# N110HM: 1989 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2015-08-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 5, 2015 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 49787 - Year built: 1989 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: September 8, 1994 - Last registry action: August 5, 2015 - Mode S code: A02CEE - Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC) - Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie) - Owner type: Corporation - Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N110HM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=110HM - Page: https://openairdocs.org/deregistered/N110HM-2015-08-05 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 Mcdonnell Douglas DC-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md ## Service difficulty reports (85, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AALA20120304011](https://openairdocs.org/sdr/AALA20120304011), Mar 4, 2012: CABLE. BROKEN. DFW - DURING TAXI OUT FOR TAKEOFF AND JUST AS TAKEOFF ROLL STARTED, RIGHT SIDE BRAKES STARTING DRAGGING CAUSING AIRCRAFT TO SHUTTER. ABORTED TAKEOFF. AIRCRAFT R - [SDR AALA20120217012](https://openairdocs.org/sdr/AALA20120217012), Feb 17, 2012: CUSP WEB. CORRODED. RIGHT CUSP WEB FROM BS 1130 TO 1134 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20120217011](https://openairdocs.org/sdr/AALA20120217011), Feb 17, 2012: CUSP WEB. CORRODED. LEFT CUSP WEB FROM BS 1250 TO 1308 CORRODED. INSTALLED NEW CUSP PER AARD 53-20-00-16. - [SDR AALA20120217010](https://openairdocs.org/sdr/AALA20120217010), Feb 17, 2012: CUSP WEB. CORRODED. RIGHT CUSP WEB FROM BS 264 TO 266 OUTBOARD OF SEAT TRACK 6 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20120217009](https://openairdocs.org/sdr/AALA20120217009), Feb 17, 2012: CUSP WEB. CRACKED. RIGHT CUSP WEB BETWEEN STATIONS 370 TO 389 CRACKED. INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20120217008](https://openairdocs.org/sdr/AALA20120217008), Feb 17, 2012: CUSP WEB. CORRODED. RIGHT CUSP FROM STATIONS 524 TO 536 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA201202130006](https://openairdocs.org/sdr/AALA201202130006), Feb 13, 2012: SKIN. DAMAGED. BS 427 LONGERON 24 LEFT DAMAGED. INSTALLED DOUBLER REPAIR PER SRM 53-04-00 FIGURE 12C. - [SDR AALA20120211TUL07](https://openairdocs.org/sdr/AALA20120211TUL07), Feb 11, 2012: CUSP WEB. CRACKED. CRACK IN EDGE OF CUSP LIGHTENING HOLE AT RIGHT HAND STATION 454. INSTALLED DOUBLER FOR EDGE OF CUSP LIGHTENING HOLE AT RIGHT STATION 454 PER AARD 53-20-00-16. - [SDR AALA20120211TUL03](https://openairdocs.org/sdr/AALA20120211TUL03), Feb 11, 2012: FLOORBEAM. DAMAGED. HOLES ELONGATED IN FLOORBEAM RIGHT SIDE STATION 845 4 INCHES FROM OUTBOARD. INSTALLED CHANNEL DOUBLERS PER EA MD80-53-021678. - [SDR AALA20120210TUL01](https://openairdocs.org/sdr/AALA20120210TUL01), Feb 10, 2012: BEAM. CORRODED. CORROSION ON LOWER CARGO DOOR BEAM AREA FROM STATIONS 1202 TO 1212. INSTALLED BEAM DOUBLER PER EA MD80-53-021705. - [SDR AALA20120212TUL03](https://openairdocs.org/sdr/AALA20120212TUL03), Feb 7, 2012: ANGLE. DAMAGED. CUSP T-ANGLE LEFT SIDE BENT FROM FRAME STATIONS 712 TO 732. SPLICE REPAIR FROM STATIONS 702 TO 741 PER SRM 53-05-00 FIGURE 25 SHEET 2. - [SDR AALA20120213TUL07](https://openairdocs.org/sdr/AALA20120213TUL07), Feb 6, 2012: CUSP WEB. CORRODED. LIGHT CORROSION AT FRAME