# N722DA: 1977 Lockheed L-1011-385-1, registration cancelled 2005-02-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 25, 2005 - Exported to: Thailand - Status when cancelled: Valid registration - Airframe: [Lockheed L-1011-385-1](https://openairdocs.org/model/lockheed-l-1011-385-1) (registry code 5265010) - Engine: [Rolls-Royce RB-211-22 series](https://openairdocs.org/engine/rolls-royce-rb-211-22-series) (registry code 54554) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs) - Serial number: 193C-1147 - Year built: 1977 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 27, 1977 - Certificate issued: January 14, 2005 - Last registry action: January 14, 2005 - Mode S code: A9AB46 - Owner when cancelled: [Jet Midwest Inc](https://openairdocs.org/faa-owner/JET%20MIDWEST%20INC) - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Corporation - Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N722DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=722DA - Page: https://openairdocs.org/deregistered/N722DA-2005-02-25 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 Lockheed L-1011-385-1: https://openairdocs.org/model/lockheed-l-1011-385-1.md ## Service difficulty reports (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL10981789](https://openairdocs.org/sdr/DLL10981789), Aug 29, 1998: SLAVE RAM. DEFECTIVE. NR 1 THROTTLE FAILED TO DEVELOP T/O THRUST WITH HIGH N2. REPLACED NR 1 ENG MASTER AND SLAVE RAM, RAN PER PFHB TEST NR 4 ALL CKS NORMAL. - [SDR DLL10981335](https://openairdocs.org/sdr/DLL10981335), Jun 21, 1998: BULKHEAD FITTING. CRACKED. REPAIR FOR CRACK, LT WING IWS 503-529, PYLON BACKUP FITTING BULKHEAD. THE LT WING PYLON BACKUP FITTING BULKHEAD BETWEEN IWS 503 AND 539 WAS FOUND WITH A 6 LONG - [SDR DLL10981261](https://openairdocs.org/sdr/DLL10981261), Jun 15, 1998: MECHANISM. FAILED TEST. L-1 AND L-2 DOORS FAILED EMERGENCY OPS, TEST PER OPN 68116, EXCEEDED TIME LIMIT. REPLACED COUNTER BALANCES. - [SDR DLL10980434](https://openairdocs.org/sdr/DLL10980434), Feb 21, 1998: BATTERY PACK. DISCHARGED. R-4 EMERGENCY LIGHT BATTERY PACK FAILED TO HOLD CHARGE. REPLACED EMERGENCY BATTERY PACK. - [SDR DLL10980366](https://openairdocs.org/sdr/DLL10980366), Feb 11, 1998: FUEL CONTROL. FAILED. T/O PWR SET ENG 1 FAILED TO ACCELERATE PROPERLY N3 LESS THAN 80 PERCENT EPR WOULD NOT GO ABOVE 1.18 {OTHERS SET AT 1.428} AND N2WAS LOWER {APPROX 80} THAN OTHER - [SDR DLL10972161](https://openairdocs.org/sdr/DLL10972161), Oct 26, 1997: POWER PACK. INOPERATIVE. EMERGENCY LIGHTS IN COACH CLASS ILLUMINATED DURING FLIGHT. CYCLED SWITCH IN COCKPIT LIGHTS EXTINGUISHED. REPLACED EMERGENCY POWER PACKS AT 1R 2L AND 4R DOORS LI - [SDR DLL10971748](https://openairdocs.org/sdr/DLL10971748), Aug 30, 1997: REAR SPAR. CORROSION. CORROSION WAS FOUND ON THE WING CENTER SECTION REAR SPAR WEB AT BOTH LBL AND RBL 102. THE CORROSION IS LOCATED ON THE AFT SIDE OF THE WEB AT THE SPAR UPPER CHOR - [SDR DLL10971747](https://openairdocs.org/sdr/DLL10971747), Aug 29, 1997: PRESSURE DECK. CRACKED. THE FUSELAGE NOSE LANDING