MEL 30-09 Pitot, Pitot/Static and Temperature Probe Heater Lights • BoredAviator

MEL 30-09

⚠ RAPPEL HOT — RESTRICTION MEL

PAS DE GIVRE · HEATER LIGHTS

Heater verified + not operated in known or forecast icing.

Qu’est-ce que c’est

Item MEL « Pitot, Pitot/Static and Temperature Probe Heater Lights » (ATA 30-09) du système antigivre / pluie sur Boeing 737-800 NG (flotte Air Inuit). Cette page est une aide équipage. Le MEL officiel AILO-0903 fait toujours foi pour le dispatch.

Item MEL

ATA 30-09 — Pitot, Pitot/Static and Temperature Probe Heater Lights.
Catégorie(s) : B, C.
Rappel délais : B — 3 jours calendaires ; C — 10 jours calendaires.

Source PDF · AILO-0903 Amdt 5 · 2026-01-08. Colonnes : CAT · 2. NUMBER INSTALLED · 3. NUMBER REQUIRED FOR DISPATCH · 4. REMARKS OR EXCEPTIONS. En-tête item : Amdt 5 · 2026-01-08.

30-09 — Pitot, Pitot/Static and Temperature Probe Heater Lights

CAT — · installé — · requis dispatch —

30-09-02 — Amber (Heater Off) Lights

CAT — · installé — · requis dispatch —

30-09-02-01 — Pitot and Pitot/Static

CAT B · installé 6 · requis dispatch 0

(M#) Except for ER operations beyond 120 minutes, may be inoperative provided: a) Associated heater function is verified to operate normally, and b) Airplane is not operated in known or forecast icing conditions.

30-09-02-02 — Temperature

CAT — · installé — · requis dispatch —

30-09-02-02A

CAT C · installé 1 · requis dispatch 1

30-09-02-02B

CAT C · installé 1 · requis dispatch 0

(M#) May be inoperative provided associated heater function is verified to operate normally before each departure.

30-09-02-02C

CAT C · installé 1 · requis dispatch 0

May be inoperative provided associated heater is inoperative

Explication (français)

Dispatch selon le MEL Air Inuit AILO-0903 (texte extrait du PDF dans l’app). Catégorie(s) de réparation : B — 3 jours calendaires ; C — 10 jours calendaires. 7 condition(s) de relief extraite(s) du tableau officiel (installé / requis / remarques). Une procédure (M#) maintenance (personnel maintenance obligatoire) s’applique avant dispatch — voir ci-dessous. Les switch names, notes et chiffres ci-dessous sont ceux du MEL. Ne pas ajouter d’étape qui n’y figure pas.

Procédure équipage — (O) / (M) / placard

1. Confirmer l’item, la catégorie et le nombre requis dans le MEL officiel (lien PDF).

2. Appliquer les procédures (O) et/ou (M) du MEL avant dispatch — texte officiel ci-dessous.

3. Placard (texte MEL) :

Apply sticker adjacent to affected Pitot, Pitot/Static Temperature Probe Heater Light.

4. Journey log / other instructions (texte MEL) :

Print the following information in the journey log sheet. (CAPT) (F/O) (PITOT) (STATIC) (L) (R) (ELEV PITOT)(TEMP PROBE) HEATER LIGHT INOP

5. Respecter toutes les restrictions du MEL — ne pas en inventer.

(O) OPERATIONS PROCEDURES — texte MEL :

None required.

(M) MAINTENANCE PROCEDURES — texte MEL (maintenance ; l’équipage vérifie que c’est fait) :

None required.

(M#) MAINTENANCE PROCEDURES — personnel maintenance obligatoire — texte MEL :

30-09-02-01 Pitot and Pitot/Static Lights: Verify that probe heater operates normally (AMM 30-00-00/901). 1. Station ground observer at associated probe heater, establish communications. 2. Ensure covers are removed from all air data probes and vanes 3. Supply electrical power to airplane (AMM 24-22-00). 4. Position the associated PITOT STATIC HEAT switch or PROBE HEAT switch to the ON position. 5. Verify that heat radiation can be detected from associated probe, indicating that heater is functioning. DO NOT TOUCH PROBE. CAUTION: DO NOT PLACE HAND ON PROBE. TEMPERATURES ARE HIGH ENOUGH TO CAUSE BURNS. DO NOT LEAVE HEATER ON LONGER THAN REQUIRED. HEATER LIFE MAY BE UNNECESSARILY SHORTENED. 6. Position the associated PITOT STATIC HEAT switch or PROBE HEAT switch to the OFF or AUTO position. 7. Restore airplane electrical system to normal. 8. Advise Dispatch. Flight Planning may be affected. 30-09-02-02B Temperature Lights Verify that probe heater operates normally prior to each departure (AMM 30-00-00/901). 1. Station ground observer at associated probe heater, establish communications. 2. Ensure covers are removed from all air data probes and vanes. 3. Supply electrical power to airplane (AMM 24-22-00). 4. For airplanes with non-aspirated TAT probes with air/ground logic for probe heater power, verification of TAT probe heater operation requires that the airplane be placed in simulated "air" mode per AMM 32-09-00. 5. Position the associated PITOT STATIC HEAT switch or PROBE HEAT switch to the ON position. For aspirated TAT probes, momentarily press/hold TAT TEST switch when verifying the TAT probe heater. 6. Verify that heat radiation can be detected from associated probe, indicating that heater is functioning. DO NOT TOUCH PROBE. CAUTION: DO NOT PLACE HAND ON PROBE. TEMPERATURES ARE HIGH ENOUGH TO CAUSE BURNS. DO NOT LEAVE HEATER ON LONGER THAN REQUIRED. HEATER LIFE MAY BE UNNECESSARILY SHORTENED. 7. Position the associated PITOT STATIC HEAT switch or PROBE HEAT switch to the OFF or AUTO position. 8. Restore airplane electrical system to normal.

Restrictions / notes (extrait MEL)

(CAPT) (F/O) (PITOT) (STATIC) (L) (R) (ELEV PITOT)(TEMP PROBE) HEATER LIGHT INOP

QRH / procédures liées dans l’app

Liens vers des pages déjà présentes (QRH). Ce ne sont pas des procédures FCOM inventées. Le QRH officiel fait foi.

QRH section 03 — Anti-Ice, Rain (index)

Aide-mémoire formation. Le MEL Air Inuit officiel (AILO-0903) Amdt 5 (2026-01-08) fait toujours foi pour le dispatch, les (O)/(M) et les restrictions. Cette page ne remplace pas le PDF.

MEL officiel · 30-09 (page 354)