. MAIN CARGO DOOR AFT HINGE SECTION IS CRACKED AT FUSELAGE SIDE BS 650. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR SIDE BS 650 AND INSTALLED NEW SECTION WITH MS - [SDR DHL2008F00024](https://openairdocs.org/sdr/DHL2008F00024), May 31, 2008: BRACKET. CRACKED. LT WING NR 1 KRUEGER FLAP ACTUATOR INBOARD AND OUTBOARD ATTACH BRACKETS ARE CRACKED IN THE CORNERS. REMOVED BRACKETS (2 EACH) IAW B727 SRM 51-30-2. FABRICATED B - [SDR DHLA200700093](https://openairdocs.org/sdr/DHLA200700093), Dec 27, 2007: OVERHEAT LOOP. MISROUTED. NR 1 STRUT OVERHEAT LIGHT AFTER T/O PERFORMED NORMAL SHUTDOWN NR 1 ENGINE PER PROCEDURE. FOUND 4 DUCT CONNECTIONS LEAKING ON DUCT FROM PRECOOLER TO THE ENG. REM - [SDR DHLA200700085](https://openairdocs.org/sdr/DHLA200700085), Dec 17, 2007: LATCH. LACK OF LUBE. FWD ENTRY DOOR WILL NOT LOCK IN OPEN POSITION. CLEANED AND LUBED FWD ENTRY DOOR LATCH ASSY. OPS CHECK NORMAL IAW AMM 52-11-01. - [SDR DHLA200700078](https://openairdocs.org/sdr/DHLA200700078), Dec 8, 2007: RUDDER CONTROL. MALFUNCTIONED. LOWER RUDDER MOVED ON ITS OWN FAR TO THE LEFT AS COMPARED WITH THE UPPER RUDDER AS SEEN ON THE RUDDER POSITION INDICATORS DURING TAKEOFF ROLL. ACFT PULLED TO TH - [SDR DHL2007750505](https://openairdocs.org/sdr/DHL2007750505), Aug 13, 2007: SKIN. DENTED. WHILE AT FLIGHTSTAR FOR AN A CHECK DISCREPANCY FUSELAGE REPAIR HAS BLIND FASTENERS INSTALLED AT STA 1203 STR22R AND DOUBLER IS DENTED. REMOVED PREVIOUS REPAIR I - [SDR DHL2007750504](https://openairdocs.org/sdr/DHL2007750504), Aug 13, 2007: DOOR FRAME. CORRODED. C2 DOOR LWR AFT FRAME CORRODED. REMOVED DOOR AFT CORNER AND DISPLACED WEB TO GAIN ACCESS IAW B727 SRM 51-30-2. CUT-OUT DAMAGED SECTION OF FRAME DIM 13 1/2" BY 6 - [SDR DHL2007750503](https://openairdocs.org/sdr/DHL2007750503), Aug 13, 2007: WEB. DENTED. DURING A CHECK DISCREPANCY, LT TORQUE BOX UPPER WEB HAS 2 DENTS AT APPROX STA 1243. CUTOUT DAMAGED AREA TWO 4" DIM IAW B727 SRM 51-40-2 FIG 1. FAB REPAIR DOUBLE - [SDR DHL2007750502](https://openairdocs.org/sdr/DHL2007750502), Aug 13, 2007: SUPPORT ANGLE. CRACKED. AFT AIRSTAIRS BS 1243 LT UPPER SUPPORT ANGLE CRACKED INSIDE OF TORQUE BOX. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2 FIG7. FABRICATED NEW ANGLE 7075-0 .063 PO - [SDR DHL2007750001](https://openairdocs.org/sdr/DHL2007750001), Aug 13, 2007: SHEAR TIE. CORRODED. WHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR AN A CHECK.REFERENCE ASTAR N/RS 093661,093687 DISCREPANCY: PILLOWING AT FASTENERS ON FUSELAGE SKIN BS 700 BETWEEN STRI - [SDR DHL2007750002](https://openairdocs.org/sdr/DHL2007750002), Jan 12, 2007: DUCT. LEAKING. NR 1 FIRE HANDLE INTERMITTENTLY GOES OFF AFTER TAKEOFF. FOUND SIX STAGE DUCT LEAKING AT FIREWALL ABOVE FIRELOOP REMOVED AND REPLACED DEFECTIVE DUCTING IAW B727 - [SDR