Mooney M20E

1,122 parts applicable to this airframe — ga_single

Part NumberStatus
102.250PMA
104.250PMA
139.275PMA
563.250PMA
579.250PMA
630053-507OEM
630053-509OEM
630053-511OEM
630053-513OEM
630056-501OEM
850-49, Rev B Group List No 850-49 dtd 1/29/86 or later FAA approved revisionPMA
850-69, Rev F Group List No 850-69 dtd 1/29/86 or later FAA approved revisionPMA
ADVMSI500PMA
All parts listed on installation inst. No. SVSPMA
D57691POEM
Dwg 3320-00046PMA
Dwg 7019PMA
HRJ0057PMA
KI300OEM
Kit Nos. 10, 11 and 20 dwg report no 10 rev 00, dtd 8/38/86PMA
Mitchell Model AK475PMA
Mitchell Model AK476PMA
RA 4ADH DWG: RA 4ADH, Rev. -, Dated 1/8/91PMA
RA 6ADH DWG. : RA 6ADH Rev. -, Dated 1/8/91PMA
RA 6ADH-1 DWG. : RA 6ADH-1, Rev. -, Dated 1/8/91PMA
RA-1J7-1 Drawing: RA1J-7-1 dated July 29, 1985PMA
RA20AOEM
RA30EPMA
RA40APMA
SA00081NYOEM
SA01005DESTC
SA01866WISTC
SA02386AKOEM
SA02511SESTC
SA02511SE (1 OF 2)STC
SA02511SE (1 OF 3)STC
SA02594SESTC
SA02738CH (PAGE 1)OEM
SA02871ATOEM
SA04046CH Page 1OEM
SA04378CHOEM
SA04568CHOEM
SA04837NYOEM
SA11888CHSTC
SA1913SOOEM
SA4503NM (PAGE 1)OEM
SA5788SWOEM
W-, W/T-, -W/G-2118, -RH or -LH, W-, W/T-, W/G-2118-187 -RH or -LHPMA
W-, W/T-, W/G-2116, W-, W/T-, W/G-2116-250PMA
W-, W/T-, W/G-2117, W-, W/T-, W/G-2117-187PMA

Airworthiness Directive activity

FAA / EASA public regulatory data

1airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it
Most recent
  • FAA AD 2023-02-04effective Feb 13, 2023Prohibition

    The FAA is adopting a new airworthiness directive (AD) for certain Mooney International Corporation Model M20C, M20D, M20E, M20F, and M20G airplanes. This AD was prompted by reports of the hybrid material elevator balance weight cracking. This AD requires inspecting to determine whether a certain elevator balance weight is installed. If installed, this AD requires inspecting each affected elevator balance weight for corrosion and cracking, and depending on the findings, either replacing each affected elevator balance weight with a non- hybrid (lead) elevator balance weight or repetitively inspecting each affected elevator balance weight. This AD also prohibits the installation of an affected elevator balance weight on any airplane. The FAA is issuing this AD to address the unsafe condition on these products.

Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.