PZL-Swidnik S.A. Airworthiness Directives

53 ADs indexed for PZL-Swidnik S.A. aircraft.

Models

PZL W-3A 13 ADs Swidnik S.A. 6 ADs F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD F.260F 1 AD S.205 - 18/F 1 AD S.205 - 18/R 1 AD S.205 - 20/F 1 AD S.205 - 20/R 1 AD AEIO-320-D1B 1 AD AEIO-320-D2B 1 AD AEIO-320-E1A 1 AD AEIO-320-E1B 1 AD AEIO-320-E2A 1 AD AEIO-320-E2B 1 AD AEIO-360-B1B 1 AD AEIO-360-B1D 1 AD AEIO-360-B1F 1 AD AEIO-360-B1F6 1 AD 107-II 1 AD 1100 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 206 1 AD 206A 1 AD 206A-1 1 AD 206A-1 (OH-58A) 1 AD 206B 1 AD 206B-1 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 210 1 AD 212 1 AD 222 1 AD 222B 1 AD 222U 1 AD 230 1 AD 234 1 AD 269A 1 AD 269A-1 1 AD 269B 1 AD 269C 1 AD 269C-1 1 AD 269D 1 AD 280 1 AD 280C 1 AD 280F 1 AD 280FX 1 AD 305 1 AD 369 1 AD 369A 1 AD 369D 1 AD 369E 1 AD 369F 1 AD 369FF 1 AD 369H 1 AD 369HE 1 AD 369HM 1 AD 369HS 1 AD 407 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 427 1 AD 429 1 AD 430 1 AD 47 1 AD 47B 1 AD 47B3 1 AD 47D 1 AD 47D1 1 AD 47E 1 AD 47G 1 AD 47G-2 1 AD 47G-2A 1 AD 47G-2A-1 1 AD 47G-3 1 AD 47G-3B 1 AD 47G-3B-1 1 AD 47G-3B-2 1 AD 47G-3B-2A 1 AD 47G-4 1 AD 47G-4A 1 AD 47G-5 1 AD 47G-5A 1 AD 47H-1 1 AD 47J 1 AD 47J-2 1 AD 47J-2A 1 AD 47K 1 AD 480 1 AD 480B 1 AD 500N 1 AD 505 1 AD 600N 1 AD A109 1 AD A109A 1 AD A109A II 1 AD A109C 1 AD A109E 1 AD A109K2 1 AD A109S 1 AD A119 1 AD AB139 1 AD AB412 1 AD AB412 EP 1 AD AS-365N2 1 AD AS-365N3 1 AD AS332C 1 AD AS332C1 1 AD AS332L 1 AD AS332L1 1 AD AS332L2 1 AD AS350B 1 AD AS350B1 1 AD AS350B2 1 AD AS350B3 1 AD AS350BA 1 AD AS350C 1 AD AS350D 1 AD AS350D1 1 AD AS355E 1 AD AS355F 1 AD AS355F1 1 AD AS355F2 1 AD AS355N 1 AD AS355NP 1 AD AW109SP 1 AD AW119 MKII 1 AD AW139 1 AD AW169 1 AD AW189 1 AD B-2 1 AD B-2A 1 AD B-2B 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-1 1 AD BO-105LS A-3 1 AD BO-105S 1 AD CABRI G2 1 AD CH-47D 1 AD CH-54A 1 AD EC 155B 1 AD EC120B 1 AD EC130B4 1 AD EC130T2 1 AD EC155B1 1 AD EC225LP 1 AD F-28 1 AD F-28A 1 AD F-28C 1 AD F-28C-2 1 AD F-28C-2R 1 AD F-28F 1 AD F-28F-R 1 AD FH-1100 1 AD K-190A 1 AD K-225 1 AD K-240 1 AD K-600 1 AD MBB-BK 117 A-1 1 AD MBB-BK 117 A-3 1 AD MBB-BK 117 A-4 1 AD MBB-BK 117 B-1 1 AD MBB-BK 117 B-2 1 AD MBB-BK 117 C-1 1 AD MBB-BK 117 C-2 1 AD MBB-BK 117 D-2 1 AD MBB-BK 117 D-3 1 AD MD900 1 AD OH-13E 1 AD OH-13H 1 AD PZL W-3A 1 AD R22 1 AD R22 ALPHA 1 AD R22 BETA 1 AD R22 MARINER 1 AD R44 1 AD R44 II 1 AD R66 1 AD S-51 1 AD S-52 1 AD S-55 1 AD S-55B 1 AD S-55C 1 AD S-58A 1 AD S-58B 1 AD S-58BT 1 AD S-58C 1 AD S-58D 1 AD S-58DT 1 AD S-58E 1 AD S-58ET 1 AD S-58F 1 AD S-58FT 1 AD S-58G 1 AD S-58H 1 AD S-58HT 1 AD S-58J 1 AD S-58JT 1 AD S-61A 1 AD S-61D 1 AD S-61E 1 AD S-61L 1 AD S-61N 1 AD S-61NM 1 AD S-61R 1 AD S-61V 1 AD S-64A 1 AD S-64E 1 AD S-64F 1 AD S-70 1 AD S-70A 1 AD S-70C 1 AD S-70C(M) 1 AD S-70C(M1) 1 AD S-70M 1 AD S-76A 1 AD S-76B 1 AD S-76C 1 AD S-76D 1 AD S-92A 1 AD S62A 1 AD SA 3180-Alouette Astazou 1 AD SA 318B-Alouette Astazou 1 AD SA 318C-Alouette Astazou 1 AD SA-365C 1 AD SA-365C1 1 AD SA-365C2 1 AD SA-365N 1 AD SA-365N1 1 AD SA-366G1 1 AD SA.315B Alouette III 1 AD SA.316B Alouette III 1 AD SA.316C Alouette III 1 AD SA.319B Alouette III 1 AD SA330J 1 AD SA341G 1 AD SA342J 1 AD SE 3130-Alouette II 1 AD SE 313B-Alouette II 1 AD SE.3160 Alouette III 1 AD TH-1L 1 AD TH-28 1 AD UH-12 1 AD UH-12A 1 AD UH-12B 1 AD UH-12C 1 AD UH-12E 1 AD UH-12E-L 1 AD UH-12L 1 AD UH-12L4 1 AD UH-1E 1 AD UH-1L 1 AD AS-365N2 1 AD AS-365N3 1 AD AS332C 1 AD AS332C1 1 AD AS332L 1 AD AS332L1 1 AD AS332L2 1 AD EC 155B 1 AD EC155B1 1 AD EC225LP 1 AD A319-111 1 AD A319-112 1 AD A319-113 1 AD A319-114 1 AD A319-115 1 AD A319-131 1 AD A319-132 1 AD A319-133 1 AD A319-151N 1 AD A319-153N 1 AD PZL-104 WILGA 80 1 AD 328-100 1 AD F.260 1 AD F.260B 1 AD F.260C 1 AD F.260D 1 AD F.260E 1 AD GTX 33 1 AD GTX 330 1 AD GTX 330D 1 AD GTX 33D 1 AD S.A. 1 AD PW-5 Smyk 1 AD PW-6U 1 AD

