# N284KH: 1975 Boeing 727-2J0, registration cancelled 2007-05-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 14, 2007 - Exported to: Colombia - Status when cancelled: Valid registration - Airframe: [Boeing 727-2J0](https://openairdocs.org/model/boeing-727-2j0) (registry code 1384045) - Serial number: 21108 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: November 20, 1997 - Certificate issued: May 2, 2007 - Last registry action: May 2, 2007 - Mode S code: A2DDC0 - Owner when cancelled: [Mid American Aerospace Ltd](https://openairdocs.org/faa-owner/MID%20AMERICAN%20AEROSPACE%20LTD) - Location: [Cedar Rapids, IA](https://openairdocs.org/faa-place/IA/Cedar%20Rapids) - Owner type: Corporation - Owner's area on the map: 42.0232° N, 91.6596° W: Placed by OpenAirDocs at the center of ZIP code 52402, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N284KH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=284KH - Page: https://openairdocs.org/deregistered/N284KH-2007-05-14 From the FAA registry file of November 12, 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 727-2J0: https://openairdocs.org/model/boeing-727-2j0.md ## Service difficulty reports (57, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GAIA06027OP](https://openairdocs.org/sdr/GAIA06027OP), Aug 25, 2006: SHUTOFF VALVE. CLOSED. DURING CLIMB THE NR 2 ENGINE OIL FILTER BYPASS/LOW PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE TEMPERATURE AND QUANTITY WERE NORMAL. THE NR 2 ENGINE FLAMED OUT - [SDR GAIA05019OP](https://openairdocs.org/sdr/GAIA05019OP), Apr 4, 2005: LIGHT. ILLUMINATED. EMERGENCY EXIT DOOR LIGHT ON ALL THE TIME. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (K) - [SDR GAIA05016OP](https://openairdocs.org/sdr/GAIA05016OP), Mar 25, 2005: BATTERY PACK. DISCHARGED. DURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LI - [SDR GAIA05002OP](https://openairdocs.org/sdr/GAIA05002OP), Jan 18, 2005: O-RING. DAMAGED. DURING CRUISE THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED, AND MADE AN UNEVENTFUL LANDING. REMOVED - [SDR GAIA04171OP](https://openairdocs.org/sdr/GAIA04171OP), Oct 19, 2004: GASKET. BLOWN. DURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A LANDING WAS MADE WITHOUT INCIDENT. - [SDR GAIA04168OP](https://openairdocs.org/sdr/GAIA04168OP), Sep 30, 2004: SEQUENCE VALVE. CRACKED. FLT 715 - ELP-FWA - ON TAKEOFF DURING GEAR RETRACTION THE FLIGHT CREW NOTICED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. AN EMERGENCY WAS DECLARED AND THE AI - [SDR GAIA02051ST](https://openairdocs.org/sdr/GAIA02051ST), May 17, 2002: STRINGER. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 5. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 5 STRINGER 15 LE - [SDR GAIA02052ST](https://openairdocs.org/sdr/GAIA02052ST), May 17, 2002: STRINGER. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 15 STRINGER 15 - [SDR GAIA02053ST](https://openairdocs.org/sdr/GAIA02053ST), May 17, 2002: SEAT TRACK. DAMAGED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE MAIN CABIN SEAT TRACK RBL 24.75 IS DAMAGED SEVERAL DIFFERENT PLACES FROM BS 480-530. ACCOMPLISHED SEAT T - [SDR GAIA02054ST](https://openairdocs.org/sdr/GAIA02054ST), May 17, 2002: STIFFENER. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBL 36.9 CRACKED AT WL 245. ACCOMPLISHED BS 1183 VERTICAL BEAM R - [SDR GAIA02055ST](https://openairdocs.org/sdr/GAIA02055ST), May 17, 2002: SKIN. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN IS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. ACCOMPLISHED FUSELAGE SKIN REPAI - [SDR GAIA02056ST](https://openairdocs.org/sdr/GAIA02056ST), May 17, 2002: WEB. CORRODED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STATION 1230 AFT FACE OF THE TAIL SKIN CAVITY BULKHEAD, CORROSION ON SUPPORT ANGLE AND WEB VISIBLE THROUGH A - [SDR GAIA02057ST](https://openairdocs.org/sdr/GAIA02057ST), May 17, 2002: WEB. CRACKED. DURING A CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1225 LBL 12, VERTICAL WEB HAS A CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED BS 1225, - [SDR GAIA02058ST](https://openairdocs.org/sdr/GAIA02058ST), May 17, 2002: WEB. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1232 LBL 14, VERTICAL WEB IS BUCKLED WITH A 3 INCH CRACK OUTBOARD OF 5TH STEP FRO - [SDR GAIA02059ST](https://openairdocs.org/sdr/GAIA02059ST), May 17, 2002: WEB. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR AREA STATION 1244 RBL 12 VERTICAL WEB HAS 1 CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED TOR - [SDR GAIA02060ST](https://openairdocs.org/sdr/GAIA02060ST), May 17, 2002: SPAR. CORRODED. DURING A C-CHECK INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING FRONT SPAR LOWER CHORD IS CORRODED UNDER AND INBOARD OF EXISTING REPAIR INSIDE L/E COVE A - [SDR GAIA02061ST](https://openairdocs.org/sdr/GAIA02061ST), May 17, 2002: SPAR. CORRODED. DURING A C-CHECK INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED LEFT WING FRONT SPAR UPPER SURFACE AT WS 410 IS CORRODED. ACCOMPLISHED LEFT WING FRONT SPAR LOWER - [SDR GAIA02062ST](https://openairdocs.org/sdr/GAIA02062ST), May 17, 2002: HINGE. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THE MAIN CARGO DOOR HINGE AFT UPPER SECTION IS CRACKED. ACCOMPLISHED MAIN CARGO DOOR HINGE UPPER AFT SECTION REPL - [SDR GAIA02063ST](https://openairdocs.org/sdr/GAIA02063ST), May 17, 2002: INTERCOSTAL. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE AFT CARGO COMPARTMENT BETWEEN BS 1030 AND 1050 AT STRINGER 25L, INTERCOSTAL IS CRACKED. ACCOMPLISHED INTER - [SDR GAIA02064ST](https://openairdocs.org/sdr/GAIA02064ST), May 17, 2002: INTERCOSTAL. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE FORWARD CARGO COMPARTMENT, INTERCOSTAL IS CRACKED BETWEEN BS 950A-950B AT STRINGER 25L. ACCOMPLISHED INTER - [SDR GAIA02065ST](https://openairdocs.org/sdr/GAIA02065ST), May 17, 2002: STRINGER. CRACKED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED STRINGER 18A RIGHT IS CRACKED AT BS 940 RUNNING AFT FROM RADIUS BLOCKS AT THE BASE OF THE HORIZONTAL LEG. ACCOMPL - [SDR GAIA02066ST](https://openairdocs.org/sdr/GAIA02066ST), May 17, 2002: SKIN. CORRODED. DURING A C-CHECK INSPECTION, IT WAS DISCOVERED DISHED FASTENERS ON FUSELAGE SKIN AT BS 351, BELOW STRINGER 26R. ACCOMPLISHED SKIN PANEL AND T-CHORD REPLACEMENT - [SDR GAIA01126ST](https://openairdocs.org/sdr/GAIA01126ST), Apr 13, 2001: DOUBLER. LEAKING. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING AT STATION 224.5 HAD A PREVIOUS DOUBLER REPAIR THAT WAS LEAKING FUEL FROM SEVERAL HI-LOCKS FAS - [SDR GAIA00795](https://openairdocs.org/sdr/GAIA00795), Dec 22, 2000: SWITCH. OUT OF ADJ. NR2 LEADING EDGE FLAP DEPLOYED IN FLIGHT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT ANY FURTHER DIFFICULTIES.ADJUSTED NR2 LEADING EDGE FLAP SWITCH, ONE TURN A - [SDR GAIA00524](https://openairdocs.org/sdr/GAIA00524), Sep 20, 2000: DOOR. MALFUNCTIONED. FLT 1729 - DEN-FWA - AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO PAST OFF, GEAR AND DOORS LIGHTS WERE ALL ILLUMINATED. CYCLED THE GEAR THREE TIMES AND THERE WAS - [SDR GAIA0088](https://openairdocs.org/sdr/GAIA0088), Feb 14, 2000: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE AT HNL, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT RETAIN A CHARGE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BAT - [SDR GAIA9974](https://openairdocs.org/sdr/GAIA9974), Jun 16, 1999: O-RING. DETERIORATED. DURING BOS-TOL - FLT 715 - DURING DESCENT AT FL280, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE WOULD ONLY PRODUCE PARTIAL POWER. THE FLIGHT CREW PERFORMED A P - [SDR GAIA9973](https://openairdocs.org/sdr/GAIA9973), Jun 8, 1999: CONNECTOR. DIRTY. FLT 504 - DURING CLIMB-OUT FROM TOL, THE NR 5 SLAT INDICATE AS NOT RETRACED WHILE ALL OTHER TRAILING AND LEADING EDGE DEVICES WERE RETRACTED. THE CAPTAIN DECLAR - [SDR GAIA9997](https://openairdocs.org/sdr/GAIA9997), Jun 7, 1999: PITOT TUBE. CLOGGED. AFTER TAKEOFF FROM AUS TO STL, FLIGHT 721, HAD THE CO-PILOTS AIRSPEED INDICATOR DECREASE 40 TO 50 KNOTS FROM THE CAPTAINS AIRSPEED INDICATOR. THE CAPTAIN DECLAR - [SDR GAIA9960A](https://openairdocs.org/sdr/GAIA9960A), May 27, 1999: PIN. MISSING. MCO - FLT 1726 - AFTER TAKEOFF, RETRACTED GEAR AND GEAR DOOR LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. PROCEEDED TO MEM AND LANDING WAS SMOOTH. BR - [SDR 98ZZZX2710](https://openairdocs.org/sdr/98ZZZX2710), Jul 2, 1998: B NUT. LOOSE. AIRCRAFT DIVERTED INTO KFLL DUE LOSS OF A-SYSTEM HYDRAULIC FLUID: FOUND B-NUT NR 1 ENGINE MAIN HYD LINE LOOSE. TIGHTENED B-NUT. CHECKED CASE DRAIN FITTINGS. PRE - [SDR 98ZZZX2546](https://openairdocs.org/sdr/98ZZZX2546), Jul 2, 1998: B-NUT. LOOSE. AIRCRAFT DIVERTED INTO KFLL. DUE LOSS OF A-SYSTEM HYDRAULIC FLUID, FOUND B-NUT NR 1 ENGINE MAIN HYDRAULIC LINE LOOSE. TIGHTENED B-NUT, CHECKED CASE DRAIN FITTIN - [SDR B4MR97031](https://openairdocs.org/sdr/B4MR97031), Sep 26, 1997: SKIN. CORRODED. DURING ROUTINE C-CHECK INSPECTION, FOUND LFT WING, O/B MID FLAP, L/E LWR SURFACE, CORROSION ON TWO AREAS. (REFERENCE: O/B ATTACHED FAIRING FWD AREA). REPAIRED I - [SDR B4MR97030](https://openairdocs.org/sdr/B4MR97030), Sep 26, 1997: ANGLE. CORRODED. DURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MLG WW, AFT BULKHEAD LWR CENTER AREA, CORROSION ON T-ANGLE. REMOVED CORROSION ON T-ANGLE, FOUND TO BE OUT OF LIMIT - [SDR B4MR97029](https://openairdocs.org/sdr/B4MR97029), Sep 26, 1997: STRUCTURE. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND LT WING L/E AREA, NR 2 L/E FLAP STA 212 HAS SUPPORT ANGLE WEB CORRODED AND CORROSION AROUND ANCHOR NUTS. FOUND CORRO - [SDR B4MR97028](https://openairdocs.org/sdr/B4MR97028), Sep 26, 1997: FLOORBEAM. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 328 FLOORBEAM AT LBL 3 HAS CORROSION. REPAIRED FLOORBEAM IAW B727 SRM 53-10-8 FIG 3. CORROSION TASK CARD NUMBER - [SDR B4MR97027](https://openairdocs.org/sdr/B4MR97027), Sep 26, 1997: SEAT TRACK. WORN. DURING ROUTINE CPCP CHECK INSPECTION, FOUND FE SEAT TRACK IS WORN. REPLACED FE SEAT TRACK IAW B727 BOEING MM CHAPTER 25-10-81. CORROSION TASK CARD NUMBER C53-22 - [SDR B4MR97026](https://openairdocs.org/sdr/B4MR97026), Sep 26, 1997: SKIN. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND TOP RT ELEVATOR ES92 AREA HAS SURFACE CORROSION OUT OF LIMITS. REPAIRED AND REPLACED A PIECE OF TOP SKIN IAW B727 SR - [SDR B4MR97025](https://openairdocs.org/sdr/B4MR97025), Sep 26, 1997: SKIN. CORROSION. DURING ROUTINE CPCP CHECK INSPECTION, FOUND FORWARD PIT FS 686 S26R TO 25R HAS SURFACE CORROSION ON INTERNAL SKIN. CORROSION OUT OF LIMITS IAW B727 SRM 53-30-1. - [SDR B4MR97024](https://openairdocs.org/sdr/B4MR97024), Sep 26, 1997: SKIN. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND RT MLG W/W OUTBD, ABOVE MLG BEAM, BETWEEN STA 930 AND 940 PRESSURE DECK SKIN AND FASTENERS HAVE CORROSION. REPAIRED - [SDR B4MR97023](https://openairdocs.org/sdr/B4MR97023), Sep 26, 1997: SUPPORT. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND COCKPIT AREA, CO-PILOT SEAT BASE SUPPORT NEEDING ANTI CORROSION TREATMENT ON BOTH AFT ATTACH POINTS. REMOVED AND REP - [SDR B4MR97022](https://openairdocs.org/sdr/B4MR97022), Sep 26, 1997: KEEL BEAM. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND KEEL BEAM RT W/W UNDER APU ANGLE CORRODED TOP AND BOTTOM. OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 51-40-4 PN - [SDR B4MR97021](https://openairdocs.org/sdr/B4MR97021), Sep 26, 1997: SEAT TRACK. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK LBL 40 STA 1140 TO 1030 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORRO - [SDR B4MR97020](https://openairdocs.org/sdr/B4MR97020), Sep 26, 1997: SEAT TRACK. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK LBL 20 STA 1140 TO 1030 CORRODED. REPAIRED SEAT TRACK PER B727 SRM 53-10-5 CORROSION WAS FOUND TO BE OUT - [SDR B4MR97019](https://openairdocs.org/sdr/B4MR97019), Sep 26, 1997: SEAT TRACK. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK RBL 20 STA 1140 TO 1030 CORROSION. REPAIRED SEAT TRACK PER B727 SRM 53-10-5 CORROSION WAS FOUND TO BE OUT - [SDR B4MR97018](https://openairdocs.org/sdr/B4MR97018), Sep 26, 1997: SEAT TRACK. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK RBL 40 STA 1140 TO 1030 CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORR - [SDR B4MR97017](https://openairdocs.org/sdr/B4MR97017), Sep 26, 1997: SEAT TRACK. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1050 TO 1070 LBL 40 SEAT TRACK CORRODED (OLD REPAIR). REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 5 - [SDR B4MR97016](https://openairdocs.org/sdr/B4MR97016), Sep 26, 1997: SEAT TRACK. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1070 TO 1090 RBL 46 SEAT TRACK CORRODED AROUND NUT PLATE AND BETWEEN TRACK AND FLOORBEAM. REMOVED AND REPLACED S - [SDR B4MR97015](https://openairdocs.org/sdr/B4MR97015), Sep 26, 1997: HEAT PLENEM. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND HEAVY CORROSION LT HEAT EXCHANGER PLENEM TOP PLATE AFT END REPAIR PREVIOUSLY ACCOMPLISHED IS CORRODED. ALSO, REPAIRE - [SDR B4MR97014](https://openairdocs.org/sdr/B4MR97014), Sep 26, 1997: SKIN. CORRODED. DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1090R FWD EDGE OF NR 3 CARGO DOOR OPENING HAS CORROSION UNDER LOWER END OF SKIN DOUBLER APPROX STR 25R. REMOVED All 57: https://openairdocs.org/deregistered/N284KH-2007-05-14/reports.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, except the copies of manufacturers’ service documents, which belong to their rights holders.