STATION 732 LEFT CUSP. INSTALLED NEW CUSP SECTION PER AARD 53-20-00-16. - [SDR AALA20120206TUL02](https://openairdocs.org/sdr/AALA20120206TUL02), Feb 6, 2012: CUSP WEB. CORRODED. LEFT CUSP FROM STATIONS 1250 TO 1308 CORRODED. INSTALLED SERVICEABLE LEFT CUSP FROM STATIONS 1250 TO 1308 PER AARD 53-20-00-16. - [SDR AALA20120205TUL01](https://openairdocs.org/sdr/AALA20120205TUL01), Feb 5, 2012: CUSP WEB. CORRODED. CORROSION OUT OF LIMITS ON RIGHT HAND CUSP FROM STATIONS 1130 TO 1134. INSTALLED DOUBLER FROM STATIONS 1130 TO 1135 PER AARD 53-20-00-16. - [SDR AALA20120204TUL02](https://openairdocs.org/sdr/AALA20120204TUL02), Feb 4, 2012: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AFT OF 1451 AFT OF LONGERON 2 RIGHT. REMOVED AND REPLACED CLIP-SHEAR TIE PER AARD 51-10-00-5. - [SDR AALA20120202TUL08](https://openairdocs.org/sdr/AALA20120202TUL08), Feb 2, 2012: CUSP WEB. CRACKED. CRACK IN RIGHT CUSP BETWEEN STATIONS 370 TO 389. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16. - [SDR AALA20120212TUL04](https://openairdocs.org/sdr/AALA20120212TUL04), Jan 25, 2012: SKIN. DAMAGED. DENT AT FUSELAGE STATION 216 JUST BELOW LONGERON 18 LEFT. INSTALLED DOUBLER REPAIR PER SRM 53-04-05 FIGURE 2 SHEET 5. - [SDR AALA20120212TUL01](https://openairdocs.org/sdr/AALA20120212TUL01), Jan 24, 2012: CUSP WEB. CORRODED. RIGHT CUSP T-CORRODED AT FRAME STATION 167. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION PER SRM 53-05-00 FIGURE 55, SHEET 2. - [SDR AALA20111107STL01](https://openairdocs.org/sdr/AALA20111107STL01), Nov 7, 2011: BUNGEE CYLINDER. INOPERATIVE. STL - CREW REPORTED NOSE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE MOVED TO THE DOWN POSITION. UNSAFE NOSE GEAR WARNING LIGHT INDICATED. PERFORMED EMERGENCY GEAR E - [SDR AALA20101216ORD01](https://openairdocs.org/sdr/AALA20101216ORD01), Dec 16, 2010: START VALVE. INOPERATIVE. ORD - CREW REPORTED RIGHT ENGINE START VALVE LIGHT ILLUMINATED DURING CLIMBOUT. REDUCED POWER AND LIGHT REMAINED ON. EMERGENCY DECLARED FLIGHT RETURNED ORD LAND - [SDR AALA20101211TUL01](https://openairdocs.org/sdr/AALA20101211TUL01), Dec 11, 2010: BOOT. DEFECTIVE. CRP - INFLIGHT MFE-DFW. CREW REPORTED TAIL TEMP HIGH LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED CRP LANDED WITHOUT INCIDENT. AIRCRAFT R - [SDR AALA20100816TUL06](https://openairdocs.org/sdr/AALA20100816TUL06), Aug 16, 2010: SHEAR TIE. CRACKED. AFT ACCESSORY SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM 51-30-05. - [SDR AALA20071038](https://openairdocs.org/sdr/AALA20071038), Jun 7, 2007: BATTERY PACK. INOPERATIVE. DFW - EMERGENCY LIGHTS AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD STORAGE COMPARTMENT FOR EMERGENCY LIGHTS AT OVERHEAD AFT GALLEY. SY - [SDR AALA20070346](https://openairdocs.org/sdr/AALA20070346), Feb 16, 2007: STRUT. DEFECTIVE. IND INFLIGHT T1077/16FEB - NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO IND AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT AND ACCOMPLISHED F - [SDR AALA20070316](https://openairdocs.org/sdr/AALA20070316), Feb 11, 2007: FUEL. CONTAMINATED. DFW INFLIGHT SAT-ORD, AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKER POPPED. UNABLE TO TRANSFER FUEL FROM CENTER TANK. LANDED DFW WITHOUT INCIDENT. SUMPED THREE GAL - [SDR AALA20060053](https://openairdocs.org/sdr/AALA20060053), Jan 27, 2006: CHARGER. INOPERATIVE. ORD - EMERGENCY LIGHT IN AFT