# N110DL: Lane Donald S PIETENPOL AIRCAMPER - Status: Valid registration - Airframe: [Lane Donald S PIETENPOL AIRCAMPER](https://openairdocs.org/model/lane-donald-s-pietenpol-aircamper) (registry code 05630E0, 2 seats) - Serial number: 001 - Type: Fixed wing single engine - Engine type: 4 cycle - Certificate issued: May 22, 2018 - Expires: May 31, 2028 - Mode S code: A02C89 - Registered owner: [Triplett Barry A](https://openairdocs.org/faa-owner/TRIPLETT%20BARRY%20A) - Location: [Walkerton, IN](https://openairdocs.org/faa-place/IN/Walkerton) - Owner type: Individual - Owner's area on the map: 41.4819° N, 86.4866° W: Placed by OpenAirDocs at the center of ZIP code 46574, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=110DL - Page: https://openairdocs.org/aircraft/N110DL 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 (Lane Donald S PIETENPOL AIRCAMPER) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N110DL. ## FAA accident and incident reports None matched to N110DL. ## 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 N110DL not matched to an aircraft (22) They name N110DL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DL767050551](https://openairdocs.org/sdr/DL767050551), Sep 15, 2005: WIRE. SHORTED. NOTICED ELECTRICAL PLASTIC ODOR NEAR CAPTAINS GLARESHIELD LIGHT CONTROL PANEL, NEAR LOWER LEFT CORNER OF WINDSCREEN. FOUND L1 WINDOW SENSOR CONNECTION BAD AND S - [SDR DL767050067](https://openairdocs.org/sdr/DL767050067), Jan 28, 2005: ENGINE. FAILED. WHILE RUNNING APU ON GND WITH PACKS ON MTC NOTICED SMOKE IN THE CABIN AND SMOKE OUT OF APU EXHAUST. FOUND APU COMPRESSOR OUTLET DRIPPING OIL. REPLACED APU. - [SDR DL767021274](https://openairdocs.org/sdr/DL767021274), Nov 1, 2002: WEDGE. DELAMINATED. AFT FLAP T/E WEDGE BONDED ASSY WAS FOUND DELAMINATED BEYOND THE SCOPE OF A LOCALIZED REPAIR. REPAIR PER ER/A 417896-14. - [SDR DL767002274](https://openairdocs.org/sdr/DL767002274), Nov 20, 2000: IDG. LACK OF LUBE. ON T/O ROLL, LT GEN DRIVE EICAS MSG CAME ON. ABORT T/O AT 100 KNTS. BPCU INDICATES SERVICE IDG. SERVICED IDG AND RAN ENGINE. - [SDR DL767002096](https://openairdocs.org/sdr/DL767002096), Oct 23, 2000: SKIN. CORRODED. CORROSION DAMAGE FOUND ON THE UPPER SURFACE OF THE CENTER WING SKIN AND IN THE UPPER SPAR CAP AT STA 955, RBL 70 - 90. IN NORDER TO VERIFY REMOVAL AND FACILITRA - [SDR DL767002097](https://openairdocs.org/sdr/DL767002097), Oct 18, 2000: BULKHEAD. WORN. HOLE FOUND ELONGATED IN THE AFT BULKHEAD OF THE NR 1 PYLON ON THE LOWER FWD GSE HOLE (6TH FROM THE TOP). THE RIVET HOLES INSTALLED PER BOEING S/B 767-54-0010 WE - [SDR DL767992631](https://openairdocs.org/sdr/DL767992631), Nov 30, 1999: SKIN. PUNCTURED. THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 1197 & 1219 AND BETWEEN STRINGERS 36L & 38L. STRINGERS 36L & 37L WERE CRACKED AND THE O/B SKIN FLANGE OF STRINGER 38L - [SDR DL767990482](https://openairdocs.org/sdr/DL767990482), Mar 2, 1999: DOOR. MISSING. PASSING 12,000 FT, FLT ATTENDANT REPORTED LOUD NOISE. ALSO, HAD LT SLIDE DOOR EICAS MSG AND OVERHEAD DISCREET EMER DOORS. SLIDE HAD DEPARTED A/C WITH FAILURE OF - [SDR DL767990442](https://openairdocs.org/sdr/DL767990442), Mar 2, 1999: SLIDE. DEPLOYED. LT OVERWING SLIDE DEPLOYED IN FLIGHT PASSING THRU FL 12 OUT OF ATL. MTC OBSERVED LINKAGE ON DOOR RELEASE MECHANISM, FOUND THIRD LINKAGE FROM FORWARD EDGE