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Aircraft record

N127NKDouglas DC-9-21

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched41 service difficulty reports

Registration
Valid
expires Sep 30, 2028
Based in
Perris, CA
owner city / state
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
41
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Perris Valley Airport INC
Owner type
Corporation
City, state
Perris, CA
Certificate issued
Sep 18, 2018
Expires
Sep 30, 2028
Airworthiness
Standard · Transport
Airworthiness date
May 12, 1995

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Douglas
Model
DC-9-21
Serial number
47361
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
85
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A06EE9

Engine

Make and model
P & W Jt8d Series
Type
Turbo-jet
Power
7,700 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2018 – nowPerris Valley Airport INCPerris, CA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (41)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Pneumatic · duct · rupturedNov 2, 2002

    LAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MX DISCOVERED BLEED AIR LEAK FROM AN UNKNOWN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Pneumatic · duct · rupturedNov 2, 2002

    LAS - TAIL COMPARTMENT HIGH TEMP ANNUNCIATOR INDICATION ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED TAIL COMPARTMENT AND ASSOCIATED PRESSURIZATION DISTRIBUTION SYSTEM FOR CAUSE OF HIGH TEMP INDICATION. MAINTENANCE DISCOVERED BLEED AIR LEAK FROM AN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · duct · crackedNov 2, 2002

    TAIL COMP HIGH TEMP ANNUNCIATOR INDIC ILLUMINATED INFLIGHT. AC RETURNED TO STATION W/O INCIDENT. MAINT INSP TAIL COMP AND ASSOC PRESS DIST SYS FOR CAUSE OF HIGH TEMP INDICATION. MAINT DISCOVERED BLEED AIR LEAK FROM AN UNKNOWN SOURCE IN THE RT AIR COND SYS. MAINT DEFERRED RT AIR COND SYS IAW MEL.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine · drive gear · failedSep 18, 2002

    ENROUTE, NR 1 ENGINE LOW OIL PRESSURE ANNUNCIATOR INDICATION ILLUMINATED. CREW COMPLIED WITH AOM EMERGENCY/ ABNORMAL PROCEDURES. PRECAUTIONARY INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED. AIRCRAFT CONTINUED TO STATION WITHOUT INCIDENT. THE ENGINE WAS REMOVED AND SENT FOR EVALUATION. THE NR 4, 7, AND 5…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · attach fitting · crackedJul 25, 2001

    LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, CRACKED DETECTED BY VISUAL INSPECTION AT VERTICAL STABILIZER LEFT DORSAL FIN ATTACH FITTING. HFEC INSPECTION CONFIRMED CRACKS EMANATING FROM EIGHT FASTENERS HOLES. REMOVED AND REPLACED DORSAL FIN ATTACH FITTING IAW DC9 SRM 51-10-2…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · aileron · delaminatedJul 25, 2001

    LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT AILERON INBOARD TAB DELAMINATION DETECTED ON LOWER OUTBOARD SIDE. DELAMINATION REPORTED TO BE AN AREA OF APPROXIMTELY 5 SQUARE INCHES. CUTOUT DELAMINATED AREA (APPROX 10 INCHES BY 3 INCHES). FABRICATED FILLER AND DOUBLER, HEAT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · pan · crackedJul 25, 2001

    LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND AFT CARGO DOOR CRACKED AROUND RIVNUT FASTENER AT LOWER FORWARD CORNER. ROUTED OUT CRACK ON AFT CARGO DOOR, FORWARD LOWER JAMB. FORMED DOUBLER REPAIR AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 52-01 FIGURE 2, 51-20-0 AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · skin · crackedJul 25, 2001

    LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, FOUND FORWARD CARGO DOOR INNER SKIN CRACKED IN THE RADIUS BELOW AFT LATCH COVER. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC9 SRM 51-10-4, 52-05 FIGURE 26A, 51-30-5, 51-30-2, AND 51-10-3. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJul 25, 2001

    LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEVEL 1 CORROSION WAS FOUND IN LOWER AFT FUSELAGE SKIN AT AFT JACK PAD AREA. CORROSION DAMAGE TO FASTENERS IN AREA ALSO DETECTED. REMOVED INTERNAL AND EXTERNAL STRUCTURE IN LOWER FUSELAGE JACK PAD AREA FOR ACCESS. REPAIRED CORRODED SKIN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · jackscrew · wornJul 25, 2001

    LCQ - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, HORIZONTAL STABILIZER JACKSCREW FAILED END PLAY CHECK PER WORK CARD 0855, SB 27A362 AND AD 2000-15-15. JACKSCREW END PLAY REPORTED AT .041 INCHES. REMOVED AND REPLACED HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WITH OVERHAULED UNIT IAW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 41 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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