# N822BX: 1967 Mcdonnell Douglas DC-8-71F, registration cancelled 2014-05-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 1, 2014
- Status when cancelled: Sale reported
- Airframe: [Mcdonnell Douglas DC-8-71F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-71f) (registry code 302199G)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 45813
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 18, 1982
- Last registry action: December 17, 2013
- Mode S code: AB3878
- Location: [Moorpark, CA](https://openairdocs.org/faa-place/CA/Moorpark)
- Owner type: Individual
- Owner's area on the map: 34.3064° N, 118.8906° W: Placed by OpenAirDocs at the center of ZIP code 93021, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N822BX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=822BX
- Page: https://openairdocs.org/deregistered/N822BX-2014-05-01

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-8-71F: https://openairdocs.org/model/mcdonnell-douglas-dc-8-71f.md

## Service difficulty reports (222, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IXXA110044O](https://openairdocs.org/sdr/IXXA110044O), Jun 4, 2011: STRIKER. BENT. DURING CRUISE, THE MLG DOOR LIGHT REMAINED ON. THE CREW CYCLED THE MAIN LANDING GEAR AND LIGHT REMAINED ON. WHEN AIRSPEED INCREASED TO 210 IAS LIGHT WENT OUT. T
- [SDR IXXA110023O](https://openairdocs.org/sdr/IXXA110023O), Feb 18, 2011: WIRE HARNESS. DEFECTIVE. DURING CLIMBOUT FROM KTOL NR ONE EGT ANALOG AND DIGITAL READ OUTS DROPPED FROM 700 DEGREE TO 420 DEGREE WITH FLUCTUATION PLUS/ MINUS 5 DEGREE, N1 AND N2 SIMILAR
- [SDR IXXA100053S](https://openairdocs.org/sdr/IXXA100053S), Oct 11, 2010: SKIN. CORRODED. DURING ROUTINE B-CHECK, INSP FOUND CORROSION ON FUSELAGE SKIN AT STA 73 LONGERON 31 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FA
- [SDR IXXA100021O](https://openairdocs.org/sdr/IXXA100021O), Mar 5, 2010: VALVE. LEAKING. DURING CRUISE, THE RT HYD PRESSURE WAS AT ZERO AND THE LT HYD WAS FLUCTUATING. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RESERVOIR DEPRE
- [SDR IXXA100016O](https://openairdocs.org/sdr/IXXA100016O), Feb 18, 2010: PUMP. CRACKED. DURING CRUISE, THE AILERON AND RUDDER REVERSION LIGHT CAME ON, THE CREW ALSO NOTICED LOSS OF HYD PRESSURE AND QUANTITY. CREW ACCOMPLISHED PROCEDURES IAW QRH NR 
- [SDR IXXA100006S](https://openairdocs.org/sdr/IXXA100006S), Dec 23, 2009: SKIN. CRACKED. LT WING LOWER SKIN CRACKED AT STATION 428.0. REPAIRED SKIN IAW CASTLE SKETCH 20100104028.
- [SDR IXXA100004S](https://openairdocs.org/sdr/IXXA100004S), Dec 23, 2009: STRINGER. CRACKED. LT WING STRINGER 62 CRACKED. REPAIRED STRINGER IAW SRM 57-2-1 AND CASTLE SKETCH 20100104018.
- [SDR IXXA100005S](https://openairdocs.org/sdr/IXXA100005S), Dec 23, 2009: STRINGER. CRACKED. LT WING STRINGER 63 CRACKED. REPAIRED STRINGER 63 IAW SRM 57-2-1 AND CASTLE SKETCH 20100104018.
- [SDR IXXA100003S](https://openairdocs.org/sdr/IXXA100003S), Dec 23, 2009: STRINGER. CRACKED. RT WING FOUND STRINGER 62 CRACKED. REPAIRED STRINGER 62 IAW SRM 57-2-2.