TAIL CONE INOPERATIVE. CLEANED BATTERY CHARGER AT AFT LAVATORY AND REPLACED FORWARD EMERGENCY LIGHT FIXTURE FOR EMERGENCY LIGHT IN - [SDR AALA20050001](https://openairdocs.org/sdr/AALA20050001), Jan 2, 2005: BATTERY PACK. DISCHARGED. RDU - OVERHEAD EMERGENCY LIGHTS AT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL O - [SDR AALA20041202](https://openairdocs.org/sdr/AALA20041202), Dec 8, 2004: BATTERY PACK. INOPERATIVE. BOS - FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR ZW0A0305901](https://openairdocs.org/sdr/ZW0A0305901), Jul 16, 2003: HYDRAULIC LINE. LEAKING. JUST AFTER TAKE OFF CREW REPORTED SMOKE IN CABIN WITH CORRESPONDING LOSS OF RH HYDRAULIC SYSTEM. FLIGHT RETURNED TO STL. CREW MANUALLY EXTENDED THE LANDING GEAR - [SDR ZW0A0303211](https://openairdocs.org/sdr/ZW0A0303211), Mar 13, 2003: CHANNEL. CRACKED. DURING CHECK-C, THE RIGHT WHEEL WELL FWD MAIN GEAR DOOR FRAME CHANNEL WAS CRACKED. REPLACED SECTION OF FRAME CHANNEL PER SRM 51-10-04, 51-20-0, 51-30-2, AND 51- - [SDR ZW0A0303210](https://openairdocs.org/sdr/ZW0A0303210), Mar 13, 2003: CHANNEL. CRACKED. DURING CHECK-C,. MAINT THE LT MAIN LANDING GEAR FORWARD INBOARD DOOR FRAME CHANNEL WAS CRACKED. REPLACED THE FWD INBOARD MLG DOOR FRAME CHANNEL PER SRM 51-30-1, - [SDR ZW0A0210802](https://openairdocs.org/sdr/ZW0A0210802), Oct 25, 2002: BATTERY. THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 20 TO 25. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-7-02 STL. --CLOSED-- - [SDR ZW0A0202601](https://openairdocs.org/sdr/ZW0A0202601), Mar 5, 2002: LONGERON. CRACKED. DURING CHECK-C MAINT LONGERON 2R HAD A CRACK JUST AFT OF STA 1429. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18. - [SDR ZW0A0202602](https://openairdocs.org/sdr/ZW0A0202602), Mar 4, 2002: LONGERON. CRACKED. DURING CHECK-C MAINT LONGERON 2L WAS CRACKED JUST AFT OF STA 1429. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18. - [SDR TWAA0001208](https://openairdocs.org/sdr/TWAA0001208), Jan 18, 2000: CARGO TRACK. CORRODED. DURING OP 16 MAINT CHECK, THE AFT CARGO BILGE AREA RT TRACK NUTPLATE HOLES CORRODED ON OTBD SIDE OF TRACK, STA 1117 TO 1136. REMOVED AND REPLACED TRACK PER SPM - [SDR TWAA0001206](https://openairdocs.org/sdr/TWAA0001206), Jan 16, 2000: DOOR FRAME. DAMAGED. DURING OP 16 MAINT CHECK, FOUND HOLE IN DOOR FRAME STA 194, LONGERON 18R. REPLACED LOWER THIRD OF DOOR JAM PER SRM 53-05 FIG 55 AND DOUGLAS REPAIR DRAWING JO601 - [SDR TWAA0001207](https://openairdocs.org/sdr/TWAA0001207), Jan 15, 2000: SUPPORT. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR PANEL SUPPORT BETWEEN STA 168 AND 200, RBL 53 IN TO RBL 56 IN. REPLACED FLOOR SUPPORT FABRICATED NEW FLOOR SU - [SDR TWAA0001303](https://openairdocs.org/sdr/TWAA0001303), Jan 14, 2000: FLOORBEAM. CORRODED. DURING CHECK-C MAINT IN THE MID CARGO BIN AT STA 522 TO 788, RT SIDE, NUT PLATE HOLES WERE CORRODED ON FLOOR TRACK. INSTALLED NEW FLOOR TRACK PER SRM 51-01, PAG - [SDR TWAA0001302](https://openairdocs.org/sdr/TWAA0001302), Jan 14, 2000: SKIN. CORRODED. DURING CHECK-C MAINT,THE FUSELAGE RT SIDE WINDOW FRAME (50R) AT STA 1155 TO 1174 WAS DAMAGED AND CORRODED LOWER SIDE. BLENDED PER SRM 53-05, FIG 111 SHEET 2 NOT - [SDR TWAA0001304](https://openairdocs.org/sdr/TWAA0001304), Jan 14, 2000: CARGO TRACK. CRACKED. DURING CHECK-C MAINT, IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK HAD CORROSION