Recent ADs

2026-02-02 Recurring

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Airworthiness Directives; PZL-Swidnik S.A. Helicopters

Unsafe Condition: The detection of corrosion on the main rotor blade (MRB) attachment bolts, which could lead to cracks and failure of one or more of the MRB attachment bolts and result in loss of an MRB and consequ...

Effective: Feb 6, 2026 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; PZL-Swidnik S.A. Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2023-11-07

final rule

Airworthiness Directives; Various Helicopters

Unsafe Condition: unsafe condition on these products.

Effective: Jun 22, 2023 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Helicopters

2022-03-15

final rule

Airworthiness Directives; Various Airplanes

Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...

Effective: Mar 21, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Airplanes

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

2022-01-03

final rule

Airworthiness Directives; Umlaut Engineering GmbH (Previously P3 Engineering GmbH) HAFEX (Halon-Free) Hand-Held Fire Extinguishers

Unsafe Condition: The spindle geometries of the fire extinguishers were found to be out of tolerance, which could cause a non-detectable seizure of the spindle that could cause the fire extinguisher to be inoperative.

Effective: Mar 7, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Umlaut Engineering GmbH (Previously P3 Engineering GmbH) HAFEX (Halon-Free) Hand-Held Fire Extinguishers

2021-22-07 Recurring

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Airworthiness Directives; Umlaut Engineering GmbH (Previously P3 Engineering GmbH) HAFEX (Halon-Free) Hand-Held Fire Extinguishers

Unsafe Condition: Prolonged exposure to high temperature conditions can dislodge the spindle in the fire extinguisher head, subsequently making the fire extinguisher inoperative.

Effective: Nov 18, 2021 Category: aircraft Compliance: Within 30 days after the effective date of this AD

Why matched: Airworthiness Directives; Umlaut Engineering GmbH (Previously P3 Engineering GmbH) HAFEX (Halon-Free) Hand-Held Fire Extinguishers

2021-18-12 Recurring

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: fractured bracket bolts

Effective: Oct 12, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

2021-18-15

final rule

Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: displaced teeth were detected on the moveable assemblies of a main rotor (MR) blade droop stop, which could result in erroneous operation of MR blade droop stop teeth during engine start-up or shut...

Effective: Oct 12, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2021-17-13

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: Damage to the wheel braking system pneumatic line fitting installed on the left-hand (LH) main landing gear (MLG) leg, which could result in loss of MLG wheel braking capability and subsequent loss...