BENT A - [SDR DL767990432](https://openairdocs.org/sdr/DL767990432), Mar 2, 1999: SLIDE. DETACHED. PASSING 21,000 FT MSL, FLT ATTENDANTS COMPLAINED OF LOUD NOISE. ALSO, HAD EICAS MSG LT SLIDE DOOR AND OVERHEAD DISCREET EMERG DOORS. AIR TURNBACK TO ATL. FOUND - [SDR DL767990388](https://openairdocs.org/sdr/DL767990388), Feb 25, 1999: SKIN. DELAMINATED. THE UPPER SKIN ON THE NR 3 SLAT TRAILING EDGE WAS FOUND WITH A 3 X 4 DENTED/DELAMINATED AREA. THE DAMAGED SKIN WAS TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43- - [SDR DL767982109](https://openairdocs.org/sdr/DL767982109), Oct 10, 1998: OVEN. CONTAMINATED. SHORTLY AFTER TAKEOFF, SMOKE OBSERVED FROM AFT GALLEY OVENS. COULD NOT DETERMINE SOURCE OF SMOKE, FOOD OR ELECTRICAL. FOUND BURNT SUBSTANCE IN CORNER OF LOWER L - [SDR DL767981726](https://openairdocs.org/sdr/DL767981726), Aug 21, 1998: FLOORBEAM. CORRODED. CORROSION DAMAGE WAS FOUND ON THE UPPER CAP OF THE OVERWING LONGITUDINAL FLOORBEAM AT RBL 54, FROM BS 850 TO THE AFT END OF THE UPPER CAP AT APPROX BS 1000. THE - [SDR DL767981707](https://openairdocs.org/sdr/DL767981707), Aug 19, 1998: FLOORBEAM. CORRODED. CORROSION WAS FOUND ON THE UPPER SURFACE OF THE BS 287 FLOORBEAM UPPER CHORD. IN ADDITION, AN EXISTING REPAIR WAS ALSO LOCATED IN THE SAME AREA. REPAIRED PER ER - [SDR DL767981469](https://openairdocs.org/sdr/DL767981469), Jul 14, 1998: WEDGE. DELAMINATED. DELAMINATION WAS FOUND ON THE NR 1 SLAT T/E WEDGE. DELAM AREA IS APPROX 4 IN DIAMETER. REPAIRED PER ERA 365245-14AD. - [SDR DL767972696](https://openairdocs.org/sdr/DL767972696), Dec 18, 1997: SKIN. PUNCTURED. THE FUSELAGE SKIN AT FS 422 BETWEEN STRINGERS 21L AND 22L WAS PUNCTURED BY GROUND EQUIPMENT. THE FINAL SKIN CUTOUT WAS 6.5 BY 5. THE DAMAGE WAS REPAIRED WITH A - [SDR DL767971572](https://openairdocs.org/sdr/DL767971572), Aug 11, 1997: UNION. BROKEN. AFTER T/O, RETRACTED GEAR, RAISED FLAPS TO 5 DEG, THEN 1 DEG AND LOST HYD FLUID IN CTR SYS. FLAPS REMAINED AT 5 DEG, RAISED WITH ALT SYS. MTC FOUND UNION (P/N S - [SDR DL767961449](https://openairdocs.org/sdr/DL767961449), Jun 17, 1996: CHECK VALVE. INOPERATIVE. AFTER T/O, A/C WOULD NOT COOL. HOT AIR ENTERED PASSENGER CABIN AND COCKPIT UNABLE TO STOP HOT AIR ISOLATED BOTH SIDES, NO HELP. REPLACED RT PACK TRIM AIR CK VAL - [SDR DL767961188](https://openairdocs.org/sdr/DL767961188), May 10, 1996: SKIN. DENTED. THE NR 1 SLAT, TRAILING EDGE WEDGE WAS FOUND DENTED IN THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767-200 SRM 51-70-10 FIG 9. - [SDR DL767954539](https://openairdocs.org/sdr/DL767954539), Nov 19, 1995: FAN. FAILED. DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN. DEACTIVATED RECIRC FAN AND ODOR DISSIPATED. REPLACED RECIRC FAN, OPERATION NORMAL. - [SDR DL767954159](https://openairdocs.org/sdr/DL767954159), Oct 17, 1995: TE WEDGE. DELAMINATION. RT WING NR 9 AND NR 11 SLAT TRAILING EDGE WEDGES HAVE AREAS OF DELAMINATION. ACCOMPLISHED REPAIRS PER DL ERA 272145-14AD. - [SDR DL767951148](https://openairdocs.org/sdr/DL767951148), Mar 14, 1995: FLAP. DELAMINATED. NR 7 INTERM REPAIR TO L/E OF O/B FLAP JUST I/B OF THE NBR 8 FLAP DRIVE IS DELAMINATED. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Lane Donald S PIETENPOL AIRCAMPER aircraft: https://openairdocs.org/model/lane-donald-s-pietenpol-aircamper/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.