- [SDR IXXA100002S](https://openairdocs.org/sdr/IXXA100002S), Dec 23, 2009: SKIN. CRACKED. RT WING LOWER SKIN CRACKED BETWEEN FWD AND AFT OF STRINGER 62. REPAIRED SKIN IAW SRM 57-2-1.
- [SDR IXXA090074O](https://openairdocs.org/sdr/IXXA090074O), Dec 15, 2009: ADI. DEFECTIVE. DURING CLIMB OUT, CAPTAIN’S FLIGHT DIRECTOR INDICATOR READ’S DIFFERENT FROM THE F/O FLIGHT DIRECTOR INDICATOR, ALSO READ’S DIFFERENT IN FLIGHT LEVEL AND DESCENT
- [SDR IXXA090070O](https://openairdocs.org/sdr/IXXA090070O), Dec 11, 2009: RELIEF VALVE. DEFECTIVE. DURING CLIMB OUT, HYD PRESSURE DROPPED TO ZERO, AILERON AND MANUAL REVERSION LIGHTS ILLUMINATED. THE CREW ACCOMPLISHED ALL PROCEDURES IAW QRH, NO LOSS OF HYD QU
- [SDR IXXA090054O](https://openairdocs.org/sdr/IXXA090054O), Sep 30, 2009: RMI. DEFECTIVE. DURING CRUISE, THE COMPASS CARD ON NR 2 RADIO MAGNETIC INDICATOR FROZE IN POSITION. AFTER SEVERAL MINUTES THE COMPASS CARD STARTED MOVING BUT IS 180 DEGREE OFF 
- [SDR IXXA090046O](https://openairdocs.org/sdr/IXXA090046O), Sep 1, 2009: FIRE LOOP. DEFECTIVE. DURING CLIMB OUT, NR 4 FIRE WARNING HORN SOUNDED, THEN SILENCED AND SOUNDED AGAIN. THE CREW DISCHARGED BOTH BOTTLES AND SHUTDOWN NR 4 ENGINE. CREW RETURNED TO D
- [SDR IXXA090045O](https://openairdocs.org/sdr/IXXA090045O), Aug 31, 2009: RADIO. DEFECTIVE. DURING CLIMB OUT, NR 2 VHF RADIO WILL NOT TRANSMIT FROM ANY POSITION. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED FIRST OBSERVERS AU
- [SDR IXXA090014O](https://openairdocs.org/sdr/IXXA090014O), Apr 1, 2009: WIRE. DEFECTIVE. DURING CRUISE FROM KPHL, BOTH AILERON AND RUDDER MANUAL LIGHTS CAME ON, HYDRAULIC SYSTEM PRESSURE INDICATED ZERO, HYDRAULIC QUANTITY SHOWS FULL. THE CREW ACCOMP
- [SDR IXXA090009O](https://openairdocs.org/sdr/IXXA090009O), Mar 10, 2009: FIRE LOOP. FALSE ACTIVATION. DURING CLIMB FROM MGUM NR 4 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED, FIRE WARNING WOULD NOT TEST. THE CREW SHUTDOWN NUMBER FOUR ENGINE PER COM PROCEDURES. WIND M
- [SDR G412008F00000](https://openairdocs.org/sdr/G412008F00000), Jun 6, 2008: GROUND WIRE. BROKEN. AFTER TAKEOFF FROM KIAH, NR 1 ENGINE FIRE WARNING SOUNDED, FIRE HANDLE LIGHT, AND MASTER FIRE WARNING LIGHT ILLUMINATED. WARNING HORN COULD BE SILENCED BUT CAME
- [SDR IXXA08SMN090S](https://openairdocs.org/sdr/IXXA08SMN090S), Feb 26, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 5 TRACK NUT BARRIER FITTING CRACKED AT STATION 70.000. REMOVED CRACKED FITTING. FABRICATE
- [SDR IXXA08SMN081S](https://openairdocs.org/sdr/IXXA08SMN081S), Feb 15, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 857.000 LONGERON 1. REMOVED CRACKED FITTING. FABRICATED FITTING PERFO
- [SDR IXXA08SMN088S](https://openairdocs.org/sdr/IXXA08SMN088S), Feb 15, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LOWER FORWARD PANEL PLATING DENTED AT STATION XW 2.000 - STA XW 91.000. REMOVED FASTENERS AS NEEDED T
- [SDR IXXA08SMN087S](https://openairdocs.org/sdr/IXXA08SMN087S), Feb 15, 2008: SKIN. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER INNER SKIN INBOARD SPLICE CRACKED AT STATION XFS 341.000. REMOVED FASTENERS AS NEE
