BoredAviator
MEL 52-05
⚠ RAPPEL HOT — RESTRICTION MEL
ΔP MAX 6.0 / 3.4 PSI · PLAFOND 27 000 / 17 000 FT
Selon le relief — cabin < 8 000 ft.
Qu’est-ce que c’est
Item MEL « Left Main Cabin Door Pressure Stop Fittings » (ATA 52-05) du système portes 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 52-05 — Left Main Cabin Door Pressure Stop Fittings.
Catégorie(s) : B.
Rappel délais : B — 3 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.

52-05 — Left Main Cabin Door Pressure Stop Fittings
CAT — · installé — · requis dispatch —
52-05-01 — Aft Airstair Door NOTE: This item provides dispatch relief for and Forward Entry only the forward main entry door and Door aft main entry door on the left side of
CAT — · installé — · requis dispatch —
the airplane. A door pressure stop consists of two mating stop fittings, one being attached to the door and the other attached to the fuselage. Either or both stop fittings may be broken or missing at a single door pressure stop location.
52-05-01B
CAT B · installé — · requis dispatch —
(M#)(O) One per door may be broken or missing provided: a) There are no visible defects on other fittings for associated door, b) Pressure differential does not exceed 6.0 psi, c) Digital cabin pressure control system AUTO or ALTN control mode operates normally, and d) Alternate procedures are established and used.
52-05-02 — Aft Door without NOTE: This item provides dispatch relief for Airstairs only the aft main entry door on the
CAT — · installé — · requis dispatch —
left side of the airplane. A door pressure stop consists of two mating stop fittings, one being attached to the door and the other attached to the fuselage. Either or both stop fittings may be broken or missing at a single door pressure stop location.
52-05-02B
CAT B · installé — · requis dispatch —
(M#)(O) One per door may be broken or missing provided: a) There are no visible defects on other fittings for associated door, b) Pressure differential does not exceed 3.4 psi, c) Digital cabin pressure control system AUTO or ALTN control mode operates normally, and d) Alternate procedures are established and used.
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. 5 condition(s) de relief extraite(s) du tableau officiel (installé / requis / remarques). Une procédure (O) opérations s’applique — voir ci-dessous (texte MEL anglais). 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 on Pressurization Control Panel.

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

Print the following information in the journey log sheet. FORWARD ENTRY DOOR STOP FITTING BROKEN OR MISSING - DO NOT EXCEED 6.0 PSI CABIN DIFFERENTIAL or AFT DOOR WITHOUT AIRSTAIRS DOOR STOP FITTING BROKEN OR MISSING - DO NOT EXCEED 3.4 PSI CABIN DIFFERENTIAL

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

(O) OPERATIONS PROCEDURES — texte MEL :

52-05-01B Forward Entry Door NOTE: Do not exceed the maximum pressure differential of 6.0 psi. Limit flight altitude to 27,000 feet or lower to maintain a cabin altitude of less than 8,000 feet. 1. Select a landing altitude of 8,000 ft. MSL on the cabin pressure control panel. Cabin altitude will ascend to slightly less than 8,000 ft. during climb to cruise altitude. NOTE: Actual landing airport altitude may be selected if flight altitude is limited to 13,000 feet. 2. Monitor differential pressure indicator during climb to ensure maximum pressure differential of 6.0 psi is not exceeded. 3. Select actual landing airport altitude after initiating descent. If required to hold during descent, it may be necessary to increase the landing altitude in accordance with the Differential Pressure Schedule below. 4. Lower cabin altitudes may be obtained by appropriate selection of flight altitude and cabin/landing altitude in accordance with the Differential Pressure Schedule below. Continued… (O) OPERATIONS PROCEDURES (continued) 52-05-02B NOTE: Do not exceed the maximum pressure differential of 3.4 psi. Limit flight altitude to 17,000 feet or lower to maintain a cabin altitude of less than 8,000 feet. 1. Select a landing altitude of 8,000 ft. MSL on the cabin pressure control panel. Cabin altitude will ascend to slightly less than 8,000 ft. during climb to cruise altitude. NOTE: Actual landing airport altitude may be selected if flight altitude is limited to 7,000 feet. 2. Monitor differential pressure indicator during climb to ensure maximum pressure differential of 3.4 psi is not exceeded. 3. Select actual landing airport altitude after initiating descent. If required to hold during descent, it may be necessary to increase the landing altitude in accordance with the Differential Pressure Schedule below. 4. Lower cabin altitudes may be obtained by appropriate selection of flight altitude and cabin/landing altitude in accordance with the Differential Pressure Schedule below.

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

None required.

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

52-05-01B Forward Entry Door and 52-05-02B Aft Door: Visually inspect remaining fittings for possible defects on affected door(s), body frames and sills (if installed) (AMM 52-00-00/901).
Restrictions / notes (extrait MEL)
FORWARD ENTRY DOOR STOP FITTING BROKEN OR MISSING - DO NOT EXCEED 6.0 PSI
CABIN DIFFERENTIAL
AFT DOOR WITHOUT AIRSTAIRS DOOR STOP FITTING BROKEN OR MISSING - DO NOT
EXCEED 3.4 PSI CABIN DIFFERENTIAL
(M#)(O) One per door may be broken or missing provided: a) There are no visible defects on other fittings for associated door, b) Pressure differential does not exceed 6.0 psi, c) Digital cabin pressure control system AUTO or ALTN control mode operates normally, and d) Alternate procedures are established and used.
(M#)(O) One per door may be broken or missing provided: a) There are no visible defects on other fittings for associated door, b) Pressure differential does not exceed 3.4 psi, c) Digital cabin pressure control system AUTO or ALTN control mode operates normally, and d) Alternate procedures are established and used.
NOTE: Do not exceed the maximum pressure differential of 6.0 psi. Limit flight altitude to 27,000
NOTE: Do not exceed the maximum pressure differential of 3.4 psi. Limit flight altitude to 17,000
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 01 — Airplane General (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 · 52-05 (page 544)