DHL2006750001](https://openairdocs.org/sdr/DHL2006750001), Nov 29, 2006: APU. MALFUNCTIONED. LOST APU BLEED AIR DURING ENGINE NR 2 START. PERFORMED EMERGENCY START MALFUNCTION CHECKLIST. APU CONTINUED TO RUN "HOT" (640 DEGREES) IN STATIC CONDITION (NO L - [SDR 2006750001](https://openairdocs.org/sdr/2006750001), Apr 11, 2006: WING. CRACKED. WING CRACKED, REMOVED AND REPLACED LEFT WING. - [SDR DHL2006750522](https://openairdocs.org/sdr/DHL2006750522), Mar 28, 2006: SKIN. DEBONDED. L/WING I/B FOREFLAP, I/B CLOSE OUT BROKEN W/UPPER SKIN DISBONDED AT I/B END. REMOVED PREVIOUS REPAIR AND FABBED FILLER APPROX 3 3/4 BY 8 1/2 DOUBLER APPROX 5 1/ - [SDR DHL2006750521](https://openairdocs.org/sdr/DHL2006750521), Mar 20, 2006: SKIN. GOUGED. FOUND L WING I/B AILERON UPPER SKIN IS GOUGED AT WS 410. CUT OUT DAMAGED AREA DIM 2X2 AND FABBED REPAIR DOUBLER FROM MAT USE 2024 T3 .04 PO 9003055 AND DIM 5 1/ - [SDR DHL2006750518](https://openairdocs.org/sdr/DHL2006750518), Mar 17, 2006: FRAME. DENTED. FOUND FRAME DENTED AT BS 700 STR 24 R. CUT OUT DAMAGED AREA SIZE 1 BY 3/4 ON FRAME STA 700 AT STR 24R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075-0 .063 - [SDR DHL2006750517](https://openairdocs.org/sdr/DHL2006750517), Mar 17, 2006: FRAME. DENTED. FRAME DENTED AT BS 680 AT STR 24R. CUT OUT DAMAGED AREA SIZE 1 X 3/4 ON FRAME STA 680 AT STR 24R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075 .063 SIZE 8 - [SDR DHL2006570519](https://openairdocs.org/sdr/DHL2006570519), Mar 17, 2006: FRAME. DENTED. FOUND FRAME DENTED AT BS 720A STR 25R. CUT OUT DAMAGED AREA SIZE 1 BY 1 ON FRAME STA 720A AT STR 25R IAW B727 SRM 51-10-1. FABBED REPAIR ANGLE FROM 7075-0 .063 - [SDR DHL2006570516](https://openairdocs.org/sdr/DHL2006570516), Mar 16, 2006: SKIN. CORRODED. CORROSION BULGE LT WING UPPER SURFACE PANEL 10" FWD OF NR 6 SPOILER WS 300. CUT OUT DAMAGED AREA 4 BY 2 1/2 IAW B727 SRM 51-10-1. FABBED DOUBLER FROM 2024 T3 .0 - [SDR DHL2006750513](https://openairdocs.org/sdr/DHL2006750513), Mar 15, 2006: SKIN. DENTED. LT T/E SIDE OF UPPER RUDDER DENTED AT RUDDER TAB COURT (2ND FROM BOTTOM). FOUND DENT TO BE OUT OF LIMITS, ROUTED OUT DAMAGED AREA SIZE 3/8 BY 3/4 IAW B727 SRM 5 - [SDR DHL2006750512](https://openairdocs.org/sdr/DHL2006750512), Mar 14, 2006: WEB. BENT. VERT STAB FWD TENSION TIE SUPPORT WEB BENT/STRESSED RT SIDE. REMOVED SUPPORT WEB ON VERT STAB FWD TENSION TIE RT SIDE IAW B727 SRM 51-30-2. FABBED WEB FROM 7075 - [SDR DHL2006570514](https://openairdocs.org/sdr/DHL2006570514), Mar 14, 2006: SKIN. CRACKED. L/WING INB FLAP, REAR SPAR LOWER CORE SHOWS CRACK AT INB AFT FLAP ACTUATING ROD CUT OUT. CUT OUT DAMAGED AREA AND FABBED REPAIR ANGLE FROM BAC 1503 100046 PO 61 - [SDR DHL2006750515](https://openairdocs.org/sdr/DHL2006750515), Mar 14, 2006: SKIN. GOUGED. RT WING OTBD FORE FLAP LEADING EDGE IS GOUGED AT WBL 442. CUT OUT DAMAGED AREA DIM 1 5/8 BY 1, FABBED REPAIR DOUBLER FROM 2024T3 .063 PO 9003110 DIM 4 1/16 BY 4 - [SDR DHL2006750508](https://openairdocs.org/sdr/DHL2006750508), Mar 13, 2006: TORQUE BOX. CRACKED. TORQUE BOX FIN REAR SPAR CHORD LWR LT SIDE APPEARS TO BE CRACKED PASSED STOP DRILL HOLE STA BS 1303 LBL 22. C/W HFEC ON BS 1303 FRAME WEB IAW B727 NDTM PT6 51-0 - [SDR DHL2006750509](https://openairdocs.org/sdr/DHL2006750509), Mar 13, 2006: SKIN. GOUGED. NR 6 SLAT TRAILING EDGE IS GOUGED AT OUTBD HOOK. ROUTED OUT GOUGE .200 RADIUS BY 6" AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. FABBED REPAIR DOU - [SDR DHL2006750511](https://openairdocs.org/sdr/DHL2006750511), Mar 13, 2006: BEAM. CRACKED. STA 1183 BULKHEAD VERTICAL BEAM IS CRACKED AT AFT FLANGE INBD AND OUTBD SIDE RBL 36. STOP DRILLED 2 CRACKS IAW S/B 727-53-0192 REV 1 DATED MAY 30 1991. REMOVED - [SDR DHL2006750510](https://openairdocs.org/sdr/DHL2006750510), Mar 13, 2006: SKIN. DENTED. NR 6 SLAT UPPER SKIN IS DENTED AT WING STA 560. FOUND DENT TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 2. REMOVED 2 RIBS FOR ACCESS AND CUT OUT DAMAGE AREA SIZ - [SDR DHL2006750507](https://openairdocs.org/sdr/DHL2006750507), Mar 13, 2006: STRUCTURE. DENTED. FOUND C2 DOOR FWD LWR END DENTED. REMOVED C-2 DOOR LWR FWD CORNER DEPRESSOR IAW B727 SRM 51-30-2. LOCATED AND DRILLED HOLES IAW B727 SRM 51-30-2 FIG NR 2. TREAT - [SDR DHL2006750506](https://openairdocs.org/sdr/DHL2006750506), Mar 12, 2006: SUPPORT BRACKET. CRACKED. NR 1 LE FLAP ACTUATOR TRUNNION SUPPORT BRACKET IS CRACKED OUTBOARD END. CONFIRMED CRACK. REMOVED SUPPORT BRACKET AT NR 1 L/E FLAP ACTUATOR TRUNNION OUTBOARD END - [SDR DHL2006750505](https://openairdocs.org/sdr/DHL2006750505), Mar 12, 2006: STIFFENER. CRACKED. FOUND LEFT WING REAR SPAR VERTICAL STIFFENER AT WS 546 INB OF NR 2 SPOILER FITTING SUPPORT IS CRACKED FROM BOTTOM END. REMOVED AND REPLACED L WING REAR SPAR VER - [SDR DHL2006750504](https://openairdocs.org/sdr/DHL2006750504), Mar 12, 2006: FRAME. CORRODED. AFT CARGO COMPT FRAME ANS SHEAR TIE ARE CORRODED WITH EXFOLIATION AND BROKEN FASTENERS AT STA 1166 BETWEEN STR 28L AND 28R. REMOVED AUX STRUCTURE FROM STA 1166 - [SDR DHL2006750503](https://openairdocs.org/sdr/DHL2006750503), Mar 12, 2006: SKIN. CORRODED. AFT CARGO COMPARTMENT, VHF ANTENNA DOUBLER HAS HEAVY CORROSION BETWEEN STR 30-29R, BETWEEN STA 1030-1050. REMOVED VHF ANTENNA AND DOUBLER BETWEEN STR 30-29R, AT All 121: https://openairdocs.org/aircraft/N750DH/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Hesterman Donald C ZENITH CH750 aircraft: https://openairdocs.org/model/hesterman-donald-c-zenith-ch750/aircraft.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.