Side-by-side
Aircraft Curtains & Literature-Pocket Sewing vs ZP210 Economy Seat
Spec comparison for two products on Aviation Souk. Both compete in Aircraft Interior Fit-Out.
Aircraft Interior Fit-Out
Aircraft Curtains & Literature-Pocket Sewing
by Lantal Textiles AG
Ready-to-install aircraft curtains and literature pockets in certified wool and polyamide mesh, sewn and pleated by Lantal under EASA Part 21G design organisation approval.
Aircraft Interior Fit-Out
ZP210 Economy Seat
by ZIM Aircraft Seating GmbH
A minimalist slim-line economy seat engineered to maximise perceived space without sacrificing structural integrity or passenger comfort.
| Cost of ownership | Aircraft Curtains & Literature-Pocket Sewing | ZP210 Economy Seat |
|---|---|---|
| Price tier | — | — |
| Lead time (weeks) | ?–? | ?–? |
| Delivery | — | — |
| Install | — | — |
| GCC airports deployed | 0 | 0 |
| Certifications | 0 | 0 |
Specs
Technical specifications.
| Spec | Aircraft Curtains & Literature-Pocket Sewing | ZP210 Economy Seat |
|---|---|---|
| Flammability standard | FAR/CS 25.853 (permanent, not topical treatment) | — |
| Smoke and toxicity compliance | ABD 0031 (Airbus) and BSS 7238 (Boeing) | — |
| Literature pocket fire standard | UN-ECE-R118 Appendix 7 & 8 | — |
| Design organisation approval | EASA Part 21 Subpart G | — |
| Airworthiness release document | EASA Form One issued per delivery | — |
| Curtain construction options | Wool, polyamide mesh, sound-absorbing wool | — |
| Pleating options | Steam-pleated or sewn-pleated | — |
| Literature pocket supply | Ex-warehouse stock for short-lead replenishment | — |
| Seat structure | — | Crystal Flex fixed shell |
| Standard recline | — | Precline (fixed default position) |
| Optional recline | — | Up to 4 inches |
| Tray table | — | Fixed single-sheet or sliding (optional) |
| IFE provision | — | Optional (power port; no standard monitor) |
| PRM accessibility | — | Aisle-side armrest standard |
| Power options | — | USB (optional) |
| Life jacket stowage | — | Secured pocket (standard) |
| Design certification basis | — | CS-25 / FAR-25 (EASA Part-21J, TSO C39c, TSO C127a) |
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