GEAR HORIZONTAL PRESSURE DECK AFT PANEL AT LBL 55 JUST FORWARD OF FS 445 WAS PREVIOUSLY REPAIRED FOR CRACKS PER THE SRM. UPON INSPECTI - [SDR DLL10971292](https://openairdocs.org/sdr/DLL10971292), Jul 3, 1997: PLUG. SHEARED. DURING CLIMBOUT, DURING FLAP RETRACTION C-SYS HYD RES FLUID LEVEL DROPPED TO .25 AND ASSOC LOW QTY LIGHT ILLUM. REPLACED RUPTURED HYD PLUG ON C-SYS HIGH PRESS F - [SDR DLL10962664](https://openairdocs.org/sdr/DLL10962664), Dec 2, 1996: BULKHEAD. CRACKED. DURING INSPECTION OF THE FS 499 BULKHEAD, ADDITIONAL CRACKS WERE FOUND. ORIGINALLY THIS LOCATION HAD BEEN MODIFIED PER A LAX SB. - [SDR DLL10962396](https://openairdocs.org/sdr/DLL10962396), Oct 26, 1996: PROX SWITCH. WORN. AFTER T/O, UPON GEAR RETRACTION RED DOOR INTRANSIT LIGHT REMAINED ON UP FRONT AND NOSE GEAR OR DOOR LIGHT REMAINED ON AT S/O PANEL. REPLACED UPLOCK AND LT NOSE - [SDR DLL10962428](https://openairdocs.org/sdr/DLL10962428), Oct 11, 1996: PRESS DECK. CRACKED. THE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A 1.5 CRACK, LOCATED AT RBL 102, JUST AFT OF FS 378 AND EXTENDS DIAGONALLY I/B AND AFT FROM THE FWD EDGE O - [SDR DLL10962427](https://openairdocs.org/sdr/DLL10962427), Oct 10, 1996: FRAME. CRACKED. AFTER BEING INSPECTED PER SI 7-69903-12AD, THE RT SIDE FUSELAGE FRAME WAS FOUND CRACKED AT THE TYPICAL LOCATION OVER THE WL 280.6 LONGERON AND DIRECTLY OVER STR - [SDR DLL10962178](https://openairdocs.org/sdr/DLL10962178), Sep 25, 1996: VANE ACTUATOR. FAILED. UPON ARRIVAL, MTC NOTICED RT I/B FLAP O/B FAIRING DAMAGE. RT I/B FLAP O/B ROD VANE ACTUATOR ASSY, WAS PROTRUDING THROUGH THE FLAP FAIRING. NEW ROD ACTUATOR AND - [SDR DLL10961670](https://openairdocs.org/sdr/DLL10961670), Jul 10, 1996: LIGHT SOCKET. FAILED. ON LAYOVER, FOUND EMERGENCY LIGHT SOCKET INOP. REPLACED EMERGENCY LIGHT SOCKET, EMERGENCY LIGHTS OP CHECK GOOD. - [SDR DLL10961231](https://openairdocs.org/sdr/DLL10961231), May 16, 1996: SPAR WEB. CRACKED. THE CENTER WING INTERMEDIATE SPARS AT FS 1043M RBL 116 AND FS 1103M LBL 116 HAD CRACKS IN WEB. ALSO, FS 1103 HAD MULTIPLE CRACKS THROUGH UPPER FASTENER HOLES. R - [SDR DLL10961189](https://openairdocs.org/sdr/DLL10961189), May 14, 1996: RIB CAP. CRACKED. THE LEFT HAND WING WAS FOUND WITH A 1 INCH CRACK IN THE IWS 555 UPPER RIB CAP. THE DAMAGED AREA WAS CUT OUT AND A NEW RIB WAS SPLICED IN, REV A ADDS FAA APROVAL - [SDR DLL10961233](https://openairdocs.org/sdr/DLL10961233), May 13, 1996: RIB CAP. CRACKED. A 1.0 CRACK WAS FOUND IN THE IWS 555 UPPER CAP BETWEEN STR 19 AND 20. A REPAIR ANGLE WAS SPLICED IN. REV A CHANGES THE FWD CUT LOCATION, REV B REMOVED FWD CUT L - [SDR DLL10960137](https://openairdocs.org/sdr/DLL10960137), Jan 18, 1996: ACTUATOR. FAILED. AFTER TAKEOFF HAD BURNING ODOR AND VISIBLE SMOKE, RETURNED HNL. RAN ALL ENGINES, COULD NOT DUPLICATE. RAN PACKS, ALL NORMAL. REPLACED NR 3 WATER SEPARATOR BAG. - [SDR DLL10960084](https://openairdocs.org/sdr/DLL10960084), Jan 13, 1996: SCREW JACK. BROKEN. ON CLIMBOUT FLAPS EXTENDED 4 TO 6 DEGREES, SLATS UP WITH NO ACTUATION OF FLAP