- [SDR IXXA08SMN085S](https://openairdocs.org/sdr/IXXA08SMN085S), Feb 15, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN DENTED AT STATION XE 246.875. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SK
- [SDR IXXA08SMN084S](https://openairdocs.org/sdr/IXXA08SMN084S), Feb 15, 2008: SKIN. MISREPAIRED. DURING ROUTINE C CHECK, FOUND AT EXTERNAL DOUBLER AFT LOWER FUSELAGE BELLY TAIL SKID FAIRING HAS IMPROPER REPAIR AT STATION FS 1745 LONGERON 35.5 LEFT. REMOVED 
- [SDR IXXA08SMN082S](https://openairdocs.org/sdr/IXXA08SMN082S), Feb 15, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FRAME FITTING CRACKED AT STATION 879.000 LONGERON 18 RIGHT TO LONGERON-19 RIGHT. REMOVED FASTENERS AS NEEDED
- [SDR IXXA08SMN089S](https://openairdocs.org/sdr/IXXA08SMN089S), Feb 15, 2008: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LEADING CENTER LEADING EDGE OUTER SKIN LOWER SHOWS IMPROPER REPAIR AT STATION XFS 385.200. REMOVED FASTENERS
- [SDR IXXA08SMN086S](https://openairdocs.org/sdr/IXXA08SMN086S), Feb 15, 2008: SKIN. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE TAIL SECTION PLATING CRACKED AT STATION FS 1766.000 TO STATION 1781.000 LONGERON10 LEFT. REMOVED FASTENER
- [SDR IXXA08SMN080S](https://openairdocs.org/sdr/IXXA08SMN080S), Feb 15, 2008: SUPPORT FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SKID SUPPORT FITTING CRACKED AT STATION 1734.000 LONGERON36. REMOVED CRACKED FITTING. CLEANED, TREATED AN
- [SDR IXXA08SMN079S](https://openairdocs.org/sdr/IXXA08SMN079S), Feb 15, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD AFT LOWER FLAP SKIN SHOWS DENTS AT STATION XE 2.000 TO STA XE 91.000. REMOVED FASTENERS AS NEEDED TO 
- [SDR IXXA08SMN078S](https://openairdocs.org/sdr/IXXA08SMN078S), Feb 15, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS DENT AND NO STANDARD REPAIR AT STATION XA 580.000 TO XA 610.000. REMOVED FASTENERS
- [SDR IXXA08SMN077S](https://openairdocs.org/sdr/IXXA08SMN077S), Feb 14, 2008: FRAME. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME LOWER FLANGE CRACKED AT STATION 480.000 LONGERON 34 RIGHT. REMOVED DAMAGED AREA. FABRIC
- [SDR IXXA08SMN076S](https://openairdocs.org/sdr/IXXA08SMN076S), Feb 14, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND ELEVATOR LEFT UPPER SKIN SHOWS DENTS AND CORROSION AT DIFFERENT POINTS AT STATION XE 146.000 AND XE 270.000. REMOVED CO
- [SDR IXXA08SMN075S](https://openairdocs.org/sdr/IXXA08SMN075S), Feb 14, 2008: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XOLDI 6.2246. REMOVED FASTENERS AS NEE
- [SDR IXXA08SMN074S](https://openairdocs.org/sdr/IXXA08SMN074S), Feb 14, 2008: SKIN. MISREPAIRED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATION XFS 304.000. REMOVED FASTENERS AS NEED
- [SDR IXXA08SMN072S](https://openairdocs.org/sdr/IXXA08SMN072S), Feb 14, 2008: SKIN. SCRATCHED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN SHOWS SCRATCHES AT STATION XE 273.000 TO STATION XE 283.000. REMOVED FASTENERS AS NEEDED TO PE
- [SDR IXXA08SMN073S](https://openairdocs.org/sdr/IXXA08SMN073S), Feb 14, 2008: FLAP. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBD FLAP UPPER PART SHOWS DENTS AT STATION XF 375.000 TO STA XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM 