AROUND SCREW HOLES ON THE FLANGE AND INSIDE THE TRACK FROM FWD BULKHEAD TO STA - [SDR TWAA0000913](https://openairdocs.org/sdr/TWAA0000913), Jan 9, 2000: SUPPORT. CRACKED. DURING OP 16 MAINT CHECK AT STA 936, RBL 6 IN, FWD SIDE FUSELAGE PANEL SUPPORT STRUCTURE HAD 1.5 IN HORIZONTAL CRACK. REPAIRED PER SRM 53-05, FIG 81 PAGE 267. - [SDR TWAA0000912](https://openairdocs.org/sdr/TWAA0000912), Jan 9, 2000: KEEL BEAM. CRACKED. DURING OP 16 MAINT CHECK AT STA 936, LBL 6 IN, THE AFT SIDE OF KEEL BEAM STRUCTURE HAD 2 EA 5 IN VERTICAL CRACKS, ONE AT RADIUS 1 1/8 AND SECOND AT RADIUS 1/2 I - [SDR TWAA0000911](https://openairdocs.org/sdr/TWAA0000911), Jan 7, 2000: SKIN. SCRATCHED. DURING OP 16 MAINT CHECK, FOUND SCRATCH ON RT SIDE OF FUSELAGE, AT WINDOW FRAME STA 514, BOTTOM OF WINDOW. BLENDED PER SRM 53-05, FIG 111 SHEET 2, NOTE 12 PAGE - [SDR TWAA0000910](https://openairdocs.org/sdr/TWAA0000910), Jan 7, 2000: FRAME. CRACKED. DURING OP 16 MAINT CHECK, THE LT MAIN LANDING GEAR DOOR, UPPER FWD CORNER INBD OF TIE IN CLIP INNER FRAME HAD .5 INCH CRACK. ACCOMP HIGH FREQ EDDY CURRENT PER 5 - [SDR TWAA0000909](https://openairdocs.org/sdr/TWAA0000909), Jan 7, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK IN THE FORWARD CARGO COMPARTMENT, FOUND CORROSION AROUND NUT PLATE HOLES ON FLOOR SUPPORT BETWEEN FLOOR TRACKS STA 437. REPLACED CORROD - [SDR TWAA0000916](https://openairdocs.org/sdr/TWAA0000916), Jan 6, 2000: FITTING. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 200, RBL 18, AT FLOOR FITTING. CORROSION WAS BEYOND LIMITS. NEW PANEL ASSEMBLED. RIVETS NAS 1097AD4-4 PER SRM 5 - [SDR TWAA0000908](https://openairdocs.org/sdr/TWAA0000908), Jan 6, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND NUT PLATE HOLES ON FLOOR SUPPORT, STA 200 RBL 5 IN TO LBL 5 IN. REMOVED CORROSION PER SPM 6-80-01, PAGE 1. FABR - [SDR TWAA0000907](https://openairdocs.org/sdr/TWAA0000907), Jan 6, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOORBEAM PANEL WEB FROM STA 160 TO 200, AND BETWEEN 6 IN LBL TO 6 IN RBL. COMPLETED REPAIR ON PANEL WEB FROM STA 1 - [SDR TWAA0000906](https://openairdocs.org/sdr/TWAA0000906), Jan 6, 2000: SEAT TRACK. CORRODED. DURING OP 16 MAINT CHECK, FOUND CABIN CORROSION IN THE CHAIR TRACK AT LBL 22 INCHES, STA 1117 TO 1309. INSTALLED NEW SEAT TRACK PER MM 53-40-01, PAGE 201. SPLIC - [SDR TWAA0000905](https://openairdocs.org/sdr/TWAA0000905), Jan 5, 2000: FLOOR WEB. CORRODED. DURING OP 16 MAINT CHECK, THE CABIN AFT SERVICE DOOR TOP OF FLOOR WEB WAS CORRODED AROUND AFT DOOR JAM AREA, TOP OF WEB AND UNDER WEB STA 1174. REPAIRED PER SRM All 85: https://openairdocs.org/deregistered/N110HM-2015-08-05/reports.md ## FAA accident and incident reports (2) 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 20010614011969I](https://openairdocs.org/incident/20010614011969I), Jun 14, 2001: Doug DC983 (N110HM), Salina, KS. (-23)Flt 457 was enroute from st. louis, MO. To denver co. when the aft baggage smoke detector illuminated. Capt [privacy data omitted] declaired an emergency… - [Incident 19990723026529I](https://openairdocs.org/incident/19990723026529I), Jul 23, 1999: Doug DC983 (N110HM), Cleveland, OH, Minor damage. (-23) Crew reported, on take off at rotation, a bird was injested into the right engine. Engine stalled several times, engine failure checklist completed. --- 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.