HANDLE. FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES FOR LANDING. GPWS INHIBITED AS PE - [SDR DLL10954718](https://openairdocs.org/sdr/DLL10954718), Dec 15, 1995: BLEED AIR. OIL FUMES. SMOKE IN REAR CABIN AREA AND ALL 5 AFT LAV SMOKE DETECTORS WENT OFF. ISOLATED NR 2 ENG BLEED, SMOKE DISSIPATED. LOCKED OUT NR 2 EJECTOR AND FWD TO MCO PER MEL 3 - [SDR DLL10953253](https://openairdocs.org/sdr/DLL10953253), Jul 26, 1995: AIR DISTR. ODOR. ON CLIMBOUT, HAD BURNING ODOR IN CABIN WITH LAV SMOKE DETECTORS ACTIVATED, RETURNED ATL. REPLACED ALL WATER SEPARATOR BAGS AND RAN PACKS OPERATION NORMAL. PERFO - [SDR DLL10953174](https://openairdocs.org/sdr/DLL10953174), Jul 22, 1995: ACM. FAILED. SHORTLY AFTER TAKEOFF, SMOKE ALARMS IN AFT CABIN WENT OFF. FLIGHT ATTENDANTS REPORTED SMOKE HAZE IN CABIN, RETURNED LAX. FOUND OIL CONTAMINATION ON NR 2 WATER S - [SDR DLL10952429](https://openairdocs.org/sdr/DLL10952429), May 26, 1995: SUPPORT. CRACKED. C-2 BB FLOOR SUPPORT CHANNEL CRACKED AT LBL 8.5 AND RBL 8.5. REPAIRED CHANNEL PER SRM 53-24-00. - [SDR DLL10952428](https://openairdocs.org/sdr/DLL10952428), May 20, 1995: FORMER. DAMAGED. TOOLING DAMAGE ON 963 FORMER FLANGE BETWEEN STRINGERS 19 AND 20, ABOVE ELECT LOAD CENTER DOOR. ROUTED OUT DAMAGE AND INSTALLED REPAIRS PER SRM 53-12-00 FIG 815. - [SDR DLL10952152](https://openairdocs.org/sdr/DLL10952152), May 17, 1995: ATTACH FITTING. CORRODED. LMLG FWD ATTACH FITTING CORRODED FWD AND AFT LUG. BORED FWD LUG TO 2.726 AND AFT LUG TO 2.727 TO REMOVE CORROSION, SIZES WITHIN LIMITS PER SRM 57-14-00. - [SDR DLL10952114](https://openairdocs.org/sdr/DLL10952114), May 13, 1995: ACTUATOR. FAILED. ON APPROACH, LEFT 3 OUTBOARD L/E SLATS WERE STUCK IN THE UP POSITION WHEN FLAPS WERE SELECTED TO 4 DEGREES. REPLACED NR 4 SLAT ACTUATOR, OPERATION NORMAL. ## FAA accident and incident reports (5) 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 19880809069539I](https://openairdocs.org/incident/19880809069539I), Aug 9, 1988: Lkheed 10113851 (N722DA), Indianapolis, IN. Passenger smoking during refueling. Refused to put cigarette out. Loud and intimidating. Removed by police. - [Incident 19850210007319I](https://openairdocs.org/incident/19850210007319I), Feb 10, 1985: Lkheed 10113851 (N722DA), Chicago, IL. Nr 2 engine did not spool up properly, RPM decay, EGT rise. Aborted takeoff. Fire reported in tailpipe. - [Incident 19810201011509I](https://openairdocs.org/incident/19810201011509I), Feb 1, 1981: Lkheed 10113851 (N722DA), Miami, FL. During taxi,after landing,pilot got right gears off taxiway and got stuck in sod. - [Incident 19800404047619I](https://openairdocs.org/incident/19800404047619I), Apr 4, 1980: Lkheed 10113851 (N722DA), Atlanta, GA. Five flight attendants injured due to unexpected turbulence in flight. - [Incident 19790112001729I](https://openairdocs.org/incident/19790112001729I), Jan 12, 1979: Lkheed 10113851 (N722DA), Boston, MA. Zg zk flames from #3 engine during taxi. Returned to the ramp. Engine checked out ok. --- 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.