- [SDR IXXA08SMN070S](https://openairdocs.org/sdr/IXXA08SMN070S), Feb 14, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO INTERCOSTAL END CLIP CRACKED AT STATION 857.000 LONGERON 18 RIGHT. REMOVED CRACKED INTERCOSTAL END CLIP. FAB
- [SDR IXXA08SMN047S](https://openairdocs.org/sdr/IXXA08SMN047S), Feb 14, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1690.000 LONGERON 28 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREA
- [SDR IXXA08SMN071S](https://openairdocs.org/sdr/IXXA08SMN071S), Feb 14, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER AFT SKIN HAS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMO
- [SDR IXXA08SMN065S](https://openairdocs.org/sdr/IXXA08SMN065S), Feb 8, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN FORWARD SHOWS DENTS BETWEEN STATION XF 160.000 - XF 213.000. PERFORMED DETAILED VISUAL IN
- [SDR IXXA08SMN067S](https://openairdocs.org/sdr/IXXA08SMN067S), Feb 8, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 847.000 LONGERON1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIM
- [SDR IXXA08SMN63S](https://openairdocs.org/sdr/IXXA08SMN63S), Feb 8, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN SHOWS DENTS AT STATION XF 434.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED
- [SDR IXXA08SMN062S](https://openairdocs.org/sdr/IXXA08SMN062S), Feb 8, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED A
- [SDR IXXA08SMN061S](https://openairdocs.org/sdr/IXXA08SMN061S), Feb 8, 2008: FITTING. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 TO STATION 980.000 LEFT BUTTOCKS LINE 45. REMOVED CORRODED F
- [SDR IXXA08SMN066S](https://openairdocs.org/sdr/IXXA08SMN066S), Feb 8, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 690.000 LONGERON 1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRI
- [SDR IXXA08SMN064S](https://openairdocs.org/sdr/IXXA08SMN064S), Feb 8, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN DENTS AT STATION XF 169.000 - XF 213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. 
- [SDR IXXA08SMN054S](https://openairdocs.org/sdr/IXXA08SMN054S), Feb 7, 2008: SKIN. SCRATCHED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN SCRATCHED BETWEEN STATION XA 737.000 AND XA 763.000. REMOVED FASTENERS AS NEEDED TO PE
- [SDR IXXA08SMN053S](https://openairdocs.org/sdr/IXXA08SMN053S), Feb 7, 2008: SUPPORT ANGLE. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FORMER CRACKED AT STATION 1766.000 LONGERON1. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP 
- [SDR IXXA08SMN052S](https://openairdocs.org/sdr/IXXA08SMN052S), Feb 7, 2008: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 20 RT. REMOVE CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA.
- [SDR IXXA08SMN058S](https://openairdocs.org/sdr/IXXA08SMN058S), Feb 7, 2008: SKIN. DENTED. DURING ROUTINE C CHECK INSPECTION, FOUND RUDDER RIGHT SKIN SIDE DENTED AT STATION ZR 276.531 TO ZR 267.218. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOV

All 222: https://openairdocs.org/deregistered/N822BX-2014-05-01/reports.md

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