Effective: Sep 7, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2021-16-20

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: A bolt part number (P/N) 3003A-6-16-3 was found broken on fairing P/N 30.23.015.00.03 installed on vibration absorber P/N 30.23.000.00.04. This condition, if not corrected, could lead to detachment...

Effective: Aug 26, 2021 Category: aircraft Compliance: Within 300 hours time-in-service after the effective date of this AD

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

2021-08-16 Recurring

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: occurrences were reported of cables found worn out; the damage consisted of reduction of the cable diameter near the swaged terminal. This condition, if not detected and corrected, could lead to re...

Effective: May 11, 2021 Category: aircraft Compliance: within 25 hours time-in-service accumulated by the hoist (hoist hours) after the effective date o...

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

2020-15-06 Recurring

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: Cracks on the Main XMSN case housing, which could lead to structural failure and loss of load carrying capabilities of the Main XSMN, possibly resulting in loss of helicopter control.

Effective: Aug 11, 2020 Category: aircraft Compliance: Within 5 hours time-in-service (TIS), and thereafter at intervals not to exceed 25 hours TIS.

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

2020-15-11 Recurring

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: Corrosion was found on the main rotor vibration absorber star during routine maintenance, which could lead to structural failure of the vibration absorber star, possibly resulting in damage to the ...

Effective: Aug 11, 2020 Category: aircraft Compliance: Within 300 hours time-in-service (TIS) or 12 months, whichever occurs first

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2020-16-03

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: An error in the Airworthiness Limitations for PZL Model PZL W-3A helicopters, which incorrectly stated the life limit for horizontal stabilizer part number (P/N) 30.13.600.00.04 up to serial number...

Effective: Aug 10, 2020 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

2020-07-22

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: occurrences of improperly locked bolts, which secure the input quill cover and graphite seal assembly of the WR-3 MGB, could lead to disconnection of the engines to the MGB mechanical link, possibl...

Effective: May 5, 2020 Category: engine Compliance: Within 25 hours time-in-service

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

2020-07-15

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Airworthiness Directives; PZL Świdnik S.A. Helicopters

Unsafe Condition: cracking in a nose landing gear (NLG) bellcrank assembly, part number (P/N) 30.42.010.01.00, due to reduced wall thickness, which resulted from a manufacturing deficiency.

Effective: Apr 29, 2020 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

2015-13-03

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Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa “PZL-Bielsko” Sailplanes

Unsafe Condition: Detachment of the rudder cable fitting block from the fuselage.

Effective: Aug 3, 2015 Category: aircraft Compliance: Within 30 days after August 13, 2015.

Why matched: Airworthiness Directives; Przedsiebiorstwo Doswiadczalno- Produkcyjne Szybownictwa ``PZL-Bielsko'' Sailplanes

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

2014-12-08

final rule

Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa “PZL-Bielsko” Model SZD-50-3 “Puchacz” Sailplanes

Unsafe Condition: Fatigue damage of the welded joint between the airbrake torque tube and the airbrake control system lever located inside the fuselage.

Effective: Jul 22, 2014 Category: aircraft Compliance: Initially within 30 days after July 22, 2014, and repetitively as specified.

Why matched: Airworthiness Directives; Przedsiebiorstwo Doswiadczalno- Produkcyjne Szybownictwa ``PZL-Bielsko'' Model SZD-50-3 ``Puchacz'' Sailplanes

2012-13-10

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Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition: Rotation of the generator air outlet collector, which could lead to restricted cyclic control stick movement and subsequent loss of control of the helicopter.

Effective: Aug 1, 2012 Category: aircraft Compliance: Within 100 hours time-in-service.

Why matched: Airworthiness Directives; PZL Swidnik S.A. Helicopters

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2011-18-07

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Airworthiness Directives; WYTWORNIA SPRZETU KOMUNIKACYJNEGO (WSK) “PZL-RZESZOW”-SPOLKA AKCYJNA (SA) PZL-10W Turboshaft Engines

Unsafe Condition: Excessive wear on spline teeth of the fuel metering pump shaft.

Effective: Oct 17, 2011 Category: aircraft Compliance: Within 50 flight hours after the effective date.

Why matched: Airworthiness Directives; WYTWORNIA SPRZETU KOMUNIKACYJNEGO (WSK) "PZL-RZESZOW''--SPOLKA AKCYJNA (SA) PZL--10W Turboshaft Engines

2009-14-10

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Airworthiness Directives; EADS-PZL “Warszawa-Okęcie” S.A. Model PZL-104 WILGA 80 Airplanes

Unsafe Condition: Severe corrosion of the steel front fuselage structural elements, which if left uncorrected, could lead to loss of strength of the structural front posts elements and consequent reduction of the st...

Effective: Aug 12, 2009 Category: aircraft Compliance: Within 12 years from date of manufacture or within the next 2 months after May 18, 2009, whicheve...

Why matched: Airworthiness Directives; EADS-PZL "Warszawa-Okecie'' S.A. Model PZL-104 WILGA 80 Airplanes

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